Canadair Sabre

Canadair Sabre

infobox Aircraft
name = CL-13 Sabre
type =Fighter
manufacturer =Canadair




caption =Canadair Sabre
designer =
first flight = 9 August 1950
introduced = 1950
retired =1980, Portugal
status =
primary user = Royal Canadian Air Force
more users = United States Air Force Royal Air Force Luftwaffe
produced =
number built =1,815
unit cost =
developed from = F-86 Sabre
variants with their own articles =

The Canadair Sabre was a fighter jet built by Canadair under licence from California-based North American Aviation Inc. The resulting variant produced was considered one of the finest "dogfighters" of its day. [Milberry 1986, p. 127, 148-149.] It was produced until 1958, and was eventually replaced with the Canadair CF-104.

Design and development

In 1948, the Canadian government decided to re-equip the RCAF with the F-86 Sabre and Canadair was contracted to produce them in Montreal, Quebec, Canada. An initial batch of ten aircraft was ordered for tool verification. The Korean War changed this to a production batch of 100 aircraft. Canadair slowly built up its production facility to make all components with related equipment obtained from other Canadian suppliers. Canadair gave the Sabre the project number CL-13.

There were six versions of the F-86 Sabre produced at Canadair. The sole Sabre Mk 1 was essentially the same as the North American Sabre F-86A. It had a General Electric J47-GE-13 turbojet of 5,200 lbf (23 kN) thrust. The Sabre Mk 2 had the same engine, although after the first 20 aircraft were produced, the remainder of the production run was distinguished in having power-assisted controls and an "all-flying" tailplane. The sole Sabre Mk 3 was the first of the Canadian Sabres to use the Avro Canada Orenda turbojet (Orenda 3 with 6,000 lbf (27 kN) thrust). The Sabre Mk 4 retained the General Electric engine and was destined for the RAF and was later passed on to other overseas air forces. The Sabre Mk 5 was the next production version, equipped with an Orenda 10 with 6,500 lbf (29 kN) thrust. A change to the Orenda 14 with 7440 lbf (33 kN) powered the Sabre Mk 6. The designation Sabre Mk 7 was mainly experimental. From 1950 to 1958, a total of 1,815 CL-13 Sabres were built at the Canadair plant in Montreal.

Operational history

The second generation of Canadair Sabre aircraft was the Mk 2, with 350 produced from 1952–1953. The RCAF received 290 of these newer aircraft. During the first half of 1952, the remaining 60 Mk 2s were supplied to the USAF for use in the Korean War. Most RCAF Mk 2 Sabres were utilized in the air defence role with NATO's No. 1 Air Division in Europe, proving itself to be an outstanding dogfighter. Others were assigned to the training role at bases in Canada. After replacement by the Sabre 5, just over 200 surviving Sabre 2s were overhauled in the UK and supplied in equal numbers to the Greek and Turkish air forces.

In mid-1952, the Sabre Mk 4 went into production with the first one flown on 28 August 1952. Apart from some minor structural and systems changes, including improved air-conditioning and gun sight, the Mk 2 and the Mk 4 were identical. Of 438 Mk 4s built, approximately 70 were used temporarily by the RCAF, all surviving examples being passed to the RAF. The other Sabre 4s went directly to the RAF under a mutual aid program, equipping 11 RAF squadrons. The majority served in West Germany with NATO, with two squadrons being based in the UK as part of Fighter Command. The Sabre Mk 4 served with the RAF until mid-1956 when they were replaced by Hawker Hunters. The survivors were overhauled in the UK, fitted with '6-3' wing modifications and handed to the USAF (which had funded these aircraft) which in turn passed most of them on to Italy's and Yugoslavia's air forces.

On 30 July 1953, the first Sabre Mk 5 flew with the Orenda 10 engine, which gave it a clear rate of climb and ceiling advantage over earlier variants. Other Mk 5 improvements included a new oxygen system and improved maneuverability and low-speed characteristics achieved by increasing the wing chord by six in (15.2 cm) at the root and three in. (7.2 cm) at the wing tip along with fitting a small vertical wing fence. Canadair would produce 370 Mk 5s with the majority designated for use in the RCAF’s Air Division squadrons in Europe to replace the Mk 2s. A total of 75 RCAF Sabre 5s were transferred to the German Luftwaffe during 1957.

The Canadair Sabre Mk 6 was the last variant and considered to be the "best" production Sabre ever built. [ Joos 1971, p.3.] It was equipped with a two-stage Orenda engine developing 7,275 lb. (3,302 kg.) of static thrust. Its altitude performance and climb rate was enhanced over the Mk 5 and the installation of a slotted wing gave it excellent low-speed characteristics. The first production model was completed on 2 November 1954 and ultimately 655 were built with production terminating on 9 October 1958. A total of 390 Mk 6s went to the RCAF with the majority replacing the existing Canadair Sabres at the Air Division squadrons in West Germany and France. The main air threats to NATO in the 1950s in Central Europe were the early variants of the Soviet MiG- the MiG-15, MiG-17, MiG-19 and MiG-21. Based on the Korean War experience, the selection of the Mk 6 Sabre to provide an effective opposition to the MiG threat proved to be a logical one. Canada’s commitment to NATO was to provide 12 squadrons located at four bases – two in France (Marville and Grostenquin) and two in West Germany (Zweibrücken and Baden Soellingen). Initially, the contribution consisted of only Sabre aircraft, however, later it was decided to include the Avro CF-100 aircraft in the defense package to provide a night and all-weather fighter capability. For the majority of their NATO service, the Canadair Sabre was considered to be the best dogfighter in European skies.Fact|date=December 2007

In addition to the RCAF deliveries, 225 Canadair Mk 6 Sabres were exported to the West German Luftwaffe, six were delivered to the Colombian Air Force and 34 went to the South African Air Force.

Canadair Sabres were dominant in the two major conflicts in which they were employed: the Korean War where F-86 Sabres racked up an impressive 11-1 kill record and the Indo-Pakistani War of 1971. In January 1966, Germany sold 90 of its Canadian Mk 6 Sabres to Iran. These aircraft were quickly transferred to Pakistan and became the main day fighter of the Pakistan Air Force.

Women's speed records

In 1952, Jacqueline Cochran, then aged 47, decided to challenge the world speed record for women, then held by Jacqueline Auriol. She tried to borrow an F-86 from the USAF, but was refused. She was introduced to an RCAF Air Vice-Marshal who, with the permission of the Canadian Minister of Defence, arranged for her to borrow "19200", the sole Sabre 3. Canadair sent a 16-man support team to California for the attempt. On 18 May 1953, Ms. Cochran set a new 100 km speed record of 1050.15 km/h (652.5 mph). Later on 3 June, she set a new 15 km closed circuit record of 1078 km/h (670 mph). While she was in California, she exceeded 1270 km/h in a dive, and thus became the first woman to exceed the speed of sound.

Golden Hawks

The Golden Hawks were a Canadian aerobatic flying team that was established in 1959 to celebrate the RCAF's 35th anniversary and the "Golden" 50th anniversary of Canadian flight, which began with the AEA Silver Dart in 1909. Initially, a six-plane team flying brilliantly-painted metallic-gold Canadair Sabre Mk 5s, was envisioned as performing for only one year, but the Golden Hawks were so popular after their single 63-show season that the team was expanded. In the following year, another plane was added to the team, allowing for a five-plane main formation with two solo jets. The Golden Hawks continued performing for three more seasons, changing to the Mk 6 in 1961, until they were disbanded on 7 February 1964, having flown a total of 317 shows across North America. [ Dempsey 2002]

Variants

;Sabre Mk 1:One built, prototype F-86A.;Sabre Mk 2:350 built, F-86E-type, 60 to USAF, three to RAF, 287 to RCAF.;Sabre Mk 3:One built in Canada, test-bed for the Orenda 3 jet engine, various other structural modifications were made to accommodate the Orenda engine.;Sabre Mk 4:438 built, production: ten to RCAF, 428 to RAF as Sabre F 4.;Sabre Mk 5:370 built, F-86F-type with Orenda engine, all to RCAF, 75 later passed to Luftwaffe.;Sabre Mk 6:655 built, 390 to RCAF, 225 to Luftwaffe, six to Colombia and 34 to South Africa.

urvivors

Below is a list of museums or sites which have a Canadair Sabre on display:

* Royal Military College of Canada
* Reynolds-Alberta Museum
* Alberta Aviation Museum
* Luftwaffenmuseum der Bundeswehr
* Western Canada Aviation Museum
* Museum of Flight
* Royal Air Force Museum (Mk 4 RCAF 19666/RAF XB812 at Cosford)
* Duncan McDonald Memorial Gardens, Trenton, Ontario

A Mk 5 variant ‘BB+237’ is (as of July 2007) being restored for static display purposes at Neuhardenberg, Germany. This aircraft was built in 1954 and served with the RCAF in France before joining the West German Air Force until its retirement in 1962. [Flypast Magazine, August 2007, Key Publishing Ltd.]

Operators

*CAN
*COL
*GER
*flag|Greece|old
*HON
*ITA
*PAK
*flag|South Africa|1928
*TUR
*UK
*USA
*YUG: "See: F-86 and CL-13 Sabre Operators (dates, quantities, versions, and squadrons)"

pecifications (Sabre Mk 5)

aircraft specifications
plane or copter?=plane
jet or prop?=jet
ref=
crew=one, pilot
capacity=
payload main=
payload alt=
length main= 37 ft 6 in
length alt= 11.43 m
span main= 37 ft 1½ in
span alt= 11.32 m
height main= 14 ft 9 in
height alt= 4.49 m
area main=
area alt=
airfoil=
empty weight main= 10,638 lb
empty weight alt= 4,825 kg
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 17,560 lb
max takeoff weight alt= 7,965 kg
more general=
engine (jet)=Orenda 10
type of jet=turbojet
number of jets=1
thrust main=
thrust alt=
thrust original=
afterburning thrust main=
afterburning thrust alt=
max speed main= 696 mph
max speed alt= 1120 km/h
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=
range alt=
ceiling main= 50,700 ft
ceiling alt= 15,450 m
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=

guns=6× 0.50 in (12.7 mm) M2 Browning machine guns (1,602 rounds in total)
rockets=variety of rocket launchers; e.g: 2× Matra rocket pods with 18× SNEB 68 mm rockets each
missiles=2× AIM-9 Sidewinders
bombs=5,300 lb (2,400 kg) of payload on four external hardpoints, bombs are usually mounted on outer two pylons as the inner pairs are wet-plumbed pylons for 2× 200 gallons drop tanks to give the Sabre a useful range. A wide variety of bombs can be carried (max standard loadout being 2 x 1,000 lb bombs plus 2 drop tanks), napalm bomb canisters and can include a tactical nuclear weapon.

avionics=

ee also

aircontent
related=
* F-86 Sabre
* FJ Fury
similar aircraft=
* MiG-15
* Dassault Mystère
* Saab 29
sequence=
lists=
List of fighter aircraft
see also=

References

Notes

Bibliography

* Childerhose, R.J. "The F-86 Sabre". New York: Arco Publishing, 1965.
* Dempsey, Daniel V. "A Tradition of Excellence: Canada's Airshow Team Heritage". Victoria: High Flight Enterprises Ltd., 2002. ISBN 0-9687817-0-5.
* Flypast Magazine, August 2007, Key Publishing Ltd.
* Joos, Gerhard W. "Canadair Sabre Mk 1-6, Commonwealth Sabre Mk 30-32 in RCAF, RAF, RAAF, SAAF, Luftwaffe & Foreign Service". Kent, UK: OSprey Publications Limited, 1971. ISBN 0-85045-024-1.
* Milberry, Larry. "The Canadair Sabre". Toronto: CANAV Books, 1986. ISBN 0-9690703-7-3.
* Pickler, Ron and Milberry, Larry. "Canadair: the First 50 Years". Toronto: CANAV Books, 1995. ISBN 0-921022-07-7.

External links

* [http://www.warbirdalley.com/f86.htm Warbird Alley: F-86 Sabre page] - Information about F-86s still flying today
* [http://www.aviation-history.com/north-american/f86.html Sabre site]
* [http://home.att.net/~jbaugher1/p86_22.html Canadair Sabres in J.Baugher site]


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