The Yang Ch’eng 53 was developed on the basis of “Yangcheng 51” and “Yangcheng 52”, with a strengthened structure.
The one built first flew in 8 November 1929. The Guangdong Air Force received the aircraft for training use.
Yangcheng No. 53
Engine: Hispano Suiza, 180 hp
Wingspan: 9.82 m
Length: 7.5 m
Height: 2.71 m
Empty weight: 454 kg
Maximum take-off weight: 1089 kg
Crew: 2
All Aero 