ANEC I Aircraft

Production Details

Design Company:

Air Navigation and Engineering Co

First Flight:

21 August 1923

ANEC I:

3 - ANEC, Addlestone

Type Specification

Applies to:

ANEC I

Type:

Single seat light aircraft

Wing:

Semi-cantilever monoplane with wing attached to top of fuselage. Wooden structure

Fuselage:

All wooden fuselage of box section with faired top deck

Tail Unit:

Cantilever tail surfaces with one-piece elevator, single fin and rudder

Landing Gear:

Main wheels on axle attached to base of fuselage. Tail skid

Power Plant:

One 696 cc Blackburne Tomtit piston engine in the nose

Accommodation:

Single seat for pilot in open cockpit under wing

Span:

32 ft 0 in

Length:

15 ft 7 in

Height:

3 ft 0 in

Wing Area:

145 sq ft

Tare:

290 lb

All-up:

470 lb

Max Speed:

74 mph

Preserved in British Museums

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