Specifications
RV7
RV7a
Van's Aircraft RV7/7a
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The RV-7 is the most successful utility kit aircraft with world-wide
acclaim.
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The RV-7 is a two-place side-byside conventional aircraft.
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RV aircraft are cantilever low wing monoplanes of traditional riveted aluminium construction. RV structures are “monocoque” or “stressed skin” design, providing strength and durability.
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The RV-7 has short, low aspect ratio, constant-chord wings, providing low wing loading with favourable stall characteristics and very good climb and altitude performance.
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The all-metal construction withstands the rigours of training without compromising cost or performance.
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The RV-7A is fitted with a rugged fixed steel landing gear (tri-gear).
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The RV-7A is designed to accommodate a Lycoming 160 hp to 200 hp engine with 2000 hr TBO.
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The RV-7A is fully aerobatic with excellent control response throughout the speed range.
Exterior Dimensions |
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Span |
25 ft |
Length |
20 ft 4 in. |
Height |
7 ft 10 in. |
Wing Area |
121 sq ft |
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Weights |
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Empty Weight |
1077 - 1130 lbs |
Gross Weight |
1800 lbs |
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Loadings |
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Wing Loading |
14.8 lb/sq ft |
Power Loading |
12.0 - 9.0 lb/hp |
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Powerplant/Systems |
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Engine |
150-200 hp |
Propeller |
Fixed or C/S |
Fuel Capacity |
42 US gal |
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Other |
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Baggage |
100 lbs |
Performance
Exterior Dimensions |
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Span |
25 ft |
Length |
20 ft 4in. |
Height |
5 ft 10 in. |
Wing Area |
121 sq ft |
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Weights |
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Empty Weight |
1061 - 1114 lbs |
Gross Weight |
1800 lbs |
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Loadings |
|
Wing Loading |
14.8 lb/sq ft |
Power Loading |
12.0 - 9.0 lb/hp |
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Powerplant/Systems |
|
Engine |
150-200 hp |
Propeller |
Fixed or C/S |
Fuel Capacity |
42 US gal |
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Other |
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Baggage |
100 lbs |
RV7
Empty weight and performance measured with Hartzell 2 Blade C/S prop
Speeds and ranges in statute mph (sm)
Solo Weight 1400 lbs/Gross Weight 1800lbs 160 hp 180 hp 200 hp |
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RV7a
Empty weight and performance measured with Hartzell 2 Blade C/S prop
Speeds and ranges in statute mph (sm)
Solo Weight 1400 lbs/Gross Weight 1800lbs 160 hp 180 hp 200 hp |
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