Stearman M-2 Speedmail
|Last surviving Stearman M-2 aircraft|
|Manufacturer||Stearman Aircraft Company|
|First flight||15 January 1929|
The Stearman M-2 Speedmail (nicknamed the Bull Stearman) was a mail-carrier aircraft produced by the Stearman Aircraft Company of Wichita, Kansas. It first flew in January 1929. The Speedmail was a single seat biplane, with two large cargo compartments in place of a front cockpit. The fuselage and tail unit were constructed from welded chrome-moly steel tube faired with wooden formers and fabric covered aft of the pilots cockpit, detachable aluminium alloy panels covered the fuselage forward of the pilots cockpit. The wings were constructed from spruce spars and plywood built-up ribs, all fabric covered. It differed from previous Stearman aircraft by having a tailwheel instead of a tailskid due to its size and weight.
Design and development
Lloyd Stearman and Mac Short, (Stearman's V.P. engineering), designed the Speedmail to the requirements of Varney Air Lines, which needed a new mail carrier with greater capacity to fly the Air Mail contracts they acquired from the U.S. Postal service while still being able to land on short, unimproved airstrips. This was achieved by using a new type of airfoil section allowing high lift at low speeds without affect the cruising speed. The result was a sturdy aircraft with a large cargo capacity.
To enable Interstate Air Lines to fly passengers on its Air Mail routes from Atlanta, Stearman enlarged the M-2, into the LT-1(Light Transport), adding a four-seat enclosed cabin in place of the forward cargo compartments, the payload capacity allowed for four passenger plus luggage and 500 pounds of cargo or mail.
A further development was the CAB-1 "Coach" which was designed with an enclosed cabin for use as a business aircraft. Unlike the LT-1, the pilot was inside the enclosed cabin and in front of the passengers. However only one was built which was later dismantled when sales failed to materialize.
Stearman then developed a scaled down version of the M-2, the Stearman 4 which was successful.
Varney Air Lines' pilots found the M-2 difficult to handle and the Wright Cyclone engine was plagued with frequent maintenance issues.
- M-2 Speedmail
- Single-engine mail transport aircraft, powered by a 525 hp (391-kW) Wright Cyclone radial engine, able to carry up to 1,000 lb (454 kg) of mail.
- Slightly larger 5-seat passenger and mail carrier, powered by a Pratt & Whitney Hornet radial piston engine.
- CAB-1 Coach
- Similar to the M-2 with enclosed cockpit filling gap between the fuselage and wing and powered with a 300 hp Wright J-6-7.
Specifications (M-2 Speedmail)
Data from Specifications of American Commercial Airplanes
- Crew: 1
- Capacity: 1,000 lb (450 kg) payload
- Length: 30 ft 2 in (9.19 m)
- Wingspan: 46 ft 0 in (14.02 m)
- Height: 11 ft 1 in (3.38 m)
- Wing area: 436 sq ft (40.5 m2)
- Empty weight: 3,442 lb (1,561 kg)
- Gross weight: 5,578 lb (2,530 kg)
- Fuel capacity: 136 US gal (113 imp gal; 510 L)
- Powerplant: 1 × Wright Cyclone nine-cylinder radial engine, 525 hp (391 kW)
- Maximum speed: 147 mph (237 km/h; 128 kn)
- Cruise speed: 126 mph (203 km/h; 109 kn)
- Range: 860 mi (747 nmi; 1,384 km)
- Service ceiling: 15,000 ft (4,600 m)
- Rate of climb: 950 ft/min (4.8 m/s)
- Related development
- Aircraft of comparable role, configuration and era
|Wikimedia Commons has media related to Stearman M-2 Speedmail.|
- Aviation March 22, 1930, pp. 607, 609, 611.
- Juptner, Joseph P. (1964). U.S. Civil Aircraft Vol.2. Los Angeles: Aero Publishers. pp. 78 to 80.
- Lopez, Alan (2012). Bull Stearman: The Story of the Stearman M-2 Speedmail. Princeton: Mountain Press
- "Specifications of American Commercial Airplanes". Aviation. Vol. 28 no. 12. March 22, 1930. pp. 606–611. (Registration required (. ))
- "Stearman, Boeing-Stearman, Stearman-Hammond, Stearman-Northrop". Aerofiles. Retrieved 2008-10-29.