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“Each day anew my team and I face up to the challenge of making sure pro. Contents • • • • • • • • • • • • • • • • Design and development [ ] The Metroliner was an evolution of the turboprop-powered business aircraft. Ed Swearingen, a (FBO), started the developments that led to the Metro through gradual modifications to the and business aircraft, which he dubbed Excalibur.

A new (but with a similar nose) and were then developed, married to salvaged and rebuilt Queen Air wings and, and Twin Bonanza; this became the SA26 Merlin, more-or-less a Excalibur. Through successive models (the SA26-T Merlin IIA and SA26-AT Merlin IIB) the engines were changed to, then turboprops. These were marketed as business aircraft seating eight to ten passengers.

An all-new aircraft was built and named the SA226-T Merlin III with a new nose, wings, landing gear, and inverted inlet Garrett engines. Ultimately a stretch of the Merlin III was designed, sized to seat 22 passengers and called the SA226-TC Metro.

Because regulations limited an airliner to no more than 19 seats if no was to be carried, the aircraft was optimized for that number of passengers. The standard engines offered were two TPE331-3UW turboprops driving three-bladed. A corporate version called the SA226-AT Merlin IVA was also marketed and initially sales of this version were roughly double that of the Metro. Prototype construction of the Metro began in 1968 and the first flight was on August 26, 1969. Swearingen Aircraft encountered financial difficulties at this stage, and late in 1971 Fairchild (which was marketing the Metro and building its wings and engine nacelles), bought 90% of Swearingen and the company was renamed Swearingen Aviation Corporation.

It was at this point that the previously cash-strapped company was able to put the Metro into production. In 1974, the original Metro models were replaced by the SA226-TC Metro II after about 20 Metros and about 30 Merlin IVAs had been built. Among the changes made were larger, squared-oval windows and optional provision for a small (RATO) rocket in the tail cone, this being offered to improve takeoff performance out of 'hot & high' airfields in the event of an engine failure. Structure Of Quality Circle Pdf. The Metro and Metro II were limited to a maximum weight of 12,500 pounds (5,670 kg) in the USA and countries using, and 5,700 kg in countries using. When this restriction was lifted the Metro II was re-certified as the Metro IIA in 1980 with a maximum weight of 13,100 pounds (5,941 kg) and the Metro II's TPE331-3 engines replaced by -10 engines of increased power. SA227-AT Merlin IVC freighter conversion VH-UZA in service, c.