The Beechcraft CT-134 Musketeer was a military training version of the Beechcraft Musketeer built for the Canadian Armed Forces, a single-engine, low-wing, four-seat light aircraft with fixed landing gear and limited aerobatic capability. The Royal Canadian Air Force needed an elementary trainer after removing the de Havilland Chipmunk from service, and a hasty purchase of twenty-four B23 Musketeers in 1971 produced the first CT-134s, modified with a cowling strake, a horizontal stabilizer strake and a ventral fin to improve spin recovery and powered by a 180 horsepower Lycoming O-360-A4G engine. A second batch of twenty-four 1982 model C23 Sundowners, designated CT-134A Musketeer II, replaced the first in late 1981. Both batches served at Portage la Prairie and Winnipeg until Slingsby Fireflys replaced them in 1992, after training about 5,000 military pilot graduates at one school alone, and pilots nicknamed the aircraft the Muskrat. Retired airframes were not sold for flying because of structural problems from years of aerobatics; they went to museums or maintenance training, and some stand as monuments.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Beechcraft CT-134 Musketeer (Wikipedia)
Of Make
Source Beechcraft CT-134 Musketeer (Wikipedia)
Sources
1. Beechcraft CT-134 Musketeer (Wikipedia)
Design and development, first delivery
The first CT-134 arrived at CFB Portage la Prairie on March 23, 1971.
Lead, type
The CT-134 was a single engine, low-wing, four-seat light aircraft with fixed landing gear and a limited aerobatic capability.
Specifications (CT-134A), powerplant
Powerplant: 1 × Lycoming O-360-A4K 4-cylinder air-cooled horizontally-opposed piston engine, 180 hp (130 kW)
Operational history, retirement
Some CT-134s still serve as monuments at a few current and former Canadian Forces Bases
Specifications (CT-134A), empty weight
Empty weight: 1,494 lb (678 kg)
Specifications (CT-134A), maximum take-off weight
Max takeoff weight: 2,450 lb (1,111 kg)
Specifications (CT-134A), maximum speed
Maximum speed: 128 kn (147 mph, 237 km/h)
Lead, builder
The Beechcraft CT-134 Musketeer is a military training derivative of the Musketeer built by Beechcraft for the Canadian Armed Forces.
Of Make: Beechcraft, Lead
The Beechcraft CT-134 Musketeer is a military training derivative of the Musketeer built by Beechcraft for the Canadian Armed Forces.
Exemplifies: Aviation, Lead, mode
The Beechcraft CT-134 Musketeer is a military training derivative of the Musketeer built by Beechcraft for the Canadian Armed Forces.
In Group: Single-Engine Piston Light Aircraft, Lead, group
The CT-134 was a single engine, low-wing, four-seat light aircraft with fixed landing gear and a limited aerobatic capability.
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