*****AIRCRAFT
“Boeing - B737-200”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Underwing
mounted
Tail configuration: Regular tail, mid set
Landing gear: Tricycle retractable
Wing Span: 28.3 m
Length: 30.5 m
Height: 11.3 m
Power plant: 2 x 64.5 kN
P&W JT8D-9A or
2 x 68.9 kN P&W JT8D-15A
or
2 x 71.2 kN P&W JT8D-17
or
2 x 77.4 kN P&W JT8D-17R
turbofans.
Optional with Hush-Kits for noise reduction.
Accommodation: Flightcrew of two and typical 115 passengers in single class,
up to 130 in
high density configuration.
Notes: Short range airliner. In service since 1969. The most used
member of first
generation of
BOEING 737 family. Stretched version of the orginal
737-100.
Production
ceased in 1988. 1144 aircraft of 737-200 were built, approx. 900
remain in
service in 1999. Mil. type: CT-43 and VC96.
Alternative names:
BOEING 737-200.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 52.390 kg
VMO - Maximum Operating Speed 400 KIAS
MMO - Maximum Operating Speed Mach 0.72 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
1 250
2 210
5 200
10 190
15 180
25 170
30 160
40 gear 150
*****Take-off*****
WTC: M
Distance: 1830
mt
V2 (IAS): 145
kts
*****Climbing*****
-(to 5000 ft)
IAS: 175
kt
ROC: 1500
ft/min
-(to FL150)
IAS: 250
kt
ROC: 1200 ft/min
-(to FL240)
IAS: 250
kt
ROC: 1000
ft/min
-(mach)
mach: 0.68
ROC: 500
ft/min
*****Cruise*****
TAS: 400
kt
MACh: 0.72 data
Ceiling: FL370
Range: 1200
NM
*****Descent
*****
- (to FL240)
mach: 0.70
ROD: 800
ft/min
- (to FL100)
IAS: 250
kt
ROD: 3500
ft/min
*****Approach*****
IAS: 210
kt
MCS: 210
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 150 kt
APC: C
Distance: 1400
mt