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AEROSPATIALE Mohawk 298
From SKYbrary Wiki
N262
Aircraft | |||||||||||
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Name | Mohawk 298 | ||||||||||
Manufacturer | AEROSPATIALE | ||||||||||
Body | Narrow | ||||||||||
Wing | Fixed Wing | ||||||||||
Position | High wing | ||||||||||
Tail | Regular tail, low set | ||||||||||
WTC | Medium | ||||||||||
APC | A | ||||||||||
Type code | L2T | ||||||||||
Aerodrome Reference Code | 3A | ||||||||||
Engine | Turboprop | ||||||||||
Engine count | Multi | ||||||||||
Position | (Front) Wing leading mounted | ||||||||||
Landing gear | Tricycle retractable | ||||||||||
Mass group | 3 | ||||||||||
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AEROSPATIALE Mohawk 298
Description
Short range commuter airliner. In service since 1963. Pressurized turbo-prop development of MH-260. Built in several versions, mainly used by French Military. Upgraded more powerful development Mohawk 298 since 1975, with new avionics and APU. Production ceased in 1978 after 110 aircraft including three Mohawk were built.
Technical Data
Wing span | 22.6 m74.147 ft |
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Length | 19.3 m63.32 ft |
Height | 6.2 m20.341 ft |
Powerplant | Variants:
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Engine model | Pratt & Whitney Canada PT6, Turboméca Bastan |
Performance Data
Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
V2 (IAS) | kts | IAS | kts | IAS | kts | IAS | kts | MACH | TAS | 200 kts | MACH | IAS | kts | IAS | kts | Vapp (IAS) | kts | ||
Distance | 1484 m | ROC | 1400 ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | 820 m | |
MTOW | 1080010,800 kg 10.8 tonnes kg |
Ceiling | FL260 | ROD | ft/min | APC | A | ||||||||||||
WTC | M | Range | 550550 nm 1,018,600 m 1,018.6 km 3,341,863.52 ft NM |
Accidents & Serious Incidents involving N262
None on SKYbrary