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**Data for each of these
characteristics can be
obtained by contacting
the EICO
Aviation Specialist
at the NAVFAC Criteria
Office.
|
The C-9B Skytrain is used for
fleet logistic support, intra-theater airlift and airlifting Naval Reservists to and from
training sites. The C-9B is the military version of the McDonnell Douglas DC-9 used for
many years on commercial airline routes. |
|
|
|
|
Aircraft Type |
Fixed Wing Transport |
|
Aircraft Manufacturer
|
McDonnell
Douglas
|
|
Engine Manufacturer |
Pratt &
Whitney
|
|
Engine Number |
JT8D-9A |
|
Type of Landing Gear |
Dual Tricycle |
|
Design Gear Load |
51,300 lbs |
|
Design Tire Pressure |
152 psi |
|
Pass/Cov Ratio Channelized |
3.85 |
|
Pass/Cov Ratio Unchannelized |
7.18 |
|
|
Wingspan |
93.30 ft |
Length (Overall) |
119.30 ft |
Height (Overall) |
27.50 ft |
Wheelbase |
53.20 ft |
Nose to centerline of main gear |
60.80 ft |
Wheel track (tread) |
16.40 ft |
Vertical clearance of wingtip at
maximum weight |
7.30 ft |
Height of jet engine on
centerline of fuselage |
** |
|
|
Minimum turning radius |
64.1 ft |
Engine operating danger areas -
idle |
100°F, 35
mph @ 100 ft Aft |
Ground clearance |
** |
Electrical Service |
Maximum kVa by aircraft
for 400Hz distribution |
** |
Mechanical Service |
Air starting system |
** |
Preconditioned air |
** |
Environmental control air |
** |
|
|
Min takeoff weight |
104.10 klbs |
Min takeoff distance at min
takeoff weight |
4,000 ft |
Min takeoff distance at min
takeoff weight with abort distance |
5,300 ft |
Max takeoff weight at peace-time |
110.00 klbs |
Max takeoff weight at war-time |
110.00 klbs |
Min takeoff distance at max
takeoff weight |
4,500 ft |
Min landing weight |
96.03 klbs |
Max landing weight |
99.00 klbs |
Min landing distance at min
landing weight |
2,450 ft |
Min landing distance at max
landing weight |
2,500 ft |
Peace-time weight used for
pavement evaluation |
** |
|