McDonnell Douglas DC-9-50

ICAO aircraft code DC95
Manufacturer McDonnell Douglas
Country United States
New price USD 5.2 million (1972)

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McDonnell Douglas DC-9-50 Specifications

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General

ICAO aircraft code
DC95
Manufacturer
McDonnell Douglas
Manufactured
1965 - 1982
Country
United States
New purchase price
USD 5.2 million (1972)

Aircraft performance

Engine:
2x Pratt & Whitney JT8D-15A
Turbofan
Power:
16,000 pound-force
Max Cruise Speed:
485 Kts
898 Km/h
Approach Speed (Vref):
130 Kts
Travel range:
1,300 Nm
2,408 Kilometers
Service Ceiling:
35,000 feet
Rate of Climb:
2000 feet / minute
10.16meter / second
Take Off Distance:
2100 meter - 6,889.68 feet
Landing Distance:
1500 meter - 4,921.20 feet

Weight & dimensions

Max Take Off Weight:
54,885 Kg
120,999 lbs
Max Landing Weight:
49,895 Kg
109,999 lbs
Max Payload:
15,265 Kg
33,653 lbs
Fuel Tank Capacity:
2,957 gallon
11,193 liter
Baggage Volume:
33.2 m3 / 1,172 ft3

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

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