***AIRCRAFT
“Fokker - F28 Fellowship”***
FOKKER F28 Mk.4000/Mk.6000
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: 27.07 m
Length: 27.4 m
Height: 8.5 m
Power plant: 3000/4000: 2 x 44 kN
RR RB 183-2 Spey-Mk555-15 P turbofans.
Accommodation: Flightcrew of two and typical 65 passengers, up to 85 in high density
configuration.
Notes: Short range regional airliner. In service since 1969. Developed
to complete the
F-27
Friendship turboprop airliner with a higher performance and larger capacity.
A family of aircraft
with versions F-28-1000/2000/3000/4000/6000 with different performance
regarding approach category and weight data. Also used in military service as
VIP and government transport. F-28-4000: length 29,61 m.
Alternative names:
Fellowship
FOKKER F-28 Fellowship.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 33.110 kg
VMO - Maximum Operating Speed 390 KIAS
MMO - Maximum Operating Speed Mach 0.70 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
8 250
11 230
18 220
25 220
45 180
*****Take-off*****
WTC: M
Distance: 1700
mt
V2 (IAS): 135
kts
V1 = VR - Takeoff Decision and
Rotation Speed at weight
Standard temperature, sea level pressure altitude, dry runway
Flaps 0 |
145 KIAS |
Flaps 8 |
138 KIAS |
Flaps 11 |
133 KIAS |
V2 - Takeoff Safety Speed at weight
Standard temperature, sea level pressure altitude, dry runway
Flaps 0 |
150 KIAS |
Flaps 8 |
143 KIAS |
Flaps 11 |
138 KIAS |
*****Climbing*****
-(to 5000 ft)
IAS: 165
kt
ROC: 2000
ft/min
-(to FL150)
IAS: 250
kt
ROC: 1500
ft/min
-(to FL240)
IAS: 250
kt
ROC: 1500
ft/min
-(mach)
mach: 0.6
ROC: 500
ft/min
*****Cruise*****
TAS: 390
kt
MACh: 0.70 data
Ceiling: FL350
Range: 1600 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): 125 kt
APC: C
Distance: 1000
mt
V1 = VR - Takeoff Decision and
Rotation Speed at weight
Standard temperature, sea level pressure altitude, dry runway
Flaps 0 |
145 KIAS |
Flaps 8 |
138 KIAS |
Flaps 11 |
133 KIAS |
V2 - Takeoff Safety Speed at weight
Standard temperature, sea level pressure altitude, dry runway
Flaps 0 |
150 KIAS |
Flaps 8 |
143 KIAS |
Flaps 11 |
138 KIAS |