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Oberlerchner JOB 15 performance and specifications
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History
Drawing on past experience in the design and production of gliders and
sailplanes, Josef Oberlerchner Holzindustrie built its first powered
design in 1957. Of wooden construction, the prototype JOB 5 was a
side-by-side two-seater powered by a 95-hp (71-kW) Continental C9012F
engine and, after completion of more than 100 hours of development flying
during 1958-9, the decision to embark upon series production was taken. A
number of designs alterations were incorporated, however the JOB15 was
evolved, larger than the prototype and with a third seat added. The
original all-wood fuselage was replaced by a steel-tubular structure with
glassfibre and fabric covering, enlarged vertical tail surfaces were
fitted, and the selected engine was the 135-hp (101-kW) Avco Lycoming
O-290-D2B. A hook was fitted to add glider-towing to the original roles of
training, touring and limited aerobatics. The prototype JOB 15 flew late
in 1960 and two more were completed in 1962 before the JOB 15-150 was
introduced, powered by a 150-hp (112-kW) Avco Lycoming O-320-A2B engine.
Eleven were built, together with 10 JOB 15/2s, before the production
ceased in June 1966. The specification applies to the JOB 15.
Specifications
Type:
three-seat light monoplane
Powerplant:
one 150-hp (112-kW) Avco Lycoming O-320-A2B flat-four piston engine
Performance:
maximum speed 146 mph (235 km/h); maximum cruising speed 121 mph (195
km/h); range 510 miles (821 km)
Weights:
empty 1,314 lb (596 kg); maximum take-off 2,050 lb (930 kg)
Dimensions:
span 33
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