McDonnell Douglas C-9

· Douglas Aircraft Corporation
Airplanes
Length
36.2712 m
Flat Wing Span
28.3464 m
Height
8.2296 m
Flat Wing Area
92.9959 m²
Max Seating
76
Cruise Speed
898.2192 km/h
Max Speed
925.9992 km/h
Max Mach
0.84 Mach
Max Ceiling
11277.6 m
Number of Engines
2
Entry Into service
1968-01-01
Number Built
48
Maximum Take-Off Weight
49.8952 t (paragliders: kg)
Maximum Range
4667.04 km

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
McDonnell Douglas C-9 49.8952 4667.04

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Boeing 717 Rolls-Royce BR700 37.7952 28.3464 106 Compare
Tupolev Tu-134 37.1 29.01 84 Compare
Embraer Lineage 1000 36.24 28.72 13 Compare
Fokker 100 35.53 28.08 97 Compare
Beriev Be-10 31.45 28.6 Compare
Mitsubishi SpaceJet Pratt & Whitney PW1000G 35.8 29.2 Compare
All data (26 fields)
Name
McDonnell Douglas C-9
Manufacturer
Douglas Aircraft Corporation
Description
The McDonnell Douglas C-9 is a retired military version of the McDonnell Douglas DC-9 airliner.
Entry Into service
1968-01-01
Service End
2005-09-01
Designer
Douglas Aircraft Corporation
Type
Military transport aircraft
Length (m)
36.2712
Height (m)
8.2296
Cockpit Crew
5
Max Seating
76
Max Speed (km/h)
925.9992
Cruise Speed (km/h)
898.2192
Max Ceiling (m)
11277.6
Rate of Climb (m/s)
15.24
Capacity Description
up to 76 pax
Max Mach (Mach)
0.84
National Origin
United States of America
Number Built
48
Powerplant Description
2 × Pratt & Whitney JT8D-9 turbofan engines
Primary Users
United States Air Force (historical), United States Navy (historical) , United States Marine Corps (historical) , Kuwait Air Force (historical)
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/McDonnell_Douglas_C-9
Flat Wing Span (m)
28.3464
Flat Wing Area (m²)
92.9959
Number of Engines
2