McDonnell Douglas DC-9-20

ICAO aircraft code DC92
Manufacturer McDonnell Douglas
Country United States

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McDonnell Douglas DC-9-20 specifications

General

ICAO aircraft code
DC92
Manufacturer
McDonnell Douglas
Manufactured
1965 - 1982
Country
United States

Aircraft performance

Engine:
2x JT8D-11
Turbofan
Power:
15,000 pound-force
Max Cruise Speed:
485 Kts
898 Km/h
Approach Speed (Vref):
127 Kts
Travel range:
1,500 Nm
2,778 Kilometers
Service Ceiling:
35,000 feet
Rate of Climb:
2500 feet / minute
12.70meter / second
Take Off Distance:
1600 meter - 5,249.28 feet
Landing Distance:
1500 meter - 4,921.20 feet

Weight & dimensions

Max Take Off Weight:
45,359 Kg
99,998 lbs
Max Landing Weight:
43,227 Kg
95,298 lbs
Max Payload:
11,501 Kg
25,355 lbs
Fuel Tank Capacity:
3,679 gallon
13,926 liter
Baggage Volume:
17 m3 / 600 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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