The Swearingen Merlin, also known as the Fairchild Aerospace Merlin was initially built by the American manufacturer Swearingen Aircraft and afterward by Fairchild. It was a pressurized business aircraft powered by twin-turboprop engines. The Merlin first flew in April 1965 and was produced until 1998.

United States
1965 to: 1998
US$0.44 million (1969)
Collins Avionics
2x Garrett AiResearch TPE-331-10U-503G
900 horsepower
Max Cruise Speed:
300 knots
556 Km/h
Approach Speed (Vref):
92 knots
Travel range:
1,938 Nautical Miles
3,589 Kilometers
Fuel Economy:
Service Ceiling:
27,000 feet
Rate of Climb:
2700 feet / minute
13.72metre / second
Take Off Distance:
1300 metre - 4,265.04 feet
Landing Distance:
900 metre - 2,952.72 feet
Max Take Off Weight:
6,000 Kg
13,228 lbs
Max Landing Weight:
5,670 Kg
12,500 lbs
Max Payload:
1,945 Kg
4,288 lbs
Fuel Tank Capacity:
650 gallon
2,461 litre
Baggage Volume:
3 m3 / 106 ft3
Seats - Economy / General:
9 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
1.45 metre - 4.76 feet
Cabin Width:
1.57 metre - 5.15 feet
Cabin Length:
7.75 metre - 25.43 feet
Exterior Length:
12.85 metre - 42.16 feet
Tail height:
5.13 metre - 16.83 feet
Fuselage Diameter:
1.6 metre - 5.25 feet
Wing Span / Rotor Diameter:
14.10 metre - 46.26 feet
Wing Tips:
No Winglets

The Merlin was a development of initial modification programs of Swearingen Aircraft. Edward Swearingen, an American aeronautical engineer started the design that concluded to the Merlin through step-by-step enhancements to the Twin Bonanza and Queen Air utility aircraft of Beechcraft, which was named Excalibur. Later on, a hybrid aircraft designed with a new fuselage and vertical fin was built which was designated as the SA26 Merlin. It was the prototype piston-engined version of the aircraft. The SA26-T Merlin II was a prototype powered with two turboprop engines. The Merlin IIA was the first production version with two Pratt and Whitney engines while the Merlin IIB was powered by two Garrett AiResearch engines.

The Merlin IIIC with SFAR-41 standard can accommodate two crew members and up to nine passengers on board. It has an external length of 12.85 meters, an external height of 2.7 meters, and a fuselage diameter of 1.6 meters. The tail height is 5.13 meters and the wheelbase is 3.6 meters. It has a wingspan of 14.10 meters and a wing area of 25.78 square meters. The cabin height is 1.45 meters, the cabin length is 7.75 meters and the cabin width is 1.57 meters. The aircraft has an empty weight of 3,697 kg, a maximum takeoff weight of 6,001 kg, and a fuel capacity of 648 US gal.

Two Garrett AiResearch TPE-331-10U-503G engines power the Merlin. It is a single-shaft turboprop with an integral gearbox, a two-stage centrifugal compressor, reverse annular combustors and a three-stage axial turbine. Each engine produces a maximum thrust of 900 shaft horsepower and drives a four-bladed Dowty Type R.321 propeller with 2.69 meters of diameter. The aircraft has a maximum cruise speed of 300 knots at 10,000 feet and a stall speed of 92 knots with flaps and landing gear down. The range at 26,000 feet with six occupants is 1,938 nautical miles and the ferry range is 2,239 nautical miles. It can fly up to 27,000 feet and can climb at a rate of 2,650 feet per minute.

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