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in the UK and is maintained to an airworthy condition. It underwent restoration to post-Lympne configuration, being completed in 2004, with a single seat, revised undercarriage and fitted with an ABC Scorpion II 30 HP engine. It can be seen flown at
Shuttleworth airshows in the summer months, as well
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inverted V twin-cylinder had the greatest capacity allowed. The wing area was increased by 28% to accommodate the extra weight by a 5 ft 2 in (1.57 m) span extension. It was also longer by almost the same amount. Engine problems kept it from flying in the competition and out of the
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flat twin engine, a larger rudder, and a more conventional undercarriage with larger wheels mounted on a cross axle attached to the lower fuselage with a pair of V-struts. In 1931 another new owner fitted a heavier 30 hp (22 kW)
169:, principally an engine capacity limit of 750 cc, and the two aircraft completed that August took part. The main prizes were for fuel economy and the second ANEC I
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189:. Afterwards it was modified with a wingspan greatly reduced from 32 ft to 18 ft 4 in (9.75 m to 5.59 m) and re-engined with a 1,000 cc
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for flights of 87.5 miles (141 km) on one gallon (4.54 L) of petrol. He later reached an altitude of 14,000 ft (4,267 m) in it.
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engine, another flat twin and, to keep the weight down, reworked it as a single seater. It was in this condition when it was acquired by
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in
December 1924, but it was not completed until the following year. The first of the two built in the United Kingdom in 1923,
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220:. E. W. Beckman, the owner of the aircraft, intended to enter it in the Low-Powered Aeroplane Competition held at
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competition. Following the revised competition rules, it was a two-seater and its more powerful 1,100 cc
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Jane's all the World's
Aircraft 1924, British Civil Aviation since 1919 Volume 1
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on 21 August 1923. It was the first aircraft with an inverted engine, a 696 cc
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The ANEC I and II, designed by W.S Shackleton, were amongst the earliest
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2-cylinder air-cooled inverted V piston engine, 16 hp (12 kW)
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27:
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173:, flown by Jimmy James, shared half of the £1,500 prize with an
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as on static display as part of the
Collection all year round.
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In 1927 a new owner refitted it with a 32 hp (24 kW)
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aircraft; they were very small, wooden, strut braced high-wing
589:. Tonbridge, Kent: Air-Britain (Historians) Ltd. p. 159.
557:. Seymour, Victoria: Finger-Four Publishing. p. 323.
654:. London: Sampson, Low, Marston & co Ltd. p. 6b.
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single-engine ultralight aircraft designed and built by
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Only one more ANEC I was constructed. It was built in
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was an enlarged version of the ANEC I built for the
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617:. Peterborough: GMS Enterprises. pp. 226–227.
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Australian-built
Aircraft and the Industry Volume 1
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87:
79:
69:
57:
49:
44:
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523:(2nd ed.). London: Putnam. pp. 34–37.
165:. The ANEC I was designed to the rules of the
116:Air Navigation and Engineering Company Limited
64:Air Navigation and Engineering Company Limited
714:Air Navigation and Engineering Company (ANEC)
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294:– ANEC I with reduced wingspan, one modified.
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705:
691:
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521:British Civil Aviation since 1919 Volume 1
197:August Bank Holiday Races, designated the
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185:in 1924, briefly carrying the RAF serial
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471:3.21 lb/sq ft (15.7 kg/m)
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453:74 mph (119 km/h, 64 kn)
365:ANEC II 3-view drawing from NACA-TM-289
465:3,000 ft (910 m) in 8minutes
459:32 mph (51 km/h, 28 kn)
638:The Shuttleworth Collection – ANEC II
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767:1920s British civil utility aircraft
652:Jane's all the World's Aircraft 1924
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398:32 ft 10 in (10.01 m)
125:. One was privately constructed in
673:British Aircraft Directory ANEC II
392:15 ft 7 in (4.75 m)
14:
668:British Aircraft Directory ANEC I
480:23.2 hp/lb (38.1 kW/kg)
410:145 sq ft (13.5 m)
241:1924 Lympne light aircraft trials
167:1923 Lympne light aircraft trials
613:Ord-Hume, Arthur W.J.G. (2000).
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328:
252:race that immediately followed.
26:
772:Single-engined tractor aircraft
438:2-bladed fixed pitch propeller
1:
553:Meggs, Keith Raymond (2009).
300:– two-seat version, one built
193:engine for entry in the 1925
787:Aircraft first flown in 1923
587:Bleriot in Britain 1899-1927
232:in the second half of 1924.
212:, who went on to design the
640:Retrieved: 8 September 2017
315:The Shuttleworth Collection
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422:470 lb (213 kg)
416:290 lb (132 kg)
313:is owned and operated by
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615:British Light Aeroplanes
519:Jackson, A. J. (1973).
404:3 ft (0.91 m)
377:General characteristics
357:Specifications (ANEC I)
83:3 (ANEC I), 1 (ANEC II)
38:Shuttleworth Collection
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276:
275:Shuttleworth's ANEC II
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352:: 1 ANEC I, 1 ANEC II
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181:was evaluated by the
175:English Electric Wren
585:Sanger, Ray (2008).
266:Richard Shuttleworth
650:Grey, C.G. (1924).
338:: 2 ANEC I aircraft
53:ultralight aircraft
45:General information
782:High-wing aircraft
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257:Bristol Cherub III
228:, was exported to
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624:978-1-870384-76-6
596:978-0-85130-399-4
564:978-1-920892-77-7
530:978-0-370-10006-7
485:Fuel consumption:
463:Time to altitude:
430:Blackburne Tomtit
309:The 1924 ANEC II
159:Blackburne Tomtit
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145:. The first
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93:First flight
80:Number built
59:Manufacturer
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487:60 mpg
444:Performance
436:Propellers:
426:Powerplant:
110:were 1920s
21:ANEC I / II
761:Categories
496:References
489:‑imp
476:Power/mass
408:Wing area:
155:Brooklands
143:monoplanes
139:ultralight
120:Addlestone
396:Wingspan:
370:Data from
336:Australia
322:Operators
305:Survivors
230:Australia
206:Australia
36:, at the
32:ANEC II,
741:ANEC III
716:aircraft
280:Variants
222:Richmond
127:Brisbane
70:Designer
746:ANEC IV
736:ANEC II
402:Height:
390:Length:
298:ANEC II
292:ANEC IA
237:ANEC II
199:ANEC IA
133:History
112:British
108:ANEC II
88:History
731:ANEC I
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593:
561:
527:
347:
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311:G-EBJO
286:ANEC I
245:Anzani
226:G-EBHR
216:, and
195:Lympne
191:Anzani
179:G-EBIL
171:G-EBIL
151:G-EBHR
147:ANEC I
123:Surrey
104:ANEC I
34:G-EBJO
384:Crew:
187:J7506
619:ISBN
591:ISBN
559:ISBN
525:ISBN
428:1 ×
235:The
106:and
102:The
96:1923
50:Type
208:by
118:at
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605:^
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201:.
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386:1
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