M-7 SERIES

The Maule M-7 Series is a highly versatile aircraft. The M-7 can be loaded with 85 gallons of fuel which gives this 235 or 260 HP workhorse extended endurance. A four door fuselage design gives you easy cabin entry/exit and access to its cavernous cargo area. The Modular Cabin design allows you to quickly change the seating/cargo configuration to fit the needs of your excursions.

Pilot plus 4 Passengers.

Pilot plus 3 Passengers and Luggage.

Pilot and Copilot plus ~42 cu. ft. of Cargo Area.

These legendary Bush Models can be outfitted with Seaplane or Amphibious Floats, Alaskan Bushwheel Tires, Extended Heavy Duty Landing Gear for backcountry flying adventures.

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M-7-235B

Oleo Strut Gear Taildragger

Engine: Lycoming (2000hr. TBO) 0-540-B4B5, 235 HP Carbureted

Useful Load: 895 lbs. (407 kg)

Take Off, Ground Roll (gross weight): 250 ft (76 m)

Landing (light weight) over obstacle: 900 ft (274 m)

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Gross Weight: 2500 lbs. (1136kg)

Empty Weight: 1605 lbs. (730 kg)

Stall Speed (full flaps / power off / light weight) (IAS): 40 mph (35 kts)

Take Off (light weight) over 50' obstacle: 600 ft (183 m)

Rate of Climb, Initial (light weight): 1500 fpm (7.6 m/s)

Service Ceiling: 20,000 ft (6096 m)

Fuel Consumption US Gals. @ 65% Power (avg.): 12 gph (45 lph)

Cruise (75% Power / Opt. Alt.) (TAS): 158 mph (137 kts)

Performance Observations as for One Person, 22 Gal. of fuel, Sea Level, Standard Day Conditions.

(Do Not Use for Flight Planning)

M-7-260

Oleo Strut Gear Taildragger

Engine: Lycoming (2000hr. TBO) 0-540-V4A5, 260 HP Fuel Injected

Useful Load: 890 lbs. (405 kg)

Take Off, Ground Roll (gross weight): 250 ft (76 m)

Landing (light weight) over obstacle: 900 ft (274 m)

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Gross Weight: 2500 lbs. (1136kg)

Empty Weight: 1610 lbs. (732 kg)

Stall Speed (full flaps / power off / light weight) (IAS): 40 mph (35 kts)

Take Off (light weight) over 50' obstacle: 600 ft (183 m)

Rate of Climb, Initial (light weight): 1650 fpm (8.4 m/s)

Landing (light weight) over obstacle: 900 ft (274 m)

Service Ceiling: 20,000 ft (6096 m)

Fuel Consumption US Gals. @ 65% Power (avg.): 14 gph (53 lph)

Cruise (75% Power / Opt. Alt.) (TAS): 162 mph (141 kts)

Performance Observations as for One Person, 22 Gal. of fuel, Sea Level, Standard Day Conditions.

(Do Not Use for Flight Planning)

MT-7-235

Aluminum Spring Gear with Hydraulic Nosewheel Assembly

Engine: Lycoming (2000hr. TBO) I0-540-W1A5, 235 HP Fuel Injected

Useful Load: 835 lbs. (380 kg)

Take Off, Ground Roll (gross weight): 250 ft (76 m)

Landing (light weight) over obstacle: 900 ft (274 m)

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Gross Weight: 2500 lbs. (1136kg)

Empty Weight: 1665 lbs. (757 kg)

Stall Speed (full flaps / power off / light weight) (IAS): 40 mph (35 kts)

Take Off (light weight) over 50' obstacle: 600 ft (183 m)

Rate of Climb, Initial (light weight): 1500 fpm (7.6 m/s)

Service Ceiling: 20,000 ft (6096 m)

Fuel Consumption US Gals. @ 65% Power (avg.): 11 gph (42 lph)

Cruise (75% Power / Opt. Alt.) (TAS): 158 mph (137 kts)

Performance Observations as for One Person, 22 Gal. of fuel, Sea Level, Standard Day Conditions.

(Do Not Use for Flight Planning)

MT-7-260

Aluminum Spring Gear with Hydraulic Nosewheel Assembly

Engine: Lycoming (2000hr. TBO) I0-540-V4A5, 260 HP Fuel Injected

Useful Load: 804 lbs. (366 kg)

Take Off, Ground Roll (gross weight): 250 ft (76 m)

Landing (light weight) over obstacle: 900 ft (274 m)

MORE DETAILS

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Gross Weight: 2500 lbs. (1136kg)

Empty Weight: 1696 lbs. (771 kg)

Stall Speed (full flaps / power off / light weight) (IAS): 40 mph (35 kts)

Take Off (light weight) over 50' obstacle: 600 ft (183 m)

Rate of Climb, Initial (light weight): 1650 fpm (8.4 m/s)

Service Ceiling: 20,000 ft (6096 m

Fuel Consumption US Gals. @ 65% Power (avg.): 14 gph (53 lph)

Cruise (75% Power / Opt. Alt.) (TAS): 162 mph (141 kts)

Performance Observations as for One Person, 22 Gal. of fuel, Sea Level, Standard Day Conditions.

(Do Not Use for Flight Planning)