FALCON BMS · Fighter

F-16C Block 50 Quick Reference

V-SPEEDS

SpeedValueDescription
Rotation10 kt below computed takeoff speed15 kt below for an afterburner takeoff; rotate to 8-12 deg
Gear up limit300 ktGear must be up and locked before exceeding 300 kt
Gear down (downwind)Below 300 kt-
Initial300 kt-
Final approach AOA11-13 degComputed final approach airspeed flown to this AOA
Aerodynamic brakingTo approx 100 ktEffective as low as 80 kt; max 13 deg AOA
Cruise / air refuelling310 kt at 30,000 ft-
Max range airspeed200 kt at 20,000 lb GWIncreases 5 kt per 1,000 lb of actual weight

POWER SETTINGS

PhaseSetting
Takeoff (brake release)Approx 90 percent RPM (GE100 / GE129)
Takeoff (MIL)Nozzle 15 percent or less after 5 sec at MIL
Takeoff (AB)Nozzle preopens up to 10 percent beyond MIL; light-off within 5 sec
Below 10,000 ft MSL300-350 kt point to point; 350-400 kt rejoins on departure
G-awareness exercise entry400-450 kt
ShutdownThrottle OFF; no oil scavenge needed on the GE129

FLAP SCHEDULE

SettingMax SpeedUse
Leading edge flapsAutomaticScheduled by the FLCS; extend downward as the aircraft lifts off
Trailing edge flapsAutomatic with gearRetract when the landing gear handle is raised
ALT FLAPS - EXTENDEmergencyUsed with BRAKES CHAN 2 if the gear handle will not lower

ENGINE LIMITS

ParameterValue
EngineF110-GE-129 (GE129)
Brake release RPMApprox 90 percent
MIL nozzle position15 percent or less after 5 sec
AB light-offWithin 5 sec above 4 degC, 10 sec at 4 degC or below
Hot start recovery (airstart)Throttle OFF, let FTIT fall below 700 degC before advancing
Airstart ENG CONTSEC for approx 10 sec, then PRI if no recovery
MAIN PWR OFF delayUntil RPM decreases through 20 percent
Post-shutdown tailpipe fireAvoid inlet and exhaust areas for 5 min
JFS accumulator recharge1 min of rotation at 12 percent RPM or above

KEY NUMBERS

ParameterValue
MLG tire speed limit225 kt groundspeed
NLG tire speed limit217 kt groundspeed
Brake energy limit23.5 million ft-lb per brake
Parking brake after landingDo not use for 30 min
Arresting cable crossingBelow 90 kt groundspeed with a centreline store
Max fuel transfer - 300 gal tank18,000 pph
Max fuel transfer - 370/600 gal tanks30,000 pph
Wing turbine pump transfer rate6,000 pph maximum
Max fuel flow, one reservoir empty25,000 pph
Negative g - afterburner10 sec
Negative g - MIL or below30 sec
CABIN PRESS caution lightAbove 27,000 ft cockpit altitude
Flameout landing runway8,000 ft minimum recommended