Aircraft Performance
| Weights (lb) | Falcon 20F, DA-20F | |||
|---|---|---|---|---|
| Max Ramp | 28,660 | |||
| Max Takeoff | 28,660 | |||
| Max Landing | 27,320 | |||
| Zero Fuel | 19,600c | |||
| BOW | 17,613 | |||
| Max Payload | 1,987 | |||
| Useful Load | 11,047 | |||
| Executive Payload | 1,800 | |||
| Max Fuel | 9,170 | |||
| Max Fuel | 9,170 | |||
| Avail Payload Max Fuel | 1,877 | |||
| Avail Fuel Max Payload | 9,060 | |||
| Avail Fuel Exec Payload | 9,170 | |||
| Limits | Falcon 20F, DA-20F | |||
| MMO | 0.870 | |||
| Transition Altitude FL/VMO | N/A | |||
| Cabin Pressurization (PSI) | 8.3 | |||
| Airport Performance | Falcon 20F, DA-20F | |||
| TO (Sea Level, ISA Temp) | 4,950 | |||
| TO (5000′, @25C) | 9,100 | |||
| Hot/High WAT | 27,383 | |||
| NBAA IFR Ranges V2 @ SL ISA, MTOW |
1,448 124 |
|||
| VREF | 105 | |||
| Landing Distance with 4 Passengers | 1,980 | |||
| Climb | Falcon 20F, DA-20F | |||
| Time to Climb/Alt | N/A | |||
| Engine Out Rate fpm | 715 | |||
| FAR 25 Engine-Out Grad (ft/nm) | 213 | |||
| Ceilings (ft) | Falcon 20F, DA-20F | |||
| Certificated | 42,000 | |||
| All Eng Srv | 42,000 | |||
| Eng Out Service | 18,200 | |||
| Sea Level Cabin | 18,200 | |||
| Long Range Cruise | Falcon 20F, DA-20F | |||
| KTAS | 399 | |||
| Fuel Flow | 1,595 | |||
| Altitude | FL 390 | |||
| Specific Range | 0.250 | |||
| High Speed Cruise | Falcon 20F, DA-20F | |||
| KTAS | 410 | |||
| Fuel Flow | 1,685 | |||
| Altitude | FL 390 | |||
| Specific Range | 0.243 | |||
| Data based on latest manufactured year | ||||