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.
![](https://mauleairinc.com/wp-content/uploads/2020/12/m71.png)
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)
![](https://mauleairinc.com/wp-content/uploads/2020/12/m72.png)
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)
![](https://mauleairinc.com/wp-content/uploads/2020/12/m73.png)
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)
![](https://mauleairinc.com/wp-content/uploads/2020/12/m74.png)
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)