What follows is the raw text from a RareAviation.com document available for download. This text can be helpful if you would like to confirm the document contains specific information you are interested in. Title: Aero Commander Model 112 Illustrated Parts Manual Link: https://rareaviation.com/product/aero-commander-model-112-illustrated-parts-manual --- RAW UNFORMATTED TEXT BELOW --- MODEL 112 Illustrated Parts Catalog SERIAL NO. 1 THRU 125 P/N M112001-4 MAY 1972 CHANGED JANUARY 1978 * Rockwell International General Aviation Division 5001 North Rockwell Avenue Bethany, Oklahoma 73008 * Rockwell International General Aviation Division Introduction Aero Commander Model 112 ILLUSTRATED PARTS CATALOG This Parts Catalog is intended as a positive means of identification of all replacement parts for the "Model 112". LINDER NO CIRCUMSTANCES SHOULD THIS CATALOG BE USED FOR MAINTE- NANCE OR REPAIR PURPOSES. This Parts Catalog is broken down into eleven major sections, and each section is divided into sub- groups. Each division will contain an illustration and a parts listing. These illustrations and parts listings will completely cover all replacement parts for the "Model 112". The following is an explanation of the parts listing. 1. The "Fig. and Index Number" column indicates the illustration figure number and part index number. See example. The 9 is the figure number and will appear only at the top of each new parts listing. The -1, -2, -3, etc., are index numbers. 2. The "Part Number" column contains the identifying part number. 3. The "Code" column indicates special uses of a part. An explanation of each letter code used per page appears at the bottom of each parts listing. 4. The "Nomenclature" column indicates the part name or description. 5. The "No. Req. " column represents the total quantity of parts used per aircraft per figure. 6. The indentures in the Nomenclature column indicate assemblies, components, and individual parts. See example a. No indenture indicates assemblies. If the aileron assembly -were ordered, it would include the six items listed under it. b. If the spar assembly were ordered, it would include the spar, doubler, and hinge. c. If you want only a hinge or doubler, order only that item. 7. The "Serial Number Affected" column gives parts usage by airplane serial number. FIG. & INDEX NO. PART NUMBER CODE t, A A MELE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 9-1 42003-1 Aileron Assembly - Left i 42003-2 Aileron Assembly - Right i -2 42245-1 Spar Assembly - Left i 42245-2 Spar Assembly - Right i -3 42246-1 Doubler - Aileron Hinge i 42246-2 Doubler - Aileron Hinge i -4 42247-1 Spar i 42247-2 Spar i -5 42248-1 Hinge i 42248-2 Hinge i -6 42249-1 Balance Weight Ass'y. - Left i 42249-2 Balance Weight Ass'y. - Right i ISSUED: May 1972 Model 112 From RareAviation.com e Rockwell International General Aviation Division e Hardware Hardware such as nuts, bolts, screws, etc., that are available as commercial items usually are not supplied by Aero Commander. The parts listing will contain those items of attaching hardware re- quired for main assemblies and installations. Part numbers, vendor numbers, etc., for these parts will follow the part name in the nomenclature column. Optional Equipment Optional equipment items will be listed in their proper sections and in the proper sequence with other parts listings. Optional equipment kits, custom kits, repair kits, and special tools will be listed under the miscellaneous section. Parts Identification When trying to identify parts, use the following steps as a guide. 1. Refer to Figure 1 (complete airplane) on page 1 and select the appropriate section. 2. Turn to Table of Contents on page vii and find the section. Note that each section is divided into various subgroups. a. Select the figure that you think would most likely contain the part you wish to identify and note page specified. 3. Find the proper illustration and select the index number for your part. If you are unable to lo- cate your part in this illustration, refer to other illustrations within the same section. 4. In the parts listing, go to the correct figure number and index number for a complete description of your part. Ordering Parts When ordering parts, the following information must be included. This will assure that you receive the correct parts in the shortest time. 1. Correct part numbers 2. Complete part description 3. Model number 4. Factory serial number 5. Quantity 6. Shipping instructions 7. Where to ship Note: When no shipping instructions are given, we reserve the right to ship the most suitable way. General Information 1. Shortages: All orders are checked before leaving our Shipping Department. A packing slip is enclosed with each shipment and claims for error and/or shortages must be made within five days after receipt. ISSUED: May 1972 ii Model 112 9 Rockwell International General Aviation Division 2. Returned Goods: No material should be returned to us without first securing our written permission, and all shipments must be made prepaid. Note: Any shipment not sent prepaid will be refused. If material is returned without written approval, material will be held at owner's risk for a period of thirty (30) days and will then be disposed of as we see fit. 3. Transportation Liabilities: Aero Commander, Inc. cannot be held liable for damages to parts in transit from the factory. If a shipment is received in a damaged condition, have the delivery man or the transportation company make a notation of the dan age on the bill of lading and file your claim with the carrier. In case of concealed damage, call the carrier and have their claim agent inspect the damage. Do not remove the part from the shipping container or attempt to repair the damage. WHEN ORDERING PARTS FOR YOUR "AERO COMMANDER MODEL 112", PLACE YOUR ORDER WITH THE DEALER OR DISTRIBUTOR FOR YOUR TERRITORY, SINCE PARTS ARE AVAILABLE ONLY THROUGH OUR DISTRIBUTOR ORGANIZATION. Revisions This Parts Catalog is a current listing of parts for the Aero Commander Model 112. Changes and additions will occur. These changes will be forwarded to you for insertion in their proper places. It is important that these changes and/or additions be inserted upon receipt, so that there will be maximum utility of this catalog. When revisions to this catalog are made, they will supersede all previous revisions. All revisions will be complete page replacements and/or additions and should be inserted as follows: 1. Replace obsolete pages with revised pages of the same page number. 2. Insert pages with page number followed by small arable letter in direct sequence with page of a common number. 3. Insert pages with page number followed by capital arable letter in direct sequence with page of a common number, but after any page with a small arable letter. The revision date appears in the lower left hand corner of each page. ISSUED: May 1972 iii Model 112 From RareAviation.com e Rockwell International General Aviation Division Current Revision List Page Issue *Title........................January 1978 i thru iii ....................May 1972 *iv ..........................January 1978 v thru viii...................May 1972 1 thru 54....................May 1972 55..........................October 1975 56 thru 84...................May 1972 *85 .......................... January 1978 86 thru 105..................May 1972 *106 thru 110.................January 1978 *110A thru HOD (Added)......January 1978 *111 thru 112.................January 1978 *112A thru 1128 (Added).......January 1978 *113 thru 114.................January 1978 *114A thru 1148 (Added).......January 1978 *115 thru 118.................January 1978 119 thru 125.................May 1972 *126.........................January 1978 *126A thru 1268 (Added).......January 1978 *127 thru 128.................January 1978 129 thru 169.................May 1972 *170.........................January 1978 *170A thru 170D (Added)......January 1978 *171 thru 175.................January 1978 176 thru 214.................May 1872 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES *The asterisk indicates pages changed, added or deleted by the current change. Changed January 1978 iv Model 112 Rockwell International General Aviation Division The "FINISH AND TRIM" plate is located on the lower left hand corner of the closeout-bulkhead in the aft cabin. The plate indicates the model year, interior scheme and the exterior paint combination. The design layout for the exterior paint combination consists of: A. Primary, the major portion of all aircraft. B. Secondary. C. Trim Stripe, for the Super Sport Design only. The following illustration is an example showing the sequence and definition of each code symbol on the "FINISH AND TRIM" plate. Finish and Trim Number (1 02C 010600) EXTERIOR COLOR COMBINATION CODE YEAR CODE---------1 = Model Year INTERIOR COLOR CODE---------02C- Indian Cold, Interior Scheme "til - Spinnaker White, Primary Exterior Color 06 - Aztec Gold, Secondary Stripe HO - Accent Trim Stripe, For Super Sport Design Only ISSUED: May 1972 Model 112 From RareAviation.com e Rockwell International General Aviation Division YEAR CODE INTERIOR COLOR CODE STANDARD SUPER SPORT CODE YEAR CODE COLOR CODE COLOR 1 1971 02A Sea Blue 22A Sea Foam Blue 2 1972 02 B Harvest Red 22B Sunset Red 3 1973 02C Indian Gold 22C Inca Gold 4 1974 02 D Wintergreen 22D Spruce Green SPORT CODE COLOR 12A Sea Foam Blue 12B Sunset Red 12C Inca Gold 12D Spruce Green EXTERIOR PAINT COLOR INDEX AND COLOR CODE DUPONT COLOR MFG. & ALBANY COLOR REF. NO. NAME YEAR C/N CODE 4996 L Spinnaker White Chrg. 70 46545 01 5254 L Amber Sherwood Chrg. 71 46538 02 5327 L Molsanne Blue Chev. 71 46539 03 4602 LH Compilation Orange Merc. 71 46543 04 5292 LH War Bonnet Yellow Corv. 71 46540 05 5130 LH Aztec Gold Chrg. 70 46544 06 5169 LH Moroccon Brown Am. Mo. 70 46541 07 5317 L Dark Green-Black Line. 71 46542 08 ISSUED: May 1972 vi Model 112 e Rockwell International General Aviation Division Table of Contents Figure Numbei Figure r Title Page Fig. List Figure Numbe: Figure r Title Page Fig. List 1 Complete Airplane 1 34 Engine Instruments Installation 114 115 35 Induction Air System Installation 116 117 SECTION I 36 Baffle Installation 120 121 WING GROUP 37 Engine Exhaust System Installation 124 125 38 Cowling Installation 126 127 2 Wing Skins 4 5 39 Nose Gear Door Installation 128 129 3 Wing Installation 8 9 4 Wing Assembly- 12 13 SECTION VI 5 Flap and Aileron Assembly 18 19 CONTROL SYSTEMS GROUP SECTION II 40 Yoke Assembly and FUSELAGE GROUP Installation 132 133 41 Rudder Pedal Installation 136 137 6 Complete Fuselage Assembly 22 23 42 Aileron Controls Installation 140 141 7 Forward Cabin Assembly 24 25 43 Rudder Controls Installation 144 145 8 Aft Cabin Assembly 30 31 44 Rudder Trim and Nose 9 Aft Fuselage Assembly 34 35 Wheel Steering Installation 146 147 10 Firewall Assembly 38 39 45 Elevator Controls Installation 150 151 11 Console Tunnel Assembly 40 41 46 Elevator Trim Installation 154 155 12 Baggage Door and Cabin Door 42 43 47 Flap Controls Installation 158 159 13 Windows and Windshield Installation 46 47 14 Heating and Defrosting System SECTION VII Installation 48 49 HYDRAULIC SYSTEMS GROUP 15 Fresh Air Vent Installation 50 51 16 Overhead Vent System Installation 52 53 48 Hydraulic System 163 17 Instrument Panel Installation 54 55 Installation 162 18 Vacuum System Installation 58 59 49 Brake System Installation 166 167 19 Pitot System Installation 60 61 SECTION VIII 20 Interior Installation 62 63 21 Crew Seat Assembly 68 69 LANDING GEAR GROUP 22 Aft Divan Assembly 72 73 50 Nose Gear Installation 170 171 SECTION III 51 Nose Gear Assembly 172 173 EMPENNAGE GROUP 52 Main Landing Gear Installation 176 177 23 Tail Surfaces Installation 78 79 53 Strut Assembly Main 24 Upper Fin Assembly 82 83 Landing Gear 180 181 25 Lower Fin Assembly 84 85 54 Brake and Wheel Assembly 184 185 26 Rudder Assembly 86 87 SECTION IX 27 Horizontal Stabilizer Assembly 88 89 28 Elevator and Trim Tab Assembly 92 93 ELECTRICAL GROUP SECTION IV 55 Electrical Equipment FUEL SYSTEM GROUP 56 Firewall Instrument Panel Electrical 188 189 29 Fuel System Installation 96 97 Installation 190 191 30 Primer and Vent Line System 57 Battery and External Power Installation 100 101 Unit Installation 194 195 31 Gascolator and Fuel Pump 58 Night Lighting Installation 198 199 Installation 102 103 SECTION X SECTION V POWER PLANT GROUP ELECTRONICS GROUP 59 Radio System Installation 202 203 32 Power Plant Installation 106 107 60 Antenna System Installation 204 205 33 Engine and Cowl Flap Controls Installation 110 111 ISSUED: May 1972 vii Model 112 From RareAviation.com * Rockwell International General Aviation Division Table of Contents Figure Figure Page Figure Figure Number Title Fig. List Number Title SECTION XI MISCELLANEOUS 61 Interior and Exterior Markings 210 211 62 Interior and Exterior Placards 212 213 Page Fig. List ISSUED: May 1972 viii Model 112 Rockwell International General Aviation Division Miscellaneous Section XI Electrical Group Section IX Empennage Group Section III Fuel System Group Section IV Electronics Group Section X Control Systems Group Section VI Wing Group Section I Fuselage Group Section II Landing Gear Group Section VIII Hydraulic Systems Group Section VII Power Plant Group Section V ISSUED: May 1972 Figure 1. Complete Airplane 1 Model 112 From RareAviation.com Notes 2 SECTION WING GROUP From RareAviation.com Section I WING GROUP 3 Rockwell International General Aviation Division Figure 2. Wing Skins 4 ISSUED: May 1972 Model 112 From RareAviation.com e Rockwell International General Aviation Division WING SKINS SECTION I Wing Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RECTO SERIAL NO'S AFFECTED 2-1 42215-1 SKIN - Outboard, Leading Edge, L.H. i One & Up 42215-2 SKIN - Outboard, Leading Edge, R.H. i 42216-1 SKIN ASSEMBLY - Fuel Tank, L.H. i 42216-2 SKIN ASSEMBLY - Fuel Tank, R.H. i -2 42216-4 SKIN - Fuel Tank, L.H. i 42216-5 SKIN - Fuel Tank, R.H. i -3 42286-3 DOUBLER - Access Panel 6 -4 59490 NUT (22NKA1-02, Esna) 96 -5 42284-3 ACCESS PANEL 6 -6 48516-1 DOUBLER - Fuel Filler 2 -7 61520 GROMMET - Fuel Filler (2805, Atlantic Rubber Co.) 2 48520-1 FUEL FLAP ASSEMBLY 2 -8 48515-1 BRACKET - Fuel Flap, Sub Assembly 2 -9 48517-1 SPRING 2 -10 48519-1 BRACKET - Fuel Flap 2 -11 48521-1 PIN - Fuel Flap 2 -12 68236 SPACER (NAS 43DD3-29) 4 -13 59462 SPEED NUT (C637-010, Tinnerman) 4 -14 59467 CLIP NUT (C1731-1032, Tinnerman) 4 -15 63921 VALVE (1000B-2A, Beta-Valve) 2 -16 59700 SCREW (AN520-C10-4) 4 42217-1 SKIN ASSEMBLY - Leading Edge, Inboard Center Wing, L.H. 1 42217-2 SKIN ASSEMBLY - Leading Edge, Inboard Center Wing, R.H. 1 -17 42217-3 SKIN - Leading Edge, Inboard Center Wing, L.H. 1 42217-4 SKIN - Leading Edge, Inboard Center Wing, R.H. 1 -18 42299-1 DOUBLER - Air Intake 2 -19 42294-1 FILTER - Air Intake 2 42218-1 SKIN ASSEMBLY - Wing Walkway, L.H. 1 42218-2 SKIN ASSEMBLY - Wing Walkway, R.H. 1 -20 42218-3 SKIN - Wing Walkway, L.H. 1 42218-4 SKIN - Wing Walkway, R.H. 1 -21 42220-1 SKIN - Wingwalk, Beaded, L.H. 1 42220-2 SKIN - Wingwalk, Beaded, R.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 5 Model 112 e Rockwell International General Aviation Division WING SKINS SECTION I Wing Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 42222-1 SKIN ASSEMBLY - Aft, Bottom Outboard, L.H. i One & Up 42222-2 SKIN ASSEMBLY - Aft, Bottom Outboard, R. H. i 2-22 42222-3 SKIN - Aft, Bottom Outboard, L.H. i 42222-4 SKIN - Aft, Bottom Outboard, R.H. i -23 42241-4 DOUBLER - Aileron Access 2 -24 59485 CLIP NUT (C8104-832, Tinnerman) 16 -25 42309-1 DOOR - Access, Pitot Head 1 -26 42314-1 DOOR - Access, Aileron Access 1 -27 59667 SCREW (AN515DD8-4) 16 -28 42223-1 SKIN - Aft, Bottom Inboard, L.H. 1 42223-2 SKIN - Aft, Bottom Inboard, R.H. 1 -29 42224-1 SKIN - Aft, Top Outboard, L.H. 1 42224-2 SKIN - Aft, Top Outboard, R.H. 1 -30 42225-1 SKIN - Aft, Top Inboard, L.H. 1 42225-2 SKIN - Aft, Top Inboard, R.H. 1 -31 42250-1 SKIN - Wheel Well, L.H. 1 42250-2 SKIN - Wheel Well, R.H. 1 -32 42260-1 STRIP - Flap Shroud, Trailing Edge, L.H. 1 42260-2 STRIP - Flap Shroud, Trailing Edge, R.H. 1 -33 56842 SCREW (AN526-1032-R6) 96 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 6 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1472 7 Model 112 Rockwell International General Aviation Division Figure 3. Wing Installation 8 ISSUED: May 1972 Model 112 From RareAviation.com e Rockwell International General Aviation Division WING INSTALLATION SECTION I Wing Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. READ SERIAL NOS AFFECTED 40001-1 WING INSTALLATION One & Up 40002-1 WING COMPLETE, L.H. i 40002-2 WING COMPLETE, R.H. i 3-1 42000-1 WING ASSEMBLY, L.H. i 42000-2 WING ASSEMBLY, R.H. i -2 42003-1 AILERON ASSEMBLY, L. H. i 42003-2 AILERON ASSEMBLY, R.H. i -3 42004-1 FLAP ASSEMBLY, L.H. i 42004-2 FLAP ASSEMBLY, R.H. i -4 42242-1 WING TIP ASSEMBLY, L.H. i 42242-2 WING TIP ASSEMBLY, R.H. i -5 42242-3 LENS, L.H. i 42242-4 LENS, R.H. i -6 59614 SCREW (AN507C832-6) 22 -7 BOLT (AN24-16) 6 -8 58769 WASHER (AN960PD416L) 12 -9 68253 SPACER (NAS43DD4-6) 12 -10 NUT (AN310-4) 6 -11 COTTER PIN (MS20665-132) 6 -12 SCREW (AN525-1032-9) 6 -13 SCREW (AN525-1032-10) 6 -14 WASHER (AN960-10L) 12 -15 NUT (MS20365-1032) 12 -16 SCREW (AN507-832R7) 34 -17 WASHER (A3135-017-1) 34 -18 40126-1 SEAL 2 -19 42292-1 SPLICE - Spar Cap, Upper 1 -20 42292-3 SPLICE - Spar Cap, Lower 1 -21 42295-1 TRUSS ASSEMBLY - B.L. 0.0 1 -22 42301-1 FITTING - Spar, B.L. 0.0 1 -23 50851 BOLT (AN4-5A) 2 -24 BOLT (AN174-12A) 8 -25 54205 BOLT (AN174-14A) 2 -26 54221 BOLT (AN175-6A) 2 -27 54241 BOLT (AN176-10A) 2 -28 54242 BOLT(AN176-35A) 2 -29 68528 BOLT (NAS 1104-4) 4 -30 68527 BOLT (NAS1104-6) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 9 Model 112 WING INSTALLATION * Rockwell International General Aviation Division SECTION I Wing Group FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER CODE NOMENCLATURE REDO AFFECTED 3-31 BOLT (NAS 1106-12) 6 One & Up -32 68525 BOLT (NAS 1106-13) 16 -33 BOLT (NAS 1106-14) 10 -34 58760 WASHER (AN960-416) 20 -35 58770 WASHER (AN960-416L) 4 -36 58780 WASHER (AN960-516) 2 -37 58790 WASHER (AN960-616) 34 -38 58794 WASHER (AN960-616L) 4 -39 NUT (MS20364-428) 4 -40 NUT (MS20364-624) 32 -41 A2172 NUT (MS20365-428) 16 -42 NUT (MS20365-524) 2 -43 NUT (MS20365-624) 4 -44 SPACER (NAS76A-4-21P) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 10 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 11 Model 112 * Rockwell International General Aviation Division Figure 4. Wing Assembly ISSUED: May 1972 12 Model 112 From RareAviation.com Rockwell International General Aviation Division WING ASSEMBLY SECTION I Wing Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 42000-1 WING ASSEMBLY, L.H. i One & Up 42000-2 WING ASSEMBLY, R.H. i 42001-1 TANK & LEADING EDGE ASSEMBLY, L.H. i 42001-2 TANK & LEADING EDGE ASSEMBLY, R.H. i 4-1 40106-1 STRINGER 2 -2 40106-2 STRINGER 2 -3 40127-1 STRINGER 4 -4 42201-1 RIB - Tip, Sta. 189.00, L.H. 1 42201-2 RIB - Tip, Sta. 189.00, R.H. 1 -5 42202-1 RIB - Sta. 165.20, L.H. 1 42202-2 RIB - Sta. 165.20, R.H. 1 42203-1 RIB ASSEMBLY - Tank, Sta. 142.40, L.H. 1 42203-2 RIB ASSEMBLY - Tank, Sta. 142.40, R.H. 1 -6 42203-3 RIB - Tank, Sta. 142.40, L.H. 1 42203-4 RIB - Tank, Sta. 142.40, R.H. 1 -7 42204-1 RIB - Tank, Sta. 119.50, L.H. 1 42204-2 RIB - Tank, Sta. 119. 50, R. H. 1 -8 42333-1 FLANGE - Fuel Tank, Outboard 4 -9 42205-1 RIB - Tank, Sta. 101.10, L.H. 1 42205-2 RIB - Tank, Sta. 101.10, R.H. 1 42206-1 RIB ASSEMBLY - Tank, Sta. 82.50, L.H. 1 42206-2 RIB ASSEMBLY - Tank, Sta. 82.50, R.H. 1 -10 42206-3 RIB - Tank, Sta. 82.50, L.H. 1 42206-4 RIB - Tank, Sta. 82.50, R.H. 1 -11 42325-1 FLANGE - Fuel Tank Outlet 2 -12 42333-1 FLANGE - Fuel Tank, Outboard 4 -13 42228-1 BAFFLE - Center, L.H. 1 42228-2 BAFFLE - Center, R.H. 1 -14 42229-1 BAFFLE - Inboard, L.H. 1 42229-2 BAFFLE - Inboard, R.H. 1 -15 42227-1 BAFFLE - Outboard, L.H. 1 42227-2 BAFFLE - Outboard, R.H. 1 -16 42002-1 SPAR ASSEMBLY - Main, Wing, L.H. 1 42002-2 SPAR ASSEMBLY - Main, Wing, R.H. 1 -17 42005-1 SPAR ASSEMBLY - Forward Auxiliary, Wing, L.H. 1 42005-2 SPAR ASSEMBLY - Forward Auxiliary, Wing, R.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 13 Model 112 Rockwell International General Aviation Division WING ASSEMBLY SECTION I Wing Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 4-18 42207-1 RIB - Leading Edge, Sta. 65.30, L.H. i One & Up 42207-2 RIB - Leading Edge, Sta. 65.30, R. H. i -19 42208-1 RIB - Leading Edge, Sta. 47.30, L.H. i 42208-2 RIB - Leading Edge, Sta. 47.30, R.H. i 42209-1 RIB ASSEMBLY - Center, Sta. 47.30, L.H. i 42209-2 RIB ASSEMBLY - Center, Sta. 47.30, R.H. i -20 42209-3 RIB - Center, Sta. 47.30, L.H. i 42209-4 RIB - Center, Sta. 47.30, R.H. i -21 42234-1 DOUBLER 2 -22 48279-4 BRACKET ASSEMBLY - Main Gear Down Position, L.H. 1 48279-5 BRACKET ASSEMBLY - Main Gear Down Position, R.H. 1 -23 42210-1 RIB - Root, Forward, Canted, L.H. 1 42210-2 RIB - Root, Forward, Canted, R.H. 1 -24 42211-1 RIB - Aft, Sta. 121.20, L.H. 1 42211-2 RIB - Aft, Sta. 121.20, R.H. 1 -25 42212-1 RIB - Aft, Sta. 47.30, L.H. 1 42212-2 RIB - Aft, Sta. 47.30, R.H. 1 -26 42213-1 RIB - Aft, Sta. 26.50, L.H. 1 42213-2 RIB - Aft, Sta. 26.50, R.H. 1 -27 42214-1 RIB - Aft, Sta. 36.90, L.H. 1 42214-2 RIB - Aft, Sta. 36.90, R.H. 1 -28 42230-1 RIB - Cove, Flap, L.H. 1 42230-2 RIB - Cove, Flap, R.H. 1 -29 42230-3 RIB - Cove, Flap, L.H. 1 42230-4 RIB - Cove, Flap, R.H. 1 -30 42231-1 SPAR - Aft, Inboard, L.H. 1 42231-2 SPAR - Aft, Inboard, R.H. 1 -31 42232-1 SPAR - Aft, Outboard, L.H. 1 42232-2 SPAR - Aft, Outboard, R.H. 1 -32 42235-1 CLOSE OUT - Wheel Well, L.H. 1 42235-2 CLOSE OUT - Wheel Well, R.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 14 Model 112 From RareAviation.com * Rockwell International General Aviation Division WING ASSEMBLY SECTION I Wing Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 4-33 42259-1 BRACKET - Sta. 121.20, L.H. i One & Up 42259-2 BRACKET - Sta. 121.20, R.H. i -34 42270-1 FITTING - Aft Spar, L.H. i 42270-2 FITTING - Aft Spar, R.H. i 42278-1 FLAP HINGE ASSEMBLY 6 -35 42263-1 ARM - Flap Hinge 6 -36 60167 BEARING (LHB-4, Heim Unibal) 6 -37 42290-1 DOUBLER - Upper, Aileron Bellcrank, L.H. 1 42290-2 DOUBLER - Upper, Aileron Bellcrank, R.H. 1 -38 42291-1 DOUBLER - Lower, Aileron Bellcrank, L.H. 1 42291-2 DOUBLER - Lower, Aileron Bellcrank, R.H. 1 -39 42279-1 FAIRING - Flap Hinge 6 -40 42328-1 SUPPORT - Wing Hinge 4 -41 42317-1 SUPPORT - Wing Walk 2 -42 42304-1 RIB - Cove, Flap, Sta. 47.30, L.H. 1 42304-2 RIB - Cove, Flap, Sta. 47.30, R.H. 1 -43 42311-1 RIB - Cove, Flap, Sta. 26.50, L.H. 1 42311-2 RIB - Cove, Flap, Sta. 26.50, R.H. 1 -44 42321-1 STRAP - Cove Rib, Sta. 26.50, L.H. 1 42321-2 STRAP - Cove Rib, Sta. 26.50, R.H. 1 -45 42322-1 STRAP - Cove Rib, Sta. 47.30, L.H. 1 42322-2 STRAP - Cove Rib, Sta. 47.30, R.H. 1 -46 42271-1 FITTING - Forward Auxiliary Spar, L.H. 1 42271-2 FITTING - Forward Auxiliary Spar, R.H. 1 -47 42282-1 CLIP - Forward Auxiliary Spar, L.H. 2 42282-2 CLIP - Forward Auxiliary Spar, R.H. 2 -48 42323-1 SUPPORT - Skin, Sta. 66.00, L.H. 1 42323-2 SUPPORT - Skin, Sta. 66.00, R.H. 1 -49 40122-1 PLACARD 2 -50 40108-1 JACK PAD 2 -51 42293-1 BRACKET ASSEMBLY - Aileron Stop, L.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 15 Model 112 e Rockwell International General Aviation Division WING ASSEMBLY SECTION I Wing Group FIG. S INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 4-51 -55 -52 -54 -55 -56 -57 -58 -59 -60 42293-2 42335-1 65541 54548 48278-1 48278-2 56850 59521 40118-1 BRACKET ASSEMBLY - Aileron Stop, R.H. STOP WASHER (AN 960-416 NUTPLATE (MS21047-L3) NUT (AN315-3) BRACKET - Main Gear Up Position, L.H. BRACKET - Main Gear Up Position, R.H. SCREW (AN526-1032-RIO) CLIP NUT (RM 52LHA-4972-10-02, Esna) TIE DOWN RING NUT PLATE (22N17A-058, Elastic Stop Nut) i 2 2 2 2 1 1 8 8 2 2 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 16 Model 112 From RareAviation.com Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 17 Model 112 NOTICE OF MISSING INFORMATION Issue\Section SEC* ~ group Page Number(s) FIG 5 PAGE 18 The above has been ordered from the source. As soon as it is received, ATP will reissue this fiche to include the above. From RareAviation.com * Rockwell International General Aviation Division SECTION I Wing Group FLAP AND AILERON ASSEMBLY FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REOD SERIAL NO'S AFFECTED 42004-1 FLAP ASSEMBLY, L.H. One & Up 42004-2 FLAP ASSEMBLY, R.H. 5-1 42253-1 SKIN - Flap, Leading Edge, L.H. i 42253-2 SKIN - Flap, Leading Edge, R.H. i -2 42254-1 SKIN - Flap, Upper Surface, L.H. i 42254-2 SKIN - Flap, Upper Surface, R.H. i -3 42255-1 SKIN - Flap, Lower Surface, L.H. i 42255-2 SKIN - Flap, Lower Surface, R.H. i -4 42262-1 SKIN - Flap Step, L.H. i 42262-2 SKIN - Flap Step, R.H. i -5 42283-1 SKIN - Flap, Inboard Beaded, L.H. i 42283-2 SKIN - Flap, Inboard Beaded, R.H. i -6 42256-1 RIB - Flap, Inboard Aft, L.H. 2 42256-2 RIB - Flap, Inboard Aft, R.H. 2 -7 42257-1 RIB - Flap, Outboard Aft, L.H. 1 42257-2 RIB - Flap, Outboard Aft, R.H. 1 -8 42258-1 RIB - Flap, Leading Edge, L.H. 3 42258-2 RIB - Flap, Leading Edge, R.H. 3 -9 42261-1 RIB - Flap, Leading Edge, L.H. 2 42261-2 RIB - Flap, Leading Edge, R.H. 2 -10 42252-1 SPAR - Flap 2 -11 42267-1 STIFFENER - Flap, T. E. 2 -12 42285-1 BRACKET - Flap Actuator, L.H. 1 42285-2 BRACKET - Flap Actuator, R.H. 1 -13 42233-1 BRACKET - Flap Hinge, L.H. 2 42233-2 BRACKET - Flap Hinge, R.H. 2 -14 42233-3 BRACKET - Flap Hinge, L.H. 1 42233-4 BRACKET - Flap Hinge, R.H. 1 42003-1 AILERON ASSEMBLY, L.H. 1 42003-2 AILERON ASSEMBLY, R.H. 1 -15 42245-1 SKIN - Aileron, L.H. 1 42245-2 SKIN - Aileron, R.H. 1 -16 42243-1 SPAR - Aileron, L.H. 1 42243-2 SPAR - Aileron, R.H. 1 -17 42246-3 RIB - Aileron, Root, L.H. 1 42246-4 RIB - Aileron, Root, R.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 19 Model 112 e Rockwell International General Aviation Division FLAP AND AILERON ASSEMBLY SECTION I Wing Group FIG. & INDEX NO. PARI NUMBER CODE NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 5-18 -19 -20 -21 -22 -23 -24 42247-1 42247-2 42249-3 42249-4 42251-1 42327-1 50026 58740 A2167 RIB - Aileron, Tip, L.H. RIB - Aileron, Tip, R.H. HORN - Aileron, L.H. HORN - Aileron, R.H. HINGE ASSEMBLY - Aileron DOUBLER - Aileron Hinge BOLT (AN3-5A) WASHER (AN960-10) NUT (MS20365-1032) i i i i 4 4 4 8 4 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 20 Model 112 From RareAviation.com SECTION FUSELAGE GROUP 21 Section II FUSELAGE GROUP From RareAviation.com Rockwell International General Aviation Division Figure 6. Complete Fuselage Assembly ISSUED: May 1972 22 Model 112 e Rockwell International General Aviation Division SECTION II Fuselage Group COMPLETE FUSELAGE ASSEMBLY FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 43000-1 FUSELAGE ASSEMBLY COMPLETE i One & Up 6-1 43001-1 FORWARD CABIN ASSEMBLY i -2 43002-1 AFT CABIN ASSEMBLY i -3 43003-1 AFT FUSELAGE ASSEMBLY i -4 43210-1 SKIN - Cabtop, Sta. 148-178 i -5 43211-1 SKIN - Cabtop, Sta. 123-148 i -6 43212-1 SKIN - Cabtop, Sta. 123, Forward i -7 43213-1 SKIN - Bottom, Sta. 123 i -8 43214-1 SKIN - R.H. Sta. 147-178 i -9 43215-1 SKIN - Bottom, L.H., Sta. 144-178 i 43215-2 SKIN - Bottom, R.H., Sta. 144-178 i -10 43215-3 SKIN - Bottom, Center, Sta. 144-178 i -11 43216-1 SKIN - Sta. 123-148, L.H. i 43216-2 SKIN - Sta. 123-148, R.H. i -12 43217-1 SKIN - Side, Sta. 84.25-123.75 i -13 43218-1 SKIN - Side, Sta. 62.38-85.00, L.H. i 43218-2 SKIN - Side, Sta. 62.38-85.00, R.H. i -14 43219-1 FLOOR - Sta. 62.50-123.90 i -15 43263-1 DOUBLER - Skin, Sta. 146 2 -16 43389-1 TUBE - Defroster Inlet 2 -17 43294-1 SKIN - Panel Top 1 -18 43305-1 PANEL - Removable, Sta. 123.90 1 -19 43353-1 SKIN - Windshield Post, L.H. 1 43353-2 SKIN - Windshield Post, R.H. 1 -20 43362-1 DORSAL - Fairing, Forward 1 -21 43365-1 DOUBLER - Dorsal Air Inlet 1 -22 43388-1 DUCT - Defroster, L.H. 1 43388-2 DUCT - Defroster, R.H. 1 -23 43399-1 DOUBLER - Skin Cutout, Sta. 119-130, L.H. 1 43399-2 DOUBLER - Skin Cutout, Sta. 119-130, R.H. 1 -24 43472-1 VENT - Cabin Exhaust 1 -25 43473-1 DOUBLER - Cabin Exhaust 1 -26 SCREW (AN507-10R7) 12 -27 65556 NUTPLATE (MS21059-08) 2 -28 68022 NUTPLATE (NAS1068-A08) 28 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 23 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 7. Forward Cabin Assembly ISSUED: May 1972 24 Model 112 * Rockwell International General Aviation Division FORWARD CABIN ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REQTD SERIAL NOS AFFECTED 43001-1 FORWARD CABIN ASSEMBLY i One & Up 7-1 43008-1 FIREWALL ASSEMBLY i 43226-1 FRAME ASSEMBLY - Sta. 85, L.H. i 43226-2 FRAME ASSEMBLY - Sta. 85, R.H. i -2 43226-3 FRAME - Sta. 85, L.H. i 43226-4 FRAME - Sta. 85, R.H. i -3 43286-1 PLATE - Front Spar Attachment, Sta. 85 2 -4 43227-1 BEAM - Door Threshold, L.H. 1 43227-2 BEAM - Door Threshold, R.H. 1 -5 43228-1 INTERCOSTAL - Side, W.L. 58, L.H. 1 43228-2 INTERCOSTAL - Side, W.L. 58, R.H. 1 -6 43232-1 CONSOLE TUNNEL ASSEMBLY 1 -7 43234-1 FITTING ASSEMBLY - Engine Mount Attachment 1 -8 43235-1 FITTING - Lower Mount Attachment 2 -9 43238-1 FITTING - Engine Mount Attachment, L.H. 1 43238-2 FITTING - Engine Mount Attachment, R.H. 1 -10 43243-1 POST - Windshield 1 -11 43244-1 FRAME - Windshield Post, L.H. 1 43244-2 FRAME - Windshield Post, R.H. 1 43245-1 STIFFENER ASSEMBLY - Cabtop, L.H. 1 43245-2 STIFFENER ASSEMBLY - Cabtop, R.H. 1 -12 43245-3 STIFFENER - Cabtop, L.H. 1 43245-4 STIFFENER - Cabtop, R.H. 1 -13 65536 NUTPLATE (MS21051-L08) 4 43249-1 TRACK ASSEMBLY - Seat 1 43249-2 TRACK ASSEMBLY - Seat 1 -14 43249-5 TRACK - Seat 1 43249-6 TRACK - Seat 1 -15 43366-1 BLOCK - Seat Stop 4 -16 CLEVIS PIN (MS20392-1C33) 2 -17 COTTER PIN (MS24665-149) 2 -18 43282-1 INTERCOSTAL - Cabtop 1 43285-1 FRAME ASSEMBLY - Sta. 85.90, L.H. 1 43285-2 FRAME ASSEMBLY - Sta. 85.90, R.H. 1 -19 43285-3 FRAME - Sta. 85.90, L.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 25 Model 112 From RareAviation.com * Rockwell International General Aviation Division SECTION II Fuselage Group FORWARD CABIN ASSEMBLY FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NOS AFFECTED 7-19 43285-4 FRAME - Sta. 85.90, R. H. i One & Up -20 43286-1 PLATE - Front Spar Attachment, Sta. 85 2 -21 43287-1 STIFFENER - Floor Board, Sta. 85 1 -22 43292-1 FRAME - Sta. 80.30, L.H. 1 43292-2 FRAME - Sta. 80.30, R.H. 1 43293-1 FRAME ASSEMBLY - Sta. 80.30 1 -23 43293-3 FRAME - Sta. 80.30 1 -24 NUTPLATE (MS21074-08K) 2 -25 43296-1 DUCT - Cabin Side Forward, L.H. 1 43296-2 DUCT - Cabin Side Forward, R.H. 1 -26 43297-1 TUBE - Cabin Duct 2 -27 43301-1 RETAINER - Seal, L.H. 1 43301-2 RETAINER - Seal, R.H. 1 -28 43302-1 FRAME - Sta. 97.60, L.H. 1 43302-2 FRAME - Sta. 97.60, R.H. 1 43303-1 SUPPORT ASSEMBLY - Rudder Bar Left Side 1 43327-1 SUPPORT ASSEMBLY - Rudder Bar Right Side 1 -29 43328-1 SUPPORT - Rudder Bar, Left Side 1 43329-1 SUPPORT - Rudder Bar, Right Side 1 -30 43330-1 SPACER - Rudder Bar Support 2 -31 60153 BEARING (FF-1213-1 Oilite) 2 -32 43309-1 FRAME - Sta. 107.44, L.H. 1 43309-2 FRAME - Sta. 107.44, R.H. 1 -33 43310-1 RETAINER - Windshield, Upper 1 -34 43311-1 FITTING ASSEMBLY - W.L. 58 2 -35 43314-1 SUPPORT - Instrument Panel 1 -36 43316-1 SUPPORT - Foot Rest 2 43325-1 WHEEL WELL ASSEMBLY 1 -37 43323-1 PANEL - Forward Wheel Well, L.H. 1 43323-2 PANEL - Forward Wheel Well, R.H. 1 -38 43324-1 COVER - Wheel Well, Forward 1 -39 43394-1 SUPPORT ASSEMBLY - Fuel Line 1 -40 43396-1 DOUBLER - Rudder Bar Support, L.H. 1 43396-3 DOUBLER - Rudder Bar Support, R.H. 1 -41 47436-1 SUPPORT-Weld Assembly 1 -42 48283-1 BRACKET-Nose Gear Up Position 1 -43 56664 SCREW (AN526-632R8) 2 -44 58720 WASHER (AN960-6) 2 -45 NUT (MS20364-632) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 26 Model 112 Rockwell International General Aviation Division FORWARD CABIN ASSE MBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NOS AFFECTED 7-46 43326-1 DOUBLER - Sta. 85. 45 2 One & Up -47 43332-1 RETAINER - Windshield, L. H. 1 43332-2 RETAINER - Windshield, R. H. 1 -48 43354-1 FRAME - Cabin Door, Latch, L. H. 1 43354-2 FRAME - Cabin Door, Latch, R.H. 1 43355-1 CHANNEL ASSEMBLY - Cabin Door, Latch, L. H. 1 43355-2 CHANNEL ASSEMBLY - Cabin Door, Latch, R.H. 1 -49 43355-3 CHANNEL - Cabin Door, Latch, L. H. 1 43355-4 CHANNEL - Cabin Door, Latch, R.H. 1 -50 65554 NUTPLATE (MS21055-L3) 2 -51 43356-1 LOOP ASSEMBLY - Cabin Door Latch 2 -52 43357-1 SPACER - Cabin Door Latch 2 -53 43392-1 TUBE 2 -54 43395-1 CLIP - Intercostal, L. H. 1 43395-2 CLIP - Intercostal, R. H. 1 -55 43424-1 CLIP - Stiffener, L. H. 1 43424-2 CLIP - Stiffener, R.H. 1 -56 43412-1 DOUBLER - Door Post, L. H. 1 43412-2 DOUBLER - Door Post, R.H. 1 -57 43466-1 BRACKET - Sta. 85, L. H. 1 43466-2 BRACKET - Sta. 85, R.H. 1 -58 43482-1 BRACKET - Seat Belt Attachment 2 46180-1 MOUNT ASSEMBLY - Nose Gear Door 2 -59 46168-1 MOUNT - Nose Gear Door 2 -60 65776 SCREW (MS24673-4) 2 -61 68008 NUTPLATE (NAS1029-A3) 4 -62 47249-1 PULLEY SUPPORT - Nose Wheel Steering, L. H. 1 47249-2 PULLEY SUPPORT - Nose Wheel Steering, R.H. 1 -63 47249-3 PULLEY SUPPORT - Nose Wheel Steering, L. H. 1 47249-4 PULLEY SUPPORT - Nose Wheel Steering, R. H. 1 -64 48328-1 TAKEOFF ASSEMBLY - Cabin Heat 2 -65 48817-1 SUPPORT BRACKET - Brake Control 1 -66 50176 BOLT (AN3-13A) 2 -67 56642 SCREW (AS525-1032-9) 16 -68 56792 SCREW (AN526-832R4) 4 -69 58718 WASHER (AN960-8) 12 -70 58750 WASHER (AN960-10L) 16 -71 65079 NUT (MS20365-832C) 6 -72 A2167 NUT (MS20365-1032) 14 -73 68085 SCREW (NAS220-8) 6 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 27 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION II Fuselage Group FORWARD CABIN ASSEMBLY FIG. INDEX NO. part NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NO'S AFFECTED 7-74 -75 -76 -77 -78 -79 -80 -81 -82 -83 -84 -85 -86 -87 -88 43474-1 43423-1 43493-1 43496-1 43498-1 43331-1 43331-2 50201 65541 COVER - Cabin Duct GUSSET - Cab Top, Sta. 100.0 GUSSET - Cab Top, Sta. 100.0 DOUBLER - Sta. 100.00 - 123.0 SHIM - Tapered TEE - Reinforcement, Sta. 118.75-130.75, L. H. TEE - Reinforcement, Sta. 118.75-130.75, R.H. BOLT (AN3-10A) BOLT (AN3-7A) BOLT (AN3-6A) WASHER (AN960-10L) WASHER (AN960-10) NUT (MS20365-1032) BOLT (AN3-14A) NUT (C9807-832, Tinnerman) NUTPLATE (MS21047-L3) 4 1 1 1 2 1 1 6 6 12 4 12 12 1 32 4 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 28 Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDO SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 29 Model 112 From RareAviation.com e Rockwell International General Aviation Division Figure 8. Aft Cabin Assembly 30 ISSUED: May 1972 Model 112 9 Rockwell International General Aviation Division AFT CABIN ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REGD SERIAL NOS AFFECTED 43002-1 AFT CABIN ASSEMBLY i One & Up 8-1 43220-1 FRAME - Baggage Door i -2 43223-1 FRAME - Cabtop, Sta. 123 i 43224-1 FRAME ASSEMBLY - Sta. 123 i -3 43224-3 FRAME, L.H. i 43224-4 FRAME, R.H. i -4 43266-1 FRAME - Rear Window, Sta. 123, L.H. i 43266-2 FRAME - Rear Window, Sta. 123, R.H. i -5 43277-1 PLATE - Frame, Sta. 123 i -6 65534 NUT PLATE (MS 21051 - L3) 4 43225-1 FRAME ASSEMBLY - Sta. 123.90 1 -7 43225-3 FRAME - Sta. 123.90 1 -8 43272-1 DOUBLER - Frame, Spar to Fuselage 2 -9 43274-1 STIFFENER - Sta. 123.90, L.H. 1 43274-2 STIFFENER - Sta. 123.90, R.H. 1 -10 43274-3 STIFFENER - Sta. 123.90, L.H. 1 43274-4 STIFFENER - Sta. 123.90, R.H. 1 -11 43276-1 ANGLE - Floor Support, Sta. 123.90 1 -12 43334-1 CLIP - Sta. 123.90, L.H. 1 43334-2 CLIP - Sta. 123.90, R.H. 1 -13 43383-1 BRACKET - Seat Mount Rear 4 -14 65556 ANCHOR NUT (MS 21059 - 08) 5 43230-1 FRAME ASSEMBLY - Sta. 126.90 1 -15 43230-3 FRAME - Sta. 126.90 1 -16 43272-1 DOUBLER - Frame, Spar to Fuselage 2 -17 65556 ANCHOR NUT (MS 21059 - 08) 5 -18 43494-1 GUSSET - Top F. Sta. 123. 00 1 -19 43240-1 FLOOR - Baggage Compartment 1 -20 43254-5 STRINGER - Aft Cabin, Sta. 126.90 - 144.82 1 43254-6 STRINGER - Aft Cabin, Sta. 126.90 - 144.82 1 43256-1 FRAME ASSEMBLY - Forward Baggage Compart- 1 ment -21 43256-3 FRAME - Forward Baggage Compartment 1 -22 40123-1 ANGLE - Tabulated 1 -23 43259-1 CLIP - Forward Baggage Frame, L.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 31 Model 112 From RareAviation.com e Rockwell International General Aviation Division AFT CABIN ASSEMBLY SECTION II Fuselage Group FIG. S INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NOS AFFECTED 8-23 43259-2 CLIP - Forward Baggage Frame, R.H. i One & Up -24 43279-1 FORMER - Forward, Canted Baggage Frame, L.H. i 43279-2 FORMER - Forward, Canted Baggage Frame, R.H. i -25 43280-1 FITTING - Canted Baggage Frame, L.H. i 43280-2 FITTING - Canted Baggage Frame, R.H. i -26 43468-1 STIFFENER - Rear Seat Support Frame, L.H. i 43468-2 STIFFENER - Rear Seat Support Frame, R.H. i -27 43378-1 DOUBLER - Canted Baggage Frame, L.H. i 43378-2 DOUBLER - Canted Baggage Frame, R.H. i -28 43451-1 PLATE - Hinge, Baggage Door 2 -29 43411-1 DOUBLER - B. L.0, Canted Baggage Frame 1 -30 43469-1 FITTING ASSEMBLY - Rear Seat Support 2 -31 65544 NUTPLATE (MS 21047-L4) 2 -32 68037 ANCHOR NUT (NAS 1027-N4) 2 43257-1 FRAME ASSEMBLY - Canted Sta. 123.90 1 -33 43257-3 FRAME - Canted, Sta. 123.90, L.H. 1 43257-4 FRAME - Canted, Sta. 123.90, R.H. 1 -34 43298-1 CHANNEL - Splice, Canted Frame 1 -35 43258-1 BEAM - Sloping, Sta. 123.90 - 147.40, L.H. 1 43258-2 BEAM - Sloping, Sta. 123.90 - 147.40, R.H. 1 -36 43260-1 BEAM - Upper Support, Baggage Door, L.H. 1 43260-2 BEAM - Upper Support, Baggage Door, R.H. 1 -37 43261-1 GUSSET - Inner, Baggage Door 2 -38 43262-1 STRINGER - Aft Cabin, Sta. 144.80 - 178.00, L.H. 1 43262-2 STRINGER - Aft Cabin, Sta. 144.80 - 178.00, R.H. 1 -39 43265-1 BEAM - Support, Baggage Floor B.L. 7.00, L.H. 1 43265-2 BEAM - Support, Baggage Floor B.L. 7.00, R.H. 1 -40 43267-1 FRAME - Upper, Rear Window, L.H. 1 43267-2 FRAME - Upper, Rear Window, R.H. 1 -41 43268-1 FRAME - Aft Window, Lower, L.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 32 Model 112 Rockwell International General Aviation Division AFT CABIN ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 8-42 -43 -44 -45 -46 -47 -48 -49 -50 -51 -52 -53 -54 -55 -56 -57 -58 -59 -60 -61 -62 -63 -64 43268-2 43299-1 43299-2 43306-1 43307-1 43393-1 43467-1 43467-2 43467-3 43467-4 65544 43475-1 43475-2 43454-1 43454-2 65554 65570 56619 56847 65543 43481-1 43481-2 43495-1 43497-1 43499-1 43499-2 43445-1 FRAME - Aft Window, Lower, R.H. BEAM - Lower Support, Baggage Floor, L.H. BEAM - Lower Support, Baggage Floor, R.H. GUSSET - Sta. 123.00 - 126.90 INTERCOSTAL - Cabtop, Sta. 123-148 CLIP - Rear Window, Sta. 153 BRACKET ASSEMBLY - Baggage Restraint, L.H. BRACKET ASSEMBLY - Baggage Restraint, R.H. BRACKET - Baggage Restraint, L.H. BRACKET - Baggage Restraint, R.H. NUTPLATE (MS 21047-L4) STEP INSTALLATION, L.H. STEP INSTALLATION, R.H. STEP ASSEMBLY, L.H. STEP ASSEMBLY, R.H. NUTPLATE (MS 21055-L3) NUTPLATE (MS 21071-L3) SCREW (AN507-1032-6) SCREW (AN526-1032-7) NUTPLATE (MS21047-L3K) NUTPLATE (MS21071-L3K) FRAME - Sta. 168.32, L.H. FRAME - Sta. 168.32, R.H. GUSSET - Top Inboard F. Sta. 123. 00 CHANNEL - Canted Frame DOUBLER - Lower Center Fuselage, L.H. DOUBLER - Lower Center Fuselage, R.H. BRACKET - Flap Sender HANDLE - (#H-505 Bivar Inc. ) BOLT (AN3-4) WASHER (AN960-10L) WASHER (AN936-B10) i i i 2 1 2 1 1 1 1 2 1 1 1 1 4 4 4 20 10 6 1 1 1 1 1 1 1 2 4 4 4 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Model 112 ISSUED: May 1972 33 From RareAviation.com Rockwell International General Aviation Division Figure 9. Aft Fuselage Assembly ISSUED: May 1972 34 Model 112 e Rockwell International General Aviation Division AFT FUSELAGE ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 43003-1 AFT FUSELAGE ASSEMBLY i One & Up 9-1 40116-1 BOLT - Stop 2 -2 54548 NUT (AN315-3) 2 -3 65546 NUTPLATE (MS21047-3) 2 -4 43201-1 FRAME - Sta. 178 1 -5 43202-1 FRAME - Sta. 205 1 -6 43205-1 FRAME - Sta. 230.50 1 -7 43206-1 BULKHEAD - Canted, Sta. 263 1 -8 43207-1 SKIN - Tailcone, L.H. 1 -9 43208-1 SKIN - Tailcone, R.H. 1 -10 43209-1 SKIN - Lower 1 -11 43250-1 STRINGER, L.H. 1 43250-2 STRINGER, R.H. 1 -12 43251-1 SKIN - Lower Corner, L.H. 1 43251-2 SKIN - Lower Corner, R.H. 1 -13 43252-1 DOUBLER - Fin Cutout 1 -14 43253-1 BUTT STRAP, L.H. 1 43253-2 BUTT STRAP, R.H. 1 -15 43270-1 GUSSET - Rudder Horn Support 1 43271-1 BEARING ASSEMBLY - Support Block 1 -16 43271-3 BLOCK - Bearing Support 1 -17 60184 BEARING (Bound Brook #F316G) 1 -18 43275-1 SPLICE - Tailcone, L.H. 2 43275-2 SPLICE - Tailcone, R.H. 2 -19 43278-1 STIFFENER - Frame Sta. 230.50 1 -20 43283-1 SPLICE - Tailcone B.L. 18.99, L.H. 1 43283-2 SPLICE - Tailcone B.L. 18.99, R.H. 1 -21 43284-1 CLIP - Floor Beam Sta. 178 2 -22 43308-1 BRACKET - Pulley, Sta. 230.50 1 -23 43361-1 DORSAL - Fairing, Center 1 43363-1 ANGLE ASSEMBLY - Dorsal Attachment, L.H. 1 43363-2 ANGLE ASSEMBLY - Dorsal Attachment, R.H. 1 -24 43363-3 ANGLE - Dorsal Attachment, L.H. 1 43363-4 ANGLE - Dorsal Attachment, R.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 35 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION II Fuselage Group AFT FUSELAGE ASSEMBLY FIG. & INDEX NO, PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 9-25 65551 NUTPLATE (MS21047-L08K) 2 One & Up -26 65540 NUTPLATE (MS21051-08K) 2 43400-1 EQUIPMENT SHELF 1 -27 43401-1 SUPPORT - Equipment Shelf, Sta. 178 - 205, L.H. 1 43401-2 SUPPORT - Equipment Shelf, Sta. 178 - 205, R.H. 1 -28 43402-1 SHELF - Equipment, Power Pack 1 -29 43410-1 PLATFORM - Battery Cradle 1 -30 43421-1 DOUBLER - Tailcone, Sta. 265.58 1 -31 43443-1 DOUBLER - Ventral Fin 1 -32 43444-1 TIE DOWN ASSEMBLY 1 -33 43448-1 VENTRAL FIN 1 -34 44004-1 LOWER FIN ASSEMBLY 1 -35 50826 BOLT (AN4-4A) 2 -36 51537 BOLT (AN5-5A) 4 -37 58760 WASHER (AN960-416) 4 -38 58780 WASHER (AN960-516) 8 -39 A2172 NUT (MS20365-428) 2 -40 NUT (MS20365-524) 4 -41 47205 BRACKET - Sta. 263 1 -42 47206-1 BRACKET - Pulley, Sta. 179.98, L.H. 1 47206-2 BRACKET - Pulley, Sta. 179.98, R.H. 1 -43 47212-1 BRACKET - Sta. 263 1 -44 47213-1 BRACKET - Pulley, Sta. 232.70, L.H. 1 47213-2 BRACKET - Pulley, Sta. 232.70, R.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 36 Model 112 Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1072 37 Model 112 From RareAviation.com * Rockwell International General Aviation Division Figure 10. Firewall Assembly 38 ISSUED: May 1972 Model 112 section ii Rockwell International firewall assembly Fuselage Group General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 10-1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -24 -25 -26 -27 43008-1 43204-1 43204-2 43204-3 43291-1 43295-1 43377-1 43415-1 43417-1 59472 46169-1 46183-1 46184-1 46191-1 46192-1 46193-1 46195-1 48303-1 48306-1 48307-1 48311-1 48312-1 48314-1 48321-1 48326-1 48327-1 48815-1 65541 65547 65554 65566 68004 FIREWALL ASSEMBLY STRAP - Firewall, L.H. STRAP - Firewall, R.H. STRAP- Firewall, Center CHANNEL - Firewall DOUBLER - Mount Attachment FIREWALL WEB BRACKET ASSEMBLY - Voltage Regulator BRACKET - Voltage Regulator NUTPLATE (K1000-08BC) SPACER STIFFENER - Firewall, L.H. STIFFENER - Firewall, R.H. BRACKET ASSEMBLY - Oil Cooler BRACKET - Oil Cooler DUCT - Oil Cooler DOUBLER - Oil Cooler BOX ASSEMBLY - Cabin Heat COVER - Cabin Heat Box TAKEOFF ASSEMBLY - Cabin Heat Box VENT - Cabin Heat Box CLOSURE - Cabin Heat Box BRACKET - Cabin Heat Box BRACKET - Control Cable BRACKET - Control Cable BRACKET - Control Cable MOUNTING BRACKET - Parking Brake Valve NUTPLATE (MS21047-L3) NUTPLATE (MS21047-L08) NUTPLATE (MS21055-L3) NUTPLATE (MS21059-L3) NUTPLATE (NAS1033-A3) i i i i i i i i i 4 2 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 18 5 2 6 2 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 39 Model 112 From RareAviation.com e Rockwell International General Aviation Division Figure 11. Console Tunnel Assembly 40 ISSUED: May 1972 Model 112 Rockwell International General Aviation Division SECTION II Fuselage Group CONSOLE TUNNEL ASSEMBLY FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NOS AFFECTED 43232-1 CONSOLE TUNNEL ASSEMBLY i One & Up u-i 43231-3 COVER - Console, Aft i 43249-1 TRACK ASSEMBLY - Seat, L.H. i 43249-2 TRACK ASSEMBLY - Seat, R.H. i -2 43249-3 TRACK - Seat, L.H. i 43249-4 TRACK - Seat, R.H. i -3 43366-1 BLOCK - Seat, Stop 4 -4 CLEVIS PIN (MS20392-1C33) 4 -5 COTTER PIN (MS24665-149) 4 -6 43318-1 YOKE SUPPORT - Console, L.H. 1 43318-2 YOKE SUPPORT - Console, R.H. 1 -7 43319-1 COVER - Console Top, Forward 1 -8 43320-1 PANEL - Console Side, L.H. 1 43320-2 PANEL - Console Side, R.H. 1 43321-1 SUPPORT ASSEMBLY - Fuel Selector 1 -9 43321-3 SUPPORT - Fuel Selector 1 -10 68007 NUTPLATE (NAS1068A3) 3 -11 43322-3 BRACKET - Tunnel, Sta. 123.86 1 -12 43373-1 FRAME - Console, Sta. 85.90 1 -13 43374-1 FRAME - Console, Sta. 96.549 1 -14 43375-1 FRAME - Console, Sta. 107.198 1 -15 43398-1 PLATE - Quadrant Stop 1 43462-1 COVER ASSEMBLY - Console 1 -16 43233-1 COVER - Console Top, Center 1 -17 43461-1 BRACKET - Throttle Switch Mounting 1 -18 43482-1 BRACKET - Seat Belt Attachment 2 -19 46128-1 BRACKET - Prop Control 1 -20 46129-1 BRACKET - Mixture Control 1 -21 46130-1 BRACKET - Carb. Heat & Throttle Control 1 -22 47223-1 DOUBLER - Sta. 92 - 67 2 -23 47306-1 PLATE - Mounting, Yoke 2 -24 47404-1 BRACKET - Support, Rudder Trim Adjust 1 -25 56642 SCREW (AN525-1032-9) 14 -26 56608 SCREW (AN526-632-4) 41 -27 58750 WASHER (AN96O-1OL) 12 -28 A2167 NUT (MS20365-1032) 12 -29 59466 NUT (C 8090-632, Tinnerman) 41 -30 59483 NUT (C9807-832, Tinner man) 4 -31 60173 BEARING (F379C, Bound Brook Bearing) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 41 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 12. Baggage Door and Cabin Door ISSUED: May 1972 42 Model 112 e Rockwell International General Aviation Division BAGGAGE DOOR AND CABIN DOOR SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RECTO SERIAL NOS AFFECTED 43010 DRAWING - Baggage Door Installation One & Up 12-1 43005-1 DOOR ASSEMBLY - Baggage i 43349-1 LATCH ASSEMBLY - Baggage Door i -2 43350-1 HOUSING - Baggage Door Latch i -3 43352-1 LEVER - Baggage Door Latch i -4 LOCK (H82A4N, Hurd Lock Co.) i -5 ROLL PIN (52-022-094-1750, Esna) i -6 43450-1 HINGE ASSEMBLY - Baggage Door 2 -7 43452-1 STRIKER PLATE - Baggage Door 1 -8 43453-1 SPACER - Striker Plate, Baggage Door 1 -9 43463-1 SEAL - Baggage Door 1 -10 56641 SCREW (AN525-832 R7) 4 -11 56637 SCREW (AN525-832 R12) 2 -12 56836 SCREW (AN526-832 R7) 4 -13 58730 WASHER (AN960D8) 10 -14 65073 NUT (MS20365D832) 6 43004 DRAWING - Cabin Door Installation - 43004-1 DOOR ASSEMBLY - Cabin (complete), L.H. 1 43004-2 DOOR ASSEMBLY - Cabin (complete), R.H. 1 -15 DOOR ASSEMBLY - Cabin, L.H. 1 DOOR ASSEMBLY - Cabin, R.H. 1 -16 40111-41 SPACER 4 -17 40112-1 SEAL - Cabin Door 2 -18 40117-1 WASHER - Upper Door Latch 2 -19 43246-1 V/INDOW - Cabin Door, L.H. 1 43246-2 WINDOW - Cabin Door, R.H. 1 -20 43344-1 HINGE - Aft Cabin Door 2 -21 43344-3 HINGE - Aft, Cabin Door 2 43347-1 LATCH ASSEMBLY - Upper Cabin Door, L.H. 1 43347-2 LATCH ASSEMBLY - Upper Cabin Door, R.H. 1 -22 40111-9 SPACER 6 -23 40117-1 WASHER - Upper Door Latch 2 -24 43342-1 RETAINER - Cabin Door Latch, L.H. 1 43342-2 RETAINER - Cabin Door Latch, R.H. 1 -25 43403-1 PLATE - Upper Door Latch 4 -26 43404-1 CAM - Upper Door Latch, L.H. 1 43404-2 CAM - Upper Door Latch, R.H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 43 Model 112 From RareAviation.com Rockwell International General Aviation Division BAGGAGE DOOR AND CABIN DOOR SECTION II Fuselage Group FIG. INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 12-27 43405-1 SPRING - Upper Door Latch, L.H. i One & Up 43405-2 SPRING - Upper Door Latch, R. H. i -28 43406-1 HOOK ASSEMBLY - Upper Door Latch, L.H. i 43406-2 HOOK ASSEMBLY - Upper Door Latch, R.H. i -29 43409-1 HANDLE - Upper Door Latch 2 -30 56929 SCREW (AN530-6R10) 2 -31 58760 WASHER (AN960-416) 4 -32 58770 WASHER (AN960-416L) 2 -33 A2167 NUT (MS20365-1032) 6 -34 65772 SCREW (MS24693-276) 6 -35 43409-1 HANDLE - Upper Door Latch 2 -36 43459-1 RETAINER - Window Cabin Door, L.H. 1 43459-2 RETAINER - Window, Cabin Door, R.H. 1 43487-1 PILOT WINDOW ASSEMBLY 1 -37 43485-1 PILOT WINDOW 1 43486-1 HINGE ASSEMBLY - Pilot Window 1 -38 43486-3 HINGE HALF - Pilot Window 1 -39 43486-5 HINGE HALF - Pilot Window 1 -40 65027 PIN (MS20253 P2-750) 1 -41 43489-1 SEAL - Pilot Window 1 -42 43488-1 LATCH - Pilot Window 1 -43 40111-71 BUSHING 1 -44 59497 WELL-NUT (B-832 Molly Co.) 24 -45 61542 HANDLE ASSEMBLY (A-847-B Gerdes Products Co.) 2 -46 59524 CAP NUT (4-40) 1 -47 WASHER (U125-0040 Associated Spring Corp.) 1 -48 59533 CAP NUT (CL CE 063-2-5) 5 -49 SCREW (AN507C440-10) 1 -50 SCREW (AN507C632-5) 5 -51 59640 SCREW (AN509-832R8) 20 -52 SCREW (AN509-8R10) 4 -53 56644 SCREW (AN525-832R9) 20 -54 59687 SCREW (AN525-10R6) 12 -55 SCREW (AN525-10R8) 12 -56 56645 SCREW (AN525-10R9) 12 -57 56929 SCREW (AN530-6R10) 2 -58 58722 WASHER (AN960-6L) 5 -59 58718 WASHER (AN960-8) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 44 Model 112 Rockwell International General Aviation Division BAGGAGE DOOR AND CABIN DOOR SECTION II Fuselage Group FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER CODE NOMENCLATURE REQD AFFECTED 12-60 58750 WASHER (AN960-10L) 24 One & Up -61 65079 NUT (MS2O365-832) 4 -62 A2167 NUT (MS20365-1032) 24 -63 65547 NUTPLATE (MS21047-L08) 16 -64 65536 NUTPLATE (MS21O51-LO8) 4 -65 GROMMET (MS35489-15) 2 -66 BUSHING (NAS 43DD0-15) 1 -67 43343-1 HINGE - Forward, Cabin Door 2 -68 43343-3 HINGE - Forward, Cabin Door 2 -69 43358-1 COVER - Cabin Door Latch, L.H. 1 43358-2 COVER - Cabin Door Latch, R. H. 1 -70 43345-1 STRIKER PLATE - Cabin Door Latch 2 -71 43346-1 SPACER - Cabin Door Handle 2 -72 43470-1 PLATE - Adjust, Cabin Door Handle 2 -73 43480-1 SPACER - Door Latch 2 -74 59632 SCREW (AN507-832R12) 4 -75 56646 SCREW (AN525-10R14) 4 -76 PIN (MS20392-245) 4 -77 A2327 COTTER PIN (MS24655-132) 4 -78 65842 FINISHING WASHER (MS27129-8) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 45 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 13. Windows and Windshield Installation ISSUED: May 1972 46 Model 112 Rockwell International General Aviation Division SECTION II Fuselage Group WINDOWS AND WINDSHIELD INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 43007 DRAWING - Window Installation One & Up 43009 DRAWING - Windshield Installation 13-1 43221-1 RETAINER - Rear Window, Lower, L.H. i 43221-2 RETAINER - Rear Window, Lower, R.H. i -2 43222-1 RETAINER - Rear Window, Upper, L.H. i 43222-2 RETAINER - Rear Window, Upper, R.H. i -3 43241-1 WINDSHIELD i -4 43242-1 RETAINER - Windshield, Bottom i -5 43247-1 WINDOW - Aft Cabin, L.H. i 43247-2 WINDOW - Aft Cabin, R.H. i -6 43269-1 RETAINER - Rear Window, F. Sta. 123, L.H. i 43269-2 RETAINER - Rear Window, F. Sta. 123, R.H. i -7 43315-1 RETAINER - Rear Window, F. Sta. 153.50 to 167.00, L.H. i 43315-2 RETAINER - Rear Window, F. Sta. 153.50 to 167.00, R.H. i -8 43348-1 SEAL - Rear Window 2 -9 43348-3 SEAL - Rear Window 2 -10 43348-5 SEAL - Rear Window 2 -11 59627 SCREW (AN525-8-7) 28 -12 65739 SCREW (MS24625-30) 82 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 47 Model 112 From FtareAviation.com Rockwell International General Aviation Division Figure 14. Heating and Defroster System Installation ISSUED: May 1972 48 Model 112 Rockwell International General Aviation Division SECTION II Fuselage Group HEATING AND DEFROSTER SYSTEM INSTALLATION FIG. & INDEX NO. PARI NUMBER GODE NOMENCLATURE NO. REffD SERIAL NO'S AFFECTED 48301 DRAWING - Heater and Defroster System Installation One & Up 14-1 46050-5 AIR DUCT - Tabulated i -2 46050-7 AIR DUCT - Tabulated i -3 46050-9 AIR DUCT - Tabulated i -4 46050-11 AIR DUCT - Tabulated i -5 46050-13 AIR DUCT - Tabulated i -6 46050-15 AIR DUCT - Tabulated i -7 46148-1 CONTROL - Push Pull, Head Type, Tabulated i -8 46148-3 CONTROL - Push Pull, Head Type, Tabulated i -9 46148-5 CONTROL - Push Pull, Head Type, Tabulated i -10 46148-7 CONTROL - Push Pull, Head Type, Tabulated i 48305-1 VALVE ASSEMBLY - Cabin Heat and Defroster i 48304-1 TAKEOFF ASSEMBLY - Cabin Heat and De- froster i -11 48313-1 PLATE - Takeoff, Cabin Heat and Defroster i -12 48316-1 REFLECTOR - Exhaust Air i -13 48331-1 TUBE - Flanged 2 -14 43389-1 TUBE - Flanged 2 -15 48308-1 SEPARATOR - Cabin Heat and Defroster Valve 4 -16 48309-1 BAFFLE - Cabin Heat Valve 2 -17 48310-1 BAFFLE - Defroster Valve 2 -18 48322-1 GATE ASSEMBLY - Cabin Heat, Right Side 1 -19 48323-1 GATE ASSEMBLY - Cabin Heat, Left Side 1 -20 48324-1 GATE ASSEMBLY - Defroster, Right Side 1 -21 48325-1 GATE ASSEMBLY - Defroster, Left Side 1 -22 50050 BOLT (AN3-6) 2 -23 587 40 WASHER (AN960-10) 2 -24 65076 NUT (MS20365 - 1032C) 2 -25 55700 COTTER PIN (AN380-2-3) 4 -26 56834 SCREW (AN526-832R6) 4 -27 A1138 SCREW (AN526-832R12) 12 -28 56852 SCREW (AN526-1032R6) 2 -29 58719 WASHER (AN960-8L) 12 -30 587 40 WASHER (AN960-10) 4 -31 65079 NUT (MS20365-832C) 16 -32 65076 NUT (MS20365- 1032C) 2 -33 65722 CLAMP (MS21918 DG40) 2 -34 60784 CLAMP (102116, Murray Corp.) 4 -35 60783 CLAMP (102218, Murray Corp.) 4 -36 60782 CLAMP (102300, Murray Corp.) 4 -37 CLAMP (A2980A-3-27, Tinnerman Products Co.) 4 -38 CLAMP (A4980A-8-92, Tinner man Products Co.) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. 49 Tabulated ISSUED: May 1972 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 15. Fresh Air Vent Installation ISSUED: May 1972 50 Model 112 Rockwell International General Aviation Division SECTION II Fuselage Group FRESH AIR VENT INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGO SERIAL NO'S AFFECTED 48301 DRAWING - Heating and Ventilation Installation One & Up 15-1 48417-1 CABLE - Control, Cabin Air i -2 48417-3 CABLE - Control, Cabin Air i 48421-1 VALVE ASSEMBLY - Cabin Air, L.H. i 48421-2 VALVE ASSEMBLY - Cabin Air, R.H. i -3 48420-1 PLATE ASSEMBLY - Cabin Air, L.H. i 48420-2 PLATE ASSEMBLY - Cabin Air, R.H. i -4 48425-1 BRACKET - Cabin Air, L.H. i 48425-2 BRACKET - Cabin Air, R.H. i -5 48426-1 BRACKET - Cabin Air, L.H. i 48426-2 BRACKET - Cabin Air, R.H. i 48428-1 LEVER ASSEMBLY - Cabin Air, L.H. i 48428-2 LEVER ASSEMBLY - Cabin Air, R.H. i -6 48423-1 PLATE - Cabin Air, L.H. i 48423-2 PLATE - Cabin Air, R.H. i -7 48424-1 LEVER - Cabin Air, L.H. i 48424-2 LEVER - Cabin Air, R.H. i -8 48429-1 PAD - Cabin Air 2 48415-1 COVER ASSEMBLY - Cabin Air 4 -9 43474-3 COVER - Cabin Duct 4 -10 VENT VALVE(#2150 Wemac Designers & Manufactures) 4 -11 56643 SCREW(AN520-10-7) 16 -12 58750 WASHER (AN960-10L) 16 -13 A2167 NUT (MS20365 -1032) 16 -14 A0398 NUT(AN365-832) 5 -15 SC R EW (A N507 - 832 -16) 2 -16 56812 SCREW(AN526-832-4) 32 -17 56834 SC R EW (AN52 6 - 832 R6) 2 -18 56838 SCREW(AN526-832R8) 1 -19 A1113 SCREW(AN526-832-10) 6 -20 58718 WASHER(AN960-8) 5 -21 CL AMP(MS21919H3) 5 -22 68232 NUT(NAS395-10) 6 -23 SPACER(NAS1057Tl~020) 1 -24 SPACER(NAS1057Tl-055) 2 -25 CLAMP(A-2980-3-27 Tinnerman) 1 -26 NUT(C9807-832 Tinnerman) 32 -27 FASTENER(C10608-017 Tinnerman) 2 -28 SCREW (AN515-4-10) 8 -29 NUT (AN340-4) 8 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 51 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 16. Overhead Vent System Installation ISSUED: May 1972 52 Model 112 section ii Rockwell International overhead vent Fuselage Group General Aviation Division SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NOS AFFECTED 16-1 48440 48441-1 DRAWING - Overhead Vent System Installation TUBE, Fwd 2 One & Up -2 48441-3 TUBE, Aft 2 -3 48443-1 DIRECTOR - Vent System 1 -4 48442-1 CAP - Vent System 4 -5 63897 AIR VALVE (#10-0549-1, Grimes Mfg. Co.) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 53 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 17. Instrument Panel Installation ISSUED: May 1972 54 Model 112 e Rockwell International General Aviation Division INSTRUMENT PANEL INSTALLATION SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 48013 DRAWING - Instrument Installation Main Panel One & Up 48014 DRAWING - Instrument Installation Sub Panel 43229-1 PANEL ASSEMBLY - Instrument i 17-1 43335-1 INSTRUMENT PANEL i -2 43369-1 STIFFENER - Instrument Panel i -3 43370-1 CHANNEL - Instrument Panel i -4 43370-3 CHANNEL - Instrument Panel 2 -5 COMPASS (#C2400LP4 Airpath Inc.) 1 -6 OUTSIDE AIR TEMPERATURE GAUGE (#1592-26 Rochester Gauges Inc.) 1 EXHAUST GAS TEMPERATURE GAUGE (#35/225 Alcor Aviation Inc.) 1 -7 INDICATOR (#210-10A Alcor Aviation Inc.) 1 -8 PROBE (#MC1-A1O6-A36 Alcor Aviation Inc.) 1 -9 LEAD (#MC1-A106-75 Alcor Aviation Inc.) 1 -10 GAUGE CLUSTER (873000 Stewart Warner Corp.) 1 -11 AMP METER (876000 Stewart Warner Corp.) 1 -12 VOLT METER (876001 Stewart Warner Corp.) 1 -13 LEFT FUEL TANK GAUGE (878001 Stewart Warner Corp.) 1 -14 RIGHT FUEL TANK GAUGE (878000 Stewart Warner Corp.) 1 -15 GAUGE CLUSTER (873002 Stewart Warner Corp.) 1 -16 CYLINDER HEAD TEMPERATURE GAUGE (880002 Stewart Warner Corp.) 1 -17 OIL PRESSURE GAUGE (883002 Stewart Warner Corp.) 1 -18 OIL TEMPERATURE GAUGE (880003 Stewart Warner Corp.) 1 -19 DUMMY GAUGE (G824866 Stewart Warner Corp.) 1 -20 CIGAR LIGHTER (#L 140232 Casco Products Inc.) 1 -21 MANIFOLD PRESSURE GAUGE (#83810-05 K oils man) MANIFOLD PRESSURE GAUGE (#6000A United 1 Instrument Co.) 1 -22 AIRSPEED INDICATOR (#1432-22B-A-A1 Pioneer) 1 AIRSPEED INDICATOR (#544-4 Aeromarine) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed October 1975 55 Model 112 From RareAviation.com Rockwell International General Aviation Division INSTRUMENT PANEL INSTALLATION SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NOS AFFECTED 17-23 -24 -25 -26 -27 -28 -29 -30 -31 -32 -33 -34 -35 -36 -37 -38 -39 TURN COORDINATOR (#1681-1681A Brittain Ind.) TURN COORDINATOR (#600-009-900 Brittain Ind.) FLAP INDICATOR GAUGE (#Q14915, Stewart Warner Corp.) SUCTION GAUGE (#3-310-5 U. M. A.) AVIATION CLOCK, 8 Day (#A -11-90 Longines Wittnauer) RATE OF CLIMB INDICATOR (#7020 United Instru- ment Go.) DIRECTIONAL GYRO (#200-5 Aim Corp.) GYRO HORIZON (#3OO-3CF Aviation Instrument Manufacturing Corp.) ALTIMETER (#Ul-5932 United Instrument Co.) TACHOMETER (#ES-551-NF Stewart Warner Corp.) SCREW (AN526-8R6) ' ' SCREW (AN530-8R6) NUT (MS20365B632) SCREW (MS35214-27) SCREW (MS35214-30) FASTENER (NAS487-20) NUT (#A1348-82 Tinnerman Products Inc.) NUT (#RM52LHA-4982-8-82 Tinnerman Products Inc.) i i i i i i i i i i n 9 12 14 29 14 9 9 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 56 Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 57 Model 112 From RareAviation.com e Rockwell International General Aviation Division 4 Figure 18. Vacuum System Installation 58 ISSUED: May 1972 Model 112 e Rockwell International General Aviation Division SECTION II Fuselage Group VACUUM SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REM SERIAL NO'S AFFECTED 18-1 62541 A PUMP - Dry, Vacuum (#200 cc) i One & Up -2 A GASKET - Vacuum Pump Mounting (B3001-A-1) i -3 A COUPLING ASSEMBLY - Pump Drive (Bl-9-1) i -4 A COUPLING - Spline, Pump Drive (Bl-4-1) i -5 61420 A FILTER ASSEMBLY - Air (#1J7-1) i -6 63922 A VALVE - Suction Regulating (#133-A-4) i -7 A FILTER - Regulating Valve (#B3005-A-l) i -8 48054-1 HOSE - Vacuum, Gyro Horizon to Air Filter i -9 48054-2 HOSE - Vacuum, Gyro Horizon to Regulating Valve i -10 48054-3 HOSE - Vacuum, Directional Gyro to Air Filter i -11 48054-4 HOSE - Vacuum, Directional Gyro to Regulating Valve i -12 48054-5 HOSE - Vacuum, Gyro Horizon to Suction Gauge i -13 48054-6 HOSE - Vacuum, Regulating Valve to Vacuum Pump i -14 48055-1 WASHER - Support i -15 48056-1 WASHER - Air Filter i -16 60859 CLAMP (QS 100-M10S, Aeroseal) 10 -17 57134 CLAMP (AN737-W22) 2 -18 59361 A FITTING (1K10-2-4) 1 -19 59362 A FITTING (1K10-4-6) 4 -20 59365 A FITTING (IK 1-6-10) 1 -21 59363 A FITTING (1K1-6-8) 1 -22 65517 PLUG (MS20913-1D) 1 A - AIRBORNE MANUFACTURING COMPANY When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 59 Model 112 From RareAviation.com e Rockwell International General Aviation Division Figure 19. Pitot System Installation ISSUED: May 1972 60 Model 112 e Rockwell International General Aviation Division SECTION II Fuselage Group PITOT SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 19-1 48601 48602-1 DRAWING - Pitot System Installation PITOT LINE - Dynamic i One & Up -2 48602-3 PITOT LINE - Dynamic i -3 48602-5 PITOT LINE - Dynamic i -4 48602-7 PITOT LINE - Dynamic i -5 48603-1 PITOT LINE - Static i -6 48603-3 PITOT LINE - Static i -7 48603-5 PITOT LINE - Static i -8 48603-7 PITOT LINE - Static i -9 48603-9 PITOT LINE - Static i -10 48603-11 PITOT LINE - Static 2 -11 48609-1 CONNECTOR - Air Speed Indicator 1 -12 48610-1 TEE - Air Speed Indicator 1 48611-3 PITOT HEAD ASSEMBLY 1 -13 48608-1 PITOT HEAD 1 -14 48612-1 GASKET - Pitot Head 1 -15 61064 CONNECTOR (#268P Imperial Eastman Corp 1 -16 48613-1 VALVE BRACKET - Pitot 1 -17 NUT (AN340-6) 1 -18 55474 NUT (AN365-632) 1 -19 SCREW (AN5266R5) 1 -20 56690 SCREW (AN526-632-12) 3 -21 56841 SCREW (AN526-1032R4) 6 -22 WASHER (AN960-6L) 1 -23 58719 WASHER (AN960-8L) 3 -24 58750 WASHER (AN960-10L) 6 -25 65074 NUT (MS20365D1032) 6 -26 65655 GROMMET (MS21266-1N) As -27 65729 CLAMP (MS21919DG4) Req. 6 -28 CLAMP (MS21919DG6) 1 -29 65725 CLAMP (MS21919DG8) 6 -30 UNION ELBOW (#265N Imperial Eastman Corp.) 3 -31 61064 CONNECTOR (#268P Imperial Eastman Corp.) 1 -32 ELBOW (#269P Imperial Eastman Corp.) 1 -33 UNION TEE (#264N Imperial Eastman Corp.) 1 -34 59441 TEE (#272P Imperial Eastman Corp.) 1 -35 VALVE (#SFX23 Gagne Associates Inc.) 1 -36 60786 CLAMP (#DEK021-0500 DEK, Inc.) 5 -37 CLAMP (#DK750 DEK, Inc.) 6 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 61 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 20. Interior Installation ISSUED: May 1972 62 Model 112 e Rockwell International General Aviation Division SECTION II Fuselage Group INTERIOR INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RECTO SERIAL NOS AFFECTED 20-1 49002-1 A GLARESHIELD ASSEMBLY - Sport and Super Sport, One & Up With Instrument Lights i 49002-501 A GLARESHIELD ASSEMBLY - Sport and Super Sport, Without Instrument Lights i 49002-503 A GLARESHIELD ASSEMBLY - Standard, With Instrument Lights i 49002-505 A GLARESHIELD ASSEMBLY - Standard, Without Instrument Lights i -2 49003-3 A WINDSHIELD FRAME ASSEMBLY, L. H. i 49003-4 A WINDSHIELD FRAME ASSEMBLY, R. H. i -3 49003-5 A WINDSHIELD FRAME ASSEMBLY, CENTER i -4 49004-7 A FORMER - Quadrant and Tunnel Cover i -5 49004-9 A COVER - Quadrant and Tunnel i -6 49012-1 A FACE PLATE - Fuel Primer i -7 49019-5 A FACE PLATE INSERT - Quadrant i 49019-7 A FACE PLATE INSERT - Quadrant, Strobe Lights i -8 49005-3 A INSTRUMENT PANEL COVER i -9 49005-5 A INSERT - Instrument Panel Cover i -10 49005-7 A INSERT - Instrument Panel Cover i -11 49005-9 A INSERT - Instrument Panel Cover i -12 49006-1 A CABIN DOOR PANEL ASSEMBLY, L. H. i 49006-2 A CABIN DOOR PANEL ASSEMBLY, R. H. i -13 49016-1 A SIDE PANEL ASSEMBLY - Super Sport, Aft, L. H. i 49016-501 A SIDE PANEL ASSEMBLY - Standard and Sport, Aft, L. H. i 49007-1 A SIDE PANEL ASSEMBLY - Super Sport, Aft., R. H. i 49007-501 A SIDE PANEL ASSEMBLY - Standard and Sport, Aft, R.H. i -14 49008-5 A OVERHEAD CONSOLE PANEL, FWD. i -15 49008-9 A OVERHEAD CONSOLE PANEL, AFT i -16 49009-1 A AFT BULKHEAD ASSEMBLY - Sport and Super Sport i 49078-1 A AFT BULKHEAD ASSEMBLY - Standard i -17 49010-3 BAGGAGE RESTRAINT i -18 49011-3 A PANEL - Baggage Door i A - When ordering upholstery parts, always include finish and trim number (see Page (v) for instructions) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 63 Model 112 From RareAviation.com * Rockwell International General Aviation Division INTERIOR INSTALLATION SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 20-19 49013-3 A PANEL - Headliner, Forward L. H. i One & Up 49013-4 A PANEL - Headliner, Forward R. H. i -20 49013-5 A PANEL - Headliner, Aft L. H. i 49013-6 A PANEL - Headliner, AftR.H. i -21 49013-7 SUPPORT - Headliner, Forward Center, L. H. i 49013-8 SUPPORT - Headliner, Forward Center, R. H. i -22 49013-9 SUPPORT - Headliner, Center, L. H. i 49013-10 SUPPORT - Headliner, Center, R. H. i -23 49013-11 SUPPORT - Headliner, Aft, L. H. i 49013-12 SUPPORT - Headliner, Aft. R.H. i -24 49013-15 CLIP - Headliner 6 -25 49013-17 SUPPORT - Headliner, Forward, L. H. 1 49013-18 SUPPORT - Headliner, Forward, R. H. 1 -26 49023-1 A PANEL ASSEMBLY - Forward Side, L. H. 1 49023-2 A PANEL ASSEMBLY - Forward Side, R. H. 1 -27 49026-1 SCUFF PLATE - Door, L. H. 1 49026-2 SCUFF PLATE - Door, R. H. 1 49024-1 SUNVISOR ASSEMBLY 1 -28 49087-1 PLATE - Sun Visor 1 -29 49089-1 SUPPORT ASSEMBLY - Suh Visor 1 -30 49050-7 VISOR, L. H. 1 49050-8 VISOR, R. H. 1 -31 NUT (AN365-832) 2 -32 SCREW (AN509-8-22) 2 -33 SCREW (AN515-8-5) 4 -34 WASHER (AN960-8L) 8 -35 CAP NUT (CLCE 0832-5, Gripco) 4 -36 CLIP (5/16 H, Weckesser) 4 -37 49027-3 A CARPET 1 -38 49027-5 A CARPET 1 -39 49027-7 A CARPET 1 49027-8 A CARPET 1 A - When ordering upholstery parts, always include finish and trim number (see Page (v) for instructions) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 64 Model 112 * Rockwell International General Aviation Division SECTION II Fuselage Group INTERIOR INSTALLATION FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REOD SERIAL NO'S AFFECTED 20-40 49027-15 SCUFF PLATE - Forward Cabin 2 One & Up -41 49027-17 A CARPET - Forward Cabin, L. H. 1 49027-18 A CARPET - Forward Cabin, R. H. 1 -42 49027-19 A CARPET - Forward Cabin, L. H. 1 49027-20 A CARPET - Forward Cabin, R. H. 1 -43 49027-21 A CARPET - Forward Cabin, L. H. 1 49027-22 A CARPET - Forward Cabin, R. H. 1 -44 49027-23 A CARPET - Forward Cabin, L. H. 1 49027-24 A CARPET - Forward Cabin, R. H. 1 -45 49029-3 A CARPET - Baggage Compartment 1 -46 49033-1 A COVER ASSEMBLY - Carpet 2 -47 49033-3 A COVER ASSEMBLY - Carpet 2 -48 49036-1 A CENTER REAR CONSOLE ASSEMBLY 1 -49 49038-1 A SKI RACK ASSEMBLY 1 -50 49049-3 A COVER - Instrument Sub Panel 1 -51 49051-3 A CLOSE OUT - Rear Divan 1 -52 48432-3 GRILL - Rear*Divan 1 -53 49054-501 A GLOVE BOX ASSEMBLY 1 49054-503 A GLOVE BOX ASSEMBLY - Stereo 1 -54 49056-3 A MAP CASE 2 -55 49056-5 A MAP CASE BACK 2 -56 49060-1 A REFRESHMENT CENTER ASSEMBLY 1 -57 49083-3 FIREWALL BLANKET 1 -58 49083-5 FIREWALL BLANKET 1 -59 49084-3 BOX ASSEMBLY - Armrest 1 -60 49084-5 A PAD ASSEMBLY - Armrest 1 -61 49084-19 A COVER - Armrest 1 -62 49080-1 A WINDLACE 2 -63 49080-3 A WINDLACE 1 49302-1 COAT HANGER ASSEMBLY 1 -64 49301-1 BRACKET - Coat Hanger 1 -65 HANGER (#1626, Herman Smith, Inc.) 1 A - When ordering upholstery parts, always include finish and trim number (see Page (v) for instructions) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 65 Model 112 From RareAviation.com Rockwell International General Aviation Division INTERIOR INSTALLATION SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 20-66 -67 -68 49303-1 49304-1 SCREW (NAS220-6) STRAP - Tape Player BRACKET - Tape Player 2 1 1 -69 -70 -71 -72 -73 -74 -75 49305-1 49018-1 48431-1 A COVER - HAT STUD & RING (21452-51F-16-00, Brownline, Inc.) STUD & RING (21452-51F-26-16, Brownline, Inc.) ASH TRAY (#489, Kent Products) HANDLE ASSEMBLY (1735-383-321, Philadelphia Handle Co.) ESCUTCHEON - Coat Hanger DUCT ASSEMBLY - Vent A - When ordering upholstery parts, always include finish and trim number (see Page (v) for instructions) 2 2 2 4 2 1 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 66 Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDO SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 67 Model 112 From RareAviation.com * Rockwell International General Aviation Division Figure 21. Crew Seat Assembly ISSUED: May 1972 68 Model 112 Rockwell International General Aviation Division CREW SEAT ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 21-1 -2 -3 -4 49031-1 49031-2 49031-501 49031-502 49031-503 49031-504 49031-505 49031-506 49031-1 49031-2 D D D D D D D D AD AD B CD CREW SEAT ASSEMBLY, Low Back, L.H. CREW SEAT ASSEMBLY, Low Back, R.H. CREW SEAT ASSEMBLY, Low Back, with INERTIA Shoulder Harness and Headrest, L.H. CREW SEAT ASSEMBLY, Low Back, with INERTIA Shoulder Harness and Headrest, R.H. CREW SEAT ASSEMBLY, Low Back with Headrest, L.H. CREW SEAT ASSEMBLY, Low Back with Headrest, R.H. CREW SEAT ASSEMBLY, Low Back with Inertia Shoulder Harness, L.H. CREW SEAT ASSEMBLY, Low Back with Inertia Shoulder Harness, R.H. SHROUD - Seat Back, Low Back, L.H. SHROUD - Seat Back, Low Back, R.H. PLUG BUTTON ( #SS-51388, United Carr, Cambridge, Mass.) SHOULDER HARNESS (#1108204 Pacific Scientific Co., Anaheim, Calif.) A. Used only with - 49031-1, 49031-2, 49031-501, 49031-502, 49031-503, 49031-504, 49031-505, 49031 506 B. Used only with - 49031 T, 49031-2, 49031-505, 49031-506 C. Used only with - 49031-1, 49031-2, 49031-503, 49031-504 D. When Ordering Upholstery Parts Always Include Finish & Trim Number (See Page (v) For Instructions) i i i i i i i i i i 4 2 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 69 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION II Fuselage Group CREW SEAT ASSEMBLY FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER CODE NOMENCLATURE REGO AFFECTED 21-5 AC REEL ASSEMBLY (#0107129, Pacific Scientific One & Up Co., Anaheim, Calif.) 2 -6 49042-1 B HEADREST ASSEMBLY, Low Back Seat 2 -7 49042-3 B CUSHION - Headrest 2 -8 BC COVER - Headrest 2 -9 49250-1 B BUSHING - Headrest 4 -10 49039-1 CUSHION - Seat Bottom 2 -11 C COVER ASSEMBLY - Seat Bottom 2 -12 49041-1 CUSHION ASSEMBLY - Seat Back 2 -13 49081-1 GUIDE 2 -14 C COVER ASSEMBLY - Seat Back 2 -15 49224-1 TORQUE TUBE 2 49225-1 PIN ASSEMBLY - SEAT STOP 4 -16 49226-1 PIN ASSEMBLY - SEAT STOP 4 -17 49227-1 LINK ASSEMBLY - SEAT STOP, WELD- MENT 4 -18 65084 CLEVIS PIN (MS20392-lc7) 4 -19 65745 COTTER PIN (MS24665-132) 4 -20 63236 SPRING (E-240-031-225, Associated Spring Corp., Conn.) 4 -21 58720 WASHER (AN960-6) 4 -22 60158 BEARING (F-257, Bond Brooke Bearing Corp., Bond Brooke, N.J.) 8 -23 62332 ROLL PIN (#59-012-062-0500, Elastic Stop Nut Div., Union, N.J.) 4 -24 65093 CLEVIS PIN (MS20392-1C23) 4 -25 58720 WASHER (AN960-6) 4 -26 A2327 COTTER PIN (MS24665-132) 4 -27 49209-1 PIN 4 -28 49242-1 ARM ASSEMBLY 4 -29 49243-1 BELLCRANK ASSEMBLY 2 A. Used only with - 49031-501, 49031-502, 49031-505, 49031-506, 49031-507, 49031-508 B. Used only with - 49031-501, 49031-502, 49031-503, 49031-504 C. When Ordering Upholstery Parts Always Include Finish & Trim Number (See Page (v) For Instructions)) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 70 Model 112 e Rockwell International General Aviation Division CREW SEAT ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 21-30 49246-1 ROLLER ASSEMBLY 8 One & Up -31 63015 SPRING (LE-045D-1, Lee Spring Co., Inc., Brooklyn, N.Y.) 4 -32 62332 ROLL PIN (59-012-062-0500, Elastic Stop Nut Div., Union, N.J.) 12 -33 PUSH NUT (P12357, Crest Products, Inc.) 8 -34 58710 WASHER (AN960-4) 8 -35 40111-53 BUSHING 4 -36 65075 NUT (MS20364-1032) 4 -37 58740 WASHER (AN960-10) 8 -38 BOLT (AN23-23) 4 -39 62109 HANDLE (407P2K1, Raytheon Burlington, Mass) 2 -40 A1226 BOLT (AN6-7A) 2 -41 NUT (MS20364-624) 2 -42 58790 WASHER (AN960-616) 4 -43 49082-1 GUIDE 2 -44 A LAP BELT ASSEMBLY, CREW SEAT (#1108006, Pacific Scientific Co., Anaheim, Calif.) 2 -45 50876 BOLT (AN4-6A) 2 -46 40111-21 BUSHING 2 -47 58760 WASHER (AN960-416) 2 -48 NUT (MS20364-428) 2 A. When Ordering Upholstery Parts Always Include Finish & Trim Number (See Page (v) For Instructions) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 71 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 22. Aft Divan Assembly ISSUED: May 1972 72 Model 112 Rockwell International General Aviation Division AFT DIVAN ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGO SERIAL NO'S AFFECTED 22-1 49032-1 E AFT DIVAN ASSEMBLY, Low Back with Headrest i One & Up 49032-501 E AFT DIVAN ASSEMBLY, Low Back with Headrest and Inertia Shoulder Harness i 49032-503 E AFT DIVAN ASSEMBLY, Low Back i 49032-505 E AFT DIVAN ASSEMBLY, Low Back with Inertia Shoulder Harness i -2 49035-3 AE SHROUD - Seat Back, Low Back, L.H. i 49035-4 AE SHROUD - Seat Back, Low Back, R.H. i -3 B PLUG BUTTON (#SS-51338, United Carr, Cambridge, Mass.) 4 -4 CE REEL ASSEMBLY (#0107129, Pacific Scientific Co., Anaheim Calif.) 2 -5 49042-1 D HEADREST ASSEMBLY, Low Back Seat 2 -6 49042-3 CUSHION - Headrest -7 E COVER ASSEMBLY - Headrest 2 -8 49250-1 D BUSHING - Headrest 4 -9 49032-7 CUSHION - Seat Bottom, L.H. 1 49032-8 CUSHION - Seat Bottom, R.H. 1 -10 E COVER ASSEMBLY - Seat Bottom 2 -11 49041-1 CUSHION ASSEMBLY - Seat Back 2 -12 49081-1 GUIDE 2 -13 E COVER ASSEMBLY - Seat Back 2 A. Used Only With 49032-1, 49032-501, 49032-503, 49032-505 B. Used Only With 49032-503 , 49032-505 C. Used Only With 49032-501, 49032-505 D. Used Only With 49032-1, 49032-501 E. When Ordering Upholstery Parts Always Include Finish & Trim Number (See Page (v) For Instructions) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 73 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION II Fuselage Group AFT DIVAN ASSEMBLY FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER CODE NOMENCLATURE REDD AFFECTED 22-14 49047-1 A CUSHION - Divider i One & Up -15 AC COVER - Divider i -16 49048-1 A CUSHION - Armrest i -17 AC COVER - Armrest i -18 49224-1 TORQUE TUBE 2 49225-1 PIN ASSEMBLY - Seat Stop 4 -19 49226-1 PIN ASSEMBLY - Seat Stop 4 -20 49227-1 LINK ASSEMBLY - Seat Stop, Weldment 4 -21 65084 CLEVIS PIN (MS20392-1C7) 4 -22 65745 COTTER PIN (MS24665-132) 4 -23 63236 SPRING (E-240-031-225 Associated Spring -24 Corp., Conn.) 4 58720 WASHER (AN960-6) 4 -25 60158 BEARING (F-257, Bond Brooke Bearing Corp., Bond Brooke, N.J.) 8 -26 62332 ROLL PIN (#59-012-062-0500, Elastic Stop Nut Div., Union, N.J.) 4 -27 65093 CLEVIS PIN (MS20392-1C23) 4 -2fL 58720 WASHER (AN960-6) 4 -29 A2327 COTTER PIN (MS24665-132 4 -30 40111-53 BUSHING 4 -31 65075 NUT (MS20364-1032) 4 -32 58740 WASHER (AN960-10) 8 -33 BOLT (AN23-23) 4 -34 62109 HANDLE (#4O7P2K1, Raytheon, Burlington, Mass 2 -35 49082-1 GUIDE 2 -36 40111-75 B BUSHING 2 -37 51750 B BOLT (AN5-17A) 2 -38 B NUT (MS20364-524) 2 -39 58790 B WASHER (AN960-616) 4 -40 50200 BOLT (AN3-14) 2 -41 58750 WASHER (AN960-10L) 2 -42 50000 BOLT (AN3-4) 4 -43 58740 WASHER (AN960-10) 4 A. Used Only With, 49032-1, 49032-501, 49032-503, 49032-505, 49032-507 B. Used Only With 49032-501, 49032-505 C. When Ordering Upholstery Parts Always Include Finish & Trim Number (See Page (v) For Instructions) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 74 Model 112 e Rockwell International General Aviation Division AFT DIVAN ASSEMBLY SECTION II Fuselage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQTD SERIAL NOS AFFECTED 22-44 -45 -46 -47 -48 -49 59460 51026 40111-21 58760 A NUT (#A4972-6-02, ESNA Corp.) LAP BELT ASSEMBLY, AFT DIVAN (#1108006 Pacific Scientific Co. Anaheim, Calif.) BOLT (AN 4-14A) NUT (MS20364-428) BUSHING WASHER (AN960-416) 4 2 4 4 4 4 One & Up A. When Ordering Upholstery Parts Always Include Finish & Trim Number (See Page (v) For Instructions) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 75 Model 112 From RareAviation.com * Rockwell International General Aviation Division (fig. I INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REG SERIAL NOS AFFECTED 1 | THIS PAGE INTENTIONALLY LEFT BLANK |When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1072 76 Model 112 SECTION EMPENNAGE GROUP From RareAviation.com 77 Section III EMPENNAGEGROUP Rockwell International General Aviation Division Figure 23. Tail Surfaces Installation ISSUED: May 1972 78 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION III Empennage Group TAIL SURFACES INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NO'S AFFECTED TAIL SURFACES INSTALLATION One & Up 23-1 44002-1 HORIZONTAL STABILIZER ASSEMBLY i -2 44003-1 UPPER FIN ASSEMBLY i -3 50851 BOLT (AN4-5A) 3 -4 50876 BOLT (AN4-6A) 5 -5 50902 BOLT (AN4-7A) 4 -6 58770 A WASHER (AN960-416L) As Req. -7 58760 A WASHER (AN960-416) As Req. -8 A2172 NUT (MS20365-428) 13 -9 62316 PLUG (BPF-1, Caplug Corp, or 413, Niagra Plastic) 2 -10 44233-1 RUDDER TIP ASSEMBLY 1 43360-1 DORSAL ASSEMBLY, Fairing Aft 1 -11 43360-3 DORSAL 1 -12 65547 NUTPLATE (MS21047-L08) 5 -13 65760 SCREW (MS24693-49) 38 -14 59636 SCREW (AN507-832R7) 13 -15 63968 WASHER (A3135.017-1, Tinnerman) 33 -16 59515 NUT (RM52LHA4972-6-82, Esna) 13 -17 59485 NUT (C8104-832, Tinnerman) 30 -18 44006-1 RUDDER ASSEMBLY 1 -19 44017-1 ELEVATOR ASSEMBLY, L.H. 1 -20 44017-2 ELEVATOR ASSEMBLY, R.H. 1 -21 44245-1 BOLT 1 -22 50825 BOLT (AN4-4A) 4 -23 50900 BOLT (AN4-7) 1 -24 50975 BOLT (AN4-12) 3 -25 56626 SCREW (AN525-10-8) 12 -26 58760 WASHER (AN960-416) 11 -27 58770 WASHER (AN960-416L) 1 -28 58750 WASHER (AN960-10L) 12 -29 58860 WASHER (AN970-4) 2 -30 A2167 NUT (MS20365-1032) 12 -31 54400 NUT (AN310-4) 6 A - MAXIMUM OF 3 WASHERS PERMISSIBLE When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 79 Model 112 * Rockwell International General Aviation Division SECTION III Empennage Group TAIL SURFACES INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REW SERIAL NOS AFFECTED 23-32 55675 COTTER PIN (AN380-2-2) 6 One & Up -33 60156 BEARING (AA347-3, Oilite) 1 -34 60152 BEARING (AA335-6, Oilite) 3 -35 40111-7 BUSHING 2 44214-1 HORN ASSEMBLY 1 -36 44271-1 HORN 1 -37 44275-1 ARM 1 -38 60159 BEARING (FF310-3, Oilite) 1 -39 BOLT (AN4-6A) 3 -40 WASHER (AN960-416) 3 -41 NUT (MS20365-428) 3 -35 43367-9 STINGER ASSEMBLY 1 -42 43367-11 STINGER 1 -43 43376-1 LENS 1 -44 40111-69 BUSHING 1 -45 59715 SCREW (AN515-8R40) 1 -46 587 1 8 WASHER (AN960-8) 1 -47 63960 WASHER (A3135-.017-24A) 12 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 80 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RECTO SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 81 Model 112 * Rockwell International General Aviation Division 17 ISSUED: May 1972 Figure 24. Upper Fin Assembly 82 Model 112 From RareAviation.com Rockwell International General Aviation Division UPPER FIN ASSEMBLY SECTION III Empennage Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 44003-1 UPPER FIN ASSEMBLY i One & Up 44215-1 SPAR ASSEMBLY - Upper Rear i 24-1 44215-3 SPAR i -2 44284-1 DOUBLER i -3 44216-1 FIN SKIN - Upper i -4 44217-1 SKIN - L.E. i -5 44218-1 RIB - L. E. i -6 44219-3 RIB - Tip i 44220-11 FIN TIP ASSEMBLY i -7 44220-3 FIN TIP i -8 59629 SCREW (AN507-832R4) 10 -9 63968 WASHER (A3135.017-1, Tinnerman) 10 -10 59493 NUT (C8107-832, Tinnerman) 10 -11 44221-1 RIB - Canted 1 -12 65544 NUTPLATE (MS21055-L4) 2 -13 44264-1 DOUBLER - Forward, Spar 1 44265-1 HINGE ASSEMBLY - Upper Fin 1 -14 44265-3 HINGE 1 -15 60151 BEARING (FF-411-1, Ollite) 1 -16 50026 BOLT (AN3-5A) 4 -17 50051 BOLT (AN3-6A) 2 -18 58740 WASHER (AN960-10) 4 -19 58750 WASHER (AN960-10L) 4 -2C A2167 NUT (MS20365-1032) 2 -21 65543 NUTPLATE (MS21047-L3K) 6 -22 44266-1 CLIP - L. E. 1 -23 44269-1 RIB - Skin Support 1 -24 44270-1 DOUBLER - Fin Skin 2 -25 44206-3 FILTER-Fin Tip 1 -26 44301-1 DOUBLER-Upper Fin Leading Edge 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 83 Model 112 Rockwell International General Aviation Division ISSUED: May 1972 Figure 25. Lower Fin Assembly 84 Model 112 From RareAviation.com Rockwell International General Aviation Division SECTION III Empennage Group LOWER FIN ASSEMBLY FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 25- -1 -2 -3 -4 -5 -6 -7 -8 44004-3 43255-1 44222-501 44223-3 44224-1 44224-3 44240-1 44240-2 44268-1 44268-2 44225-3 44225-4 44316-1 LOWER FIN ASSY FITTING Front Spar to Stabilizer RIB UPPER - Lower Fin (replaces p/n 44222-3) SPAR - Forward Lower Fin SPAR ASSY - Lower Rear Fin WEB FITTING - Rear Spar to Stabilizer, L.H. FITTING - Rear Spar to Stabilizer, R.H. CAP - Fin Spar, L.H. CAP - Fin Spar, R.H. SKIN - Lower Fin, L.H. SKIN - Lower Fin, R.H. FITTING - Front Spar to Stabilizer i i i i i i i i i i i 1 i One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 85 Model 112 e Rockwell International General Aviation Division ISSUED: May 1972 Figure 26. Rudder Assembly 86 Model 112 From RareAviation.com e Rockwell International General Aviation Division RUDDER ASSEMBLY SECTION III Empennage Group FIG. & INDEX PART NO. SERIAL NOS NO. NUMBER CODE NOMENCLATURE REGD AFFECTED 44006-1 RUDDER ASSEMBLY i One & Up 26-1 40113-1 SHIM - Rudder 2 -2 44228-3 SPAR - Rudder 1 -3 44229-3 SKIN - Rudder 1 -4 44231-1 ROOT RIB - Rudder 1 44232-1 HORN ASSEMBLY - Rudder 1 -5 44278-1 HORN WELDMENT 1 44283-1 ARM ASSEMBLY - Rudder Horn 1 -6 44283-3 ARM 1 -7 59383 BEARING (191. -. 125 Bound Brook) 2 -8 50851 BOLT (AN4-5A) 2 -9 58770 WASHER (AN 960-416L) 2 -10 A2172 NUT (MS20365-428) 2 -11 44254-3 FITTING - Upper Rudder 1 -12 44318-1 DOUBLER - Rudder 2 -13 44319-1 RIB - Rudder Tip 1 -14 44320-1 BALANCE WEIGHT - Rudder 1 -15 50001 BOLT (AN3-4A) 4 -16, 51026 BOLT (AN4-14A) 1 -17 58740 WASHER (AN960-10) 4 -18 58770 WASHER (AN960-416L) 1 -19 58860 WASHER (AN970-4) 1 -20 65071 NUT (MS20364-428) 1 -21 A2167 NUT (MS20365-1032) 4 -22 59515 NUT (RM52LHA4972-6-82) 14 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 87 Model 112 Rockwell International General Aviation Division Figure 27. Horizontal Stabilizer Assembly ISSUED: May 1972 88 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION III Empennage Group HORIZONTAL STABILIZER ASSEMBLY FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. RECTD SERIAL NO'S AFFECTED 44002-3 HORIZONTAL STABILIZER ASSEMBLY i One & Up 27-1 44201-5 SPAR - Stabilizer Rear i -2 44203-3 SPAR - Stabilizer Forward 2 -3 44204-1 LEADING EDGE - Horizontal Stabilizer 2 -4 44205-3 RIB - Leading Edge, B. L. 4. 80 2 -5 44207-3 ROOT RIB - Stabilizer, L. H. 1 44207-4 ROOT RIB - Stabilizer, R. H. 1 -6 44208-3 SPLICE PLATE - Stabilizer 2 -7 44226-9 DOUBLER - Horizontal Stabilizer 2 -8 44226-11 DOUBLER - Horizontal Stabilizer 2 -9 44226-13 DOUBLER - Horizontal Stabilizer 2 -10 44235-3 SKIN - Upper Center Stabilizer 1 -11 44236-3 SKIN - Lower Center Stabilizer 1 44257-1 FITTING ASSEMBLY - Horizontal Stabilizer, L. H. 1 44257-2 FITTING ASSEMBLY - Horizontal Stabilizer, R. H. 1 -12 44257-3 FITTING - Horizontal Stabilizer, L. H. 1 44257-4 FITTING - Horizontal Stabilizer, R. H. 1 -13 60151 BEARING (FF-411-1, Oilite) 2 -14 44261-5 SPLICE - Forward Spar 1 -15 44262-3 RIB - Stabilizer, B.L. 69.35 1 44262-4 RIB - Stabilizer, B.L. 69.35 1 44263-1 FITTING ASSEMBLY - Stabilizer To Elevator, L. H. 1 44263-2 FITTING ASSEMBLY - Stabilizer To Elevator, R. H. 1 -16 44263-3 FITTING - Stabilizer To Elevator 2 -17 60184 BEARING (F316G, Compo 66H, Bound Brook) 2 -18 44304-3 DOUBLER - Spar, Stabilizer 1 44306-1 RIB - Stabilizer, B.L. 23.58, L. H. 1 44306-2 RIB - Stabilizer, B.L. 23.58, R.H. 1 -19 44306-3 RIB - Stabilizer, B.L. 23.58, L. H. 1 44306-4 RIB - Stabilizer, B.L. 23.58, L. H. 1 -20 47532-7 BRACKET 2 -21 44307-3 RIB - Stabilizer, B.L. 35.37, L. H. 1 44307-4 RIB - Stabilizer, B.L. 35.37, R.H. 1 -22 44308-3 RIB - Stabilizer, B.L. 47.16, L. H. 1 44308-4 RIB - Stabilizer, B.L. 47.16, R.H. 1 -23 44309-3 RIB - Stabilizer, B.L. 58.95, L. H. 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 89 Model 112 Rockwell International General Aviation Division SECTION III Empennage Group HORIZONTAL STABILIZER ASSEMBLY FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NOS AFFECTED 44309-4 RIB - Stabilizer, B.L. 58.95, R.H. i One & Up 27-24 44311-3 COVER - Access, Stabilizer 2 -25 44312-5 SKIN - Stabilizer, L. H. 1 44312-6 SKIN - Stabilizer, R. H. 1 -26 44312-7 SKIN - Stabilizer, L. H. 1 44312-8 SKIN - Stabilizer, R. H. 1 44313-1 HINGE ASSEMBLY - Elevator Center, L. H. 1 44313-2 HINGE ASSEMBLY - Elevator Center, R.H. 1 -27 44313-3 HINGE - Elevator Center 2 -28 60184 BEARING (F316G, Compo 66H, Bound Brook) 2 -29 44314-3 SUPPORT - Hinge, Stabilizer 1 44314-4 SUPPORT - Hinge, Stabilizer 1 47527-1 BRACKET ASSEMBLY - Elevator Trim 1 -30 47527-3 BRACKET - Elevator Trim 1 -31 47527-5 ANGLE - Elevator Trim 3 -32 47527-7 BRACKET - Elevator Trim 1 -33 50051 BOLT (AN3-6A) 8 -34 50851 BOLT (AN4-5A) 8 -35 SCREW (AN525-832-6) 8 -36 58740 WASHER (AN960-10) 8 -37 58750 WASHER (AN960-10L) 4 -38 58780 WASHER (AN960-416L) 8 -39 A2172 NUT (MS20365-428) 8 -40 A2167 NUT (MS20365-1032) 4 -41 NUT PLATE (MS21053-L3) 4 -42 NUT PLATE (22NAI-048, Esna Corp. ) 2 -43 NUT PLATE (C8107-832, Tinnerman ) 8 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 90 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG.& INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 91 Model 112 e Rockwell International General Aviation Division Figure 28. Elevator and Trim Tab Assembly ISSUED: May 1972 92 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION III Empennage Group ELEVATOR & TRIM TAB ASSEMBLY FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REGD SERIAL NOS AFFECTED 44017-1 ELEVATOR ASSEMBLY, L. H. i One & Up 44017-2 ELEVATOR ASSEMBLY, R.H. i 44020-1 TRIM TAB ASSEMBLY - Elevator, L. H. i 44020-2 TRIM TAB ASSEMBLY - Elevator, R. H. i 28-1 44020-3 SKIN - Trim Tab, L. H. i 44020-4 SKIN - Trim Tab, R. H. i -2 44020-5 HINGE HALF - Elevator Trim Tab 4 -3 44020-7 HINGE PIN - Elevator Trim Tab 2 -4 40141-1 SHIM 4 -5 44336-3 RIB - Elevator Trim Tab 2 -6 44337-3 HORN - Elevator Trim Tab 2 -7 55599 NUT (AN365-1032) 4 -8 56631 SCREW (AN525-10-16) 2 -9 SCREW (AN525-10-24) 2 -10 58770 WASHER (AN960-416L) 4 44211-7 SPAR ASSEMBLY - Elevator Fwd., L. H. 1 44211-8 SPAR ASSEMBLY - Elevator Fwd., R.H. 1 -11 44211-9 SPAR - Elevator, L. H. 1 44211-10 SPAR - Elevator, R.H. 1 -12 44211-11 DOUBLER - Elevator Spar, L. H. 1 44211-12 DOUBLER - Elevator Spar, R.H. 1 -13 44285-1 FITTING - Elevator Forward Spar 2 -14 44322-3 BALANCE WEIGHT - Elevator 2 44323-1 SKIN ASSEMBLY - Elevator, L. H. 1 44323-2 SKIN ASSEMBLY - Elevator, R. H. 1 -15 44323-11 SKIN - Elevator, L. H. 1 44323-12 SKIN - Elevator, R.H. 1 -16 44323-13 DOUBLER - Elevator 2 -17 44324-3 TIP - Elevator 2 -18 44325-3 RIB - Elevator, B.L. 39.60 2 -19 44326-3 RIB - Elevator, B.L. 23. 482 2 -20 44327-3 SPAR - Elevator, Aft 2 -21 44328-3 RIB - Elevator, B.L. 56.25 2 -22 44329-3 RIB - Elevator, B.L. 73.78 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 93 Model 112 e Rockwell International General Aviation Division SECTION III Empennage Group ELEVATOR & TRIM TAB ASSEMBLY FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDO SERIAL NO'S AFFECTED 28-23 -24 -25 -26 -27 -28 -29 -30 -31 -32 -33 -34 -35 -36 44330-3 44331-3 44332-3 44333-3 44335-3 50026 51440 59636 58750 58770 A2172 A2167 59493 RIB - Elevator, B.L. 73.78, Aft RIB - Elevator, B.L. 70.75 RIB - Elevator, Root HINGE - Elevator, Center SKIN - Elevator Balance BOLT (AN3-5A) BOLT (AN4-34A) SCREW (AN507-832R7) WASHER (AN960-10L) WASHER (AN960-416L) NUT (MS20365-428) NUT (MS20365-1032) WASHER (A3135-. 017-1 Tinnerman) NUT (C 8107-832 Tinnerman) 2 2 2 4 2 8 2 36 16 4 2 8 36 36 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 94 Model 112 From RareAviation.com SECTION J FUEL SYSTEM GROUP Section IV FUEL SYSTEM GROUP From RareAviation.com * Rockwell International General Aviation Division Figure 29. Fuel System Installation ISSUED: May 1972 96 Model 112 Rockwell International General Aviation Division SECTION IV Fuel System Group FUEL SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 29-1 46001-1 46094-3 FUEL SYSTEM INSTALLATION - Engine Compart- ment GASCOLATOR i i One & Up -2 48216-1 AUXILIARY FUEL PUMP ASSEMBLY i -3 50826 BOLT (AN4-4A) 2 -4 58760 WASHER (AN960-416) 2 -5 A2172 NUT (MS20365-428) 2 -6 46099-41 FUEL LINE ASSEMBLY 1 -7 46099-70 FUEL LINE ASSEMBLY 1 -8 46136-1 HOSE ASSEMBLY 1 -9 46136-7 HOSE ASSEMBLY 1 -10 46189-1 SUPPORT-Clamp 1 -11 46190-1 SCREW 2 -12 57420 CLAMP (AN742-12) 1 -13 57568 UNION (AN815-6) 2 -14 P7575 NIPPLE (AN816-6-2) 1 -15 61403 NIPPLE (C3069X4X2, Weatherhead Co.) 1 -16 61402 ELBOW (C5405X8X4, Weatherhead Co.) 1 -17 58038 ELBOW (AN833-6) 1 -18 58399 NUT (AN924-6) 1 -19 65945 GASKET (MS29512-06) 2 -20 59689 SCREW (AN526-1032-7) 1 -21 55602 NUT (AN365-1032C) 1 48501-1 FUEL SYSTEM INSTALLATION - Cabin & Wings 1 -22 46099-1 FUEL LINE-Fuselage, Console 1 -23 46099-3 FUEL LINE-Fuselage, L.H. 1 46099-4 FUEL LINE-Fuselage, R.H. 1 -24 46099-5 FUEL LINE-Wing 2 -25 46099-7 FUEL LINE-Drain 1 48514-1 FILLER CAP ASSEMBLY 2 -26 48522-1 MOULDING 2 -27 O-RING (MS29513-012) 2 -28 63328 STUD (2600SW-22, Camloc) 2 -29 63959 RETAINER (2600LW, Camloc) 2 -30 48528-1 STRAINER ASSEMBLY 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 97 Model 112 From RareAviation.com Rockwell International General Aviation Division SECTION IV Fuel System Group FUEL SYSTEM INSTALLATION FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER GODE NOMENCLATURE REDD AFFECTED 29-31 48513-1 SEAL 2 One & Up -32 FUEL SELECTOR ASSEMBLY (A-400-1 Gerdes) 1 -33 50075 BOLT (AN3-7) 3 -34 56844 SCREW (AN526-1032-8) 5 -35 56870 SCREW (AN526-1032-12) 2 -36 56880 SCREW (AN526-1032-14) 1 -37 57575 UNION (AN815-8D) 2 -38 57585 NIPPLE (AN816-2D) 1 -39 57605 NIPPLE (AN816-4D) 1 -40 57640 NIPPLE (AN816-8D) 1 -41 A1421 UNION (AN832-8) 1 -42 58409 NUT (AN924-8) 1 -43 58750 WASHER (AN960-10L) 6 -44 A2167 NUT (MS20365-1032) 6 -45 A2231 ELBOW (MS20823-8D) 2 -46 66155 GROMMET (MS35489-155) 2 -47 65725 CLAMP (MS21919DG8) 8 -48 68244 SPACER (NAS43DD3-10) 2 -49 SPACER (NAS43DD3-16) 2 -50 68245 SPACER (NAS43DD3-28) 1 -51 59382 BUSHING (SB437-4 Heyco) 1 -52 59413 BUSHING (SB437-5 Heyco) 1 -53 60268 BUSHING (P20-3 Bearing & Drives Inc.) 3 -54 NUT MOS Molly Co.) 2 -55 KNOB ASSEMBLY (A 1030 Gerdes) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 98 Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 99 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 30. Primer and Vent Line System Installation ISSUED: May 1972 100 Model 112 e Rockwell International General Aviation Division SECTION IV Fuel System Group PRIMER & VENT LINE SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 46012-1 PRIMER SYSTEM INSTALLATION i One & Up 30-1 46099-19 TUBE ASSEMBLY - Console i -2 46099-21 TUBE ASSEMBLY - Aft, Firewall i -3 46099-23 TUBE ASSEMBLY - Forward, Firewall i -4 P5236 PRIMER PUMP (K-2402-2, Kohler Co.) i -5 57999 UNION (AN832-2) i -6 P0264 WASHER (AN960-516) i -7 58369 NUT (AN924-2) i -8 65674 CLAMP (MS21919-2) i -9 68242 SPACER (NAS43DD3-24) i -10 56623 SCREW (AN520-10R13) i -11 65076 NUT (MS20365-1032C) i -12 65674 CLAMP (MS21919-2) i 59690 SCREW (AN520-10R7) i 65076 NUT (MS20365- 1032C) i 48509-1 VENT LINE SYSTEM INSTALLATION i -13 48524-1 VENT LINE ASSEMBLY, L.H. - Center i 48524-2 VENT LINE ASSEMBLY, R. H. - Center i -14 48525-1 VENT LINE ASSEMBLY, L.H. - Inboard i 48525-2 VENT LINE ASSEMBLY, R.H. - Inboard i -15 48526-1 VENT LINE ASSEMBLY - BL 0.0 i -16 57567 UNION (AN815-6D) 2 -17 57970 TEE (AN824-6D) 1 -18 59386 BUSHING (SB562-6, Heyco) 1 -19 65660 CLAMP (MS21919DG6) 2 -20 56841 SCREW (AN526-1032-4) 4 -21 58750 WASHER (AN960-10L) 4 -22 A2167 NUT (MS20365-1032) 4 -23 48819-1 CLIP 2 -24 48518-1 TUBE ASSEMBLY - Tank 2 -25 46099-25 TUBE ASSEMBLY - L.H. 1 -26 46099-26 TUBE ASSEMBLY - R.H. 1 -27 59382 BUSHING (SB-437-4, Heyco) 4 -28 59412 BUSHING (OCB-875-7, Heyco) 4 -29 A1346 NIPPLE (AN816-6D) 6 -30 57604 NIPPLE (AN816-4-4D) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 101 Model 112 From RareAviation.com * Rockwell International General Aviation Division Figure 31. Gascolator and Fuel Pump Installation 102 ISSUED: May 1972 Model 112 Rockwell International General Aviation Division SECTION IV Fuel System Group GASCOLATOR & FUEL PUMP ASSEMBLY FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NO'S AFFECTED 31-1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 46094-1 61098 P6499 P5520 P4113 P4526 P3533 61123 48216 63683 P5288 P3966 P4128 GASCOLATOR ASSEMBLY - Fuel COVER (500 BP, Kern Mfg. Co.) WIRE BAIL (No. 8, Latour) SCREEN (130P, Kern Mfg. Co.) GASKET - Coprene (No. 8, Latour) GLASS BOWL (No. 8, Latour) CASTING - Bottom (No. 8, Latour) DRAIN VALVE (CAV-UOH-4, Saf-Air Co.) AUXILIARY FUEL PUMP ASSEMBLY QUICK DISONNECT (32448, Amp, Inc.) FUEL PUMP (478360, Bendix Corp.) FILTER - Screen (479135, Bendix Corp.) GASKET - Cover (479136, Bendix Corp.) i i i i 2 1 1 1 1 1 1 1 1 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 103 Model 112 From RareAviation.com Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REW SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 104 Model 112 SECTION POWER PLANT GROUP From RareAviation.com Section V POWER PLANT GROUP 105 Rockwell International General Aviation Division Figure 32. Power Plant Installation Changed January 1978 106 Model 112 From RareAviation.com Rockwell International General Aviation Division POWER PLANT INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 32- -1 46300-1 HC-E2Y(K,R) -1B/7666A DRAWING - Power Plant Installation PROPELLER ASSY (Mfg by Hartzell - alt p/n HC- E2YR-1BF/F7666A) 1 One & Up -2 46390-3 SPINNER ASSY (Mfg by Glode - 4 63 90-3 P-poll shed) i -3 46102-503 TUBE - Engine Breather (ATTACHING PARTS) i -4 A2980-A12 CLAMP 2 -5 AN520-10R8 MS20365-1032C SCREW NUT * 2 2 -6 46092-15 HOSE - Electric Fuel Pump Drain 1 -7 46092-7 HOSE - Crankcase Fuel Drain 2 -8 46092-9 HOSE - Mechanical Fuel Pump Drain (ATTACHING PARTS) 1 -9 SAE #8 CLAMP 2 -10 46092-13 HOSE - Crankcase Oil Drain (ATTACHING PARTS) 1 -11 SAE #14 CLAMP 2 -12 46092-11 HOSE - Crankcase Breather (ATTACHING PARTS) 1 -13 GS8 Type F 46304-1 CLAMP (Mfd by Murray Corp.) * ENGINE BUILDUP 2 REF -14 46005-3 ENGINE ASSY (Mfg by Lycoming p/n IO-360-C1D6) 1 -15 46201-3 GOVERNOR ASSY - Propeller 1 -16 46309-1 MOUNT ASSY - Engine and Nose Gear (ATTACHING PARTS) 1 -17 AN6-22A BOLT 4 -18 AN6-45A AN960-616L MS20365-624C BOLT WASHER NUT * 1 10 5 -19 46050-17 AIR DUCT - Tabulated (ATTACHING PARTS) 1 -20 102100 CLAMP (Mfg by Murray Corp.) * 2 -21 HDLF VALVE - Oil Drain (Mfg by Handy Drain) (alt p/n BJ1000AH-4V Mfg by Auto Valve,Inc.) 1 -22 Q-22440 FUEL DRAIN (Mfg by Q-E Manufacturing Co.) 1 -23 J-12334-1 DAMPER (Mfg by Lord Manufacturing Co.) 2 -24 J-2218-61 WASHER (Mfg by Lord Manufacturing Co.) 6 -25 J-7763-1 MOUNT (Mfg by Lord Manufacturing Co.) 4 -26 J-9612-8 MOUNT (Mfg by Lord Manufacturing Co.) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 107 Model 112 Rockwell International General Aviation Division POWER PLANT INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 32-27 Y-16440-2-148 SPACER (Mfg by Lord Manufacturing Co.) 2 One & Up (ATTACHING PARTS) -28 AN7-43 BOLT 2 -29 AN7-44 BOLT 2 AN960-716 WASHER 4 AN310-7 NUT 4 AN380-3-3 PIN - Cotter 4 * -30 AN815-6 UNION 1 -31 AN816-6 NIPPLE 1 -32 MS29512-06 GASKET 2 -33 AN833-6 ELBOW 1 -34 AN924-6 NUT 1 46011-1 OIL COOLER INSTL REF -35 46194-3 OIL COOLER 1 (ATTACHING PARTS) AN3-4 BOLT 8 AN960-10L WASHER 8 MS20365-1032C NUT 8 * -36 40111-3 BUSHING - Grip 4 (ATTACHING PARTS) -37 AN3-41 BOLT 4 AN960-10 WASHER 4 MS20365-1032C NUT 4 * 46196-1 ADAPTER ASSY - Oil Cooler 1 (ATTACHING PARTS) -38 No Number SCREW (#8 sheet metal Type A Truss Head 0.50 in.long) 4 * -39 46046-15 SEAL 2 -40 46197-1 ADAPTER 1 -41 46136-3 HOSE ASSY 1 -42 46136-5 HOSE ASSY 1 (ATTACHING PARTS) -43 C3046A-18-92 CLAMP (Mfg by Tinnerman Products Corp.) 2 -44 AN526-1032R10 SCREW 1 MS20365-1032C NUT 1 * -45 46188-1 BRACKET (ATTACHING PARTS) -46 C3046A-12-92 CLAMP (Mfg by Tinnerman Products Corp.) 1 -47 AN520-10R8 SCREW 1 MS20365-1032C NUT 1 * -48 AN816-8 NIPPLE 1 -49 MS20823-8D FITTING 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 108 Model 112 From RareAviation.com e Rockwell International General Aviation Division POWER PLANT INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 32-50 -51 -52 -53 MS20823-8 46078-1 AN3-5A AN3-7A AN960-10 MS20365-1032C ELBOW EXTENSION - BOLT BOLT WASHER NUT * Mixture Control (ATTACHING PARTS) i REF 1 1 2 2 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 109 Model 112 Rockwell International General Aviation Division Figure 33. Engine and Cowl Flap Controls Installation (Sheet 1 of 4) 110 Model 112 Changed January 1978 From RareAviation.com Figure 33. Engine and Cowl Flap Controls Installation (Sheet 2 of 4) Changed January 1978 110A Model 112Rockwell International General Aviation Division F X42 41A Figure 33. Engine and Cowl Flap Controls Installation (Sheet 3 of 4) Changed January 1978 110B Model 112 From RareAviation.com Rockwell International General Aviation Division G X42 7 Figure 33. Engine and Cowl Flap Controls Installation (Sheet 4 of 4) Changed January 1978 HOC Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED[this page intentionally left blank IWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 110D Model 112 From RareAviation.com e Rockwell International General Aviation Division ENGINE & COWL FLAP CONTROLS INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGO SERIAL NO'S AFFECTED 33- 46302 46115-1 ENGINE CONTROLS INSTL QUADRANT ASSY L INSTL REF REF One & Up -1 46116-1 THROTTLE ASSY 1 -2 46117-501 LEVER - Propeller 1 -3 46133-3 LEVER - Mixture 1 -4 46133-1 LEVER - Carburetor Heat (ATTACHING PARTS) 1 -5 46134-1 BOLT 1 -6 46211-1 HANDLE * 1 -7 46127-1 PLATE - Friction 8 -8 46126-1 SPACER 1 -9 46126-3 SPACER 1 -10 46126-5 SPACER 2 -11 46211-3 BUSHING 1 -12 46212-1 ROD (ATTACHING PARTS) 1 -13 P18843 NUT (Mfg by Crest Products, Inc.) * 2 -14 46206-1 KNOB - Carburetor Heat 1 -15 46208-1 KNOB - Propeller 1 -16 46209-1 KNOB - Mixture (ATTACHING PARTS) 1 -17 MS24693C27 SCREW * 3 -18 46207-1 KNOB - Throttle (ATTACHING PARTS) 1 -19 MS24693C27 46135-509 SCREW * CONTROL CABLE ASSY - Throttle (ATTACHING PARTS) 1 1 -20 MS20365-1032C NUT 2 -21 RA1039-ZN CLAMP 1 -22 AN520-416-10 MS20365-428C SCREW NUT 1 1 -23 56525-031 CLAMP 1 -24 AN526-832-10 MS20365-832C SCREW NUT 1 1 -25 A32010 CLAMP - Cable (Mfg by Morse Controls) 1 -26 A35777 SHIM (Mfg by Morse Controls) 1 -27 MS16998-10 MS20365-1032C SCREW NUT * 2 2 -28 46135-3 CABLE - Control (Mfg by American Chain & Cable Co.) 1 -29 HF-5 BALLJOINT (Mfg by Heim Universal) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 111 Model 112 Rockwell International General Aviation Division ENGINE & COWL FLAP CONTROLS INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. RECTO SERIAL NOS AFFECTED 33- 46135-509 CONTROL CABLE ASSY - Propeller i One & Up (ATTACHING PARTS) -30 MS20365-1032C NUT 2 -31 RA1039-ZN CLAMP 1 -32 AN520-416-10 SCREW 1 MS20365-428C NUT 1 -33 MS21919DG4 CLAMP 1 -34 AN3-14A BOLT 1 -35 40111-35 BUSHING 1 AN960-10 WASHER 1 MS20365-1032C NUT 1 -36 A32010 CLAMP - Cable (Mfg by Morse Controls) 1 -37 A35777 SHIM (Mfg by Morse Controls) 1 -38 MS16998-10 SCREW 2 MS20365-1032C NUT 2 -39 MS21919DG4 CLAMP 1 -40 MS21919DG12 CLAMP 1 -41 AN520-10-7 SCREW 1 MS20365-1032C NUT 1 * -42 46135-3 CABLE - Control (Mfg by American Chain & 1 Cable Co.) -43 HF-5 BALLJOINT (Mfg by Heim Universal) 2 46135-511 CONTROL CABLE ASSY - Mixture 1 (ATTACHING PARTS) -44 AN23-12 BOLT 1 AN310-3 NUT 1 MS24665-132 PIN - Cotter 1 -45 RAI 03 9- ZN CLAMP 1 -46 AN520-416-10 SCREW 1 MS20365-428C NUT 1 -47 MS21919DG4 CLAMP 1 -48 A32010 CLAMP - Cable (Mfg by Morse Controls) 1 -49 A35777 SHIM (Mfg by Morse Controls) 1 -50 MS216998-10 SCREW 1 MS20365-1032C NUT 1 -51 MS20365-1032C NUT 1 * -52 46135-5 CABLE - Control (Mfg by American Chain & 1 Cable Co.) -53 HF-5 BALLJOINT (Mfg by Heim Universal) 1 -54 MS35812-1 CLEVIS 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 112 Model 112 From RareAviation.com e Rockwell International General Aviation Division ENGINE & COWL FLAP CONTROLS INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 33- 46135-513 CONTROL CABLE ASSY - Alternate Air i One & Up (ATTACHING PARTS) -55 AN23-12 BOLT i AN310-3 NUT i MS24665-132 PIN - Cotter i -56 RA1039-ZN CLAMP i -57 AN520-416-10 SCREW i MS20365-428C NUT i -58 A32019 CLAMP - Cable (Mfg by Morse Controls) i -59 A35777 SHIM (Mfg by Morse Controls) i -60 MS216998-10 SCREW i MS20365-1032C NUT i -61 MS20365-1032C NUT i * -62 46135-7 CABLE - Control i -63 HF-5 BALLJOINT (Mfg. by Heim Universal) i -64 MS35812-1 CLEVIS i -65 46202-5 GROMMET - Firewall 2 -66 MT340 GROMMET HOLDER (Mfg by Arens Controls) 1 (ATTACHING PARTS) -67 AN520-10-5 SCREW 2 * -68 46202-5 GROMMET - Firewall 1 -69 46202-11 GROMMET - Firewall 1 -70 MT340 GROMMET HOLDER (Mfg by Arens Controls) 1 (ATTACHING PARTS) -71 AN520-10-5 SCREW 2 * -72 46202-3 GROMMET Firewall 3 -73 46227-1 GROMMET HOLDER 1 (ATTACHING PARTS) -74 AN520-10-5 SCREW 3 * -75 40111-11 BUSHING 2 46316-1 COWL FLAP CONTROL INSTL REF -76 46331-7 CABLE ASSY - Cowl Flap, LH 1 46331-5 CABLE ASSY - Cowl Flap, RH 1 (ATTACHING PARTS) -77 AN315-3R NUT 4 AN936-A10 WASHER 2 -78 A2980-A-12 CLAMP (Mfg by Tinnerman Products Corp.) 1 -79 MS21919DG4 CLAMP 1 -80 AN520-10R8 SCREW 1 MS20365-1032C NUT 1 -81 AN23-12 BOLT 1 AN960-10 WASHER 2 AN310-3 NUT 1 MS24665-132 PIN - Cotter 1 * When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 112A Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED[this page intentionally left blank IWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 112B Model 112 From RareAviation.com e Rockwell International General Aviation Division ENGINE & COWL FLAP CONTROLS INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REDO SERIAL NO'S AFFECTED 33-82 -83 -84 -85 -86 -87 -88 -89 -90 -91 MS35812-1 46331-9 AN315-3R AN936-A10 46353-1 AN515-8-8 MS20365-832 46326-1 46330-1 40111-43 AN526-1032-16 AN960-10 MS20365-1032 AN931-4-7 CLEVIS CABLE ASSY (ATTACHING PARTS) NUT WASHER * SHIELD (ATTACHING PARTS) SCREW NUT * LINK CLAMP BUSHING (ATTACHING PARTS) SCREW WASHER NUT * GROMMET 2 1 1 2 1 3 3 1 1 2 1 1 1 1 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 113 Model 112 e Rockwell International General Aviation Division Figure 34. Engine Instruments Installation Changed January 1978 114 Model 112 From RareAviation.com Rockwell International General Aviation Division ENGINE INSTRUMENTS INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGO SERIAL NO'S AFFECTED 34- -1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -24 -25 -26 46303-1 46100-1 MT342 AN526-1032R5 MS20365-1032C 46202-13 46320-1 AN919-0 MS21919DG6 46136-47 MS21919DG12 AN526-1032R8 MS20365-1032C AN837-3 AN924-3 AN960-616 46099-97 AN919-2 46099-13 46014-1 MS39326-8 C3046A-8-92 AN526-1032R8 MS20365-1032C AN839-4 AN924-4 AN960-716 46099-9 MS20822-4D- HXX 46319-1 C3046A-12-92 AN526-1032-R8 MS20365-1032C ENGINE INSTRUMENTS INSTL SHAFT ASSY - Tachometer HOLDER - Grommet (Mfgby Arens Controls, Inc.) (ATTACHING PARTS) SCREW NUT * GROMMET TUBE ASSY REDUCER CLAMP HOSE ASSY (ATTACHING PARTS) CLAMP SCREW NUT * ELBOW (ATTACHING PARTS) NUT WASHER * TUBE ASSY REDUCER TUBE ASSY HOSE (ATTACHING PARTS) CLAMP CLAMP (Mfg by Tinnerman Products, Inc.) SCREW NUT * ELBOW (ATTACHING PARTS) NUT WASHER * TUBE ASSY - Manifold Pressure Fuel Flow SNUBBER (Mfg by Chemiquip Products, Inc.) TUBE ASSY CLAMP (Mfgby Tinnerman Products, Inc.) SCREW NUT * REF 1 1 3 3 3 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 2 1 1 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 114A Model 112 Rockwell International General Aviation Division ENGINE INSTRUMENTS INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 34-27 AN919-0 REDUCER i One & Up -28 MS35489-20S GROMMET i -29 46136-27 HOSE ASSY i (ATTACHING PARTS) -30 MS21919DG12 CLAMP i -31 AN526-1032-R8 SCREW i MS20365-1032C NUT i * -32 AN837-3 ELBOW i (ATTACHING PARTS) -33 AN924-3 NUT i AN960-616 WASHER i * -34 AN894-32 EXPANDER i -35 46099-19 TUBE ASSY - Pressure i -36 AN816-2D NIPPLE 2 -37 AN833-2D ELBOW 1 (ATTACHING PARTS) -38 AN924-3D NUT 1 AN960-516 WASHER 1 * -39 46136-29 HOSE ASSY 1 (ATTACHING PARTS) -40 MS21919DG6 CLAMP 1 * -41 AN837-2 ELBOW 1 (ATTACHING PARTS) -42 AN924-2 NUT 1 AN960-516 WASHER 1 * -43 46099-19 TUBE ASSY - Vent 1 -44 MS35489-14S GROMMET 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1977 1148 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDO SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 115 Model 112 Rockwell International General Aviation Division Figure 35. Induction Air System Installation Changed January 1978 116 Model 112 From RareAviation.com Rockwell International General Aviation Division SECTION V Power Plant Group INDUCTION AIR SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGD SERIAL NOS AFFECTED 35- 46317-1 INDUCTION AIR SYSTEM INSTL REF One & Up -1 46007-3 ENGINE EXHAUST SYSTEM INSTL (see Figure 37) REF -2 46050-19 DUCT - Air (ATTACHING PARTS) 2 -3 102304 CLAMP (mfg by Murray Corp.) *_ __ 2 -4 46118-3 DUCT ASSY (ATTACHING PARTS) 1 -5 MS21919DG50 CLAMP 2 -6 AN526-1032R10 MS20365-1032C SCREW NUT * 2 2 -7 C3046A-16-92 CLAMP (Mfg by Tinnerman Products, Inc.) 1 -8 46050-23 DUCT - Air (ATTACHING PARTS) 1 -9 102322 46216-1 CLAMP (Mfg by Murray Corp.) * BOX ASSY - Air Filter (ATTACHING PARTS) 2 1 -10 S-033528-8 SCREW * 5 -11 46220-1 BOX 1 -12 AN526-832R8 SCREW 4 -13 8-832 WELLNUT (Mfg by USM Corp.) 4 -14 615045-501 46304-1 46348-3 FILTER - Air (Mfg by Filter Div. Rockwell International Corp.) ENGINE BUILDUP (see Figure 32) BOX ASSY - Induction Air (ATTACHING PARTS) 1 REF 1 -15 MS20074-04-30 AN960-416L 46383-1 BOLT WASHER * PAN ASSY - Upper (ATTACHING PARTS) 4 8 1 -16 AN526-632R5 SCREW 9 -17 AN526-632R6 AN960-4L MS20365-632C SCREW WASHER (under nut) NUT * 2 11 11 -18 46358-1 BRACKET ASSY 1 -19 46357-3 DOUBLER 1 -20 46059-1 PAN - Upper 1 -21 46384-1 SPACER 4 -22 46341-3 BELL ASSY 1 -23 46321-1 GASKET 1 -24 46043-5 VALVE ASSY 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 117 Model 112 4* Rockwell International General Aviation Division INDUCTION AIR SYSTEM INSTALLATION SECTION V Power Plant Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REQD SERIAL NOS AFFECTED 35- -25 -26 -27 -28 -29 -30 -31 -32 -33 -34 46039-5 46038-1 46036-1 AN931-6-16 6L6-F 46388-5 46347-1 46342-1 46042-3 46042-5 46046-9 46046-11 46046-13 46321-1 PLATE ASSY SEAL PLATE GROMMET BUSHING BRACKET PAN ASSY - Lower PAN - Lower TAKEOFF TAKEOFF SEAL SEAL SEAL GASKET i i i 2 2 1 1 1 1 1 1 1 1 1 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 118 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 119 Model 112 e Rockwell International General Aviation Division 4/Z Figure 36. Baffle Installation ISSUED: May 1972 120 Model 112 From RareAviation.com * Rockwell International General Aviation Division SECTION V Power Plant Group BAFFLE INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 46060-1 BAFFLE INSTALLATION BAFFLE ASSEMBLY - Left Front i One & Up 46063-1 BAFFLE ASSEMBLY - Right Front i 36-1 46064-1 BAFFLE - Right Front i -2 46061-1 BAFFLE - Left Front i -3 46085-1 COVER - Baffle 2 -4 46086-1 COVER - Baffle 2 -5 46062-17 SEAL 1 -6 46062-19 SEAL 1 -7 46122-1 SPRING - Flat 6 -8 46098-1 TAKEOFF 1 -9 46095-1 SCREEN 1 46065-1 BAFFLE ASSEMBLY - Left Side, Front 1 46067-1 BAFFLE ASSEMBLY - Left Side, Rear 1 46069-1 BAFFLE ASSEMBLY - Right Side, Front 1 46071-1 BAFFLE ASSEMBLY - Right Side, Rear 1 -10 46066-1 BAFFLE - Left Side, Front 1 -11 46068-1 BAFFLE - Left Side, Rear 1 -12 46070-1 BAFFLE - Right Side, Front 1 -13 46072-1 BAFFLE - Right Side, Rear 1 -14 46062-5 SEAL 1 -15 46062-7 SEAL 1 -16 46062-9 SEAL 1 -17 46062-11 SEAL 1 -18 46062-13 SEAL 1 -19 46062-15 SEAL 1 -20 46105-1 REINFORCEMENT 8 46074-1 BAFFLE ASSEMBLY - Right Rear 1 -21 46075-1 BAFFLE - Right Rear 1 -22 46108-1 RIGHT FIN BAFFLE - Right Rear 1 -23 46109-1 LEFT FIN BAFFLE - Right Rear 1 -24 46084-1 BRACKET - Right Rear Baffle 1 -25 46062-3 SEAL 1 46076-1 BAFFLE ASSEMBLY - Left Rear 1 -26 46077-1 BAFFLE - Left Rear 1 -27 46082-1 COVER - Baffle 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 121 Model 112 e Rockwell International General Aviation Division BAFFLE INSTALLATION SECTION V Power Plant Group FIG. & INDEX PA 07 NO. SERIAL NO'S NO. NUMBER CODE NOMENCLATURE REDO AFFECTED 36-28 46083-1 BRACKET - Baffle i -29 46106-1 BAFFLE - Engine i -30 46062-1 SEAL i 46123-1 BAFFLE ASSEMBLY - Front i -31 46124-1 BAFFLE - Front i -32 46125-1 SEAL i -33 46062-41 SEAL i -34 46062-43 SEAL i -35 46062-45 SEAL i -36 46062-47 SEAL i -37 46150-1 BRACKET - Front Baffle i -38 46107-1 BRACKET - Rear i -39 63240 SPRING (LEO37C-4, Lee Spring) 4 -40 50876 BOLT (AN4-6A) 1 -41 56596 SCREW (AN526-420-8) 12 -42 56837 SCREW (AN526-832-8) 24 -43 64999 CAP SCREW (MS16997-44) 1 -44 58770 WASHER (AN960-416L) 13 -45 58719 WASHER (AN960-8L) 40 -46 58722 WASHER (AN960-6L) 18 -47 66168 LOCK WASHER (MS35333-40) 12 -48 58750 WASHER (AN960-10L) 1 -49 AO398 NUT (MS20365-832) 24 -50 A2172 NUT (MS20365-428) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 122 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 123 Model 112 e Rockwell International General Aviation Division Figure 37. Engine Exhaust System Installation ISSUED: May 1972 124 Model 112 From RareAviation.com Rockwell International General Aviation Division SECTION V Power Plant Group ENGINE EXHAUST SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RECTD SERIAL NOS AFFECTED 46007-1 ENGINE EXHAUST SYSTEM INSTALLATION One & Up MUFFLER ASSEMBLY (#099005-026, Elano Corp) i 37-1 MUFFLER (#099005-142, Elano Corp.) i -2 SHROUD ASSEMBLY (#099005-143, Elano Corp.) i -3 RISER ASSEMBLY (#099005-120, Elano Corp) 4 -4 CLAMP (#099005-401, Elano Corp.) 8 -5 50627 BOLT (AN3-4A) 16 -6 55149 NUT (MS20365-1032C) 16 -7 SCREW (Type 8B/Z, Elano Corp.) 7 -8 NUT (C6052-8Z-1, Tinnerman) 7 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 125 Model 112 Rockwell International General Aviation Division X24 10 A Figure 38. Cowling Installation (Sheet 1 of 2) Changed January 1978 126 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 38. Cowling Installation (Sheet 2 of 2) Changed January 1978 126A Model 112 e Rockwell International General Aviation Division SECTION V Power Plant Group COWLING INSTALLATION FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 38- 46318 COWLING INSTL REF One & Up -1 AW4-60 STUD (Mfg by DZUS Fastener Co.,Inc.) 2 -2 X5133-21 RING - Retaining (Mfg by Waldes Kohinoor ,Inc.) 2 -3 X485-275 SPRING PLATE ASSY (riveted) (Mfg by DZUS 2 Fastener Co.,Inc.) -4 46251-1 SPRING (riveted) 2 -5 46232-1 PIN 2 (ATTACHING PARTS) -6 MS20365-1032C NUT 1 AN960-10 WASHER 1 * 46151-501 COWLING ASSY - Top 1 -7 46151-11 COWLING - Top 1 -8 514-1X1AA LATCH (Mfg by Rex Chainbelt, Inc.) 4 (ATTACHING PARTS) -9 AN515-8-14 SCREW (fwd latch) 2 AN515-8-10 SCREW (aft latch) 2 AN960-8 WASHER 2 MS20365-832C NUT 2 -10 AN507C632R10 SCREW (fwd latch) 2 AN960-6 WASHER 2 MS21042-06 NUT 2 * -11 46239-1 SPRING 4 -12 46233-3 CLIP 2 46142-1 DOOR ASSY - Oil Check 1 -13 KM610-32 LATCH 1 -14 46145-1 DOOR 1 -15 46143-1 SHIM 1 -16 46144-1 HINGE 1 -17 46146-1 DOUBLER 1 46160-3 COWLING ASSY - Bottom 1 -18 46160-11 COWLING - Bottom 1 (ATTACHING PARTS) -19 AN525-10R10 SCREW 2 C-185 WASHER (mfg by Stimpson Co. ,Inc.) 2 A-1902 EYELET (Mfg by Stimpson Co., Inc.) 2 -20 AN525-10R8 SCREW 6 C-185 WASHER (Mfg by Stimpson Co. ,Inc.) 6 A1159 EYELET (Mfg by Stimpson Co. ,Inc.) * 6 -21 46030-1 SEAL 1 -22 46030-3 SEAL 1 -23 R-1425N SEAL, LH - Scoop (Mfg by Rubatex Corp.) AR -24 46162-1 NOSE GEAR DOOR ASSY, LH (see Figure 39) REF -25 46162-3 NOSE GEAR DOOR ASSY, RH (see Figure 39) REF When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 1268 Model 112 From RareAviation.com * Rockwell International General Aviation Division SECTION V Power Plant Group COWLING INSTALLATION FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 38-26 46172-501 RETAINER ASSY - Landing Light 1 One & Up -27 46172-503 RETAINER ASSY - Landing Light i (ATTACHING PARTS) -28 AN507-1032R20 SCREW 3 -29 A3235-020-1 WASHER (under screw head) (Mfg by Tinnerman 3 Products Corp.) -30 LC-042G-6 SPRING (Mfg by Lee Spring Co.) 3 -31 MS21075-3 NUTPLATE 3 * -32 4509 LIGHT (Mfg by General Electric) 1 -33 51L8-1AA STRIKE (Mfg by Rex Chainbelt, Inc.) 4 (ATTACHING PARTS) -34 AN507C632R14 SCREW (fwd strike) 2 AN507C632R10 SCREW (aft strike) 2 MS21043-06 NUT 2 * 46336-501 COWL FLAP ASSY, LH 1 46336-2 COWL FLAP ASSY, RH 1 (ATTACHING PARTS) -35 AN526-1032R10 SCREW 4 AN960-10L WASHER 8 MS21044N3 NUT 4 * -36 46156-501 COWL FLAP, LH 1 46156-2 COWL FLAP, RH 1 -37 46337-501 STIFFENER, LH 1 46337-2 STIFFENER, RH 1 -38 46157-1 HINGE ASSY 2 -39 46338-1 BRACKET 2 (ATTACHING PARTS) AN526-1032R6 SCREW 1 MS20364-1032C NUT 1 *. -40 46233-5 CLIP (replaces 46233-1) (riveted) 2 -41 46161-3 SUPPORT ASSY - Nose Landing Gear Door 1 (ATTACHING PARTS) MS24694-C5 SCREW AR A3135-017-1 WASHER (Mfg by Tinnerman Products, Inc.) AR AN960-8L WASHER AR MS21042-08 NUT AR * -42 46387-1 BRACKET 2 -43 46387-2 BRACKET 2 -44 46386-1 BRACKET 1 -45 46386-2 BRACKET 1 -46 46159-3 BRACKET 1 -47 46159-4 BRACKET 1 -48 46161-5 FRAME 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 127 Model 112 Rockwell International General Aviation Division Figure 39. Nose Gear Door Installation ISSUED: May 1972 128 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION V Power Plant Group NOSE GEAR DOOR INSTALLATION FIG. & INDEX NO. PART NUMBER 45003-1 46091-1 39-1 46103-1 -2 46179-3 -3 51454 -4 54706 -5 55350 -6 -7 58860 -8 65079 -9 -10 -11 -12 46166-1 -13 50101 -14 50951 -15 53474 -16 54706 -17 58760 -18 I -19 65076 -2C 66141 -21 68247 1 "2" 68239 1 "2J 68329 -2' t 60148 1 "2E 63016 -2( 5 62663 -2 7 62662 CODE NOMENCLATURE NO. RECTO SERIAL NO'S AFFECTED NOSE GEAR DOOR INSTALLATION OPERATING MECHANISM INSTALLATION - Nose Gear Doors BUMPER STOP ASSEMBLY - Nose Gear Doors LEVER ASSEMBLY - Nose Gear Doors SLIDE BLOCK - Nose Gear Doors BOLT (AN4-44A) NUT (AN316-4R) NUT (AN364-428C) SCREW (AN526-832R30) WASHER (AN970-4) NUT (MS20365-832C) BUSHING (#AA-304-ll, Amplex Div.) SPRING (#LC-045E-18, Lee Spring) BUMPER (#59W, Atlantic Inida Rubber) CONNECTING ROD - Nose Gear Doors BOLT (AN3-10A) BOLT (AN4-11A) BOLT - EYE (AN42-13A) NUT (AN316-4R) WASHER (AN960-416) NUT (MS20365-428C) NUT (MS20365-1032C) WASHER (MS 35338-44) SPACER (NAS43HT3-32) SPACER (NAS43HT3-59) BUSHING (NAS73-3-OO8) BUSHING (FF-S20-5, Amplex Div.) SPRING (LE-063E-7, Lee Spring) ROD END (SPFL-4S, Superior) ROD END (SPF-4, Superior) One & Up i i i i 2 2 2 2 2 2 2 2 2 2 4 2 2 2 6 4 6 2 2 2 2 2 2 2 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Model 112 ISSUED: May 1972 129 e Rockwell International General Aviation Division SECTION V Powerplant Group NOSE GEAR DOOR INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NO'S AFFECTED 46162-1 DOOR ASSEMBLY - Nose Gear, L. H. i One & Up 46162-3 DOOR ASSEMBLY - Nose Gear, R. H. i 39-28 46147-1 BRACKET - Nose Gear Doors, L. H. 2 46147-2 BRACKET - Nose Gear Doors, R. H. 2 -29 46163-1 SKIN - Door, L. H. 1 46163-3 SKIN - Door, R. H. 1 -30 46164-1 HINGE - Door, L. H. 1 46164-2 HINGE - Door, R. H. 1 -31 46165-1 HINGE - Door, L. H. 1 46165-2 HINGE - Door, R. H. 1 -32 46167-1 PAN - Door, L. H. 1 46167-3 PAN - Door, R. H. 1 -33 46170-1 SPACER - Nose Gear Door 8 -34 55337 NUT (AN363-1032) 16 -35 56631 SCREW (AN525-10-16) 16 -36 58740 WASHER (AN960-10) 8 -37 60147 BEARING (FF520-10 Oilite) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 130 Model 112 From RareAviation.com SECTION CONTROL SYSTEMS GROUP 131 Section VI CONTROL SYSTEMS GROUP From RareAviation.com e Rockwell International General Aviation Division Figure 40. Yoke Assembly and Installation ISSUED: May 1972 132 Model 112 e Rockwell International General Aviation Division SECTION VI Control System Group YOKE ASSEMBLY AND INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 47007-5 YOKE INSTALLATION i One & Up 47007-7 YOKE ASSEMBLY i 40-1 40121-3 BOLT i -2 47229-13 YOKE - Weld Assembly i -3 47231-1 SPROCKET 2 -4 47231-3 SPROCKET 3 -5 47233-1 SHAFT - Control Column 1 -6 47234-1 SPACER 1 -7 47236-1 SHAFT - Pilot Input 2 -8 47238-1 UNIVERSAL JOINT - Aileron Control 2 -9 47239-1 SPACER 3 -10 47247-1 SHAFT - Idler 1 47334-1 ARM ASSEMBLY - Elevator Controls 1 47335-1 ARM ASSEMBLY - Elevator Controls 1 -11 47334-3 ARM - Elevator Controls 1 -12 47335-3 ARM - Elevator Controls 1 -13 59395 BEARING (#191 Bound Brook Corp.) 2 -14 BOLT (AN173-7) 1 -15 54207 BOLT (AN174-10A) 2 -16 54203 BOLT (AN174-11A) 3 -17 54228 BOLT (AN175-36A) 1 -18 54425 NUT (AN310-5) 1 -19 54450 NUT (AN310-6) 1 -20 50951 BOLT (AN4-11A) 8 -21 51776 BOLT (AN5-20A) 1 -22 58750 WASHER (AN960-10L) 1 -23 58760 WASHER (AN960-416) 13 -24 58770 WASHER (AN960-416L) 3 -25 58781 WASHER (AN960-516L) 3 -26 58780 WASHER (AN960-516) 2 -27 58794 WASHER (AN960-616L) 1 -28 58805 WASHER (AN960-816) 2 -29 65033 PULLEY (MS20220-2) 2 -30 NUT (MS20364-428) 11 -31 NUT (MS20364-524) 2 -32 A2167 NUT (MS20365-1032) 1 -33 A2172 NUT (MS20365-428) 2 -34 55424 NUT (MS20365-524) 1 -35 65745 COTTER PIN (MS24665-132) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 133 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION VI Control System Group YOKE ASSEMBLY AND INSTALLATION FIG. & INDEX NO, PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 40-36 65763 COTTER PIN (MS24665-233) i One & Up -37 60171 BEARING (CSF379C-075D, Bound Brook Corp) 2 -38 60172 BEARING (CSF504BA-1000, Bound Brook Corp) 6 -39 40111-40 BUSHING 2 -40 47240-1 CONTROL WHEEL 2 -41 47241-1 SHAFT - Wheel Input 2 -42 47310-1 STOP - Wheel 2 -43 47311-1 SPACER - Universal Joint 2 -44 47312-1 CONTROL LOCK 1 -45 47313-1 MOUNTING - Input Shaft 2 -46 47314-1 O-RING - Control Wheel 2 -47 47315-1 COLLAR - Shaft, Wheel Input 2 -48 50627 BOLT (AN3-4A) 8 -49 54209 BOLT (AN174-16A) 2 -50 BOLT (AN25-11A) 2 -51 51126 BOLT (AN4-17A) 2 -52 58740 WASHER (AN960-10) 8 -53 58750 WASHER (AN960-10L) 8 -54 58770 WASHER (AN960-416L) 4 -55 58781 WASHER (AN960-516L) 6 -56 55360 NUT (MS20364-524) 2 -57 A2167 NUT (MS20365-1032) 8 -58 A2172 NUT (MS20365-428) 4 -59 62664 RETAINER RING (1N187, Eaton Yale & Towne) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 134 Model 112 Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 135 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 41. Rudder Pedal Installation ISSUED: May 1972 136 Model 112 * Rockwell International General Aviation Division SECTION VI Control System Group RUDDER PEDAL INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 47002-1 47002-3 DRAWING - Rudder Controls Installation, Single Toe Brakes DRAWING - Rudder Controls Installation, Dual Toe Brakes One & Up 41-1 40111-23 BUSHING 2 -2 40111-25 BUSHING 4 -3 40111-27 BUSHING 4 47217-1 PEDAL ASSEMBLY - Rudder, L.H. 2 47217-2 PEDAL ASSEMBLY - Rudder, R.H. 2 -4 47217-3 PEDAL - Rudder, L.H. 2 47217-4 PEDAL - Rudder, R.H. 2 -5 60183 BEARING (#F753S-.250, Bound Brook Corp.) 8 -6 47250-1 SHAFT WELDMENT - Pedal Support 1 47252-1 SUPPORT BRACKET ASSEMBLY - Rudder Shaft 2 -7 47252-3 SUPPORT BRACKET - Rudder Shaft 2 -8 60179 BEARING (#F1003C, Bound Brook Corp.) 2 -9 47254-1 SHAFT WELDMENT - Pedal Support 1 47257-1 PUSHROD ASSEMBLY - Rudder 1 -10 47257-5 PUSHROD - Rudder 1 -11 47267-1 CLEVIS - Rudder Pushrod 2 47257-3 PUSHROD ASSEMBLY - Rudder 1 -12 47257-7 PUSHROD - Rudder 1 -13 47267-1 CLEVIS - Rudder Pushrod 2 -14 47259-1 WASHER - Rudder Pedal Shaft 4 -15 47261-1 SHAFT ASSEMBLY 1 -16 60112 BEARING (#F750, Bound Brook Corp.) 2 -17 47262-1 SPACER - Bellcrank Mounting 1 -18 47266-1 RETAINER 2 -19 47268-1 WASHER - Bellcrank 2 -20 47269-1 PEDAL SUPPORT ASSEMBLY 1 -21 65035 PULLEY (MS20220-1) 1 -22 51802 BOLT (AN5-22A) 1 -23 58780 WASHER (AN960-516) 1 -24 55424 NUT (MS20365-524) 1 -25 47270-1 PEDAL SUPPORT ASSEMBLY 1 -26 65035 PULLEY (MS20220-1) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 137 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION VI Control System Group RUDDER PEDAL INSTALLATION FIG. & INDEX PART NO. SERIAL NOS NO. NUMBER CODE NOMENCLATURE REDD AFFECTED 41-27 51802 BOLT (AN5-22A) i One & Up -28 58780 WASHER (AN960-516) i -29 55424 NUT (MS20365-524) i -30 47401-1 BELLCRANK ASSEMBLY - Rudder Trim i -31 60180 BEARING (#F1003C-.90, Bound Brook Corp.) i -32 47330-1 A PEDAL SUPPORT ARM 2 -33 53254 A BOLT (AN23-13) 2 -34 53374 A BOLT (AN23-24) 2 -35 54375 A NUT (AN310-3) 4 -36 50628 BOLT (AN3-44A) 1 -37 50876 BOLT (AN4-6A) 6 -38 50976 BOLT (AN4-12A) 4 -39 51051 BOLT (AN4-15A) 2 -40 53252 BOLT (AN23-UA) 4 -41 53254 BOLT (AN23-13) 4 -42 58750 WASHER (AN960-10L) 5 -43 58770 WASHER (AN960-416L) 12 -44 54375 NUT (AN31O-3) 4 -45 A2167 NUT (MS20365-1032) 1 -46 A2172 NUT (MS20365-428) 12 -47 65745 COTTER PIN (MS24665-132) 4 A - Used only when single toe brakes are installed When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 138 Model 112 * Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 139 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 42. Aileron Controls Installation ISSUED: May 1972 140 Model 112 MtW Rockwell International SECTION VI . . . AILERON CONTROLS Control System Group General Aviation Division INSTALLATION FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 47001-1 47506-1 DRAWING - Aileron Controls Installation BRACKET ASSEMBLY - Aileron i One & Up 42-1 47219-1 BRACKET - Balance Cable, Aileron i -2 47507-1 BRACKET - Drive Cable, Aileron i -3 47221-1 BRACKET - Drive Cable, Aileron i 47501-2 CABLE GUARD ASSEMBLY 5 -4 47501-8 PIN - Cable Guard 5 -5 47501-9 COVER - Cable Guard 5 47227-1 PUSHROD ASSEMBLY - Aileron Control 2 -6 47227-3 PUSHROD - Aileron Control 2 -7 54706 NUT (AN316-4R) 2 -8 A0240 NUT (AN316-4L) 2 -9 62661 ROD END BEARING (HF4-R, Heim Corp.) 2 -10 62676 ROD END BEARING (HF4-L, Heim Corp.) 2 47222-1 BELLCRANK ASSEMBLY - Aileron, L.H. 1 47222-2 BELLCRANK ASSEMBLY - Aileron, R.H. 1 -11 47222-3 BELLCRANK - Aileron, L.H. 1 47222-4 BELLCRANK - Aileron, R.H. 1 -12 59406 BEARING (FB-810-4, Boston Gear) 4 47232-1 CHAIN ASSEMBLY - Aileron Control 1 47232-7 A CHAIN ASSEMBLY - Aileron Control 1 -13 47232-3 CHAIN 1 -14 47232-5 CHAIN 1 -15 65574 TURNBUCKLE (MS21251-3S) 1 -16 65576 EYE END L.H. (MS21254-3LS) 1 -17 65577 EYE END R.H. (MS21254-3RS) 1 -18 65620 CLIP (MS21256-1) 2 -19 47210-1 CABLE ASSEMBLY 2 47210-16 CABLE ASSEMBLY (5/32") 2 -20 47210-2 CABLE ASSEMBLY 2 47210-17 CABLE ASSEMBLY (5/32") 2 -21 47210-3 CABLE ASSEMBLY 1 47210-18 CABLE ASSEMBLY (5/32") 1 -22 47210-4 CABLE ASSEMBLY 1 47210-19 CABLE ASSEMBLY (5/32) 1 A USED WHEN 5/32" CONTROL CABLES ARE IN- STALLED When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 141 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION VI Control System Group AILERON CONTROLS INSTALLATION FIG. & INDEX NO. PART NUMBER GODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 42-23 40111-15 BUSHING 2 One & Up -24 40111-55 BUSHING 2 -25 40111-57 BUSHING 2 -26 65033 PULLEY (MS20220-2) 5 -27 65585 TURNBUCKLE (MS21251-B5S) 3 -28 65620 CLIP (MS21256-1) 6 -29 50001 BOLT (AN3-4A) 8 -30 50050 BOLT (AN3-6) 4 -31 50950 BOLT (AN4-11) 2 -32 50975 BOLT (AN4-12) 2 -33 51552 BOLT (AN5-11A) 3 -34 53373 BOLT (AN24-14) 2 -35 53378 BOLT (AN24-17) 2 -36 54375 NUT (AN310-3) 4 -37 54400 NUT (AN31O-4) 8 -38 55599 NUT (AN365-1032A) 8 -39 55425 NUT (AN365-524A) 3 -40 58710 WASHER (AN960-4) 3 -41 58760 WASHER (AN960-416) 8 -42 58770 WASHER (AN960-416L) 4 -43 58781 WASHER (AN960-516L) 3 -44 58750 WASHER (AN960-10L) 12 -45 58860 WASHER (AN970-4) 8 -46 65745 COTTER PIN (MS24665-132) 12 -47 NUT (#A109-014-l, Tinnerman Products) 10 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 142 Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1472 143 Model 112 From RareAviation.com e Rockwell International General Aviation Division Figure 43. Rudder Controls Installation ISSUED: May 1972 144 Model 112 e Rockwell International General Aviation Division SECTION VI Control System Group RUDDER CONTROLS INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RE(TD SERIAL NO'S AFFECTED 47002 DRAWING - Rudder Controls Installation One & Up 43-1 47210-9 CABLE ASSEMBLY i 47210-24 CABLE ASSEMBLY (5/32") i -2 47210-10 CABLE ASSEMBLY i 47210-25 CABLE ASSEMBLY (5/32") i -3 47210-14 CABLE ASSEMBLY i 47210-26 CABLE ASSEMBLY (5/32") i -4 47210-15 CABLE ASSEMBLY i 47210-27 CABLE ASSEMBLY (5/32") i 47501-2 CABLE GUARD ASSEMBLY 2 -5 47501-8 PIN - Cable Guard 2 -6 47501-9 COVER - Cable Guard 2 -7 51552 BOLT (AN5-11A) 2 -8 53252 BOLT (AN23-11) 4 -9 58750 WASHER (AN960-10L) 4 -10 58781 WASHER (AN960-516L) 2 -11 54375 NUT (AN310-3) 4 -12 55424 NUT (MS20365-524) 2 -13 65033 PULLEY (MS20220-2) 5 -14 65745 COTTER PIN (MS24665-132) 4 -15 65585 TURNBUCKLE (MS21251-B5S) 2 -16 65620 CLIP (MS21256-1) 4 -17 NUT (A109-014-1, Tinnerman Products, Inc.) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 145 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 44. Rudder Trim and Nose Wheel Steering Installation ISSUED: May 1972 146 Model 112 e Rockwell International General Aviation Division SECTION VI Control System Group RUDDER TRIM AND NOSE WHEEL STEERING INSTL FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NOS AFFECTED 47400 DRAWING - Rudder Trim and Nose Wheel Steering Installation One & Up 44-1 40102-1 PULLEY 4 -2 40111-43 BUSHING 2 -3 46202-1 GROMMET - Firewall 2 -4 47403-1 NUT - Barrel, Rudder Trim 1 -5 47405-1 SHAFT - Rudder Trim Adjustment 1 -6 47406-5 BRACKET - Nose Gear Steering 2 -7 47410-1 SHAFT ASSEMBLY - Rudder Trim Indicator 1 -8 47411-1 LINK - Rudder Trim Indicator 1 -9 47412-1 DISC - Rudder Trim Indicator 1 -10 47414-1 KNOB - Rudder Trim 1 47420-7 CABLE AND BUNGEE ASSEMBLY - Nose Gear Steering 2 -11 47426-1 TUBE - Spring Box 2 -12 47427-1 TUBE ASSEMBLY 2 -13 47428-1 RETAINER - Nose, Gear Steering 2 -14 47429-1 WIRE RETAINER - Nose Gear Steering 2 -15 50301 BOLT (AN3-20A) 2 -16 58740 WASHER (AN960-10) 4 -17 A1621 WASHER (AN960-1416L) 2 -18 65075 NUT (MS20364-1032) 2 -19 CLEVIS END (MS210252-3LS) 2 -20 SPRING (LE-063-10, Lee Spring Co.) 2 -21 SPRING (LHC-177P-3, Lee Spring Co.) 2 -22 47420-9 CABLE ASSEMBLY - Nose Gear Steering 2 -23 47425-1 COUPLING - Nose Wheel Steering 2 -24 47432-1 STOP - Weld Assembly 1 -25 47433-1 RETAINER 1 47501-2 CABLE GUARD ASSEMBLY 2 -26 47501-8 PIN - Cable Guard 2 -27 47501-9 COVER - Cable Guard 2 -28 50003 BOLT (AN3-3A) 1 -29 50051 BOLT (AN3-6A) 1 -30 50875 BOLT (AN4-6) 2 -31 53353 BOLT (AN23-8) 1 -32 53252 BOLT (AN23-11) 2 -33 BOLT (AN23-15) 2 -34 BOLT (AN23-20) 2 -35 53410 BOLT (AN24-30) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft, ISSUED: May 1972 147 Model 112 From RareAviation.com Rockwell International General Aviation Division SECTION VI Control System Group RUDDER TRIM AND NOSE WHEEL STEERING INSTL FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NO'S AFFECTED 44-36 54400 NUT (AN310-4) 2 One & Up -37 54825 NUT (AN320-3) 7 -38 54850 NUT (AN320-4) 2 -39 NUT (AN363-440) 1 -40 56598 SCREW (AN520-10-5) 4 -41 59679 SCREW (AN530-6R4) 2 -42 58743 WASHER (AN960-C10) 6 -43 58750 WASHER (AN960-10L) 6 -44 58770 WASHER (AN960-416L) 4 -45 58790 WASHER (AN960-616) 8 -46 A2167 NUT (MS20365-1032) 2 -47 TURNBUCKLE (MS21251-B3S) 2 -48 65620 CLIP (MS21256-1) 4 -49 65745 COTTER PIN (MS24665-132) 11 -50 BUSHING (CS252BA0375, Bound Brook Corp.) 2 -51 BUSHING (P20-5, Bunting Bearings Inc.) 2 -52 61573 GROMMET HOLDER (MT340, Arens Controls Inc) 2 -53 NUT (A109-014-1, Tinnerman Products, Inc.) 4 -54 PUSH NUT (012040-012, Tinnerman Products Inc) 2 -55 NUT (#4, Pal Nut, PALNUTCo.) 1 -56 RETAINER RING (#5133-37, Waldes Kohinoor Inc; 3 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 148 Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGO SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 149 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 45. Elevator Controls Installation ISSUED: May 1972 150 Model 112 e Rockwell International General Aviation Division SECTION VI Control System Group ELEVATOR CONTROLS INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RECTD SERIAL NOS AFFECTED 45-1 47004-1 40111-19 DRAWING - Elevator Controls Installation BUSHING 2 One & Up -2 40111-37 BUSHING 1 -3 47203-1 PUSHROD ASSEMBLY - Elevator 1 -4 60157 BEARING (#FF-310, OiliteCorp.) 1 -5 47210-5 CABLE ASSEMBLY 1 47210-20 CABLE ASSEMBLY (5/32) 1 -6 47210-6 CABLE ASSEMBLY 1 47210-21 CABLE ASSEMBLY (5/32) 1 -7 47210-7 CABLE ASSEMBLY 1 47210-22 CABLE ASSEMBLY (5/32) 1 -8 47210-8 CABLE ASSEMBLY 1 47210-23 CABLE ASSEMBLY (5/32) 1 47501-1 CABLE GUARD ASSEMBLY 1 -9 47501-6 PIN - Cable Guard 1 -10 47501-7 COVER - Cable Guard 1 47501-3 CABLE GUARD ASSEMBLY 1 -11 47501-10 PIN - Cable Guard 1 -12 47501-11 COVER - Cable Guard 1 -13 47214-1 CAM - Elevator Stop 2 47509-1 BELLCRANK ASSEMBLY - Elevator 1 -14 47209-1 LEVER ASSEMBLY - Elevator 1 -15 47204-3 LEVER - Input, Elevator Bellcrank 1 -16 40111-17 BUSHING 2 -17 50926 BOLT (AN4-10A) 2 -18 58770 WASHER (AN960-416L) 2 -19 A2172 NUT (MS20365-428) 2 -20 60170 BEARING (#189BB, Bound Brook Corp.) 2 -21 60181 BEARING (F314R, Bound Brook, Corp.) 2 -22 BOLT (AN23-10) 2 -23 50351 BOLT (AN3-22A) 2 -24 50900 BOLT (AN4-7) 1 -25 50924 BOLT (AN4-10) 1 -26 51226 BOLT (AN4-23A) 1 -27 52108 BOLT (AN5-50A) 1 -28 52112 BOLT (AN5-54A) 1 -29 53254 BOLT (AN23-13) 2 -30 54400 NUT (AN310-4) 2 -31 54825 NUT (AN320-3) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 151 Model 112 From RareAviation.com -A Rockwell International General Aviation Division ELEVATOR CONTROLS INSTALLATION SECTION VI Control System Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDO SERIAL NO'S AFFECTED 45-32 -33 -34 -35 -36 -37 -38 -39 -40 -41 -42 -43 -44 -45 -46 -47 A2167 A2172 55424 58750 58740 58760 58770 58780 58781 65033 65585 65620 65745 68252 NUT (MS20365-1032) NUT (MS20365-428) NUT (MS20365-524) WASHER (AN96O-1OL) WASHER (AN960-10) WASHER (AN96O-416) WASHER (AN960-416L) WASHER (AN960-516) WASHER (AN960-516L) PULLEY (MS20220-2) TURNBUCKLE (MS21251-B5S) CLIP (MS21256-1) COTTER PIN (MS24665-132) SPACER (NAS 43DD5-45) NUT (#A109-014-l, Tinner man Products, Inc.) BUSHING (#SB-1000-12, Kayman Man. Co.) 2 1 2 4 2 4 6 2 2 3 2 2 6 1 4 2 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 152 Model 112 Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NOS AFFECTED| THIS PAGE INTENTIONALLY LEFT BLANK |When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 153 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 46. Elevator Trim Installation ISSUED: May 1972 154 Model 112 MB Rockwell International SECTION VI A ELEVATOR TRIM Control System Group General Aviation Division INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQfD SERIAL NOS AFFECTED 47006-1 DRAWING - Elevator Trim Installation One & Up 46-1 47210-11 CABLE ASSEMBLY i -2 47210-12 CABLE ASSEMBLY i -3 47210-13 CABLE ASSEMBLY i 47501-5 CABLE GUARD ASSEMBLY i -4 47501-12 PIN - Cable Guard i -5 47501-13 COVER - Cable Guard i -6 47273-1 BRACKET - Elevator Trim Pulley i 47274-1 SPROCKET ASSEMBLY - Elevator Trim i -7 47272-1 BRACKET ASSEMBLY - Elevator Trim Idler Sprocket i -8 47293-3 SPROCKET - Elevator Trim 2 -9 47500-5 SPACER 2 -10 58760 WASHER (AN960-416) 2 -11 58770 WASHER (AN960-416L) 2 -12 54400 NUT (AN310-4) 2 -13 65745 COTTER PIN (MS24665-132) 2 -14 60168 BEARING (#250S, Bound Brook Corp.) 2 -15 47277-1 GUIDE BLOCK - Elevator Trim Cable 2 47279-1 CHAIN ASSEMBLY - Elevator Trim 1 -16 CHAIN (#ASA 25, Cullman Wheel Co.) 1 -17 CONNECTOR LINK (#ASA 25, Cullman Wheel Co.) 2 47290-1 ACTUATOR ASSEMBLY - Elevator Trim 1 -18 47291-1 JACKSCREW - Elevator Trim 1 -19 47292-1 HOUSING - Elevator Trim 1 -20 47293-1 SPROCKET - Elevator Trim 1 -21 47296-1 STOP - Elevator Trim 2 -22 47333-1 HOUSING - Elevator Trim 1 -23 58803 WASHER (AN960 C816L) 2 -24 65756 COTTER PIN (MS24665-153) 2 -25 60155 BEARING (#F500A-75, Bound Brook) 2 47299-1 ELEVATOR TRIM - Wheel and Indicator Installation 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 155 Model 112 From RareAviation.com -O Rockwell International General Aviation Division ELEVATOR TRIM INSTALLATION SECTION VI Control System Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 47300-1 ELEVATOR TRIM - Wheel Assembly i One & Up 47295-1 SHAFT ASSEMBLY - Trim Wheel i 46-26 47295-3 TAB - Trim Wheel i -27 47318-1 SHAFT - Elevator Trim Wheel i -28 47319-1 INDICATOR - Elevator Trim i -29 RING (#C2311-012, Tinnerman Products Co.) i -30 47294-1 TRIM WHEEL i -31 47326-1 PLATE - Trim Wheel i -32 56931 SCREW (AN531-6-6) 3 -33 58760 WASHER (AN960-416) 2 -34 52336 PIN (#SP-062-625, Driv Lok, Inc.) 2 -35 47323-1 SUPPORT ASSEMBLY - Trim Wheel 2 -36 47327-1 SPRING - Trim Indicator 1 -37 58770 WASHER (AN960-416L) 2 -38 65757 COTTER PIN (MS24665-152) 3 -39 47301-1 PUSHROD ASSEMBLY - Elevator Trim 1 -40 50026 BOLT (AN3-5A) 2 -41 50126 BOLT (AN3-11A) 2 -42 57001 BOLT (AN4-13A) 1 -43 53245 BOLT (AN21-12) 1 -44 53300 BOLT (AN23-16) 1 -45 NUT (&A109-014-1, Tinnerman Products, Inc.) 2 -46 55599 NUT (AN365-1032) 2 -47 54559 NUT (AN315-3R) 2 -48 54824 NUT (AN32O-1) 1 -49 54825 NUT (AN320-3) 1 -50 55400 NUT (AN365-428A) 1 -51 58722 WASHER (AN960-6L) 1 -52 58750 WASHER (AN960-10L) 5 -53 58770 WASHER (AN960-416L) 1 -54 66132 WASHER (MS35335-32) 3 -55 65020 PULLEY (MS20219-2) 2 -56 65030 PULLEY (MS20220-2) 4 -57 65575 TURNBUCKLE (MS21251-B2S) 2 -58 65620 CLIP (MS21256-1) 4 -59 65759 COTTER PIN (MS24665-5) 1 -60 65745 COTTER PIN (MS24665-132) 1 -61 65901 SCREW (MS27039-1-15) 3 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 156 Model 112 e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NOS AFFECTED[this page intentionally left blank IWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 157 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 47. Flap Controls Installation ISSUED: May 1972 158 Model 112 * Rockwell International General Aviation Division SECTION VI Control System Group FLAP CONTROLS INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 47-1 47003-1 40111-21 DRAWING - Flap Mechanism and Motor Installation BUSHING i One & Up -2 40111-31 BUSHING i -3 40111-29 BUSHING i 47216-1 TORQUE TUBE ASSEMBLY - Flap i -4 47508-1 ARM ASSEMBLY, L.H. - Torque Tube i 47508-2 ARM ASSEMBLY, R. H. - Torque Tube i -5 47280-1 TORQUE TUBE - Flap Actuation i -6 47288-1 LEVER ASSEMBLY - Torque Tube i -7 47284-1 RETAINER - Torque Tube 2 47287-1 MOUNT ASSEMBLY - Torque Tube, L.H. 1 47287-2 MOUNT ASSEMBLY - Torque Tube, R.H. 1 -8 47287-3 MOUNT - Torque Tube 2 -9 60182 BEARING (#F1502B-75, Bound Brook Corp.) 2 -10 47286-1 MOUNTING BRACKET - Flap Actuator 1 47224-1 PUSHROD ASSEMBLY - Flap 2 -11 47224-3 PUSHROD - Flap 2 -12 A0240 NUT (AN316-4L) 2 -13 54706 NUT (AN316-4R) 2 -14 62676 ROD END BEARING (#HF-4L, Heim Universal) 2 -15 62661 ROD END BEARING (#HF-4R, Heim Universal) 2 47516-1 FLAP MOTOR ASSEMBLY 1 -16 47275-1 TUBE ASSEMBLY - Flap Actuator 1 -17 55349 NUT (AN364-428) 1 -18 ACTUATOR ASSEMBLY (#D145-00-25, 1 -19 57026 Commercial Aircraft Products) BOLT (AN4-14A) 1 -20 51052 BOLT (AN4-15) 1 -21 51051 BOLT (AN4-15A) 1 -22 51076 BOLT (AN4-16A) 4 -23 51151 BOLT (AN4-20A) 6 -24 51376 BOLT (AN4-30A) 2 -25 53376 BOLT (AN24-15A) 1 -26 53377 BOLT (AN24-16A) 1 -27 54400 NUT (AN310-4) 1 -28 A2172 NUT (MS20365-428) 16 -29 58760 WASHER (AN960-416) 4 -30 58770 WASHER (AN960-416L) 17 -31 65742 COTTER PIN (MS29665-13) 1 -32 60169 BEARING (#313-1.00, Bound Brook Corp.) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 159 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 160 Model 112 SECTION HYDRAULIC SYSTEMS GROUP From RareAviation.com 161 Section VII HYDRAULIC SYSTEMS GROUP e Rockwell International General Aviation Division Figure 48. Hydraulic System Installation ISSUED: May 1972 162 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION VII Hydraulic Systems Group HYDRAULIC SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGO SERIAL NO'S AFFECTED 48801-1 HYDRAULIC SYSTEM INSTALLATION One & Up 48808-1 HYDRAULIC POWER PACK ASSEMBLY 48-i 48803-1 SUPPORT MANIFOLD - Hydraulic Power Pack i -2 50851 BOLT (AN4-5A) 4 -3 57605 NIPPLE (AN816-4D) 3 -4 58769 WASHER (AN960PD416L) 4 -5 58934 "O" RING (AN6227B-7) 4 -6 62508 MOTOR LIFT ASSEMBLY (105932B,Presolite) 1 -7 40111-39 BUSHING 4 -8 46099-43 HYDRAULIC LINE 1 -9 46099-45 HYDRAULIC LINE 1 -10 46099-47 HYDRAULIC LINE 1 -11 46099-49 HYDRAULIC LINE 1 -12 46099-51 HYDRAULIC LINE 1 -13 46099-53 HYDRAULIC LINE 1 -14 46099-55 HYDRAULIC LINE 1 -15 46099-57 HYDRAULIC LINE 1 -16 46099-59 HYDRAULIC LINE 1 -17 46099-61 HYDRAULIC LINE 1 -18 46099-63 HYDRAULIC LINE 1 -19 46099-65 HYDRAULIC LINE 1 -20 46099-67 HYDRAULIC LINE 1 -21 46099-69 HYDRAULIC LINE 1 -22 46099-71 HYDRAULIC LINE 1 -23 46099-73 HYDRAULIC LINE 1 -24 46099-81 HYDRAULIC LINE 1 -25 46099-83 HYDRAULIC LINE 1 -26 46136-13 HOSE ASSEMBLY 1 -27 46136-15 HOSE ASSEMBLY 1 -28 46136-17 HOSE ASSEMBLY 2 -29 46136-11 HOSE ASSEMBLY 2 -30 48813-1 KNOB 1 -31 48233-1 ACTUATING CYLINDER - Main Landing Gear, L.H. 1 48233-2 ACTUATING CYLINDER - Main Landing Gear, R.H. 1 -32 48805-1 ACTUATING CYLINDER - Nose Landing Gear 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 163 Model 112 * Rockwell International General Aviation Division SECTION VII Hydraulic Systems Group HYDRAULIC SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 48-33 58251 REDUCER (AN919-2) 2 One & Up -34 53352 BOLT (AN23-22A) 1 -35 50149 BOLT (AN3DD12A) 2 -36 50898 BOLT (AN4DD7A) 4 -37 55349 NUT (AN364-428) 4 -38 55381 NUT (AN364D1032) 3 -39 58379 NUT (AN924-3) 2 -40 A2167 NUT (MS20365-1032) 2 -41 58390 NUT (AN924-4D) 7 -42 57968 TEE (AN824-4D) 3 -43 58053 TEE (AN834-4D) 2 -44 65738 SCREW (MS24621-27) 5 -45 58463 GROMMET (AN931A5-9) 4 -46 58801 WASHER (AN960D716) 4 -47 58774 WASHER (AN960PD416) 4 -48 58745 WASHER (AN960D10) 4 -49 WASHER (AN945-4P) 4 -50 58850 WASHER (AN970-3) 1 -51 P7691 WASHER (AN960D10L) 3 -52 ELBOW (MS20822-4D) 5 -53 ELBOW (MS20823-4D) 1 -54 58056 ELBOW (AN 837-3) 2 -55 57747 ELBOW (AN821-4D) 1 -56 58037 ELBOW (AN833-4D) 7 -57 68257 SPACER (NAS43DD3-32) 1 -58 68256 SPACER (NAS43HT3-23) 1 -59 60779 CLAMP (C3049A-4-108, Tinnerman Products, Inc) 2 -60 60778 CLAMP (C3050A-4-108, Tinnerman Products, Inc) 5 -61 65659 CLAMP (MS21919DG4) 2 -62 65705 CLAMP (MS21919DG12) 3 -63 63239 SPRING (LC-022D-1, Lee Spring Co.) 1 -64 SHUT-OFF VALVE (A-115-4, Gerdes Products) 1 -65 56847 SCREW (AN526-1032R7) 1 -66 56881 SCREW (AN526-1032R14) 1 -67 57565 UNION (AN815-4D) 1 -68 65936 PACKING (MS28778-3) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 164 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 165 Model 112 Rockwell International General Aviation Division Figure 49. Brake System Installation ISSUED: May 1972 166 Model 112 From RareAviation.com Rockwell International General Aviation Division SECTION VII Hydraulic Systems Group BRAKE SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQfD SERIAL NOS AFFECTED 48810-1 BRAKE SYSTEM INSTALLATION - Single One & Up 48810-3 BRAKE SYSTEM INSTALLATION - Dual 49-1 40111-41 BUSHING 2 -2 40111-49 A BUSHING 3 40111-49 B BUSHING 5 -3 40111-67 BUSHING 1 -4 46099-31 A HYDRAULIC LINE 1 -5 46099-33 A HYDRAULIC LINE 1 -6 46099-35 HYDRAULIC LINE 1 -7 46099-37 HYDRAULIC LINE 1 -8 46099-39 HYDRAULIC LINE 1 -9 46099-40 HYDRAULIC LINE 1 -10 46099-75 B HYDRAULIC LINE 1 -11 46099-77 B HYDRAULIC LINE 1 -12 46099-85 B HYDRAULIC LINE 1 -13 46099-87 B HYDRAULIC LINE 1 -14 46136-21 B HOSE ASSEMBLY 2 -15 46136-11 A HOSE ASSEMBLY 2 -16 46136-11 B HOSE ASSEMBLY 4 -17 46136-25 HOSE ASSEMBLY 2 48812-1 CABLE ASSEMBLY - Park Brake 1 -18 48812-3 CABLE 1 -19 SLEEVE (182GPC332P, Nicro Press) 2 -20 48819-1 CLIP 4 -21 64005 WRAP (500002-1) A/R -22 P3468 CABLE (64-032-348, Arens Controls, Inc.) 1 -23 56853 SCREW (AN526-1032R7) 11 -24 SCREW (AN526-1032R12) 2 -25 A SCREW (AN526-1032R24) 3 B SCREW (AN526-1032R24) 5 -26 SCREW (AN526-1032R28) 1 -27 57565 UNION (AN815-4D) 4 -28 57747 A ELBOW (AN821-4D) 4 57747 B ELBOW (AN821-4D) 8 -29 57770 A ELBOW (AN822-4D) 2 57770 B ELBOW (AN822-4D) 6 A Used with single brake installation only. B Used with dual brake installation only. When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 167 Model 112 * Rockwell International General Aviation Division SECTION VII Hydraulic Systems Group BRAKE SYSTEM INSTALLATION FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER CODE NOMENCLATURE REQD AFFECTED 49-30 57940 ELBOW (AN823-4D) 2 One & Up -31 A WASHER (AN960-10) 6 B WASHER (AN960-10) 8 -32 WASHER (AN960-10L) 11 -33 A NUT (MS20365C1032) 6 B NUT (MS20365C1032) 8 -34 NUT (MS20365D1032) 11 -35 65729 CLAMP (MS21919DG4) 14 -36 A2297 CLAMP (MS21919DG5) 2 -37 65707 CLAMP (MS21919DG10) 10 -38 65727 CLAMP (MS21919DG8) 2 -39 CLAMP (QS100M60) 2 -40 MASTER BRAKE CYLINDER ASSEMBLY -Pilots (A-049-3P, Gerdes Products) 2 -41 B MASTER BRAKE CYLINDER ASSEMBLY - Co- Pilots (A-110-9, Gerdes Products) 2 A Used with single brake installation only. B Used with dual brake installation only. When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 168 Model 112 From RareAviation.com SECTION LANDING GEAR GROUP 169 Section VIII LANDING GEAR GROUP From RareAviation.com Rockwell International General Aviation Division X42 29A Figure 50. Nose Gear Installation (Sheet 1 of 3) Changed January 1978 170 Model 112 Rockwell International General Aviation Division A X42 28 Figure 50. Nose Gear Installation (Sheet 2 of 3) Changed January 1978 170A Model 112 From RareAviation.com * Rockwell International General Aviation Division Figure 50. Nose Gear Installation (Sheet 3 of 3) Changed January 1978 170B Model 112 SECTION VIII Landing Gear Group Rockwell International General Aviation Division NOSE GEAR INSTALLATION FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER NOMENCLATURE REGO AFFECTED 50- 45002 NOSE LANDING GEAR INSTL REF One & Up -1 45207-1 PIN (ATTACHING PARTS) 1 -2 AN3C13A AN960C10 MS20365-1032C BOLT WASHER NUT * 2 2 2 -3 NAS70CL765- 1313 WASHER 2 -4 45209-1 RETAINER (ATTACHING PARTS) 2 -5 NAS428H4-4 AN960-416L BOLT WASHER 1 1 -6 52-022-094-0375 PIN - Roll (Mfg by Amerace ESNA Corp.) * 1 -7 AN960D1216 WASHER AR -8 P227 NOSE LANDING GEAR ASSY (see Figure 51) REF -9 P227-18 PIN (ATTACHING PARTS) 2 -10 AN4-22A AN960-416L LHTE-048W BOLT WASHER NUT * 1 1 1 -11 P227-27 SPRING - Inner 1 -12 P227-28 SPRING - Outer 1 -13 45318-1 DRAG BRACE ASSY (see Figure 51) (ATTACHING PARTS) REF -13A AN6-30A AN960-616 MS20365-624 BOLT WASHER NUT * 1 2 1 -14 48838-501 ACTUATING CYLINDER - Nose Landing Gear (replaces p/n 48835-501) (ATTACHING PARTS) 1 -15 AN4-15 AN960C416 AN960-416L LHTE-048W MS24665-132 BOLT WASHER WASHER NUT PIN - Cotter * 2 2 2 2 2 -16 N5000-62MD RING - Snap (Mfg by Gerdes Products,Inc.) 1 -17 A-585-A PLATE - Cover (Mfg by Gerdes Products,Inc.) 1 -18 A-1029-A SPRING (Mfg by Gerdes Products, Inc.) 1 -19 A-1031-A PISTON - Detent Cylinder (Mfg by Gerdes Products,Inc.) 1 -20 2-012 O-RING (Mfg by Gerdes Products, Inc.) 1 -21 A-1032-A BODY - Valve Detent Cylinder (Mfg by Gerdes Products, Inc.) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 1700 Model 112 From RareAviation.com e Rockwell International General Aviation Division NOSE GEAR INSTALLATION SECTION VIII Landing Gear Group Ifig. 1 INDEX NO. PART NUMBER NOMENCLATURE NO. REOC SERIAL NO'S AFFECTED 150-22 S-0310-904R O-RING i One & Up I -23 HMX4M BEARING - Rod (Mfg by Gerdes Products, Inc.) (ATTACHING PARTS) i -24 AN316-5 NUT - Check i I -25 MS35333-41 WASHER i I -26 A-2002-A SHAFT (Mfg by Gerdes Products, Inc.) i I -27 17-437 WIPER - Rod i 1 -28 MS28774-111 RING - Backup i 1 -29 MS28775-111 O-RING i I -30 A-2189-B CAP - End (Mfg by Gerdes Products, Inc.) (ATTACHING PARTS) i I -31 MS28775-028 O-RING i I -32 A-2191-A NUT - Jam (Mfg by Gerdes Products, Inc.) * i I -33 A-2188-A CYLINDER (Mfg by Gerdes Products, Inc.) 1 -34 A-1833-A LABEL (Mfg by Gerdes Products, Inc.) i -35 A-2187-A PISTON (Mfg by Gerdes Products, Inc.) (ATTACHING PARTS) i I -36 MS20365-428 NUT - Lock i -37 MS28774-214 RING - Backup 2 1 -38 MS28775-214 O-RING 1 1 -39 MS28775-028 O-RING 1 1 -40 A-1046-A BUSHING (Mfg by Gerdes Products, Inc.) 1 -41 A-2003-A CAP - End (Mfg by Gerdes Products, Inc.) (ATTACHING PARTS) 1 I -42 COML SETSCREW (6-32 x 1/8 in.long) * 1 I -43 48804-1 SHIMMY DAMPENER ASSY 1 | -44 N5000-125MD RING - Snap (Mfg by Gerdes Products, Inc.) 2 I -45 A-656-A CAP - End (Mfg by Gerdes Products, Inc.) 1 j -46 2-013 O-RING (Mfg by Gerdes Products, Inc.) 2 1 ~47 2-022 O-RING (Mfg by Gerdes Products, Inc.) 2 1 ~48 COML SETSCREW (oval point, 10-32 x 3/16 in.long) 1 j -49 COML CYLON BALL (1/8-inch dia.) 1 I -50 MS24665-134 PIN - Cotter 1 I -51 A-1188-A SPRING (Mfg by Gerdes Products, Inc.) 1 1 -52 2-119 O-RING (Mfg gy Gerdes Products, Inc.) 1 | -53 2-006 O-RING (Mfg by Gerdes Products, Inc.) 1 1 -54 A-1186-A PISTON (Mfg by Gerdes Products, Inc.) 1 I -55 A-328-A1 PISTON (Mfg by Gerdes Products, Inc.) 1 I -56 COML PIN - Roll 1 I -57 A-324-A CAP - End (Mfg by Gerdes Products, Inc.) 1 1 -58 A-1184-A SHAFT (Mfg by Gerdes Products, Inc.) 1 1 -59 A-1185-A HOUSING (Mfg by Gerdes Products, Inc.) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 170D Model 112 e Rockwell International General Aviation Division SECTION VIII Landing Gear Group NOSE GEAR INSTALLATION FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 50-60 A-1194-A BUSHING (Mfg by Gerdes Products, Inc.) WHEEL AND TIRE ASSY - Nose (tube type) i One & Up -61 45007-1 i -62 5.00 x 5 TIRE - Tube Type (4 ply, Type HI) i -63 5.00 x 5 40-77 (A) TUBE WHEEL ASSY - Nose (for tube type tire) (Mfg by Van Sickle Ind.) i i -64 153-8 SEAL (Mfg by Van Sickle Ind.Inc.) 4 -65 154-6 SEAL - Felt (Mfg by Van Sickle Ind.Inc.) 2 -66 155-2 RING - Snap (Mfg by Van Sickle Ind.Inc.) 2 -67 08125 162-28 CONE (Mfg by Van Sickle Ind.Inc.) WHEEL HALF ASSY - Female (Mfg by Van Sickle Ind. Inc.) 2 1 -68 152-25 08231 WHEEL HALF (Mfg by Van Sickle Ind.Inc.) CUP - Bearing (Mfg by Van Sickle Ind.Inc.) 1 1 -69 217-1 161-31 GROMMET - Valve Stem (Mfg by Van Sickle Ind. Inc.) WHEEL HALF ASSY - Male (Mfg by Van Sickle Ind. Inc.) (ATTACHING PARTS) 1 1 -70 AN4-22A AN960-416 MS20365-428 BOLT WASHER NUT 3 6 3 -71 151-27 45003-1 WHEEL HALF - Male (Mfg by Van Sickle Ind. Inc.) CUP - Bearing (Mfg by Van Sickle Ind.Inc.) OPERATING MECHANISM INSTL (see Figure 39) 1 REF -72 45237-1 AXLE 1 -73 45236-1 SPACER 2 -74 45238-1 CTTP AxIa (ATTACHING PARTS) 2 -75 AN4-57A AN960C416 LHTE-048W BOLT WASHER NUT * 1 1 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 171 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 51. Nose Gear Assembly Changed January 1978 172 Model 112 * Rockwell International General Aviation Division NOSE GEAR ASSEMBLY SECTION VIII Landing Gear Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 51- P227 NOSE LANDING GEAR ASSY (see Figure 50 for NHA) i One & Up P227-1 BODY AND TRUNNION ASSY i -1 P227-2 TRUNNION i (ATTACHING PARTS) -2 AN173-37A BOLT 2 AN960-10L WASHER 4 LHTM-02W NUT (Mfg by Cleveland Aircraft Products) 2 * -3 45370-1 ARM, Spring 1 (ATTACHING PARTS) -4 AN3-13A BOLT 2 AN960-10 WASHER 2 MS20365-1032 NUT 2 * -5 P242-8 BUSHING 1 -6 P227-22 PIN - Stop 1 -7 P227-25 WASHER - Trunnion 2 -8 25OQ BUSHING (0.31 in.long) (Mfg by Bound Brook) 2 -9 P227-4 TUBE - Torque 1 -10 P227-29 WASHER - Spacer AR -11 AA-401-3 BUSHING (Mfg by Oilite) 2 -12 P227-6 BEARING 1 -13 P227-26 BUSHING 1 -14 P217-33 WASHER 1 -15 375C BUSHING (0.49 in.long) (Mfg by Bound Brook) 2 P227-7 BODY & COLLAR ASSY - Nose Landing Gear 1 -16 P227-8 BODY 1 -17 P227-24 COLLAR 1 (ATTACHING PARTS) -18 45383-1 PIN 2 45274-1 FORK ASSY - Nose Landing Gear 1 (ATTACHING PARTS) -19 AN4-32A BOLT 1 AN960-416L WASHER 2 MS20365-428 NUT 1 * -20 45222-1 COLLAR - Lower 1 (ATTACHING PARTS) -21 NAS335A21 SCREW 2 -22 NAS335A17 SCREW 2 AN960-516L WASHER 4 MS20365-524 NUT 4 * -23 45372-3 PLATE 1 -24 45239-1 FORK 1 -25 45272-1 TUBE 1 -26 45273-1 PLUG 1 -27 MS28775-120 O-RLNG 1 -28 AA-401-3 BUSHING (Mfg by Oilite) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 173 Model 112 From RareAviation.com Rockwell International General Aviation Division NOSE GEAR ASSEMBLY SECTION VIII Landing Gear Group FIG. & INDEX NO. PART NUMBER NOMENCLATURE NO. REQ'D SERIAL NOS AFFECTED 51-29 P227-9 ORIFICE TUBE ASSY i One & Up -30 P217-14-9 PLATE - Orifice i -31 MS16625-3087 RETAINER i -32 P217-19 BEARING - Upper i -33 MS16624-3143 RETAINER i -34 P217-17 BEARING - Lower i -35 MS28775-134 O-RING i -36 MS28782-27 RING - Backup 2 -37 AN6227-27 O-RING 1 -38 AN6231-17 SCRAPER 1 -39 MS16625-285 RETAINER 1 -40 MS28782-11 RING - Backup 1 -41 AN6227-11 O-RING 1 -42 5160-75MD RETAINER (Mfg by Waldes Kohinoor, Inc.) 1 -43 S-0310-902R O-RING 1 VS743 VALVE - Air (Mfg by Eaton Corp.) 1 VI-3 02-BO CORE - Air Valve (Mfg by Eaton Corp.) 1 637 CAP - Air Valve (Mfg by Eaton Corp.) 1 P217-4 TORQUE LINK ASSY - Upper 1 (ATTACHING PARTS) -44 AN175-30 BOLT 1 AN960-516L WASHER 3 AN310-5 NUT 1 MS24665-134 PIN - Cotter 1 -45 NAS464P4-15 BOLT 1 AN960-416L WASHER 3 AN320-4 NUT 1 MS24665-134 PIN - Cotter 1 * -46 P217-5 LINK - Torque 1 -47 F-250-F BUSHING (replaces p/n P227-31) (Mfg by 1 Bound Brook) -48 P227-17 PLATE 1 (ATTACHING PARTS) -49 MS24694-C-48 SCREW 2 * P217-7 TORQUE LINK ASSY - Lower 1 (ATTACHING PARTS) -50 AN175-30A BOLT 1 AN960-516L WASHER 4 LHTE-054W NUT 1 * -51 P217-8 LINK - Torque -52 P227-31 BUSHING 1 45318-1 DRAG BRACE ASSY - Nose Gear (see Figure 50 1 for NHA) When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 174 Model 112 e Rockwell International General Aviation Division NOSE GEAR ASSEMBLY SECTION VIII Landing Gear Group FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER NOMENCLATURE RECTO AFFECTED 51- 755002-1 DRAG BRACE ASSY - Upper i One & Up (ATTACHING PARTS) -53 AN6-27 BOLT 1 AN960-616 WASHER 2 AN310-6 NUT 1 MS24665-301 PIN - Cotter 1 -54 755004-1 BRACE - Drag Upper 1 -55 P242-7 BUSHING 2 -56 250Q BEARING (0.312 in.long) (Mfg by Bound Brook) 2 -57 F375E BEARING (0.36 in.long) (Mfg by Bound Brook) 2 45317-501 DRAG BRACE ASSY - Lower 1 -58 755005-1 BRACE - Drag Lower 1 -59 F375C BEARING (0.36 in.long) (Mfg by Bound Brook) 4 -60 48804-1 SHIMMY DAMPENER ASSY (see Figure 50 for NHA) REF (ATTACHING PARTS) -61 AN173-12 BOLT 1 AN960C-10 WASHER 2 AN960C-10L WASHER 1 AN320-3 NUT 1 MS24665-152 PIN - Cotter 1 -62 AN174-20 BOLT 1 AN960C416 WASHER 3 AN320-4 NUT 1 MS24665-153 PIN - Cotter 1 * When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. Changed January 1978 175 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 52. Main Landing Gear Installation ISSUED: May 1972 176 Model 112 e Rockwell International General Aviation Division SECTION VIII Landing Gear Group MAIN LANDING GEAR INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 45001-3 MAIN LANDING GEAR INSTALLATION, L.H. One & Up 45001-4 MAIN LANDING GEAR INSTALLATION, R.H. 52-1 45017-1 MAIN LANDING GEAR ASSEMBLY, L.H. i 45017-2 MAIN LANDING GEAR ASSEMBLY, R.H. i 45312-1 SIDE BRACE ASSEMBLY, L.H. i 45312-2 SIDE BRACE ASSEMBLY, R.H. i 45303-1 SIDE BRACE ASSEMBLY - Upper, L.H. i 45303-2 SIDE BRACE ASSEMBLY - Upper, R.H. i -2 45304-1 SIDE BRACE - Upper, L.H. i 45304-2 SIDE BRACE - Upper, R.H. i -3 P254-14 BUSHING 4 45306-1 SIDE BRACE ASSEMBLY - Lower, L.H. 1 45306-2 SIDE BRACE ASSEMBLY - Lower, R.H. 1 -4 P254-5 SIDE BRACE - Lower, L. H. 1 P254-11 SIDE BRACE - Lower , R. H. 1 -5 45313-1 BUSHING 2 -6 BEARING (BSSR-12290, Southwest Products Co.) 2 -7 RETAINER (RR156C, Spirolox) 2 -8 P252-32 BUSHING 2 -9 P254-7 BOLT 2 -10 BOLT (AN174-20A) 2 -11 A0278 NUT (AN320-12) 2 -12 58769 WASHER (AN960PD416L) 4 -13 58821 WASHER (AN960-1216) 2 -14 COTTER PIN (MS24665-357) 2 -15 LOCK NUT (LHTE048W, Esna) 2 -16 45210-1 COLLAR 2 -17 45369-1 BOLT 2 42330-1 FITTING ASSEMBLY - Main Landing Gear, Forward) 2 -18 42273-1 FITTING 2 -19 RING (IN-175, Eaton, Yale & Towne Inc.) 2 -20 60113 BEARING (LHSS-16, Heim Universal Corp.) 2 -21 42274-1 FITTING - Main Landing Gear Side Stay 1 42274-2 FITTING - Main Landing Gear Side Stay 1 42231-1 FITTING ASSEMBLY - Main Landing Gear AFT 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 177 Model 112 From RareAviation.com Rockwell International General Aviation Division MAIN LANDING GEAR INSTALLATION SECTION VIII Landing Gear Group FIG. & INDEX PART NO. SERIAL NOS NO. NUMBER GODE NOMENCLATURE REGO AFFECTED 52-22 42272-1 FITTING - Main Landing Gear AFT 2 One & Up -23 RING (IN-175, Eaton, Yale & Towne Inc.) 2 -24 60113 BEARING (LHSS-16, Heim Universal, Inc.) 2 -25 P252-33 SPRING 2 -26 P254-45 SPACER 2 -27 50902 BOLT (AN4-7A) 24 -28 51425 BOLT (AN4-32A) 2 -29 52997 BOLT (AN8-31) 2 -30 54500 NUT (AN310-8) 2 -31 54850 NUT (AN320-4) 2 -32 A0278 NUT (AN320-12) 2 -33 A0284 NUT (AN320-15) 2 -34 55349 NUT (AN364-428) 2 -35 55750 COTTER PIN (AN380-3-3) 2 -36 58760 WASHER (AN960-416) 24 -37 58770 WASHER (AN960-416L) 2 -38 58790 WASHER (AN960-616) 6 -39 58805 WASHER (AN960-816) 6 -40 58821 WASHER (AN960-1216) 4 -41 58822 WASHER (AN960-1216L) 2 -42 65765 COTTER PIN (MS24665-283) 2 -43 COTTER PIN (MS24665-293) 4 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 178 Model 112 Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 179 Model 112 From RareAviation.com Rockwell International General Aviation Division Figure 53. Strut Assembly Main Landing Gear ISSUED: May 1972 180 Model 112 e Rockwell International General Aviation Division SECTION VIII Landing Gear Group STRUT ASSEMBLY MAIN LANDING GEAR FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NOS AFFECTED 45017-1 STRUT ASSEMBLY - Main Landing Gear, L.H. i One & Up 45017-2 STRUT ASSEMBLY - Main Landing Gear, R.H. i 53-1 45201-1 PISTON - Main Landing Gear 2 45202-3 PISTON ROD ASSEMBLY - Main Landing Gear 2 -2 45213-1 PISTON ROD - Main Landing Gear 2 -3 BEARING (LHA-9, Heim Universal Corp.) 4 -4 45204-1 PISTON TUBE - Main Landing Gear 2 -5 45205-1 PISTON PIN - Main Landing Gear 2 -6 45217-1 TRUNNION - Main Landing Gear, L.H. 1 45217-2 TRUNNION - Main Landing Gear, R.H. 1 -7 45211-1 BEARING - Main Landing Gear 2 -8 45212-1 ORIFICE - Main Landing Gear 2 -9 45214-1 TRUNNION PIN - Main Landing Gear 2 -10 45215-1 COLLAR - Main Landing Gear 2 -11 45260-1 STUD - Side Brace 2 -12 P252-18 AXLE - Main Landing Gear 2 -13 P252-21 YOKE, L.H. 1 P252-22 YOKE, R.H. 1 -14 45258-1 PIN - Knee Joint 2 -15 P252-27 ROD - Pin 2 -16 P252-29 SPACER - Wheel 2 -17 P252-30 NUT - Axel 2 -18 45259-1 BUSHING 4 -19 P252-42 STUD 2 -20 45019-1 A STUD 2 42308-1 BUMPER ASSEMBLY - Up Stop 2 -21 42308-3 PLATE 2 -22 BUMPER (9102-Q, Rubbercraft) 2 -23 SCREW (AN520-10-12) 2 -24 A0358 NUT (AN365-1032) 2 -25 58750 WASHER (AN960-10L) 2 -26 51276 BOLT (AN4-25A) 2 -27 51326 BOLT (AN4-27A) 2 -28 51425 BOLT (AN4-32A) 4 A Used Only on R.H. Assembly When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 181 Model 112 From RareAviation.com Rockwell International General Aviation Division STRUT ASSEMBLY MAIN LANDING GEAR SECTION VIII Landing Gear Group FIG. & INDEX PART NO. SERIAL NO'S NO. NUMBER CODE NOMENCLATURE REQ'D AFFECTED 5? 29 51852 BOLT (AN5-24A) 8 One & Up -30 58760 WASHER (AN960-416) 6 -31 58770 WASHER (AN960-416L) 2 -32 58780 WASHER (AN960-516) 8 -33 O-RING (AN6230-10) 2 -34 A2172 NUT (MS20365-428) 8 -35 NUT (MS20365-524) 8 -36 COTTER PIN (MS24665-293) 2 -37 RING (MS28774-331) 4 -38 65935 O-RING (MS28775-224) 2 -39 O-RING (MS28775-331) 2 -40 SCRADER RING (MS28776-23) 2 -41 AIR VALVE (MS28889-1) 2 -42 SCREW (MS35265-47) 2 -43 ROLL PIN (59-018-078-1000, Esna) 2 -44 RETAINING RING (N5000-200, Waldes Truarc) 4 -45 RETAINING RING (N5000-275, Waldes Truarc) 2 -46 RETAINING RING (N5000-300, Waldes Truarc) 2 -47 RETAINING RING (RST-225, Spirolox) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 182 Model 112 e Rockwell International General Aviation Division FIG.& INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REM SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. 183 Model 112 From RareAviation.com * Rockwell International General Aviation Division Figure 54. Brake and Wheel Assembly ISSUED: May 1972 184 Model 112 * Rockwell International General Aviation Division SECTION VIII Landing Gear Group BRAKE AND WHEEL ASSEMBLY FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 54-1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 -12 -13 -14 P5508 BRAKE ASSEMBLY (30-79, Cleveland Aircraft Products) BRAKE CYLINDER ASSEMBLY (091-05500, Cleveland Aircraft Products) SCREW - Bleeder (FC6446, Cleveland Aircraft Products) CAP - Bleeder (183-00100, Cleveland Air- craft Products) PRESSURE PLATE ASSEMBLY (073-01100, Cleveland Aircraft Products) BACKPLATE ASSEMBLY (074-01000, Cleveland Aircraft Products) FITTING - Tube (104-00500, Cleveland Aircraft Products) PISTON ASSEMBLY (092-01600, Cleveland Aircraft Products) BOLT (103-11600, Cleveland Aircraft Pro- ducts) WASHER (095-10200, Cleveland Aircraft Products) CYLINDER (061-04000, Cleveland Aircraft Products) ANCHOR BOLT (069-00400, Cleveland Air- craft Products) NUT (094-10300, Cleveland Aircraft Pro- ducts) TORQUE PLATE ASSEMBLY (075-07900, Cleve- land Aircraft Products) WHEEL ASSEMBLY (40-113A, Cleveland Aircraft Products) OUTER WHEEL HALF (162-04700, Cleveland Aircraft Products) RING - Gear Seal (153-00900, Cleveland Air- craft Products) 2 2 2 2 2 2 2 2 4 8 2 4 4 2 2 2 8 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 185 Model 112 From RareAviation.com Rockwell International General Aviation Division BRAKE AND WHEEL ASSEMBLY SECTION VIII Landing Gear Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGO SERIAL NOS AFFECTED 54-15 FELT - Gear Seal (154-00800, Cleveland Air- craft Products) 4 One & Up -16 RING - Snap (155-00100, Cleveland Aircraft Products) 4 -17 CONE - Bearing (214-00200, Cleveland Aircraft Products) 4 -18 INNER WHEEL HALF (161-04900, Cleveland Aircraft Products) 2 -19 BRAKE DISC ASSEMBLY (164-04300, Cleveland Aircraft Products) 2 -20 BOLT (103-11000, Cleveland Aircraft Products) 6 -21 WASHER (095-10400, Cleveland Aircraft Products) 6 -22 NUT (094-10300, Cleveland Aircraft Products) 6 -23 63903 INNER TUBE 600-6 2 -24 P6164 TIRE, TYPE III, 600-6, 4 PLY RATING 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 186 Model 112 SECTION ELECTRICAL GROUP From RareAviation.com Section IX ELECTRICAL GROUP 187 e Rockwell International General Aviation Division ISSUED: May 1972 Figure 55. Electrical Equipment Firewall 188 Model 112 From RareAviation.com Rockwell International General Aviation Division SECTION IX Electrical System Group ELECTRICAL EQUIPMENT FIREWALL FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 55-1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -24 -25 48002-1 43008-1 48299-1 68801 56801 A2406 59705 63949 56616 A1641 63122 62539 50826 P0253 A2172 P5332 56846 48264-1 63273 A0398 61574 56598 ELECTRICAL SYSTEM INSTALLATION FIREWALL ASSEMBLY GEAR WARNING BELL ASSEMBLY SPACER (NAS 1057T3-035) SCREW (AN526-832R12) TERMINAL STRIP (MS27212-2-7) SCREW (AN5156R6) NUT (NAS679AO6) OVERVOLTAGE RELAY (X16799, Prestolite Co.) SCREW (AN525-832R10) WASHER (AN960-8L) SHUNT (SW407616-P9, Stewart Warner) SOLENOID - Starter (SAN4204, Prestolite) SOLENOID - Relay (71311222, RBM Control) BOLT (AN4-4A) WASHER (AN960-416) NUT (MS20365-428) VOLTAGE REGULATOR (VSF-7202/3, Prestolite) SCREW (AN526-832R9) STRAP ASSEMBLY - Ground TERMINAL STRIP (17-141, Cinch Jones) SCREW (AN526-832R13) NUT (MS20365-832) GROMMET HOLDER (MT342, Arens) GROMMET ( ) GROMMET ( ) SCREW (AN520-10R5) i 3 3 1 2 2 1 2 6 1 1 1 6 6 6 1 4 1 1 4 4 3 3 6 9 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 189 Model 112 Rockwell International General Aviation Division Figure 56. Instrument Panel Electrical Installation ISSUED: May 1972 190 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION IX Electrical System Group INSTRUMENT PANEL ELECTRICAL INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 48002-1 ELECTRICAL SYSTEM INSTALLATION i One & Up 48240-1 MAIN PANEL ELECTRICAL INSTALLATION i 48290-1 CIRCUIT BREAKER SWITCH PANEL ASSEMBLY i 48237-1 CIRCUIT BREAKER SWITCH ASSEMBLY i 56-1 60434 CIRCUIT BREAKER (2010 2-AC-15, Texas Instrument) 4 -2 60435 CIRCUIT BREAKER (20TC 2-AC-10, Texas Instrument) 1 -3 60436 CIRCUIT BREAKER (20TC 2-AC-5, Texas Instrument) 1 -4 48225-1 BUSS BAR 1 -5 59619 SCREW (AN507-632R4) 12 48244-1 SWITCH BRACKET ASSEMBLY 1 -6 48245-1 BRACKET 1 -7 P7O78 NUT PLATE (NAS697 A06) 6 48231-1 SWITCH ASSEMBLY - Flap Actuator 1 -8 65853 TOGGLE SWITCH (MS25201-6) 1 -9 48261-1 HANDLE - Flap Switch 1 -10 59621 SCREW (AN507-632-6) 1 -11 63274 TERMINAL STRIP (5-141, Cinch Jones) 1 -12 56625 SCREW (AN526-632R6) 6 -13 56801 SCREW (AN526-832R12) 4 -14 A1641 WASHER (AN960-8L) 4 -15 A0398 NUT (MS20365-832) 4 48239-1 LANDING GEAR SWITCH & WARNING LIGHT INSTALLATION 1 48287-1 LANDING GEAR SWITCH & LIGHT ASSEMBLY 1 -16 61572 LAMPHOLDER - Green (5148-636-609, Drake) 3 -17 61252 LAMP (330) 3 -18 63407 SWITCH - Landing Gear (8906 K2516, Cutler-Hammer) 1 48215-1 DIMMER INSTALLATION 1 48291-1 DIMMER ASSEMBLY 1 -19 P5360 RHEOSTAT (0 110, Ohmi 2 -20 62129 KNOB (RB-67-0-OC-M, Rogan) 2 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 191 Model 112 e Rockwell International General Aviation Division INSTRUMENT PANEL ELECTRICAL INSTALLATION SECTION IX Electrical System Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NOS AFFECTED 56-21 48241-1 SUB-PANEL INSTALLATION i 63776 IGNITION & STARTER SWITCH (10-357210-1, Bendix) i -22 63777 POSITION INDICATING DIAL (10-187468, Bendix) -23 48249-1 BUS BAR i -24 60444 CIRCUIT BREAKER (MP-1648-001-70, Mechanical Products) i -25 60443 CIRCUIT BREAKER (MP-1600T-35, Mechanical Products) i -26 60440 CIRCUIT BREAKER (MP-1600T-10, Mechanical Products) 5 -27 60442 CIRCUIT BREAKER (MP-1600T-5, Mechanical Products) 12 -28 P3565 CIRCUIT BREAKER (109-205-101, Wood) 1 -29 63275 48272-1 TERMINAL STRIP (10-164, Cinch Jones) MASTER SWITCH & BATTERY CIRCUIT BREAKER ASSEMBLY 1 -30 63412 SWITCH (8143K21-E13P50, Cutler Hammer) 1 -31 61578 LAMPHOLDER (4090-308, Drake) 4 -32 62153 LAMP (1813) 4 -33 61421 FILTER CAP - Red (1813/8, APM Hexseal Corp.) 4 -34 56608 SCREW (AN526-632-4) 4 -35 55377 NUT (MS20364-632) 4 48211-1 STALL WARNING HORN INSTALLATION 1 -36 56836 SCREW (AN526-832R7) 4 -37 A1641 WASHER (AN960-8L) 4 -38 A0398 NUT (MS20365-832) 4 48267-1 STALL WARNING HORN ASSEMBLY 1 -39 43416-1 BRACKET 1 -40 43420-1 PLATE - Insulator 1 -41 61652 HORN (A-2933, Delta Electronics) 1 -42 56792 SCREW (AN526-832R4) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 192 Model 112 From RareAviation.com e Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 193 Model 112 e Rockwell International General Aviation Division Figure 57. Battery and External Power Unit Installation ISSUED: May 1972 194 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION IX Electrical System Group BATTERY & EXTERNAL POWER UNIT INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. RECTO SERIAL NOS AFFECTED 48246-1 BATTERY INSTALLATION i 57-1 BATTERY (S-25, Rebat) i A BATTERY (R-35-Rebat) i 48224-1 RELAY INSTALLATION - Battery Box i 43425-1 BATTERY BOX ASSEMBLY i -2 43426-1 BATTERY BOX i 43430-1 BRACKET ASSEMBLY 3 -3 43431-1 BRACKET 3 -4 62619 RECEPTACLE (99833-C. 130, Cinch) 3 43442-1 COVER ASSEMBLY 1 -5 43427-1 COVER 1 -6 43432-1 ISOLATION PAD 3 -7 43434-1 SEAL - Battery Hold Down 2 -8 43435-1 SEAL - Box Cover 1 -9 43436-1 SEAL - Box Cover 1 -10 43437-1 BRACKET 3 -11 59266 STUD (98292-1-110, Cinch) 3 -12 62357 PIN (99836, Cinch) 3 -13 66591 SCREW (MS35493-25) 4 -14 43438-1 DOUBLER 2 -15 43440-1 BRACKET 2 -16 66175 GROMMET (MS35489-41) 2 -17 48268-1 DOUBLER 2 -18 62551 SOLENOID (71111224, RBM Controls) 3 -19 50826 BOLT (AN4-4A) 6 -20 P0253 WASHER (AN960-416) 6 -21 55401 NUT (MS20365-428C) 6 -22 43418-1 TUBE - Battery Drain 1 -23 66182 CLAMP (MS35842-10) 1 -24 66161 GROMMET (MS35489-16) 1 -25 P0007 BOLT (AN3-43A) 2 -26 A1616 WASHER (AN960-10) 4 -27 A2167 NUT (MS20365-1032) 2 A - Optional Equipment When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 195 Model 112 Rockwell International General Aviation Division BATTERY & EXTERNAL POWER UNIT INSTALLATION SECTION IX Electrical System Group FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 57-28 -29 -30 -31 -32 -33 -34 -35 48226-1 A0052 43455-1 43456-1 43457-1 43458-1 63002 A0130 AO358 EXTERNAL POWER UNIT INSTALLATION A.P.U. RECEPTACLE (AN2552-3A) BRACKET DOOR HINGE ASSEMBLY DOUBLER DOOR SPRING (50-10-102-10, Southco) BOLT (AN3-7A) NUT (AN365-1032) i i i i i i i 2 2 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 196 From RareAviation.com Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REOD SERIAL NO'S AFFECTEDTHIS PAGE INTENTIONALLY LEFT BLANKWhen Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 197 Model 112 e Rockwell International General Aviation Division Figure 58. Night Lighting Installation ISSUED: May 1972 198 Model 112 From RareAviation.com * Rockwell International General Aviation Division SECTION IX Electrical System Group NIGHT LIGHTING INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NOS AFFECTED 48012 DRAWING - Night Lighting Installation One & Up 58-1 43501-1 BRACKET - Power Supply i 48107-1 DIMMER RELAY ASSEMBLY i -2 RELAY (1R-1225-2C-12D, Guardian Inc.) i -3 62303 PLUG (1-480-319-0, AMP Inc.) i 48209-1 TIME DELAY ASSEMBLY i -4 48208-1 BRACKET - Time Delay i -5 RELAY (1R-1225-2C-12D, Guardian Inc.) i -6 TUBE SOCKET (47C0415, Allied Electric Inc.) i -7 48214-1 BRACKET - Dimmer Control i -8 48227-1 COUPLER - Dimmer Control i -9 48234-1 SHAFT - Dimmer Control i 48243-1 STROBE SWITCH ASSEMBLY i -10 63410 SWITCH (8142K21E6P50 i, Cutler - Hammer) i -11 62301 PLUG (1-480305, Amp Inc.) i 48270-1 NAV LITE ASSEMBLY - Wing, L.H. i 48271-1 NAV LITE ASSEMBLY - Wing, R.H. i -12 62303 PLUG (1-480319-0,Amp Inc.) 2 -13 NAV LITE , L.H. (A1815A-R12, Grimes Mfg. Company) 1 -14 NAV LITE, R.H. (A1815A-G12, Grimes Mfg. Company) 1 48273-1 NAV LITE ASSEMBLY - Rear 1 -15 62309 PLUG (1-480-426-0, Amp Inc.) 1 -16 NAVE LITE (A2064-12, Grimes Mfg. Co.) 1 -17 POST LIGHT (A8970B-1-330, Grimes Mfg. Co.) 4 -18 62192 LAMP (336, G. E.) 2 -19 LAMPHOLDER (2506-1, Leecraft Mfg. Co.) 2 -20 LIGHT (51-G3-1135T, Leecraft Mfg. Co.) 2 -21 LIGHT (2690A14, Industrial Devices Inc.) 2 -22 STROBE LIGHT (A434-14, Whelen Engineering Co.) 2 -23 STROBE LIGHT (A430-14, Whelen Engineering Co.) 1 STROBE LIGHT (X2RD, Aeroflash Signal Corp.) 3 -24 STROBE LIGHT (A408-14, Whelen Engineering Co.) 1 STROBE LIGHT (XIEB, Aeroflash Signal Corp.) 1 -25 STROBE LIGHT (A450, Whelen Engineering Co.) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 199 Model 112 Rockwell International General Aviation Division NIGHT LIGHTING INSTALLATION SECTION IX Electrical System Group FIG. INDEX NO, PART NUMBER CODE NOMENCLATURE NO. REQ'D SERIAL NO'S AFFECTED 58-26 -27 -28 -29 -30 -31 -32 -33 63418 63417 62203 STROBE LIGHT (X1EC, Aeroflash Signal Corp.) POWER SUPPLY (73140, Aeroflash Signal Corp.) POWER SUPPLY (HDT3-14, Whelen Engineering Co.) POWER SUPPLY (A1EB-12, Aeroflash Signal Corp.) POWER SUPPLY (HD-14, Whelen Engineering Co.) SWITCH (1DM21, Micro Switch) SWITCH (1DM1, Micro Switch) SWITCH (P3-32112, Otto Controls Div.) RELAY (12C180, Amperite) LIGHT ASSEMBLY (10-0527-1, Grimes) LIGHT ASSEMBLY (312111, Leecraft Mfg. Co.) i 3 1 1 1 1 2 1 1 5 1 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 200 Model 112 From RareAviation.com SECTION ELECTRONICS GROUP 201 Section X ELECTRONICS GROUP From RareAviation.com Rockwell International General Aviation Division Figure 59. Radio System Installation ISSUED: May 1972 202 Model 112 e Rockwell International General Aviation Division SECTION X Electronics Group RADIO SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 59-1 48700 48701 48702 48054-13 DRAWING - Radio System Installation DRAWING - Narco Radio Installation DRAWING - King Radio Installation TUBE - Plastic, R.H. i One & Up -2 48054-15 TUBE - Plastic, L.H. i -3 48054-13 TUBE - Plastic, R.H. i -4 48054-17 TUBE - Plastic, L.H. i 48715-1 BRACKET ASSEMBLY - URG-2 i -5 48715-3 BRACKET i -6 NUTPLATE (AN362-F632) 4 48717-1 FLANGE PLATE ASSEMBLY - Radio Air 2 -7 46098-1 TAKEOFF - Air 4 -8 48716-1 FLANGE PLATE - Radio Air 2 -9 48718-1 SCOOP - Radio Air 2 -10 48728-1 WICK ASSEMBLY - Static Discharge 3 -11 48739-1 BRACKET - Speaker 2 -12 49087-1 PLATE - Sunvisor 1 -13 49087-3 PLATE - Sunvisor 1 -14 55474 NUT (AN365-632) 10 -15 A0398 NUT (AN365-832) 2 -16 SCREW (AN509-8-22) 2 -17 A109 3 SCREW (AN526-632-8) 10 -18 56838 SCREW (AN526-832R8) 1 -19 58720 WASHER (AN960-6) 10 -20 58719 WASHER (AN960-8L) 2 -21 58734 WASHER (AN960D8L) 8 -22 NUT (MS20364-832) 1 -23 SCREW (MS24618-31) 8 -24 63187 SPEAKER (P5, Electronic Research) 2 -25 62256 MICROPHONE (61600-01, Telex) 1 -26 CAPACITOR (48P60, Sprague Products Co.) 1 -27 62098 JACK (JJ-033, Amp Inc.) 2 -28 62099 JACK (JJ-034, Amp Inc.) 2 -29 PLUG (1480318, Amp Inc.) 1 When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 203 Model 112 From RareAviation.com e Rockwell International General Aviation Division Figure 60. Antenna System Installation 204 ISSUED: May 1972 Model 112 e Rockwell International General Aviation Division SECTION X Electronics Group ANTENNA SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REGD SERIAL NO'S AFFECTED 48705 DRAWING - Antenna Installation One & Up 60-1 43360-5 A DORSAL FAIRING ASSEMBLY - Antenna i 48725-1 ANTENNA ASSEMBLY - Omni i -2 48721-1 CABLE ASSEMBLY - Omni Antenna i -3 48722-1 BASE BLOCK - Omni Antenna i -4 48724-1 ANTENNA - Omni 2 -5 55149 NUT (AN345C10) 4 -6 A2167 NUT (MS20365-1032) 2 -7 48731-1 DOUBLER - Broadband Antenna 1 -8 48732-1 STIFFENER - Sense Antenna 1 -9 48733-1 DOUBLER - Sense Antenna 1 -10 48734-1 CLIP - Antenna 1 -11 48735-1 BRACKET - Antenna 1 -12 48736-1 STRAP - Antenna 1 -13 48738-1 DOUBLER - Antenna 1 -14 50026 BOLT (AN3-5A) 10 -15 54977 NUT (AN340-6) 14 -16 NUT (AN340C8) 10 -17 55125 NUT (AN345-10) 2 -18 SCREW (AN515C8-14) 10 -19 56611 SCREW (AN526-632-5) 14 -20 56910 SCREW (AN526-1032-20) 2 -21 58621 WASHER (AN936B6) 14 -22 WASHER (AN960C8L) 10 -23 58750 WASHER (AN960-10L) 10 -24 SCREW (MS24693S272) 2 -25 SCREW (NAS221-21) 2 -26 SPACER (NAS43DD3-64) 2 -27 62090 INSULATOR (6007, Johnson Insulator) 1 -28 INSULATOR ASSEMBLY (37F081, Type 135-40, Johnson Insulator) 1 -29 60740 SPRING (NAF1086-4, Johnson Insulator) 1 -30 ANTENNA ASSEMBLY (UDA-3, Narco Avionics) 1 -31 ANTENNA ASSEMBLY (AT-50, Narco Avionics) 1 -32 ANTENNA ASSEMBLY (071-1006-10, King Radio Corp.) 1 82102 ANTENNA ASSEMBLY (2321E, Bendix Radio Div.) 1 -33 ANTENNA ASSEMBLY (01073-10, Narco Avionics) 1 A When 43360-5 is installed, 43360-1 should be omitted. When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 205 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION X Electronics Group ANTENNA SYSTEM INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 60-34 -35 -36 -37 -38 -39 -40 82142 80058 80059 ANTENNA ASSEMBLY (AD-8, Antenna Development Company) ANTENNA ASSEMBLY (EMB10-14, Communications Components Corp.) ANTENNA ASSEMBLY (AT908A, Bendix Radio Div.) ANTENNA ASSEMBLY (DMN42-1, Dome and Margolin Inc.) ANTENNA ASSEMBLY (VNA-10, Narco Avionics) ANTENNA ASSEMBLY (SA10-94, Communications Components Corp.) ANTENNA ASSEMBLY (DMC58-1, Dome and Margolin Inc.) ANTENNA ASSEMBLY (AT-907A, Bendix Radio Div.) ANTENNA ASSEMBLY (AD-11, Antenna Development Company) ANTENNA ASSEMBLY (VHF-1, Meriden Electronics Corp.) ANTENNA ASSEMBLY (VHF-1B, Meriden Electronics Corp.) ANTENNA ASSEMBLY (AT-912A, Bendix Radio Div.) ANTENNA ASSEMBLY (GS10-06, Communications Components Corp.) ANTENNA ASSEMBLY (A-326-A, Aircraft Radio Corp.) ANTENNA ASSEMBLY (AT-904A, Bendix Radio Div.) ANTENNA ASSEMBLY (RGS10-48, Communications Components Corp.) i i i i i i 2 2 2 1 1 1 1 1 1 1 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 206 Model 112 * Rockwell International General Aviation Division SECTION X Electronics Group AUTOPILOT INSTALLATION FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NOS AFFECTED 48101 DRAWING - Autopilot System Installation One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 207 Model 112 From RareAviation.com Rockwell International General Aviation Division FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED| THIS PAGE INTENTIONALLY LEFT BLANK |When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 208 Model 112 SECTION MISCELLANEOUS From RareAviation.com 209 Section XI MISCELLANEOUS Rockwell International General Aviation Division W| Aero CommanderkFigure 61. Interior and Exterior Markings ISSUED: May 1972 210 Model 112 From RareAviation.com * Rockwell International General Aviation Division SECTION XI Miscellaneous Group INTERIOR AND EXTERIOR MARKINGS FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REDD SERIAL NO'S AFFECTED 61-1 -2 -3 -4 -5 -6 49046-1 49064-3 49064-5 49064-7 49067-3 49067-4 49085-1 DECAL - Exterior Name Plate DECAL - Exterior Identification DECAL - Exterior Identification DECAL - Exterior Identification DECAL - Exterior Logo, L. H. DECAL - Exterior Logo, R.H. MEDALLION - Control Wheel One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 211 Model 112 Rockwell International General Aviation Division Aero Commander Division North American Rockwell MODEL NO. SERIAL NO. T. C. NO. P. C. NO. ALBANY, GEORGIA FUEL 100 OCTANE MIN 30 GAL. USABLE NO OPEN CLOSED NOSE NOSE LEFT RGHT RUDDER TRIM WARNING RELEASE AIR IN STRUT BEFORE DISASSEMBLY DESIGN MANEUVERING SPEED- MAX. LANDING GEAR SPEED-- MAX. SPEED 20 ELAPS______ MAX. COWL FLAP SPEED____ ALL MARKINGS AND PLACARDS ON THIS AIRPLANE APPLY TO ITS OPERATION AS A NORMAL CATEGORY AIRPLANE. FOR UTILITY CATEGORY OPERATION REFER TO the airplane flight manual. NO PASSENGERS IN REAR SEAT OR BAGGAGE IN BAGGAGE COMPARTMENT DURING UTILITY CATEGORY OPERATIONS. CLOSE N1002J 14 OPEN THIS AIRPLANE IS APPROVED FOR FLIGHT IN DAY/NIGHT VFR HER WHEN EOUIPPED IN ACCORDANCE WI TH FAR 01. F| |GHT INTO KNOWN ICING CONDITIONS PROHIBITED. NO ACROBATIC MANEUVERS ARE APPROVED FOR NORMAL CATEGORY OPERATION. INTENTIONAL SPINS ARE PROHIBITED. 15 OIL CAP 8 QTS TEMP E SAE NO. ABOVE 60 30 90 0- 70 BELOW 10 50 40 30 20 AERO COMMANDER DIV. NORTH AMERICAN ROCKWELL PART NO. | ________________ SERIAL NO. | ________________ DATE MFG. |________________ SERVICING INSTRUCTIONS REMOVE AIR VALVE AND FULLY EXTEND STRUT. WITH VALVE IN VERTICAL POSITION, FILL. TO OVERFLOWING WITH MIL-H-5606 HYDRAULIC FLUID. FULLY COMPRESS STRUT TO REMOVE EXCESS OIL. REPLACE AIR VALVE. WITH NO LOAD ON STRUT INFLATE WITH NITROGEN OR CLEAN DRY AIR TO E^PS.IG. TIRE PRESSrnPSLG 11 o LANDING GEAR EMERGENCY DOWN PULL OUT AND PUSH DOWN _______ BAGGAGE DOOR LIGHT FINISH & TRIM __________________ DO NOT OPEN IN EXCESS OF 130 KNOTS o 17 DEC NC FR CT ON LOCK F igure 62. Interior and Exterior Placards ISSUED: May 1972 212 Model 112 From RareAviation.com e Rockwell International General Aviation Division SECTION XI Miscellaneous Group INTERIOR AND EXTERIOR PLACARDS FIG. & INDEX NO. PART NUMBER CODE NOMENCLATURE NO. REQD SERIAL NO'S AFFECTED 62-1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 -12 -13 -14 -15 -16 -17 40125-1 40131-1 40132-1 40133-1 40133-2 40134-1 45315-1 45316-1 47412-1 49071-1 49071-3 49076-1 49077-1 49077-2 49086-1 49092-1 49307-1 49307-3 49307-7 PLACARD - Manufacture Identification PLACARD - Fuel PLACARD - Oil PLACARD - Door Latch, L.H. PLACARD - Door Latch, R.H. PLACARD - No Step PLATE - Caution PLATE - Identification DISK - Rudder Trim Indicator PLACARD - Limitation PLACARD - Airspeed PLACARD - Emergency Gear Down PLACARD - Door Open & Close, L.H. PLACARD - Door Open & Close, R.H. PLACARD - Pilot Window PLACARD - Registration PLACARD - Finish & Trim PLACARD - Baggage Light PLACARD - Friction Lock i i i i i 2 3 3 1 1 1 1 1 1 1 1 1 1 1 One & Up When Ordering, Always Specify Part Number, Nomenclature And Serial Number of Aircraft. ISSUED: May 1972 213 Model 112