Fokker F100

MSFS 2024 - QUICK REFERENCE

V-SPEEDS
SpeedValueDescription
V1~128 KIASTakeoff decision speed (weight/conditions dependent)
Vr~130 KIASRotation speed
V2~140 KIASTakeoff safety speed
Vle200 KIASMax gear extended / transit speed
Vfe (Flap 8)220 KIASMax speed flaps 8 degrees
Vfe (Flap 15)200 KIASMax speed flaps 15 degrees
Vfe (Flap 25)170 KIASMax speed flaps 25 degrees
Vfe (Flap 42)150 KIASMax speed flaps full (42 degrees)
Vapp~130 KIASApproach speed (typical landing weight)
Vref~122 KIASLanding reference speed (flap 25)
Vmo320 KIAS / Mach 0.77Maximum operating speed
POWER SETTINGS
PhaseSetting
Takeoff (TOGA)90-95% N1
Initial Climb85-88% N1 (Climb Thrust)
Cruise (FL280-330)Mach 0.73-0.75 / ~80% N1
DescentIDLE / Autothrottle managed
Approach~55-65% N1 (speed managed)
Ground Idle~20-22% N1
FLAP SCHEDULE
SettingMax SpeedUse
0 (UP)AnyCruise / Climb
8 deg< 220 KIASTakeoff (standard) / Initial approach
15 deg< 200 KIASTakeoff (short field) / Intermediate approach
25 deg< 170 KIASApproach / Landing
42 deg (FULL)< 150 KIASFinal approach and landing
ENGINE LIMITS
ParameterValue
Max EGT (Takeoff)880 C
Max EGT (Continuous)840 C
Max EGT (Start - abort limit)950 C
Max N1 (Takeoff)100%
Max N2 (Takeoff)100%
Idle N2~60-65%
Oil Pressure (Normal)40-90 PSI
Oil Temp (Max)155 C
Max Takeoff Thrust (Tay 620)61.6 kN (13,850 lbf) per engine
KEY NUMBERS
ParameterValue
Fuel Capacity~13,400 L (10,800 kg)
Fuel Burn (cruise)~2,000-2,400 kg/hr total
MTOW45,810 kg
MLW39,000 kg
Max Zero Fuel Weight36,000 kg
Takeoff Roll (MTOW, ISA SL)~1,820 m (5,970 ft)
Landing Roll~1,200 m (3,940 ft)
Pattern Speed200 KIAS (initial) / 130 KIAS (final)
Max Crosswind (Takeoff)29 kts
Max Crosswind (Landing)25 kts
Typical Cruise AltitudeFL280-FL370
Seating97-107 passengers