TCDS 3A23

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 3A23 Revision 34 MAULE Bee Dee M-4 M-5-180C MXT-7-160 M-4-180V M-4 M-5-200 MX-7-180A M-9-235 M-4C M-5-210C MXT-7-180A M-4S M-5-210TC MX-7-180B M-4T M-5-220C M-7-235B M-4-180C M-5-235C M-7-235A M-4-180S M-6-180 M-7-235C M-4-180T M-6-235 MX-7-180C M-4-210 M-7-235 M-7-260 M-4-210C MX-7-235 MT-7-260 M-4-210S MX-7-180 M-7-260C M-4-210T MX-7-420 M-7-420AC M-4-220 MXT-7-180 MX-7-160C M-4-220C MT-7-235 MX-7-180AC M-4-220S M-8-235 M-7-420A M-4-220T MX-7-160 MT-7-420 January 27, 2022 LOG OF REVISIONS Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 Rev. No. 34 32 32 32 31 32 32 32 32 31 32 32 32 32 34 32 32 32 32 32 32 Page No. 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 Rev. No. 32 32 32 32 32 32 32 32 32 32 32 32 32 33 32 32 32 32 32 30 31 Page No. 43 44 45 46 47 48 49 Rev. No. TYPE CERTIFICATE DATA SHEET NO. 3A23 This data sheet which is part of Type Certification No. 3A23 prescribes conditions and limit under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: MAULE AEROSPACE TECHNOLOGY, INC. 2099 GEORGIA HIGHWAY 133 SOUTH MOULTRIE, GEORGIA 31788 Type Certificate Holder Record: Maule Aircraft Corporation transferred type certificate 3A23 to Maule Aerospace Technology, Inc. on June 18, 1982. I. Model Bee Dee M-4, 4 PCLM (Normal Category), Approved August 10, 1961 Model M-4, 4 PCLM (Normal Category), Approved February 21, 1963 Model M-4C, 4 PCLM (Normal Category), Approved October 7, 1965 Model M-4S, 4 PCLM (Normal Category), Approved March 15, 1966 Model M-4T, 2 PCLM (Normal Category), Approved March 15, 1966 (M-4 same as Bee Dee M-4 except for minor changes.) (M-4C same as Model M-4 except for modified right fuselage truss, larger rear doors to facilitate cargo loading, and other minor changes.) (M-4S same as Model M-4 except for minor changes.) (M-4T same as Model M-4 except no rear seats or rear door and other minor changes.) Engine Continental O-300-A or B Fuel 80/87 minimum grade aviation gasoline Engine limits For all operations, 2700 rpm (145 hp) (See NOTE 3 for climb) Propeller and McCauley 1A170-DM7460 propeller limits Diameter: Not over 74 in., not under 73 in. No further reduction permitted. Static rpm at maximum permissible throttle setting: Not over 2200, not under 2100 No additional tolerance permitted. Rev. 34 2 of 46 3A23 McCauley 1C172-MDM7647 to 7656 (Eligible on s/n 24, 46-94, 1C-11C, 1S-3S, 1T-3T ) (Eligible on s/n 3-23, 25-45 when modified per Maule Modification Kit No. 36) Diameter: Not over 76 in., not under 74.5 in. No further reduction permitted. Static rpm at maximum permissible throttle setting: Not over 2250, not under 2100 No additional tolerance permitted. Airspeed limits (CAS) Landplane and Skiplane: (See NOTE 11 for airspeeds) C.G. range Landplane: (+15.0) to (+23.0) at 2100 lbs. (+11.0) to (+23.0) at 1400 lbs. or less NOTE: With fuel in optional auxiliary tanks, aft C.G. restricted to (+18.0). See Service Bulletin No. 18, Airplane Flight Manual Supplement (AFMS) No. 4 is required. Skiplane: Models M-4, M-4C with Fli-Lite 3000 MK IIIA Skis (+13.0) to (+23.0) at 1850 lbs. (+10.6) to (+23.0) at 1550 lbs. or less Models M-4, M-4C with FluiDyne A2000A Skis (+15.0) to (+23.0) at 2100 lbs. (+11.0) to (+23.0) at 1400 lbs. or less Straight line variation between points given. Empty weight C.G. range None Maximum weight Landplane: 2100 lbs. Skiplane: Fli-Lite 3000 MK IIIA Skis: 1850 lbs. Federal A2000A Skis: 2100 lbs. Number of seats 4 (2 at +18 to +21, 2 at +53) (Bee Dee M-4, M-4, M-4C, M-4S) 2 (+18 to +21) (M-4T) Maximum baggage 100 lbs. (+72) (Bee Dee M-4, M-4) 100 lbs. (+20), 175 lbs. (+42) (M-4C, M-4S, M-4T) 125 lbs. (+70) (M-4C, M-4S) Fuel capacity 43 gal. (40 gal. usable; two 21.5 gal. tanks in wings at +24) (See NOTE 1 for data on system fuel.) Oil capacity 8 qt. (-37), 4 qt. Minimum (See NOTE 1 for data on system oil.) Control surface Wing flaps Down 1st Notch 15º +3º movements 2nd Notch 35º +3º Aileron Up 20º + 1 Down 20º +1º Elevator Up 25º + 2º Down 21º +1º Elevator tab Up 14º + 1º Down 25º +1º (Bee Dee M-4, s/n 3-14, M-4, s/n 15- 43, unless modified by Maule SL#9 dated 11/8/65) Up 8º + 2º/-1º Down 25º + 1º (M-4, s/n 44-94, unless modified by Maule SL#9 dated 11/8/65) Up 11º + 3º Down 25º +1º (All M-4C, S, and T and M-4, s/n 3-94 modified by Maule SL#9 dated 11/8/65) Rudder Right 21º + 1º Left 21º +1º Rudder tab Right 48º + 4º Left 48º +4º Serial numbers eligible Model Bee Dee M-4, 3-14 Model M-4, 15-94 Model M-4C, 1C-3C Model M-4S, 1S-3S Model M-4T, 1T-3T Production basis (No longer in production) II. Model M-4-210, 4 PCLM (Normal Category), Approved September 24, 1964 Model M-4-210C, 4 PCLM (Normal Category), Approved October 7, 1965 Model M-4-210S, 4 PCLM (Normal Category), Approved March 15, 1966 Model M-4-210T, 2 PCLM (Normal Category), Approved March 15, 1966 (Same as M-4, M-4C, M-4S, and M-4T except for the installation of a Continental IO-360-A or D engine.) Rev. 34 3 of 47 3A23 Engine Continental IO-360-A Continental IO-360-D for s/n 1086C and up Fuel 100/100LL minimum grade aviation gasoline Engine limits IO-360-A: Maximum continuous hp, rpm, in. Hg. alt. Critical altitude 195-2800-26.2-2250 ft. Sea level 195-2800-26.5 Takeoff hp (5 min.) 210-2800 F.T. IO-360-D: F.T. all operations 210 hp - 2800 rpm Propeller and McCauley constant speed model D2A3467/76C-2 (used on A engine) or propeller limits D2A34C67N/S76C-2 (used on A or D engine) Diameter: 74 in., no further reduction permitted. Pitch settings at 30 in. sta.: low 12.5º high 23º Spinner: Cessna 0552016-1 McCauley D-2771-1 assembly (used on A or D eng.) Governor (hydraulic): Woodward F210452 or B210680 Airspeed limits (CAS) Landplane, Floatplane, and Skiplane: (See NOTE 11 for airspeeds) C.G. range Landplane: For s/n 1001-1045, 1001C-1074C, 1079C, 1080C: (+15.0) to (+23.0) at 2100 lbs. (+11.0) to (+23.0) at 1400 lbs. or less For s/n 1075C, 1081C-1117C: (+16.0) to (+19.6) at 2300 lbs. (+15.0) to (+23.0) at 2100 lbs. (+11.0) to (+23.0) at 1400 lbs. or less NOTE: S/n 1001-1035 when modified per Maule SL#7 and SL#15 and s/n 1036- 1045, 1001C-1074C, 1079C, 1080C when modified per Maule SL#15 dated 11/12/68 are eligible for the above C.G. range at 2300 lbs. GW. Skiplane: Models M-4-210, M-4-210C with Fli-Lite 3000 MK IIIA Skis: (+13.0) to (+23.0) at 2100 lbs. (+10.6) to (+23.0) at 1550 lbs. or less Models M-4-210, M-4-210C with Federal A2000A Skis: (+15.0) to (+23.0) at 2100 lbs. (+11.0) to (+23.0) at 1400 lbs. or less Models M-4-210, M-4-210C with Federal C2200H or C3000H Skis: (+12.6) to (+18.4) at 2100 lbs. (+9.6) to (+18.4) at 1620 lbs. or less Floatplane: EDO 248A2440, 248B2440 or Fleet 2500 Floats: (+15.5) to (+20.5) at 2300 lbs. (+11.0) to (+20.5) at 1600 lbs. or less CAP 62-2000 Floats: (+15.6) to (+20.5) at 2220 lbs. (+12.0) to (+20.5) at 1700 lbs. or less Straight line variation between points given. Empty weight C.G. range None Maximum weight Landplane: 2300 lbs. or 2100 lbs. (Reference C.G. Range-landplane) Skiplane: 2100 lbs. Floatplane: Fleet 2500, EDO 248A2440 or 248B2440 Floats: 2300 lbs. CAP 62-2000 Floats: 2220 lbs. Number of seats 4 (2 at +18 to +21, 2 at +53)(M-4-210, M-4-210C) Maximum baggage 100 lbs. (+72)(M-4-210) 100 lbs. (+20), 175 lbs. (+42)(M-4-210C) 125 lbs. (+70)(M-4-210C) Fuel capacity 43 gal. (40 gal. usable; two 21.5 gal. tanks in wings at +24) Optional wing auxiliary tanks - 23 gal. (23 gal. usable; two 11.5 gal. tanks in outerwings at +22.2) Rev. 34 4 of 46 3A23 (Fuel in the optional auxiliary tanks not approved in combination with skis or floats.) (See NOTE 1 for data on system fuel.) Oil capacity 10 qt. (-37), 7 qt. Minimum (See NOTE 1 for data on system oil.) Control surface Wing flaps Down 1st Notch 15º +3º movement 2nd Notch 35º +3º Aileron Up 20º + 1º Down 20º +1º Elevator Up 25º + 2º Down 21º +1º Elevator tab Up 11º + 3º Down 25º +1º (M-4-210, s/n 1051 and up; all M-4-210C, -210S and -210T; and M-4-210 s/n 1001-1050 modified per Maule SL#9 dated 11/8/65) Up 8º +2º /-1º Down 25º +1º (M-4-210, s/n 1001-1050 unless modified per Maule SL#9 dated 11/8/65) Rudder Right 21º + 1º Left 21º +1º Rudder tab Right 48º + 4º Left 48º +4º Serial numbers Model M-4-210, 1001-1045 eligible Model M-4-210C, 1001C-1117C Model M-4-210S, 1001S and up (none built) Model M-4-210T, 1001T and up (none built) Production basis (No longer in production) III. Model M-4-220, 4 PCLM (Normal Category), Approved October 18, 1966 Model M-4-220C, 4 PCLM (Normal Category), Approved October 18, 1966 Model M-4-220S, 4 PCLM (Normal Category), Approved October 18, 1966 Model M-4-220T, 2 PCLM (Normal Category), Approved October 18, 1966 (Same as M-4, M-4C, M-4S and M-4T except for the installation of a Franklin 6A-350-C1 engine.) Engine Franklin 6A-350-C1 Fuel 100/100LL minimum grade aviation gasoline Engine limits Takeoff (5 min.) 2800 rpm, F.T. (220 hp). For all other operations, 2800 rpm at 26.5 in. hg. (194 hp) (See NOTE 8 if Service Letter 27 is installed) Propeller and McCauley constant speed model 2A31C21/84S-8 or -6 propeller limits Diameter: Not over 78 in.; not under 74 in. Pitch settings at 30 in. sta.: low 12.8º high 23.1º Spinner: Cessna 0552016-1 McCauley constant speed model 2A34C22-N/S84SF-6 or -8 Diameter: Not over 78 in.; not under 74.5 in. Pitch settings at 30 in. sta.: low 11.5º high 22º Spinner: McCauley D4101 assembly NOTE: This installation also requires incorporation of Maule Drawings 5030F, rev. D, 5090B, rev. D, and 5043F, rev. G or later revisions. Governor: Woodward 210453 or 210660 Airspeed limits (CAS) Landplane, Floatplane, and Skiplane: (See NOTE 11 for airspeeds) C.G. range Landplane: (+15.6) to (+19.0) at 2300 lbs. (+14.5) to (+20.5) at 2100 lbs. (+11.1) to (+20.5) at 1500 lbs. or less Model M-4-220S, s/n 2001S only: (+15.0) to (+20.5) at 2100 lbs. (+11.0) to (+20.5) at 1400 lbs. or less NOTE: With fuel in optional wing auxiliary tanks, aft C.G. restricted to +18.0. Skiplane: Federal C2200H Skis: (+12.6) to (+18.4) at 2100 lbs. (+9.6) to (+18.4) at 1620 lbs. or less Model M-4-220C only: Federal A2000A Skis (+14.5) to (+20.5) at 2100 lbs. Rev. 34 5 of 47 3A23 (+11.1) to (+20.5) at 1500 lbs. or less Fli-Lite 3000 MK IIIA Skis (+14.5) to (+20.5) at 2300 lbs. (+11.1) to (+20.5) at 1500 lbs. or less Floatplane: EDO 248A2440, 248B2440 or Fleet 2500 Floats: (+15.5) to (+20.5) at 2300 lbs. (+11.0) to (+20.5) at 1600 lbs. or less Straight line variation between points given. Empty weight C.G. range None Maximum weight Landplane: 2300 lbs. (M-4-220C) 2100 lbs. (s/n 2001S only) Skiplane: 2100 lbs. Floatplane: 2300 lbs. Number of seats 4 (2 at +18 to +21, 2 at +53) (M-4-220C, M-4-220S) Maximum baggage 100 lbs. (+20), 175 lbs. (+42) (M-4-220C, M-4-220S) 125 lbs. (+70) (M-4-220C, M-4-220S) Fuel capacity 43 gal. (40 gal. usable; two 21.5 gal. tanks in wings at +24) Optional wing auxiliary tanks 23 gal. (23 gal. usable; two 11.5 gal. tanks in wings at +22.2) (Fuel in the optional auxiliary tanks not approved in combination with skis or floats) (See NOTE 1 for data on system fuel.) Oil capacity 8.8 qt.(-37), 5.8 qt. Minimum (See NOTE 1 for data on system oil.) Control surface Wing flaps Down 1st Notch 15º +3º movements 2nd Notch 35º +3º Aileron Up 20º +1º Down 20º +1º Elevator Up 25º +2º Down 21º +1º Elevator tab Up 11º +3º Down 25º +1º Rudder Right 21º +1º Left 21º +1º Rudder tab Right 48º +4 Left 48º +4º Serial numbers eligible Model M-4-220, 2001 and up (None built) Model M-4-220C, 2001C-2190C Model M-4-220S, 2001S and up (One built) Model M-4-220T, 2001T and up (None built) Production basis (No longer in production) IV. Model M-4-180C, 4 PCLM (Normal Category), Approved October 20, 1970 Model M-4-180S, 4 PCLM (Normal Category), Approved October 20, 1970 Model M-4-180T, 2 PCLM (Normal Category), Approved October 20, 1970 (Same as M-4C, M-4S and M-4T except for the installation of Franklin 6A-335-B1A engine.) Engine Franklin 6A-335-B1A Fuel 80/87 minimum grade aviation gasoline Engine limits For all operations, 2800 rpm (180 hp) Propeller and McCauley constant speed model 2A34C22-N/S84SF-6 propeller limits Diameter: Not over 78 in.; not under 76.5 in. Pitch settings at 30 in. sta.: low 11.5º high 22º Spinner: McCauley D4180 with C4181 bulkhead assembly, B3243 front support, B3410-16 or -32 shim. Governor: Woodward 210453 or 210660 Airspeed limits (CAS) Landplane: (See NOTE 11 for airspeeds) C.G. Range Landplane: (+15.6) to (+19.0) at 2300 lbs. Rev. 34 6 of 46 3A23 (+14.5) to (+20.5) at 2100 lbs. (+11.1) to (+20.5) at 1500 lbs. or less Straight line variation between points given. NOTE: With fuel in optional wing auxiliary tanks, aft C.G. restricted to (+18.0). See Service Bulletin No. 18, AFMS No. 2 is required. Empty weight C.C. Range None Maximum weight 2300 lbs. Number of seats 4 (2 at +18 to +21, 2 at +53) (M-4-180C) Maximum baggage 100 lbs. (+20), 175 lbs. (+42) (M-4-180C) 125 lbs. (+70) (M-4-180C) Fuel capacity 43 gal. (40 gal. usable; two 21.5 gal. tanks in wings at +24) (See NOTE 1 for data on system fuel.) Oil capacity 8.8 qt. (-37), 5.8 qt. Minimum (See NOTE 1 for data on system oil.) Control surface Wing flaps Down 1st Notch 15º +3º movements 2nd Notch 35º +3º Aileron Up 20º +1º Down 20º +1º Elevator Up 25º +2º Down 21º +1º Elevator tab Up 11º +3º Down 25º +1º Rudder Right 21º +1º Left 21º +1º Rudder tab Right 48º +4º Left 48º +4º Serial numbers eligible Model M-4-180C, 3001C-3006C Model M-4-180S, 3001S and up (None built) Model M-4-180T, 3001T and up (None built) Production basis (No longer in production) V. Model M-5-210C, 4 PCLM (Normal Category), Approved December 28, 1973 (Same as M-4-210C except modified empennage, increased span flaps, smaller ailerons, modified C.G. range and other minor changes.) Engine Continental IO-360-D Fuel 100/100LL minimum grade aviation gasoline Engine limits 210 hp at 2800 rpm all operations Propeller and McCauley constant speed model D2A34C67N/S76C-2 propeller limits Diameter: 74 in., no further reduction permitted. Pitch settings at 30 in. sta.: low 12.5º high 23º Spinner: McCauley spinner assembly D-2771-1 Governor (hydraulic): Woodward B210680 or F210452 Airspeed limits (CAS) Landplane, Floatplane, and Skiplane: (See NOTE 11 for airspeeds) C.G. range Landplane: (+16.0) to (+20.5) at 2300 lbs. (+15.0) to (+20.5) at 2100 lbs. (+12.0) to (+20.5) at 1600 lbs. or less All s/n modified per Maule SL#45 and SL#46: (+17.0) to (+20.5) at 2500 lbs. (+15.0) to (+20.5) at 2100 lbs. (+12.0) to (+20.5) at 1600 lbs. or less Floatplane: EDO 248A2440 or 248B2440 Floats: (+16.0) to (+18.0) at 2300 lbs. (+12.0) to (+18.0) at 1600 lbs. or less EDO 248B2400 Floats with modification per Maule Drawing 9173A: (+15.6) to (+19.0) at 2500 lbs. (+12.0) to (+19.0) at 1600 lbs. or less Rev. 34 7 of 47 3A23 Pee Kay 2300 Floats: (+15.5) to (+20.0) at 2300 lbs. (+14.0) to (+20.0) at 1800 lbs. or less Wipline 2350 Amphibious Floats (Aircraft requires M-7A wings installed per MK#69) (+14.1) to (+19.0) at 2500 lbs. (+12.6) to (+19.0) at 2090 lbs. or less Note: M-5-210C s/n 6001C-6014C, 6039C, 6043C-6045C requires compliance to Maule SL#28 when equipped with EDO 248A2440/B2440 floats. Skiplane: Fluidyne C2200H Skis (+12.5) to (+20.0) at 2300 lbs. (+9.5) to (+20.0) at 1600 lbs. or less Fli-Lite 3000 MK IIIA Skis (+16.0) to (+20.0) at 2300 lbs. (+12.0) to (+20.0) at 1600 lbs. or less Straight line variation between points given. Empty weight C.G. range None Maximum weight Landplane, Skiplane and Floatplane: 2300 lbs. Landplane modified per SL#45 and SL#46: 2500 lbs. Floatplane modified per 9173A: 2500 lbs. Number of seats 4 (2 at +20, 2 at +50) Maximum baggage 100 lbs. (+20), 175lbs. (+42), 125 lbs. (+70) Fuel capacity 43 gal. (40 gal. usable; two 21.5 gal. tanks in wings at +23.3) Optional wing auxiliary tanks 23 gal. (23 gal. usable; two 11.5 gal. tanks in wings at +22.2) See NOTE 16 if Modification Kit No. 15 is installed. (See NOTE 1 for data on system fuel.) Oil capacity 10 qt. (-37) 7 qt. Minimum (See NOTE 1 for data on system oil.) Control surface Wing flaps Down 1st Notch 15º +3º movements 2nd Notch 35º +3º Modified per Down 1st Notch 20º +3º Maule SL#46 2nd Notch 40º +3º Aileron Up 20º +1º Down 20º +1º Elevator Up 25º +2º Down 21º +1º Elevator tab Up 12º +4º Down 29º +2º Rudder Right 21º +1º Left 21º +1º Rudder tab Right 48º +4º Left 48º +4º Serial numbers eligible Model M-5-210C, 6001C-6206C (See NOTE 13 for float installation requirements.) Production basis (No longer in production) VI. Model M-5-220C, 4 PCLM (Normal Category), Approved December 28, 1973 (Same as M-4-220C except modified empennage, increased span flaps, smaller ailerons, and other minor changes.) Engine Franklin 6A-350-C1 Fuel 100/100LL minimum grade aviation gasoline Engine limits 220 hp at 2800 rpm, all operations Propeller and McCauley constant speed model 2A34C22-N/S84SF-6 or -8 propeller limits Diameter: Not over 78 in., not under 74.5 in. Pitch settings at 30 in. sta.: low 11.5º high 22º Spinner: McCauley D4180 with C4181 bulkhead assembly, B3243 front support, B3410-16 or -32 shim Governor: Woodward 210453 or 210660 Rev. 34 8 of 46 3A23 Airspeed limits (CAS) Landplane, Floatplane, and Skiplane: (See NOTE 11 for airspeeds) C.G. range Landplane: (+16.0) to (+20.5) at 2300 lbs. (+15.0) to (+20.5) at 2100 lbs. (+12.0) to (+20.5) at 1600 lbs. or less All s/n modified per Maule SL#48 and SL#51: (+17.0) to (+20.5) at 2500 lbs. (+15.0) to (+20.5) at 2100 lbs. (+12.0) to (+20.5) at 1600 lbs. or less Floatplane: EDO 248A2440 or 248B2440 Floats: (+16.0) to (+18.0) at 2300 lbs. (+12.0) to (+18.0) at 1600 lbs. or less EDO 248B2400 Floats with modification per Maule Drawing 9173A: (+15.6) to (+19.0) at 2500 lbs. (+12.0) to (+19.0) at 1600 lbs. or less Pee Kay 2300 Floats: (+15.5) to (+20.0) at 2300 lbs. (+14.0) to (+20.0) at 1800 lbs. or less NOTE: M-5-220C, s/n 5002C, 5019C, 5020C, 5022C-5024C requires compliance to Maule SL#28 when equipped with EDO 248A2440/B2440 floats. Skiplane: FluiDyne C2200H Skis (+12.5) to (+20.0) at 2300 lbs. ( +9.5) to (+20.0) at 1600 lbs. or less Straight line variation between points given. Empty weight C.G. range None Maximum weight Landplane, Skiplane and Floatplane: 2300 lbs. Landplane modified per SL#48 and SL#51: 2500 lbs. Floatplane modified per 9173A: 2500 lbs. Number of seats 4 (2 at 15.1 to +18.1, 2 at 50) Maximum baggage 100 lbs. (+20), 175lbs. (+42), 125 lbs. (+70) Fuel capacity 43 gal. (40 gal. usable; two 21.5 gal. tanks in wings at +23.3) Optional wing auxiliary tanks 23 gal. (23 gal. usable; two 11.5 gal. tanks in wings at +22.2) See NOTE 16 if Modification Kit No. 15 is installed. (See NOTE 1 for data on system fuel.) Oil capacity 8.8 qt. (-37) 5.8 qt. minimum (See NOTE 1 for data on system oil.) Control surface Wing flaps Down 1st Notch 15º +3º movements Modified per 2nd Notch 35º +3º Maule SL#48 Down 1st Notch 20º +3º 2nd Notch 40º +3º Aileron Up 20º +1º Down 20º +1º Elevator Up 25º +2º Down 21º +1º Elevator tab Up 12º +4º Down 29º +2º Rudder Right 21º +1º Left 21º +1º Rudder tab Right 48º +4º Left 48º +4º Serial numbers eligible Model M-5-220C, 5001C-5057C. (See NOTE 13 for float installation requirement.) Production basis (No longer in production) VII. Model M-5-235C, 4 PCLM (Normal Category), Approved April 6, 1976 (Same as M-5-220C except for nacelle, engine, propeller and electrical system.) Engine Lycoming O-540-J1A5D, O-540-J3A5, IO-540-W1A5D, IO-540-W1A5, or O-540-B4B5 Fuel 100/100LL minimum grade aviation gasoline Rev. 34 9 of 47 3A23 Engine limits 235 hp at 2400 rpm, all operations (O-540-J/IO-540-W) 235 hp at 2575 rpm, all operations (O-540-B) Propeller and propeller limits (See NOTE 14 for propeller information) Airspeed limits (CAS) Landplane, Floatplane, and Skiplane: (See NOTE 11 for airspeeds) C.G. range Landplane: S/n 7001C-7026C, 7028C, 7030C-7032C, 7037C (+16.0) to (+20.5) at 2300 lbs. (+12.0) to (+20.5) at 1600 lbs. or less or - S/n 7001C-7026C, 7028C, 7030C-7032C, 7037C with expanded C.G. limits per Maule SL#36 (+12.5) to (+20.5) at 2300 lbs. (+10.5) to (+20.5) at 1700 lbs. or less or -S/n 7001C-7320C, 7322C-7346C, 7348C,7349C modified per Maule SL#43 (+13.2) to (+20.5) at 2500 lbs. (+10.5) to (+20.5) at 1700 lbs. or less or -S/n 7001C-7320C, 7322C-7346C, 7348C, 7349Cmodified per Maule SL#44 (+12.5) to (+20.5) at 2300 lbs. (+11.7) to (+20.5) at 1700 lbs. or less or -S/n 7001C-7320C, 7322C-7346C, 7348C, 7349C modified per Maule SL#43 and SL#44 and s/n 7321C, 7347C, 7351C, 7363C, 7369C and up (+13.2) to (+20.5) at 2500 lbs. (+11.7) to (+20.5) at 1700 lbs. or less Floatplane: EDO 248A2440, 248B2440 or Aqua 2400 Floats: (+14.3) to (+20.0) at 2530 lbs. (+13.3) to (+20.0) at 2100 lbs. or less Pee Kay 2300 Floats: (+14.3) to (+20.0) at 2500 lbs. (+13.3) to (+20.0) at 2100 lbs. or less EDO 248B2440, Aqua 2400, or EDO 797-2500 amphibious Floats (Floatplanes modified per Maule drawing 9143A (B2440's), 9166A (2400’s) or 9057A (amphibs)): (+14.0) to (+19.0) at 2750 lbs. (+10.5) to (+19.0) at 1600 lbs. or less Skiplane: FluiDyne C2200H, C3000H, C3000M or Fli-Lite 3000 MK IIIA Skis: (+12.5) to (+20.0) at 2300 lbs. (+9.5) to (+20.0) at 1600 lbs. or less FluiDyne A2500A Skis: (+12.9) to (+20.5) at 2300 lbs. (+11.7) to (+20.5) at 1700 lbs. or less Fli-Lite MK IIIA Skis (Skiplanes modified per Maule drawing 9081A): (+13.2) to (+20.0) at 2500 lbs (+11.7) to (+20.0) at 1700 lbs. or less FluiDyne C3000M or C3000H Skis (Skiplanes modified per Maule drawing 9158A for C3000M or 9174A, Rev. C or later for C3000H): (+13.2) to (+20.0) at 2500 lbs. (+10.7) to (+20.0) at 1700 lbs. or less Straight line variation between points given. Empty weight C.G. range None Maximum weight Landplane: 2300 lbs. Floatplane: 2530 lbs. (EDO 2440 only), 2500 lbs. (PeeKay 2300) Skiplane: 2300 lbs. Landplanes modified per Maule SL#43 and s/n 7321C, 7347C, 7350C and up: 2500 lbs. Floatplanes modified per Maule drawing 9143A (EDO B2440), 9166A(Aqua 2400), or 9057A (EDO amphibs): 2750 lbs. Skiplanes modified per Maule drawing 9081A (Fli-Lites), 9158A (C3000M), or 9174A (C3000H): 2500 lbs. Number of seats 4 (2 at +20, 2 at +50) Maximum baggage 100 lbs. (+20), 175lbs. (+42), 125 lbs. (+70) Rev. 34 10 of 46 3A23 Fuel capacity 43 gal. (40. gal. usable; two 21.5 gal. tanks in wings at +24) Optional wing auxiliary tanks 23 gal. (23 gal. usable; two 11.5 gal. tanks in wings at +24) See NOTE 16 if Modification Kit No. 15 is installed. (See NOTE 1 for data on system fuel.) Oil capacity IO-540: 8 qt. (-34), 5 qt. minimum O-540: 12 qt. (-34), 9 qt. minimum (See NOTE 1 for data on system oil.) Control surface Wing flaps (s/n 7001C-7320C, 7322C-7346C, 7348C-7350C, 7352C-7362C, 7364C-7368C): movements Down 1st Notch 15º +3º 2nd Notch 35º +3º (s/n 7321C, 7347C, 7351C, 7363C, 7369C and up and airplanes modified per Maule SL#44): Down 1st Notch 20º +3º 2nd Notch 40º +3º Aileron Up 20º +1º Down 20º +1º Elevator Up 25º +2º Down 21º +1º Elevator tab Up 12º +4º Down 29º +2º Elevator tab w/piano hinge Up 12º +2º Down 38º +2º Rudder Right 21º +1º Left 21º +1º Rudder tab Right 48º +4º Left 48º +4º Serial number eligible Model M-5-235C, 7001C and up