User:Ak yeti/sandbox: Difference between revisions
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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. --> |
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{|{{Infobox Aircraft Begin |
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|name= M-9 |
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}}{{Infobox Aircraft Type |
}}{{Infobox Aircraft Type |
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|type=Four-seat cabin monoplane |
|type=Four-seat cabin monoplane |
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|produced=1974-1983 |
|produced=1974-1983 |
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|number built= over 855 |
|number built= over 855 |
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|developed from=[[Maule M- |
|developed from=[[Maule M-7]] |
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|variants with their own articles= |
|variants with their own articles= |
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}} |
}} |
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| ⚫ | |||
Powerplant | Lycoming IO-540-W1A5, 235 hp @ 2,400 rpm |
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Recommended TBO | 2,000 hr |
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Propeller | McCauley 3-blade 80 in. dia constant speed |
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Length | 23 ft 8 in |
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Height | 6 ft 3 in |
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Wingspan | 32 ft 11 in |
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Wing area | 165.6 sq ft |
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Wing loading | 16.9 lb/sq ft |
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Power loading | 11.9 lb/hp |
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Seats | 5 |
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Cabin length | 8 ft 3 in |
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Cabin width | 3 ft 6 in |
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Cabin height | 3 ft 8 in |
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Empty weight | 1,700 lb |
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Empty weight, as tested | 1,706 lb |
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Max gross weight | 2,800 lb |
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Useful load | 1,100 lb |
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Useful load, as tested | 1,094 lb |
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Payload w/full fuel | 590 lb |
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Payload w/full fuel, as tested | 584 lb |
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Fuel capacity, std | 89.6 gal (85 gal usable) |
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537.6 lb (510 lb usable) |
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Baggage capacity | 170 lb |
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PERFORMANCE |
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Takeoff distance, ground roll | 406 ft |
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Takeoff distance over 50-ft obstacle | 791 ft |
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Max demonstrated crosswind component | 12 kt |
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Rate of climb, sea level | 800 fpm |
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Cruise speed/endurance w/45-min rsv, std fuel |
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(fuel consumption) |
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@ 75% power, best economy | 137 kt/5.7 hr |
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7,500 ft | (78 pph/13 gph) |
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@ 65% power, best economy | 122 kt/6.2 hr |
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7,500 ft | (72 pph/12 gph) |
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Service ceiling | 20,000 ft |
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Landing distance over 50-ft obstacle | 900 ft |
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Landing distance, ground roll | 250 ft |
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Limiting and Recommended Airspeeds |
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VX (best angle of climb) | 65 KIAS |
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VY (best rate of climb) | 78 KIAS |
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VA (design maneuvering) | 109 KIAS |
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VFE (max flap extended) | 82 KIAS |
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VNO (max structural cruising) | 126 KIAS |
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VNE (never exceed) | 156 KIAS |
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VS1 (stall, clean) | 53 KIAS |
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VSO (stall, in landing configuration) | 43 KIAS |
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| ⚫ | |||
Latest revision as of 21:49, 9 December 2018
| M-9 | |
|---|---|
| Role | Four-seat cabin monoplane |
| National origin | United States |
| Manufacturer | Maule Aircraft Company |
| Designer | Belford Maule |
| First flight | 1971 |
| Introduction | 1974 |
| Produced | 1974-1983 |
| Number built | over 855 |
| Developed from | Maule M-7 |
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