A 1989 hang glider.
Wing area: 15.8 m²
Wing span: 9.75 m
Aspect ratio: 6
Hang glider weight: 26 kg
Nose angle: 120°
Vega Drachenbau Alfa
1980->
Vector Ultralight Fox V5
Developed by Swiss Hans Gygax, the Fox is a tube and fabric microlight, available with tandem or side by side seating.
Vector Ultralight SA
1998:
Rua Bruno SEBRA 60 / Jacare
BZ-20971 Rio de Jaieiro
Brazil
UL builder
Vector Aircraft Vector / Aerodyne Vector / Sky King International Vector 627SR
Developed by Klaus Hill from the Hummer, the 600 is a three axis control ultralight. A monowing with upright V-tail. Tail control surfaces and spoilers are operated through a mixer stick. Construction consists of tubing with the wings and tail surfaces covered by Dacron. Power is a Zenoah in pusher configuration mounted forward of the wing. A 2.33:2 reduction unit turns a two-blade wooden Vector prop. Shock-mounted tricycle gear uses rubber cushions: The nosewheel is not steerable, and there are no brakes. Units delivered by June 1981 100+.
Vector Aircraft Vector Article
Seen for the first time at Sun’n’Fun at Lakeland in Florida in March 1982, the Vector 610 is a modified version of the earlier Vector 600 which itself was direct descended from the Humbug that Klaus Hill redesigned on leaving Hummer in 1978. Jointly with Gemini International Inc. the Skysports International company was founded in 1980 to sell the first production Vector 600s. This company was then absorbed by Vector Aircraft Corp, itself bought up by Aerodyne Systems Inc at the end of 1982.
Compared with its predecessor, the Vector 610 includes several modifications, principally enlarged spoilerons, semi elliptic saumons at the wing tips, structural strengthening and, for the production models in the USA, the adoption of the Zenoah G25B 22hp engine. This replaced the two Chrysler Power Bee engines, each developing 9 hp, which equipped the last Vector 600 machines produced. In Europe, the British supplied Robin EC25PS of 22 hp output at 6500 rpm or the EC34PM of 32hp at 6500 rpm (with a reduction drive of 2.6/1) is fitted in preference to the Zenoah. The Vector 610, a mono-wing with upright V-tail, features no rudder pedals, with the control stick operating both spoilerons and the V-tail elevons through a mixer stick. Construction consists of tubing with the wings and tail surfaces covered by Dacron. Single seat single engined high wing mono¬plane with unconventional three axis control. Wing has unswept leading edge, swept forward trailing edge and tapering chord; V tall. Pitch/yaw control by elevon; roll control by one third span spoilerons; control inputs through stick for pitch/yaw/roll. Wing braced from above by kingpost and cables, from below by cables; wing profile; double-surface. Undercarriage has three wheels in tricycle formation with additional tailwheel; no suspension on nosewheel and rubber suspension on main wheels. No ground steering. No brakes. Aluminium tube framework. without pod. Engine mounted at wing height driving pusher propeller. 6061T6 anodized aluminium, 3/32 inch 7×7 stainless steel cable, AN hardware.
Prices: in the US, the Vector 610 is available in kit form requiring 30 h for completion at a price of $4890 (March ’83). A supplementary kit to retrofit a steerable nosewheel costs $225, a set of three wheel fairings is available for $185 and spring steel landing gear for $150. Glass fibre Sealord 100A floats are available at $1195 and finally, especially noteworthy, is the SR control system kit for retrofit at $275, which transforms the Vector 600 and 610 to three axis control with a rudder bar.
In March 1983 Aerodyne System’s Vector received the first ultralight airworthiness certificate granted by the West German Ministry of Traffic to a US-built ultralight. The certificate allows sale of Vectors in the West German Federal Republic.
Shown for the first time at Sun’n’Fun in Lakeland, Florida in March 1983, the Vector 627 is basically a re engined Vector 610, with certain structural modifications to the tail to increase rigidity and reduce vibration. Instead of the Zenoah (US) and Robin EC25PS (Europe) engines, the 627 uses the Rotax Type 377 motor.
The Rotax develops 10 hp more than the engine it replaces and in addition is mated to a toothed belt drive, a combination which gives the new aircraft considerably better performance than its predecessor, with the possible exception of the EC34PM engined machine. A torsional resonance damper is built into the reduction system.
The new aircraft comes in two forms the standard 627 which uses the 610’s control arrangements, and the 627SR which incorporates rudder pedals linked to nosewheel steering to give conventional three axis control, push right go right nosewheel steering connected to yaw control. A novel feature of the 627SR is that the control linkages can be modified in a matter of seconds to bring the aircraft back to stick only control as on the standard 627. The 627SR utilises a side mounted joy stick, rudder pedals, nose wheel steerable through rudder pedals. Control stick and rudder pedals activate ruddervators and spoilerons for independent three-axis aerodynamic control. Upright V-tail monoplane with double-surfaced wing supported by kingpost and cable bracing. engine forward of wing, prop behind, 2.03:1 reduction drive unit turns a two-bladed wooden prop. LANDING GEAR: Shock-mounted tricycle gear uses bungee cord suspension. Manufacture later transferred to Aerodyne, then Sky King International as the Sky King International Vector 627SR.
Konig 3cyl. radial engine of 24 hp
600
Gross wt: 445 lbs
Wingspan, 34 ft
Wing area, 133 sq.ft
Aspect ratio, 8.33
Overall length, 18 ft
Empty weight, 195 lbs
Usable payload (include fuel), 250 lbs
Wing loading, 3.34
L/D power-off glide ratio, 8:1
Cruise speed (85% power), 50 mph
Stall speed, 26 mph
Approach speed, 30 mph
Flair speed, 25 mph
Liftoff speed, 25 mph
Takeoff roll distance, 100 ft
Rate of climb, 425 + fpm
Fuel capacity, 3 Usgal
Range at cruise, 80 mi
Engine displacement, 14.78 cu,in
Rated hp, 22 hp
Static thrust, 143 lbs
First year built: 1980
610
Engine: Zenoah G2SB 1, 22 hp at 7000 rpm
Propeller diameter and pitch 52 x 24 inch, 1.32 x 0.60 m
Reduction ratio 2.33/1
Static thrust 170 lbs
Power per unit area 0.14 hp/sq.ft, 1.5 hp/sq.m
Fuel capacity 5. 0 US gal, 4.2 Imp gal, 18.9 litre in main tank
Length overall 18ft, 5.48 m
Height overall 8.0ft, 2.43m
Wing span 35.2ft, 10.72m
Sweepback 0 deg
Total wing area 154 sq.ft, 4.3sq.m
Wing aspect ratio 6.7/1
Nosewheel diameter overall 11.5 inch, 29cm
Main wheels diameter overall 11.5 inch, 29cm
Empty weight 195 lb, 88kg
Max take off weight 445 lb, 202 kg
Payload 250 lb, 113 kg
Max wing loading 2.89 lb/sq.ft, 14.1 kg/sq.m
Max power loading 20.2 lb/hp, 9.15 kg/hp
Load factors; +5.7, 2.85 ultimate
Max level speed 50 mph, 80 kph
Never exceed speed 55 mph, 88kph
Max cruising speed 45mph, 72kph
Economic cruising speed 40mph, 64kph
Stalling speed 26 mph, 42 kph
Max climb rate at sea level 600 ft/min, 3.0 m/s
Min sink rate 216 ft/min, 1.1 m/s
Best glide ratio with power off 8/1
Take off distance 100 ft, 30 m
Landing distance 200 ft, 60 m
Range at average cruising speed 125 mile, 201 km
627
Engine: Rotax 377, 32 hp at 6250 rpm
Propeller diameter and pitch 52x23ft, 1.32×0.58m
Toothed belt reduction, ratio 2.0/1
Max static thrust 220 lb, 100kg
Power per unit area 0.21 hp/sq.ft, 2.2 hp/sq.m
Fuel capacity 5.0 US gal, 4.2 Imp gal, 18.9 litre
Length overall 18ft, 5.48 m
Height overall 8.0ft, 2.43m
Wing span 35.2ft, 10.72m
Sweepback 0 deg
Total wing area 154 sq.ft, 4.3sq.m
Wing aspect ratio 6.7/1
Nosewheel diameter overall 11.5 inch, 29cm
Main wheels diameter overall 11.5 inch, 29cm
Empty weight 254 lb, 115kg
Max take off weight 500 lb, 227kg
Payload 246 lb, 112kg
Max wing loading 3.24 lb/sq.ft, 15.8kg/sq.m
Max power loading 15.6 lb/hp, 7.1kg/hp
Load factors +5.7, 2.8 design
Max level speed 55mph, 88kph
Cruising speed 48mph, 77kph
Stalling speed 27mph, 43kph
Max climb rate at sea level 800 ft/min, 4.1 m/s
Best glide ratio with power off 8/1
627SR
Engine: Rotax 377, 32 hp at 6250 rpm
Propeller diameter and pitch 52x23ft, 1.32×0.58m
Toothed belt reduction, ratio 2.0/1
Max static thrust 220 lb, 100kg
Power per unit area 0.21 hp/sq.ft, 2.2 hp/sq.m
Fuel capacity 5.0 US gal, 4.2 Imp gal, 18.9 litre
Length overall 18ft, 5.48 m
Height overall 8.0ft, 2.43m
Wing span 35.2ft, 10.72m
Sweepback 0 deg
Total wing area 154 sq.ft, 4.3sq.m
Wing aspect ratio 6.7/1
Nosewheel diameter overall 11.5 inch, 29cm
Main wheels dia¬meter overall 11.5 inch, 29cm
Empty weight 254 lb, 115kg
Max take off weight 500 lb, 227kg
Payload 246 lb, 112kg
Max wing loading 3.24 lb/sq.ft, 15.8kg/sq.m
Max power loading 15.6 lb/hp, 7.1kg/hp
Load factors +5.7, 2.8 design
Vne: 63 mph
Max level speed 55mph, 88kph
Cruising speed 48mph, 77kph
Stalling speed 27mph, 43kph
Approach speed 40 mph
Liftoff speed 30 mph
Max climb rate at sea level 800 ft/min, 4.1 m/s
Best glide ratio with power off 8/1
Vector Aircraft Corp
1982: 394 Somers Rd., Ellington, CT 06029, USA.
1983: Aerodyne Systems Inc, 194 Millers Falls Road, Turners Fails, Massachusetts 01376, USA.
UL builder
Vans RV-9
The RV-9/9A wing is longer and narrower than the wings of the RV-4/6/8 series, and uses a new Roncz airfoil. The increased span allows it to climb well on low power and glide a long way. The flaps are a long span, slotted, high lift design that allows the airplane to land slower than many primary trainers. A simplified constant-chord horizontal tail and large vertical tail are proportioned to work with the longer wing. The fuselage and cabin are identical to the RV-7/7A and there are the same sliding/tip-up canopy and trigear/tailwheel landing gear options.
The RV-9/9A uses a 118 hp Lycoming (taken from a Cessna 152) to power the prototype. The result was an efficient airplane with respectable short field capability, excellent cruise speed (165 mph). The airframe is engineered to accept the 160 hp Lycoming O-320.
The RV-9 first flew on 15 June 2000, piloted by VanGrunsven. The RV-9A, a tail wheel version of the RV-9, made its maiden flight on 4 March 2002, also piloted by VanGrunsven.
RV-9
Engine: 118 hp
Span: 28 ft
Length: 20 ft 5 in
Height: 6 ft
Wing Area: 124 sq ft
Empty Weight: 1015 – 1057 lbs
Gross Weight: 1600 – 1750 lbs
Wing Loading: 12.9 – 14.1lb/sq ft
Power Loading: 13.6 – 10.9 lb/hp
Engine: 118 -160 hp
Propeller: Fixed or C/S
Fuel Capacity: 36 US gal
Baggage: 75 lbs
Top Speed: 172 mph
Cruise 75% @ 8000 ft: 166 mph
Cruise 55% @ 8000 ft: 150 mph
Stall Speed: 48 mph
Takeoff Distance: 525 ft
Landing Distance: 355 ft
Rate of Climb: 1,000 fpm
Ceiling: 14,500 ft
Range 75% @ 8000 ft: 875 sm
Range 55% @ 8000 ft: 1,035 sm
RV-9
Engine: 135 hp
Span: 28 ft
Length: 20 ft 5 in
Height: 6 ft
Wing Area: 124 sq ft
Empty Weight: 1015 – 1057 lbs
Gross Weight: 1600 – 1750 lbs
Wing Loading: 12.9 – 14.1lb/sq ft
Power Loading: 13.6 – 10.9 lb/hp
Engine: 118 -160 hp
Propeller: Fixed or C/S
Fuel Capacity: 36 US gal
Baggage: 75 lbs
Top Speed: 178 mph
Cruise 75% @ 8000 ft: 174 mph
Cruise 55% @ 8000 ft: 157 mph
Stall Speed: 49 mph
Takeoff Distance: 500 ft
Landing Distance: 410 ft
Rate of Climb: 1,150 fpm
Ceiling: 16,000 ft
Range 75% @ 8000 ft: 745 sm
Range 55% @ 8000 ft: 910 sm
RV-9
Engine: 160 hp
Span: 28 ft
Length: 20 ft 5 in
Height: 6 ft
Wing Area: 124 sq ft
Empty Weight: 1015 – 1057 lbs
Gross Weight: 1600 – 1750 lbs
Wing Loading: 12.9 – 14.1lb/sq ft
Power Loading: 13.6 – 10.9 lb/hp
Engine: 118 -160 hp
Propeller: Fixed or C/S
Fuel Capacity: 36 US gal
Baggage: 75 lbs
Top Speed: 196 mph
Cruise 75% @ 8000 ft: 188 mph
Cruise 55% @ 8000 ft: 168 mph
Stall Speed: 50 mph
Takeoff Distance: 475 ft
Landing Distance: 450 ft
Rate of Climb: 1,400 fpm
Ceiling: 19,000 ft
Range 75% @ 8000 ft: 710 sm
Range 55% @ 8000 ft: 860 sm
RV-9A
Engine: 118 hp
Span: 28 ft
Length: 20 ft 5 in
Height: 7 ft 10 in
Wing Area: 124 sq ft
Empty Weight: 1028 – 1075 lbs
Gross Weight: 1600 – 1750 lbs
Wing Loading: 12.9 – 14.1 lb/sq ft
Power Loading: 13.6 -10.9 lb/hp
Engine: 118 -160 hp
Propeller: Fixed or C/S
Fuel Capacity: 36 US gal
Baggage: 75 lbs
Top Speed: 170 mph
Cruise 75% @ 8000 ft: 164 mph
Cruise 55% @ 8000 ft: 148 mph
Stall Speed: 48 mph
Takeoff Distance: 525 ft
Landing Distance: 375 ft
Rate of Climb: 950 fpm
Ceiling: 14,000 ft
Range 75% @ 8000 ft: 865 sm
Range 55% @ 8000 ft: 1025 sm
RV-9A
Engine: 135 hp
Span: 28 ft
Length: 20 ft 5 in
Height: 7 ft 10 in
Wing Area: 124 sq ft
Empty Weight: 1028 – 1075 lbs
Gross Weight: 1600 – 1750 lbs
Wing Loading: 12.9 – 14.1 lb/sq ft
Power Loading: 13.6 -10.9 lb/hp
Engine: 118 -160 hp
Propeller: Fixed or C/S
Fuel Capacity: 36 US gal
Baggage: 75 lbs
Top Speed: 176 mph
Cruise 75% @ 8000 ft: 172 mph
Cruise 55% @ 8000 ft: 155 mph
Stall Speed: 49 mph
Takeoff Distance: 500 ft
Landing Distance: 410 ft
Rate of Climb: 1,100 fpm
Ceiling: 15,500 ft
Range 75% @ 8000 ft: 735 sm
Range 55% @ 8000 ft: 900 sm
RV-9A
Engine: 160 hp
Span: 28 ft
Length: 20 ft 5 in
Height: 7 ft 10 in
Wing Area: 124 sq ft
Empty Weight: 1028 – 1075 lbs
Gross Weight: 1600 – 1750 lbs
Wing Loading: 12.9 – 14.1 lb/sq ft
Power Loading: 13.6 -10.9 lb/hp
Engine: 118 -160 hp
Propeller: Fixed or C/S
Fuel Capacity: 36 US gal
Baggage: 75 lbs
Top Speed: 194 mph
Cruise 75% @ 8000 ft: 186 mph
Cruise 55% @ 8000 ft: 166 mph
Stall Speed: 50 mph
Takeoff Distance: 475 ft
Landing Distance: 450 ft
Rate of Climb: 1,400 fpm
Ceiling: 18,500 ft
Range 75% @ 8000 ft: 700 sm
Range 55% @ 8000 ft: 850 sm
Vans RV-8
In 1995, Van’s decided to re-visit the tandem seating concept. Even though the side-by-side RV-6/6A had become the most popular homebuilt design ever, there was still a significant percentage of pilots who really wanted centerline seating. The consensus seemed to be that a roomier tandem airplane with better cross-country capability would be popular.
A one-of-a-kind demonstrator was built and introduced at Oshkosh in 1995. The response left no doubt about the desire for an airplane like the RV-8. The RV-8 went on the market in 1996 and complete kits were available by the end of 1998. In short order, it was followed by the kit for the tricycle gear RV-8A.
The RV-8/8A retains the fighter-like feel of centerline seating, but the wider fuselage contains cockpits that accommodate large people in comfort. Two baggage compartments, one forward and one aft, keep even large amounts of luggage well within the weight and balance envelope. Pilots up to 6’7″ fit in the front. A Tall Pilot option is available. (It was used by one successful builder who describes himself as 6’ 10″, although we think he might be taller). Factory demo pilots have flown demo rides with passengers up to 6’9″ and 260 lbs in the back.
The large 42 gallon fuel capacity long range and high cruise speeds. At the aerobatic gross weight of 1600 lbs., the RV-8/8A complies with the +6/-3G standards of the FAA’s Aerobatic Category and can still carry two people, making it possible for a new pilot to get aerobatic instruction before he or she starts rolling and looping.
The sliding canopy is built around a sturdy steel roll bar and fixed windshield. It must remain closed in flight, but the standard fresh air ducts provide plenty of fresh air to both seats. The RV-8/8A is designed to be flown from the front seat, although a rear stick is provided and a rear throttle and rudder pedals are optional.
The RV-8/8A was designed to accept the 200 horsepower IO-360 Lycoming. The prototype with this engine demonstrated really remarkable performance. With a single occupant, it would take off in 250’ and climb out at 2600 fpm. The fact that the RV-8 can accept a large engine doesn’t mean that it needs it. The traditional engine options – 150-180 hp Lycomings – have been retained (probably the majority of flying RV-8/8As are powered by a 180 hp engine) and with these lighter engines, performance is still exciting – and the handling even better.
Kits sold for $14,770-14,995, and a quick-build for $21,750-21,995.
The change that allowed the change in aerobatic gross weight is the use of longer and heavier spar caps and heavier carry-through bulkhead bars. Other parts also needed to be changed to accommodate the larger pieces. The kit serial numbers are issued when a customer gets their tail kit. This means that a low serial number may have the 1600 lb aerobatic gross wing and centre section, while a higher serial number may have the 1550 lb aerobatic gross wing and centre section. Check the packing list for the wing kit and if it says “1” after the spar and centre section, then it’s the 1600 lb gross version. If no ‘1’ then it’s the 1550 lb gross.
RV-8
Engine: 160 hp
Prop: Hartzell 2 Blade C/S
Span: 24 ft
Length: 21 ft
Height: 5 ft 7 in
Wing Area: 116 sq ft
Empty Weight: 1067 – 1120 lbs
Gross Weight: 1800 lbs
Wing Loading: 15.5 lb/sq ft
Power Loading: 12 – 9 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 125 lbs
Top Speed: 205 mph
Cruise 75% @ 8000 ft: 195 mph
Cruise 55% @ 8000 ft: 173 mph
Stall Speed: 58 mph
Takeoff Distance: 650 ft
Landing Distance: 500 ft
Rate of Climb: 1,400 fpm
Ceiling: 18,500 ft
Range 75% @ 8000 ft: 855 sm
Range 55% @ 8000 ft: 1,030 sm
RV-8
Engine: 180 hp
Prop: Hartzell 2 Blade C/S
Span: 24 ft
Length: 21 ft
Height: 5 ft 7 in
Wing Area: 116 sq ft
Empty Weight: 1067 – 1120 lbs
Gross Weight: 1800 lbs
Wing Loading: 15.5 lb/sq ft
Power Loading: 12 – 9 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 125 lbs
Top Speed: 213 mph
Cruise 75% @ 8000 ft: 203 mph
Cruise 55% @ 8000 ft: 180 mph
Stall Speed: 58 mph
Takeoff Distance: 575 ft
Landing Distance: 500 ft
Rate of Climb: 1,650 fpm
Ceiling: 20,500 ft
Range 75% @ 8000 ft: 790 sm
Range 55% @ 8000 ft: 955 sm
RV-8
Engine: 200 hp
Prop: Hartzell 2 Blade C/S
Span: 24 ft
Length: 21 ft
Height: 5 ft 7 in
Wing Area: 116 sq ft
Empty Weight: 1067 – 1120 lbs
Gross Weight: 1800 lbs
Wing Loading: 15.5 lb/sq ft
Power Loading: 12 – 9 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 125 lbs
Top Speed: 221 mph
Cruise 75% @ 8000 ft: 210 mph
Cruise 55% @ 8000 ft: 187 mph
Stall Speed: 58 mph
Takeoff Distance: 500 ft
Landing Distance: 500 ft
Rate of Climb: 1,900 fpm
Ceiling: 22,500 ft
Range 75% @ 8000 ft: 780 sm
Range 55% @ 8000 ft: 940 sm
RV-8A
Engine: 160 hp
Prop: Hartzell 2 Blade C/S
Span: 24 ft
Length: 20 ft 10 in
Height: 7 ft 4 in
Wing Area: 116 sq ft
Empty Weight: 1067 – 1120 lbs
Gross Weight: 1800 lbs
Wing Loading: 15.5 lb/sq ft
Power Loading: 12 – 9 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 125 lbs
Top Speed: 203 mph
Cruise 75% @ 8000 ft: 193 mph
Cruise 55% @ 8000 ft: 171 mph
Stall Speed: 58 mph
Takeoff Distance: 650 ft
Landing Distance: 500 ft
Rate of Climb: 1,350 fpm
Ceiling: 17,500 ft
Range 75% @ 8000 ft: 845 sm
Range 55% @ 8000 ft: 1020 sm
RV-8A
Engine: 180 hp
Prop: Hartzell 2 Blade C/S
Span: 24 ft
Length: 20 ft 10 in
Height: 7 ft 4 in
Wing Area: 116 sq ft
Empty Weight: 1067 – 1120 lbs
Gross Weight: 1800 lbs
Wing Loading: 15.5 lb/sq ft
Power Loading: 12 – 9 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 125 lbs
Top Speed: 211 mph
Cruise 75% @ 8000 ft: 201 mph
Cruise 55% @ 8000 ft: 178 mph
Stall Speed: 58 mph
Takeoff Distance: 575 ft
Landing Distance: 500 ft
Rate of Climb: 1,600 fpm
Ceiling: 19,500 ft
Range 75% @ 8000 ft: 780 sm
Range 55% @ 8000 ft: 945 sm
RV-8A
Engine: 200 hp
Prop: Hartzell 2 Blade C/S
Span: 24 ft
Length: 20 ft 10 in
Height: 7 ft 4 in
Wing Area: 116 sq ft
Empty Weight: 1067 – 1120 lbs
Gross Weight: 1800 lbs
Wing Loading: 15.5 lb/sq ft
Power Loading: 12 – 9 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 125 lbs
Top Speed: 219 mph
Cruise 75% @ 8000 ft: 208 mph
Cruise 55% @ 8000 ft: 184 mph
Stall Speed: 58 mph
Takeoff Distance: 500 ft
Landing Distance: 500 ft
Rate of Climb: 1,800 fpm
Ceiling: 21,500 ft
Range 75% @ 8000 ft: 770 sm
Range 55% @ 8000 ft: 930 sm
Engine: Lycoming O-360, 200 hp
Wing span: 7 m
Wing area: 10.1 sq.m
MAUW: 1080 kg
Empty weight: 484 kg
Fuel capacity: 166 lt
Max speed: 357 kph
Cruise speed: 341 kph
Minimum speed: 82 kph
Climb rate: 9.5 m/s
Seats: 2
Fuel consumption: 40 lt/hr
Kit price (1998): $13,000
Vans RV-7
The RV-7 is the pre-punched fuselage of the RV-9 and the pre-punched wings and tail of the RV-8 married together. It comes in tail wheel or nosewheel, and sliding or tilt up canopy. The RV-7/7A replaced the RV-6/6A.
About 70% of our customers prefer side by side seating and the RV-7/7A has a roomy cockpit that will easily accept two 6’ + adults with sufficient leg, head and elbow room to stay comfortable for three to four hours at a time. The seating arrangement puts both occupants on an equal footing – standard dual controls and optional dual brakes give either occupant full control with equal visibility.
The RV-7/7A retains all the traditional RV virtues. It is an all-around sport airplane, with excellent cross-country capability, fine aerobatic qualities and superior handling. A typical RV-7 can hold two FAA standard pilots, 100 lbs. of baggage and full tanks: 42 gallons. At the aerobatic gross weight of 1600 lbs., the RV-7/7A complies with the +6/-3G standards of the FAA’s Aerobatic Category and can still carry two people, making it possible for a new pilot to get aerobatic instruction before he or she starts rolling and looping.
Both sliding and tip-up canopies are available. Both may be opened for taxi ventilation.
All RVs are capable of very short take-offs and landings and the RV-7/7A is no exception. Equipped with any Lycoming engine between 150 and 200 hp, and either a fixed-pitch or constant-speed propeller, it will leave the ground quickly and climb at impressive rates. The rugged fixed steel landing gear (tailwheel or tri-gear) makes it possible to operate from almost any airstrip, including grass or dirt.
RV-7
Engine: 160 hp
Prop: Hartzell 2 Blade C/S
Span: 25 ft 0in.
Length: 20 ft 4 in.
Height: 5 ft 10 in
Wing Area: 121 sq ft
Empty Weight: 1061 – 1114 lbs
Gross Weight: 1800 lbs
Wing Loading: 14.8 lb/sq ft
Power Loading: 12.0 – 9.0 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 100 lbs
Top Speed: 201 mph
Cruise 75% @ 8000 ft: 191 mph
Cruise 55% @ 8000 ft: 172 mph
Stall Speed: 58 mph
Takeoff Distance: 650 ft
Landing Distance: 500 ft
Rate of Climb: 1,400 fpm
Ceiling: 18,500 ft
Range 75% @ 8000 ft: 835 sm
Range 55% @ 8000 ft: 1,025 sm
RV-7
Engine: 180 hp
Prop: Hartzell 2 Blade C/S
Span: 25 ft 0in.
Length: 20 ft 4 in.
Height: 5 ft 10 in
Wing Area: 121 sq ft
Empty Weight: 1061 – 1114 lbs
Gross Weight: 1800 lbs
Wing Loading: 14.8 lb/sq ft
Power Loading: 12.0 – 9.0 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 100 lbs
Top Speed: 209 mph
Cruise 75% @ 8000 ft: 199 mph
Cruise 55% @ 8000 ft: 179 mph
Stall Speed: 58 mph
Takeoff Distance: 575 ft
Landing Distance: 500 ft
Rate of Climb: 1,650 fpm
Ceiling: 20,500 ft
Range 75% @ 8000 ft: 775 sm
Range 55% @ 8000 ft: 950 sm
RV-7
Engine: 200 hp
Prop: Hartzell 2 Blade C/S
Span: 25 ft 0in.
Length: 20 ft 4 in.
Height: 5 ft 10 in
Wing Area: 121 sq ft
Empty Weight: 1061 – 1114 lbs
Gross Weight: 1800 lbs
Wing Loading: 14.8 lb/sq ft
Power Loading: 12.0 – 9.0 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 100 lbs
Top Speed: 216 mph
Cruise 75% @ 8000 ft: 206 mph
Cruise 55% @ 8000 ft: 186 mph
Stall Speed: 58 mph
Takeoff Distance: 500 ft
Landing Distance: 500 ft
Rate of Climb: 1,900 fpm
Ceiling: 22,500 ft
Range 75% @ 8000 ft: 765 sm
Range 55% @ 8000 ft: 935 sm
RV-7A
Engine: 160 hp
Prop: Hartzell 2 Blade C/S
Span: 25 ft 0 in
Length: 20 ft 4 in
Height: 7 ft 10 in
Wing Area: 121 sq ft
Empty Weight: 1077 – 1130 lbs
Gross Weight: 1800 lbs
Wing Loading: 14.8 lb/sq ft
Power Loading: 12.0 – 9.0 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 100 lbs
Top Speed: 199 mph
Cruise 75% @ 8000 ft: 189 mph
Cruise 55% @ 8000 ft: 170 mph
Stall Speed: 58 mph
Takeoff Distance: 650 ft
Landing Distance: 500 ft
Rate of Climb: 1,350 fpm
Ceiling: 17,500 ft
Range 75% @ 8000 ft: 825 sm
Range 55% @ 8000 ft: 1015 sm
RV-7A
Engine: 180 hp
Prop: Hartzell 2 Blade C/S
Span: 25 ft 0 in
Length: 20 ft 4 in
Height: 7 ft 10 in
Wing Area: 121 sq ft
Empty Weight: 1077 – 1130 lbs
Gross Weight: 1800 lbs
Wing Loading: 14.8 lb/sq ft
Power Loading: 12.0 – 9.0 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 100 lbs
Top Speed: 207 mph
Cruise 75% @ 8000 ft: 197 mph
Cruise 55% @ 8000 ft: 177 mph
Stall Speed: 58 mph
Takeoff Distance: 575 ft
Landing Distance: 500 ft
Rate of Climb: 1,600 fpm
Ceiling: 19,500 ft
Range 75% @ 8000 ft: 765 sm
Range 55% @ 8000 ft: 940 sm
RV-7A
Engine: 200 hp
Prop: Hartzell 2 Blade C/S
Span: 25 ft 0 in
Length: 20 ft 4 in
Height: 7 ft 10 in
Wing Area: 121 sq ft
Empty Weight: 1077 – 1130 lbs
Gross Weight: 1800 lbs
Wing Loading: 14.8 lb/sq ft
Power Loading: 12.0 – 9.0 lb/hp
Engine: 150-200 hp
Propeller: Fixed or C/S
Fuel Capacity: 42 US gal
Baggage: 100 lbs
Top Speed: 213 mph
Cruise 75% @ 8000 ft: 204 mph
Cruise 55% @ 8000 ft: 183 mph
Stall Speed: 58 mph
Takeoff Distance: 500 ft
Landing Distance: 500 ft
Rate of Climb: 1,850 fpm
Ceiling: 21,500 ft
Range 75% @ 8000 ft: 755 sm
Range 55% @ 8000 ft: 925 sm
Vans RV-6 / Aeronautical Industrial Engineering and Project Management Company Ltd. / AIEP Air Beetle / T18
Soon after the RV-4 proved that a two seat RV was practical, prospective customers began asking for a side-by-side RV.
When the demand became too big to ignore, Van went back to the drafting board. Using what he’d learned from the RV-3 and RV-4, he designed the RV-6.
He made it 43 inches wide and gave it a baggage compartment behind the seats. The wing on the RV-4 worked so well that there was no point in changing it, so he didn’t. The canopy was a forward opening bubble that closed almost seamlessly and the fuel capacity was increased.
The RV-6 made its first flight in 1985. When all the flight testing was done, it was only three miles per hour slower than the RV-4.
One limit to RV sales had always been the fact that they were all tailwheel airplanes. Installing a nose wheel solved the problem. The RV-6A featured a very simple tricycle gear, with steel rod main gear legs and a free castoring nosewheel. The nosegear leg was supported by the steel engine mount and required no complicated steering mechanisms or shock absorbers. The modification resulted in very little weight gain and almost negligible performance loss.
After the RV-6A was flying, Van’s designed a sliding canopy option on both the RV-6 and RV-6A.
Kits were priced at $11,810-12,565, and a quick-build kit at $19,320-19,995.
Eustace Bowhay, of Salmon Arm, BC, is a pilot with vast experience in both land and water aircraft. He carefully researched the matter and decided that the RV-6 had the potential to be an excellent floatplane. After consulting engineers, he designed a float installation and submitted it to the Canadian authorities for engineering approval. The Canadian Ministry of Transport determined that the RV-6 was strong enough, without modification, to handle the added stresses and loads imposed by flying off water. Cruise speeds, with the 180 hp Lycoming and constant speed prop, were 150 statue miles per hour. The water handling characteristics were excellent and the airplane was easy to land and taxi on land or water.
After flying the airplane on both wheels and straight floats for two years, Eustace and Jim decided they could have the best of both worlds, and installed amphibious floats. These worked just as well.
In 2005, Eustace, then over 80, decided that it was time to step out of the cockpit. C-GHAY was converted back to wheels and sold. Eustace died in 2006
Aeronautical Industrial Engineering And Project Management Company Ltd. / AIEP, in Nigeria was established 1979 to assemble kits of the Van’s RV-6A, known locally as Air Beetle and used by the Nigerian Air Force as the T18 trainer.
The RV 6s normal limit of plus or minus 6g, fully aerobatic in the sports category. The carburetted 160 hp Lycoming 0 320H2AD. Empty weight is 1010 lbs and the 1600 lb MAUW and full fuel of 144 litres.
Climb speed of 90 kts brings only about 2350 rpm, with around 1200 fpm indicated. This RV 6 will climb at 1600 fpm at MAUW at its best angle speed of 65 kts. Cruise at 75 percent power is slightly better than 150 kts, not much slower than full power.
Variation:
Aviation Industries of Iran AVA-202
RV-6
Engine: Lycoming O-320, 150 hp
Span: 23 ft
Length: 20 ft 2 in
Height: 5 ft 3 in
Wing Area: 110 sq ft
Empty Weight: 965 lbs
Gross Weight: 1600 lbs
Wing Loading: 14.5 lb/sq ft
Power Loading: 10 lb/hp
Engine: 150-180 hp
Propeller: fixed or C/S
Fuel Capacity: 38 US gal
Baggage: 60 lbs
Top Speed: 197 mph
Cruise 75% @ 8000 ft: 186 mph
Cruise 55% @ 8000 ft: 168 mph
Stall Speed: 55 mph
Takeoff Distance: 550 ft
Landing Distance: 500 ft
Rate of Climb: 1,355 fpm
Ceiling: 15,800 ft
Range 75% @ 8000 ft: 775 sm
Range 55% @ 8000 ft: 950 sm
RV-6
Engine: Lycoming O-320, 160 hp
Span: 23 ft
Length: 20 ft 2 in
Height: 5 ft 3 in
Wing Area: 110 sq ft
Empty Weight: 965 lbs
Gross Weight: 1600 lbs
Wing Loading: 14.5 lb/sq ft
Power Loading: 10 lb/hp
Engine: 150-180 hp
Propeller: fixed or C/S
Fuel Capacity: 38 US gal
Baggage: 60 lbs
Top Speed: 201 mph
Cruise 75% @ 8000 ft: 190 mph
Cruise 55% @ 8000 ft: 171 mph
Stall Speed: 55 mph
Takeoff Distance: 535 ft
Landing Distance: 500 ft
Rate of Climb: 1,500 fpm
Ceiling: 17,400 ft
Range 75% @ 8000 ft: 775 sm
Range 55% @ 8000 ft: 950 sm
RV-6
Engine: 180 hp
Span: 23 ft
Length: 20 ft 2 in
Height: 5 ft 3 in
Wing Area: 110 sq ft
Empty Weight: 965 lbs
Gross Weight: 1600 lbs
Wing Loading: 14.5 lb/sq ft
Power Loading: 10 lb/hp
Engine: 150-180 hp
Propeller: fixed or C/S
Fuel Capacity: 38 US gal
Baggage: 60 lbs
Top Speed: 209 mph
Cruise 75% @ 8000 ft: 198 mph
Cruise 55% @ 8000 ft: 178 mph
Stall Speed: 55 mph
Takeoff Distance: 475 ft
Landing Distance: 500 ft
Rate of Climb: 1,790 fpm
Ceiling: 20,800 ft
Range 75% @ 8000 ft: 720 sm
Range 55% @ 8000 ft: 880 sm
RV-6A
Engine: 150 hp
Span: 23 ft
Length: 19 ft 9 in
Height: 6 ft 8 in
Wing Area: 110 sq ft
Empty Weight: 985 lbs
Gross Weight: 1650 lbs
Wing Loading: 15 lb/sq ft
Power Loading: 10.3 lb/hp
Engine: 150-180 hp
Propeller: fixed or C/S
Fuel Capacity: 38 US gal
Baggage: 60 lbs
Top Speed: 195 mph
Cruise 75% @ 8000 ft: 184 mph
Cruise 55% @ 8000 ft: 166 mph
Stall Speed: 55 mph
Takeoff Distance: 560 ft
Landing Distance: 500 ft
Rate of Climb: 1,305 fpm
Ceiling: 14,750 ft
Range 75% @ 8000 ft: 760 sm
Range 55% @ 8000 ft: 875 sm
RV-6A
Engine: 160 hp
Span: 23 ft
Length: 19 ft 9 in
Height: 6 ft 8 in
Wing Area: 110 sq ft
Empty Weight: 985 lbs
Gross Weight: 1650 lbs
Wing Loading: 15 lb/sq ft
Power Loading: 10.3 lb/hp
Engine: 150-180 hp
Propeller: fixed or C/S
Fuel Capacity: 38 US gal
Baggage: 60 lbs
Top Speed: 199 mph
Cruise 75% @ 8000 ft: 188 mph
Cruise 55% @ 8000 ft: 169 mph
Stall Speed: 55 mph
Takeoff Distance: 535 ft
Landing Distance: 500 ft
Rate of Climb: 1,450 fpm
Ceiling: 16,300 ft
Range 75% @ 8000 ft: 760 sm
Range 55% @ 8000 ft: 875 sm
RV-6A
Engine: 180 hp
Span: 23 ft
Length: 19 ft 9 in
Height: 6 ft 8 in
Wing Area: 110 sq ft
Empty Weight: 985 lbs
Gross Weight: 1650 lbs
Wing Loading: 15 lb/sq ft
Power Loading: 10.3 lb/hp
Engine: 150-180 hp
Propeller: fixed or C/S
Fuel Capacity: 38 US gal
Baggage: 60 lbs
Top Speed: 207 mph
Cruise 75% @ 8000 ft: 196 mph
Cruise 55% @ 8000 ft: 176 mph
Stall Speed: 55 mph
Takeoff Distance: 485 ft
Landing Distance: 500 ft
Rate of Climb: 1,740 fpm
Ceiling: 19,700 ft
Range 75% @ 8000 ft: 705 sm
Range 55% @ 8000 ft: 810 sm
Vans RV-4
Of the Van’s RV series, the RV-4 was by far the most popular. The two-seat RV-4 was developed from the company’s single-seat RV-3 and the philosophy behind the design of the RV-4 was to have a two-seat aircraft that handled as close as possible to the single-seat RV-3. When the RV-4 first flew in August, 1979, the result was a tandem seating arrangement, which allowed the frontal area to be kept to a minimum, and gave it a top speed of only about 8 knots less than the RV-3. Further, its handling characteristics are said to be “virtually identical” a result that surprised even the Oregon-based kit manufacturer.
The RV-4 is an aerobatic, two-place tandem, low wing monoplane of aluminum monocoque (stressed skin) construction. The propeller is a Cassidy Pacesetter 200 wood prop, which experience with the RV-3 has proven to have excellent overall performance. The engine used was a new Lycoming 0-320. Fuel is carried in two integral wing leading edge tanks. The standard canopy is a single-piece bubble which opens to the side.
It is flown from the front seat only, but the kit includes a stick for the rear-seater. It is designed for engines of 150-160 horsepower, although engines as small as 125 hp and as large as 180 work well and are commonly installed.
The RV-4 is capable of “sport” aerobatics. It was reported that around 600 were flying worldwide and the kit price was $10,905.
Engine: Lycoming 150 hp
Prop: fixed pitch wood
Span: 23 ft
Length: 20 ft 4 in
Height: 5 ft 5 in
Wing Area: 110 sq ft
Empty Weight: 905 – 913 lbs
Gross Weight: 1500 lbs
Wing Loading: 13.64 lb/sq ft
Power Loading: 10.0 – 8.33 lb/hp
Engine: 150-180 hp
Propeller: Fixed or C/S
Fuel Capacity: 32 US gal
Baggage: 50 lbs
Top Speed: 201 mph
Cruise 75% @ 8000 ft: 189 mph
Cruise 55% @ 8000 ft: 171 mph
Stall Speed: 48 mph
Top Speed: 200 mph
Cruise 75% @ 8000 ft: 188 mph
Cruise 55% @ 8000 ft: 170 mph
Stall Speed: 54 mph
Takeoff Distance: 475 ft
Landing Distance: 425 ft
Rate of Climb: 1,500 fpm
Ceiling: 18,000 ft
Range 75% @ 8000 ft: 640 sm
Range 55% @ 8000 ft: 790 sm
Engine: Lycoming 160 hp
Prop: fixed pitch wood
Span: 23 ft
Length: 20 ft 4 in
Height: 5 ft 5 in
Wing Area: 110 sq ft
Empty Weight: 905 – 913 lbs
Gross Weight: 1500 lbs
Wing Loading: 13.64 lb/sq ft
Power Loading: 10.0 – 8.33 lb/hp
Engine: 150-180 hp
Propeller: Fixed or C/S
Fuel Capacity: 32 US gal
Baggage: 50 lbs
Top Speed: 205 mph
Cruise 75% @ 8000 ft: 193 mph
Cruise 55% @ 8000 ft: 174 mph
Stall Speed: 48 mph
Top Speed: 204 mph
Cruise 75% @ 8000 ft: 192 mph
Cruise 55% @ 8000 ft: 173 mph
Stall Speed: 54 mph
Takeoff Distance: 450 ft
Landing Distance: 425 ft
Rate of Climb: 1,650 fpm
Ceiling: 19,500 ft
Range 75% @ 8000 ft: 640 sm
Range 55% @ 8000 ft: 790 sm
Engine: Lycoming 180 hp
Prop: fixed pitch wood
Span: 23 ft
Length: 20 ft 4 in
Height: 5 ft 5 in
Wing Area: 110 sq ft
Empty Weight: 905 – 913 lbs
Gross Weight: 1500 lbs
Wing Loading: 13.64 lb/sq ft
Power Loading: 10.0 – 8.33 lb/hp
Engine: 150-180 hp
Propeller: Fixed or C/S
Fuel Capacity: 32 US gal
Baggage: 50 lbs
Top Speed: 213 mph
Cruise 75% @ 8000 ft: 201 mph
Cruise 55% @ 8000 ft: 182 mph
Stall Speed: 48 mph
Top Speed: 212 mph
Cruise 75% @ 8000 ft: 200 mph
Cruise 55% @ 8000 ft: 180 mph
Stall Speed: 54 mph
Takeoff Distance: 400 ft
Landing Distance: 425 ft
Rate of Climb: 1,950 fpm
Ceiling: 23,000 ft
Range 75% @ 8000 ft: 590 sm
Range 55% @ 8000 ft: 725 sm
All Aero 