AIRCRAFT SPECIFICATION NO. 2A3

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). 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. Page 5 of 53 2A3 II. Model M20A (cont’d) Production basis None. Prior to original certification of each aricraft 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 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. 2A3 Page 6 of 53 II. Model M20A (cont’d) Weight F.S. (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, 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 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 Page 7 of 53 2A3 II. Model M20A (cont’d) Weight F.S. Interior Equipment 401. FAA Approved Airplane Flight Manual (a) Flight Manual dated February 12, 1958 Miscellaneous 601. Stall Warning Indicator (a) Safe-Flight, Model R 1 lb. +28.0 602. Vacuum Pumps (Required IFR, Optional VFR) (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) 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. Oil Capacity 2 gal. (-7.4) Control Surface Movements Wing Flaps Down 21½° ± 1° Aileron Up 12½° to 17° Down 8° ± ½° 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. 2A3 Page 8 of 53 III. Model M20B (cont’d) 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 aricraft 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. (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. Page 9 of 53 2A3 III. Model M20B (cont’d) Weight F.S. 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 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. 2A3 Page 10 of 53 III. Model M20B (cont’d) Weight F.S. Miscellaneous 601. Stall Warning Indicator (a) Safe-Flight, Model R 1 lb. +28.0 602. Vacuum Pumps (Required IFR, Opt. VFR) (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. 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) Page 11 of 53 2A3 IV. Model M20C (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° + 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. 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 aricraft 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. 2A3 Page 12 of 53 IV. Model M20C (cont’d) 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. (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 Page 13 of 53 2A3 IV. Model M20C (cont’d) Weight F.S. 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. -19.5 302. 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 2A3 Page 14 of 53 IV. Model M20C (cont’d) (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) (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 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) Page 15 of 53 2A3 V. Model M20D (cont’d) 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 aricraft 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. -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 2A3 Page 16 of 53 V. Model M20D (cont’d) 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 -29.18 (c) Spinner assembly, McCauley, D-3338 -25.5 (d) Front plate assembly, McCauley, D-3353 3.5 lbs. -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. +4.0 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 (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 Page 17 of 53 2A3 V. Model M20D (cont’d) Weight F.S. 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. Interior Equipment 401. FAA Approved Airplane Flight Manual (a) Flight Manual, dated October 15, 1962, required for S/N 1 and 101 through 200. (b) Flight Manual Supplement, dated May 14, 1963. 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) (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 2A3 Page 18 of 53 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) 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° Page 19 of 53 2A3 VI. Model M20E (cont’d) 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 aricraft 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 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 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, 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 2A3 Page 20 of 53 VI. Model M20E (cont’d) Weight F.S. (IN) 2. Hartzell constant speed propeller installation (a) Propeller, Hartzell HC-C2YK-1B hub, 7666A-2 blades See Notes 5 and 7. 53.75 lbs. -30.16 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 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. Page 21 of 53 2A3 VI. Model M20E (cont’d) Weight F.S. (in.) 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. +50.0 602. Vacuum Pumps (Required. IFR, Optional VFR) (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. 2A3 Page 22 of 53 VII. Model M20F (cont’d) 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° + 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. 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. Page 23 of 53 2A3 VII. Model M20F (cont’d) Production basis None. Prior to original certification of each aricraft 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. 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 2A3 Page 24 of 53 VII. Model M20F (cont’d) Weight F.S. 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. (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 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 21-1179 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) (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 Page 25 of 53 2A3 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) 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. 2A3 Page 26 of 53 VIII. Model M20G (cont’d) 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 aricraft 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.: 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. -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.: Low 13° ± 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. -34.18 Page 27 of 53 2A3 VIII. Model M20G (cont’d) Weight F.S. (IN) (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. 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 2A3 Page 28 of 53 VIII. Model M20G (cont’d) Weight F.S. (IN) 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) (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 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. Page 29 of 53 2A3 IX. Model M20J (cont’d) 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° 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 5 ¾° Elevator Trim Assist Unit With stabilizer set at 3° negative setting to the thrust line, adjust trim assist bungees 740188 for an elevator position of 19° +/- 1° at the zero spring position of the bungees. (This rigging to be obtained before installation of the 740171 extension springs). (Aircraft with serial numbers 24-1038 and up) Wing Flaps T.O. Position Down 15° +/- 1° Landing Down 33° + 0°/-2° Aileron Up 12½° to 14½° 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 5 ¾° Elevator Trim Assist Unit With stabilizer set at 3° negative setting to the thrust line, adjust trim assist bungees 740188 for an elevator position of 9° ± 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. 24-0002 thru 24-0090 (excluding 24-0084). Leveling screws located above the tailcone access door. Spirit level is used to level S/N 24-0084, S/N 24-0091, and on. Serial numbers eligible Serial No. 24-0002 and up. 2A3 Page 30 of 53 IX. Model M20J (cont’d) Export eligibility See Note 14. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a)(1) or 1(a)(2), (b), (c), or 2(a)(1), 2(b)(1) and 1(c), 101(a), (b), or (c), 102(a), 103(a), 104(a) or (b), 201(a), 202(a), 205(a), 206(a), 301(a) and 303(a), 301(b) and 303(b), 302(a) or (b) or (c), 401(a) or (b) or (c) or (d) or (e) or (f) or (g) or (h) or (i) or (j) or (k) or (l) or (m), 601(a), (b) or (c), 602(a) or (b) or (c) or (d) or (e). Specifications Pertinent to Model Datum For M20J, 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 M20J CAR 3, effective November 1, 1949, as amended to May 18, 1954, with paragraph 3.74 of Amendment 3-13 dated August 25, 1955; 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. In lieu of corresponding CAR 3 paragraphs, where applicable - FAR 23, effective February 1, 1965; paragraph 23.29 as amended to March 1, 1978, paragraphs 23.45 through 23.77 as amended to February 17,1987, paragraphs 23.1441 through 23.1449, as amended to June 17, 1970; FAR 36, effective September 20, 1976. Production basis None. Prior to original certification of each aricraft 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) (1) Propeller, McCauley, B2D34C212 hub, 78CDA-4 blades (See Notes 10, 16) 49.5 lbs. -35.5 Pitch setting at 30.0 in. sta.: (S/N 24-0002 thru 24-0083, 24-0085 thru 24-0170) Low 14° ± 0. 2° High 27.5° ± 0.2° (S/N 24-0171 thru 24-0377, 24-0002 thru 24-0083, 24-0085 thru 24-0170 if S.B. M20-198 is complied with) Low 14° ± 0. 2° High 29.5° ± 0.5° (a) (2) Propeller, McCauley, B2D34C214 hub, 90DHB-16E blades or -16EP blades 49.5 lbs. -35.5 (See Notes 11, 16) Pitch setting @ 30.0 in. Sta. (S/N 24-0378 & on) Low 13.9° ± 0. 2° High 33.0° ± 0.5° Diameter: Maximum 74 in. Minimum allowable for repairs 73 in. No further reduction permitted. No reduction permitted when equipped with deice boots. (b) Spinner assembly, Mooney, 680031-505 4.8 lbs. -35.0 (c) Propeller governor, McCauley, C290D5F/T17 2.75 lbs. -1.40 2. Hartzell constant speed propeller installation (a) (1) Propeller, Hartzell HC-C2YK-1BF hub, F7666A-3Q blades 54.25 lbs. -35.5 Page 31 of 53 2A3 IX. Model M20J (cont’d) Weight F.S. Pitch setting at 30.0 in. sta.: Low 14.1° ± .1° High 29.3° to 31.3° Diameter: 73.0 in. No further reduction permitted. (S/N 24-1038 and ON) (b) (1) Mooney Spinner assembly, 680031-507 (S/N 24-1038 and ON) 4.8 lbs. -35.0 Engines and Engine Accessories (Fuel and Oil System) 101. Fuel Pumps (a) One, engine driven, P/N AC 6440296 or 6441234 1.6 lb. +6.5 (b) One, electric, Dukes, 4140-00-19A, 1499-00-19 1.91 lbs. +6.5 (or alternate) Weldon, P/N 8163A 2.4 lbs. +6.5 (c) Weldon, P/N 8163B (S/N 24-3000 and ON) 2.4 lbs. +6.5 102. Oil Radiator (a) Stewart-Warner, 8432F1 or 8432L 2.4 lbs. -3.8 103. Induction Air Filter (a) Donaldson, P13-0234 or Bracket, BA6210 or Air Maze, 125997-010 1 lb. -25.5 104. Starters (a) Prestoline, MZ5206 or MZ4218 or MZ4222 (S/N 24-0001 thru 24-2999) 17.8 lbs. -23.0 (b) Prestolite, MHB-4016 (S/N 24-3000 and ON) 17.8 lbs. -23.0 Landing Gear 201. Two Main Wheel/Brake Assemblies, 6.00-6 (a) Cleveland Wheel /Brake Assembly, *Wheel, 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) Goodyear, 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. Alternators (a) Alternator, 60 amp, Prestolite, ALY8420, ALY8403, ALY6420 or ALY8420M (S/N 24-0001 thru 24-2999) 10.3 lbs. -24.5 (b) Alternator, 70 amp, Prestolite, ALU6421-LS (S/N 24-3000 and on) 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 (24-0001 thru 24-2999) 27 lbs. +110.8 (b) Gill, G-242 (S/N 24-3000 thru 24-3200, 24-3202 thru 24-3217) 27 lbs. +110.8 (c) Gill, G-243 (S/N 24-3201, 24-3218 and thru 24-TBA) 29.5 lbs. +110.8 (d) Concorde, RG24-11M, or -15 26.5 lb. +110.8 (S/N 24-3201, 24-3218 and thru 24-TBA) 2A3 Page 32 of 53 Model M20J (cont’d) Weight F.S. 303. Voltage Regulators (a) OECO, 20082* 1.4 lbs. +2.0 or Electrodelta VR 414* or Electrodelta VR 415 or VR 415D or Mooney 800270-505 0.6 lbs. +2.0 (S/N 24-0001 thru 24-2999) 1.3 lb. *Use 800331-721 adapter when OECO or VR 414 is replaced by VR415, VR415D or 800270-505 regulator. (b) Precise Flight, DGR-2, or Electrodelta, VR 802 (S/N 24-3000 and ON) 0.6 lbs. +2.0 or 800270-501 0.3 lb. +2.0 Interior Equipment 401. FAA Approved Airplane Flight Manual (a) Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual dated September 27, 1976, for 24-0002 through 24-0083 and 24-0085 through 24-0377. See Note 2. (b) Pilot’s Operating Handbook dated November 15, 1977, for S/N 24-0084, 24-0378 thru 24-0763. See Note 2. (c) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 12-28-78, S/N 24-0764 thru 24-1037. See Note 2. (d) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated August 29, 1980, for S/N 24-1038 thru 24-1213. See Note 2. (e) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 9/4/81 for S/N 24-1214 thru 24-1417. See Note 2. (f) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 9/6/83 for S/N 24-1418 thru 24-1499. (g) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 10/12/84 for S/N 24-1500 thru 24-2999 (#1231). Excludes M20J Advanced Trainer, see (j) below. (h) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 6/2/86 for S/N 24-3000 thru 24-3078. (i) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 11-22-88, for S/N 24-3079 thru 24-3153. (j) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 8-89 for S/N 24-1686-14 thru 24-2999. (ATS’s only) (k) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 3-90 for S/N 24-3154 thru 24-3217, excluding S/N 24-3201. (l) Pilot’s Operating Handbook and FAA approved Airplane Flight Manual, dated 7-91, for 24-3201. 24-3218 thru 24-3373. (m) Pilots Operating Handbook and FAA approved Airplane Flight Manual, dated 1-96 for S/N 24-3374 thru 24-TBA. Miscellaneous 601. Warning Systems (a) Gear warning indicator, Mallory, SC 628P 1 lb. -2.5 (b) Stall warning indicator, Mallory, SC 628 1 lb. +50.0 (c) Stall/Gear Warning indicator, IAI, 950D-0309-000 1.1 lb. + 4.24 602. Vacuum pumps (a) **Airborne, 200CC (24-0001 thru 24-2999) or 3.5 lb. -5.0 (b) **Airborne, 211CC (24-0001 thru 24-2999) 2.5 lbs. -5.0 (c) Airborne, 241CC-17 (alternate) S/N 24-3000 and ON. 3.4 lbs. -5.0 (d) **Airborne, 241CC (alternate - all counter clockwise applications) (24-0001 thru 24-2999) or 3.4 lbs. -5.0 (e) **Sigma Tek, IU128-003 and IU128-005 or -006 (alternate - all applications) (24-0001 thru 24-2999) 3.4 lbs. -5.0 X. Model M20K, 4 PCLM (Normal Category); Approved November 16, 1978 Engine Teledyne Continental Motors TSIO-360-GB1, -GB3, -GB4 (S/N 25-0001 thru 25-0780); TSIO-360-LB1 (S/N 25-0781 thru 25-0889). See Note 17. TSIO-360-MB1 (S/N 25-1000 and 25-1999). TSIO-360-MB2 (S/N 25-2000 thru 25-2012) See NOTE 21. Page 33 of 53 2A3 X. Model M20K (cont’d) TSIO-360-SB2 (S/N 25-2000 thru 25-TBA) See NOTE 21. Fuel 100LL or 100/130 octane minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m., 40.0 in. MP (210 HP); except -MB-(1) & (2), 36.0 in. MP. & -SB2, 2,600 RPM, 39.0 in. Hg. MP (220 HP). Airspeed Limits S/N 25-0001 thru -0889 25-1000 and Up Maneuvering 135 m.p.h. (117 kts) IAS 123 KIAS Never exceed 225 m.p.h. (195 kts) IAS 195 KIAS Flaps extended 125 m.p.h. (109 kts) IAS 109 KIAS Landing gear retraction 122 m.p.h. (106 kts) IAS 106 KIAS Landing gear extension 150 m.p.h. (130 kts) IAS 140 KIAS Landing gear extended 150 m.p.h. (130 kts) IAS 165 KIAS Maximum structural cruising 200 m.p.h. (174 kts) IAS 174 KIAS C.G. Range Landing gear extended) (+43.5) to (+49.3) at 2900 lbs. (+40.6) to (+49.3) at 2360 lbs. or less (Straight line variation between points given). Retraction moment + 615 in. -lb. Empty Weight C.G. Range None Maximum Weight 2900 lbs. (S/N 25-0001 thru 25-2012) (See NOTE 21) 3130 lbs. (S/N 25-2000 thru 25-TBA) (See NOTE 21) 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 72.0 gal. (S/N 25-0001 thru 25-0446); 75.6 gal. usable) (S/N 25-0447 and on). (Two integral tanks in wings at +48.59) See NOTE 1 for data on unusable fuel. Oil Capacity 2 gal. (-22.19) Maximum Operating Altitude 24,000 feet for S/N 25-0001 thru 25-0999 28,000 feet for S/N 25-1000 thru 25-1999. (See NOTE 19.) 25,000 feet for S/N 25-2000 thru 25-TBA. (See NOTE 19.) Control Surface Movements Wing Flaps T.O. Position Down 10° ± 1° Landing Down 33° + 0°/-2° Aileron Up 12½° to 14½° 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 3.8° to 4.2° Down 6.5° to 7.0° Elevator Trim Assist With stabilizer set at maximum positive setting and elevators full down. Adjust turnbuckle for 14.0 to 16.0 lb. on tensionmeter, tensionmeter reading 20 lbs. maximum permissible. Check for positive clearance between cable end and pulley sheave. Leveling means Edge of skin splice over aft fuselage radio access panel. Spirit level is used to level. (Serial No. 25-0002 thru 25-0246) Leveling screws located above the tailcone access door. Spirit level is used to level. (Serial No. 25-0247 and on) 2A3 Page 34 of 53 X. Model M20K (cont’d) Weight F.S. (in.) Serial No’s. Eligible Serial No. 25-0001 and up. Export Eligibility See Note 14. Required equipment Serial No. 25-0001 thru 25-0999. In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a) (1) or 1(a) (2) & (b) & (c) or 2(a) & (b) & (c), 101(a), 103(a), 104(a), 201(a), 202(a), 205(a), 206(a), 301(a) and 303(a), 302(a), 401(a) or (b) or (c) or (d) or (e), 601(a) (b), 602(a) or (b), (c). Serial No. 25-1000 thru 25-1999. In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a) (2) (b) (c) or 2(a) (b), 101(b), 103(b), 104(b), 201(a), 202(a), 205(a), 206(a), 301(b) and 303(b), 302(b), & (c), 401(f) or (g) or (h), 601(a) (b) or (c), 602(a) or (b) or (c). S/N 25-2000 and ON. In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a)(2)(b)(c) or 2(a)(b), 101(b), 103(b), 104(b), 201(a), 202(a), 205(a), 206(a), 301(b) and 303(b), 302(b) or (c), 401(i) or (j), 601(a)(b) or (c), 602(a) or (b) or (c). Datum For M20K, 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 M20K (Serial Number 25-0001 through 25-2012) See Note 21. CAR 3, effective November 1, 1949, as amended to May 18, 1954, with paragraph 3.74 of Amendment 3- 13 dated August 25, 1955; CAR 3 effective May 15, 1956, as amended to October 1, 1959, paragraphs 3.109, 3.112, 3.115, 3.118, 3.120, and 3.441; in lieu of corresponding CAR 3 paragraphs, where applicable --FAR 23, effective February 1, 1965; as amended to September 14, 1969, paragraph 23.33,23.901 through 23.953, 23.955 through 23.963, 23.967 through 23.1047, 23.1121 through 23.1193, 23.1351 through 23.1401, 23.1527, 23.1553, as amended to June 17, 1970, paragraphs 23.1441 through 23.1449; as amended to February 1, 1977; paragraphs 23.1091 through 23.1105; as amended March 1, 1978, paragraph 23.29; FAR 36, effective September 20, 1976. Model M20K (Serial Number 25-2013 and on) See Note 21. CAR 3, effective November 1, 1949, as amended to May 18, 1954, with paragraph 3.74 of Amendment 3-13; CAR 3 effective May 15, 1956, as amended to October 1, 1959, paragraphs 3.109, 3.112, 3.115, 3.118, 3.120, and 3.441; in lieu of corresponding CAR 3 paragraphs, where applicable-- FAR 23, effective February 1, 1965; paragraphs 23.33, 23.901 through 23.953, 23.955 through 23.963, 23.967 through 23.1047, 23.1121 through 23.1193, 23.1351 through 23.1401, 23.1527, 23.1553, of amendment 23-7; paragraphs 23.1441 through 23.1449 of amendment 23-9; paragraphs 23.1091 through 23.1105 of amendment 23-17; paragraph 23.1301 of amendment 23-20; paragraph 23.29 of amendment 23-21; paragraph 23.1529 of amendment 23-26, paragraphs 23.45 through 23.77 of amendment 23-34; paragraph 23.1587 of amendment 23-45; paragraphs 23.1323 and 23.1325 of amendment 23-42; FAR 36, latest amendment at time of certification. Production basis None. Prior to original certification of each aricraft 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. Page 35 of 53 2A3 X. Model M20K (cont’d) Propeller and Propeller Accessories - Fuselage Station Location Weight F.S. 1. McCauley constant speed propeller installation (a) (1) Propeller, McCauley, 2A34C216, 90DHB-16E blades 55.2 lbs. -45.32 Pitch setting at 30.0 in. sta.: Low 14.7° ± 0. 2° High 33.0° ± 0.5° Diameter 74.0 in. No reduction permitted. (S/N 25-0001 thru 25-0999) (a) (2) Propeller, McCauley, 2A34C221 hub, 90DHC-16E or 90DHC-16EP blades 55.2 lbs. -45.32 Pitch settings at 30 in. sta.: Low 14.7° ± 0.2° High 38.0° ± 0.5° Diameter: 74 in. No reduction permitted. (S/N 25-1000 thru 25-2008) or (S/N 25-0001 thru 25-0999 providing S.I. M20-75 has been complied with) (b) Spinner assembly, Mooney, 680032-501 4.8 lbs. -45.32 (c) Propeller governor, McCauley, C290D3F/T20 2.75 lbs. -32.10 2. Hartzell constant speed propeller installation (a) Propeller hub blades assembly Hartzell, hub BHC-J2YF-1BF, blades F8459A-11Q 54.00 lbs. -45.32 Pitch settings at 30.0 in. sta.: Low 14.7° ± 0.1° High 30.0° to 32° (See Note 18.) Diameter: 73.0 in. No reduction permitted. (S/N 25-0001 thru 25-1999) (b) Spinner assembly, Hartzell, A2295 (S/N 25-0001 thru 25-1999) 4.5 lbs. -45.32 (c) Propeller Governor, McCauley, C290D3F/T() 2.75 lbs. -32.10 Engines and Engine Accessories (Fuel and Oil System) 101. Fuel Pumps (a) One, electric, Dukes, 4140-00-19A, or 1499-00-19 1.91 lbs. +6.5 or Weldon, 10054A (S/N 25-0001 thru 25-0999) 2.7 lbs. +6.5 (b) Weldon, 10054B (S/N 25-1000 and on) 2.7 lbs. +6.5 103. Induction Air Filter (a) Donaldson, P13-6287 or Airmaze, 125685-004 1 lb. -14.0 (b) Airmaze, ED04011 00736 (S/N 25-1000 and on) .5 lb. -23.92 104. Starters (a) Teledyne Continental Motors, 634592 (same as Prestolite, MCL 6501 or 646238) 18.1 lbs. -9.1 (b) TCM, 646275 (S/N 25-0001 and on) 18.1 lbs. -9.1 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. 2A3 Page 36 of 53 X. Model M20K (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. Alternators/Generators (a) Alternator, 70 amp, TCM, 643008 (12V) 11.7 lbs. -6.9 (Same as Prestolite, ALX-9425A or ALX-9425B) See Note 15. (Opt.) 80 amp, TCM, 649281 (12V) (b) 70 amp, TCM, 646719 (24V) 11.7 lbs. -6.9 (Opt.) 70 amp, TCM, 649280 (24V) (Opt.) 70 amp, TCM, 649172 (24V) 10.3 lbs. -5.5 (c) Optional 10 Amp, Generator Electro-Mech, EM8012 5.8 lbs. -5.04 302. Batteries (a) Auto-Lite, R-35 or Prestolite, R-35 or Gill, 6-GCAB-11 or PS6-11, or Rebat, R-37 (S/N 25-0001 thru 25-0999) 27 lbs. +110.8 (b) Gill G242 (S/N 25-1000 thru 25-1196) 27 lbs. +110.8 (c) Gill, G-243 (S/N 25-1197 and ON) 29.5 lbs. +110.8 (d) Concorde, RG24-11M, or -15 26.5 lb. +110.8 (S/N 24-3201, 24-3218 and thru 24-TBA) 303. Voltage Regulators (a) OECO, 20082* 1.4 lbs. +2.0 or Electrodelta VR414* or VR415 or VR415D or Mooney 800270-505 0.6 lbs. +2.0 (b) Precise Flight, DGR-2, or Electrodelta, VR 802 (1 or 2 ea.) or 800270-503 (S/N 25-1000 and ON) 0.6 lbs. +2.0 *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) Pilot’s Operating Handbook dated November 16, 1978, for S/N 25-0001 thru 25-0446. See Note 2. (b) Pilot’s Operating Handbook dated August 29, 1980, for S/N 25-0447 thru 25-0612. See Note 2. (c) Pilot’s Operating Handbook dated September 4, 1981 for S/N 25-0613 thru 25-0780. See Note 2. (d) Pilot’s Operating Handbook dated September 6, 1983, for S/N 25-0781 thru 25-0841. (e) Pilot’s Operating Handbook dated October 12, 1984, for S/N 25-0842 thru 25-0889. (f) Pilot’s Operating Handbook dated December 16, 1985, for S/N 25-1000 thru 25-1066. (g) Pilot’s Operating Handbook dated September 18, 1986, for S/N 25-1067 thru 25-1224. (h) Pilot’s Operating Handbook dated March 1990 for S/N 25-1225 thru 25-1999. (i) Pilot’s Operating Handbook, dated 4/97 for S/N 25-2000 thru 25-2012 (See NOTE 21) (j) Pilot’s Operating Handbook, dated 7/97 for S/N 25-2000 thru 25-TBA( See NOTE 21) Miscellaneous 601. Warning Systems (a) Gear warning indicator, Mallory, SC 628P 1 lb. -2.5 (b) Stall warning indicator, Mallory, SC 628 1 lb. +50.0 (c) Stall/Gear Warning indicator, IAI, 950D-0309-000 1.1 lb. + 4.24 602. Vacuum pumps (a) ***Airborne, 200CC or 3.5 lb. -3.8 (b) ***Airborne, 211CC 2.5 lbs. -3.8 Page 37 of 53 2A3 X. Model M20K (cont’d) Weight F.S. (c) Sigma-TEK, 1U128-003 and 1U128-005 (alternate for all applications) 3.4 lbs. -3.8 ***Airborne, 241CC (alternate all counter-clockwise applications) 3.4 lbs. -3.8 ***Airborne, 242CW-10 (alternate all clockwise applications) 3.4 lbs. -3.8 (d) ***Airborne, 241CC-15 (alternate all clockwise applications) 3.4 lbs. -3.8 (e) ***Airborne, 242CW (alternate all clockwise applications) 3.4 lbs. -3.8 (f) Sigma-TEK, 1U128-006 (Alt) 3.4 lbs. -3.8 XI. Model M20L, 4 PCLM (Normal Category); Approved February 25, 1988 Engine Porsche PFM 3200 N03 Fuel 100 LL min-grade aviation gasoline Engine Limits For all operations, 2343 RPM (217 HP) Airspeed Limits Maneuvering 135 m.p.h. (117 knots) IAS Never exceed 225 m.p.h. (195 knots) IAS Flaps extended 127 m.p.h. (110 knots) IAS Landing gear retraction 120 m.p.h. (106 knots) IAS Landing gear extension 150 m.p.h. (129 knots) IAS Landing gear extended 150 m.p.h. (129 knots) IAS Maximum structural cruising 200 m.p.h. (174 knots) IAS C.G. Range (+43.5) to (+49.3) at 2900 lbs. (Landing gear extended) (+41.0) to (+49.3) at 2430 lbs. or less (Straight line variation between points given). Retraction moment 615 in. -lb. Empty Weight C.G. Range None Maximum Weight 2900 lbs. No. of Seats 4 (2 at +34.0 to +39.0, 2 at +70.0) Maximum Baggage 120 lbs. (+101.0), 10 lbs. (+125.0) Fuel Capacity 60.5 gallons (Two integral tanks in wings at +48.43) (usable) See NOTE 1 for data on unusable fuel. Oil Capacity 13.5 qt. total; 7 qt. in oil tank Maximum Operating Altitude N/A Control Surface Movements Wing Flaps T.O. PositionDown 10° ± 1° Landing Down 33° + 0°/-2° Aileron Up 12½° to 14½° 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 3.8° to 4.2° Down 6.5° to 7.0° Elevator trim assist With stabilizer set at maximum positive setting and elevators full Down, adjust turnbuckle for a 14.0 to 16.0 lbs. tensionmeter reading on cable, tensionmeter reading (20 lb. max. permissible.) Check for positive clearance between cable end and pulley end and pulley sheave. 2A3 Page 38 of 53 XI. Model M20L (cont’d) Leveling means Leveling screws located above the tailcone access door. Spirit level is used to level. Serial No’s. Eligible Serial No. 26-0001 and up. Required equipment Serial No. 26-0001 thru 26-TBA. In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a) (b) (c), 101(a), 102(a), 103(a), 104(a), 106(a), 201(a), 202(a), 205(a), 206(a), 301(a), 302(a), 303(a), 304(a) (b), 401(a), 601(a). Datum For M20L, datum is 13 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 M20L CAR 3, effective November 1, 1949, as amended to May 18, 1954, with paragraph 3.74 of Amendment 3-13 dated August 25, 1955; paragraphs 3.109, 3.112, 3.115, 3.118, 3.120, and 3.441 of CAR 3 effective May 15, 1956, as amended to October 1, 1959. In lieu of corresponding CAR 3 paragraphs where applicable FAR 23, effective February 1, 1965, paragraph 23.29 as amended to March 1, 1978, paragraph 23.33, as amended to September 14, 1969; paragraph 23.853(d), as amended to December 20, 1973; paragraphs 23.901 through 23.953, 23.955 through 23.963, 23.967 through 23.1063, as amended to September 14, 1969, paragraphs 23.1091 through 23.1105, as amended to February 1, 1977; paragraphs 23.1121 through 23.1193, 23.1351 through 23.1401 as amended to September 14, 1969; paragraphs 23.1441 through 23.1449, as amended to June 17, 1970, paragraphs 23.1527, 23.1553, as amended to September 14, 1969, paragraph 23.1557, as amended to December 20, 1973; FAR 36, effective September 20, 1976. Exemption No. 4753 dated February 13, 1987, and 4753A dated June 9, 1987, granted an exemption from 23.991(a)(1). Special conditions No. 23-ACE-35 effective November 11, 1987, established requirements for single power control lever, protection of electronic ignition system from lightning and unwanted effects of radio frequency (RF) energy. Production basis None. Prior to original certification of each aricraft 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 Approved for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer. Propeller and Propeller Accessories - Fuselage Station Location Weight F.S. 1. Hartzell constant speed propeller installation (a) Hartzell, BHC-J2YF-1C hub, blades B7421 43.2 lbs. -51.50 Pitch setting at 30.0 in. sta.: Low 15.3° ± .1° High 40° ± 1° Diameter: 74.0 in. No reduction permitted. (b) Spinner assembly, Hartzell, D5413 4.5 lbs. -51.50 (c) Propeller governor, Woodward, A210778 2.8 lbs. -12.48 Engines and Engine Accessories (Fuel and Oil System) 101. Fuel Pumps (a) 933.620.001.00 (3 required main and emergency) 2.2 lbs. +17.62 933.620.00 (boost) (1 required) 2.2 lbs. +19.25 Page 39 of 53 2A3 XI. Model M20L (cont’d) Weight F.S. 102. Oil Radiator (a) Mooney, 620058-501 or Lori, L8600805 5.8 lbs. (dry) -39.08 103. Induction Air Filter (a) 933.110.141.01 .78 lb. -10.97 104. Starter (a) 933.604.001.00 8 lbs. -40.1 106. Fuel filter (a) 933.110.380.01 .88 lbs. -.81 Landing Gear 201. Two Main Wheel/Brake Assemblies (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, wheel assembly, 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. Alternators (a) 70 amp, Porsche, 933.603.004.00 (2 required) 13.672 lbs. -12.80(left) 13.672 lbs. -10.60(right) 302. Batteries (a) Gill, (Teledyne) G243 (2 required) 29.5 lbs. (ea.) +146.0 (b) Concorde, RG24-11M or -15 (2 required) 26.5 lbs. +146.0 303. Voltage Regulators (a) Overvoltage control (2 required) Electrodelta. OS-400 0.4 lbs. +16.25 304. Ignition boxes and coils (a) Ignition box, 933.602.007.07 3.09 lbs. (ea.) +64.99 (2 required) (b) Coil, 933.602.005.02 or 933.602.005.01 2.205 lbs. (ea.) -3.62 (2 required) Interior Equipment 401. FAA Approved Airplane Flight Manual (a) Pilot’s Operating Handbook dated 2/88 for S/N 26-0001 thru 26-0041. 2A3 Page 40 of 53 XI. Model M20L (cont’d) Miscellaneous Weight F.S. (in) 601. Warning Systems (a) Stall/gear warning, IAI-950D-0309-000 1.1 lb. +4.24 XII. Model M20M, 4 PCLM (Normal Category); Approved June 28, 1989 Engine Textron-Lycoming TIO-540-AF1A Textron-Lycoming, TIO-540-AF1B (OPT. 27-0001 THRU 27-0210) Standard 27-0211 Thru 27-TBA Fuel 100 LL or 100 octane min-grade aviation gasoline Engine Limits For all operations, 2575 r.p.m., 38.0 in. MP (270 HP) Airspeed Limits Maneuvering 146 m.p.h. (127 knots) IAS Never exceed 225 m.p.h. (195 knots) IAS Flaps extended 127 m.p.h. (110 knots) IAS Landing gear retraction 122 m.p.h. (106 knots) IAS Landing gear extension 161 m.p.h. (140 knots) IAS Landing gear extended 190 m.p.h. (165 knots) IAS Maximum structural cruising 200 m.p.h. (174 knots) IAS C.G. Range 3200 lb. C.G. limits (Landing gear extended) (+45.0) to (+51.0) at 3200 lbs. S/N 27-0001 thru 27-0052 (+43.0) to (+51.0) at 3000 lbs. (+41.0) to (+51.0) at 2430 lbs. or less (Straight line variation between points given). Retraction moment 615 in. -lbs. C.G. Range 3368 lb. C.G. limits (Landing gear extended) (+46.0) to (+51.0) at 3368 lbs. S/N 27-0053 and on, and (+44.0) to (+51.0) at 3300 lbs. aircraft S/N 27-0001 (+41.0) to (+51.0) at 2430 lbs. or less thru 27-0052 that (Straight line variation between points given). have complied with Retraction moment 615 in. -lbs. Mooney S/B M20-248. Empty Weight C.G. Range None Maximum Weight 3200 lbs. S/N 27-0001 thru S/N 27-0052. 3200 lbs. Landing, 3368 lbs. takeoff for S/N 27-0053 and on, and those aircraft S/N 27-0001 thru 27-0052 that have complied with Mooney Service Bulletin M20-248. No. of Seats 4 (2 at +34.0 to +39.0, 2 at +70.7) Maximum Baggage 120 lbs. (+101.5), 10 lbs. (+126) Fuel Capacity 89 U.S. gallons (Two integral tanks in wings at +49.23) (usable) See NOTE 1 for data on unusable fuel. Oil Capacity 10 qt. (at -24.76 in.) Maximum Operating Altitude 25,000 ft. See Note 19. Control Surface Movements Wing Flaps T.O. Position Down 10° ± 1° Landing Down 33° + 0°/-2° Aileron Up 12½° to 14½° Down 8° ± 1° Aileron static position Down 0° to 2° Page 41 of 53 2A3 XII. Model M20M (cont’d) Elevator Up 22° +0°, -2° Down 22° +0°, -2° Rudder Left 23° to 24° Right 23° to 24° Stabilizer (L.E.) Up 3.8° to 4.2° Down 6.5° to 7.0° Elevator trim assist With stabilizer set at maximum positive setting and elevators Full down. Adjust turn buckle for a 14.0 to 16.0 lb. tensionmeter reading on cable. Check for positive clearance between cable end and pulley sheave. Leveling means Leveling screws located above the tailcone access door on left side. Spirit level is to be placed on screws for level. Serial No’s. Eligible Serial No. 27-0001 and up. Export Eligibility See Note 14. 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 (c), (d), or (f), 101(a) (b), 102(a), 103(a) or (b), 104(a), 201(a), 202(a), 205(a), 206(a), 301(a), 302(a), 303(a), 401(a) or (b) or (c), 601(a), 602(a), (b) or (c). Datum For M20M, datum is 13 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 M20 CAR 3 effective November 1, 1949, as amended to May 18, 1954, paragraph 3.74 as amended to August 25, 1955; paragraphs 3.109, 3.112, 3.115, 3.118, 3.120, and 34.441 of CAR 3 effective May 15, 1956, as amended to October 1, 1959. In lieu of corresponding CAR 3 paragraphs, where applicable - FAR 23, effective February 1, 1965; paragraph 23.29 as amended to March 1, 1978, paragraph 23.33, as amended to September 14, 1969; paragraphs 23.901 through 23.953, 23.955 through 23.963, 23.967 through 23.1063, as amended to September 14, 1969; paragraphs 23.1091 through 23.1105, as amended to February 1, 1977; paragraphs 23.1121 through 23.1193, 23.1351 through 23.1399 as amended to September 14, 1969, paragraphs 23.1401 as amended to August 11, 1971; paragraphs 23.1441 through 23.1449 as amended to June 17, 1970, paragraphs 23.1521 as amended to December 1, 1978; paragraph 23.1525; paragraph 23.1527, as amended to September 14, 1969; paragraphs 23.1545, 23.1549, 23.1553 as amended to December 1, 1978, paragraph 23.1557, as amended to December 20, 1973; paragraph 23.1559 as amended to March 1, 1978; paragraph 23.1563 as amended to September 14, 1969; paragraph 23.1583 as amended to December 1, 1978; FAR 36 effective September 20, 1976, as amended to December 22, 1988. Production basis 27-0001 thru 27-0273: 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. PC11SW: 27-0274 thru 27-0316; PC13SW: 27-0317 and subsequent. 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) McCauley, B3D32C417 hub blades 82 NRD-7 75.0 lbs. -49.5 Pitch setting at 30.0 in. blade station: Low 15.1° ± 0.2° High 43.0° ± 0.5° Diameter: 75.0 in. 2A3 Page 42 of 53 XII. Model M20M (con’t) No reduction permitted. (b) Spinner assembly, McCauley D-6204 4.8 lbs. -51.00 (c) Spinner assembly, McCauley D-6204-1 4.8 lbs. -51.00 (d) Propeller governor, McCauley C290D( )/T27 3.2 lbs. -35.80 (e) Propeller de-icing boots, McCauley 690003-501 (S/N 27-0001 and on) 9 lbs. -49.50 (f) Propeller governor, McCauley DC 290D(x)/T(x) 3.2 lbs. -35.80 Engines and Engine Accessories (Fuel and Oil System) 101. Fuel Pumps (a) Electric, Weldon, A10051-D 1.9 lbs. +6.50 (b) Engine driven, Lear-Siegler, RG17980J 2.0 lb. -3.00 102. Oil Radiator (a) Stewart-Warner, 10614R 7.5 lbs. -32.0 103. Induction Air Filter (a) Air-Maze, ED04028 or (b) Donaldson, P5242257 1 lb. -36.0 104. Starter (a) Starter, geared, Textron-Lycoming, 31 B21064 18 lbs. -35.5 Landing Gear 201. Two Main Wheel/Brake Assemblies, 6.00-6 (a) *Cleveland Wheel Assembly, Wheel, Model No. 40-86/Brake Assembly No. 30-56A 19 lbs.