AIRCRAFT
“McDonnell Douglas - MD80/81/82”
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: 32.8 m
Length: 45.1 m
Height: 9.05 m
Power plant: 2 x 89kN Pratt & Whitney JT8D-217A/C
Accommodation: Flightcrew of two and 152 passengers in two classes,
up to 172 in
single class configuration.
Notes: Short to medium range
airliner. In service since 1980. Series -80, -81, -82
and 88 are
very similar in terms of performance.
ICAO
designators MD80, MD81, MD82 and MD88.
Produced until
December 1999.
Alternative names:
MCDONNELL DOUGLAS
MD-82.
*****Total Flight
Simulator aircraft weight with full fuel*****
000,000 lbs - 67.812 kg
VMO - Maximum Operating Speed 440 KIAS
MMO - Maximum Operating Speed Mach 0.76 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
0 0° 250(pich 5°)
1 15° 220(pich 3°)
2 20° 200(pich 3°)
3 35° 170(pich 2°)
4 50° 160(pich -0°)
150(pich1°)
140(pich3°)
130(pich5°)
120(pich9°)
full gear 160(pich -0°)
150(pich1°)
140(pich3°)
130(pich5°)
120(pich9°)
*****Take-off*****
WTC: M
Distance: 2052
mt
V2 (IAS): 140
kts
*****Climbing*****
-(to 5000 ft)
IAS: 170
kt
ROC: 2500
ft/min
-(to FL150)
IAS: 290
kt
ROC: 2800
ft/min
-(to FL240)
IAS: 290
kt
ROC: 2000
ft/min
-(mach)
mach: 0.75
ROC: 1000
ft/min
*****Cruise*****
TAS: 440
kt
MACh: 0.76 data
Ceiling: FL370
Range: 2052
NM
*****Descent
*****
- (to FL240)
mach: 0.75
ROD: 1500
ft/min
- (to FL100)
IAS: 290
kt
ROD: 1500
ft/min
*****Approach*****
IAS: 250
kt
MCS: 210
kt
ROD: 1000
ft/min
*****Landing*****
Vht
(IAS): 150 kt
APC: C
Distance: 1585
mt