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The Grumman F2F was a single-engine, biplane fighter aircraft with retractable undercarriage, serving as the standard fighter for the United States Navy between 1936 and 1940. It was designed for both carrier- and land-based operations. Grumman's success with the two-seat FF-1, which was significantly faster than even the single-seat fighters of its time, resulted in a contract for the single-seat XF2F-1. Armed with two 0.30 in (7.62 mm) machine guns above the cowl, the new design also incorporated watertight compartments to reduce weight and improve survivability in the event of a water landing. The prototype first flew on 18 October 1933, equipped with the experimental 625 hp (466 kW) XR-1534-44 Twin Wasp Junior radial engine, and reached a top speed of 229 mph (369 km/h) at 8,400 ft (2,600 m) – 22 mph (35 km/h) faster than the FF-1 at the same altitude. Maneuverability also proved superior to the earlier two-seat aircraft. The Navy ordered 54 F2F-1 fighters on 17 May 1934, with the first aircraft delivered 19 January 1935.[citation needed] One additional aircraft (BuNo 9997) was ordered to replace one which crashed on 16 March 1935, bringing the total to 55, with the final F2F-1 delivered on 2 August 1935.[citation needed] The F2F-1 had a relatively long service life for the time, serving in front-line squadrons from 1935 to late 1939, when squadrons began to receive the F3F-3 as a replacement. By September 1940, the F2F had been completely replaced in fighter squadrons and was relegated to training and utility duties. The last F2F-1s were stricken from the list of naval aircraft in early 1943. Variants XF2F-1 United States Navy designation for the Grumman Model G-8 prototype with a 625 hp (466 kW) XR-1534-44 Twin Wasp Junior radial engine, one built F2F-1 Production variant with a 700 hp (522 kW) R-1535-72 Twin Wasp Junior radial engine, 55 built.

The Mitsubishi Ki-21, formal designation "Type 97 Heavy Bomber" (九七式重爆撃機, Kyūnana-shiki jūbakugekiki) was a Japanese heavy bomber during World War II. It began operations during the Second Sino-Japanese War participating in the Nomonhan Incident, and in the first stages of the Pacific War, including the Malayan, Burmese, Dutch East Indies and New Guinea Campaigns. It was also used to attack targets as far-flung as western China, India and northern Australia. The Allies designated it under the reporting names "Sally" /"Gwen". In 1936, the Imperial Japanese Army Air Service issued a requirement for a new heavy bomber to replace both the Ki-20 (Army Type 92 Heavy Bomber) and the Ki-1 (Army Type 93 Heavy Bomber). The design called for a crew of at least four, top speed of 400 km/h (250 mph), endurance of at least five hours, and a bombload of 750 kg (1,650 lb). The design parameters were very ambitious for the mid-1930's; few twin-engine bombers anywhere in the world could exceed such performance at that time. Both Mitsubishi and Nakajima were asked to build two prototypes each, a further proposal from Kawasaki was rejected. The Mitsubishi design was an all-metal mid-wing cantilever monoplane with retractable landing gear, ventral bomb bay and two radial engines. The first prototype flew on 18 December 1936, with the second prototype, which differed in replacing the dorsal turret of the first prototype with a long greenhouse canopy, following later in the month. In the resulting competition, Mitsubishi's Ki-21 and Nakajima's Ki-19 were found to be similar, with the Ki-21 having better performance, while the Nakajima design was a better bombing platform and had more reliable engines. In order to make a final decision, two further prototypes were ordered from both Mitsubishi and Nakajima, with Mitsubishi instructed to change its own 615 kW (825 hp) Mitsubishi Ha-6 radial engines for the Nakajima Ha-5 engines used by the Nakajima design and vice versa, while the Ki-21 gained a revised glazed nose similar to that of the Ki-19 and revised tail surfaces. Thus modified, the Ki-21 proved superior and was ordered into production in November 1937 as the "Army Type 97 Heavy Bomber Model 1A". Production aircraft began to enter service in August 1938, supplementing and then replacing the Fiat BR.20 bombers which had been purchased as an interim measure. Several improved versions followed before the production of the type ended in September 1944. A total of 2,064 aircraft were built, 1,713 by Mitsubishi and 351 by Nakajima. Variants Ki-21 Prototype models with various engines and armament combinations for evaluation. Final version with Nakajima Ha-5 engine. 8 built Ki-21-Ia (Army Type 97 Heavy Bomber, Model IA) First production model, with 634 kW (850 hp) Nakajima Ha-5-kai engines. Most were built by Mitsubishi, 143 manufactured by Nakajima Ki-21-Ib (Army Type 97 Heavy Bomber, Model IB) Improved version with additional 7.7 mm (0.303 in) machine guns, larger bomb compartment and flaps, redesigned tail. 120 built by Mitsubishi, 351 (including Ki-21 Ib and Ic) by Nakajima Ki-21-Ic (Army Type 97 Heavy Bomber, Model IC) Improved type with one additional 7.7 mm (0.303 in) machine gun, increased fuel capacity, 160 built by Mitsubishi Ki-21-II Evaluation model with more powerful engines, 4 built Ki-21-IIa (Army Type 97 Heavy Bomber, Model IIA) Production model based on Ki-21-II, 590 built Ki-21-IIb (Army Type 97 Heavy Bomber, Model IIB) Final production version based on Ki-21-IIa with modified canopy, clear upper cabin replaced by rotating turret, 688 built. MC-20-I (Army Type 100 Transport, Model I) Unarmed civilian transport version, converted from Ki-21-Ia; approximately 100 aircraft were converted.

The General Aircraft Limited GAL.49 Hamilcar or Hamilcar Mark I was a large British military glider produced during the Second World War, which was designed to carry heavy cargo, such as the Tetrarch or M22 Locust light tank. When the British airborne establishment was formed in 1940 by the order of Prime Minister Winston Churchill it was decided to develop a large glider which would be able to transport heavy equipment in support of airborne troops. General Aircraft Limited were chosen in January 1941 to develop this glider, which they designated the GAL.49 'Hamilcar'. It was designed to transport a light tank or two Universal Carriers. A number of problems, which included vacillation by the War Office on the number of gliders it wanted and poor management by GAL, led to delays in the production of the Hamilcar and it was not until mid-1943 that the first production glider was assembled. These problems were only partially solved and production of the glider continued to be slow, hampered by difficulties in finding suitable locations to store and construct them once their parts were produced. A total of 344 Hamilcars had been built when production ended in 1946. Hamilcars were used on three occasions,and only in support of British airborne forces. They first saw action in June 1944, when approximately thirty were used to carry Ordnance QF 17 pounder anti-tank guns, transport vehicles and Tetrarch light tanks into Normandy in support of British airborne forces during Operation Tonga. In September 1944 a similar number of Hamilcars were used to transport anti-tank guns, transport vehicles and supplies for airborne troops as part of Operation Market Garden. They were used a third and final time in March 1945 during Operation Varsity when they transported M22 Locust light tanks and other supplies. The gliders proved to be successful in all three operations, although their slow speed and large size made them easy targets for anti-aircraft fire, which resulted in a number of gliders being damaged or destroyed. A powered variant of the Hamilcar was produced, the Hamilcar Mark X, to extend the range of the Hamilcar so it could serve in the Pacific War; the conflict in the Pacific ended before the design could see combat. The Hamilcar was constructed primarily from wood, mainly birch and spruce, with fabric-covered plywood forming the skin, and high grade steel reinforcement beams in critical areas. It had a wingspan of 110 feet (34 m), a length of 68 feet (21 m) and a height of 20 feet (6.1 m) to the top of the fin with the tail down. It weighed 18,400 pounds (8,300 kg) when empty, and could transport a military load of 17,600 pounds (8,000 kg) to give a total weight of 36,000 pounds (16,000 kg). The whole aircraft was broken down into smaller sections for transport. It was so large and heavy that it required the largest and most powerful aircraft to pull it off the airfield and subsequently tow it; four-engined bombers were used, most frequently the Handley Page Halifax. Both wing and cockpit were set above the fuselage to provide the greatest amount of room for the cargo compartment, and to ensure that they did not interfere with the loading of vehicles; the compartment measured approximately 32 feet 31.5 inches (10.554 m), 7 feet 10.5 inches (2.400 m) inches wide and between 6 feet (1.8 m) and 7 feet 7 inches (2.31 m) inches in height. The nose of the glider was hinged and opened to the side for ease of loading vehicles and cargo, and the crew of two pilots were seated in tandem in a cockpit on the top of the fuselage, which was accessed via an internal ladder and was fifteen feet above ground; they were eventually protected by a bullet-proof windscreen and a plate of armour behind the second pilot. An intercom was also added to provide communication between the pilots and the personnel below them. An initial design feature, which was eventually removed prior to full-scale production, was the installation of an under-fuselage hatch which would allow the prone firing of a Bren light machine gun as the glider approached the landing zone. When the parts for a Hamilcar were completed and the glider was erected, it was flown to RAF North Luffenham in Rutland to have its specific cargo placed on board, and it was then flown to RAF Tarrant Rushton, which had been selected as the Hamilcar training and operational base in November 1943. It was not possible to tow the glider empty, so any empty gliders usually carried Universal Carriers or concrete blocks as ballast. For more information on the development, design, operational history and variants of the Hamilcar, click here.

The KS-3 agricultural aircraft was the forerunner of the Yeoman Cropmaster, and was built at Bankstown, NSW, by Kingsford Smith Aviation Services (KSAS) in the 1950s. KSAS was well versed with the Wackett, having been involved in overhauling some 50 ex-RAAF Wacketts for the Netherlands East Indies Air Force (NEIAF) in 1946. In 1957 KSAS modified a Wackett VH-AJB (c/n 274) to improve performance. In February 1957 further modifications were made and, following tests, another Wackett VH-AJH (c/n 283) was converted for agricultural use by the installation of a hopper in the front cockpit. First flight was made on 26 March 1957, and this aircraft, known as the KS-1, could carry a 295 kg (650 lb) payload. In August 1957 further modifications were made, including a new hopper and louvre box, and the KS-1 became known as the KS-2. The Chief Pilot of Airwork Pty Ltd of Perth, WA flew the aircraft and asked that the hopper be placed behind the pilot to improve visibility and for ease of loading, and a Wackett (c/n 363) was so converted. Following initial use of the aircraft for a period as noted, this Company recommended changes to the conversion to make it more suitable in its design role. The result was the KS-3, which had a completely re-designed fuselage and a modified wing. The hopper was placed in a hole cut out of the centre-section of the wooden wing, and the control system was re-designed to bypass the hopper, which was installed in what was previously the rear cockpit, which had a capacity of 13 m³/364 litres (459 sq ft/80 Imp gals) and was built of aluminium. Another Wackett VH-FBD¹ (c/n 299) was converted but this aircraft, along with the prototype PL-7 Tanker, was destroyed in a hangar fire at Bankstown on 17 January 1958. KSAS then reserved registrations VH-FBD to VH-FBM for the first production batch of ten aircraft. Another KS-3 VH-FBE (c/n 365) was completed and flown on 24 December 1957. A fourth Wackett (c/n 410) was converted, being test flown and registered on 27 June 1958, becoming VH-FBD². Surplus equipment was removed and, despite the installation of the 123 kw (165 hp) Warner Super Scarab engine, which was considered a little under-powered for this role, the aircraft was found to have a reasonable performance. First customer delivery was VH-FBF (c/n 375) to Airwork in Western Australia, this aircraft having been slightly damaged in the hangar fire referred to but, being repaired, flying for the first time on 21 February 1958. Later the KS-2 VH-AJH (c/n 283) was overhauled, brought up to KS-3 specifications, and bought by Airwork. All KS-3 Cropmasters were operated by Air Culture Pty Ltd, having been obtained from Airwork, in association with Yeoman Aviation Pty Ltd of Claremont, WA, the aircraft being operated under the Yeoman Aviation airwork licence. In 1958 KSAS put to the Department a submission it would build an all-metal wing and tail for all future production aircraft, indicating it had orders for 12 aircraft at that time. It also proposed a tricycle undercarriage and installation of either a 179 kw (240 hp) Continental or a 201 kw (270 hp) Lycoming engine. In this regard Yeoman Aircraft was set up to build the new aircraft, and Yeoman later went on to develop and build the YA-1 Cropmaster, Air Culture being the major user. Air Culture operated the KS-3s until May 1961 when legislation forced their retirement because of Departmental policy on plywood box-spar construction of wings. The aircraft were used extensively for dusting and spraying operations, as well as sowing wheat, and were the first aircraft in Australia to be used for this type of operation. KS-3s built were: VH-FBD¹ (c/n 299) registered in December 1957, but destroyed in a hangar fire at Bankstown on 17 January 1958; VH-FBD² (c/n 410) registered on 27 June 1958 and wrecked when it ground looped at Borden, WA on 27 November 1961; VH-FBE (c/n 365) registered from December 1957 to May 1961; VH-FBF (c/n 375) registered from March 1958 to April 1961 when it crashed at Northampton, WA; and VH-AJH (c/n 283) which, after retirement from agricultural operations, was flown in the private category from May 1963 to April 1964. After having had its hopper removed and side windows fitted, it was stored for some years until placed on display at the Royal Australian Air Force (RAAF) Association Heritage Museum at Bull Creek in Perth, WA in 1976. In 2008 VH-AJH (ex A3-49) was obtained, and placed on display, by the Queensland Air Museum at Caloundra.

The Northrop BT was an American two-seat, single-engine monoplane dive bomber built by the Northrop Corporation for the United States Navy. At the time, Northrop was a subsidiary of the Douglas Aircraft Company. While unsuccessful in its own right, the BT was subsequently redesigned into the Douglas SBD Dauntless, which would form the backbone of the Navy's dive bomber force. The design of the initial version began in 1935. It was powered by a 700 hp (520 kW; 710 PS) Pratt and Whitney XR-1535-66 double row air-cooled radial engine and had hydraulically actuated perforated split flaps (dive brakes), and main landing gear that retracted backwards into fairing "trousers" beneath the wings. The perforated flaps were invented to eliminate tail buffeting during diving maneuvers. The next iteration of the BT, the XBT-1, was equipped with a 750 hp (560 kW; 760 PS) R-1535. This aircraft was followed in 1936 by the BT-1, powered by an 825 hp (615 kW; 836 PS) R-1535-94 engine. One BT-1 was modified with a fixed tricycle landing gear and was the first such aircraft to land on an aircraft carrier. The final variant, the XBT-2, was a BT-1 modified to incorporate landing gear which folded laterally into recessed wheel wells, leading edge slots, a redesigned canopy, and was powered by an 800 hp (600 kW; 810 PS) Wright XR-1820-32 radial. The XBT-2 first flew on 25 April 1938, and after successful testing the Navy placed an order for 144 aircraft. In 1939 the aircraft designation was changed to the Douglas SBD-1 with the last 87 on order completed as SBD-2s. By this point, Northrop had become the El Segundo division of Douglas aircraft, hence the change. The U.S. Navy placed an order for 54 BT-1s in 1936 with the aircraft entering service during 1938. BT-1s served on USS Yorktown and Enterprise. The type was not a success in service due to poor handling characteristics, especially at low speeds, "a fatal flaw in a carrier based aircraft." It was also prone to unexpected rolls and a number of aircraft were lost in crashes. Variants XBT-1 Prototype, one built. BT-1 (Specifications below) Production variant, 54 built. BT-1S A BT-1 (c/n346, BuNo 0643) was fitted with a fixed tri-cycle undercarriage. This aircraft was damaged in a crash on 6 February 1939, returned to Douglas and repaired to BT-1 standard. Comparison between the XBT-1 (BuNo 9745) and XBT-2 (BuNo 0627) on 4 December 1936 XBT-2 One BT-1 modified with fully retractable landing gear and other modifications. BT-2 Production variant of the XBT-2, 144 on order completed as SBD-1 and SBD-2. Douglas DB-19 One BT-1 (c/n346, BuNo 0643), the former BT-1S, was modified as the DB-19 which was tested by the Imperial Japanese Navy as the Douglas DXD1 (long designation - Douglas Navy Experimental Type D Attack Aircraft)