Martin 4-0-4

ICAO aircraft code M404
Country United States

The Martin 4-0-4 was an American pressurized passenger airliner built by the Glenn L.

Specifications

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Martin 4-0-4 Specifications

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General

ICAO aircraft code
M404
Manufacturer
Glenn L. Martin Company
Manufactured
1951 - 1953
Country
United States

Aircraft performance

Engine:
2x Pratt & Whitney R-2800-CB16
Piston
Power:
2,400 HP
Max Cruise Speed:
271 Kts
502 Km/h
Approach Speed (Vref):
70 Kts
Travel range:
2,300 Nm
4,260 Kilometers
Service Ceiling:
29,000 feet
Rate of Climb:
1905 feet / minute
9.68meter / second
Take Off Distance:
600 meter - 1,968.48 feet
Landing Distance:
530 meter - 1,738.82 feet

Weight & dimensions

Max Take Off Weight:
20,366 Kg
44,899 lbs
Max Landing Weight:
18,231 Kg
40,192 lbs
Max Payload:
4,050 Kg
8,929 lbs
Fuel Tank Capacity:
2,000 gallon
7,571 liter

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.

About the Martin 4-0-4

The Martin 4-0-4 was an American pressurized passenger airliner built by the Glenn L. Martin Company. In addition to airline use initially in the United States, it was used by the United States Coast Guard and United States Navy as the RM-1G (later as the VC-3A).

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