De Havilland Hercules: Difference between revisions

Revision as of 08:11, 15 March 2007

Revision as of 22:38, 27 March 2007

Line 61:

|max takeoff weight main= 15,600 lb

|max takeoff weight alt= 7076 kg

|engine (prop)=[[Bristol Jupiter VI]] VI

|type of prop= radial piston

|number of props=3