McDonnell Douglas DC-9-10

ICAO aircraft code DC91
Manufacturer Douglas Aircraft Co.
Country United States

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McDonnell Douglas DC-9-10 Specifications

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General

ICAO aircraft code
DC91
Manufacturer
Douglas Aircraft Co.
Manufactured
1965 - 1969
Country
United States

Aircraft performance

Engine:
2x Pratt & Whitney JT8D-7
Turbofan
Power:
14,000 pound-force
Max Cruise Speed:
484 Kts
896 Km/h
Approach Speed (Vref):
132 Kts
Travel range:
1,450 Nm
2,685 Kilometers
Service Ceiling:
35,000 feet
Rate of Climb:
2800 feet / minute
14.22meter / second
Take Off Distance:
1615 meter - 5,298.49 feet
Landing Distance:
1320 meter - 4,330.66 feet

Weight & dimensions

Max Take Off Weight:
41,100 Kg
90,609 lbs
Max Landing Weight:
37,100 Kg
81,791 lbs
Max Payload:
18,000 Kg
39,683 lbs
Fuel Tank Capacity:
3,693 gallon
13,979 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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