Beechcraft

Queen Air 88

The Beechcraft Queen Air 88 is a twin‑engine, piston‑driven utility aircraft that first flew in 1960 and entered production the following year. Developed from the earlier Model 65 Travel Air, the Queen Air series was designed to bridge the gap between light single‑engine planes and larger pressurized transports, offering greater payload, range, and cabin comfort for corporate, commuter, and military customers. The 88 variant is powered by two Lycoming TIO‑540‑A1C6D engines delivering 295 hp each, driving constant‑speed propellers. Its all‑metal low‑wing construction, retractable landing gear, and spacious cabin—typically configured for six to eight passengers—contribute to stable cruise performance of about 220 kt and a maximum range of roughly 1,200 nm. Notable design features include a balanced control system, optional de‑icing boots, and provisions for auxiliary fuel tanks, making the aircraft adaptable to diverse environments. Over 2,600 Queen Airs were built, and the 88 model became a workhorse for regional airlines, air‑ambulance services, and government agencies worldwide. Its blend of reliability, operating economy, and versatility solidified the Queen Air’s reputation as a cornerstone of mid‑century general aviation and paved the way for Beechcraft’s later King Air turboprop lineage.

Classification

Production & History

Units Produced
47

Design & Classification

Country of Origin
Manufacturer
Beechcraft
Developer
Beechcraft
Wikidata ID
Q18018683