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+ Home > Platforms > Schedules > Flight Request > Partnerships > New Technologies
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Twin Otter
The de Havilland Twin Otter aircraft is a high wing, twin
engine, turbo prop aircraft capable of carrying up to
twenty passengers in the commuter role. The aircraft has
a wing span of 65 ft (19.8 m), length of 51 ft 9 in (15.7
m) and a maximum take-off weight of 12,500 lbs. (5670
kg). The Twin Otter is one of the de Havilland family
of "bush" aircraft noted for their rugged construction
and Short Take Off and Landing (STOL) performance. |
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| Owner/Operator: |
NASA-GSFC-WFF |
NASA-GRC |
| Type: |
Conventional Aircraft |
Conventional Aircraft |
| Duration: |
7 Hours |
3.5 Hours |
| Useful Payload: |
5,000 lbs |
3,600 lbs |
| Gross Take-off Weight: |
12000 lbs |
11000 lbs |
| Onboard Operators: |
8 (including flight crew) |
7 (including flight crew) |
| Max Altitude: |
25,000 ft. |
25,000 ft. |
| Air Speed: |
160 knots |
140 knots |
| Range: |
500 Nmi |
450 Nmi |
| Power: |
8400 W, 300 A at 28 VDC |
200A at 28Vdc |
| POC: |
Anthony Guillory
757-824-2161 |
Al Micklewright
216-433-2036 |
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