*****AIRCRAFT
“Fokker - F100”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Both sides of rear fuselage
Tail configuration: T-tail
Landing gear: Tricycle retractable
Wing Span: 28.1 m
Length: 35.5 m
Height: 8.5 m
Power plant: 2 x 44 kN R-R
RB.183 Mk 555-15P or
2 x 61,2 kN RR Tay Mk 620-15 or
2 x 67.6 kN R-R Tay Mk 650-15 turbofans
Accommodation: Flightcrew of two and typical 100 passengers in two classes, 107 in
single class and up to 122 in high density configuration.
Notes: Short to medium range airliner. In service since 1988. FOKKERs
largest jet aircraft. 100 seat based on stretched development of F28
Fellowship, simultaneously with development of the turboprop F50. The FOKKER
100 was offered in a number of versions. Production ceased in 1997.
Alternative names:
FOKKER 100.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 43.390 kg
VMO - Maximum Operating Speed 405 KIAS
MMO - Maximum Operating Speed Mach 0.73 Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: M
Distance: 1700
mt
V2 (IAS): 135
kts
*****Climbing*****
-(to 5000 ft)
IAS: 165
kt
ROC: 2500
ft/min
-(to FL150)
IAS: 250
kt
ROC: 2000
ft/min
-(to FL240)
IAS: 250
kt
ROC: 1500
ft/min
-(mach)
mach: 0.6
ROC: 1000
ft/min
*****Cruise*****
TAS: 405
kt
MACh: 0.73 data
Ceiling: FL350
Range: 3100 NM
*****Descent
*****
- (to FL240)
mach: 0.68
ROD: 800
ft/min
- (to FL100)
IAS: 250
kt
ROD: 3500
ft/min
*****Approach*****
IAS: 230
kt
MCS: 200
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 130 kt
APC: C
Distance: 1400
mt