
Israel Ludlow’s Jamestown Exposition Glider on floats during its unsuccessful trials on Hampton Roads, piloted by the aeronaut Capt. T. T. Lovelace and towed by the tug Potomac on August 21, 1907.

Israel Ludlow’s Jamestown Exposition Glider on floats during its unsuccessful trials on Hampton Roads, piloted by the aeronaut Capt. T. T. Lovelace and towed by the tug Potomac on August 21, 1907.

LSA legal
Cruise: 103 mph
Stall: 42 mph
Range: 645 sm
Rate of climb: 1200 fpm
Takeoff dist: 600 ft
Landing dist: 500 ft
Engine: Jabiru, 80 hp
HP range: 80-150
Fuel capacity: 20 USG
Empty weight: 618 lb
Gross weight: 990 lb
Length: 18.3 ft
Wing span: 26 ft
Wing area: 80 sq.ft
Cockpit width: 44 in
Landing gear: nose wheel

The US agent for plans and kits was Micro Technologies Inc.
Top speed: 220 mph
Cruise: 165 mph
Stall: 60 mph
Range: 600 nm
Rate of climb: 1000 fpm
Takeoff dist: 1300 ft
Landing dist: 500 ft
Service ceiling: 14,000 ft
Engine: Lycoming O-320, 150 hp
HP range: 150-180
Fuel capacity: 50 USG
Empty weight: 1000 lb
Gross weight: 1600 lb
Height: 5 ft
Length: 18 ft
Wing span: 26 ft
Wing area: 90 sq.ft
Seats: 2
Landing gear: nose

Designed in 1988, the retractable L7 can fit up to 200 hp without modification. The 5 x 4 ft door permits large item loading, or parachute dropping.
Top speed: 142 mph
Cruise: 110 mph
Stall: 44 mph
Range: 560 nm
Rate of climb: 500 fpm
Takeoff dist: 1540 ft
Landing dist: 1700 ft
Service ceiling: 13,00 ft
Engine: Lycoming O-235, 115 hp
HP range: 115-180
Fuel capacity: 30 USG
Empty weight: 1150 lb
Gross weight: 1750 lb
Height: 8 ft
Length: 21 ft
Wing span: 34 ft
Wing area: 133 sq.ft
Seats: 2
Landing gear: nose or tail wheel/retractable

A motorglider with either nose or tail wheel. It can be flown with a 28 ft wing and O-235 engine. A removable wing extension was optional. The wings fold and detach.
The US agent for plans and kits was Micro Technologies Inc.
Top speed: 110 mph
Cruise: 98 mph
Stall: 44 mph
Range: 621 nm
Rate of climb: 450 fpm
Takeoff dist: 1480 ft
Landing dist: 1600 ft
Service ceiling: 14,000 ft
Engine: Limbach, 80 hp
Fuel capacity: 20 USG
Empty weight: 990 lb
Gross weight: 1480 lb
Height: 8 ft
Length: 22 ft
Wing span: 15 ft
Wing area: 180 sq.ft
Seats: 2
Landing gear: nose or tail wheel
Engine: Lycoming O-235
Wing span: 9 m
Wing area: 13 sq.m
MAUW: 750 kg
Empty weight: 490 kg
Fuel capacity: 150 lt
Max speed: 260 kph
Cruise speed: 230 kph
Minimum speed: 100 kph
Climb rate: 3 m/s
Seats: 2
Fuel consumption: 28 lt/hr
Plan price (1998): 2500 Fttc

Designed as a 2, 3, or 4 place with and identical airframe. Was available as either nose or tail wheel.
The US agent for plans and kits was Micro Technologies Inc.
Top speed: 165 mph
Cruise: 118 mph
Stall: 54 mph
Range: 620 nm
Rate of climb: 520 fpm
Takeoff dist: 1450 ft
Landing dist: 1600 ft
Service ceiling: 13,000 ft
Engine: Lycoming O-320, 150 hp
HP range: 108-180
Fuel capacity: 50 USG
Empty weight: 1150 lb
Gross weight: 1900 lb
Height: 6 ft
Length: 20 ft
Wing span: 31 ft
Wing area: 133 sq.ft
Seats: 2-4
Landing gear: nose
1998-2001: 7 Allee des Acacias, 603330 Lagny Le Sec, France
Offers plans and some components to construct L.5 side-by-side two-seat (or 3/4-seat) low-wing monoplane (first flown 1976) and L.6 tandem two-seat low-wing monoplane (first flown 1991).

In 1922 John Leeming started to design his fifth glider, which became the LPW Glider, as the cheapest possible way to get airborne, but even the cost of materials worried him. He knew that Avro had made 8,340 Avro 504K trainers, and many were then stored but unwanted.
Leeming approached Avro to seek scrap materials, and met Clement Wood of the Sales staff, who turned out to be a kindred spirit. They raided the “scrap pile” and probably got major components needing minor repairs. The most costly items were two bicycle wheels that cost full price.
The LPW Glider was built by John Leeming, Tom Prince, and Clement Wood who later formed the Lancashire Aero Club.
The original was converted from an Avro 504K trainer.

Leeming cut off the nose and front cockpit, and faired it in. Wing panels were fixed to the top fuselage longerons and braced from upper pylons and the bottom of the fuselage.
The thin wings had two spars, so the lift bracing wires also added torsional stiffness; a picture shows that the outer wings twisted nose-up.
The result was an enclosed body rather than the later open framework. But gliding performance wouldn’t be too good, with a large fuselage and so many bracing wires. The glider flew on 24 May 1924 from Alexandra Park Aerodrome in Manchester being towed into the air by a car. Based on simple assumptions, it probably stalled at 25 knots, had minimum sink of 3 knots at 30 knots, and maximum glide 12 to 1.

Flying took place at Alexandra Park aerodrome, in the middle of Manchester, starting 24 May 1924, car towing, having trouble with the long grass.
Rope length was quoted as 200 feet, so straight hops were all that was possible. Several pilots flew on many occasions. Leeming crashed the LPW in September 1924 when flying for press photographers on a windier day than usual. Struggling to fly level in the gusts, he didn’t notice how high he had reached so quickly.

The driver looked back and saw the glider above, probably feared that the rope would fall on him, stopped the car and ran away. The glider stalled, and didn’t recover, probably through the wind gradient; Leeming wasn’t hurt, but the glider was badly smashed.
The wreck was rebuilt, fitted with an engine, and used for taxiing practice for new recruits, but it never flew. Leeming says that it was too heavy, probably too nose-heavy.


A 75% scale replica of Sopwith Camel F9509 designed and built by John Lowther.
Engine: Webster 5-cyl radial.
Blenheim, New Zealand.
Built a Sopwith Camel replica.