The proposed Model 900 has been conceived by the Philippine Aircraft Development Company as a rugged multi-engine utility aircraft for single-pilot operation, with seating for up to five passengers plus baggage, or the equivalent in freight. Design work began in the latter part of 1947, and the existence of the project was announced in August 1948, when construction of a prototype was authorized by the Ministry of Transport.
General characteristics (projected):
Crew: 1; accommodation for up to six persons total
Length: 10.52 m
Wingspan: 14.76 m
Height: 4.0 m
Wing area: 26.75 sq m
Empty weight: 1,453 kg
Gross weight: 2,270 kg
Powerplant: four Ranger 6-440C cylinder inline inverted air-cooled aero-engines each rated at 140 hp
Projected performance:
Maximum speed: 250 kph
Endurance: 7 hours @ 70% maximum power
Service ceiling: 4,800 m
Take-off run: 300 m