The M-5-180C is an initial production variant of the Maule M-5 aircraft. This single-engine aircraft was developed from the earlier Maule M-4, specifically designed for improved Short Takeoff and Landing (STOL) performance. The M-5, which entered production in 1974, features a 30% increase in flap area and enlarged tail surfaces compared to its predecessor. The M-5-180C is powered by a 180-horsepower Lycoming O-360-C1F engine, with over 94 units built during its manufacturing run between 1974 and 1983.
MAULE AIR, founded by B.D. Maule in the 1950s, has a foundational history in building utility and tailwheel aircraft. The company is known for producing aircraft valued for their utility and backcountry flying capabilities.
A selection of maintenance platforms and stands is indispensable for accessing the M-5-180C. Modular Stepover Platforms and Bridge Decks offer access across the wing and engine pylon areas, crucial for servicing the Lycoming engine, fuel tanks, and wing surfaces. For the Nose Section, including the engine inlet/exhaust and undercowl, Super Maintenance Platforms provide elevated access. For working on the landing gear (NLG and MLG) and the lower forward fuselage for systems like the Environmental Control System, tools like Platform Ladder Warthog and Super Service Stand are excellent solutions. Cantilever Platforms and Ultraraise systems allow detailed access to the tail section (empennage), including the vertical and horizontal stabilisers and rudder, ensuring thorough maintenance across the entire airframe.
