*****AIRCRAFT “Fokker - F70”*****

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: 29.1 m

Length: 30.9 m

Height: 8.5 m

Power plant: 2 x 61.6 kN Rolls-Royce TAY Mk 620 turbofans.

Accommodation: Flightcrew of two and 79 passengers in single class configuration.

Notes: Short range regional airliner. In service since 1994. Shortened development

of the 100 seat class FOKKER 100 as replacement of the FOKKER F28.

FOKKER 70A optimised for US carriers, 70ER extra fuel tanks for extended range operation.

Also used in military service as VIP and government transport.

Production ceased in 1997.
Alternative names:
FOKKER 70.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 36.740 kg

VMO - Maximum Operating Speed 430 KIAS

MMO - Maximum Operating Speed Mach 073 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

 

Weight and Speed specifications

Maximum Take Off Weight  - MTOW

80,828 lbs

Maximum Landing Weight - MLW

74,844 lbs

Maximum Zero Fuel Weight - MZFW

70,345 lbs

Maximum Operating Speed - VMO

320 KIAS

Maximum Operating Speed Mach - MMO

.77 Mach

Rough Air Speed - VRAS/MRAS

250 KIAS/.65 Mach

Maximum Gear Operating Speed  - VLO

200 KIAS

Maximum Landing Gear Extension Speed - VLE

200 KIAS/.82 Mach

Maximum altitide (ceiling)

35,000 ft

Maximum range (with full payload)

1,600 NM

Maximum # of passenger @ 200 lbs payload ea.

79

 

*****Maximum Flap Placard Speeds*****

Flaps degr       KIAS

8                      250

15                    220

25                    220

45                    180

 

 

*****Take-off*****

WTC:               M

Distance:         1300 mt

V2 (IAS):         125 kts

 

V1 = VR - Takeoff Decision and Rotation Speed at weight 44,000 lbs
Standard temperature, sea level pressure altitude, dry runway

Flaps 0

147 KIAS

Flaps 8

139 KIAS

Flaps 15

136 KIAS

V2 - Takeoff Safety Speed at weight 44,000 lbs
Standard temperature, sea level pressure altitude, dry runway

Flaps 0

150 KIAS

Flaps 8

142 KIAS

Flaps 15

138 KIAS

 

*****Climbing*****

-(to 5000 ft)

IAS:                 155 kt

ROC:               3000 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:                430 kt

MACh:             0.73 data

Ceiling:            FL350

Range: 1100 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):        120 kt

APC:                B

Distance:         1200 mt

 

VREF - Landing Approach Speed with flaps 42, gear down
Standard temperature, sea level pressure altitude, dry runway

28,000 kg

109 KIAS

44,000 kg

133 KIAS