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Grumman Aerospace  GRUMMAN J2F DUCK


General information
Type Utility amphibian
National origin United States
Manufacturer Grumman
Columbia Aircraft Corp
Primary users United States NavyUnited States Army Air Forces
United States Coast Guard
United States Marine Corps
Number built 584
History
Introduction date 1936
First flight 2 April 1936
Developed from Grumman JF Duck
.
History GRUMMAN AEROSPACE
GRUMMAN J2F DUCK ( DESIGNATION G-15)
INTRODUCTION DATE 1936 FIRST FLIGHT 2 APRIL 1936

Operational history

The J2F was used by the U.S. Navy, Marines, Army Air Forces, and Coast Guard. Apart from general utility and light transport duties, its missions included mapping, scouting/observation, anti-submarine patrol, air-sea rescue work, photographic surveys, reconnaissance, and target tug.

J2Fs of the utility squadron of US Patrol Wing 10 were destroyed at Mariveles Naval Section Base, Philippines, by a Japanese air raid on 5 January 1942. The only Duck to survive the attack had a dead engine but had been concealed at Cabcaben airfield during the Battle of Bataan, to be repaired afterwards with a cylinder removed from a destroyed J2F-4 submerged in Manila Bay. Following repairs the J2F-4 departed after midnight on 9 April 1942, overloaded with five passengers and the pilot, Roland J.Barnick, becoming the last aircraft to depart Bataan before the surrender of the Bataan to the Japanese only hours later. Among its passengers was Carlos P. Romulo (diplomat, politician, soldier, journalist, and author), who recounted the flight in his 1942 best-selling book I Saw the Fall of the Philippines (Doubleday, Doran & Company, Inc., Garden City, New York 1943, pp. 288–303), for which he received the Pulitzer Prize for Correspondence.

Variants

J2F-3 at NAS Jacksonville in 1940
J2F-6 painted as an OA-12 at the National Museum of the United States Air Force
J2F-1
Initial production version with 750 hp R-1820-20 engines, 29 built.
OA-12
Air-sea rescue conversion for the United States Army Air Forces (and later United States Air Force, OA-12A).

 

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Km

Take off Distance

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Range

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Km/H

Aircraft Speed

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Max Crew

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Grumman Aerospace Corporation,

Grumman Aerospace Corporation
GRUMMAN AEROSPACE GRUMMAN J2F DUCK
( DESIGNATION G-15) INTRODUCTION DATE 1936 FIRST FLIGHT 2 APRIL 1936

1

General characteristics

  • Crew: 2
  • Capacity: 2 survivors / passengers
  • Length: 34 ft 0 in (10.36 m)
  • Wingspan: 39 ft 0 in (11.89 m)
  • Height: 13 ft 11 in (4.24 m)
2

Powerplant

  • Empty weight: 5,480 lb (2,486 kg)
  • Gross weight: 7,700 lb (3,493 kg)
  • Powerplant: 1 × Wright R-1820-54 Cyclone 9-cylinder air-cooled radial piston engine, 900 hp (670 kW)
  • Propellers: 3-bladed constant-speed propeller
plane
3

Specifications

  • Maximum speed: 190 mph (310 km/h, 170 kn)
  • Cruise speed: 155 mph (249 km/h, 135 kn)
  • Stall speed: 70 mph (110 km/h, 61 kn)
  • Range: 780 mi (1,260 km, 680 nmi)
  • Service ceiling: 20,000 ft (6,100 m)
4

Aircraft of comparable role

    • Guns: 1 × Browning .30 cal machine gun (7.62 mm) on flexible mount in rear cockpit
    • Bombs: 2× 100 lb (45 kg) bombs or 325 lb (147 kg) depth charges underwing
Special Links Grumman Aerospace Corporation,  Grumman F2F Duck 

Links to Youtube & Others

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Grumman Aerospace GRUMMAN J2F DUCK

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Youtube Link

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