Saro A.33 Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
14 October 1938 |
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A.33: |
1 - Saunders-Roe Limited |
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Type Specification | |
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Applies to: |
Saunders-Roe A.33 |
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Type: |
Longe range monoplane patrol flying boat |
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Wing: |
Parasol wing monoplane. Wing is all metal structure and of Monospar design with fabric covering |
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Hull: |
All metal two step hull with wide stabilising sponsons. Hull suspended from wing by N type struts which attached at outer engine nacelles and the sponsons |
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Tail Unit: |
Conventional tapered tailplane with divided elevators fixed to base of single fin and rudder |
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Landing Gear: |
None |
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Power Plant: |
Four 830 hp Bristol Perseus XII piston engines in nacelles on wing |
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Accommodation: |
Crew of seven, pilot, copilot, engineer, radio operator and three gunners in enclosed cockpit and cabin |
Armament: |
Intended to carry nose and tail turrets and two beam positions in dorsal hump each with at least one gun. 2,000 lb bomb load on underwing mountings |
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Dimensions | |
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Span: |
95 ft |
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Length: |
75 ft |
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Height: |
22 ft 8.5 in |
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Wing Area: |
1,194 sq ft |
Weights | |
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Maximum: |
41,500 lb |
Performance | |
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Max Speed: |
200 mph |
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Climb: |
8 min 20 sec to 3,300 ft |
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Service Ceiling: |
14,280 ft |
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Normal Endurance: |
12 hr |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |