Short Tucano
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Tucano | |
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Short Tucano of No. 72 Squadron RAF |
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Type | Trainer aircraft |
Manufacturer | Short Brothers |
Status | Active |
Primary users | Royal Air Force Kenya Air Force Kuwait Air Force |
Developed from | Embraer EMB-312 Tucano |
The Short Tucano T Mk 1 is a two seat turboprop basic trainer used by the RAF. It is also used by the Air Forces of Kenya and Kuwait.
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[edit] Design and development
The Short Tucano was developed by the British Short Brothers company in order to meet a requirement to replace the Jet Provost as the basic trainer for the RAF, as laid down in Air Staff Target 412. It is an adaptation of the Embraer EMB-312 Tucano fitted with the more powerful 1100 shp Garrett turboprop engine in place of the EMB-312's 750 shp Pratt & Whitney Canada PT6 engine, to give higher climb performance.
Aside from a different powerplant, the other differences between the Short Tucano and the EMBRAER Tucano are:
- A strengthened airframe.
- A new cockpit layout similar to the Hawk advanced trainer.
- A four, as opposed to three, bladed propeller.
- Ventral airbrake and restyled wingtips.
- The fitting of Martin-Baker MB 8LC ejection seats for both crew.
- A new oxygen system
- A new flight data recorder
- A modified canopy
The Tucano was selected in 1985 in preference to the Swiss Pilatus PC-9 and the British Hunting Firecracker. The first Garrett engined Tucano flew in Brazil on 14 February 1986, with the first Shorts built production aircraft flying on 30 December 1986 [1] . The decision to replace the 750 PT-6 engine used in the standard EMBRAER model with the 1100shp Garrett TPE331-12B engine and "bird-strike" proofing of the cockpit canopy to UK standards (combined with the fitting of Martin Baker ejection seats) caused a number of problems which delayed the introduction of the aircraft, so that it was 1989 by the time it came into service. Most of the delay was understandable, given the cumulative effect of the major changes to the original design.
[edit] Operational history
Since first deliveries to the RAF in 1989, the Tucano has been operated primarily from No 1 Flying Training School at RAF Linton-on-Ouse to provide basic fastjet flying training to RAF and RN student pilots. The deployment is officially to 72 (Reserve) Squadron and 207 (Reserve) Squadron. Student pilots fly around 130 hours during their training course on the Tucano before progressing to the Hawk T1 aircraft at RAF Valley.
In service the Tucano has proven to be 70% cheaper to operate than its predecessor. With a greater range and endurance than the Jet Provost, it can fly two consecutive sorties before being refuelled. One of the key performance requirements was that it can climb to 15,000ft in six minutes, in comparison to the Jet Provost's 15 minutes; this gave considerably more training value for each one-hour sortie.
[edit] Variants
- Tucano T1
- Two-seat basic trainer for the RAF.
- Tucano Mk.51
- Export version for Kenya.
- Tucano Mk.52
- Export version for Kuwait.
[edit] Operators
[edit] Specifications (Tucano)
Data from Jane's All the World's Aircraft, 1988-1989 [1]
General characteristics
- Crew: 1-2
- Length: 32 ft 4 in (9.86 m)
- Wingspan: 37 ft 0 in (11.28 m)
- Height: 11 ft 1¾ in (3.40 m)
- Wing area: 208 ft² (19.3 m²)
- Empty weight: 4,447 lb (2,017 kg)
- Loaded weight: lb (kg)
- Useful load: lb (kg)
- Max takeoff weight: 7,220 lb (3,275 kg)
- Powerplant: 1× Garrett TPE331-12B turboprop, 1,100 shp (820 kW)
Performance
- Never exceed speed: 280 kn (322 mph, 518 km/h)
- Maximum speed: 274 kn (315 mph, 507 km/h) (at 10,000-15,000 ft)
- Cruise speed: 220 knots (253 mph, 407 km/h) (economy cruise)
- Stall speed: 69 kn (80 mph, 128 km/h) (flaps and gear down)
- Range: 900 nmi (1,035 miles, 1,665 km)
- Service ceiling 34,000 ft (10,365 m)
- Rate of climb: 3,510 ft/min (17.8 m/s)
- Wing loading: 28.6 lb/ft² (140 kg/m²)
- Power/mass: 0.152 hp/lb (0.250 kW/kg)
Armament
- Provision for 1,000 lb (454 kg) of stores on four underwing hardpoints
[edit] See also
Related development
Comparable aircraft
Related lists
[edit] References
- ^ a b Taylor, JWR (Editor) (1988). Jane's All the World's Aircraft, 1988-1989. Coulsdon, Surrey: Jane's Information Group. ISBN 0 7106-0867-5.
[edit] External links
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