Performance Database
 |
|
CHALLENGER 600 |
|
Engines |
|
| Make | Lycoming |
| Model | ALF-502L or -2C |
| HP/Thrust lbs per engine | 7.500 |
| TBO (hours) | 4.000 |
Fuselage Dimension |
|
| Length (ft) | 68.40 |
| Height (ft) | 20.70 |
| Wing Span (ft) | 64.30 |
| Passengers | 11 + 2 Crew |
| Volume Interior (cu.ft) | 1.035 |
| Volume Baggage (cu.ft) | 115 |
| Pressurization (psi) | 9.3 |
Weights (lbs) |
|
| Max Ramp | 41.400 |
| Max Takeoff | 41.250 |
| Zero Fuel | 28.500 |
| Basic Operating | 24.150 |
| Max Landing | 36.000 |
| Useful Load | 17.250 |
| Maximum Payload | 6.850 |
| Payload with full fuel | 2.610 |
Fuel Capacity |
|
| Standard lbs/gal | 15.069 / 2.216 |
| Optional lbs/gal | 16.665 / 2487 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 5.700 |
| 5000 +20C BFL (ft) | 8.750 |
Landing Performance (ft) |
|
| FAA Field Length | 3.050 |
Range (NM) |
|
| Max Range | 2.909 |
| Full passengers | 2.800 (2.900) |
| Two passengers (200 lbs each) | 2.900 (3.050) |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 3.400 |
| Engine Out (fpm) | 743 |
| Initial Cruise Altitude | 37.000 |
| Time to Cruise Altitude (minutes) | 27 |
Speeds (Knots) |
|
| Vso (Landing) | 102 |
| Normal Cruise TAS | 442 |
| Vmo (Max Operating) IAS | 365 |
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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