M-7 Series
The Maule M-7 is the ultimate blend of power, durability, and versatility. Designed for backcountry adventures and everyday reliability, the M-7 delivers exceptional STOL performance, ample payload capacity, and rugged construction to tackle any terrain. Whether you’re flying into remote airstrips, hauling gear, or enjoying a weekend escape, the M-7 is built to take you further.
Oleo Strut Gear Taildragger
M-7-235B
Engine: Lycoming 0-540-B4B5 / IO-540-W1A5 (2000hr. TBO)
Useful Load (Average): 895 lbs. (407 kg)
Take Off, Ground Roll (light weight): 250 ft (76 m)
Landing (light weight) over obstacle: 900 ft (274 m)
Gross Weight: 2500 lbs. (1136kg)
Empty Weight: 1605 lbs. (728 kg)
Stall Speed (full flaps / power off / light weight) (IAS): 40 mph (35 kts)
Take Off, Ground Roll (light weight): 250 ft (76 m)
Take Off (light weight) over 50′ obstacle: 600 ft (183 m)
Rate of Climb, Initial (light weight): 1500 fpm (7.6 m/s)
Landing (light weight) over obstacle: 900 ft (274 m)
Service Ceiling: 15,000 ft (4572 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)
Oleo Strut Gear Taildragger
M-7-260
Engine: IO-540-V4A5 (2000hr. TBO)
Useful Load: 890 lbs. (433 kg)
Take Off, Ground Roll (light weight): 250 ft (92 m)
Landing (light weight) over obstacle: 600 ft (274 m)
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)
Service Ceiling: 15,000 ft (4572 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)
Aluminum Spring Gear with Hydraulic Nosewheel Assembly
MT-7-235
Engine: Lycoming IO-540-W1A5 (2000hr. TBO)
Useful Load: 835 lbs. (380 kg)
Take Off, Ground Roll (light weight): 250 ft (76 m)
Landing (light weight) over obstacle: 900 ft (274 m)
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 (5.1 m/s)
Service Ceiling: 15,000 ft (4572 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)
Aluminum Spring Gear with Hydraulic Nosewheel Assembly
MT-7-260
Engine: Lycoming IO-540-W1A5 (2000hr. TBO)
Useful Load: 804 lbs. (366 kg)
Take Off, Ground Roll (light weight): 250 ft (76 m)
Landing (light weight) over obstacle: 900 ft (274 m)
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, Ground Roll (light weight): 250 ft (76 m)
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: 15,000 ft (4572 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)