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On October 9, 2025 I changed this site's theme to what I feel is a much better design than previous themes. Some pages will not be affected by this design change, but other pages that I changed and new pages I added in the last several days need to have some of their photos re-sized so they will display properly with the new theme design. Thank you for your patience while I make these changes over the next several days. -- Ray Merriam

Armstrong Whitworth Siskin: British Fighter

Armstrong-Whitworth Siskin IIIA, RCAF, 20 Training Squadron, B Flight, Camp Borden, Ontario.

The Armstrong Whitworth Siskin was a sesquiplane single-seat fighter aircraft developed and produced by the British aircraft manufacturer Armstrong Whitworth Aircraft. It was also the first all-metal fighter to be operated by the Royal Air Force (RAF), as well as being one of the first new fighters to enter service following the end of the First World War.

Development of the Siskin was heavily influenced by RAF Specification Type I, including its initial use of the ABC Dragonfly radial engine. Making its first flight in May 1919, the Siskin possessed good qualities in spite of the Dragonfly's poor performance. In the following year, the much better Armstrong Siddeley Jaguar was installed and flight with this powerplant was made on 20 March 1921. In response to Air Ministry Specification 14/22, the aircraft was redesigned with an all-metal structure, and orders were placed in 1922.

In May 1924, the first of the RAF's Siskin IIIs were delivered to No. 41 Squadron at RAF Northolt. Eleven squadrons would operate the type. Relatively popular with pilots, it served for over eight years before the last of them were replaced by Bristol Bulldogs during October 1932. In addition to the RAF, various other nations evaluated the Siskin and several placed orders. The Royal Canadian Air Force (RCAF) introduced the type in the late 1920s and operated its Siskins until shortly after the outbreak of the Second World War. Several Siskins were also entered in various air races.

Development

Background

The Armstrong Whitworth Siskin was a development of the Siddeley-Deasy S.R.2 Siskin designed by Major F. M. Green (formerly chief engineer of the Royal Aircraft Factory) of the Siddeley-Deasy Motor Car Company. A major impetus for the aircraft's development was the Air Ministry's issuing of RAF Specification Type I, which called for a single-seat fighter that was powered by the ABC Dragonfly radial engine. The Dragonfly would prove to be a disappointment as it failed to meet its anticipated performance.

The SR.2 Siskin was a single-bay biplane of wood and fabric construction. It angular in form, with little attention paid to obvious avenues for drag reduction. Perhaps its most distinctive feature was its fixed conventional landing gear, which had relatively lengthy oleo strut shock absorbers carrying the axle, which was in turn connected by radius rods to a pair of V-struts situated behind the axle. Its wings were of unequal span. It was powered by a single ABC Dragonfly radial engine, which was installed on the nose in a streamlined cowling. To regulate the engine's temperature, each individual cylinder had its own cooling channel. Armament consisted of a pair of Vickers machine guns mounted directly in front of the pilot.

The Siskin made its first flight in May 1919. While the initial aircraft was powered by the intended Dragonfly engine, it would only deliver 270 hp (200 kW) rather than the expected 320 hp (240 kW). Despite early promise, the Dragonfly was disastrous, being less powerful, unreliable, and prone to overheating while excessive vibration resulted in crankshaft failures after only a few hours of use. Despite the engine, the Siskin displayed generally good properties, possessing favorable stability and handling characteristics, along with performance that could outmatch its direct rivals for RAF orders.

Redesign

In 1919, Siddeley-Deasy merged with Armstrong Whitworth, with the aviation interests becoming Armstrong Whitworth Aircraft. Siddeley-Deasy had inherited the design of the RAF 8 fourteen-cylinder radial engine and its designer Sam D. Heron. By 1920, this engine, as the Jaguar, had been developed sufficiently to replace the Dragonfly. A prototype Siskin fitted with a Jaguar flew on 20 March 1921. Air Ministry officials were impressed but urged Armstrong Whitworth to continue developing the aircraft as only an all-metal design would be acceptable to the Royal Air Force (RAF).

During 1922, Air Ministry Specification 14/22 was issued for an all-metal single-seat high performance landplane. The Siskin was submitted leading to an order for a single Jaguar-powered prototype. Aside from the engine change, Major Green redesigned it with an all-metal structure, as the Siskin III. The all-metal Siskin was the start of the British transition to metal for military aircraft.

Into Production

On 13 October 1922, an initial contract for three production aircraft was placed, and a follow-on order for a further six followed on 26 January 1923, including a single two-seat variant. The Siskin III made its first flight on 7 May 1923. A comprehensive evaluation was conducted, during which the ailerons were tapered to prevent them jamming, as happened during one test flight. Shortly thereafter, Armstrong Whitworth commenced construction of the production standard Siskin, the first of which were delivered to the Royal Air Force (RAF) in January 1924 for flight trials on No. 41 Squadron. The fighter was constructed with a composite wood and aluminum frame, covered in doped linen fabric.

Following the orders from the RAF, Armstrong Whitworth worked on securing export sales for the Siskin. Siskin sales played a major role in the company's fortunes for a time. Romania ordered 65 aircraft, but cancelled the order following a fatal accident at Whitley Abbey, Coventry on 18 February 1925 when a Romanian pilot died in a crash on takeoff, during acceptance tests. Political pressure by France may have also contributed to the order's cancellation however.

The Siskin IIIA was the main production version, which was first ordered during 1926, and was the first all-metal framed aircraft to be procured in quantity for the RAF. This variant was to have been powered with a Jaguar IV, but was given a supercharged Jaguar IVA engine instead. The supercharger had little effect on performance below 10,000 ft (3,000 m), but greatly improved speed and climb above that height. The Royal Canadian Air Force received 12 IIIAs between 1926 and 1931 after evaluating two Siskin IIIs.

Early production examples were built by Armstrong Whitworth but due to production demands for the Atlas, some Siskin IIIA production was subcontracted out to Blackburn, Bristol, Gloster, and Vickers.

Operational History

Royal Air Force

During May 1924, the RAF's first Siskin IIIs were delivered to No. 41 Squadron at RAF Northolt. Shortly thereafter, No. 111 Squadron also received the model; its adoption enabled No. 111 to become the RAF's first high-altitude fighter squadron. The Siskin III was relatively popular amongst its pilots, being a highly maneuverable aircraft, although slightly underpowered. Between 1925 and 1931, Siskins were frequently presented at RAF exhibitions of flying; one particular feat performed was the linking of three aircraft by cords between their interplane struts, necessitating careful formation flying to not break these cords until the finishing maneuver was performed.

During September 1926, the first deliveries of the improved Siskin IIIA variant were made to No. 111 Squadron. In total, the Siskin was operated by eleven RAF squadrons. By 1931, the type was showing its age, leading to the Air Ministry considering either to recondition them or to procure new-built fighters to replace them. During October 1932, the final Siskins in RAF service were withdrawn, the type having been replaced by the newer and more capable Bristol Bulldog.

Sweden

The second Siskin II aircraft was sold to the Royal Swedish Air Force in 1925. It was equipped with skis and flown in an experimental capacity for a time.

Canada

Between 1926 and 1939, Canada operated a sizable fleet of Siskins. During 1926, the British Air Ministry had dispatched a pair of Siskin IIIs to Canada, where they underwent testing by the Royal Canadian Air Force (RCAF) under winter flying conditions by test pilot Clennell H. Dickins. The Siskin was considered a modern type at the time of its acquisition by the RCAF, which opted to purchase the Mark IIIA. The Canadian procurement involved both new-built aircraft and second-hand RAF Siskins being supplied to numerous RCAF squadrons.

The Siskin equipped the Fighter Flight at Camp Borden and Trenton. During 1937, the Flight became No. I (Fighter) Squadron, and was transferred from Trenton to Calgary in August 1938. RCAF Siskins were also frequently used in aerial displays and long distance tours around North America.

The unit continued to operate the Siskin up until the outbreak of the Second World War, shortly after which the type was rapidly retired and replaced by Hawker Hurricane monoplane fighters. Following the Siskin's withdrawal by the RCAF, the airframes were turned over to various technical establishments for use as instructional airframes.

Like its RAF counterparts, in 1929, a three-plane Siskin air demonstration team was formed at Camp Borden, Ontario – the RCAF's first official flight demonstration team. The aerobatic team put on popular solo and formation displays from coast to coast.

Air Racing

The Siskin frequently participated in air racing, often triumphing in such events. Multiple examples were entered into the 1924 King's Cup air race, one of which achieving the fastest course time despite arriving fourth. In the 1925 King's Cup, a Siskin V flown by Flight Lieutenant Barnard emerged as the winner, having reportedly achieved a speed in excess of 151 mph (243 km/h).

Variants

Siddeley Deasy S.R.2 Siskin: Prototype fighter aircraft built by Siddeley-Deasy and powered by Dragonfly engine. Three built.

Siskin II: fabric covered steel-tube fuselage and wooden wings. Two built, one two-seater and one single-seater.

Siskin III: all-metal production version (64 built for RAF)

Siskin IIIA: main production variant ordered in 1926 (Total 348 built, 340 for RAF, eight for RCAF)

Siskin IIIB: prototype with improved engine. Single example converted from Siskin IIIA.

Siskin IIIDC: two-seat dual control version (Total 53 built, 47 for RAF, two for RCAF, two for AST, two for Estonia) a further 32 were converted from Siskin IIIs.

Siskin IV: civil racing version (one built)

Siskin V: single-seat fighter for Romania. 65 ordered and at least 10 completed before order cancelled. Two used for racing.

Operators

Military Operators

Canada

Royal Canadian Air Force

Fighter Flight

No. 1 Squadron (1937–1939)

Siskins Aerobatic team (1929–1932)

Estonia

Estonian Air Force - operated two Siskin IIIDCs from 1930 to 1940.

Sweden

Royal Swedish Air Force

United Kingdom

Royal Air Force

No. 1 Squadron

No. 17 Squadron

No. 19 Squadron

No. 25 Squadron

No. 29 Squadron

No. 32 Squadron

No. 41 Squadron

No. 43 Squadron

No. 54 Squadron

No. 56 Squadron

No. 111 Squadron

Civil Operators

United Kingdom

Air Service Training

General Information

Type: Fighter

Manufacturer: Sir W.G. Armstrong Whitworth Aircraft Limited

Designer: F.M. Green

Primary users:

Royal Air Force

Royal Canadian Air Force

Royal Swedish Air Force

Number built: 485

Introduction date: 1923

First flight: May 1919 as Siddeley-Deasy S.R.2 Siskin

Retired: 1932

Variants: Armstrong Whitworth Starling

Specifications (Siskin IIIA)

Crew: 1

Length: 25 ft 4 in (7.72 m)

Wingspan: 33 ft 2 in (10.11 m)

Height: 10 ft 2 in (3.10 m)

Wing area: 293 sq ft (27.2 m2)

Empty weight: 2,061 lb (935 kg)

Max takeoff weight: 3,012 lb (1,366 kg)

Powerplant: 1 × Armstrong Siddeley Jaguar IV 14-cylinder air-cooled radial piston engine, 385 hp (287 kW)

Propellers: 2-bladed fixed-pitch propeller

Maximum speed: 156 mph (251 km/h, 136 kn) at sea level

Range: 280 mi (450 km, 240 nmi)

Endurance: 72 minutes

Service ceiling: 27,000 ft (8,200 m)

Rate of climb: 2,953 ft/min (15.00 m/s)

Time to altitude: 10,000 ft (3,000 m) in 7 minutes and 5 seconds

Guns: Two × 0.303 in (7.7 mm) Vickers machine guns

Bombs: Four × 20 lb (9.1 kg) bombs under-wing

Bibliography

Angelucci, Enzo. World Encyclopedia of Military Aircraft. London: Jane's Publishing, 1981.

Dempsey, Daniel V. A Tradition of Excellence: Canada's Airshow Team Heritage. Victoria, BC: High Flight Enterprises, 2002.

Donald, David (ed.). The Encyclopedia of World Aircraft. London: Aerospace Publishing, 1997.

Gerdessen, F. "Estonian Air Power 1918 – 1945". Air Enthusiast, No. 18, April – July 1982. pp. 61–76.

Gunston, Bill. World Encyclopaedia of Aero Engines. Book Club Associates, 1986

Jackson, A.J. British Civil Aircraft since 1919, Volume 1. London: Putnam, 2nd Edition, 1973.

Lumsden, Alec. "On Silver Wings — Part 5". Aeroplane Monthly, February 1991, Vol 19 No 2, Issue 214. pp. 72–78.

Mason, Francis K. The British Fighter Since 1912. Annapolis, Maryland: Naval Institute Press, 1992.

Meekcoms, K J and Morgan, E B. The British Aircraft Specification File. Tonbridge, Kent, UK: Air-Britain, 1994.

Milberry, Larry. Aviation in Canada. Toronto: McGraw-Hill Ryerson Limited, 1979.

Milberry, Larry. 60 Years: The RCAF and CF Air Command 1924–1984. Toronto: Canav Books, 1984.

Ritchie, Sebastian (1997). Industry and Air Power The Expansion of British Aircraft Production 1935-1941. Routledge Taylor and Francis Group.

Tapper, Oliver. Armstrong Whitworth Aircraft since 1913. London:Putnam, 1988.

Thetford, Owen. "On Silver Wings — Part 6". Aeroplane Monthly, March 1991, Vol 19 No 3, Issue 215, pp. 138–144. London: IPC.

 

The Siskins aerobatic team. The Royal Canadian Air Force's first flight demonstration/aerobatic team, 1932. (Royal Canadian Air Force photo)

Armstrong Whitworth Siskin III, J7147, construction no. 31, issued to No. 41 Squadron on 7 May 1924. It was destroyed in a flying accident on 9 October 1924. (SDASM Archives)

29 Squadron Siskin lineup, late 1920s. (RAF photo)

RCAF Siskin IIIDC, circa 1937 (PAC Photo).

RAF Armstrong-Whitworth Siskin IIIa from No. 41 Squadron at Northolt being serviced with oxygen, circa 1920s. (RAF photo)

 Armstrong-Whitworth Siskin IIIA RCAF 21 Training Squadron, B Flight, Camp Borden, Ontario. (SDASM Archives)

Armstrong Whitworth Siskin on skis. (Photo from L'Aéronautique, 1 April 1929)

Armstrong-Whitworth Siskins at Leaside aerodrome. (City of Toronto Archives, listed under the archival citation Fonds 1244, Item 4512)

 Armstrong-Whitworth Siskin Mark III, serial number J7178, at an airfield in Egypt during tropical trials, June-December 1925. (Imperial War Museum photo HU 70791)

Armstrong-Whitworth Siskin Mk.II.

 

Avro Tutor: British Basic Trainer

Avro Tutor, RCAF, s/n 185, circa 1934. (SDASM Archives)

The Avro Type 621 Tutor is a two-seat British radial-engined biplane from the interwar period. It was a simple but rugged basic trainer that was used by the Royal Air Force as well as many other air arms worldwide.

Design and Development

The Avro Model 621 was designed by Roy Chadwick as an Avro private venture metal replacement for the Avro 504. Conceived as a light initial pilot trainer, the biplane design featured heavily staggered equal-span, single-bay wings; the construction was based on steel tubing (with some wooden components in the wing ribs) with doped linen covering. A conventional, fixed divided main undercarriage with tailskid was used in all but the latest aircraft, which had a tailwheel.

The Model 621 was powered either by a 155 hp (116 kW) Armstrong Siddeley Mongoose or Armstrong Siddeley Lynx IV (180 hp/130 kW) or IVC (240 hp/179 kW) engine; later Lynx-powered models had the engine enclosed in a Townend ring cowling. The Mongoose-powered version was called the 621 Trainer and the more numerous Lynx-engined aircraft the Tutor. The Tutor also differed by having a more rounded rudder.

The first flight of the prototype G-AAKT was in September 1929, piloted by Avro chief test pilot Captain Harry Albert "Sam" Brown.

Operational History

Production was started against an order for three Tutors from the Irish Free State and 21 Trainers from the Royal Air Force. The RAF required a replacement for the wooden Avro 504, and after three years of trials against other machines such as the Hawker Tomtit it was adopted as their basic trainer, supplanting the 504 in 1933 and remaining in this role until 1939. As well as the first batch of 21 Trainers, a total of 381 Tutors and 15 Avro 646 Sea Tutors were eventually ordered by the RAF. RAF units to operate the type in quantity included the Royal Air Force College, the Central Flying School and Nos. 2, 3, 4 and 5 Flying Training Schools.

Subsequently, the Model 621 achieved substantial foreign sales. A.V. Roe and Co exported 29 for the Greek Air Force, six for the Royal Canadian Air Force, five for the Guangxi AF, three for the Irish AF (where it was known as the Triton) and two for each of the South African and Polish AFs. In addition 57 were license-built in South Africa, and three license-built by the Danish Naval Shipyard.

A total of 30 Tutors were exported to the Greek Air Force and at least 61 were license-built in Greece by KEA. A number of Greek Tutors was incorporated in combat squadrons after Greece's entrance in WWII, used as army cooperation aircraft.

Known for its good handling, the type was often featured at air shows. Over 200 Avro Tutors and five Sea Tutors remained in RAF service at the beginning of the Second World War.

The 621 was designed as a military trainer and few reached the civil registers. In the 1930s, in addition to ten prototypes and demonstrators, two were used by Alan Cobham's Flying Circus and two trainers were retired from the RAF into private use. One 621 was used from new by Australian National Airways. After the war another four ex-RAF 621s appeared on the civil register.

Variants

Avro 621 Trainer (Mongoose powered): Two-seat primary training aircraft.

Avro 621 Tutor (Lynx powered): Two-seat primary training aircraft.

Avro 621 Tutor II: One aircraft was modified into a two-bay biplane.

Avro 623: Three-seat version of the Type 621 Tutor upgraded for use in Tanganyika as aerial survey aircraft. Three were built between May and December 1930 and issued to the Director of Surveys of Tanganyika. Powered by a 240 hp Armstrong-Siddeley Lynx IV.

Avro 646 Sea Tutor: Two-seat seaplane fitted with twin floats, 15 built

PWS-18: Polish-built license version with 200 hp (150 kW) Wright J-5 engine. 40 built 1935–36. Still in service with Polish Air Force in 1939.

Operators

Czechoslovakia: Czechoslovak Air Force pilots operated at least one aircraft in 310 Fighter Squadron RAF.

Denmark: Royal Danish Navy operated five aircraft.

Canada: Royal Canadian Air Force operated six aircraft.

China: Chinese Nationalist Air Force (Kwangsi Airforce) operated five aircraft.

Iraq: Iraqi Air Force operated three aircraft.

Ireland: Irish Air Corps operated three aircraft.

Greece: Hellenic Air Force operated about 90 aircraft.

Poland: Polish Air Force received two aircraft from Avro, plus 40 from PWS.

South Africa: South African Air Force operated 60 aircraft.

United Kingdom:

Royal Air Force received 417 aircraft.

Royal Navy Fleet Air Arm

Surviving Aircraft

G-AHSA was used for communication duties during the Second World War, struck off December 1946 and purchased by Wing Commander Heywood. After suffering engine failure in the early stages of the filming of Reach for the Sky, it was purchased by the Shuttleworth Collection and restored to flying condition.

Up to the end of 2003, G-AHSA was still flying as K3215 in RAF trainer yellow. Since January 2004 it has flown painted as K3241 in the colors of the Central Flying School. (The real K3241 built in 1933, served RAF College Cranwell, until transferred to the CFA in 1936.)

General Information

Type: Trainer

National origin: United Kingdom

Manufacturer: Avro

Designer: Roy Chadwick

Primary user: Royal Air Force

Number built: 606

Introduction date: 1933

First flight: September 1929

Retired: 1941

Variants:

Avro 626

PWS-18

Specifications (Tutor)

Crew: 2

Length: 26 ft 4.5 in (8.039 m)

Wingspan: 34 ft 0 in (10.36 m)

Height: 9 ft 7 in (2.92 m)

Wing area: 301 sq ft (28.0 m2)

Empty weight: 1,844 lb (836 kg)

Gross weight: 2,493 lb (1,131 kg)

Powerplant: 1 × Armstrong Siddeley Lynx IVC 7-cylinder air-cooled radial piston engine, 240 hp (180 kW)

Propellers: 2-bladed fixed-pitch propeller

Maximum speed: 120 mph (190 km/h, 100 kn)

Cruise speed: 97 mph (156 km/h, 84 kn)

Range: 250 mi (400 km, 220 nmi)

Service ceiling: 16,000 ft (4,900 m)

Rate of climb: 910 ft/min (4.6 m/s)

Bibliography

Cynk, Jerzy B. (1971). Polish Aircraft 1893–1939. London: Putnam.

Halley, J.J. (1976). Royal Air Force Aircraft K1000 to K9999. Tonbridge, Kent, UK: Air-Britain (Historians) Ltd.

Jackson, A.J. (1990). Avro Aircraft since 1908 (2nd ed.). London: Putnam Aeronautical Books.

Jenks, Roy (March 1979). "RAF Piston Trainers: No. 4: Avro Tutor". Aeroplane Monthly. Vol. 7, no. 3. pp. 142–147.

Thetford. O. (1957). Aircraft of the Royal Air Force 1918–57. London: Putnam.

Vančata, Pavel (2006). "Cechoslováci v zahraničním odboji". Revi (bi-monthly magazine) (in Czech). No. 65. Ostrava-Poruba: REVI Publications.

 

Avro Tutor, 21 May 1937. (RAF photo)

The sole surviving Tutor wearing the 1930s yellow training color scheme at RAF Abingdon in 1968. (Ruth AS, 15 June 1968)

Avro Tutor of Shuttleworth collection 7 September 2008. G-AHSA was used for communication duties during the Second World War, struck off December 1946 and purchased by Wing Commander Heywood. After suffering engine failure in the early stages of the filming of Reach for the Sky, it was purchased by the Shuttleworth Collection and restored to flying condition. Up to the end of 2003, G-AHSA was still flying as K3215 in RAF trainer yellow. Since January 2004 it has flown painted as K3241 in the colors of the Central Flying School. (The real K3241 built in 1933, served RAF College Cranwell, until transferred to the CFA in 1936.) (TSRL, 9 September 2008)

Avro Tutor ‘K3241’ (G-AHSA). Owned and operated by the Shuttleworth Collection. Her actual military serial is 'K3215'. Seen displaying at the collections Evening Airshow, Old Warden Aerodrome, Bedfordshire, UK. (Alan Wilson, 17 June 2017)

Avro 621 Trainer 3-view drawing from NACA Aircraft Circular No.119, 1 June 1930. ( NACA Aircraft Circular)

Avro 621 Trainer photo from NACA Aircraft Circular No.119, 1 June 1930. (NACA Aircraft Circular)

Avro 621 Trainer photo from NACA Aircraft Circular No.119. (NACA Aircraft Circular)

Avro 621 Tutor of the Hellenic air force. The British Avro 621 Tutor was chosen as the basic training airplane in the Hellenic Air Force reconstitution program in the period between 1936 and 1940, prevailing in a competition held by the Ministry of Air Force in 1935, with the D.H. Moth II being the second choice. Thirty British-built airplanes were delivered in 1936 and 62 more were to be domestically produced. In December of 1939 59 Avro 621 were available, while 30 more airplanes were under production at the State Airplane Factory, the production line pace being about seven airplanes per month. In documents of this period is noted that many training squadrons were “under composition”, waiting for their airplanes to be delivered. Many of them were re-fitted to be able of inverted flight, while others were equipped with night illumination instruments or target towing equipment. Their use also included acrobatics training, night flying and weapons training. A small number of Avro 621 Tutor was incorporated to the combat squadrons at the outbreak of WWII, where they undertook liaison airplane duties. At least 4 Avro 621 escaped to Egypt. 

Avro 621 Tutor, RCAF Station Rockcliffe, Ontario, 19 September 1939. (Library and Archives Canada Photo, MIKAN No. 3581425) 

Avro 621 Tutor, s/n 188, of No. 110 (AC) Squadron, Ottawa, Ontario, 19 September 1939.  (Library and Archives Canada Photo, MIKAN No. 3642468)

Avro 621 Tutor, RCAF s/n 186, Camp Borden, Ontario. (Barrie Historical Archive)

Avro Tutor, DH-60GM Moths, serial numbers 155, 152 and 154, Fleet Fawn Mk. I, serial number 203, Avro Tutor, serial number 187, 3 September 1937.  (Library and Archives Canada Photo, MIKAN No. 3199002)

Avro 621 Tutor, RCAF, serial number 187, No. 111 (CAC) Squadron, RCAF Station Rockcliffe, Ontario, 9 June 1939.  (Library and Archives Canada Photo, MIKAN No. 3198994)

Avro 621 Tutor, serial number 188. 188 was first used for pilot training at Camp Borden. To Ottawa Car on 24 February 1932, unknown duration or reason. With the Test and Development Flight at RCAF Station Rockcliffe, Ontario, dates not known. To Armstrong Siddeley in Canada for reconditioning, 3 May 1936 to 13 November 1937, at a cost of $7,227.67. Had 421:00 logged time when it arrived. To Rockcliffe when completed, acceptance test flown by Test & Development Flight on 15 September 1939. To No. 110 (AC) Squadron (Auxiliary), from De Lesseps Aerodrome, Weston, Ontario on 21 September 1939. Category B crash in Weston, at 13:40 on 11 December 1938. To Ottawa Car for crash repairs, 17 January 1939 to 16 September 1939, at a cost of $2,892.26. Had 495:50 logged time when it arrived. To RCAF Station Ottawa when completed. Became Instructional Airframe A 32 on 11 July 1940. Used at No. 1 Technical Training School at St. Thomas, Ontario.  (Library and Archives Canada Photo, MIKAN No. 3580691)

Avro 621 Tutor, serial number 188.  (Library and Archives Canada Photo, MIKAN No. 3580690)

Avro 621 Tutor, serial number 188.  (Library and Archives Canada Photo, MIKAN No. 3580919)

Avro 621 Tutor, serial number 188.  (Library and Archives Canada Photo, MIKAN No. 3580920)

Avro 621 Tutor, RCAF No. 7 Squadron, P/O Stuart and P/O Reeves, 31 July 1939.  (Library and Archives Canada Photo, MIKAN No. 3581401) Avro Tutor, RCAF (Serial No. 189) was first used for pilot training at Camp Borden. To Armstrong Siddeley in Canada for "all mods", 7 May 1936 to 30 October 1937, at a cost of $7,551.27. Had 645:17 logged time when it arrived. To Rockcliffe for rigging when completed, then to No. 7 (GP) Squadron at RCAF Station Ottawa. Probably with No. 10 (AC) Squadron (Auxiliary) at Weston after this, but not confirmed. Took part in summer exercises at Camp Borden, Ontario, 1938. To Ottawa Car for further work, 13 December 1938 to 31 May 1939, at a cost of $2,961.28. Had 861:37 total time when it arrived. To RCAF Station Ottawa when completed. To No. 110 (AC) Squadron (Auxiliary), from De Lesseps Aerodrome, Weston, Ontario, also on 31 May 1939. To the Technical Training School at St. Thomas, Ontario on 9 January 1940. Became Instructional Airframe A 33 on 11 July 1940. 

Avro 621 Tutor (serial number 224), A 45, c/n 463, Reg. No. CF-ANQ, new trainer. Registration issued to Armstrong-Siddeley Motors Ltd. of Ottawa on 8 June 1930. Evaluated by RCAF in August 1930, had Mongoose engine at that time. Later received Lynx engine. Purchased by RCAF in 1937, became their serial number 224Also reported as a Model 626. Registration CF-ANQ used for trials before delivery to RCAF. Operated by No. 12 (AC) Squadron (No. 112 (AC) Sqn. (Aux.) from 15 November 1937), Winnipeg, Manitoba, 1937 to 1940. Later became Instructional Airframe A 45. (Library and Archives Canada Photo, MIKAN No. 3580451)
 
Avro 621 Tutor, serial number K3225. 

Avro 621 Tutor cockpit.

Avro Tutor, Hellenic air force, serial number E.59.

Avro Tutor, serial number K4798.

Avro Tutor, serial number K3215.

Tutor K3249 was built to contract 195190/32 by A.V.Roe & Co. Ltd. at Newton Heath, Chadderton and was delivered to Kenley on 15 May 1933. After being accepted for RAF service at Kenley it was taken on charge on 24 October 1933 by 5 FTS at Sealand. It was also allocated to 2 FTS but this allocation was not taken up. On 1 May 1936 it was transferred to 16 Squadron at Old Sarum and on 18 June 1937 it was transferred to the Station Flight at Debden. On 11 November 1937 it was transferred to the Station Flight at Aldergrove with whom it was still on the books with when the landing at Coniston took place on 8 March 1938. The following day it is listed as being transferred to H.Q.P. (Headquarters Pool) at Catterick but there is no indication of whether it was flown there or transported by road but it seems that it is likely that it was simply flown from Coniston to Catterick as there is no indication of the aircraft as having to be repaired in the published history of the aircraft. It appears to have remained at Catterick and on 14 September 1939 it was taken on charge by 609 Squadron at Catterick, it was then transferred to 219 Squadron also at Catterick on 10 October 1939 and was used as a run about aircraft for both 609 and 219 Squadrons. On 1 March 1940 it ran out of fuel and collided with a hedge in a forced landing at Rugeley, Staffordshire. Following the mishap on 1 March 1940 it was deemed beyond repair and was struck off charge. 

Avro Tutor, serial number K3244, at 23 Elementary and Reserve Flying Training School, Rochester, UK.

Avro 646 Sea Tutor, serial number K3372, RAF.

Avro Tutor, serial number 113, Danish air force.