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PZL Warszawa-Okecie M-26 Iskierka

A 1986 single-piston-engined, retractable-gear design intended for military pilot selection and civilian pilot training, the M-2600 prototype flew on July 18, 1986, powered by a 153kW engine. Some assemblies from the M-20 Mewa (licence-built Piper Seneca) were used in the Iskierka’s wing, tail unit, landing gear, and electrical systems.

PZL Mielec M 26 Iskierka
Engine: Lycoming AEIO 540 L1B, 221 hp
Length: 27.231 ft / 8.3 m
Height: 9.843 ft / 3.0 m
Wingspan: 28.215 ft / 8.6 m
Wing area: 150.696 sq.ft / 14.0 sq.m
Max take off weight: 3087.0 lb / 1400.0 kg
Weight empty: 2072.7 lb / 940.0 kg
Max. weight carried: 1014.3 lb / 460.0 kg
Max. speed: 184 kts / 340 km/h
Landing speed: 59 kts / 110 km/h
Cruising speed: 167 kts / 310 km/h
Initial climb rate: 1574.8 ft/min / 8.00 m/s
Wing loading: 20.50 lb/sq.ft / 100.0 kg/sq.m
Range: 875 nm / 1620 km
Crew: 2

 

 


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