Huff-Daland LB-1

From Wikipedia, the free encyclopedia

Huff-Daland LB-1
Type Single engine biplane bomber
Manufacturer Huff-Daland
Maiden flight 1923
Introduced 1923
Primary user United States Army Air Service
Number built 10

The Huff-Daland LB-1 was an American biplane light bomber aircraft operated by the United States Army Air Service in the 1920s.

Derived from the XLB-1 prototype bought by the Army in 1923, the LB-1 development aircraft was powered by a single Packard 2A-2540 engine and carried an extra crewman. It proved underpowered in service trials, and was replaced by the twin-engined XLB-3.

Contents

[edit] Specifications

General characteristics

  • Crew: Four
  • Length: 46 ft 2 in (14.07 m)
  • Wingspan: 60 ft 6 in (20.27 m)
  • Gross weight: 12,415 lb (5,631 kg)
  • Powerplant: 1 × Packard 2A-2540 water-cooled vee engine, 800 hp (600 kW)

Performance

  • Maximum speed: 120 mph (190 km/h)
  • Range: 430 miles (700 km)
  • Service ceiling: 11,150 ft (3,400 m)

Armament

  • 5 × .30 machine guns
  • 2,750 lb (1,250 kg) of bombs


Related lists

[edit] References

[edit] Notes

[edit] Bibliography

United States Air Force stub This United States Air Force article is a stub. You can help Wikipedia by expanding it.
This United States Army article is a stub. You can help Wikipedia by expanding it.
United States military stub This United States military article is a stub. You can help Wikipedia by expanding it.