***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 73,000 lbs
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 73,000 lbs
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 73,000 lbs
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 73,000 lbs
Standard temperature, sea level pressure altitude, dry runway

Flaps 0

150 KIAS

Flaps 8

143 KIAS

Flaps 11

138 KIAS