Handley Page Basic Trainer Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
1 May 1950 |
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H.P.R.2: |
2 - Handley Page |
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Type Specification | |
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Applies to: |
Handley Page (Reading) H.P.R.2 |
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Type: |
Single engined basic trainer |
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Wing: |
Low wing cantilever monoplane. Inner section to undercarriage is flat without taper, outer section has dihedral and taper |
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Fuselage: |
Circular section fuselage |
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Tail Unit: |
Cantilver tailplane with single fin and rudder |
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Landing Gear: |
Tail wheel type fixed undercarriage. Single wheel main gear. Tailwheel |
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Power Plant: |
One Armstrong Siddeley Cheetah 18 in nose |
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Accommodation: |
Side by side seating for two in enclosed cabin |
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Dimensions | |
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Span: |
37 ft |
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Length: |
29 ft 11 in |
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Height: |
Unknown |
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Wing Area: |
223 sq ft |
Weights | |
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Maximum: |
4,350 lb |
Performance | |
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Speed: |
175 mph |
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Endurance: |
2.84 hours |
Preserved in British Museums | |
None known | |
Web Sites | |