*****AIRCRAFT
“McDonnell Douglas - DC9-30”*****
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: 27.3 m
Length: 36.4 m
Height: 8.38 m
Power plant: Series 10: 2 x 54,5 kN
P&W JT8D-7 turbofans.
Series 20/30: 2 x 64,5 kN
P&W JT8D-9 or 2 x 66,7 kN P&W JT8D-15
turbofans.
Accommodation: Flightcrew of two and typical 90 (80 in DC9-10/20) passengers,
max. 105 in
high density configuration.
Notes: Short to medium range airliner. In service since 1965. First
short range airliner in new design with rear fuselage mounted engines, T-tail
and swept wings.
Built in these
versions: - 10 initial type (ICAO Designator: DC91) - 30 stretched version
(ICAO Designator: DC93) with more powerful engines, - 20 (ICAO Designator:
DC92) combines
fuselage of -10 with engines of -30. The DC-9-30 was converted as
freighter and
mil. type C-9. 94 aircraft of -10, 5 of -20 and 520 of -30 remain in service in
1999. DC-9-10:
Wing span 27,25m Length 31,82m MTOW 41177 kg. DC-9-20: Wing span
28,5m Length
31,82m MTOW 44492 kg.
Alternative names:
DOUGLAS DC-9-30,
MCDONNELL DOUGLAS DC-9-30.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 49.940 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 3°)
1 1° 230(pich 3°)
2 2° 230(pich 3°)
3 5° 210(pich 5°)
4 10° 200(pich 4°)
5 15° 190(pich 4°)
6 25° 180(pich 4°)
170(pich 5°)
160(pich 7°)
7gear 30° 160(pich 5°)
150(pich 7°)
140(pich 8°)
130(pich 10°)
*****Take-off*****
WTC: M
Distance: 2100
mt
V2 (IAS): 140
kts
*****Climbing*****
-(to 5000 ft)
IAS: 170
kt
ROC: 2000
ft/min
-(to FL150)
IAS: 290
kt
ROC: 1500
ft/min
-(to FL240)
IAS: 290
kt
ROC: 1000
ft/min
-(mach)
mach: 0.74
ROC: 1000
ft/min
*****Cruise*****
TAS: 440
kt
MACh: 0.76 data
Ceiling: FL370
Range: 1500
NM
*****Descent
*****
- (to FL240)
mach: 0.76
ROD: 1000
ft/min
- (to FL100)
IAS: 290
kt
ROD: 3500
ft/min
*****Approach*****
IAS: 220
kt
MCS: 210
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 127 kt
APC: C
Distance: 1500
mt