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General| Model | MX-7-180 |
|---|---|
| Engine | Lycoming O-360 |
| Horsepower | 180 hp |
| Max Takeoff Weight | 2, 500 lb (1, 134 kg) |
| Takeoff Distance | 500 ft (152 m) |
| Seating Capacity | 4 |
| Manufacturer | Maule Air, Inc. |
| Type | Light aircraft |
| Length | 23 ft |
| Service Ceiling | 14, 000 ft |
| Rate of Climb | 1, 000 ft/min |
| Fuel Capacity | 50 US gal (189 L) |
Specifies the maximum weight and acceptable center of gravity limits for the aircraft.
Outlines approved flight maneuvers and details the aircraft's fuel capacity.
Details critical airspeed limitations and power plant operating parameters.
Defines permissible flight load factors and lists essential cockpit placards.
Covers preflight inspection procedures and operating checklists for normal flight.
Details normal flight operations, flap settings, climb performance, and rudder trim.
Specifies limitations for door-off operation, noise levels, and anti-collision light usage.
Covers fundamental emergency rules and procedures for engine fires during starting and after starting.
Details procedures for takeoff aborts, engine failures, and airstarts.
Addresses electrical fires, engine fires in flight, smoke, structural damage, spins, and alternator failure.
Summary of the aircraft's weight and balance data as delivered from the factory.
Procedure for calculating weight and center of gravity using loading charts and envelopes.
Introduction to aircraft servicing and requirements for inspection periods.
Guidelines for pilot preventive maintenance and aircraft alterations or repairs.
