Performance Database
 |
|
CHALLENGER 605 |
|
Engines |
|
| Make | General Electric |
| Model | CF34-3B |
| HP/Thrust lbs per engine | 8,729 |
Fuselage Dimension |
|
| Length (ft) | 68.4 |
| Height (ft) | 20.7 |
| Wing Span (ft) | 64.3 |
| Passengers | 9 + 2 Crew |
Weights (lbs) |
|
| Max Ramp | 48,300 |
| Max Takeoff | 48,200 |
| Zero Fuel | 32,000 |
| Basic Operating | 26,985 |
| Max Landing | 38,000 |
| Maximum Payload | 5,015 |
| Payload with full fuel | 1,315 |
Fuel Capacity |
|
| Standard lbs/gal | 20,000/2,985 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 5,840 |
| 5000 +20C BFL (ft) | 9,165 |
Landing Performance (ft) |
|
| FAA Field Length | 2,777 |
Range (NM) |
|
| Max Range | 4,045 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 1,761 |
| Engine Out (fpm) | 581 |
Speeds (Knots) |
|
| Normal Cruise TAS | 470 |
| Vmo (Max Operating) IAS | 348 |
Ceiling (ft) |
|
| Certified Ceiling | 41,000 |
Specifications are provided as introductory information only and
are subject to verification by the buyer during a prepurchase inspection
of the aircraft. The aircraft is offered subject to prior sale,
price changes and/or removal from the market without notice.
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