AIRCRAFT SPECIFICATION NO. 2A3

(or alternate) Facet, (Balkamp) P/N 476-027............................................... 2 lbs. ....................... +19.0 102. .......Oil Radiator (a) Harrison, 8523425........................................................................................ 3 lbs. ....................... -18.0 (b) Harrison, 8526250........................................................................................ 2 lbs. ....................... -18.0 103. .......Induction Air Filter (a) Air Maze, 13219 .......................................................................................... 1 lb........................... -17.0 104. .......Starters (a) Delco-Remy, 1109657 ................................................................................. 17 lbs. ...................... -18.0 105. .......AuxiliaryFuel Tank (a) Mooney Instl. Dwg. 6071 ............................................................................ 11 lbs. ...................... +68.0 Landing Gear: 201. .......Two, Main Wheel/Brake Assemblies, 6.00-6 (a) Cleveland Wheel/Brake Assy, Model No. 38500-HA/Brake Assy, C-2000H .............................................. 14 lbs. ....................... +64.5 202. .......Two main wheel, 6-ply rating, tires (a) 6.00-6, Type III w/ regular tubes ................................................................. 17 lbs. ...................... +64.5 205. .......One, Nose Wheel, 5.00-5 (a) Goodyear, Model L5NDB, Assy. No. 95206532 ........................................ 3 lbs. ....................... -2.0 (b) Cleveland, Model 40-33............................................................................... 4 lbs. ....................... -2.0 206. .......One, Nose Wheel Tire, 4-Ply Rating, tire (a) 5.00-5, Type III w/ regular tube ................................................................... 7 lbs. ....................... -2.0 Electrical Equipment: 301. .......Generators (a) 20 amp, Delco-Remy, 1101899 ................................................................... 11 lbs. ...................... -19.5 (b) 35 amp, Delco-Remy, 1101900 ................................................................... 17 lbs. ...................... -19.5 302. .......Batteries (a) Reading, S-24............................................................................................... 24 lbs. ...................... +2.5 (b) Reading, R-33 .............................................................................................. 29 lbs. ...................... +2.5 303. .......Voltage Regulators (a) 20 amp, Delco-Remy 118735B.................................................................... 2 lbs. ....................... +7.0 (b) 35 amp, Delco-Remy 1118704 or ................................................................ 2 lbs. ....................... +7.0 VR300-14-35 or D GR-7-H-35 Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Flight Manual, dated August 24, 1955. Rev 52 4 of 58 2A3 I. Model M20 (cont’d) Miscellaneous: 601. .......Stall Warning Indicator (a) Safe-Flight, Model R.................................................................................... 1 lb........................... +28.0 602. .......Vacuum Pumps (Required IFR, Optional VFR) see NOTE 24 (a) Pesco, 3P-194-FA or .................................................................................... 4.0 lbs. ..................... 0.0 (b) Garwin. G450L ............................................................................................ 4.0 lbs. ..................... 0.0 II. Model M20A, 4 PCLM (Normal Category) Approved February 13, 1958 Engine Textron-Lycoming O-360-A1A or AID (Carburetor MA4-5, Flow Setting P/N 10-3878, 10-3878-M or 10-4164-1). Fuel 100LL or 91/96 octane minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (180 hp) Airspeed Limits Maneuvering......................................... 130 m.p.h. (113 knots) True Ind. Maximum structural cruising................ 150 m.p.h. (130 knots) True Ind. Never exceed ........................................ 183 m.p.h. (159 knots) True Ind. Flaps extended ...................................... 100 m.p.h. ( 87 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. C.G. Range (+47.0) to (+49.4) at 2450 lbs. (Landing gear extended) (+40.7) to (+49.4) at 1920 lbs. or less (Straight line variation between points given). Retraction moment 536 in.-lbs. Empty Weight C.G. Range None Maximum Weight 2450 lbs. No. of Seats 4 (2 at +36.5 to +41.5, 2 at +70.7) Maximum Baggage 120 lbs. (+93) Fuel Capacity 49 gal. Three tanks: Two 17.5 gal. tanks in wings at +47.6, one 14 gal. tank in fuselage at +68. (See Note 3.) See Note 1 for data on unusable fuel. Oil Capacity 2 gal. (-7.4) Control Surface Movements Wing Flaps .............................................................. Down ...... 21½° ± 1 Aileron ............................ Up ....... 15  2 ............ Down ....... 9° ± ½° Elevator .......................... Up ....... 24  ½° ........... Down ...... 10½° ± 1 Rudder ........................... Left ....... 18° ± ½° ........... Right ........ 18° ± ½° Stabilizer (L.E.) ............... Up ....... 1½ + 0/-½°...... Down ...... 3½ + 0/-½ Serial No’s. Eligible 1201 through 1700 and 1700A. Under the delegation option provisions of Part 21 of the FAR, Delegation Option Manufacturer No. SW-1 is authorized to approve design and production changes on airplane Serial Numbers 1201 through 1700A. Leveling means Door sill (parallel to thrust line). Spirit level is used to level. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), (b), and (c) or (d) or 2(a), (b), and (c) or (d) or 3(a), (b), and (c) or (d) or (e) or (f) or (g) or 4(a), (b), and (c) or (d), or (e) or (f) or (g), 101(a), (b), 102(a) or (b), 103(a), 104(a), 201(a) or (b), 202(a), 205(a) or (b), 206(a), 301(a) and 303(a) or 301(b) and 303(b), 302(a), 401(a), 601(a). Rev. 52 5 of 58 2A3 II. Model M20A (cont’d) Datum For M20A, datum is the centerline of the nose gear support bolts and is fuselage station 0.00. The Leading Edge of the wing at wing station 59.25 is 33.00 inches aft of fuselage station 0.00. Certification basis Date of application for Type Certificate April 9, 1952. Type Certificate No.2A3 issued August 24, 1955. No exemptions. Model M20A-CAR 3, effective November 1, 1949, as amended to May 18, 1954. Production basis None. Prior to original certification of each aircraft manufactured subsequent to March 7, 1969, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Equipment Approval for the installations of all items of equipment listed herein has been obtained by the aircraft manufacturer. Propeller and Propeller Accessories Weight F.S. 1. .... McCauley constant speed propeller installation (a) Propeller, McCauley 2D36C14 hub, 78KM-4 blades. ......................................... 59 lbs. . ..................... -31.5 Pitch setting at 30 in. sta.: Low 12.7° ± 0.2° High 27.5° ± 0.5° Diameter: Maximum 74 in. Minimum allowable for repairs 72 in. No further reduction permitted. (b) Spinner assembly, McCauley, D-2135/2136........................................................ 3 lbs. . ...................... -31.5 (c) Propeller governor, Woodward 210105 ............................................................... 3 lbs. . ...................... +4.0 (d) Propeller governor, Woodward, 210345 .............................................................. 3 lbs. . ...................... +4.0 2. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC92ZK-8D hub, 8447-12A blades ...................................... 65 lbs. . ..................... -29.5 Pitch settings at 27.0 in. sta.: Low 15.4° High 30.1° Diameter: Maximum 72 in. Minimum allowable for repairs 70 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-6 ....................................................................... 3 lbs. . ...................... -28.0 (c) Propeller governor, Woodward, 210105 .............................................................. 3 lbs. ....................... +4.0 (d) Propeller governor, Woodward, 210345 .............................................................. 3 lbs. . ...................... +4.0 3. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell, HC-C2YK-1 or HC-C2YR-1 hub, 7666-2 blades................. 53.75 lbs. .................. -30.16 See Notes 5 and 7. Pitch settings at 30.0 in. sta.: Low 13.0 ± 0° (See Note 6) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (c) Propeller governor, Woodward, 210105 .............................................................. 3 lbs. . ...................... + 4.0 (d) Propeller governor, Woodward, 210345 .............................................................. 3 lbs. . ...................... + 4.0 (e) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb........................ +3.6 (f) Propeller governor, Edo Aire, 34828014 ............................................................. 3 lb........................... +4.0 (g) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lb...................... +4.0 Rev 52 6 of 58 2A3 II. Model M20A (cont’d) Weight F.S. 4. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell, HC-C2YK-1B hub, 7666A-2 blades..................................... 53.75 lbs. .................. -30.16 See Notes 5 and 7. Pitch setting at 30.0 in. sta.: Low 13.0 ± 0° (see Note 6) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (c) Propeller governor, Woodward, 210105 .............................................................. 3 lbs. ....................... + 4.0 (d) Propeller governor, Woodward, 210345 .............................................................. 3 lbs. ....................... + 4.0 (e) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb........................ +3.6 (f) Propeller governor, Edo Aire, 34828014 ............................................................. 3 lb........................... +4.0 (g) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lb...................... +4.0 Engines and Engine Accessories (Fuel and Oil System): 101. .......Fuel Pumps (a) One, engine-driven, AC type AH, P/N 5594068.......................................... 3 lbs. ....................... + 1.2 (b) One, electric Bendix, 476087 (or alternate) Facet, (Balkamp) P/N 476-027 .................................................................... 2 lbs. ....................... +19.0 102. .......Oil Radiator (a) Harrison, 8523425........................................................................................ 3 lbs. ....................... -18.0 (b) Harrison, 8526250........................................................................................ 2 lbs. ....................... -18.0 103. .......Induction Air Filter (a) Air Maze, 13219 .......................................................................................... 1 lb........................... -17.0 104. .......Starters (a) Delco-Remy, 1109673 ................................................................................. 18 lbs. ...................... -18.0 105. .......Auxiliary Fuel Tank (a) Mooney Installation Drawing 6071.............................................................. 11 lbs. ...................... +68.0 Landing Gear: 201. .......Two, Main Wheel/Brake Assemblies, 6.00-6 (a) Cleveland Wheel Assy, Parker Hannifin, Model No. 38500-HA/Brake Assy, C-2000H .............................................. 14 lbs. ...................... +64.5 (b) Cleveland wheel/brake Assembly Model No. 27-100/ Brake assembly. No. 35-200 ........................................................................ 14 lbs. ...................... +64.5 202. .......Two main wheel tires, 6.00-6 (a) 6.Ply Rating, Type III w/ regular tubes........................................................ 17 lbs. ...................... +64.5 205. .......One, Nose Wheel, 5.00-5 (a) Goodyear, Model L5NDB, Assy. No. 95206532 ........................................ 3 lbs. ....................... -2.0 (b) Cleveland, Model 40-33............................................................................... 4 lbs. ....................... -2.0 206. .......One, Nose Wheel Tire, 5.00-5, (a) 4-Ply Rating, Type III, w/regular tube ......................................................... 7 lbs. ....................... -2.0 Rev. 52 7 of 58 2A3 II. Model M20A (cont’d). Electrical Equipment: 301. .......Generators (a) 20 amp, Delco-Remy, 1101899 ................................................................... 11 lbs. ...................... -19.5 (b) 35 amp, Delco-Remy, 1101900 ................................................................... 17 lbs. ...................... -19.5 302. .......Batteries (a) Reading, R-33 .............................................................................................. 29 lbs. ...................... +2.5 303. .......Voltage Regulators (a) 20 amp, Delco-Remy 1118735B.................................................................. 2 lbs. ....................... +7.0 (b) 35 amp, Delco-Remy 1118704 or 1119224 or ............................................ 2 lbs. ....................... +7.0 50 amp, VR 300-14-50 or DGR-7-H-50 ...................................................... 2 lbs. ....................... +7.0 Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Flight Manual dated February 12, 1958 Miscellaneous: Weight F.S. 601. .......Stall Warning Indicator (a) Safe-Flight, Model R.................................................................................... 1 lb...........................+28.0 602. .......Vacuum Pumps (Required IFR, Optional VFR) see NOTE 24 (a) Pesco, 3P-194-FA or .................................................................................... 4.0 lbs. ..................... 0.0 (b) Garwin, G450L ............................................................................................ 4.0 lbs. ..................... 0.0 III. Model M20B, 4 PCLM (Normal Category); Approved December 14, 1960 Engine Textron-Lycoming O-360-A1 A or A1 D (Carburetor MA4-5, Flow Setting P/N 10-3878, 10-3878-M, or 10-4164-1). Fuel 100LL or 91/96 octane min. grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (180 hp) (Note 5) Airspeed Limits Maneuvering......................................... 130 m.p.h. (113 knots) True Ind. Maximum structural cruising) .............. 150 m.p.h. (130 knots) True Ind. Never exceed ........................................ 183 m.p.h. (159 knots) True Ind. Flaps extended ...................................... 100 m.p.h. ( 87 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. C.G. Range (+47.0) to (+50.1) at 2450 lbs. (Landing gear extended) (+42.0) to (+50.1) at 2030 lbs. or less (Straight line variation between points given). Retraction moment 536 in.-lbs. Empty Weight C.G. Range None Maximum Weight 2450 lbs. No. of Seats 4 (2 at +36.5 to +41.5, 2 at +70.7) Maximum Baggage 120 lbs. (+93.0) Fuel Capacity 48 gals. usable (Two integral tanks in wings at +48.43) See NOTE 1 for data on unusable fuel. Rev 52 8 of 58 2A3 II. Model M20B (cont’d). Oil Capacity 2 gal. (-7.4) Control Surface Movements Wing Flaps ............................................................... Down ........21½° ± 1 Aileron..............................Up .......12½ to 17 ....... Down ......... 8° ± 1° Aileron static position............................................... Down ......... 0° to 2° Elevator ...........................Up .......24  1° ............. Down ........10½° ± 1 Rudder ............................ Left .......18° ± 1° ............. Right .........18° ± 1° Stabilizer (L.E.) ................Up .......1° to 2½° ........... Down ........3½ to 4½ Serial No’s. Eligible 1701 through 1851, 1853 through 1939. Under the delegation option provisions of Part 21 of the Federal Aviation Regulations, Delegation Option Manufacturer No. SW-1 is authorized to approve design and production changes on airplane Serial Numbers 1701 through 1851, 1853 through 1939. Leveling means Door sill (parallel to thrust line). Spirit level is used to level. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), (b) and (c) or 2(a), (b), and (c), or 3(a), (b) and (c), 101(a) and (b), 102(a) or (b), 103(a), 104(a), 201(a) or (b), 202(a), 205(a) or (b), 206(a), 301(a), 302(a), 303(a), 401(a), 601(a). Datum Datum is the centerline of the nose gear support bolts and is fuselage station 0.00. The Leading Edge of the wing at wing station 59.25 is 33.00 inches aft of fuselage station 0.00. Certification basis Date of application for Type Certificate April 9, 1952. Type Certificate No. 2A3 issued August 24, 1955. No exemptions. CAR 3, effective November 1, 1949, as amended to May 18, 1954. Production basis None. Prior to original certification of each aircraft manufactured subsequent to March 7, 1969, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Equipment Approval for the installations of all items of equipment listed herein has been obtained by the aircraft manufacturer. Propeller and Propeller Accessories: Weight F.S. 1. .... McCauley constant speed propeller installation (a) Propeller, McCauley 2D36C14 hub, 78KM-4 blades. ......................................... 59 lbs. ...................... -31.5 Pitch setting at 30 in. sta.: Low 12.7° ± 0.2° High 27.5° ± 0.5° Diameter: Maximum 74 in. Minimum allowable for repairs 72 in. No further reduction permitted. (b) Spinner assembly, McCauley, D-2135/2136........................................................ 3 lbs. ....................... -31.5 (c) Propeller governor, Woodward, 210345 .............................................................. 3 lbs. ....................... + 4.0 2. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1 or HC-C2YR-1 hub, 7666-2 blades.................. 53.75 lb..................... -30.16 See Notes 5 and 7. Pitch settings at 30.0 in. sta.: Low 13.0° ± 0 (See Note 6) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. Rev. 52 9 of 58 2A3 III. Model M20B (cont’d) Weight F.S. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (c) Propeller governor, Woodward, 210345 .............................................................. 3 lbs. ....................... +4.0 (d) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb......................... +3.6 (e) Propeller governor, Edo Aire, 34828014 ............................................................. 3 lb........................... +4.0 (f) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lb....................... +4.0 3. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell, HC-C2YK-1 B hub, 7666A-2 blades.................................... 53.75 lbs. .................. -30.16 See Notes 5 and 7. Pitch settings at 30.0 in. sta.: Low 13.0 ± 0° (See Note 6) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (c) Propeller governor, Woodward, 210345 .............................................................. 3.0 lb........................ + 4.0 (d) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb........................ +3.6 (e) Propeller governor, Edo Aire 34828014 .............................................................. 3.0 lb........................ +4.0 (f) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lb...................... +4.0 Engines and Engine Accessories (Fuel and Oil System): 101. .......Fuel Pumps (a) One, engine-driven, AC type AH, P/N 5594068.......................................... 3 lbs. ....................... + 1.2 (b) One, electric Bendix, 476087 (or alternate) Facet, (Balkamp) P/N 476-027............................................... 2 lbs. ....................... +19.0 102. .......Oil Radiator (a) Harrison, 8523452........................................................................................ 3 lbs. ....................... -18.0 (b) Harrison, 8526250........................................................................................ 2 lbs. ....................... -18.0 103. .......Induction Air Filter (a) Air Maze, 13219 .......................................................................................... 1 lb...........................-17.0 104. .......Starters (a) Delco-Remy, 11096-89 or 1109519 or 1109511.......................................... 17.8 lbs. ................... -18.0 Landing Gear: 201. .......Two, Main Wheel/Brake Assemblies, 6.00-6 (a) Cleveland Wheel Assy, Model No. 27-100/Brake Assy No. 35-200 .......... 14 lbs. ...................... See Note 8. (b) Cleveland wheel/brake Assembly Model No. 40-24/ Brake assembly. No. 30-5 ............................................................................ 19 lbs. ...................... +64.5 202. .......Two main wheel , 6-ply rating, tires (a) 6.00-6, Type III w/ regular tubes ................................................................. 17 lbs. ...................... +64.5 205. .......One, Nose Wheel, 5.00-5 (a) Goodyear, Model L5NDB, Assy. No. 95206532 ........................................ 3 lbs. ....................... -2.0 (b) Cleveland, Model 40-33............................................................................... 4 lbs. ....................... -2.0 206. .......One, Nose Wheel, 4-ply rating tire (a) 5.00-5, Type III w/ regular tube ................................................................... 7 lbs. ....................... -2.0 Rev 52 10 of 58 2A3 III. Model M20B (cont’d) Electrical Equipment: 301. .......Generators (a) 50 amp, Delco-Remy, 1101915 Gen............................................................ 16.6 lbs. ................... -19.5 302. .......Batteries (a) Auto-Lite, R-35............................................................................................ 27 lbs. ...................... +2.5 303. .......Voltage Regulators (a) 50 amp, Delco-Remy 1119224 or 1119224C or VR300-14-50 or DGR-7-H-50 ..................................................................... 2 lbs. ....................... +7.0 Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Flight Manual Supplement, dated July 16, 1962. Miscellaneous : Weight F.S. 601. .......Stall Warning Indicator (a) Safe-Flight, Model R.................................................................................... 1 lb...........................+28.0 602. .......Vacuum Pumps (Required IFR, Opt. VFR) see NOTE 24 (a) Pesco, 3P-194-FA or .................................................................................... 4.0 lbs. ..................... 0.0 (b) Garwin, G450L ............................................................................................ 4.0 lbs. ..................... 0.0 IV. Model M20C, 4 PCLM (Normal Category); Approved October 20, 1961 Engine Textron-Lycoming O-360-A1D or O-360-A1A (Carburetor MA4-5, Flow Setting P/N 10-3878, 10-3878-M, or 10-4164-1). Fuel 100LL or 100/130 min. grade aviation gasoline (See Note 9) Engine Limits For all operations, 2700 r.p.m. (180 hp) Airspeed Limits (Aircraft with serial numbers to 680001) Maneuvering......................................... 132 m.p.h. (115 knots) True Ind. Never exceed ........................................ 189 m.p.h. (164 knots) True Ind. Flaps extended ...................................... 100 m.p.h. ( 87 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. Maximum structural cruising................ 150 m.p.h. (130 knots) True Ind. (Aircraft with serial numbers to 680001 to 690001) Maneuvering......................................... 132 m.p.h. (115 knots) True Ind. Never exceed ........................................ 189 m.p.h. (164 knots) True Ind. Flaps extended ...................................... 125 m.p.h. (109 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. Maximum structural cruising................ 150 m.p.h. (130 knots) True Ind. (Aircraft with serial numbers to 690001 thru 700091 and 20-0001 and up) Maneuvering......................................... 132 m.p.h. (115 knots) True Ind. Never exceed ........................................ 200 m.p.h. (174 knots) True Ind. Flaps extended ...................................... 125 m.p.h. (109 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. Maximum structural cruising................ 175 m.p.h. (152 knots) True Ind. Rev. 52 11 of 58 2A3 IV. Model M20C (cont’d) C.G. Range (+46.5) to (+49.0) at 2575 lbs. (Landing gear extended) (+42.0) to (+49.0) at 2100 lbs. or less (Straight line variation between points given). Retraction moment 588 in. -lbs. Empty Weight C.G. Range None Maximum Weight 2575 lbs. No. of Seats 4 (2 at +36.5 to +44.0, 2 at +70.0) Maximum Baggage 120 lbs. (+93.0), 10 lbs. (+114) Fuel Capacity Serial No. 1852, 1940, through 2622 - 48 gals. (Two integral tanks in wings at +48.4) Serial No. 2623 and up - 52 gals. (Two integral tanks in wings at +48.4) See NOTE 1 for data on unusable fuel. Oil Capacity 2 gallons (-7.4) Control Surface Movements (Aircraft with serial numbers up to 690001) Wing Flaps .................................... T.O. Position .... Down ........ 15° ± 1° ....................................................... Landing ............ Down ........ 33° + 0°, -2° Aileron..............................Up ....... 12½° to 17° ...... Down ........ 8° ± 1° Aileron static position............................................... Down ........ 0° to 2° Elevator ...........................Up ....... 24  1° ............ Down ....... 10½° ± 1 Rudder ............................ Left ....... 23° to 24 ......... Right ........ 23° to 24° Stabilizer (L.E.) ................Up ....... 1 to 2½° ............ Down ....... 4½ + 5 Elevator Trim Assist Unit With stabilizer set at 3½° negative setting to the thrust line, adjust trim assist unit (740044) for elevator up angle of 19° ± ½° at the zero spring travel position. (Aircraft with serial numbers 690001-700091, 20-0001 and up) Wing Flaps .................................... T.O. Position .... Down ........ 15° ± 1° ....................................................... Landing ............ Down ........ 33° + 0°, -2° Aileron..............................Up ....... 12½° to 17° ...... Down ........ 8° ± 1° Aileron static position............................................... Down ........ 0° to 2° Elevator ...........................Up ....... 22  2° ............ Down ....... 22° ± 2 Stabilizer (L.E.) ................Up ....... ½° to 1 ............ Down ....... 5¼ to 5¾ Rudder ............................ Left ....... 23 to 24° ......... Right ........ 23° to 24° Elevator Trim Assist Unit With stabilizer set at 3½ negative setting to the thrust line, adjust trim assist bungees (740188) for elevator position of 10° ± 1 at the zero spring travel position of the bungees. Leveling means Edge of skin splice over aft fuselage radio access panel. Spirit level is used to level. Serial No’s. Eligible Serial No. 1852, 1940-3466, 670001-670123, 670125-670134, 670136-670149, 680001- 680077, 680079-680099, 680101-680198, 690001-690096, 690098, 700001-700052, 700055-700089, 700091, 20-0001 thru 20-1258. Under the delegation option provisions of Part 21 of the Federal Aviation Regulations, Delegation Option Manufacturer No. SW-1 is authorized to issue Airworthiness Certificates for Airplane Serial Numbers 2920, 2938, 2959, 2960, through 690022. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), (b), and (c) or (d) or (e) or 2(a), (b) and (c), or (d) or 3(a), (b) and (c), or (d), or (e), 101(a) or (c) and (b) or (d), 102(a) or (b), 103(a), 104(a) or (b), 201(a) or (b) or (c), 202(a), 205(a) or (b) or (c), 206(a), 301(a) and 303(a) or 301(b) and 303(b) or 301(c) and 303(c), 302(a), 401(a) or (b) or (c) or (d) or (e) or (f), 601(a) or (b) or (c) and (d). See Note 13. Rev 52 12 of 58 2A3 IV. Model M20C (cont’d) Datum For M20C, datum is the centerline of the nose gear support bolts and is fuselage station 0.00. The Leading Edge of the wing at wing station 59.25 is 33.0 inches aft of fuselage station 0.00. Certification basis Date of application for Type Certificate April 9, 1952. Type Certificate No. 2A3 issued August 24, 1955. No exemptions. Model M20C. CAR 3, effective November 1, 1949, as amended to May 18, 1954. Production basis None. Prior to original certification of each aircraft manufactured subsequent to March 7, 1969, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Equipment Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer. Propeller and Propeller Accessories: Weight F.S. 1. .... Hartzell constant speed propeller installation (a) Hartzell HC-C2YK-1 or HC-C2YR-1 hub, 7666-2 blades .................................. 53.75 lbs. .................. -30.16 See Notes 5 and 7. Pitch setting at 30.0 in. sta.: Low 13.0 ± 0° See Note 6. High 29.0° ± 2° Diameter: Max. 74 in. Min. allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (835-33 for S/N 69-0001 & ON) (c) Propeller governor Hartzell D-1 -4 or D-1 -6 or H-1 or H-1 L ........................................................... 4.5 lb........................ +3.6 (d) Propeller governor, Edo Aire 34828014 .............................................................. 3.0 lbs. .................... +3.6 (e) Propeller governor, McCauley, C 290D5/T24 ..................................................... 2.75 lbs. ................... +3.6 2. .... McCauley constant speed propeller installation (a) Propeller, McCauley, 2D34C53-A hub, 74E-0 blades......................................... 49.25 lbs. .................. -30.31 Pitch settings at 30.0 in. sta.: Low 12.7° ± 2° High 27.5° ± 0.5° Diameter: Max. 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner dome, McCauley, D-2808, D-3148 bulkhead and fillet assembly ..................................................................................................... 3.28 lbs. ................... -29.18 (c) Propeller governor, Woodward 210452 ............................................................... 3.0 lbs. ..................... +4.0 (d) Propeller governor, EDO Aire, 34828014 ........................................................... 3.0 lbs. ..................... +3.6 3. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1 B hub 7666A-2 blades...................................... 53.75 lbs. .................. -30.16 See Notes 5 and 7. Pitch settings at 30.0 in. sta.: Low 13.0° ± 0° (See Note 6.) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. Rev. 52 13 of 58 2A3 IV. Model M20C (cont’d) Weight F.S. (b) Spinner assy, Hartzell, 835-20 ............................................................................. 3.25 lbs. ................... -29.18 (835-33 for S/N 69-0001 & ON) (c) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lbs. ................... +3.6 (d) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lbs. ..................... +3.6 (e) Propeller governor, Edo Aire, 34828014 ............................................................. 3.0 lbs. ..................... +3.6 Engines and Engine Accessories (Fuel and Oil System): 101. .......Fuel Pumps (a) One, engine-driven, AC type AH, P/N 5594068.......................................... 3 lbs. ....................... + 1.2 (b) One, electric Bendix, 476087 (or alternate) Facet, (Balkamp) P/N 476-027 ............................................................................... 2 lbs. ....................... +19.0 (c) One, engine-driven, AC type AH P/N GP5623467+A, 5656880, 6440152, 6440174, 6441271, or 6440295.................................... 1.5 lbs. .................... +1.2 (d) One, electric, Dukes, 4140-00-21A or 1499-00-21 or (alternate) Weldon, P/N 8164A..................................................................................... 1.91 lb...................... -1.5 102. .......Oil Radiator (a) Harrison, 8526250........................................................................................ 2 lbs. ....................... -18.0 (b) Stewart-Warner, Model #8406-E1 or 8406J ................................................ 2.8 lbs. .................... -18.0 103. .......Induction Air Filter (a) Air Maze, 13219 .......................................................................................... 1 lb........................... -17.0 104. .......Starters (a) Delco-Remy, 11096-89 or 1109519 or 1109511.......................................... 17.8 lbs. ................... -18.0 (b) Prestolite, MZ4206 or MZ24218 or MZ4222 .............................................. 17.8 lbs. ................... -18.0 Landing Gear: 201. .......Two, Main Wheel/Brake Assemblies, 6.00-6 (a) Cleveland Wheel Assembly, Model No. 27-100/ Brake Assembly No. 35-200 ........................................................................ 14 lbs. ...................... See Note 8. (b) Cleveland Wheel Assembly Model No. 40-24/ Brake Assembly No. 30-5 ............................................................................ 19 lbs. ...................... See Note 8. (c) *Cleveland, Wheel/Brake Assembly Wheel Assembly No. 40-86,/ Brake Assembly No. 30-56A ....................................................................... 19 lbs. ...................... See Note 8. *Optional - Cleveland, 40-86E, 30-56D 202. .......Two main wheel, 6-ply rating, tires (a) 6.00-6, Type III with regular tubes .............................................................. 17 lbs. ...................... See Note 8. 205. .......One, Nose Wheel, 5.00-5 (a) Goodyear Model L5NDB, Assy. No. 95206532 .......................................... 3 lbs. ....................... See Note 8 (b) Cleveland Model 40-33................................................................................ 4 lbs. ....................... See Note 8 (c) Cleveland Model 40-87................................................................................ 2.6 lbs. ..................... See Note 8 206. .......One, Nose Wheel, 4-Ply Rating tire (a) 5.00-5, Type III w/ regular tube ................................................................... 7 lbs. ....................... See Note 8. Electrical Equipment: 301. .......Generators and Alternators (a) Generator, 50 amp, Delco-Remy, 1101915.................................................. 16.6 lbs. ................... -19.5 (b) Alternator, 60 amp, Prestolite, ALY 8420, ALY 8403, ALY 6420 or ALY 8420M .......................................................................... 10.3 lbs. ................... -19.5 (c) Alternator, 70 amp, Prestolite ALX 8403 .................................................... 10.3 lbs. ................... -19.5 Rev 52 14 of 58 2A3 IV. Model M20C (cont’d) 302. .......Batteries (a) Auto-Lite, R-35 or Prestolite, R-35 or Gill, 6-GCAB-11 or PS6-11 or Rebat, R-37 ............................................................................ 27 lbs. ...................... +2.5 303. .......Voltage Regulators (a) 50 amp, Delco-Remy 1119224 or 1119224C or VR300-14-50 or DGR-7-H-50 ..................................................................... 2 lbs. ....................... +7.0 (b) OECO, 20082* ............................................................................................ 1.4 lbs. .................... +7.0 or Electrodelta VR 414* .............................................................................. 0.6 lbs. .................... +7.0 or Electrodelta VR 415 or VR 415D or Mooney 800270-505................................................................................ 0.6 lbs. .................... +7.0 *Use 800331-721 Adapter when Oeco or VR414 is replaced by VR415, VR415D or 800270-505 regulator. Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Flight Manual, dated October 20, 1961, required for S/N 1852, 1940 through 2622. (b) Flight Manual dated August 21, 1970, for S/N 700005 and on. M20C S/N 20-0001 thru 20-0009. (c) Flight Manual dated January 1974, for S/N 20-0010 through 20-1146. See Note 2. (d) Flight Manual dated December 1974, for S/N 20-1147 through 20-1172. See Note 2. (e) Flight Manual dated August 1975, for S/N 20-1173 through 20-1185. See Note 2. (f) Flight Manual dated October 1975, for S/N 20-1186 through 20-1218. See Note 2. Superseded by (g). (g) Pilot’s Operating Handbook dated October 15, 1977, for S/N 20-1240 and on (replaces (f) for S/N 20-1186 and on.) Miscellaneous : Weight F.S. 601. .......Warning Systems (a) Stall Warning Indicator, Safe-Flight, Model R ............................................ 1 lb........................... +28.0 (b) Dual warning indicator, Safe-Flight, Model 283.......................................... 2 lbs. ....................... + 2.5 (c) Gear warning indicator, Mallory, SC 628 P................................................. 1 lb........................... +50.0 (d) Stall warning indicator, Mallory, SC 628 .................................................... 1 lb........................... +50.0 602. .......Vacuum Pumps (Required IFR, Optional VFR) see NOTE 24 (a) Airborne, 113A1, or ..................................................................................... 4.0 lbs. ..................... 0.0 (b) Airborne, 113A5, or ..................................................................................... 4.0 lbs. ..................... 0.0 (c) Airborne, 200CC, or..................................................................................... 3.5 lbs. ..................... 0.0 (d) Airborne, 211CC.......................................................................................... 2.5 lbs. ..................... 0.0 V. Model M20D, 4 PCLM (Normal Category); Approved October 15, 1962 Engine Textron-Lycoming O-360-A1D or 0-360-A2D (Carburetor MA4-5, Flow Setting P/N 10-3878, 10-3878-M, or 10-4164). Fuel 100LL or 91/96 octane min. grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (180 hp) Airspeed Limits Maneuvering......................................... 132 m.p.h. (115 knots) True Ind. Never exceed ........................................ 189 m.p.h. (164 knots) True Ind. Flaps extended ...................................... 100 m.p.h. ( 87 knots) True Ind. Maximum structural cruising................ 147 m.p.h. (128 knots) True Ind. C.G. Range (+46.5) to (+49.0) at 2575 lbs. (Fixed gear) (+42.0) to (+49.0) at 2100 lbs. or less (See Note 4) (Straight line variation between points given). Empty Weight C.G. Range None Rev. 52 15 of 58 2A3 V. Model M20D (cont’d) Maximum Weight 2575 lbs. or 2500 lbs. with Item 3 installed. No. of Seats 4 (2 at +36.5 to +44.0, 2 at +70.7) Maximum Baggage 120 lbs. (+93.0) Fuel Capacity Serial No. 1, 101-200 - 48 gals. (Two integral tanks in wings at +48.4) Serial No. 201 and up - 52 gals. (Two integral tanks in wings at +48.4) See NOTE 1 for data on unusable fuel. Oil Capacity 2 gal. (-7.4) Control Surface Movements Wing Flaps ................ ...........Landing ............. Down ......... 33 + 0, -2 Aileron.................. Up ...........12½ to 17 ....... Down ......... 8° ± 1 Aileron.......................Static Position ............... Down ......... 0° to 2° Elevator ............... Up ...........24  1° ............. Down ......... 10½° ± 1 Rudder ................ Left ...........23 to 24 .......... Right .......... 23° to 24° Stabilizer (L.E.) .... Up ...........1° to 2½° ........... Down ......... 4½ to 5 Elevator Trim Assist Unit With stabilizer set at 3½ negative setting to the thrust line, adjust trim assist unit 740044 for elevator up angle of 12 ± ½° at the zero spring travel position. The elevator up angle changes to 19 ± ½° when conversion to retractable gear in accordance with Mooney Drawing 950082 is accomplished. Leveling means Edge of skin splice over aft fuselage radio access panel. Spirit level is used to level. Serial No’s. Eligible Serial No. 1, 101 through 260. Under the delegation option provisions of Part 21 of the Federal Aviation Regulations, Delegation Option Manufacturer No. SW-1 is authorized to issue Airworthiness Certificates for Airplane Serial Nos. 256 thru 260; and approve design and production changes on Airplane Serial Numbers 1, 101 through 260. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a) (b), and (c) or (d) or (e) or 2(a), (b), (c) or 3(a), (b), (c) and (d) or 4(a) (b), and (c), or (d) or (e), 101(a) or (c) and (b), 102(a), 103(a), 104(a) or (b), 201(a) or (b), 202(a), 205(a) or (b) or (c), 206(a), 301(a), 302(a), 303(a), 401(a), or (b), 601(a). See Note 13. Specifications Pertinent to Model: Datum For M20D, datum is the centerline of the nose gear support bolts and is fuselage station 0.00. The Leading Edge of the wing at wing station 59.25 is 33.00 inches aft of fuselage station 0.00. Certification basis Date of application for Type Certificate April 9, 1952. Type Certificate No. 2A3 issued August 24, 1955. No exemptions. Model M20D CAR 3 effective November 1, 1949, as amended to May 18, 1954. Production basis None. Prior to original certification of each aircraft manufactured subsequent to March 7, 1969, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Equipment Approval for the installations of all items of equipment listed herein has been obtained by the aircraft manufacturer. Rev 52 16 of 58 2A3 V. Model M20D (cont’d) Propeller and Propeller Accessories: Weight F.S. 1. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1 or HC-C2YR-1 hub, 7666-2 blades.................. 53.75 lbs. .................. -30.16 See Notes 5 and 7. Pitch setting at 30.0 in. sta.: Low 13.0° ± 0° (See Note 6.) High 29.0° ± 2° Diameter: Maximum 74 in. Min. allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (c) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1 L ............................ 4.5 lbs. ..................... + 3.6 (d) Propeller governor, Edo Aire 34828014 .............................................................. 3.0 lbs. ..................... + 3.6 (e) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lb. ..................... + 3.6 2. .... McCauley constant speed propeller installation (a) Propeller, McCauley 2D34C53-A hub, 74E-0 blades.......................................... 49.25 lbs. .................. -30.31 Pitch setting at 30.0 in. sta.: Low 12.7° ± 2° High 27.5° ± 0.5° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner dome, McCauley D-2808, D-3148 bulkhead and fillet assembly ................................... 3.28 lbs. ................... -29.18 (c) Propeller governor, Woodward, 210452 .............................................................. 3.0 lbs. .................... + 4.0 3. .... McCauley fixed pitch propeller installation (a) Propeller, McCauley, 10172/MFA hub, 7460 blades........................................... 33.2 lbs. ................... -27.9 Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. Static RPM: Max. 2460./Min. 2360 No additional tolerance permitted. (b) Spinner assembly, McCauley, D-3337................................................................. 3.5 lbs. .................... -29.18 (c) Spinner assembly, McCauley, D-3338................................................................. ................................... -25.5 (d) Front plate assembly, McCauley, D-3353............................................................ ................................... -27.9 4. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell, HC-C2YK-1B hub, 7666A-2 blades..................................... 53.75 lbs. .................. -30.16 See NOTES 5 and 7. Pitch setting at 30.0 in. sta.: Low 13.0° ± 0° (See Note 6.) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (c) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lbs. ................... + 3.6 (d) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb......................... +3.6 (e) Propeller governor, Edo Aire, 34828014 ............................................................. 3 lb........................... +3.6 Engines and Engine Accessories (Fuel and Oil System): 101. .......Fuel Pumps (a) One, electric Bendix, 476087 (or alternate) Facet, (Balkamp) P/N 476-027............................................... 2 lbs. ....................... +19.0 Rev. 52 17 of 58 2A3 V. Model M20D (cont’d) Weight F.S. (b) One, engine driven, AC type AH, P/N GP5623467+A, 5656880, 6440152, 6440174, 6441271, or 6440295 ................................................................................... 1.5 lbs. .................... +1.2 (c) One, electric, Dukes, 4140-00-21A or 1499-00-21 (or alternate) Weldon, P/N 8164A ............................................................... 1.91 lbs. ................... -1.5 102. .......Oil Radiator (a) Harrison, 8526250........................................................................................ 2 lbs. ....................... -18.0 103. .......Induction Air Filter (a) Air Maze, 13219 .......................................................................................... 1 lb........................... -17.0 104. .......Starters (a) Delco-Remy, 11096-89 or 1109519 or 1109511.......................................... 17.8 lbs. ................... -18.0 (b) Prestolite, MZ4206 or MZ4218 or MZ4222 ................................................ 17.8 lbs. ................... -18.0 Landing Gear: 201. .......Two main wheel/brake assemblies, 6.00-6 (a) Cleveland, wheel assembly Model No. 27-100/ Brake assembly, No. 35-200 ........................................................................ 14 lbs. ...................... See Note 8. (b) Cleveland, wheel assembly Model No. 40-24/ Brake assembly, No. 30-5 ............................................................................ 19 lbs. ...................... See Note 8. 202. .......Two main wheel, 6-ply rating, tires (a) 6.00-6, Type III, w/regular tubes ................................................................. 17 lbs. ...................... See Note 8. 205. .......One nose wheel, 5.00-5 (a) Goodyear, Model L5NDB, assembly no. 95206532 .................................... 3 lbs. ....................... See Note 8. (b) Cleveland, Model 40-33............................................................................... 4 lbs. ....................... See Note 8. (c) Cleveland, Model 40-87............................................................................... 2.6 lbs. .................... See Note 8. 206. .......One nose wheel, 4-ply rating, tire (a) 5.00-5, Type III w/regular tube .................................................................... 7 lbs. ....................... See Note 8. Electrical Equipment: 301. .......Generators (a) 50 amp, Delco-Remy, 1101915 ................................................................... 16.6 lbs. ................... -19.5 302. .......Batteries (a) Auto-Lite R-35............................................................................................. 27 lbs. ...................... + 2.5 or Prestolite R-35 or Gill 6-GCAB-11 or PS6-11 or Rebat R-37 303. .......Voltage Regulators (a) 50 amp, Delco-Remy 111922I or 1119224C or VR300-14-50 or DGR-7-H-50 .............................................................................................. 2 lbs. ....................... +7.0 If 940019 alternator retrofit kit is installed (b) OECO, 20082*............................................................................................. 1.4 lbs. .................... +7.0 or Electrodelta VR 414* .............................................................................. 0.6 lbs. .................... +7.0 or Electrodelta VR 415 or VR 415D or Mooney 800270-505 ..................... 0.6 lbs. .................... +7.0 *Use 800331 - 721 adapter when Oeco or VR 414 is replaced by VR 415, VR415D or 800270-505 regulator. Rev 52 18 of 58 2A3 V. Model M20D (cont’d) Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Owners Manual,dated October 15, 1962, for S/N 1, 101 thru 200 (See Note 4) (b) Owners Manual (Supplement), dated May 14, 1963. S/N 1, 101 thru 260(See Note 4). (c) Owners Manual, dated 1965 for S/N 1, 101 thru 260 (See Note 4). Miscellaneous: 601. .......Warning systems (a) Stall warning indicator Safe-Flight, Model R................................................. 1 lb........................... +28.0 602. .......Vacuum Pumps (Required IFR, Optional VFR) see NOTE 24 (a) Airborne, 113A1 or ...................................................................................... 4.0 lbs. ..................... 0.0 (b) Airborne, 113A5 or ...................................................................................... 4.0 lbs. ..................... 0.0 (c) Airborne, 200 cc or ...................................................................................... 3.5 lbs. ..................... 0.0 (d) Airborne, 211 cc........................................................................................... 2.5 lbs. ..................... 0.0 VI. Model M20E, 4 PCLM (Normal Category); Approved September 4, 1963 Engine IO-360-A1A (fuel injector, Model RSA-5AD1, P/N 2524054-1) See Note 20. Fuel 100LL or 100/130 octane minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (200 hp) Airspeed Limits (Aircraft with Serial Numbers to 690001) Maneuvering......................................... 132 m.p.h. (115 knots) True Ind. Never exceed ........................................ 189 m.p.h. (164 knots) True Ind. Flaps extended ...................................... 100 m.p.h. ( 87 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. Maximum structural cruising................ 150 m.p.h. (130 knots) True Ind. (Aircraft with serial numbers to 690001-700061 and 21-0001 and up) Maneuvering......................................... 132 m.p.h. (115 knots) True Ind. Never exceed ........................................ 200 m.p.h. (174 knots) True Ind. Flaps extended ...................................... 125 m.p.h. (109 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. Maximum structural cruising................ 175 m.p.h. (152 knots) True Ind. C.G. Range (+46.5) to (+49.0) at 2575 lbs. (Landing gear extended) (+42.0) to (+49.0) at 2100 lbs. or less (Straight line variation between points given). Retraction moment 588 in. -lb. Empty Weight C.G. Range None Maximum Weight 2575 lbs. No. of Seats 4 (2 at +36.5 to +44.0, 2 at +70.7) Maximum Baggage 120 lbs. (+93.0), 10 lbs. (+114) Fuel Capacity 52 gals. (Two integral tanks in wings at +48.4) See NOTE 1 for data on unusable fuel. Oil Capacity 2 gal. (-6.5) Rev. 52 19 of 58 2A3 VI. Model M20E (cont’d) Control Surface Movements (Aircraft with serial numbers up to 690001) Wing Flaps ..................................T.O. Position ........... Down .....15 ± 1 .....................................................Landing ................... Down .....33 + 0, - 2 Aileron..........................Up .........12½ to 17 ............. Down .....8° ± 1 Aileron static position................................................... Down ..... 0° to 2° Elevator ........................Up .........24  1° ................... Down .....10½° ± 1 Rudder ........................ Left .........23 to 24 ................ Right ......23 to 24 Stabilizer (L.E.) ............Up .........1° to 2½ ................. Down .....4½ to 5 Elevator Trim Assist Unit With stabilizer set at 3½ negative setting to the thrust line, adjust trim assist unit 740044 for elevator up angle of 19 ± ½° at the zero spring travel position. (Aircraft with serial numbers up to 690001-700061, 21-0001 thru 21-1180) Wing Flaps ..................................T.O. Position .......... Down .....15 ± 1 .....................................................Landing ................... Down .....33 + 0 / -2 Aileron..........................Up .........12½ to 17 ............. Down .....8° ± 1 Aileron static position................................................... Down ..... 0° to 2° Elevator .......................Up .........22  2° ................... Down .....22° ± 2 Stabilizer (L.E.) ............Up .........½° to 1° ................... Down .....5¼° to 5¾° Rudder ........................ Left .........23 to 24 ................ Right ......23 to 24 Elevator Trim Assist Unit With stabilizer set at 3½ negative setting to the thrust line, adjust trim assist bungees (740188) for elevator position of 10 ± 1 at the zero spring travel position of the bungees. Leveling means Edge of skin splice over aft fuselage radio access panel. Spirit level is used to level. Serial No’s. Eligible Serial No. 101-400, 470-1217, 1219, 1221, 1223-1308, 670001-670062, 690001-690073, 700001-700039, 700041-700043, 700045-700052, 700055, 700056, 700060, 700061, 21- 0001 thru 21-1180. Under the delegation option provisions of Part 21 of the Federal Aviation Regulations, Delegation Option Manufacturer No. SW-1 is authorized to issue Airworthiness Certificates for Airplane Serial Numbers 460, 607, 622, 625 through 690029. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), (b) or (d) or (e) and (c) or (f) or (g), or 2(a), (b) or (d) or (e) and (c) or (f) or (g) or (h), 101(a), (b), 102(a), 103(a), 104(a) or (b), 201(a) or (b) or (c), 202(a), 205(a) or (b) or (c), 206(a), 301(a) and 303(a) or 301(b) and 303(b) or 301(c) and 303(b), 302(a), 401(b) or (c) or (d) or (e), 601(a) or (b) or (c) and (d). See Note 13. Specifications Pertinent to Model Datum For M20E, datum is the centerline of the nose gear support bolts and is fuselage station 0.0. The Leading Edge of the wing at wing station 59.25 is 33.00 inches aft of fuselage station 0.00. Certification basis Date of application for Type Certificate April 9, 1952. Type Certificate No. 2A3 basis issued August 24, 1955. No exemptions. Model M20E, CAR 3, effective November 1, 1949, as amended to May 18, 1954. Production basis None. Prior to original certification of each aircraft manufactured subsequent to March 7, 1969, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Rev 52 20 of 58 2A3 VI. Model M20E (cont’d) Equipment Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer. Propeller and Propeller Accessories with Fuselage - Station Locations: Weight F.S. 1. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1 or HC-C2YR-1 hub, 7666-2 blades.................. 53.75 lbs. .................. -30.16 (See Notes 6 and 7.) Pitch setting at 30.0 in. sta.: Low 14.0° ± 0° (See Note 6) High 29.0° ± 2 Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -29.18 (c) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.50 lbs. ................... +3.6 (d) Spinner assembly, Mooney, 680014-000............................................................. 3.6 lbs. .................... -29.18 (e) Spinner assembly, Mooney, 680014-501............................................................. 3.6 lbs. .................... -29.18 (f) Propeller governor, Edo Aire, 34828014 ............................................................. 3.0 lbs. .................... +3.6 (g) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lbs. ................... +3.6 2. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1B hub, 7666A-2 blades...................................... 53.75 lbs. .................. -30.16 (See Notes 6 and 7.) Pitch settings at 30.0 in. sta.: Low 14.0° ± 0° (See Note 6.) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell 835-20 ...................................................................... 3.25 lbs. ...................-29.18 (c) Spinner assembly, Hartzell, 835-33 ..................................................................... 3.25 lbs. ...................-29.18 (d) Spinner assembly, Hartzell, 835-33P ................................................................... 3.25 lbs. ...................-29.18 (e) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lbs. ................... +3.6 (f) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb........................ +3.6 (g) Propeller governor, Edo Aire, 34828014 ............................................................. 3.0 lb........................ +3.6 Engines and Engine Accessories (Fuel and Oil System): 101. .......Fuel Pumps (a) One, electric, Dukes, 4140-00-19A.............................................................. 1.91 lb...................... -1.5 (b) One, engine-driven AC 5656696A, 6440160, GP5656999, Type JJ, 6440296, or 6441234 ..................................................................... 1.6 lbs. ..................... +1.2 102. .......Oil Radiator (a) Stewart-Warner, P/N 8432A or 8432E or 8432F or or 8432F1 or 8432L (S/N 200 and up) ......................................................... 2.4 lbs. .................... -18.0 103. .......Induction Air Filter (a) Donaldson, P10-4065 or P11-3576 .............................................................. 1.2 lb........................ -19.5 104. .......Starters (a) Delco-Remy, 11096-89 or 1109519 or 1109511.......................................... 17.8 lbs. ................... -18.0 (b) Prestolite, MZ4206 or MZ4218 or MZ4222 ................................................ 17.8 lbs. ................... -18.0 Rev. 52 21 of 58 2A3 VI. Model M20E (cont’d) Weight F.S. (in.) Landing Gear: 201. .......Two Main Wheel/Brake Assemblies, 6.00-6 (a) Cleveland, wheel assembly, Model No. 27-100/Brake Assembly No. 35-200.......................................... 14 lbs. ...................... See Note 8. (b) Cleveland, wheel assembly, Model No. 40-24/ Brake Assembly No. 30-5 ............................................................................ 19 lbs. ...................... See Note 8. (c) *Cleveland, wheel assembly, Model No. 40-86/ Brake Assembly No. 30-56A ....................................................................... 19 lbs. ...................... See Note 8. *Optional - Cleveland, 40-86E, 30-56 202. .......Two main wheel, 6-ply rating, tires (a) 6.00-6, Type III w/ regular tubes ................................................................. 17 lbs. ...................... See Note 8. 205. .......One, Nose Wheel, 5.00-5 (a) Goodyear Model L5NDB, Assy. No. 95206532 .......................................... 3 lbs. ....................... See Note 8 (b) Cleveland Model 40-33................................................................................ 4 lbs. ....................... See Note 8 (c) Cleveland Model 40-87................................................................................ 2.6lbs. ...................... See Note 8 206. .......One, Nose Wheel, 4-Ply Rating tire (a) 5.00-5, Type III w/ regular tube ................................................................... 7 lbs. ....................... See Note 8. Electrical Equipment: 301. .......Generators and Alternators (a) Generator, 50 amp, Delco-Remy, 1101915.................................................. 16.6 lbs. ................... -19.5 (b) Alternator, 60 amp, Prestolite, ALY-8420 ................................................... 10.3 lbs. ................... -19.5 (c) Alternator, 70 amp, Prestolite, ALX-8403 ................................................... 10.3 lbs. ................... -19.5 302. .......Batteries (a) Auto-Lite, R-35 or Prestolite, R-35 or Gill, 6-GCAB-11 or PS6-11, or Rebat, R-37 ............................................................................ 27 lbs. ...................... +105.8 303. .......Voltage Regulators (a) 50 amp, Delco-Remy 1119224 or 1119224C or VR300-14-50 or DGR-7-H-50 .............................................................................................. 2 lbs. ....................... +7.0 If 940019 alternator retrofit kit is installed. (b) OECO, 20082*............................................................................................. 1.4 lbs. .................... +7.0 or Electrodelta VR 414* .............................................................................. 0.6 lbs. .................... +7.0 or Electrodelta VR 415 or VR 415D or Mooney 800270-505 ..................... 0.6 lbs. .................... +7.0 *Use 800331-721 adapter when OECO or VR414 is replaced by VR415, VR415D or 800270-505 regulator. Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Flight Manual dated September 3, 1963, for S/N 101 through 1308. (b) Flight Manual dated August 21, 1970, for S/N 700028 and ON. S/N 21-0001 thru 21-0023 (Aerostar). (c) Flight Manual dated January 1974, for S/N 21-0024 through 21-1160. See Note 2. (d) Flight Manual dated December 1974, for S/N 21-1161 through 21-1180. See Note 2. Miscellaneous: Weight F.S. (IN) 601. .......Warning Systems (a) Stall warning indicator, Safe-Flight, Model R ............................................. 1 lb........................... +28.0 (b) Dual warning indicator, Safe-Flight, Model 283.......................................... 2 lbs. ....................... +2.5 (c) Gear warning indicator, Mallory, SC 628P.................................................. 1 lb........................... +50.0 (d) Stall warning indicator, Mallory, SC 628. ................................................... 1 lb........................... +50.0 Rev 52 22 of 58 2A3 VI. Model M20E (cont) 602. .......Vacuum Pumps (Required. IFR, Optional VFR) see NOTE 24 (a) Airborne, 113A1 or ...................................................................................... 4.0 lbs. ..................... 0.0 (b) Airborne, 113A5 or ...................................................................................... 4.0 lbs. ..................... 0.0 (c) Airborne, 200CC or...................................................................................... 3.5 lbs. ..................... 0.0 (d) Airborne, 211CC.......................................................................................... 2.5 lbs. ..................... 0.0 VII. Model M20F, 4 PCLM (Normal Category); Approved July 25, 1965 Engine Textron-Lycoming IO-360-A1A (Bendix fuel injector, Model RSA-5AD1, P/N 2524054-1) See Note 20. Fuel 100LL or 100/130 octane min. grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (200 hp) Airspeed Limits Maneuvering....................................... 135 m.p.h. (117 knots) True Ind. Never exceed ...................................... 200 m.p.h. (174 knots) True Ind. Flaps extended .................................... 105 m.p.h. ( 91 knots) True Ind. (All aircraft to S/N 680001) Flaps extended .................................... 125 m.p.h. (109 knots) True Ind. (S/N 680001-700072 and 22-0001 and on) Landing gear extended ....................... 120 m.p.h. (104 knots) True Ind. Maximum structural cruising.............. 175 m.p.h. (152 knots) True Ind. C.G. Range (+45.0) to (+50.1) at 2740 lbs. (Landing gear extended) (+41.8) to (+50.1) at 2470 lbs. (+41.0) to (+50.1) at 2250 lbs. or less (Straight line variation between points given). Retraction moment 615 in. -lbs. Empty Weight C.G. Range None Maximum Weight 2740 lbs. No. of Seats 4 (2 at +31.5 to +39.0, 2 at +70.7 to 75.2) Maximum Baggage 120 lbs. (+95.5), 10 lbs. (+119.0) Fuel Capacity 64 gals. (Two integral tanks in wings at +48.4) See NOTE 1 for data on unusable fuel. Oil Capacity 2 gal. (-11.5) Control Surface Movements Wing Flaps ................................T.O. Position ......... Down ........15 ± 1 ...................................................Landing ................. Down .........33 + 0 / -2 Aileron..............................Up ...12½ to 17 ........... Down ........8° ± 1 Aileron static position............................................... Down .........0° to 2° Elevator ...........................Up .......22 ± 2° ............. Down ........22° ± 2 Rudder ............................ Left .......23 to 24 .......... Right .........23 to 24 Stabilizer (L.E.) ................Up .......½° to 1 ............. Down ........5¼° to 5¾° Elevator Trim Assist Unit (for Aircraft with Serial Nos. to 680001): With stabilizer set at 3½ negative setting to the thrust line, adjust trim assist unit 740128 for elevator up angle of 5  1 at the zero spring travel position. Rev. 52 23 of 58 2A3 VII. Model M20F (cont’d) Elevator Trim Assist Unit (for Aircraft with Serial Nos. 680001 and up): With stabilizer set at 3 negative setting to the thrust line, adjust trim assist bungees 740188 for elevator position of 19  1 at the zero spring travel position of the bungees. (This rigging to be obtained before installation of the 740171 extension springs). Leveling means Edge of skin splice over aft fuselage radio access panel. Spirit level is used to level. Serial No’s. Eligible Serial No. 660002-660004, 670001-670363, 670365-670385, 670387-670482, 670484-670539, 680001-680206, 690003-690090, 690092, 700001-700061, 700063-700066, 700070-700072, 22-0001 thru 22-1439. Under the delegation option provisions of Part 21 of the Federal Aviation Regulations, Delegation Option Manufacturer No. SW-1 is authorized to issue Airworthiness Certificates on Airplane Serial Numbers 660002 through 690035. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), (b) and (c) or (d) or (e), or 2(a), (b) or (c), (d) or (e) or (f), 101(a), (b), 102(a), 103(a), 104(a), 201(a), 202(a), 205(a), 206(a), 301(a), and 303(a) or 301(b), and 303(b) or 303(c) and 303(d), 302(a), 401(a) or (b) or (c) or (d) or (e) or (f), 601(a) or (b) and (c). See Note 13. Datum For M20F, datum is 5.00 inches aft of the centerline of the nose gear support bolts and is fuselage station 0.00. The Leading Edge of the wing at wing station +59.25 is 33.00 inches aft of fuselage station 0.00. Certification basis Model M20F CAR 3 effective November 1, 1949, as amended to May 18, 1954, with paragraphs 3.109, 3.112, 3.115, 3.118, and 3.120 of CAR 3 effective May 15, 1956, as amended to October 1, 1959. Production basis None. Prior to original certification of each aircraft manufactured subsequent to March 7, 1969, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Equipment Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer. Propeller and Propeller Accessories: Weight F.S. 1. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1 or HC-C2YR-1 hub, 7666-2 blades.................. 53.75 lbs. .................. -35.16 See Notes 5 and 7. Pitch setting at 30.0 in. sta.: Low 14.0° ± 0° (See Note 6) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Mooney, 680014-501............................................................. 3.6 lbs. ..................... -34.18 (c) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.50 lbs. ................... -1.4 (d) Propeller governor, Edo Aire, 34828014 ............................................................. 3.0 lbs. ..................... -1.4 (e) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lb....................... -1.4 2. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1B hub, 7666A-2 blades See Notes 5 and 7................................................................................................. 53.75 lbs. .................. -35.16 Pitch setting at 30.0 in. sta.: Low 14.0 ± 0° (see Note 6) High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. Rev 52 24 of 58 2A3 VII. Model M20F (cont’d) Weight F.S. No further reduction permitted. (b) Spinner assembly, Hartzell 835-33 ...................................................................... 3.25 lbs. ................... -34.18 (c) Spinner assembly, Hartzell, 835-33P ................................................................... 3.25 lbs. ................... -34.18 (d) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb........................ -1.4 (e) Propeller governor, Edo Aire, 34828014 ............................................................. 3 lb........................... -1.4 (f) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lbs. ................... -1.4 Engines and Engine Accessories (Fuel and Oil System): 101. .......Fuel Pumps (a) One, electric, Dukes, 4140-00-19A.............................................................. 1.91 lb...................... -1.5 (b) One, engine-driven P/N AC 5656696A, 6440160, GP5656999, Type JJ, 6440296, or 6441234 ..................................................................... 1.6 lbs. .................... -3.8 102. .......Oil Radiator (a) Stewart-Warner, P/N 8432A or 8432E or 8432F or or 8432F1 or 8432L .................................................................................... 2.4 lbs. .................... -23.0 103. .......Induction Air Filter (a) Donaldson, P10-4065 or P11-3576 .............................................................. 1.2 lb........................ -24.5 104. .......Starters (a) Prestolite, MZ4206 or MZ4218 or MZ4222 ................................................ 17.8 lbs. .................... -23.0 Landing Gear: 201. .......Two Main Wheel/Brake Assemblies, 6.00-6 (a) *Cleveland wheel assembly, Model No. 40-86/ Brake Assembly No. 30-56A ....................................................................... 19 lbs. ...................... See Note 8. *Optional - Cleveland, 40-86E, 30-56D 202. .......Two main wheel, 6-ply rating, tires (a) 6.00-6, Type III w/ regular tubes ................................................................. 17 lbs. ...................... See Note 8. 205. .......One, Nose Wheel, 5.00-5 (a) Cleveland Model 40-87................................................................................ 2.6 lbs. .................... See Note 8. 206. .......One, Nose Wheel, 6-Ply Rating tire (a) 5.00-5, Type III w/ regular tube ................................................................... 7 lbs. ....................... See Note 8. Electrical Equipment: 301. .......Generators and Alternators (a) Generator, 50 amp, Delco-Remy, 1101915.................................................. 16.6 lbs. ................... -24.5 (b) Alternator, 60 amp, Prestolite, ALY-8420 or (alternate) ALY8403, ALY6420 or ALY8420M ......................................... 10.3 lbs. ................... -24.5 (c) Alternator, 70 amp, Prestolite, ALX-8403 ................................................... 10.3 lbs. ................... -24.5 302. .......Batteries (a) Auto-Lite, R-35 or Prestolite, R-35 or Gill, 6-GCAB-11 or PS6-11, or Rebat, R-37 ............................................................................ 27 lbs. ......................+110.8 303. .......Voltage Regulators (a) 50 amp, Delco-Remy 1119224 or 1119224C or VR300-14-50 or DGR-7-H-50 .............................................................................................. 2 lbs. ....................... +2.0 If 940019 alternator retrofit kit is installed. Rev. 52 25 of 58 2A3 VII. Model M20F (cont’d) (b) OECO, 20082*............................................................................................. 1.4 lbs. .................... +2.0 or Electrodelta VR 414* .............................................................................. 0.6 lbs. .................... +7.0 or Electrodelta VR 415 or VR 415D or Mooney 800270-505 ..................... 0.6 lbs. .................... +7.0 *Use 800331-721 adapter when OECO or VR414 is replaced by VR415, VR415D or 800270-505 regulator. Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Flight Manual dated August 21, 1970, for S/N 700035 and ON, S/N 22-0001 through 22-0012 (Aerostar). See Note 2. (b) Flight Manual dated November 17, 1969, for S/N 700005 and ON. See Note 2. (c) Flight Manual dated January 1974, for S/N 22-0013 through 22-1178. See Note 2. (d) Flight Manual dated December 1974, for S/N 22-1179 through 22-1272. See Note 2. (e) Flight Manual dated August 1975, for S/N 22-1273 through 22-1305. See Note 2. (f) Flight Manual dated October 1975 for S/N 22-1306 through 22-1438. See Note 2. Miscellaneous: 601. .......Warning Systems (a) Dual warning indicator, Safe-Flight, Model 283.......................................... 2 lbs. ....................... -2.5 (b) Gear warning indicator, Mallory, SC 628P.................................................. 1 lb........................... -2.5 (c) Stall warning indicator, Mallory, SC 628. ................................................... 1 lb........................... +50.0 602. .......Vacuum Pumps (Required IFR, Optional VFR) see NOTE 24 (a) Airborne, 113A1 or ...................................................................................... 4.0 lbs. ..................... -5.0 (b) Airborne, 113A5 or ...................................................................................... 4.0 lbs. ..................... -5.0 (c) Airborne, 200CC or...................................................................................... 3.5 lbs. ..................... -5.0 (d) Airborne, 211CC.......................................................................................... 2.5 lbs. ..................... -5.0 VIII. Model M20G, 4 PCLM (Normal Category); Approved November 13, 1967 Engine Textron-Lycoming O-360-A1D (Carburetor MA 4-5, Flow Setting P/N 10-3878-M, or 10-4164-1) Fuel 100LL or 100/130 octane min. grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (180 hp) Airspeed Limits Maneuvering......................................... 135 m.p.h. (117 knots) True Ind. Never exceed ........................................ 200 m.p.h. (174 knots) True Ind. Flaps extended ...................................... 125 m.p.h. (109 knots) True Ind. Landing gear extended ......................... 120 m.p.h. (104 knots) True Ind. Maximum structural cruising................ 175 m.p.h. (152 knots) True Ind. C.G. Range (+42.5) to (+50.1) at 2525 lbs. (Landing gear extended) (+41.8) to (+50.1) at 2470 lbs. (+40.5) to (+50.1) at 2113 lbs. or less (Straight line variation between points given). Retraction moment 615 in. -lb. Empty Weight C.G. Range None Maximum Weight 2525 lbs. No. of Seats 4 (2 at +31.5 to +39.0, 2 at +70.7 to +75.2) Maximum Baggage 120 lbs. (+95.5), 10 lbs. (+119) Rev 52 26 of 58 2A3 VIII. Model M20G (cont’d) Fuel Capacity 52 gals. (Two integral tanks in wings at +48.4) See NOTE 1 for data on unusable fuel. Oil Capacity 2 gal. (-11.5) Control Surface Movements Wing Flaps ................................T.O. Position ......... Down ........15 1 ...................................................Landing ................. Down .........33 + 0/ -2 Aileron..............................Up .......12½ to 17 ....... Down ......... 8 ± 1 Aileron static position............................................... Down ......... 0 to 2 Elevator ...........................Up .......22° + 0°, 2°........ Down ........22° + 0°, -2° Rudder ............................ Left .......23 to 24 .......... Right .........23 to 24 Stabilizer (L.E.) ................Up .......½ to 1 ............. Down ........5¼ to 5 ¾ Elevator Trim Assist Unit (for Aircraft with Serial Nos. to 680001): With stabilizer set at 3½ negative setting to the thrust line, adjust trim assist unit 740128 for elevator up angle of 5° +/- 1 at the zero spring travel position. Elevator Trim Assist Unit (for Aircraft with Serial Nos. 680001 and up): With stabilizer set at 3 negative setting to the thrust line, adjust trim assist bungees 740188 for elevator position of 19° +/- 1 at the zero spring travel position of the bungees. (This rigging to be obtained before installation of the 740171 extension springs). Leveling means Edge of skin splice over aft fuselage radio access panel. Spirit level is used to level. Serial No’s. Eligible Serial No. 680001 thru 680164, 690001 thru 690020, 700001 thru 700006. Under the delegation option provisions of Part 21 of the Federal Aviation Regulations, Delegation Option Manufacturer No. SW-1 is authorized to issue Airworthiness Certificates on Airplane Serial Numbers 680001 thru 690009. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a) (b) (c) or (d) or (e), or 2(a) (b) (c), or 3(a) (b) (c) or (d) or (e), 101(a) or (c) and (b), 102(a) or (b), 103(a), 104(a) or (b), 201(a), 202(a), 205(a), 206(a), 301(a) and 303(a) or 301(b) or (c) and 303(b), 302(a), 401(a), 601(a) or (b) and (c). See Note 13. Datum For M20G, datum is 5.00 inches aft of the centerline of the nose gear support bolts and is fuselage station 0.00. The Leading Edge of the wing at wing station 59.25 is 33.00 inches aft of fuselage station 0.00. Certification basis Date of application for Type Certificate April 9, 1952. Type Certificate No. 2A3 issued August 24, 1955. No exemptions. Model M20G CAR 3, effective November 1, 1949, as amended to May 18, 1954. Production basis None. Prior to original certification of each aircraft manufactured subsequent to March 7, 1969, an FAA representative must perform a detailed inspection for workmanship, materials and conformity with the approved technical data and a check of the flight characteristics. Equipment Approval for the installations of all items of equipment listed herein has been obtained by the aircraft manufacturer. Propeller and Propeller Accessories: Weight F.S. 1. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1 or HC-C2YR-1 hub, 7666-2 blades.................. 53.75 lbs. .................. -35.16 See Notes 5 and 7. Pitch setting at 30.0 in. sta.: (See Note 6) Low 13.0° ± 0° High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. Rev. 52 27 of 58 2A3 VIII. Model M20G (cont’d) Weight F.S. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -34.18 (c) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.50 lbs. ................... -1.4 (d) Propeller governor, Edo Aire 34828014 .............................................................. 3.0 lbs. .................... -1.4 (e) McCauley governor, C290D5/T24....................................................................... 2.75 lbs. ................... -1.4 2. .... McCauley constant speed propeller installation (a) Propeller, McCauley, 2D34C53-A hub, 74E-0 blades......................................... 49.25 lbs. .................. -35.31 Pitch setting at 30.0 in. sta.: Low 12.7° ± 2° High 27.50° ± 0.5° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner dome, McCauley, D-2808, bulkhead & fillet assembly, D-3148............ 3.28 lbs. ................... -34.18 (c) Propeller governor, Woodward, 210452 .............................................................. 3.0 lbs. .................... -1.0 3. .... Hartzell constant speed propeller installation (a) Propeller, Hartzell, HC-C2YK-1B hub, 7666A-2 blades..................................... 53.75 lbs. .................. -35.16 See Notes 5 and 7. Pitch setting at 30.0 in. sta.: (See Note 6) Low 13° ± 0° High 29.0° ± 2° Diameter: Maximum 74 in. Minimum allowable for repairs 72.5 in. No further reduction permitted. (b) Spinner assembly, Hartzell, 835-20 ..................................................................... 3.25 lbs. ................... -34.18 (c) Propeller governor, Hartzell, D-1-4 or D-1-6 or H-1 or H-1L ............................. 4.5 lb......................... -1.4 (d) Propeller governor, Edo Aire, 34828014 ............................................................. 3.0 lb........................ -1.4 (e) Propeller governor, McCauley, C290D5/T24 ...................................................... 2.75 lb....................... -1.4 Engines and Engine Accessories (Fuel and Oil System) 101. .......Fuel Pumps (a) One, electric, Bendix 476087 (or alternate) Facet, (Balkamp) P/N 476-027............................................... 2.0 lbs. .................... +14.0 (b) One, engine-driven AC type AH, P/N GP5623467 + A, 5656880, 6440152, 6440174, 6441271, or 6440295.................................... 1.5 lbs. .................... -3.8 (c) One, electric, Dukes, 4140-00-21A or 1499-00-21 (or alternate) Weldon, P/N 8164A ............................................................... 1.91 lb...................... +6.5 102. .......Oil Radiator (b) Harrison, 8526250........................................................................................ 2 lbs. ....................... -23.0 (a) Stewart-Warner, Model #8406-E1 or 8406J ................................................ 2.8 lbs. .................... -23.0 103. .......Induction Air Filter (a) Air Maze, 13219 .......................................................................................... 1 lb........................... -22.0 104. .......Starters (a) Delco-Remy, 11096-89 or 1109519 or 1109511.......................................... 17.8 lbs. ................... -23.0 (b) Prestolite, MZ4206 or MZ4218 or MZ4222 ................................................ 17.8 lbs. ................... -23.0 Landing Gear: 201. .......Two Main Wheel/Brake Assemblies, 6.00-6 (a) Cleveland Wheel Assembly, Model No. 40-86/ Brake Assembly No. 30-56A ....................................................................... 19 lbs. ...................... See Note 8. *Optional - Cleveland, 40-86E, 30-56D. 202. .......Two main wheel, 6-ply rating, tires (a) 6.00-6, Type III w/ regular tubes ................................................................. 17 lbs. ...................... See Note 8. Rev 52 28 of 58 2A3 VIII. Model M20G (cont’d) Weight F.S. 205. .......One, Nose Wheel, 5.00-5 (a) Cleveland, Model 40-87 ................................................................................. 2.6 lbs. .................... See Note 8. 206. .......One, Nose Wheel, 6-Ply Rating tire (a) 5.00-5, Type III w/ regular tube ................................................................... 7 lbs. ....................... See Note 8. Electrical Equipment: 301. .......Generators and Alternators (a) Generator, 50 amp, Delco-Remy, 1101915.................................................. 16.6 lbs. ................... -24.5 (b) Alternator, 60 amp, Prestolite, ALY8420, ALY8403, ALY6420 or ALY8420M ............................................................................ 10.3 lbs. ................... -24.5 (c) Alternator, 70 amp, Prestolite, ALX8403 .................................................... 10.3 lbs. ................... -24.5 302. .......Batteries (a) Auto-Lite, R-35 or Prestolite, R-35 or Gill, 6-GCAB-11 or PS6-11, or Rebat, R-37 ............................................................................ 27 lbs. ...................... +2.5 303. .......Voltage Regulators (a) 50 amp, Delco-Remy 1119224 or 1119224C or VR300-14-50 or DGR-7-H-50 .............................................................................................. 2 lbs. ....................... +2.0 (b) OECO, 20082*............................................................................................. 1.4 lbs. .................... +2.0 or Electrodelta VR 414* .............................................................................. 0.6 lbs. .................... +7.0 or Electrodelta VR 415 or VR 415D or Mooney 800270-505 ..................... 0.6 lbs. .................... +7.0 *Use 800331-721 adapter when OECO or VR 414 is replaced by VR415, VR415D or 800270-505 regulator. Interior Equipment: 401. .......FAA Approved Airplane Flight Manual (a) Flight Manual dated November 17, 1969, for S/N 700005 and ON. See Note 2. Miscellaneous: Weight F.S. (IN) 601. .......Warning Systems (a) Dual warning indicator, Safe-Flight, Model 283.......................................... 2 lbs. ....................... -2.5 (b) Gear warning indicator, Mallory, SC 628P.................................................. 1 lb........................... -2.5 (c) Stall warning indicator, Mallory, SC 628 .................................................... 1 lb........................... +50.0 602. .......Vacuum Pumps (Required IFR, Optional VFR) see NOTE 24 (a) Airborne, 113A1 or ...................................................................................... 4.0 lbs. ..................... -5.0 (b) Airborne, 113A5 or ...................................................................................... 4.0 lbs. ..................... -5.0 (c) Airborne, 200CC or...................................................................................... 3.5 lbs. ..................... -5.0 (d) Airborne, 211CC.......................................................................................... 2.5 lbs. ..................... -5.0 IX. Model M20J, 4 PCLM (Normal Category); Approved September 27, 1976 Engine Textron-Lycoming IO-360-A1B6D or IO-360-A3B6D or IO-360-A3B6. (Bendix fuel injector, Model RSA 5AD1, P/N 2524054) See Note 12 and Note 20. Fuel 100LL or 100/130 octane minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (200 hp) Airspeed Limits Maneuvering......................................... 136 m.p.h. (118 knots) IAS Never exceed ........................................ 200 m.p.h. (174 knots) IAS *Never exceed ........................................ 225 m.p.h. (195 knots) IAS Rev. 52 29 of 58 2A3 IX. Model M20J (cont’d) Flaps extended (full flaps) .................... 127 m.p.h. (110 knots) IAS ****(15° flaps) ............................................. 145 m.p.h. (126 knots) IAS Landing gear retraction......................... 110 m.p.h. ( 96 knots) IAS ** “ “ “ ............................ 123 m.p.h. (107 knots) IAS Landing gear extension......................... 120 m.p.h. (104 knots) IAS *** “ “ “ ............................ 152 m.p.h. (132 knots) IAS **** “ “ “ ............................ 159 m.p.h. (138 knots) IAS Landing gear extended ......................... 120 m.p.h. (104 knots) IAS *** “ “ “ ............................ 152 m.p.h. (132 knots) IAS **** “ “ “ ............................ 186 m.p.h. (162 knots) IAS Maximum structural cruising................ 175 m.p.h. (152 knots) IAS * “ “ “ ............................ 200 m.p.h. (174 knots) IAS * Serial No’s. 24-0171 and on, (and 24-0002 through 24-00170 if S.B. M20-198 is complied with). ** Serial No’s. 24-0084, 24-0378 thru 24-TBA. *** Serial No’s. 24-0084, 24-0378 thru 24-2999, 24-3079 thru 24-TBA (and previous S/N’s if SB M20-209 is complied ith). **** Serial No. 24-3000 thru 24-3078. S/N 24-0001 thru 24-3200, 24-3202 thru 24-3217 -- 2740 lbs. gross weight. C.G. Range (+45.0) to (+50.1) at 2740 lbs. (Landing gear extended) (+41.8) to (+50.1) at 2470 lbs. (+41.0) to (+50.1) at 2250 lbs. or less (Straight line variation between points given). Retraction moment 615 in. -lbs. S/N 24-3201, 24-3218 thru 24-TBA, and 24-1686 thru 24-3200, 24-3202 thru 24-3217 when c/w MAC dwg. No. 940071 and insertion of applicable AFM supplement - 2900 lbs. gross weight. C.G. Range (+45.0) to (+50.1) at 2900 lbs. (Landing gear extended) (+43.8) to (+50.1) at 2740 lbs. (+41.8) to (+50.1) at 2470 lbs. (+41.0) to (+50.1) at 2250 lbs. or less (Straight line variation between points given). Retraction moment 615 in. -lbs. Empty Weight C.G. Range None Maximum Weight 2740 lbs. - S/ N 24-0001 thru 24-3200, 24-3202 thru 24-3217) 2900 lbs. - S/N 24-3201, 24-3218 and ON and S/N 24-1686 thru 24-3200, 24-3202 thru 24-3217 when c/w MAC dwg. No. 940071 and insertion of applicable AFM Supplement into the appropriate AFM. No. of Seats 4 (2 at +34.0 to +39.0, 2 at +70.7) Maximum Baggage 120 lbs. (+95.5), 10 lbs. (+119) Fuel Capacity 64 gals. (Two integral tanks in wings at +48.4) See NOTE 1 for data on unusable fuel. Oil Capacity 2 gal. (-11.5) Maximum Operating Altitude See Note 19 Control Surface Movements (Aircraft with Serial Numbers 24-0002 thru 24-1037) Wing Flaps ................................T.O. Position ......... Down ........15° +/- 1 ...................................................Landing ................. Down .........33 + 0/-2 Aileron..............................Up .......12½ to 17 ....... Down ......... 8° ± 1 Aileron static position............................................... Down ......... 0 to 2 Rev 52 30 of 58 2A3 IX. Model M20J (cont’d) Elevator ............................