U-21 Ute
| Specifications | |
|---|---|
| Aircraft | KING AIR A-90 |
| Length | 39.11 ft |
| Height | 15.5 ft |
| Wing Span | 45.11 ft |
| Weights |
Ramp Weight LBS: 10,500 (U-21A,B,C,D,H) Ramp Weight LBS: 11,500 (U-21F) Ramp Weight LBS: 14,500 (U-21J) Take Off Weight: 11,500 Landing Weight: 11,210 Zero Fuel Weight: 9,200 BOW: 7,100 |
| Fuel Cap | 3,149 lbs/std. |
| Useful Load | 4,110 lbs |
| Payload with Full Fuel | 1,251 lbs |
| Maximum Payload | 2,100 lbs |
| Max Range full Fuel | 1,384 miles |
| Power Plant |
PT6A-20 (U-21A,B,C,D,H)
P&W PT6A-28 680 SHP (U-21F) P&W PT6A-42 (U-21J) |
| Accommodations |
Crew 1 Passengers (Typical) 7 Passengers (Maximum) 9 |
| Rate of Climb |
All Engines 1,963 FT/MIN One Engine Out 452 FT/MIN |
| Max Cert. Alt. | 24,850 feet |
| Engine Out Ceiling | 9,300 feet (mid weight) |
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