DC91
DOUGLAS DC-9-10
DOUGLAS DC-9-10
Aircraft
Name
DC-9-10
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, high set
WTC
M
Type Code
L2J
RFF Category
6
Engine
Jet
Engine Count
Multi
Position
Both sides of rear fuselage
Landing gear
Tricycle retractable
Manufactured as
MCDONNELL DOUGLAS DC-9-10
DOUGLAS DC-9-10
DC91
The McDonnell Douglas DC-9 (initially known as the Douglas DC-9) is a twin-engine, single-aisle jet airliner. It was first manufactured in 1965 with its maiden flight later that year. The DC-9 was designed for frequent, short flights. The final DC-9 was delivered in October 1982. The DC91 is member of the DC-9 family of aircraft.
Technical Data
Wing span (metric)
27.25 m
Length (metric)
31.82 m
Height (metric)
8.38 m
Powerplant
2 x Pratt & Whitney JT8D-5 or -7 (62.3 kN) thrust each.
Engine Model(s)
Pratt & Whitney JT8D
Indicative Performance Data
Take-Off
V2
115 kts
Distance
1615 m
MTOW
41100 kg
Initial Climb (to 5000 ft)
IAS
150 kts
ROC
2800 ft/min
Initial Climb (to FL150)
IAS
240 kts
ROC
2500
Initial Climb (to FL240)
IAS
240 kts
ROC
2000 ft/min
MACH Climb
MACH
0.72
ROC
1500 ft/min
Cruise
TAS
380 kts
MACH
0.74
Ceiling
350
Range
1265 NM
Initial Descent (to FL240)
MACH
0.74
ROD
1000 ft/min
Descent (to FL100)
IAS
250 kts
ROD
2300 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
180 kts
ROD
n/a
Approach
Vapp (IAS)
132 kts
Distance
1320 m
