Sopwith Triplane Typhoon

Avro 652 and 652A Anson

The Type 652A Anson was produced in more numbers than any other Avro Type. This page just summarises the specification details and production totals for each variant, along with production totals for the various manufacturers.
For full production details of each variant, follow the links below.

For Production Tables of Type 652A Anson Military Variants see here.
For Production Tables of Type 652A Anson Civil Variants see here.

Contents

Type Description
Projected Variants

Type Description

  • Type 652
  • Low wing monoplane light transport to meet an Imperial Airways specification for a light airliner to transport four passengers for up to 420 miles. The fuselage was a box beam of welded steel tubes, fabric covered over spruce formers and stringers to a more rounded shape. The nose forward of the cockpit was an all light alloy monocoque structure, as were the engine nacelles back to the main spar. The one piece monoplane wing, of plywood and spruce construction with plywood covering, followed Avro's earlier adaption of Fokker's construction methods. The tailplane was also of plywood and spruce construction, with plywood covering. The rudder of the second prototype originally featured a horn balance, but this was later replaced by the mass balanced rudder similar to the first prototype. Each passenger was provided with a large rounded cabin window and cabin access was via a large door on the port aft side, a toilet being located to the aft starboard side. A mail/luggage compartment was located in the nose, the duralumin nose cone being hinged for access. The main undercarriage members, hand cranked, retracted forward into the engine nacelles, leaving the mainwheel projecting slightly underneath the engine cowling when fully retracted. Two 270 h.p. Armstrong Siddeley Cheetah V powerplants.
Type 652 Specification
Span Length Height Wing Area Empty Wt Max AUW Cruise Speed Maximum Speed Range Service Ceiling
56 ft 6 in 42 ft 3 in 13 ft 1 in 463 sq ft 5100 lb 7400 lb 165 mph/ 143 kn 175 mph/ 152 kn 790 mi 21500 ft
17.22 m 12.88 m 3.99 m 43.01 m2 2313 kg 3357 kg 266 km/h 282 km/h 1271 km 6553 m

  • Type 652 Mk.II
  • A variant for the Egyptian Government, it maintained the Type 652 fuselage but with glazed cockpit roof and a single long rectangular cabin window on each side. The wing, with smaller nacelles and close cowled engines, was almost Identical to the Anson I. Two 310 h.p. Armstrong Siddeley Cheetah IX powerplants.
  • Type 652A Anson Mk.I
  • Coastal patrol or trainer derivative of Type 652 to Specification 18/35 to meet the requirements of OR.23 for a General Coastal Reconnaissance Aircraft and manufactured under Specifications 16/37 and 34/37. Similar to the Type 652, the prototype featured rectangular cabin windows in place of the earlier type's rounded type, with the entry door moved to the starboard side, a horn balanced rudder and a gunners position in the upper fuselage above the main spar, fitted with a single Lewis machine gun in an Armstrong Whitworth turret. The roof line was slightly lower than the Type 652 and whereas that of the Type 652 was gracefully curved, that of the Anson was nearer a constant depth over the main cabin area, then featuring a distinct drop in line as it transitioned to a narrower rear fuselage. A crew of three was carried: pilot, wireless operator/gunner and navigator/bomb aimer, who could use a sliding panel in the extreme nose for his bomb aiming duties. A bomb load of 360 lb could be carried under the centre section, and the pilot was provided with a Vickers machine gun on the port side. The prototype was fitted with two 295 h.p. Armstrong Siddeley Cheetah VI powerplants in close fitting lobed cowlings with smaller diameter nacelles than the Type 652.
    Production aircraft differed slightly from the prototype, with a higher, continuous line of cabin windows, a mass balanced rudder and larger span tailplane. Starting with Contract 766119/38, the cockpit glazing was revised, with a flatter windscreen and the addition of roof glazing, along with the addition of metal framed ailerons and the hydraulically operated Schrenk flaps. Two 350 h.p. Armstrong Siddeley Cheetah IX or, from serial NL121, 395 h.p. XIX powerplants, the later aircraft featuring larger diameter, cylindrical, cowlings to prevent overheating.
    313 Anson Mk.Is Trainers supplied to Air Gunnery Schools were fitted with the Bristol B.1 Mk.VI turret, hydraulically operated by electric motors under the floor.

Type 652A Anson Mk.I Specification
Span Length Height Wing Area Empty Wt Max AUW Cruise Speed Maximum Speed Range Service Ceiling
56 ft 6 in 42 ft 3 in 13 ft 1 in 463 sq ft 5375 lb 7665 lb 158 mph/ 137 kn 188 mph/ 163 kn 660 mi 19000 ft
17.22 m 12.88 m 3.99 m 43.01 m2 2438 kg 3477 kg 254 km/h 303 km/h 1062 km 5791 m

  • Type 652A Anson Mk.II
  • Canadian built trainer. As Mk.I trainer but with reduced cabin glazing, redesigned and hydraulically operated main undercarriage and a Vidal moulded plywood veneer nose. Two 330 h.p. Jacobs L-6MB R-915 powerplants.
  • Type 652A Anson Mk.III
  • Canadian conversion of British built Anson Mk.I trainers fitted with two 330 h.p. Jacobs L-6MB R-915 powerplants.
  • Type 652A Anson Mk.IV
  • Canadian conversion of British built Anson Mk.I trainers and Canadian Mk.III's fitted with two 300 h.p. Wright Whirlwind R-760-E1 powerplants.
  • Type 652A Anson Mk.V
  • Canadian built navigation trainer fitted with a new fuselage and fin of Vidal moulded plywood, the remaining structure being as the Mk.II. Three round windows were fitted each side of the cabin, with an astrodome in the roof for navigational training and a glazed nose cap for bomb aimer training. The inner wing spars each contained a bomb bay with capacity for four light bombs each, with provision for eight further bombs under the fuselage. Two 450 h.p. Pratt and Whitney Wasp Junior R-985-AN12B powerplants.
  • Type 652A Anson Mk.VA
  • Early Mk.V aircraft built using Mk.II components.
  • Type 652A Anson Mk.VP
  • Mk.V modified for photographic reconnaissance. Internally, the fuselage was capable of being fitted out with vertical or oblique cameras.
  • Type 652A Anson Mk.VI
  • Gunnery training variant of Mk.V fitted with the Bristol B.1 Mk.VI turret.
  • Type 652A Anson Mk.X
  • Military transport. Mk.I with strengthened floor.
  • Type 652A Anson Mk.XI
  • Navigation trainer and light transport to meet the requirements of OR.141 and OR.143. New fuselage structure with raised roof, three new, square, windows per side and a hydraulically operated undercarriage. The cabin access door was relocated to the port side. Several were completed as ambulances with hinged wing root fillets on the port side to allow stretchers to be pushed into the cabin. Two 395 h.p. Armstrong Siddeley Cheetah XIX powerplants.
  • Type 652A Anson Mk.XII
  • As Mk.XI fitted with two 420 h.p. Armstrong Siddeley Cheetah XV powerplants and Rotol constant speed propellers.
  • Type 652A Anson Mk.18
  • General purpose variant of Avro 19 Series 2 with two 420 h.p. Armstrong Siddeley Cheetah XVII powerplants.
  • Type 652A Avro 19
  • (Also known as the Avro XIX, carrying on the pre-war civil naming series that ended at the Type 642 Avro Eighteen): 9 seat civil transport variant of Mk.XII featuring oval windows, to satisfy the Brabazon feeder liner specification of 1944. Series 1 aircraft featured wooden wings, those of the Series 2 were metal and of one foot greater span, along with a metal tailplane. Two 420 h.p. Armstrong Siddeley Cheetah XV powerplants.

Type 652A Avro 19 Series 2 Specification
Span Length Height Wing Area Empty Wt Max AUW Cruise Speed Maximum Speed Range Service Ceiling
56 ft 6 in 42 ft 3 in 13 ft 10 in 440 sq ft 6576 lb 10400 lb 149 mph/ 129 kn 171 mph/ 149 kn 660 mi 16000 ft
17.22 m 12.88 m 4.22 m 40.88 m2 2983 kg 4717 kg 240 km/h 275 km/h 1062 km 4877 m

  • Type 652A Anson Mk.XIX
  • (Later C.Mk.19) RAF communications and transport version of the Avro 19.
  • Type 652A Anson T.20
  • General purpose trainer version of the C.Mk.19 Srs.2 for Southern Rhodesia to Specification T.24/46 to meet the requirements of OR.212. It was fitted with a transparent nose for the bomb aimer and bomb racks to carry sixteen practice bombs were fitted under the fuselage and inner winner wings. An astrodome was located over the forward cabin in place of the forward roof window.
  • Type 652A Anson T.21
  • Navigational trainer version of the C.Mk.19 Srs.2 to Specification T.25/46 to meet the requirements of OR.212. Similar to the T.Mk.20 but without the bombing equipment and transparent nose.
  • Type 652A Anson T.22
  • Radio trainer version of the C.Mk.19 Srs.2 to Specification T.26/46 to meet the requirements of OR.224. It lacked the astrodome of the T.20 and T.21.
  • Federal AT-20
  • Designation of the Anson Mk.II in USAAF service.

Projected Variants

  • Type 652A Anson
  • Convertible civil/military variant for the SAAF to Specification 33/35.
  • Type 652A Anson
  • Trainer variant of the Type 652A to Specification 3/36.
  • Type 652A Anson
  • Flying classroom to meet the requirements of Specification T.3/49.
  • Type 652A Anson Mk.VII
  • Reserved for Canadian variant. Not used.
  • Type 652A Anson Mk.VIII
  • Reserved for Canadian variant. Not used.
  • Type 652A Anson Mk.IX
  • Reserved for Canadian variant. Not used.
  • Type 652A Anson Mk XIII
  • Turreted gunnery trainer powered by two Cheetah XI or XIX powerplants.
  • Type 652A Anson Mk XIV
  • Turreted gunnery trainer powered by two Cheetah XV powerplants.
  • Type 652A Anson Mk XV
  • Navigation trainer.
  • Type 652A Anson Mk XVI
  • Bombing trainer.


Total Type 652 Production
Type Built New Conv Canc'd Total
 Type 652 2 2
 Type 652 Mk.II 1 1
3 (0) 0

Total Type 652A Anson and Avro 19 Production By Mark
Type Built New Conv Canc'd Total
 Anson Mk.I (see note 4) 6989 (2) 200 7191
 Anson Mk.II 1832 1832
 Anson Mk.III (156) 156
 Anson Mk.IV (168) 168
 Anson Mk.V 972 (1) 973
 Anson Mk.VA 77 77
 Anson Mk.VI 1 1
 Anson Mk.X 103 (17) 121
 Anson Mk.XI 90 600 690
 Anson Mk.XII 264 264
 Anson Mk.18 12 (1) 13
 Anson Mk.18C 12 12
 Anson Mk.XIX/C.19 Series 1 115 532 647
 Anson Mk.XIX/C.19 Series 2 183 (7) 100 290
 Avro 19 Series 1 11 (4) 15
 Avro 19 Series 2 12 (13) 25
 Anson T.20 60 25 85
 Anson T.21 252 37 289
 Anson C.21 (27) 27
 Anson T.22 34 11 45
11019 (396) 1505

Type 652A Anson - UK Production
Military Variants By Mark and Manufacturer
Constructor Mk.I Mk.X Mk.XI Mk.XII Mk.18 Mk.XIX Srs.1 Mk.XIX Srs.2 T.20 T.21 T.22 Total
 Avro, Newton Heath (1) 4759 4759
 Avro, Yeadon (1) 2230 103 90 264 115 26 2828
 Avro, Chadderton 12 157 60 252 34 515
6989 103 90 264 12 115 183 60 252 34 8102
Air Ministry Contracts Associated With Anson Production
Contract Requisition Production Spec (5)
[26][27]
Total Remarks
352855/34 1
421119/35 57/35 18/35 162 12 aircraft transferred to 427630/35 for Australia
427630/35 38 To Australia
497338/36 128/35 3/36 78 26 aircraft transferred to 427630/35 for Australia
497339/36 129/35 18/35 35 39 less 3 aircraft transferred to Finland, 1 to Estonia
633200/37 3/37 16/37P 28
690658/37 118/37 34/37 88 10 aircraft transferred to 748829/38 for Australia
748829/38 10 To Australia
766119/38 57/38 I/P4 832 850 less 12 to Greece, 6 to Turkey.
766229/38 (I/P7) 0 Cancelled
B12565/39 57/38 (I/P5) 200
B20357/39 1/E1/39 (I/P6) 255
B32842/39 1/E1/39 (I/P6) 45
B61695/39 4/E1/39 (I/P8) 1000
B137211/40 4/E1/40 (I/P8) 4400
Acft/3077 XI ard XII/P1 267 268 less 1 aircraft transferred to Contract Acft/5615 for Misrair, Egypt.
Acft/5037 XI ard XII/P1 138 161 less 23 direct to civil :
3 To Misrair SAE, Almaza, Egypt, under Contract Acft/5615
2 To the Imperial Ethiopian Air Force, under Contract Acft/5691
14 To Railway Air Services, Speke, under Contract Acft/5819.
4 To Ministry of Civil Aviation, under Contract Acft/5986
Acft/5615 5 To Misrair, Egypt, 1 ex Acft/3077, 3 ex Acft/5037 plus PH806.
Acft/5680 XI ard XII/P1 (Mk.XIX)
T.24/46 (T.20)
93 2 aircraft transferred to 6/Acft/923 - See Note 13
Acft/5691 2 To Ethiopian Air Force
Acft/5819 14 Civil Contract, Railway Air Services
Acft/5986 5 Civil Contract, Ministry of Civil Aviation (4 ex-Acft/5037 plus 1 new)
Acft/6103 XI ard XII/P1 29 VP511 taken from RAF contract and became the prototype Mk.18
6/Acft/811 T.24/46 (T.20)
T.25/46 (T.21)
T.26/46 (T.22)
90
6/Acft/923 2 Prototype T.20 and T.22 - See Note 13
6/Acft/1019 T.25/46, T.26/46 80
6/Acft/1396 T.24/46, T.25/46 92
6/Acft/1595 2 To Southern Rhodesia for locust control
6/Acft/2084 1 G-AKUD, ex VM373, to A&AEE for locust control tests
6/Acft/2473 T.25/46 20
6/Acft/3634 T.25/46, T.26/46 25
B20357/39 1/E1/39 (I/P6) 255
Civil Variants By Mark and Manufacturer
Constructor Type 652 Type 652
Mk.II
Anson
Mk.18C
Avro 19
Series 1
Avro 19
Series 1
Total
 Avro, Newton Heath 2 1 3
 Avro, Yeadon 10 1 11
 Avro, Chadderton 12 1 11 24
2 1 12 11 12 38

Type 652A Anson - Canadian Production
Military Variants By Mark and Manufacturer
Constructor Mk.II Mk.V Mk.VA Mk.VI Total
 Canadian Car 341 259 41 641
 de Havilland Canada 375 375
 Federal Aircraft 1 1 2
 MacDonld Bros. 299 712 36 1047
 National Steel Car 736 1 737
 Ottowa Car 80 80
Total 1832 972 77 1 2882

Anson Work Orders

The table below is taken directly from the Avro Anson summary [15], with the exception of the indicated ammendment to 7799/14 and the addition of this authors Comments and Correlation.

Works
Order
Customer and Remarks Where
Built
Qty Mark Authors Comments and Correlation
1 3&4 10 11 12 18 18C 19 20 21 22
 4233  Prototype N.H. 1 1  K4771 to Contract 352855/34.
 4825  RAF N.H. 162 162  K6152 - K6211, K6224 - K6325 to Contract 421119/35.
 5213  RAF N.H. 78 78  K8742 - K8791, K8813 - K8839 and K8845 to Contract 497338/36.
 5214  RAF N.H. 35 35  K8703 - K8737 to Contract 497339/36.
 5445  Australia N.H. 38 38  C/n's 967-978, 1008-1028 and 1053-1057.
 5662  RAF N.H. 28 28  L7046 - L7073 to Contract 633200/37.
 5883  RAF N.H. 88 88  L7903 - L7912, L7923 through N1339 to Contract 690658/37.
 6057  Australia N.H. 10 10  C/ns 1079-1088.
 17734  Finland N.H. 3 3  C/ns 939-941.
 18513  Estonia N.H. 1 1  C/n 951.
 18532  Ireland N.H. 2 2  C/ns 980-981.
 19266  Ireland N.H. 2 2  C/ns 1033-1034.
 20717  Greece N.H. 12 12  12 aircraft diverted from batches N5130 - N5178 and N5182 - N5220.
 21766  Turkey N.H. 6 6  C/ns 1127-1132.
 6080  RAF N.H. 1332 1332  500 a/c (N4856 through N5385) and 350 a/c (N9526 through N9999)
  to Contract 766119/38, 200 a/c (R3303 through R3351) to Contract
  B12565/39, 300 a/c (R9567 through R9969) to Contract B32842/39,
 less 18 diverted to Greece and Turkey.
 7600  RAF N.H. 950 1000  W1505 through W2665 to Contract B61695/39.
    Y 50  
 7799  RAF N.H. 750 750  4400 a/c to Contract B137211/40:
 AW443 through AX656 - 750 delivered as Mk.I.
 DG689 through DJ700 - 700 delivered as Mk.I.
 EF805 through EG704 - 600 a/c delivered as Mk.I.
 LS978 through LV332 - 750 delivered as Mk.I.
 MG102 through MH237 - 799 delivered as Mk.I, one a/c as Mk.XII.
 NK139 through NL251 - 800 delivered as 592 Mk.Is, 103 Mk.Xs,
 90 Mk.XIs and 15 Mk.XII.
 223 a/c in the AWxxx and DGxxx range, intended as Mk.IV,
 were completed as Mk.I.
 7799/9  RAF N.H. 39 700
    Y 661
 7799/14  RAF Y 600 168* 223 103 90 16
 7799/46  RAF Y 750 750
 7796/55  RAF Y 800 800
 7796/70  RAF Y 800 800
 8824  RAF and MCA. Of the 24 Mk.19
 aircraft, 11 were built to
 Washington Standard.
 The 13 Mk.I a/c were fitted with
 Bristol Turrets
Y 267 13 230 24  PH528 through PH845, PH858, PH859, PH861 - PH865: to Contract
 Acft/3077, delivered as 248 Mk.XII and 19 Mk.XIX.
 (Mk.19 PH860 to c/n 1285 for Misr per W.O.9239).
 9169  RAF. 59 of these had M.W., of Y 92 138  TX154 through VL363 (161 a/c) to Contract Acft/5037 less:
   which 13 were built at Yeadon. C 46  TX246, TX248, TX249 (W.O.9239) - 3 a/c.
 VL358, VL359 (W.O.9247) - 2 a/c.
 VL360 - VL263, TX240 - TX245, TX247, TX250 - TX252 (W.O.9262) - 14 a/c.
 TX201, TX202, TX236, TX255 (W.O.9294) - 4 a/c.
 9239  Egypt, Misr Airworks Y 5 5  C/ns 1285 (ex PH860), 1327 - 1329 (Ex TX246, TX248, TX249)
 = 4 aircraft. See Note 2.
 9247  Emperor of Ethiopia Y 2 2  C/ns 1273, 1274. (Ex VL358, VL359)
 9249  RAF (Incl Rhodesia) - M.W. C 93 84 9  VM307 through VM418 (84 Mk.19, 9 Mk.20) to Contract Acft/5680.
 9262  Railway Air Services Y 14 14  C/ns 1275 - 1278 (Ex VL360 - VL263),
 1317 - 1326 (Ex TX240 - TX245, TX247, TX250 - TX252).
 9294  MCA Y 5 5  C/ns 1286, 1287 (Ex TX201, TX202), 1330, 1331 (Ex TX236, TX255),
 1332 (new)
 9295  Originally for Iraq, diverted to RAF C 27 29  VP509 - VP5110, VP512 - VP538 to Contract Acft/6103.
   M.W. Y 2  VP511 diverted as c/n 1509 to Afghanistan.
 Sales 5000  RAF (Incl Rhodesia) - M.W. C 90 48 30 12  VS491 through VS603 to Contract 6/Acft/811.
 Sales 5001  Prototypes - M.W. C 2 1 1  VM305, VM306 to Contract 6/Acft/923
 Sales 5002  RAF - M.W. C 80 67 13  VV239 through VV370 to Contract 6/Acft/1019.
 Sales 5004  RAF (Incl Rhodesia) - M.W. C 92 2 90  VV866 through VV999 to Contract 6Acft/1396.
 Sales 5005  MCS Insecticide a/c - M.W. C 2 2  C/ns 1423, 1424
 Sales 5007  RAF - M.W. C 20 20  WB446 - WB465 to Contract 6/Acft/2473.
 35771  Smith and Sons - M.W. Y 1 1  C/n 1333
 35662  Irish Dept. of Defence - M.W. Y 3 3  C/ns 1313 - 1315.
 35815  Belgium Y 1 1  C/n 1312.
 35815/6  Belgium Y 2 2  C/ns 1357, 1358
 36420  Hunting Air Travel Y 3 3  C/ns 1351 - 1353.
 36421  Westminster Airways Y 1 1  C/n 1360.
 36425  Sivwright Airways Y 1 1  C/n 1359.
 36743  Sivwright Airways - M.W. C 1 1  C/n 1376.
 36537  Belgium C 1 1  C/n 1363.
 36532  Belgian Congo Airways - M.W. C 2 2  C/ns 1361, 1362.
 36570  Short and Harland C 1 1  C/n 1364.
 36463  Hunting Air Travel - M.W. C 1 1  C/n 1375.
 Sales 101  Indian Air Survey - M.W. C 1 1  C/n 1377.
 Sales 103  Bharat Airways.
 1 was originally Canadian
 Demonstrator - M.W.
C 2 2  C/ns 1383, 1384.
 Sales 105  Royal Afghan AF - M.W. C 13 13  C/ns 1465 - 1476, 1509.
 Sales 108  India. Civilian aircrew trainer
 M.W.
C 12 12  C/ns 1477 - 1488.
 50056  Argentine, private. Cheetah 17
 engines - M.W.
C 1 1  C/n 1507.
 (none)  Avro Staff machine. G-AGPG Y 1 1  C/n 1212
 11494  RAF C 25 17 8  WD402 through WD436 to Contract 6/Acft/3634.
 13450  RAF C 28 28  WJ509 through WJ561 to Contract 6/Acft/5932.
8138 6779 223 103 90 246 13 12 326 60 252 34

* The Avro document gives 3968 for W.O.7799/14 Mk.I, which is actually the sum of all the Mk.I a/c to the various subsections of W.O. 7799; it has been corrected here to give the required W.O.7799/14 total.

Abbreviations used in table:
N.H. - Newton Heath
Y - Yeadon
C - Chadderton
M.W. - Metal Wing and Tailplane

Presumably the Avro table gives produced Marks as ordered as opposed to as produced. The Avro table and the tables produced on this site give very similar results, the differences being explained by aircraft being produced to a different Mark than originally ordered.


Notes

  1. The disposition of Mk.I range DG689-DJ700 between Newton Heath and Yeadon has been deduced from the MAP production records over the relevant period, showing 39 aircraft produced at Yeadon, the remaining 661 therefore coming from Newton Heath.
  2. The normal understanding is that a total of 11020 Ansons of all marks were produced, this figure presumably coming from Avro's Anson summary [15], reproduced here in the Anson Work Orders table. This same document, under W.O.9239, gives a total of 5 new Anson Mk.XIX being supplied to Misrair of Egypt, but only the four indicated aircraft have been reliably identified. A memo located in AVIA 49/229, dated December 1945, indicates that this fifth aircraft is Mk.XII PH806, supplied to Misrair under Contract Acft/5616 (though this Contract was apparently dated 16 January 1946). Sturtivant has this as SU-ADJ, delivered sometime in late 1945 [1], and A.M. Form 78 [2] has PH806 as transferred to Civil Contract on 28 September 1945. If PH806 is indeed the fifth aircraft, then it has already been accounted for under Avro Work Order 8824. Accordingly this author is forced to conclude, unless further evidence comes to light, that the Avro account is incorrect and the final total should be 11019.
    However, it must be noted that Avro c/n 1206 has not been identified, so the final result may still be 11020!
  3. Conversions are from Mark to Mark and do not include civil conversions from military.
  4. Includes first prototype K4771.
  5. Between 1937 and 1945, Production Specifications were designated by the type and mark of aircraft, suffixed by the letter P and a sequence number identifying the individual order, i.e. "Anson I/P4", was the 4th Production Specification for the Anson Mk.I. (Note the aircraft type has been omitted from the table for convenience). Those in parentheses are assumed, based on Meekcoms and Morgan [26].

Production References

  1. The Anson File, Ray Sturtivant (Air-Britain Publications, 1988)
  2. Avro Aircraft Since 1908, A.J. Jackson (Putnam, 1965 and 1990)
  3. Avro Anson Marks I, III, IV and X, Alan W. Hall and Eric Taylor (Almark Publications, 1972)
  4. Air Britain RAF Aircraft Register Series, Various Volumes (Air-Britain Publications)
  5. The British Roundel Various Issues (Roundel Research Publications)
  6. Australian and New Zealand Military Aircraft Serial Numbers at http://adf-serials.com/
  7. Canadian Aircraft Since 1909, K.M. Molson and H.A. Taylor (Putnam, 1982)
  8. Canadian Military Aircraft Serial Numbers at CASPIR (Canadian Aircraft Serials Personnel Information Resource) at the Canadian Warplane Heritage Museum
  9. Aerodrome of Democracy: Canada and the British Commonwealth Air Training Plan 1939-1945, F.J. Hatch (Minister of Supply and Services Canada, 1983)
  10. Rhodesian Air Training Scheme, 1940 - 1954, Aeromilitaria 2013/3 (Air-Britain Publications)
  11. Rhodesian Air Training Scheme, 1940 - 1954, Aeromilitaria 2016/2 (Air-Britain Publications)
  12. Canadian Military Aircraft: Serials and Photographs, 1920-1968, John A. Griffin (Canadian War Museum, Ottawa, 1969)
  13. Anson c/ns at Historic CCAR (Canadian Civil Aircraft Register) Project at http://www.historicccar.ca/notes#Anson
  14. Argentine Civil Ansons at http://loudandclearisnotenought.blogspot.com/2012/08/lv-agn-avro-652a-anson-v-mdf-191.html
  15. Avro document on Anson production dated January 1952 held by the Aviation Library at Farnborough.
  16. The First 30 Years of Aviation in Afghanistan, Part 2 by Lennart Andersson (http://www.artiklar.z-bok.se/afghanistan-2.html)
  17. Civil and Military Aviation in Iran 1924-1949, Part 2 by Lennart Andersson (http://www.artiklar.z-bok.se/Iran-2.html)
  18. Iraqi military Ansons at http://iraqimilitary.org/forums/viewtopic.php?t=20
  19. Portugeuse military Ansons at http://ex-ogma.blogspot.com/2009/03/avioes-da-am-avro-652a-anson.html
  20. RAF Air Historical Branch: RAF Aircraft Movement Card (A.M. Form 78) (Dept of Archive and Aviation Records, RAF Museum, Hendon, Records MFC-77-15-1 through -6)
  21. RAF Air Historical Branch: Contract Delivery Cards (Dept of Archive and Aviation Records, RAF Museum, Hendon, Records MFC-78-8-1)
  22. RAF Air Historical Branch: Delivery Serial Ledger (A.M. Form 622) (Dept of Archive and Aviation Records, RAF Museum, Hendon, Records MF-1 thru 5)
  23. National Archives of Australia NAA: A1196 1/501/213 Purchase of (Beaufort) Aircraft for RAAF Policy
  24. National Archives of Australia NAA: A14487 12/AB/2182 Air Board Agenda 2182 (RAAF) - Supply of Avro Anson aircraft and Cheetah engines - Overseas Indent No. 613
  25. Aeronaves Militares Portuguesas, Adelino Cardoso, 2nd Edition (Lisboa 2009)
  26. British Aircraft Specifications File, K.J. Meekcoms and E.B. Morgan (Air-Britain Publications, 1994)
  27. Ministry of Aircraft Production Aeroplane Price Books (Dept of Archive and Aviation Records, RAF Museum, Hendon, Records X005-2126/)

Page Revision History

Revised at Version 2.1.0
  • Deleted old note 5.
  • Added new Note 5.
  • Summary Tables updated in accordance with changes to Military Variants.
Revised at Version 2.0.0
  • Improved Type Description details and added Specification details.
  • Added Contracts Table.
  • Added Note 5.
  • Modified note 2.
Revised at Version 1.4.0
  • Added Works Order table.
  • Revised Note 2.
  • Balance between Yeadon and Chadderton military production corrected.
Revised at Version 1.3.0
  • All Anson pages completely updated and rewritten.