User:Ak yeti/sandbox

The Maule M-5 is an American four-seat cabin monoplane designed and built by the Maule Aircraft Company.

Powerplant | Lycoming IO-540-W1A5, 235 hp @ 2,400 rpm

Recommended TBO | 2,000 hr

Propeller | McCauley 3-blade 80 in. dia constant speed

Length | 23 ft 8 in

Height | 6 ft 3 in

Wingspan | 32 ft 11 in

Wing area | 165.6 sq ft

Wing loading | 16.9 lb/sq ft

Power loading | 11.9 lb/hp

Seats | 5

Cabin length | 8 ft 3 in

Cabin width | 3 ft 6 in

Cabin height | 3 ft 8 in

Empty weight | 1,700 lb

Empty weight, as tested | 1,706 lb

Max gross weight | 2,800 lb

Useful load | 1,100 lb

Useful load, as tested | 1,094 lb

Payload w/full fuel | 590 lb

Payload w/full fuel, as tested | 584 lb

Fuel capacity, std | 89.6 gal (85 gal usable)

537.6 lb (510 lb usable)

Baggage capacity | 170 lb

PERFORMANCE Takeoff distance, ground roll | 406 ft

Takeoff distance over 50-ft obstacle | 791 ft

Max demonstrated crosswind component | 12 kt

Rate of climb, sea level | 800 fpm

Cruise speed/endurance w/45-min rsv, std fuel

(fuel consumption)

@ 75% power, best economy | 137 kt/5.7 hr

7,500 ft | (78 pph/13 gph)

@ 65% power, best economy | 122 kt/6.2 hr

7,500 ft | (72 pph/12 gph)

Service ceiling | 20,000 ft

Landing distance over 50-ft obstacle | 900 ft

Landing distance, ground roll | 250 ft

Limiting and Recommended Airspeeds VX (best angle of climb) | 65 KIAS

VY (best rate of climb) | 78 KIAS

VA (design maneuvering) | 109 KIAS

VFE (max flap extended) | 82 KIAS

VNO (max structural cruising) | 126 KIAS

VNE (never exceed) | 156 KIAS

VS1 (stall, clean) | 53 KIAS

VSO (stall, in landing configuration) | 43 KIAS