Aichi D3A (Val)


	The Aichi D3A (Val)
	The Aichi D3A (Val)


	Aichi D3As prepare to takeoff for the attack on United States military installations at Pearl Harbor, December 7,1941. (Photo: National Archives)
	On December 7,1941, the Japanese Imperial Navy launched 353 aircraft from six carriers,¹ in a surprise attack, against United States military installations, on the island of Oahu, Hawaii. The aircraft included Mitsubishi A6M2s (Zero), Nakajima B5Ns (Kate) and Aichi D3As (Val). The Aichi D3A led the first wave of attacks, and it was the first Japanese aircraft to drop bombs on American targets.² 129, Aichi D3As were used as part of the Japanese task force that attacked Pearl Harbor.³ Despite its obsolescence, the D3A took part in all major Japanese carrier operations in the first ten months of the war, after the attack on Pearl harbor. Before WW II, they saw only limited action from land bases in China and Indo-China. During the campaign in the Indian Ocean, D3As placed more than 82% of their bombs on target during attacks on the cruisers, HMS Cornwall, and HMS Dorsetshire and the carrier HMS Hermes in April, 1942.⁴

Inspired by the Heinkel He 70, the D3A was designed as a carrier-based dive-bomber to replace the D1A2, Navy Type 96 Carrier Bomber. The Navy ordered two prototypes with the first prototype being completed in December, 1937. The first prototype was the Nakajima D3N1, powered by the 730-hp Nakajima Hakari 1 radial engine but showed many shortcomings during initial flight-testing. It was found to be under-powered, and had a tendency to snap-roll in tight turns. The dive brakes, similar to the Junkers Ju 87, vibrated violently when nosed over at 90 degrees, and had to be strengthened as diving speeds were increased. However, the aircraft did show promise, because it had a strong airframe and the overall handling characteristics were good, with the exception of the snap-roll problem. The second prototype was the Aichi D3A1, configured with a fixed landing gear to eliminate extra weight and maintenance problems of a retractable landing gear system. The Aichi prototype was extensively modified to overcome the shortcomings of the Nakajima design. Engine power was increased to 840 hp with a Mitsubishi Kinsei 3 , fourteen-cylinder radial engine, and a redesigned cowling was installed. The wing span was increased, the vertical stabilizer was enlarged, and improved dive brakes were installed. The better performing Aichi D3A1 was selected to go into production under the designation Navy Type 99 Carrier Bomber Model 11. ⁵


The production D3A1s engine power was increased with a 1,000 hp Mitsubishi Kinsei 43, engine, or 1,070 hp Kinsei 44, engine. The wing area was decreased slightly and a large dorsal fin was installed, to correct directional stability problems. The aircraft was equipped with only two forward-firing 7.7 mm Type 97 machine-guns and one flexible rear-firing 7.7 mm Type 92 machine gun. The normal bomb load was a single 250 kg (551 lb) bomb, carried under the fuselage, which swung down and forward on arms before it was released. Two additional 60 kg (132 lb) bombs could be carried on wing racks, located under each wing outboard of the dive brakes. ⁶ In June 1942, the D3A was further improved with a more powerful 1,300 hp Kinsei 54 engine and went into production as the D3A2. It featured an increased range to 915 miles (1,472 km) with a fuel capacity of 1,079 liters (237-4 Imp gal). Externally, the aircraft was almost identical to the D3A1 with the exception of a propeller spinner and a rear canopy section that was longer and more pointed. It was designated Navy Type 99 Carrier Bomber Model 22 and began to replace the Model 11 in front-line units in the autumn of 1942. When the much faster Yokosuka Suisei became available, the D3A2s were relegated to land-based units and operated from the smaller carriers, which had decks too short for the Suisei's higher landing speed. In 1944, when the American forces returned to the Philippines, D3A2s took an active part in the bitter fighting, but were hopelessly outclassed and suffered heavy losses. By then, many D3A1s and D3A2s were operated by training units in Japan and several were modified as Navy Type 99 Bomber Trainer Model 12s (D3A2-K).⁷ During the last year of the war, D3A2s were mostly relegated to second-line duties. They also engaged in kamikaze attacks and experienced a high loss rate, with poor compensating results.⁸

The production D3A1s engine power was increased with a 1,000 hp Mitsubishi Kinsei 43, engine, or 1,070 hp Kinsei 44, engine. The wing area was decreased slightly and a large dorsal fin was installed, to correct directional stability problems. The aircraft was equipped with only two forward-firing 7.7 mm Type 97 machine-guns and one flexible rear-firing 7.7 mm Type 92 machine gun. The normal bomb load was a single 250 kg (551 lb) bomb, carried under the fuselage, which swung down and forward on arms before it was released. Two additional 60 kg (132 lb) bombs could be carried on wing racks, located under each wing outboard of the dive brakes. ⁶

In June 1942, the D3A was further improved with a more powerful 1,300 hp Kinsei 54 engine and went into production as the D3A2. It featured an increased range to 915 miles (1,472 km) with a fuel capacity of 1,079 liters (237-4 Imp gal). Externally, the aircraft was almost identical to the D3A1 with the exception of a propeller spinner and a rear canopy section that was longer and more pointed. It was designated Navy Type 99 Carrier Bomber Model 22 and began to replace the Model 11 in front-line units in the autumn of 1942. When the much faster Yokosuka Suisei became available, the D3A2s were relegated to land-based units and operated from the smaller carriers, which had decks too short for the Suisei's higher landing speed. In 1944, when the American forces returned to the Philippines, D3A2s took an active part in the bitter fighting, but were hopelessly outclassed and suffered heavy losses. By then, many D3A1s and D3A2s were operated by training units in Japan and several were modified as Navy Type 99 Bomber Trainer Model 12s (D3A2-K).⁷ During the last year of the war, D3A2s were mostly relegated to second-line duties. They also engaged in kamikaze attacks and experienced a high loss rate, with poor compensating results.⁸

Specifications:
	D3A1	D3A2
Dimensions:
Wing span:	47 ft 1 15/16 in (14.365 m)	47 ft 1 15/16 in (14.365 m)
Length:	33 ft 5 3/8 in (10.195 m)	33 ft 5 3/8 in (10.195 m)
Height:	12 ft 7 15/32 in (3.847 m)	12 ft 7 15/32 in (3.847 m)
Weights:
Empty:	5,309 lb. (2,408 kg)	5,666 lb. (2,570 kg)
Loaded:	8,047 lb (3,650 kg)	8,378 lb (3,800 kg)
Performance:
Maximum Speed:	240 mph (209 kt) @ 9,845 ft (3,000 m)	267 mph (232 kt) @ 20,340 ft (6,200 m)
Service Ceiling:	30,500 ft. (9,300 m)	34,450 ft. (10,500 m)
Range:	840 miles (1,351 km)	915 miles (1,472 km)

Powerplant D3A1:	Powerplant D3A2:
Mitsubishi Kinsei 43, 1,000 hp or, Kinsei 44, 1,070 hp. engine.	Kinsei 54, 1,300 hp engine.
Armament:
Two forward-firing 7.7 mm Type 97 machine-guns and one flexible rear-firing 7.7 mm Type 92 machine gun. A single 250 kg (551 lb) bomb carried under the fuselage and two additional 60 kg (132 lb) bombs carried on wing racks.

Endnotes

1. David Mondey, ed. The International Encyclopedia of Aviation. New York, Crown Publishers, Inc., 1977. 217.
2. Rene J. Francillon, Japanese Aircraft of the Pacific War, Aichi D3A. Annapolis, Maryland: Naval Institute Press, 1995. 271.
3. David Mondey. The Concise Guide to Axis Aircraft of World War II. New York: Smithmark Publishers, 1996. 9.
4. Francillon. 274.
5. Ibid. 272-273.
6. Ibid. 273.
7. Ibid. 275.
8. Mondey. 10.

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