Anderson Greenwood AG-14
Anderson Greenwood · United States · first flew 1947 · light aircraft
The Anderson Greenwood AG-14 was a two-seat utility aircraft developed in the United States shortly after the Second World War. It used a Continental C90 four-cylinder engine of 90 hp driving a pusher propeller.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, fuselage-mounted |
| F — Fuselage | All-metal shoulder-wing monoplane with a pod-and-boom fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- All-metal shoulder-wing monoplane with a pod-and-boom fuselage
- Pusher propeller behind the cabin
- Fixed tricycle undercarriage with side-by-side seating
A shoulder-wing pod-and-boom aircraft with a pusher propeller and a tricycle undercarriage.
Specifications
- The Anderson Greenwood AG-14 has a length of 6.71 m (22 ft).
- It has a wingspan of 10.54 m (35 ft).
- Its maximum speed is 193 km/h (120 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It first flew in 1947 and entered service in 1950.
Variants
The design led to the XAZ-1 Marvelette.
Where you'll see it
A total of five were built.
Related aircraft
AircraftIQ — the aircraft field guide: 8,606 recognition guides, live overhead identification, works offline.