| Aircraft Data Learjet 25D |
|
| Weights | |
| Ramp Weight LBS: | 15,500 |
| Take Off Weight: | 15,000 |
| Landing Weight: | |
| Zero Fuel Weight: | |
| BOW: | 8,591 |
| Fuel Cap/lbs/std. | 6,098 |
| Useful Load | 6,909 |
| Payload with Full Fuel | |
| Maximum Payload | |
| Max Range full Fuel | 1,437 |
| NBAA IFR Fuel Reserves | 1,014 |
| Power Plant | |
| Manufacturer | GE |
| Model | CJ-610-8A |
| Thrust | 2,950 lbs. |
| Thrust Reversers |
|
| FAR 36 Noise Levels | |
| T/Off EPNDB | |
| Sideline | |
| Approach | |
| Meets Stage 3 Restrictions | |
| Speeds | |
| VMC Ground | |
| VMC Air | |
| V2 | |
| VREF | |
| Pressurization | |
| Pressure Differential Psi | 9.4 |
| Sea Level Cabin to Ft | |
| Cabin @ Max. Cert. Alt. | |
| Accommodations | |
| Seats Crew | 2 |
| Passengers (Typical) | 7 |
| Passengers (Maximum) | 10 |
| Vol. - Total Pass Cabin Cu Ft | |
| Baggage Total | |
| Internal % | |
| Dimensions | |
| Length | 47.7 |
| Height | 12.3 |
| Wing Span | 35.7 |
| Main Door Size INCH | |
| Performance | |
| Rate of Climb | |
| All Engines FT/MIN | |
| One Engine Out | 1,910 |
| Initial Cruise Alt Ft. | |
| Max Cert. Alt. | 51,000 |
| Time to Init Cruise Alt Min. | |
| Engine Out Ceiling (mid weight)Ft. | |
| Cruise Speed (KTAS)-Norm/LR | 446 |
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