Waco PG-2A

The Waco PG-2A was a unique powered development of the successful Waco CG-4 Hadrian standard glider. In 1943, the US military had originally developed a prototype powered-version of the Hadrian with two Franklin flat-four piston engines in nacelles beneath the wings. The object of this conversion was to allow the glider to return under its own power after completing a mission. After tests with this prototype, a further ten conversions of the aircraft were ordered with Ranger L-440-7 piston engines. These production versions were then known by the PG-2A designation.

The service trials were apparently of interest to the RCAF and one PG-2A was briefly tested here in Canada during the immediate post-war period.

aircraft specifications
CDN Reg:
US/NATO Reg.:
Manufacturer: Waco Aircraft Company
Crew / Passengers: two pilots and up to 13 troops
Power Plant(s): two Ranger L-440-7 piston engines
Performance:
Weights:
Dimensions: Span: 83 ft 8 in ( 25.50 m) Length: 48 ft 4 in (14.73 m) Height: 12 ft 7 in ( 3.84 m) Wing Area: 852 sq ft ( 79.15 sq m)
Armament: None
A view of the sole Waco PG-2A glider in RCAF colours. (J McNulty photo)

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