PZL

PZL-110 Koliber

The PZL‑110 Koliber is a light, two‑seat, high‑wing trainer and sport aircraft produced by the Polish aerospace company PZL‑Mielec. Its development began in the early 1970s as a response to the growing demand for an economical, easy‑to‑maintain airplane suitable for aero‑clubs, flight schools, and private owners. The prototype first flew on 25 May 1975, and series production started in 1977, continuing until the early 1990s with more than 250 units built.

Key features include an all‑metal construction, a fixed tricycle landing gear, and a 115 hp Lycoming O‑235 engine that provides stable handling and modest performance – a cruise speed of around 160 km/h and a range of 800 km. The Koliber’s spacious cabin, large windows, and forgiving stall characteristics have made it a popular platform for pilot training and recreational flying. Its straightforward design also allows for easy modification, leading to variants equipped with floats or advanced avionics.

In Polish aviation history the Koliber symbolizes the post‑war revitalisation of domestic aircraft manufacturing. It helped sustain a network of local aero‑clubs, contributed to pilot proficiency, and demonstrated PZL’s ability to produce reliable, cost‑effective aircraft for the general aviation market.

Classification

Design & Classification

Manufacturer
PZL
Wikidata ID
Q11802035