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Attempting to gain a share of the post-World War II demand for civil airliners, the Glenn L. Martin Company flew on 22 November 1946 the prototype of a twin-engine 36/40-seat transport designated Martin 2-0-2. The first of these entered service in October 1947, but the loss of a 2-0-2 in 1948 as a result of wing structural failure led to modification of other in-service aircraft and production of this version was brought to an end. The prototype of an improved Martin 3-0-3 had been flown on 20 June 1947, but with a need to redesign the wing structure it was decided instead to develop a new Martin 4-0-4. This incorporated the wing structural revisions and introduced a pressurised and slightly lengthened fuselage, accommodating as standard a crew of three or four and 40 passengers. When production ended in early 1953 a total of 103 had been built, this number including two supplied to the Coast Guard as staff transports under the designation RM-1G (later RM-1Z and finally VC-3A); they were subsequently transferred to the US Navy.
 | A three-view drawing (672 x 940) |
| MODEL | Martin 2-0-2 |
| ENGINE | 2 x 2400hp Pratt Whitney R-2800 CB-16 |
| WEIGHTS |
| Take-off weight | 19504 kg | 42999 lb |
| Empty weight | 10659 kg | 23499 lb |
| DIMENSIONS |
| Wingspan | 28.42 m | 93 ft 3 in |
| Length | 21.74 m | 71 ft 4 in |
| Height | 8.66 m | 28 ft 5 in |
| Wing area | 80.27 m2 | 864.02 sq ft |
| PERFORMANCE |
| Cruise speed | 499 km/h | 310 mph |
| Ceiling | 6705 m | 22000 ft |
| Range | 3220 km | 2001 miles |
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