M-7 Series
The Maule MX-7 Series is a fun and easy to fly STOL aircraft. Powered by a 180hp Lycoming 4 cylinder engine it provides a perfect blend of performance and fuel efficiency! All MX-7-180 models have an available Auto-Fuel STC for Unleaded Mogas. The MX-7 Series is very agile and versatile with a large ~38 cu. ft. cargo area and high useful load. This is an excellent aircraft for law enforcement and military missions.
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)