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MSFS 2024 · General Aviation
Hawker 800XP (FlightFX) Quick Reference
V-SPEEDS
| Speed | Value | Description |
|---|---|---|
| Vmo (Ventral Tank Empty) | 335 KIAS | Sea level to 12,000 ft, then reducing 1 KIAS per 680 ft to 310 KIAS at FL290 |
| Vmo (Ventral Tank Full) | 280 KIAS | Up to 33,730 ft, until the ventral fuel is transferred and the tank reads empty |
| Mmo | M0.80 | Indicated Mach number |
| Va | 196 KIAS | Maneuvering speed |
| Vra / Mra | 230 KIAS / M0.70 | Rough air penetration |
| Vlo / Vle | 220 KIAS | Gear operating and gear extended |
| V1 | 127 KIAS | 28,000 lb, sea level, flaps 0°, 15 °C. Read the takeoff V-speed tables for the actual weight, altitude and temperature |
| Vr | 136 KIAS | 28,000 lb, sea level, flaps 0°, 15 °C |
| V2 | 144 KIAS | 28,000 lb, sea level, flaps 0°, 15 °C |
| Vfto | 170 KIAS | Final takeoff speed at 28,000 lb, flaps 0° |
| Verc | 187 KIAS | En-route climb speed at 28,000 lb |
| Vref (Flaps 45°, MLW) | 127 KIAS | At 23,350 lb |
| Vref Range | 108 KIAS at 17,000 lb to 127 KIAS at 23,350 lb | Above MLW: 129 KIAS at 24,000 lb up to 137 KIAS at 28,000 lb |
| Minimum Single-Engine Vref | 111 KIAS | - |
| Vref Additives | Icing +10 / No flap +15 / Icing and no flap +30 KIAS | - |
| Vapp | Vref + 10 KIAS | Set automatically by the FMS, adjustable in the PFD REFS menu |
POWER SETTINGS
| Phase | Setting |
|---|---|
| Takeoff | N1 per the Take Off N1 reference tables - APR armed, cabin air OFF |
| Normal Climb | 160 KIAS at 1,000 ft, 250 KIAS from 5,000 ft to 32,000 ft, then 0.70 IMN |
| Optimum Time-to-Height Climb | 250 KIAS to 28,000 ft, then 0.63 IMN |
| High Speed Cruise | VMO / MMO at maximum cruise thrust |
| Intermediate Cruise | 280 KIAS / 0.75 IMN |
| Long Range Cruise | 230 / 220 KIAS / 0.70 IMN |
| Maximum Cruise Thrust | N1 per table, ITT limit 932 °C |
| Maximum Continuous Thrust | N1 per table, ITT limit 968 °C - abnormal or single-engine use only, not a cruise setting |
| Descent | 0.76 IMN / 285 / 250 KIAS - 1,000 fpm to FL370, then idle to 1,500 ft |
| Turbulence | 230 KIAS / 0.70 Mach |
FLAP SCHEDULE
| Setting | Max Speed | Use |
|---|---|---|
| 0° (UP) | Any | Takeoff (V-speed tables published for 0° and 15°), climb and cruise |
| 15° | 220 KIAS max | Takeoff, and the missed approach retraction setting |
| 25° | 175 KIAS max | Intermediate setting |
| 45° | 165 KIAS max | Landing - required before lift dump |
| 75° (Lift Dump) | Ground only | Airbrake handle to DUMP after touchdown with flaps at 45° |
ENGINE LIMITS
| Parameter | Value |
|---|---|
| Engine | 2x Honeywell TFE731-5BR-1H, 4,660 lbf each (flat rated to ISA +15 °C) |
| ITT - Start / Relight (AFM) | 978 °C unrestricted, 996 °C for 10 s, over 996 °C for 5 s |
| ITT - Takeoff (AFM) | 978 °C for 5 min, 1,006 °C for 5 s, 1,016 °C for 2 s |
| ITT - APR Operating (AFM) | 996 °C for 5 min, including the time at initial takeoff thrust |
| ITT - Maximum Continuous Thrust | 968 °C - not a normal cruise setting |
| ITT - Maximum Cruise Thrust | 932 °C |
| N1 / N2 Maximum (AFM) | 100% / 100.8%; overspeed 103% / 103% for 5 s |
| DEEC Overspeed Shutdown | 107% N1 / 109% N2 |
| Oil Pressure (AFM) | 38-46 psi takeoff, MCT and climb; 25 psi minimum at idle; 55 psi transient for 3 min |
| Oil Temperature (AFM) | 127 °C max to 30,000 ft, 140 °C above; 149 °C transient for 2 min; -40 °C minimum start, 30 °C minimum takeoff |
| OIL LO PRESS Warning | Below 23 psi, clears above 25 psi (gauge 0-70 psi) |
| Engine Anti-Ice | Expect +20 to +50 °C ITT when engaged |
| Fuel Introduction | HP cock lever up at 15% N2 |
| APR | Triggers on a greater than 5% N2 split while armed |
| Generator Load | 300 A continuous each |
| Battery | 23 V minimum; charge rate below 20 A before takeoff |
| APU RPM | 110% maximum |
| APU EGT | 732 °C normal; 974 °C for 10 s or 870 °C for 15 s during start |
| APU Altitude | Start up to 20,000 ft, operate up to 30,000 ft - not approved in icing |
KEY NUMBERS
| Parameter | Value |
|---|---|
| MRW | 28,120 lb (12,755 kg) |
| MTOW | 28,000 lb (12,701 kg) |
| MLW | 23,350 lb (10,591 kg) |
| MZFW | 18,450 lb (8,369 kg) |
| Basic Operating Weight (Typical) | 16,010 lb |
| Max Payload | 2,440 lb (1,750 lb with full fuel) |
| Fuel Capacity | 10,000 lb - 1,486 US gal (1,474 usable) |
| Ventral Tank | About 1,500 lb (224 US gal) - full or empty only, transfer at 3,300 lb wing fuel |
| Fuel Imbalance | 500 lb maximum between wings |
| Max Cabin Differential | 8.55 psi (negative 0.5 psi) |
| Service Ceiling | 41,000 ft |
| Max Cruise Speed | 447-449 kts |
| NBAA IFR Range | 2,540 nmi |
| Takeoff Field Length (28,000 lb, SL, 15 °C, Flaps 0°) | 5,377 ft |
| Landing Field Length (23,350 lb, SL, Flaps 45°) | 4,420 ft dry / 5,090 ft wet (factored) |
| TKS Anti-Ice Fluid | 10 US gal, about 108 minutes |