N94BF Specifications
Service Times:
- Total time since factory IRAN: 1,679 hours
- Total time on engine: 162 hours
- Next annual/100 hour inspection: February 2009
Instruments:
Instruments are stock Russian with English labels, except for the following
US equipment:
- Airspeed and altitude
- Collins radios
- Collins HSI and AI
- Garmin GPS 155XL
- STEC 55 Autopilot
- Shadin Digital Flowmeter System
- U.S. military O2 system
- Ejection seats have been deactivated
Engine:
- Type: AI-25 TL twin-shaft turbofan engine
- Bypass ratio: 1.98
- Maximum static thrust: 16.87 kN
- Specific fuel consumption: 56.9 kg/hr/kN
- Air flow: 46.75 kg/s
- Overall pressure ratio: 9.5
Dimensions:
| Wing Span |
9.46 m |
31 ft |
| Length, overall |
12.13 m |
39 ft 10 in |
| Height, overall |
4.77 m |
15 ft 8 in |
| Basic empty weight |
3,400-3,580 kg |
7,496-7,892 lb |
| Max ramp weight |
5,670 kg |
12,500 lb |
| Internal fuel capacity |
1,050 kg |
2,314 lb |
| Max level speed |
750 km/h |
450 KTAS |
| Never-exceed speed (sea level) |
910 km/h |
491 KTAS |
| Max rate of climb (approx.) |
21 m/s |
4,130 ft/min |
| Service ceiling (approx.) |
11,000 m |
36,000 ft |
| Take-off distance |
540 m |
1,770 ft |
| Landing distance |
550 m |
1,800 ft |
| Stall speed (dirty) |
158 km/h |
85 KTAS |
| Max structural limit |
+8g; -4g |
|
|
