CT-134 Musketeer

Infobox Aircraft
name= CT-134 Musketeer


caption= CT-134As from 3 Canadian Forces Flying Training School at CFB Portage la Prairie, Manitoba, 1982.
type= Basic trainer
national origin= United States
manufacturer= Beech Aircraft Corporation
designer=
first flight=
introduced= 1971
retired= 1992
status=
primary user= Canadian Armed Forces
more users=
produced=
number built= 48
unit cost=
developed from= Beechcraft Musketeer
variants with their own articles=

The Beechcraft CT-134 Musketeer was a military training derivative of the Musketeer built by Beechcraft for the Royal Canadian Air Force. The CT-134 was a single engine, low-wing, four-seat light aircraft with fixed landing gear and a limited aerobatic capability.

Design and development

In the early 1960s the Royal Canadian Air Force’s standard elementary training aircraft was the de Havilland DHC-1 Chipmunk. Flight instruction was completed by student pilots on the DHC-1 before they progressed to the then-brand-new Canadair CT-114 Tutor jet trainer. A decision was made by RCAF HQ to remove the DHC-1s from service and not replace them, as it was felt that the CT-114 was easy enough to fly that initial training was not needed. The CT-114 quickly developed a wash-out rate of near 95% amongst student jet pilots and it was clear that an elementary trainer was needed. Due to the RCAF’s previous customer relationship with Beechcraft while operating that company's Expeditor twin-engine aircraft, a hasty purchase of twenty-four 1971 model B23 Musketeers was made.cite web |url = http://www.airforce.forces.gc.ca/site/equip/historical/musketeerlst_e.asp |title = Beech CT-134 Musketeer |date = 2004-04-06 |author = Air Force Public Affairs / Department of National Defence |accessdate = 2007-09-17 ] The first CT-134 arrived at CFB Portage la Prairie on March 23, 1971.Milberry, Larry: "Sixty Years - The RCAF and Air Command 1924-1984", page 384. McGraw Hill Ryerson Canav Books, 1984. ISBN 0-07-549484-1]

The new trainers were designated CT-134 Musketeer in the then Canadian Armed Forces. The aircraft purchased were standard Model B23s equipped with the O-360-A4G engine of 180 bhp, modified by the addition of a cowling strake, horizontal stabilizer strake and ventral fin to improve spin recovery performance. They were initially serial numbered as 13401-13424, but were re-numbered 134001-134024 to avoid confusion with other CF aircraft serial numbers.

The initial batch of CT-134s was replaced in late 1981 with a purchase of twenty-four more aircraft. These were 1982 model Beechcraft C23 Sundowners and were designated by the CF as CT-134A Musketeer II. These were numbered 134025-134048.

The CT-134 was approved for limited aerobatics, including loops, rolls, chandelles and lazy eightsDAOT: "C-12-134-000/MC-000 Canadian Forces Technical Order Operating Checklist Musketeer CT 134,", CFTMPC, 10 Jul 79]

Operational history

Both batches of Musketeers served with 3 Canadian Forces Flying Training School and the Canadian Forces Flying Instructor School at CFB Portage la Prairie Manitoba and the Canadian Forces Central Flying School in Winnipeg until they were replaced by Slingsby Fireflys operated under contract by Bombardier Aerospace in 1992. During their 21 years of service the CT-134 and CT-134A fleet at 3 CFFTS trained about 5000 Canadian military pilot graduates.

In operational service the CT-143 suffered very few accidents. One of the few serious accidents occurred on 23 March 1990 when Musketeer 134229 had an engine failure on take-off from Erickson Municipal Airport at Erickson, Manitoba while giving familiarization flights to Royal Canadian Air Cadets. The accident was caused by fuel starvation and the aircraft was written off.Milberry, Larry: "Aircom: Canada's Air Force", pages 82-83. Canav Books, 1991. ISBN 0-921922-05-0 6]

Maintenance of the CT-134 fleet was primarily carried out by the CFB Portage la Prairie Base Aircraft Maintenance Engineering Organization, with Depot Level Inspection and Repair (DLIR) being conducted by Field Aviation at Calgary International Airport in Calgary, Alberta.

Upon retirement the CT-134s and CT-134As were not sold for flying use due to the structural problems they all suffered from years of aerobatics. cite web|url = http://www.rcaf.com/aircraft/trainers/musketeer/index.php?name=Musketeer|title = Beech CT-134 MUSKETEER|accessdate = 2008-04-01|last = AEROWARE / RCAF.com |authorlink = |year = undated] Instead they were donated to museums or used for air force and civil maintenance training. Some CT-134s still serve as monuments at a few current and former Canadian Forces Bases as well as Royal Canadian Legion halls, a distinction held by very few light aircraft in this class.

In Canadian military service the aircraft was referred to by student and instructor pilots by the nickname Muskrat.

Variants

;CT-134:Military version of the B24 Musketeer, powered by a Lycoming O-360-A4G powerplant of 180 hp, 24 built.;CT-134A:Military version of the C24 Sundowner, powered by a Lycoming O-360-A4K powerplant of 180 hpDAOT: "C-12-134-A00/MC-000 Canadian Forces Technical Order Operating Checklist Musketeer CT 134A,", CFTMPC, 06 Jan 83] , 24 built.

Military operators

;CAN
* Canadian Armed Forces/Canadian Forces
** 3 Canadian Forces Flying Training School
** Canadian Forces Central Flying School
** Canadian Forces Flying Instructor School

pecifications

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=C-12-134-000/MC-000 Operating Checklist Musketeer CT 134, CFTMPC, 10 Jul 79
crew=Student and instructor
capacity=2 passengers
payload main=
payload alt=
length main= 25 ft 8.5 in
length alt= 7.85 m
span main= 32 ft 9 in
span alt= 10.00 m
height main= 8 ft 2.4 in
height alt= 2.50 m
area main= 146 ft²
area alt= 13.6 m²
airfoil=NACA 63A415 [ cite web|url = http://www.ae.uiuc.edu/m-selig/ads/aircraft.html|title = The Incomplete Guide to Airfoil Usage|accessdate = 2008-06-28|last = Lednicer|first = David|authorlink = |year = 2007|month = October]
empty weight main= 1,560 lb
empty weight alt= 707 kg
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 2,450 lb (normal) / 2,150 lb (aerobatic)
max takeoff weight alt= 1,110 kg/ 974 kg
more general=
engine (prop)= Lycoming O-360-A4G
type of prop=air-cooled, 4-cylinder piston engine
number of props=1
power main= 180 hp
power alt= 136 kW
power original=
max speed main=124 knots
max speed alt= 231 km/h
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main= 152 knots
never exceed speed alt= 283 km/h
range main= 675 miles
range alt=1,257 km
ceiling main= 13,000 ft
ceiling alt= 3,962 m
climb rate main= 880 ft/min
climb rate alt= 268 m/min
loading main=16.8 lb/ft²
loading alt= 82 kg/m²
thrust/weight=
power/mass main=13.6 lb/hp
power/mass alt=8.2 kg/kW
more performance=
armament=
avionics=

ee also

aircontent
related=
* Beechcraft Musketeer
* Beechcraft Duchess

similar aircraft=
* T-41 Mescalero

lists=
see also=

References

External links

* [http://www.airforce.forces.gc.ca/site/equip/historical/musketeerlst_e.asp Canadian Forces Official CT-134 Muskateer history page]