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Martin 2-0-2

Twin-piston-engine US piston airliner, 1946 From Wikipedia, the free encyclopedia

Martin 2-0-2
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The Martin 2-0-2 was an airliner introduced in 1947. The twin piston-engined fixed-wing aircraft was designed and built by the Glenn L. Martin Company.

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Design and development

Glenn L. Martin, president of the company, intended that the Model 2-0-2 would be a replacement for the Douglas DC-3. It was also known as the "Martin Executive".

The first flight of the model was in November 1946. Full civilian certification was gained in August 1947, several months before competing aircraft types. The total production of 2-0-2s and 2-0-2As was 47 aircraft.[1]

The aircraft was not pressurized, but was considered a long-range airliner. The fatal crash in 1948 of Northwest Airlines Flight 421 revealed a serious structural problem in the wings. Structural metal fatigue was the problem in a major wing spar. Alloy 7075-T6 was used, which is susceptible to stress-corrosion cracking and low toughness. The airliner was grounded and modifications were made. The wing components were redesigned and the engines replaced. The changed type was designated the Martin 2-0-2A.

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Operational history

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Japan Airlines Martin 2-0-2 "Mokusei" (1951)
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Former TWA Martin 2-0-2A of Southeast Airlines (Florida) at Miami in 1970

On November 13, 1945 Pennsylvania Central Airlines purchased a fleet of 35 Martin 2-0-2s from the Glenn Martin Company for $7,000,000.[2] Two weeks later, Colonial Airlines announced that they would purchase 20 airplanes for $4,000,000, scheduled for delivery in 1947.[3] Early in the next year, Martin announced that Pennsylvania Central Airlines had ordered 15 more 2-0-2s, bringing the total aircraft on order in early January 1947 to 137 aircraft, with a sales value of $27,000,000.[4] Despite the announcement of these large orders, the contract terms allowed the airlines to cancel them without any penalty.[5] The 2-0-2 was unpressurised, unlike the competing Convair 240. Therefore, as delays in production built up, all airlines except Northwest, TWA, LAN, and LAV cancelled their orders and only 31 2-0-2s and 12 2-0-2As were actually delivered to the airlines.[5] The first scheduled flight was on Northwest between Minneapolis and Chicago on 13 October 1947.

The 2-0-2 was the first airplane subjected to the U.S. Civil Aeronautics Administration's then-new "Accelerated Service Test," introduced May 15, 1947. In this test, an airliner was to undergo a rigorous 150-hour test, attempting to squeeze one year's service into a week to 10 days of flying. The 2-0-2 made such a test visiting about 50 cities in seven days. At each city, comprehensive inspections were made of the aircraft systems to assess how wear or malfunction would occur.[6]

TWA and Northwest, initial customers of the 2-0-2, eventually sold theirs to California Central and Pioneer Airlines. Later, Allegheny Airlines acquired many of the 2-0-2s as part of the company's expansion plans, beginning June 1, 1955. Eventually, they acquired a total of 18 aircraft.

Only one of this type of aircraft is known to survive,[citation needed] at the Aviation Hall of Fame and Museum of New Jersey.

This airliner was eventually developed into the Martin 4-0-4, which was more successful.

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Variants

The Martin Company designated the following quantities for the airlines (though not all were built), listed by Martin Model number:[citation needed]

2-0-2
twin engine prototype: 3, in 1946
2-0-2FL
twin engine commercial transport, Chile: 4, in 1947
2-0-2NW
twin engine commercial transport, Northwest Airlines: 25, in 1947
2-0-2LAV
twin engine commercial transport, Venezuela: 2, in 1947
2-0-2A
twin engine commercial transport, Trans World Airlines: 21, in 1947
2-0-2E
twin engine commercial transport, Eastern Airlines: 25, in 1947

Operators

♠ original operators

 Chile
 Colombia
  • Aeroproveedora
 Japan
 Mexico
  • Servicios Aéreos Baja
 Panama
  • RAPSA Panama
 United States
 Venezuela
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Accidents and incidents

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The Martin 2-0-2 had 13 hull-loss accidents and incidents, of which nine were fatal accidents.[11]

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Specifications (Martin 2-0-2)

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3-view silhouette drawing of the Martin 2-0-2NW

Data from Jane's All The World's Aircraft 1951–52[23]

General characteristics

  • Crew: 2
  • Capacity:
    • 40 passengers or
    • 9,270 lb (4,200 kg) payload
  • Length: 71 ft 4 in (21.74 m)
  • Wingspan: 93 ft 3 in (28.42 m)
  • Height: 28 ft 5 in (8.66 m)
  • Wing area: 864 sq ft (80.3 m2)
  • Empty weight: 25,086 lb (11,379 kg)
  • Max takeoff weight: 39,900 lb (18,098 kg)
  • Powerplant: 2 × Pratt & Whitney R-2800 CA-18 Double Wasp 18-cylinder air-cooled radial engine, 1,800 hp (1,300 kW) each (Normal power), 2,400 hp (1,800 kW) (take-off with water injection)
  • Propellers: 3-bladed Hamilton Standard 2H17K3-48R, 13 ft 1 in (3.99 m) diameter

Performance

  • Maximum speed: 311 mph (501 km/h, 270 kn) at 14,000 ft (4,300 m)
  • Cruise speed: 293 mph (472 km/h, 255 kn) at 12,000 ft (3,700 m)
  • Stall speed: 76 mph (122 km/h, 66 kn)
  • Range: 635 mi (1,022 km, 552 nmi) 36 passengers, baggage and 1,000 lb (450 kg) cargo, reserves for 200 mi (170 nmi; 320 km) plus 45 minutes
  • Service ceiling: 33,000 ft (10,000 m)
  • Rate of climb: 2,200 ft/min (11 m/s)
  • Take-off run to 50 ft (15 m): 1,565 ft (477 m)
  • Landing run from 50 ft (15 m): 1,720 ft (520 m)
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See also

Related development

Aircraft of comparable role, configuration, and era

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Notes

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References

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