Bell XFL Airabonita

XFL Airabonita
Role	Fighter
Manufacturer	Bell Aircraft
First flight	13 May 1940
Status	Cancelled
Primary user	United States Navy
Number built	1
Unit cost	$125,000
Developed from	Bell P-39 Airacobra

The Bell XFL Airabonita was a United States experimental shipboard interceptor aircraft developed for the United States Navy by Bell Aircraft Corportation of Buffalo, New York. It was similar to and a parallel development of the U.S. Army Air Corps’ land-based P-39 Airacobra, differing mainly in the use of a tailwheel undercarriage in place of the P-39's tricycle gear. Only one prototype was manufactured.

Design and development

The XFL-1 (Bell Model 5) was powered by a single 1,150 hp (858 kW) Allison XV-1710-6 twelve cylinder, two bank Vee, liquid-cooled engine installed amidships behind the pilot and driving a three bladed Curtiss Electric propeller in the nose through a 10.38 ft (3.16 m) extension shaft. The aircraft had provisions for a single 37 mm (1.46 in) Oldsmobile T9 cannon which could be replaced by a .50 in (12.7 mm) Browning M2/AN machine gun through the propeller shaft and two .30 in (7.62 mm) machine guns in the fuselage nose. It first flew on 13 May 1940.

Although based on the P-39, the XFL-1 utilised a conventional tail-wheel undercarriage and the coolant radiators were housed externally in fairings under the wings instead of within the wing center section. The Allison engine was the first of its type to be tried out by the Navy and lacked the turbosupercharger fitted to the XP-39.

Operational history

The XFL-1 in flight

In January 1938, the U.S. Navy issued a specification for a light carrier-based fighter to replace the obsolete biplanes then in use. On 11 April 1938, Bell, Brewster, Curtiss, Grumman and Vought-Sikorksy submitted proposals but only three received contracts. Two of them were awarded contracts for one prototype each on 30 June 1938; these were for the Grumman XF5F-1 Skyrocket and the Vought-Sikorsky XF4U-1 Corsair. The third contract, which was signed on 8 November, went to Bell Aircraft for one XFL-1 Airabonita. All three aircraft made their first flight in 1940, the XF5F-1 on 1 April, the XFL-1 on 13 May and the XF4U-1 on 29 May.

Subsequent tests were prolonged because of difficulties with the Allison engine and problems with the balance of the aircraft. Official evaluation began in July 1940 but the XFL-1 failed to be certified for carrier operations because of main landing gear problems. The prototype was returned to Bell for modifications in December 1940 and returned to the Navy on 27 February 1941 at Naval Air Station Anacostia, District of Columbia. Based on the test results, the Navy decided not to order production of the aircraft.

In February 1942, the XFL-1 was transferred to the Aircraft Armament Unit at U.S. Naval Air Station Patuxent River, Maryland. It was later used, grounded, for armament tests, and later destroyed. For many years its remains were visible at the dump at NAS Patuxent River.

As a possible further reason for the rejection it is often stated that the Navy's position during that era was that all its aircraft should use air-cooled engines (while the Allison was liquid-cooled). This appears unfounded speculation. The U.S. Navy "would consider a liquid-cooled engine installation provided a material increase in performance over air-cooled engine can be shown."

In addition, the Allison engine had only a single-speed supercharger, consequently, its altitude performance was much inferior to other naval fighters of the period such as the Grumman F4F Wildcat.

Lastly, the Airabonita had to compete against the considerably faster Vought F4U Corsair, the first U.S. Navy fighter to exceed 400 mph (644 km/h) in level flight.

Operators

United States

• United States Navy

Specifications (XFL-1 Airabonita)

XFL-1

Data from

General characteristics

• Crew: One
• Length: 29 ft 9 in (9.07 m)
• Wingspan: 35 ft 0 in (10.67 m)
• Height: 12 ft 9 in (3.89 m)
• Wing area: 232 ft² (21.6 m²)
• Empty weight: 5,161 lb (2,341 kg)
• Loaded weight: 6,651 lb (3,017 kg)
• Max. takeoff weight: 7,212 lb (3,271 kg)
• Powerplant: 1 × Allison XV-1710-6 V-12 piston engine, 1,150 hp (858 kW)

Performance

• Maximum speed: 307 mph (464 km/h)
• Range: 1,072 mi (1,725 km)
• Service ceiling: 30,900 ft (9,421 m)
• Rate of climb: 2,630 ft/min (13.4 m/s)
• Wing loading: 29 lb/ft² (140 kg/m²)
• Power/mass: 0.17 hp/lb (280 W/kg)

Armament

• Guns:
  
  • 2 × 0.30 cal (7.62 mm) machine guns
  • 1 × 0.50 cal (12.7 mm) machine gun or 37 mm cannon

See also

Related development

• Bell P-39 Airacobra
• Bell P-63 Kingcobra

References

Bibliography

• Angelucci, Enzo. "The American Fighter".
• Bowers, Peter M. "Airborne Cobra Pt.II". Airpower, Vol. 9, No. 1, January 1979.
• Dorr, Robert F. and Jerry C. Scutts. Bell P-39 Airacobra. Ramsbury, Marlborough, Wiltshire, UK: The Crowood Press Ltd., 2000. ISBN 1-86126-348-1.
• Green, William. "Bell XFL-1 Airabonita". War Planes of the Second World War, Volume Four: Fighters. London: Macdonald & Co. (Publishers) Ltd., 1961 (6th impression 1969), pp. 13–14. ISBN 0-356-01448-7.
• Green, William and Gordon Swanborough. "Bell XFL-1 Airabonita". WW2 Aircraft Fact Files: US Navy and Marine Corps Fighters. London: Macdonald and Jane's Publishers Ltd., 1976, p. 3. ISBN 0-356-08222-9.
• Kinzey, Bert. "XFL-1 Airabonita". P-39 Airacobra - in detail. Carrollton, Texas: Squadron/Signal Publications Inc., 1999, p. 8. ISBN 978-1-88897-416-4.
• Pelletier, A.J. "Bell Aircraft since 1935".
• Thomason, Tommy. Bell XFL-1 Airabonita (Naval Fighters Number Eighty-One). Simi Valley, California: Ginter Books, 2008. ISBN 0-942612-81-7.
• Tomalik, Jacek. Bell P-6 Kingcobra, XFL-1 Airabonita, P-39 Airacobra (Monografie Lotnicze 59) (in Polish). Gdansk, Poland: AJ-Press, 2001. ISBN 83-7237-034-6.

• Wagner, Ray. "American Combat Planes Of The 20th Century".