THE ARMY AIR CORPS
To listen to Recce Flight Click on
the Badge. HISTORY
Although the present Corps dates only from 1957, its origins can
be traced to the early days of World War II. In 1942 demands for battlefield
air reconnaissance and direction of artillery fire led to the formation of Air
OP (Air Observation Post) squadrons of light observation aircraft,
piloted by Royal Artillery officers. The same year saw the raising of an Army
Air Corps comprising the Glider Pilot Regiment and the Parachute
Regiment (Army Order 21/42). In 1944 the recently formed Special Air Service
Regiment was also incorporated in the Corps. In 1945 the SAS was (temporarily) disbanded; the Parachute
Regiment was divorced from the Corps in 1949 to join the Infantry of the
Line, and in 1950 the original Army Air Corps was disbanded. The remaining
glider pilots were retrained to fly powered aircraft and were formed into Light
Liaison Flights operating alongside or as part of the Air OP squadrons. It soon became clear that the Army had an increasing need of
light aircraft and helicopter support for a variety of tasks, and under Army
Order 82 of 1957 the existing Army Air Corps was formed from the Air
OP and Light Liaison units. Its depot and training center were located, as
today, at Middle Wallop, Hampshire, a former RAF station. From 1957 until 1973 the new
Army Air Corps consisted of a small cadre of Officer and NCO pilots
supplemented by volunteers attached from other Arms. Ground crew duties were
also performed by attached soldiers, mainly from the Royal Armoured Corps and
Royal Artillery. However in 1973 the Army Air Corps began to recruit its own
ground crew soldiers. Private soldiers in the Corps are known as Air
Troopers. Since 1957 all field maintenance, recovery and repair of the
Corps’ aircraft have been carried out by attached personnel of the Royal
Electrical and Mechanical Engineers. EARLY FIXED-WING LIGHT AIRCRAFT
de HAVILLAND CHIPMUNK T.10 WB 610 The Chipmunk was the de Havilland Co’s successor to the
world-famous Tiger Moth biplane. Unlike the Tiger Moth, however, it was first
designed by the Canadian branch of de Havilland at With the appearance of the Chipmunk in England, the Air Ministry
decided to adopt the type as an ab initio trainer to Spec. 8/48 after
tests at Boscombe Down with G-AKDN, fitted out to full RAF requirements with
blind-flying panels, radio and manually operated variable pitch airscrew.
Production of the RAF version began with WB 549 and the type was designated
Chipmunk T.10. Total output of Chipmunks for the RAF was 740, the last being
delivered on The first RAF Chipmunks were delivered to the Oxford University
Air Squadron, where they superseded Tiger Moths at Kidlington early in 1950.
Thereafter the Chipmunk became standard equipment in all 17 University Air
Squadrons and was also chosen as the basic type for the 20 or so Reserve
Flying Schools of the RAF Voluntary Reserve, where it was flown by the
‘week-end pilots’ until the schools were closed as an economy measure in
1952-1953. During the expansion of the RAF pilot-training programme in
1951-1952 the Chipmunk was chosen for the ab initio instruction of
National Service pilots, who afterwards took advanced training on Oxfords. At
the A point worthy of note is that HRH the Duke of Edinburgh took his
first flying instruction in a Chipmunk (WP 861) at White Waltham in November
1952. Technical Data (Chipmunk T.10) |
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Description: Manufacturers: Power Plant: Dimensions: Weights: Performance: |
Two-seat
elementary trainer. All-metal stressed-skin construction. Maker’s
designation, DHC 1. de Havilland
Aircraft Co. Ltd., Hatfield, Hertfordshire. One
145-horsepower de Havilland Gipsy Major 8. Span, 34 feet 4
inches. Length, 25 feet 8 inches. Height, 7 feet 1 inch. Wing area, 172
square feet. Empty, 1,417
pounds. Loaded, 2,000 pounds. Maximum speed, 138 miles/hour at sea level. Cruising, 119
miles/hour. Climb, 800 feet/minute; 7.3 minutes to 5,000 feet. Range, 300
miles. Endurance, 2.3 hours. Service ceiling, 16,000 feet.
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BRITISH TAYLORCRAFT AUSTER Mk I to Mk V
Auster Mk I, LB 278 This series of light-cabin monoplanes was supplied to the RAF
throughout the Second World War by Taylorcraft Aeroplanes ( In 1942 the Auster Mk II (130-horsepower Lycoming) appeared, but
only two were built, owing to shortage of American engines, and the next main
production type was the Auster Mk III (prototype LB 319) with 130-horsepower
Gypsy Major 1, of which 467 were built. At the end of 1943, when Lycoming
engines once again became available, production switched to the Auster Mk IV
(prototype MT 453) with 130-horsepower Lycoming, of which 255 were built. The
Auster Mk IV introduced a third seat, all earlier models being two-seaters.
The last of the wartime Austers was the Mk V (prototype MT 356), similar to
the Mk IV, but with a blind-flying panel. Some Mk Vs were used on
communications duties as well as AOP. Total output of the Auster Mk V was
780, terminating with TW 520 delivered on Squadron Allocations
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2nd
Tactical Air Force: Desert
Air Force: |
Nos. 653, 658, 659
and 662 Squadrons with 8, 12 and 30 Corps. Nos. 652, 657, 660, 661, 664 and
665 Squadrons with 1 Corps and 2 Canadian Corps. Nos. 651, 654, 655 and 663 Squadrons of 253 Wing. Also Nos. 656, 666, 671, 672 and 673 Squadrons. |
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Technical Data (Auster Mk IV) |
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Description: Manufacturers: Power Plant: Dimensions: Weights: Performance: Armament: |
Three-seat AOP. Composite wood and metal structure, fabric covered.
Maker’s designations: Model D/1 (Auster Mk I), Model F (Auster Mk III), Model
G (Auster Mk IV) and Model J (Auster Mk V). Taylorcraft Aeroplanes ( One 130-horsepower Lycoming O-290-3. Span, 36 feet. Length, 22 feet 5 inches. Height, 8 feet. Wing
area, 167 square feet. Empty, 1,100 pounds. Loaded, 1,700 pounds. Maximum speed, 130 miles/hour at sea level. Cruising, 110
miles/hour. Range, 250-300 miles. None carried. |
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AUSTER AOP Mk VI
WJ 374 By 1945 Auster light-cabin monoplanes had become an indispensable
part of the military aviation scene. Since 1941 they had operated on all
battlefronts with great success and had demonstrated their versatility as
artillery spotters and light communications aircraft capable of operating
from the smallest airfields. They were flown by Royal Artillery officers and
serviced on the ground by RAF personnel. For the post-war Air Observation Post squadrons the Auster AOP Mk
VI was selected. The Auster Mk VI incorporated all the experience gained in
the manufacture of over 1,600 wartime Austers, but substituted the de
Havilland Gipsy Major for the American Lycoming engine, had a lengthened
undercarriage leg and increased fuel capacity. The most striking external
difference, however, was the introduction of auxiliary aerofoil flaps
extending aft of the trailing edge of the wing in place of the earlier split
flaps. These factors combined to reduce still further the already remarkably
short take-off and landing runs. The prototype Auster AOP Mk VI (TJ 707) made
its initial flight on The Auster Mk VI entered service in 1947, going to No. 657 Squadron
and an Operational Training Unit at RAF Andover. Eventually the Auster Mk VI
replaced earlier models with AOP squadrons in Also supplied to the RAF were 77 dual-control trainer versions,
known as the Auster T.VII. The prototype (VF 665) first flew in 1947. Auster AOP Mk VIs of No 1903 Flight (part of No 656 Squadron)
gave excellent service in the Korean War and in Malaya No. 656’s AOP Mk VIs
operated against the terrorists. One AOP Mk VI (VF 626) flew nearly 3,500
hours before being retired in 1955. Squadron Allocations
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Regular AOP: Royal
Auxiliary Air Force AOP: |
Nos. 651, 652, 656 and 657 Squadrons. Nos. 661, 662,
663, 664 and 666 Squadrons. |
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Technical Data (Auster Mk VI) |
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Description : Manufacturers: Power Plant: Dimensions: Weights: Performance: |
Two-seat AOP. Composite wood and metal structure, fabric covered.
Maker’s designation: Model K. Auster Aircraft Ltd., Rearsby, Leicester. One 145-horsepower de Havilland Gipsy Major 7. Span, 36 feet. Length, 23 feet 9 inches. Height, 8 feet 4½
inches. Wing area, (including flaps), 187 square feet. Empty, 1,413 pounds. Loaded, 2,160 pounds. Maximum speed,
124 miles/hour at 1,000 feet. Cruising, 108 miles/hour. Initial climb, 810
feet/minute. Service ceiling, 14,000 feet. |
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AUSTER AOP Mk IX
WZ 664 Almost a year after the last Auster AOP Mk VI for the RAF left
the Auster factory a completely new design, eventually to supersede the Mk VI
in the AOP Squadrons, was ready for its first flight at Rearsby airfield.
This was the Auster AOP Mk IX, the first of which (WZ662) made its maiden
flight on Unlike the earlier Austers, nearly 2,000 of which were supplied
to the British Army and RAF, the Auster AOP Mk IX was not developed from a
civil aircraft, but was designed from the outset as a military type. More
powerful than earlier Austers and employing greater wing area, with large
flaps and drooping ailerons, the Auster AOP Mk IX can be used not only for
Air Observation Post duties, but also for such work as casualty evacuation,
cable-laying, photographic sorties and light transport. Access to the cabin,
through three wide doors, is particularly easy, and there are such additional
refinements as cabin temperature control and a magnificent field of view
through 53 square feet of Perspex. For AOP duties pilot and observer only are
carried, but provision is made for a third seat. An unusual feature is that
the rear cockpit floor is rapidly detachable by removing six bolts, whereupon
a new floor is substituted, carrying equipment to suit the aircraft for an
alternative range of duties. Drooping ailerons assist short take-offs and
landings, the runs being 110 yards and 50 yards respectively. The simple but
rugged undercarriage enables landings to be made on all types of surface,
from thick mud to ploughed fields, a great asset in an AOP aircraft. The AOP Mk IX was first demonstrated at the 1954 SBAC Display,
where the third production aircraft (WZ 664) appeared. At the 1955 Display,
WZ 715 was flown. Initial deliveries of the AOP Mk IX to the RAF were made early in
1955, some of the first aircraft being based at Middle Wallop. Later in 1955,
Auster AOP Mk IXs commenced operations against the terrorists in Technical Data (Auster AOP Mk IX) |
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Description: Manufacturers: Power Plant: Dimensions: Weights: Performance: |
Two/three-seat AOP or light liaison aircraft. Metal structure,
metal and fabric covered. Auster Aircraft Ltd., Rearsby, Leicester. One 180-horsepower Blackburn Cirrus Bombadier 203. Span, 36 feet 5 inches. Length, 23 feet 8½ inches. Height, 8 feet
5 inches. Wing area, 197½ square feet. Empty, 1,461 pounds. Loaded, 2,130 pounds. Maximum speed,
127 miles/hour. Cruising, 110 miles/hour. Initial climb, 930 feet/minute.
Range, 246 miles. Service ceiling, 18,500 feet. |
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de HAVILLAND DHC-2 BEAVER Mk 1 Nearly 1,700 DHC-2 Beaver light utility transports were built,
the first flying in 1947. Carrying either seven passengers or freight, the
Beaver has proved capable of operating in very rough, remote areas. The
Beaver Mk 1 was produced in both civil and military forms, some 968 of the
latter variant going to the US Army/USAF as the U-6A. Beavers have been
fitted with floats and skis. A later development is the Turbo-Beaver Mk 3,
which has the Pratt & Whitney radial engine replaced by a PT6A turboprop.
This changes the nose shape significantly. The Mk 3 can carry 10 passengers,
cruises at 252 km/hour and has a range of 1,090 km. Technical Data (de Havilland DHC-2 Beaver Mk 1
EARLY LIGHT HELICOPTERS SAUNDERS-ROE SKEETER AOP Mk 10
XK 773 The Skeeter AOP Mk 10 and T.11 ordered by the Army and RAF are
developments of the Skeeter Mk 1 which first flew on Technical Data (Saunders-Roe Skeeter AOP Mk 10) |
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Manufacturers: Power Plant: Dimensions: Weights: Performance: |
Saunders-Roe
Ltd. One
183-horsepower de Havilland Gipsy Major 30 engine. Main rotor diameter, 32 feet. Length, 31 feet 1½ inches. Loaded, 2,200
pounds. Maximum speed,
101 miles/hour. |
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SAUNDERS-ROE SKEETER AOP Mk 12
Photograph contributed by George MILLIE XL 763 The first Skeeter AOP Mk 12 to be delivered into service at 652
Light Aircraft Squadron, |
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Manufacturer:
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Saunders-Roe (Westland Division) Ltd.
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SUD-AVIATION SE 3130 ALOUETTE II
SA 318C All the helicopters in this family are basically similar and
differ principally in their power-plants. The prototype were built as SE
3120’s and powered by a Salmson 9 engine; production types were designated SE
3130 and subsequently SE 313B Alouette II. Production totalled more than 900.
The Astazou-powered SA 318C first flew in 1961 and when production ended in
1975 more than 350 had been built. The SA 315B Lama is an Artouste-powered
version built to an Indian requirement, while the Cheetah is a licence-built
version produced by HAL for the Indian Army. The Lama has been sold to
operators in more than twenty countries. The version built for the Army
Air Corps was the SE 3130 Alouette II powered by an Artouste gas-turbine
engine. Technical Data (Sud-Aviation SE 3130
Alouette II) |
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Manufacturers: Country of origin: Power Plant: Dimensions:
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Sud-Aviation, le Bourget, la
Courneuve, Paris. One Artouste gas-turbine. Rotor diameter, 36 feet 1¾ inches
(11.02 metres). Length,
33 feet 8 inches (10.26 metres).
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