Mooney aircraft M20C E F G IPC parts manual

NIO ON EY PARTS CATALOG IssvEo 1976 REV. JUNE 1917 APPLICABLE TO THE FOLLOWING AIRCRAFT RANGER ~(CHAPARRAL MODEL SERIAL NUMBER MODEL SERIAL NUMBER 1968 M20C 680001 thru 680198 1969 M2dE 690001 thru 690073 1969 M20C 690001 thru 690098 1970 M20E 700001 thru 700061 1970 M20C 700001 thru 700091 1971 M20E 21-0001 rhru 21-0023 1971 M20C 20-0001 thru 20-0009 1974 M20E 21-0024 thru 21-0060 1974 M20C 20-0010 thru ?0-004_6 1975 M20E 21-1161 thru 21-1180 1975 20-1147 thru 20-1185 1976 M20C 20-1186 h ON END EXECUTIVE ~(STATESMAN MO DE L SERIAL NUMBER MODEL SERIAL NUMBER 1968 M20F 680001 thru 680206 1968 M20G 680001 thru 680164 1969 M20F 690001 thru 690092 1969 M20G 690001 thtu 690020 1970 M20F 700001 rhru 700072 1970 M20G 700001 thru 700006 1971 M20F 22-0001 thru 22-0012 1974 M20F 22-0013 thru 22-0078 END i975 M20F 22-1179 thru 22-1305 1976 M20F 22-1306 8 ON MOONEY AIRCRAFT CORPORATION f~L P.O. BOX 72 KERRVILLE,TEXAS 78028 SUBSIDIARY OF REPUBLIC STEEL MANUAL NUMBER MAN 205 A www.repairmanuals4u.com

LIST OF REVISED PAGES ISSUED INSERT LATEST REVISED PAGES--DESTROY SUPERSEDED PAGES. DATE OF DATE OF PAGE NUMBER LATEST REVISION PAGE NUMBER LATEST REVISION "36 June, 1917 *38 June, 1917 "39 June, 1977 *48 June, 1977 *51 June, 1977 *52 June, 1977 *53 June, 1977 "54/55 BLAN~K June, 1977 *119 June, 1977 "139 June, 1977 "140 June, 1977 *187 June, 1977 *221 thru 328 Added *THE ASTERISK INDICATES PAGES REVISED, ADDED, OR DELETED BY THE CURRENT REVISION. ADDITIONAL COPIES OR CURRENT REVISIONS OF THIS PUBLICATION MAY BE PURCHASED FROM YOUR LOCAL MOONEY DISTRIBUTOR OR DEA LER. www.repairmanuals4u.com

FOREWORD placement parts for Mooney M20 series aircraft, 1968 models and on.This illustrated parts catalog is designed to assist in the identification of standard re-The 1965-1967 parts catalog should be referenced for parts applicable to aircraft serial numbers prior to 680001. INTRODUCTION The Introduction section should be read carefully to become familiar with the catalog arrangement and the cor- rect procedure in ordering parts. A group assembly index is included to help locate figure illustrations in the catalog. GROUP ASSEMBLY PARTS LISTINGS The body of the catalog lists all standard replaceable parts in the aircraft. No attempt has been made to list optional equipment items. Each illustration is accompanied by an assembly breakdown in its adjacent text. Those parts not listed separately are items that lose their identity through being an integral part of assemblies which would be impracticable to stock other than as complete assemblies. Common hardware used in tube and wire routing is not listed, since such items are seldom replaced or are readily available at aircraft maintenance stations. APPENDIX The numerical index lists all Mooney-manufactured parts in the catalog and the pages on which they are entered. TO LOCATE A PART One or both of the indexes can be used in locating parts in the body of the catalog: The GROUP ASSEMBLY INDEX in the introduction section of the manual lists titles and page numbers of all group assembly illustrations in the catalog. Illustration index numbers refer to index numbers in the adjoining texts (parts callouts). The NUMERICAL INDEX in the appendix section of the manual tabulates all Mooney-manufactured part numbers listed in the catalog body with the pages on which they are entered. The following is a brief explanation of the columns and abbreviations in the parts listings: The FIGURE INDEX NO. column shows the illustration figure number only at the top of each parts listing page. The figure number is followed by a dash and the index number. These index numbers are key ed to those in the accompanying illustration. Encircled illustration index numbers, without leader lines, are used to designate the entire adjacent assembly shown as a unit. Index numbers should not be used in identifying parts for ordering purposes. The PART NUMBER column identifies the item by its assembly or detail part number. This is the part number to be used in making an order. Mooney print numbers are used In preference to vendor numbers where possible. The DESCRIPTION column is divided into subcolumns to show the analysis by partition assemblies into parallel levels of subassemblies and detailparts. Attaching hardware or parts, indented with the symbol are required for installation of one unit of the foregoing assembly. ~itructural rivets are not tabu- lated, since they are often replaced in larger sizes. The abbreviation’TJI" designates the more signif- Lcant nonlllustrated Items. Attaching hardware or parts immediately follow the item they attach and pre- cede any detail parts of the foregoing assembly in the text callout, unless the detail parts of the assembly are not individuallv illustrated. When detail parts of the assembly are not individually portrayed, the attaching parts follow the detail parts. An assernblv includes all constituent subassemblies ordetail parts effective for the same model and serial number land color when applicable) that follow in that listing with a greater degree of indention to the right. Thus, a detail part can be traced to its respective higher assembly (that to which it assembles) by reading up to the first assembly listing or group of related assemblies in the first subcolumn to the left. Parts of the same description, differing only as left and right hand units, are listed together and are followed by both identical component parts and those which are peculiar to either the left or right hand as- semblles. Series of nonillustrated detail parts are listed by their spatial order within the assembly as follows: forward to aft, top to bottom, inboard to outboard, and left to right. www.repairmanuals4u.com

It should be noted that some portrayed assemblies bearing encircled index numbers omit some of the more significant detailparts (such as skins) for the purpose of clarity. Abbreviations used in the description column are as follows: ~2 attaching parts WS wing station IB inboard NI not illustrated FS fuselage station OB outboard LH left hanci BL butt line LE leading edge RH right hand AR as required TE trailing edge Each entry in the UNITS PER ASSEMBLY column represents the total number of that part or assembly used In or for one unit of the next higher assembly. Consequently, when an entry has an indented or part description, its units per assembly column shows the number of items required to complete or attach one of the next higher assembly of which it is a component or an attaching part. The EFFECTIVITY column is blank where the part is applicable to all M20 series aircraft released from the factory October 15, 1967 through the latest catalog revision date on the lead page. An entry in the effectivity column indicates a special or limited use of that part. When the effectivity of a part is re- stricted to model the following letter codes are used; "C" limits the applicability of that part to aircraft with serial number 680001C ON; "E" limits the applicability of that part to the M20E model, serial number 690001 ON; "F" limits the applicability of that part to the M20F model, serial number 680001 ON;’%" limits the applicability of that part to the M20G model, serial number 680001 ON. When effectivities change within the model year, the symbol plus a Roman numeral refers to a footnote serial number explanation printed on the last page of the figure text. HOW TO ORDER PARTS Place your order with the Mooney Marketing or Service Center in your area. Parts are available only through the authorized Mooney facilities, and all orders received at the factory that originate from other sources will be referred to the appropriate facility for processing. Always specify the PART NUMBER, DESCRIPTION and QUANTITY of parts desired. Be sure to include the part CODE NUMBER when listed in the Parts Price List manual and indicate the MODEL and SERIAL NUMBER of the aircraft for which the parts are intended. Give complete address information including the zip code. When the method of shipment (freight, express, parcel pust, air express, air freight, or air parcelpost) is not specified, or when thenature oftheshipmentrequires special handling, parts will be shipped by the means most suitable to the shipper. LIABILITIES Orders are double checked before leaving the shipping department, and a packing slip is enclosed in the shipment. Claims for errors or shortages must be made within three days after receipt of orders, and no material should be returned without first obtaining written permission from the factory. Goods returned without notice will be held at owner’s risic for thirty days and then be disposed of at the company’s discretion. Transportation charges for returned goods must be prepaid or the shipment will be refused. Mooney Corporation cannot be held liable for damage to parts incurred in transit. If a shipment is received in a damaged condition, have the de- livery man or shipping company make a notation of the damage and file the claim with the carrier. CAUTION This parts catalog is intended only to aid in the ordering of replacement parts. The illustrations omit many details for the sake of clarity. Dimensions, systems routing, and irrelevant details have been intentionally dis- torted for maximum economy of space utilization. Therefore, it is essential that the illustrations not be used as guides for reassembly and installation of parts. www.repairmanuals4u.com

GROUP ASSEMBLY INDEX www.repairmanuals4u.com

WING GROUP 6 POWER PLANT GROUP 2 FUSELAGE TAIL CONE GROUP 7 SYSTEMS GROUP, MISC. 3 EMPENNAGE GROUP 8 CABIN INTERIOR GROUP 4 CHASSIS GROUP 9 EXTERIOR TRIM GROUP 5 CONTROL SYSTEMS GROUP 10 ELECTRICAL GROUP 3 d 2 7~ ~1 ~n7, r t LMI:~ 9) (5 6 10 4 www.repairmanuals4u.com

GROUP ASSEMBLY INDEX PAGE WING GROUP FIG. 1 WING ASSEMBLY INSTALLATION 2 FIG. 2 WING MAIN SPAR MAIN LANDING GEAR ATTACH ASSEMBLIES 6 FIG. 3 WING STUB REAR SPAR ASSEMBLIES 12 FIG. 4 WING CENTER SECTION 16 FIG. 5 WING SKINS INSPECTION COVERS 24 FIG. 6 WING OUTBOARD SECTION 28 FIG. 7 WING AILEiRON FLAP ASSEMBLIES ..32 FUSE LAGE GROUP FIG. 8 ENGINE COWL;ING 36 FIG. 9 CABIN TUBULAR STRUCTURE 40 FIG. 10 FIREWALL ASSEMBLY CABIN SKINS 48 FIG. 11 BELLY SKINS AND INSPECTION COVERS 56 FIG. 12 TAIL CONE SECTION 60 FIG. 13 FLOORBOARD SECTION 68 FIG. 14 INSTRUMENT PANEL STRUCTURE (1968) 74 FIG. 14A INSTRUMENT PANEL STRUCTURE (1969-1974) 78 FIG. 14B INSTRUMENT PANEL STRUCTURE (1975 ON) 84 FIG. 15 CABINDOOR (1968-1975) 86 FIG. 15A CABIN DOOR (1975 later) 90 FIG. 16 BAGGAGE DOOR 94 FIG. 17 WINDSHIELD WINDOWS ~96 EMPENNAGE GROUP FIG. 18 EMPENNAGE ASSEMBLY INSTALLATION 102 FIG. 19 HORIZONTAL STABILIZER STINGER ASSEMBLY 104 FIG. 20 VERTICAL STABILIZER ASSEMBLY INSTALLATION 110 FZG. 21 ELEVATOR RUDDER ASSEMBLY INSTALLATION (1968).....~ 114 FIG. 21A ELEVATOR RUDDER ASSEMBLY INSTALLATION (LATE 1968 ON) .118 CHASSIS GROUP FIG. 22 MAIN GEAR ASSEMBLY INSTALLATION ..........122 FIG. 23 NOSE GEAR ASSEMBLY INSTALLATION ..........126 FTG. 24’- WHEEL TIRE ASSEMBLIES .130 FIG. 25 MANUAL GEAR RETRACTION SYSTEM .132 FIG. 25A ELECTRIC GEAR RETRACTION SYSTEM ..........136 FIG. 26 GEAR DOOR ASSEMBLIES RETRACTION MECHANISMS .142 www.repairmanuals4u.com

PAGE FLIGHT CONTROL SYSTEMS GROUP FIG, 27 AILERON CONTROL SYSTEM 146 FIG, 28 ELEVATOR CONTROLSYSTEM 150 FIG, 29 RUDDER CONTROL NOSE GEAR STEERING SYSTEM 156 FIG, 30 FLAP CONTROL SYSTEM (KYDRAULIC) 160 FIG, ’30A FLAP CONTROLSYSTEM (ELECTRIC) 166 FIG. 31 TRIM CONTROL SYSTEM 170 FIG, 32 POS~IVE CONTROL SYSTEM 174 POWER PLANT GROUP FIG, 33 ENGINE PROPELLER INSTALLATION 178 FIG, 34 INDUCTIONSYSTEM 182 FIG, 35 EXHAUST SYSTEM 186 FIG, 36-FUELSYSTEM. .,..,,,,.,,,,,,_ 190 FIG, 37 FUEL AND MANIFOLD PRESSURE SYST‘EMS 196 FIG. 38 ENGINE CONTROLS (1968thru 1974)............ 198 FIG, 38A ENGINE CONTROLS (1975 on) 206 FIG, 39 OIL SYSTEM 214 FIG. 40 ENGINE BAFFLE SYSTEM (M20C G) 218 FIG, 40A ENGINE BAFFLE SYSTEM (M20E Fl 222 MISCELLANEOUS SYSTEMS GROUP FIG, 41 FLIGHT INSTRUMENTS (1969 on) 228 FIG, 41A FLIGHT INSTRUMENTS (1968) 232 FIG, 42 ENGINE INSTRUMENTS (1969 oIj 236 FIG, 42A ENGINE INSTRUMENTS (1968) 240 FIG, 43 VACUUMSYSTEM 244 FIG, 44 PITOT STATIC PRESSURE SYSTEMS 248 FIG, 45 CABIN HEATING SYSTEM (1968 thru 1974) 252 FIG, 45A CABIN HEATING SYSTEM (1975 on) 260 FIG, 46 OVERHEAD VENTILATION SYSTEM 264 FIG, 47 HYDRAULIC BRAKE SYSTEM 268 FIG, 48 COWL FLAP CONTROL SYSTEM 274 FIG, 49 RETRACTABLE AND FIXED STEP 278 CABIN INTERIOR GROUP FIG, 50 FRONT SEAT ASSEMBLIES 282 FIG, 51 REAR SEAT ASSEMBLIES 286 FIG, 52 CABININTERIOR FURNISHINGS (C E) 292 FIG, 52A CABIN INTERIOR FURNISHINGS (F G) 296 FIG, 53 CABININSULATION 302 FIG, 54 DECALS PLACARDS (1968) 304 FIG, 54A DECALS PLACARDS (1968) 306 FIG, 54B DECALS PLACARDS (1968) 308 vi www.repairmanuals4u.com

PAGE FIG. 55 DECALS PLACARDS (1969-1975) 310 FIG;. 55A DECALS PLACARDS (1969-1975). 312 FIG. 55B DECALS PLACARDS (1969-1975). 314 FIG. 55C DECALS PLACARDS (1969-1975). 316 FIG. 56 DECALS PLACARDS (1976) 318 FIG. 56A DECALS PLACARDS (1976) 326 FIG. 56B DECALS PLACARDS (1976) 322 EXTERIOR TRIM GROUP FIG. 57 PAINT CHART 324 FIG. 57A MATERIAL PAINT CHART (1968-1973) 325 FIG. 57B MATERIAL PAINT CHART (1974-1916) 326 ELECTRICAL SYSTEM GROUP NOTE: For electrical system schematics and parts listings see Service Maintenance Manual (Manual #106). vii/viii Blank www.repairmanuals4u.com

VVIN G GROUP www.repairmanuals4u.com

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Mooney aircraft M20C E F G IPC parts manual

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