Westland Wessex Aircraft
| |
Production Details | |
Design Company: |
|
First Flight: |
21 February 1929 |
Westland IV: |
2 - Westland |
Wessex: |
8 - Westland |
Type Specification | |
Applies to: |
Westland Wessex |
Type: |
Commercial monoplane to company design |
Wing: |
High wing braced monoplane. Wooden structure with fabric covering. Wings are untapered and slightly swept |
Fuselage: |
Square section fuselage of wooden structure with fabric covering |
Tail Unit: |
Braced tailplane on top of fuselage forward of fin with single fin and rudder |
Landing Gear: |
Main wheels on oleo legs under outboard engine with axle and radius rod to fuselage lower longeron. Tail wheel |
Power Plant: |
Three 140 hp Armstrong Siddeley Genet Major IA five-cylinder radial air-cooled engines, one in nose and two under the wings, driving two bladed propellers |
Accommodation: |
Two crew and four passenger seated in enclosed cabin |
Dimensions | |
Span: |
57 ft 6 in |
Length: |
38 ft |
Height: |
9 ft 6 in |
Wing Area: |
490 sq ft |
Weights | |
Empty: |
3,981 lb |
Loaded: |
6,300 lb |
Performance | |
Max Speed: |
122 mph |
Climb: |
680 ft/min at sea level |
Ceiling: |
14,900 ft |
Range: |
420 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
http://www.jaapteeuwen.com/ww2aircraft/html%20pages/WESTLAND%20WESSEX.htm |