The 1931 three seat Sky-Lark was designed by Arnold H Galvin, a Lincoln School of Flying A&E instructor, and built as a class project.
It was registered N11050 to John Evans of Lincoln. Power was a 120hp Cessna-Anzani.
The last design of the Lincoln Aircraft Corp was the parasol wing Lincoln Playboy of 1931. A two place pusher powered by a 25 hp Lincolcn Rocket engine, the aircraft could attain a top speed of 80 mph and cruis at 70 mph. The price in 1931 was US$800.
Page acquired the rights to the New Swallow and redesigned this as the three-seater Lincoln-Page LP-3 in 1928, an attempt to catch up with developments in light aircraft design.
The first sport single-seater of note in the early 1920s was the Lincoln “Sport,” which was a biplane originall~ developed as a homebuilt by S.S. Swanson in 1923. It was put into limited production by the Lincoln Aircraft Co., of Lincoln, Nebraska, when Swanson became chief engineer there. The production model died for lack of a market because there were still plenty of cheap World War 1 surplus single seaters around for the sporting types. The Lincoln design was perpetuated as a homebuilt, however, when the plans were published in Modern Mechanics magazine in the early 1930s.
Capable of 100 mph and fully aerobatic.
Engine: Bristol Cherub III.
Max speed: 100 mph.
Between 1923 and 1925 offered the Lincoln-Standard Tourabout, a three-seat rework of the Standard J.1 of 1916.
Ray A. Page established Nebraska Aircraft Corporation at Lincoln, Nebraska, during the First World War, and was a builder of the Lincoln Standard, a two-bay biplane circa 1920.
Replica
Mexicana Lincoln Standard Replica
Four cylinder, single & double ignition, four stroke engines for light & ultralight aircraft & motorgliders.
L-2400 DA3BX
Four cylinder, four stroke engines for light & experimental aircraft with double magneto ignition, with 92hp; produce 2400 EFI engine with liquid cooled cylinder heads, dual electronic ignition, 100hp take off power at 2900rpm; type certification per JAR-22 sub-part H; dev. turbocharged version of C-2400 EFI
L-2400 DE3 X
Cycle: 4 stroke
No cylinders: 4
Bore: 97 mm
Stroke: 82 mm
Compression: 8.5
Displacement: 2424 cc
Cooling: air/liquid
Ignition: Double magneto
Weight: 87.5 kg
Max pwr: 90 hp at 3200 rpm
Price 1998: 20 700 DM
The Limbach L2000 is a series of German piston aero-engines designed and built by Limbach Flugmotoren. First run circa 1980, they are four-cylinder, four-stroke, air-cooled horizontally opposed, piston engines with a power output of 75 to 80 hp (56 to 60 kW).
Variants:
L2000 DA
Certified in 1989 as a double-ignition tractor engine with carburettor in the back, top location, alternator in the front, starter in the front. 75 hp (56 kW)
L2000 E0
Certified in 1980 as a single-ignition tractor engine with carburettor in the back, bottom location, alternator in the back, starter in the back. 80 hp (60 kW)
L2000 EA
Certified in 1980 as a single-ignition tractor engine with carburettor in the back, top location, alternator in the front, starter in the front. 80 hp (60 kW)
L2000 EB
Certified in 1980 as a single-ignition tractor engine with two carburettors in the back, bottom location, alternator in the back, starter in the back. 80 hp (60 kW)
L2000 EC
Certified in 1980 as a single-ignition pusher engine with carburettor in the back, bottom location, alternator in the back, starter in the back. 80 hp (60 kW)
Applications:
Aeromot AMT-100 Ximango
AV Leichtflugzeuge Vagabund
Grob G 109
Hoffmann HK 36 Super Dimona
ICA IS-28
JPM 01 Médoc
Lucas L-6A
Scheibe SF 36A (EA)
Valentin Taifun
Weller UW-9 Sprint
Whisper Aircraft Whisper
Specifications:
L200 E0
Type: Four-cylinder, four-stroke air-cooled flat piston engine
Bore: 90 mm
Stroke: 78.4 mm
Displacement: 1.994 cc
Length: 627 mm
Width: 775 mm
Height: 415 mm
Dry weight: 70 kg
Fuel type: Mogas and 100LL Octane petrol
Cooling system: Air-cooled
Power output: 51 kW at 3,000 rpm (max continuous)
Compression ratio: 8:5 – 8:9:1
L-200 EA
Cycle: 4 stroke
No cylinders: 4
Bore: 90 mm
Stroke: 78.4 mm
Compression: 8.6
Displacement: 1994 cc
Cooling: air
Ignition: magneto
Weight: 69 kg
Max pwr: 80 hp at 3400 rpm
Price 1998: 16 400 DM
Four cylinder, single & double ignition, four stroke engines for light & ultralight aircraft & motorgliders.
Four cylinder, single & double ignition, four stroke engines for light & ultralight aircraft & motorgliders.
