*****AIRCRAFT
“McDonnel Douglas MD95”*****
REFERENCE INFORMATION (by others)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Both sides of rear fuselage
Tail configuration: T tail
Landing gear: Tricycle retractable
Wing Span: 32.9 m
Length: 46.5 m
Height: 9.3 m
Power plant: 30: 2 x 111.21 kN
IAE V2500-D5 turbofans.
55: 2 x 124.55 kN IAE V2528
D5 turbofans.
Flightcrew of
two and 153 passengers in two classes,
up to 172 in single class configuration.
Notes: Short to medium range airliner. In service
since 1994.
More powerful, stretched development of DC-9 family.
MD-90-30 standard version, MD-90-30T licence production
by TRUNKLINERS, China, and MD-90-55 optimized for
extended range.
Short fuselage development MD-95, renamed by BOEING to
717-200
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 78.245 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
1 inside 250(5°)
2 0 250(3°)
3 4 230(3°)
4 11 210(3°)
5 15 200(3°)
6 24 180(3°)
7 28 170(3°)
8 40 160(3°)
150(4°)
140(5°)
130(7°)
120(11°)
Gear dwn 160(3°)
150(4°)
140(6°)
130(8°)
120(12°)
*****Take-off*****
WTC: M
Distance: 2200
mt
V2 (IAS): 140
kts
*****Climbing*****
-(to 5000 ft)
IAS: 170
kt
ROC: 3200
ft/min
-(to FL150)
IAS: 290
kt
ROC: 2500
ft/min
-(to FL240)
IAS: 290
kt
ROC: 2500
ft/min
-(mach)
mach: 0.74
ROC: 1000
ft/min
*****Cruise*****
TAS: 435
kt
MACh: 0.76 data
Ceiling: FL370
Range: 2200 NM
*****Descent
*****
- (to FL240)
mach: 0.76
ROD: 1000
ft/min
- (to FL100)
IAS: 290
kt
ROD: 3500
ft/min
*****Approach*****
IAS: 250
kt
MCS: 210
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 140 kt
APC: C
Distance: 1600
mt