Hall XP2H

XP2H-2
Role	Patrol flying boat
National origin	United States of America
Manufacturer	Hall-Aluminum Aircraft Corporation
First flight	November 15, 1932
Primary user	United States Navy
Number built	1

The Hall XP2H-1 was an American prototype four-engined biplane flying boat of the 1930s. Intended as an experimental very long range maritime patrol aircraft, a single example was built. The XP2H-1 was the largest four engine biplane aircraft ever procured by the US Navy. ^[1]

Development and design

In 1930, the United States Navy ordered a single example of a large flying boat from the Hall-Aluminum Aircraft Corporation, to meet a requirement for an experimental very-long range patrol aircraft. The resulting design was designated XP2H-1 and was a four engined biplane. It had an all-aluminium hull, a scaled up version of that used in Hall's smaller PH flying boat, which accommodated a crew of six. The wings were of fabric skinned aluminium construction and were of trapezoidal shape. The engines, Curtiss V-1570 Conquerors were mounted in tandem push-pull pairs between the wings.^[2][3]

The XP2H-1 first flew on November 15, 1932, and was extensively tested, demonstrating excellent performance, being 11 mph (18 km/h) faster than predicted.^[4] It was possible to cruise on just two engines to extend range, and in 1935, the XP2H-1 was used to carry out a non-stop flight between Norfolk, Virginia and Coco Solo, Panama Canal Zone in 1935, taking 25 hours and 15 minutes to fly the 2,000 miles (3,200 km).^[5] It was destroyed later in the year attempting a landing in open water.^[6] No further P2Hs were built, with the US Navy equipping its patrol squadrons with smaller flying boats such as the Consolidated P2Y.

Operators

 United States

• United States Navy

Specifications

Data from General Dynamic Aircraft and their Predecessors ^[4]

General characteristics

• Crew: 6
• Length: 64 ft 6½ in (19.68 m)
• Wingspan: 112 ft 0 in (34.15 m)
• Height: 25 ft 6 in (7.77 m)
• Wing area: 2,742 ft² (254.8 m²)
• Empty weight: 20,856 lb (9,840 kg)
• Loaded weight: 35,393 lb (16,087 kg)
• Max takeoff weight: 43,193 lb (19,633 kg)
• Powerplant: 4 × Curtiss V-1570-54 Conqueror V-12 water cooled, 600 hp (448 kW) each

Performance

• Maximum speed: 121 knots (225 km/h, 139.6 mph) at sea level
• Cruise speed: 104 knots (193 km/h, 120 mph)
• Range: 1,870 nmi (3,462 km, 2,150 mi)
• Ferry range: 2,913 nmi (5,394 km, 3,350 mi) (maximum range)
• Service ceiling: 10,900 ft (3,320 m)
• Climb to 5,000 ft (1,525 m): 8.7 min

Armament

• Guns: Five flexibly mounted 0.3 in Browning machine guns in nose, dorsal waist and tail positions
• Bombs: 2,000 lb (909 kg) bombs

See also

Aircraft of comparable role, configuration and era

• Short Singapore
  

References

1. ^ Test Pilot AIRPOWER, September 1974 pp. 11-12
2. ^ Wegg 1990, pp.113-114.
3. ^ Flight January 24, 1935, p.94.
4. ^ ^{a b} Wegg 1990, p.114.
5. ^ Flight 21 February 1935, p.195.
6. ^ Loftin 1985, Chapter 8: Boats in the Sky :Biplane Flying-Boat Developments, 1920-30.

• "For Long Range Patrol". Flight, 24 January 1925. p. 94.
• "A Long Distance Flight" Flight, 21 February 1925, p. 195.
• Boyne, Walter J. "The Flying Hallmarks: The Hall Aluminium Classics". The Best of Wings Magazine. Washington, DC:Brasseys, 2001. ISBN 9781574883688. pp. 52–61.
• Loftin, Laurence K. Quest for Performance:The Evolution of Modern Aircraft,SP-468. Washington, DC: National Aeronautics and Space Administration, History Office, Scientific and Technical Information Branch, 1985.
• Wegg, John. General Dynamic Aircraft and their Predecessors. London:Putnam, 1990. ISBN 0-85177-833-X.