Parnall Perch Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
10 December 1926 |
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Perch: |
1 - George Parnall and Company |
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Type Specification | |
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Applies to: |
Parnall Perch |
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Type: |
Two-seat naval training aircraft to specification 5/24 |
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Wing: |
Two bay biplane with unswept, equal span, staggered wings. Wooden structure with fabric covering. Ailerons on all four wings |
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Fuselage: |
Wooden fuselage with fabric covering, attached to wing at lower longeron |
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Tail Unit: |
Strut braced tailplane with single fin and rudder |
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Landing Gear: |
Crossaxle type landing gear on oleo and radius rod. Tailskid |
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Power Plant: |
One 270 hp Rolls-Royce Falcon III twelve cylinder vee water-cooled engine in the nose driving a two bladed wooden propeller |
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Accommodation: |
Side by side seats for two in open cockpit aft of the wing |
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Dimensions | |
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Span: |
40 ft |
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Length: |
29 ft 6 in |
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Height: |
13 ft |
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Wing Area: |
Unknown |
Weights | |
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Empty: |
2,800 lb |
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Loaded: |
4,500 lb |
Performance | |
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Max Speed: |
115 mph |
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Climb: |
5,000 ft in 11 min |
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Service Ceiling: |
12,000 ft |
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Range: |
500 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |