A 1925 convertible cargo/passenger two-seat biplane, registered N699. With an all-wood fuselage, the passenger compartment was convertible to mail or cargo hold.
Engine: Salmson Z-9, 260 hp
Wingspan: 29’6″
Length: 23’3″
Speed: 130 mph
Range: 400 mi
Seats: 3
Four-Runner is an original design based on the squarish but fast Wittman Tailwind and Thorp T-18. A four-place cabin, high-wing monoplane, the fuselage and tail are 4130 steel tubing, fabric-covered. Wings, flaps and ailerons are pop-riveted aluminum. Gear legs are from a Cessna 170B.
Built in 1974, the registration is N73CW.
Engine: IO-360 AlA, 180-hp
Wingspan: 25’3”
Gross Wt: 2250 lb
Empty Wt: 1250 lb
Fuel capacity: 50 USG
Top speed: 175 mph
Cruise: 155 mph
Stall (clean) 56 mph
Climb rate 1100 fpm
Range 1000 sm
The Wood CF-1 was a single place open cockpit biplane, registered N46W. Built in 1965, CF-1 N65W C/N 1 was registered N46W and powered by a Lycoming 0-290 engine.
Built in 1929, the Woodford Special was described to CAA simply as “An arch-wing monoplane of Special Design.”
A single place, open cockpit, high-wing monoplane powered by a 110hp Anzani, The registration N899E s/n OL2-29 was cancelled on 6 January 1933.
In 1963 Dick Wood of Kansas City MO. Built the single place cabin biplane, the Liten Vinge (Little Wing), registered N201DW. The Liten Vinge was aerobatic capable and first flew in May 1963.
Engine: Continental C-85-8, 85hp
Wingspan: 22’0″
Length: 17’0″
Useful load: 465 lb
Max speed: 125 mph
Cruise speed: 115 mph
Range: 400 mi
Seats: 1
The 1955 CR-1 Little Monster built by Charles A Wood of Clay Center KS., N2752C, used some Piper J-3 parts used in construction. It was a high wing monoplane with a two place cabin.
Engine: Continental A-65, 65 hp
Wingspan: 25’9″
Length: 19’0″
Max speed: 120 mph
Cruise speed: 95 mph
Stall: 40 mph
Range: 400 mi
Seats: 2
Equipped with a 40 hp ABC inline four, built by Tsoe K. Wong. Designed and built in the UK in 1913, and initially flown there, the craft was later shipped to Kuala Lumpur, in what was then known as the Federated Malay States. The craft met its end on July 19 1914, due to a demo flight that concluded with a fairly emphatic crash.
A single seat partially enclosed autogyro. Composite body, airframe of round tubing. Steel parts are T45 and powder coated, alloy members are anodized. Large rudder. Two versions: one with 17 USG tank; one with 15 USG tank and low profile seat to allow a full blown canopy. Designed by Chris Jullian. Engine: Rotax 582 or Honda. Prop: 3 blade wood. Rotor blades: 23’ Rotor Hawk aluminium.
Rotax 532
Min speed: 20 mph
Cruise: 60-80 mph
Top speed: 115 mph
Gross wt: 1432 lbs
Width: 5’
Height: 7’6”
Length: 12’
The Wolseley Aries III or A.R.9 was a British nine-cylinder, air-cooled radial aero engine that first ran in 1933, it was designed and built by Wolseley Motors. Intended for the military trainer aircraft market few were produced as Wolseley withdrew from the aero-engine market in 1936, see Airspeed Ltd.. A larger capacity version was known as the Wolseley Scorpio, further enlarged versions, the Leo and Libra were test run but did not fly.
Variants:
A.R.9 Mk I
203 horsepower (151 kW).
A.R.9 Mk II
205 horsepower (153 kW). Higher permissible rpm version of Mk I.
A.R.9 Aries Mk III
225 horsepower (168 kW), low boost supercharger fitted.
Scorpio I
250 horsepower (186 kW), (230 bhp at 2,250 rpm), increased bore (111mm x 120 mm) to give a displacement of 9,477 cc, increased compression ratio. Reduction gearing.
Scorpio II and III
250 horsepower (186 kW), designed to run on 87 octane fuel with 6.5:1 ratio.
Leo
280 horsepower (209 kW), few details, not flown or produced.
Libra
390 hp at 6,000 ft. 725 lbs (329 kg). Tested but not flown or produced.
Applications:
Airspeed Envoy
Hawker Tomtit
Specifications:
A.R.9 Aries Mk III
Type: 9-cylinder, single row, radial engine
Bore: 4.19 in (106 mm)
Stroke: 4.75 in (120 mm)
Displacement: 588.6 cu in (9.654 L)
Length: 42 in (1,067 mm)
Diameter: 41.25 in (1,048 mm)
Dry weight: 510 lb (231 kg)
Valvetrain: Overhead valve
Supercharger: Single speed, geared induction fan, slight positive pressure
Fuel type: Petrol
Cooling system: Air-cooled
Reduction gear: Epicyclic spur geared, right-hand tractor, reduction ratio 0.629:1
Power output: 225 hp (168 kW) at 2,475 rpm (maximum power)
Specific power: 0.38 hp/cu in (17.4 kw/L)
Compression ratio: 5.35:1
Power-to-weight ratio: 0.49 hp/lb (0.72 kW/kg)
The Wolseley Aquarius I or A.R.7 was a British seven-cylinder, air-cooled radial aero engine that first ran in 1933, it was designed and built by Wolseley Motors. Intended for the military trainer aircraft market few were produced, as Wolseley withdrew from the aero-engine market in 1936.
Applications:
Hawker Tomtit
A.R.7
Type: 7-cylinder, single row, radial engine
Bore: 4.188 in (106 mm)
Stroke: 4.75 in (120 mm)
Displacement: 458 cu in (7.5 L)
Length: 36.4 in (925 mm)
Diameter: 40.25 in (1,029 mm)
Dry weight: 375 lb (170 kg)
Valvetrain: Overhead valve
Fuel type: Petrol
Cooling system: Air-cooled
Reduction gear: Direct drive, left-hand tractor
Power output: 170 hp (127 kW) at 2,475 rpm (maximum power)
Specific power: 0.37 hp/cu in (16.9 kw/L)
Compression ratio: 5.35:1
Power-to-weight ratio: 0.45 hp/lb (0.75 kW/kg)
All Aero 