Military Wiki
B-10 being flown during a training session at Maxwell Field
Role Bomber aircraft
Manufacturer Glenn L. Martin Company
Designer Peyton M. Magruder
First flight 16 February 1932
Introduction November 1934
Retired 1949 Royal Thai Air Force
Primary users United States Army Air Corps
Netherlands East Indies AF
Turkish Air Force
Chinese Nationalist Air Force[1]
Argentinian Air Force
Produced 1933-1940
Number built 121 B-10
82 model 166
32 B-12
348 of all variants including 182 export versions
Unit cost
Variants Martin Model 146

The Martin B-10 was the first all-metal monoplane bomber to go into regular use by the United States Army Air Corps, entering service in June 1934.[3] It was also the first mass-produced bomber whose performance was superior to that of the Army's pursuit aircraft of the time.[4]

The B-10 served as the airframe for the B-12, B-13, B-14, A-15 and O-45 designations using Pratt & Whitney engines instead of Wright Cyclones. A total of 348 of all versions were built. Biggest users were the USA, with 166, and the Netherlands, with 121.

Design and development

Martin B-10 during exercises over Oahu, Hawaii, 1941

Martin B-10B airplane

The B-10 began a revolution in bomber design. Its all-metal monoplane build, along with its features of closed cockpits, rotating gun turrets, retractable landing gear, internal bomb bay, and full engine cowlings, would become the standard for bomber designs worldwide for decades.[4] It made all existing bombers completely obsolete. In 1932, Martin received the Collier Trophy for designing the XB-10.

The B-10 began as the Martin Model 123, a private venture by the Glenn L. Martin Company of Baltimore, Maryland. It had a crew of four: pilot, copilot, nose gunner and fuselage gunner. As in previous bombers, the four crew compartments were open, but it had a number of design innovations as well.[5][6]

These innovations included a deep belly for an internal bomb bay and retractable main landing gear. Its 600 hp (447 kW) Wright SR-1820-E Cyclone engines provided sufficient power. The Model 123 first flew on 16 February 1932 and was delivered for testing to the U.S. Army on 20 March as the XB-907. After testing it was sent back to Martin for redesigning and was rebuilt as the XB-10.[5][6]

The XB-10 delivered to the Army had major differences from the original aircraft. Where the Model 123 had NACA cowling rings, the XB-10 had full engine cowlings to decrease drag.[2] It also sported a pair of 675 hp (503 kW) Wright R-1820-19 engines, and an 8 feet (2.4 m) increase in the wingspan, along with an enclosed nose turret. When the XB-10 flew during trials in June, it recorded a speed of 197 mph (317 km/h) at 6,000 ft (1,830 m). This was an impressive performance for 1932.[4]

Following the success of the XB-10, a number of changes were made, including reduction to a three-man crew, addition of canopies for all crew positions, and an upgrade to 675 hp (503 kW) engines. The Army ordered 48 of these on 17 January 1933. The first 14 aircraft were designated YB-10 and delivered to Wright Field, starting in November 1933. The production model of the XB-10, the YB-10 was very similar to its prototype.

Operational history

Martin B-10B during exercises

Martin B-12 at March Field, California, 19 November 1935

In 1935, the Army ordered an additional 103 aircraft designated B-10B. These had only minor changes from the YB-10. Shipments began in 1935 July. B-10Bs served with the 2d Bomb Group at Langley Field, the 9th Bomb Group at Mitchel Field, the 19th Bomb Group at March Field, the 6th Composite Group in the Panama Canal Zone, and the 4th Composite Group in the Philippines. In addition to conventional duties in the bomber role, some modified YB-10s and B-12As were operated for a time on large twin floats for coastal patrol.[7][8]

The Martin Model 139 was the export version of the Martin B-10. With an advanced performance, the Martin company fully expected that export orders for the B-10 would come flooding in.

The Army owned the rights to the Model 139 design. Once the Army's orders had been filled in 1936, Martin received permission to export Model 139s, and delivered versions to several air forces. For example, six Model 139Ws were sold to Siam in April 1937, powered by Wright R-1820-G3 Cyclone engines; 20 Model 139Ws were sold to Turkey in September 1937, powered by R-1820-G2 engines.

On 19 May 1938, during the Sino-Japanese War, two Chinese Nationalist Air Force B-10s successfully flew to Japan. However, rather than dropping bombs, the aircraft dropped propaganda leaflets.[9]

The Dutch Martins fought round the clock in the defence of Singapore and the Netherlands East Indies. The model 166 had superior performance compared to the Japanese medium bombers in the theatre.


At the time of its creation, the B-10B was so advanced that General Henry H. Arnold described it as the air power wonder of its day. It was half again as fast as any biplane bomber, and faster than any contemporary fighter. The B-10 began a revolution in bomber design; it made all existing bombers completely obsolete.[2]

Rapid advances in bomber design in the late 1930s meant that the B-10 was eclipsed by the time the United States entered World War II. The 139s in combat in China and South East Asia suffered the same disadvantages as the other early war medium bombers, i.e. not enough armour and guns, while it couldn't outrun the latest fighters. Nevertheless, the 166 had the highest performance of all the medium bombers in the theatre at the time, early 1942.

An abortive effort to modernize the design, the Martin Model 146, was entered into a USAAC long-distance bomber design competition 1934–1935, but lost out to the Douglas B-18 and much bigger Boeing B-17. It's interesting to note that the B-18 wasn't that much better than the B-10 and actually inferior to the latest B-10 version, the model 166.


Martin XB-907

Martin YB-10

Martin B-12

Martin B-12A

Martin XB-14

Martin Model 123

Private venture of Martin company, predecessor of the XB-10, served as prototype for the series, 1 built.[10]

US Army designation for the Model 123 in evaluation,[10] with open cockpits and two Wright SR-120-E, delivered Apr '32.
Modified XB-907 after Martin returned it to U.S. Army for further operational trials,[2] with larger wingspan and two Wright R-1820-19.
Designation of the prototype when purchased by the United States Army Air Corps, Modified XB-907A with enclosed cockpits and turret and single strut landing gear.[4][11]

Martin Model 139, 139A and 139B

Army Air Corps versions, 165 built.

Model 139A, test and production version of the XB-10 with crew reduced to three members, and two 675 hp/503 kW R-1820-25, 14 built, some flown temporarily as float planes.[7]
The YB-10A was different from a YB-10 only in its engines. It used Wright R-1820-31 turbo-supercharged radials, allowing it to attain speeds of 236 mph (380 km/h). This made it the fastest aircraft of the B-10 series. Despite this advantage, only one was built, as a test aircraft.[7]
According to one source, two additional aircraft ordered in 1936.[7]
Model 139, main production version with two 775 hp (578 kW) R-1820-33 engines, 105 built, delivered Aug '36.[7]
According to one source this was, these were B-10Bs converted as target tugs.[7] According to Martin's own archive, this was the designation of the YB-10 after testing, then used for airmail and Alaska missions, 13 of the 14 built were still in service in Apr '40.
One former NEIAF Model 139WH-3A model impressed in July 1942 and flown from Australia to the United States.[7]
Model 139B. With 250 or 500 gallons flotation chambers for safety on overwater flights, and two Pratt & Whitney R-1690-11 "Hornet" radial engines. These 775 hp (578 kW) engines gave similar performance to those on the B-10B (218 mph/351 km/h), seven built, 5 still in service in Apr '40.[7]
The production version of the YB-12 with provision for a 365 gal (1,381 l) fuel tank in the bomb bay, giving the B-12A a combat range of 1,240 mi (1,995 km), 25 built, 23 still in service in Apr '40.[7]
Re-engined version of the YB-10 powered by two 700 hp (522 kW) Pratt & Whitney R-1860-17 radial engines. Ten were on order but cancelled before production started, not built.[7]
To test the new 900 hp Pratt & Whitney YR-1830-9 "Twin Wasp" radial engines, one built which was converted back to YB-12 after testing.[7]
Proposed attack variant of the YB-10 with two 750 hp (559 kW) R-1820-25 engines, was never built. The contract fell to the A-14 Shrike.[12]
With two 750 hp Wright R-1820-17, proposed high-speed observation role, one built.

Model 139W

The export versions, 100 built (182 including the 166, see below).

Model 139WA
Martin demonstrator for Argentina
Model 139WAA
Export version for Argentine Army, 26 built, delivered Apr '38.
Model 139WAN
Export version for the Argentine Navy, 12 built, delivered Nov '37.
Model 139WC and WC-2
Export version for China, 6 and 3 built, delivered in Feb and Aug '37.[3][13]
Model 139WH
Export version for the Netherlands, used in the Netherlands East Indies. Produced in block series WH(-1) (13 built, delivered Feb '37) and WH-2 (26 built, delivered March '38).
Model 139WR
Single demonstrator to the Soviet Union.[7][13]
Model 139WSM and WSM-2
Export version for Siam, 3 and 3 built, delivered in Mar and Apr '37.[7]
Model 139WSP
Proposed licence built version to be built by CASA of Spain, production blocked by U.S. State Department.
Model 139WT
Export version for Turkey, 20 built, delivered Sep '37.[3]

Model 166

Final version, a.k.a. 139WH-3 and 139WH-3A, 82 built.

Export version for the Netherlands, used in the Netherlands East Indies. Redesigned wings, nose and single 'glass house' canopy, bomb shackles between engines and fuselage, and better engines. The WH-3 had two 900 hp (671 kW) R-1820-G5 (40 built, delivered Sep '38), the WH-3A had two 1,000 hp (671 kW) R-1820-G-105A (42 built, delivered Mar '40). With the bomb shackles the bomb load could be doubled for a shorter range. A total of 121 of all types were built for the Dutch.[7]


Side view of Dutch Martin Model 166

 Republic of China (1912–1949)
 The Netherlands
Thailand Siam
 Soviet Union
 United States


B-10 on display at the National Museum of the United States Air Force

  • The only surviving complete B-10 is on display at the National Museum of the United States Air Force at Wright-Patterson Air Force Base near Dayton, Ohio. The aircraft is painted as a B-10 used in the 1934 Alaskan Flight. It was an export version sold to Argentina in 1938. The aircraft survived as a ground crew trainer, and was still being used by the Argentine Air Force for training its ground crews as late as the 1960s. The Air Force Museum conducted an exhaustive search for any surviving B-10 remains, and eventually learned of the aircraft. In 1970, the incomplete airframe was donated by the Government of Argentina to the U.S. Government in a formal ceremony attended by the U.S. ambassador. The aircraft was restored by the 96th Maintenance Squadron (Mobile), Air Force Reserve, at Kelly Air Force Base, Texas, in 1973–1976, and placed on display in 1976.[18]
  • Various parts of crashed B-10s, such as turrets and wings, were retrieved from the jungle of Borneo and are now on display in the Militaire Luchtvaart Museum (Military Aviation Museum) at Soesterberg, the Netherlands.[19]

Specifications B-10B & model 166

Data from United States Military Aircraft Since 1909[20]

General characteristics

  • Crew: 4: pilot, co-pilot/radio operator, bombardier/gunner, gunner
  • Length: 44 ft 9 in & same (13.6 m)
  • Wingspan: 70 ft 6 in & same (21.5 m)
  • Height: 15 ft 5 in & 11 ft 5 in (4.7 m & 3.5 m)
  • Wing area: 678 ft² & 683 ft² (63 m² & 64 m²)
  • Empty weight: 9,681 lb & 10,322 lb (4.391 kg & 4,682 kg)
  • Loaded weight: 14,700 lb & 15,624 lb (6,680 kg & 7,085 kg)
  • Max. takeoff weight: 16,400 lb (7,440 kg)
  • Powerplant: 2 × Wright R-1820-33 (G-102) "Cyclone" radials, 775 hp & 1,000 hp (578 kW & 746 kW) each


  • Maximum speed: 213 mph & 241 mph (185 kn, 343 km/h & 210 kn, 388 km/h)
  • Cruise speed: 193 mph & 186 mph (168 kn, 311 km/h & 161 kn, 299 km/h)
  • Range: 1,240 mi & 1,740 mi (1,078 nmi, 1,996 km & 1,510 nmi, 2,800 km)
  • Service ceiling: 24,200 ft & 28,215 ft (7,380 m & 8,600 m)
  • Rate of climb: 1,380 ft/min & 1,939 ft/min (420 m/min & 591 m/min)
  • Wing loading: 21.7 lb/ft² & 22.9 lb/ft² (106 kg/m² & 111 kg/m²)
  • Power/mass: 0.105 hp/lb & 0.128 hp/lb (0.173 W/kg & 0.211 W/kg)


  • Guns: 3 × .30 in (7.62 mm) Browning machine guns in nose, dorsal and belly positions
  • Bombs: 2,260 lb & 4,520 lb (1,030 kg & 2,060 kg)

See also



  1. Broshot, James A. "Dutch Air Force Order of Battle in the Dutch East Indies, 30 November 1941." Forgotten Campaign: The Dutch East Indies Campaign 1941-1942. Retrieved: 17 July 2011.
  2. 2.0 2.1 2.2 2.3 Fitzsimons 1969, p. 1846.
  3. 3.0 3.1 3.2 Jackson 2003, p. 246.
  4. 4.0 4.1 4.2 4.3 Eden and Moeng 2002, p. 931.
  5. 5.0 5.1 "Flying Fish–Our Army's Newest Plane Hits Terrific Speeds (photo of Model 123, US Army designation XB-907, in flight)." Popular Science, October 1932. Retrieved: 22 December 2010.
  6. 6.0 6.1 "M-list." Aerofiles. Retrieved: 22 December 2010.
  7. 7.00 7.01 7.02 7.03 7.04 7.05 7.06 7.07 7.08 7.09 7.10 7.11 7.12 7.13 Eden and Moeng 2002, p. 932.
  8. Swanborough and Bowers 1964, p. 331.
  9. Dunn, Richard L. "Illusive <sic> Target: Bombing Japan from China.", 2006. Retrieved: 16 May 2013.
  10. 10.0 10.1 Fitzsimons 1967/1969, p. 1845.
  11. "Photo of XB-10." Retrieved: 17 July 2011.
  12. Swanborough and Bowers 1964, p. 332.
  13. 13.0 13.1 Baugher, Joe. "Martin B-10". American Military Aircraft, 11 July 1999. Retrieved: 13 June 2010.
  14. "Donation of the Martin B-10." National Museum of the United States Air Force. Retrieved: 13 June 2010.
  15. Photos as well as paintings of ROC
  16. Young 1984, p. 23.
  17. Casius 1983, p. 20.
  18. "USAF Fact Sheet Martin B-10." National Museum of the United States Air Force. Retrieved: 13 June 2010.
  19. "Martin B-10" (in Dutch). Netherlands Military Aviation Museum. Retrieved: 22 December 2010.
  20. Swanborough and Bowers, 1964, p. 333.


  • Bridgwater, H.C. and Peter Scott. Combat Colours Number 4: Pearl Harbor and Beyond, December 1941 to May 1942. Luton, Bedfordshire, UK: Guideline Publications, 2001. ISBN 0-9539040-6-7.
  • Casius, Gerald. "Batavia's Big Sticks." Air Enthusiast, Issue Twenty-two, August–November 1983, pp. 1–20. Bromley, Kent, UK: Pilot Press Ltd, 1983. ISSN 0413-5450.
  • Eden, Paul and Soph Moeng, eds. The Complete Encyclopedia of World Aircraft. London: Amber Books Ltd., 2002. ISBN 0-7607-3432-1.
  • Fitzsimons, Bernard, ed. The Illustrated Encyclopedia of the 20th Century Weapons and Warfare. New York: Purnell & Sons Ltd., 1969, First edition 1967. ISBN 0-8393-6175-0.
  • Jackson, Robert. The Encyclopedia of Military Aircraft. London: Parragon Publishing, 2003. ISBN 1-4054-2465-6.
  • Glenn L. Martin Aviation Museum. Martin Aircraft Specifications.
  • Núñez Padin, Jorge. Martin 139W en Argentina(in Spanish). Buenos Aires, Argentina: Monografías Aeronaves en Argentina, 2007. ISBN n/a.
  • Swanborough, F. Gordon and Peter M. Bowers. United States Military Aircraft Since 1909. New York: Putnam, 1964. ISBN 0-85177-816-X.
  • Taylor, John W. R. "Martin B-10". Combat Aircraft of the World from 1909 to the Present. New York: G.P. Putnam's Sons, 1969. ISBN 0-425-03633-2.
  • Young, Edward M. "France's Forgotten Air War". Air Enthusiast Issue Twenty Five, August–November 1984, pp. 22–33. Bromley, Kent: Pilot Press. ISSN 0413-5450.

External links

This page uses Creative Commons Licensed content from Wikipedia (view authors).