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
Manufacturered as
DOUGLAS DC-9-10
MCDONNELL 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: 
27.25 m
Length: 
31.82 m
Height: 
8.38 m
Powerplant: 

2 x Pratt & Whitney JT8D-5 or -7 (62.3 kN) thrust each.

Engine Model: 
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

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