Trainer Aircraft | Page 2 | World Defense

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LM | T-33 T-Bird/Shooting Star


T-33 T-Bird:Shooting Star  .jpg


  • Origin
  • USA
  • Type
  • two-seat jet trainer
  • Max Speed
  • 966 km/h / 600 mph
  • Max Range
  • 860 km / 1,345 miles
  • Dimensions
  • span 11.85 m (38 ft 10.5 in) length 11.51 m (37 ft 9 in) height 3.56 m (11 ft 8 in)
  • Weight
  • empty 3667 kg (8,0841 b); maximum take-off 6551 kg (14,442 Ib)
  • Powerplant
  • one 2449-kg (5,400-lb) dry thrust Allison J33-A-35 turbojet
  • Armament
  • bombs, rockets, and gun pods
  • Operators:
Bolivia, Ecuador, Ecuador (AT-33), Iran, Mexico, Mexico (AT-33), Paraguay, Paraguay (AT-33), Thailand, Turkey
 

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Japan | Mitsubishi T-2



Mitsubishi T-2  .jpg

  • Origin
  • Japan
  • Type
  • supersonic advanced flying, weapon and combat trainer
  • Max Speed
  • 921 kt / 1,061 mph
  • Max Range
  • 2,600 km / 1,616 miles
  • Dimensions
  • span 7.88 m / 25 ft 10.2 in
  • length 17.86 m / 58 ft 7.1 in
  • height 4.39 m / 14 ft 4.8 in
  • Weight
  • empty 6,307 kg / 13,904 lb
  • maximum take-off 12,800 kg / 28,219 lb
  • Powerplant
  • two 3315-kg (7,308-lb) afterburning thrust Ishikawajima-Harima TF40-IHI-801A (Rolls-Royce/Turbomeca Adour Mk 801 A) turbofans
  • Armament
  • one 20-mm JM61 Vulcan six-barrel cannon with 750 rounds; provision for 2722 kg (6,000 lb) of disposable stores, including AAMs, ASMs, free-fall or guided bombs, rocket-launcher pods, drop tanks and ECM pods, carried on five external hardpoints and two wing tip stations
  • Operators:
  • Japan
 

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Nanchang K-8 Karakorum


Nanchang K-8 Karakorum  .jpg

  • Origin
  • China/Pakistan
  • Type
  • two-seat basic trainer and light ground attack aircraft
  • Max Speed
  • 497 mph/800 km/h
  • Max Range
  • 924 miles/1,487 km
  • Dimensions
  • span 31 ft 7 in/9.63 m, length 38 ft/11.58 m, height 13 ft 10 in/4.22 m
  • Weight
  • empty weight 5,924 lbs/2,687 kg, max take-off weight 9,546 lbs/4,330 kg
  • Powerplant
  • one AlliedSignal TFE731-2A-2A turbofan engine with 3,597 lbs static thrust (K-8J) Progress Al-25 turbofan engine with 4,946 lbs static thrust
  • Armament
  • 1x23mm cannon bay under the fuselage and four wing pylons for bombs, rocket pods, or missiles. Maximum weapons load 2,079 lbs/943 kg
  • Operators:
Bolivia, Myanmar, Sri Lanka, China, Egypt, Ghana, Morocco, Pakistan, Sudan, Tanzania, Venezuela, Namibia, Zambia, Zimbabwe
 

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Northrop T-38 Talon

Northrop T-38 Talon  .jpg


  • Origin
  • USA
  • Type
  • two-seat supersonic basic trainer
  • Max Speed
  • 745 kt / 858 mph
  • Max Range
  • 1759 km / 1,093 miles
  • Dimensions
  • span 7.70 m / 25 ft 3 in length 14.14 m / 46 ft 4.5 in height 3.92 m / 12 ft 10.5 in
  • Weight
  • empty 3254 kg / 7,174 lb max. take-off 5361 kg / 11,820 lb
  • Powerplant
  • two 1746-kg (3,850-ib) dry thrust General Electric J85-GE-5 turbojets
  • Armament
  • none
  • Operators: Germany, Portugal, Turkey, Taiwan, United States
 

Justin

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Pilatus PC-7 Turbo Trainer


Pilatus PC-7 Turbo Trainer  .jpg


  • Origin
  • Switzerland
  • Type
  • Tandem two-seat basic trainer
  • Max Speed
  • 264 mph / 425km/h
  • Max Range
  • 1 250 km / 777 miles
  • Dimensions
  • Span 34ft 1.5 in (10.40 m) length, 31 ft 11 in (9.75m) height, 10ft 67 in (3.21 m)
  • Weight
  • Empty 2,866 Ib (1 300kg); max. take-off (clean), 4,189lb (1 900kg)
  • Powerplant
  • Tandem two-seat basic trainer Whitney PT6A-25A turboprop
  • Armament
  • Six wing hardpoints permit external loads up to maximum of 5,952lb (2700kg)
  • Operators: Angola, Austria, Botswana, Bolivia, Myanmar, Brunei, Chile, France, Guatemala, Iran, Mexico, Malaysia, Netherlands, South Africa, Switzerland, United Arab Emirates, Uruguay

 

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Pilatus PC-9


Pilatus PC-9  .jpg


  • Origin
  • Switzerland
  • Type
  • tandem-seat multi-stage trainer
  • Max Speed
  • 300 kt / 345 mph
  • Max Range
  • 1,538 km / 955 miles
  • Dimensions
  • span 10.12 m / 33 ft 2.4 in length 10.18 m / 33 ft 4.8 in height 3.26 m / 10ft 8.3 in
  • Weight
  • empty 1,685 kg / 3,715 lb maximum take-off 3,200 kg / 7,055 lb
  • Powerplant
  • one 857-kW (1,150-shp) Pratt & Whitney Canada PT6A-62 turboprop flat-rated at 708 kW (950 shp)
  • Armament
  • as required and fitted by individual users, but not supplied by Pilatus; the aircraft can carry up to 1040 kg (2,293 Ib) of disposable stores, including bombs, cluster bombs, rocket-launcher pods, cannon or machine gun pods and drop tanks, on six external hardpoints
  • Operators: Angola, Australia, Myanmar, Cyprus, Greece (T-6A), Croatia, Saudi Arabia, Slovenia, Switzerland, Thailand, United States (T-6A)
 

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Rockwell International T-2C Buckeye

Rockwell International T-2C Buckeye  .jpg


  • Origin
  • USA
  • Type
  • general-purpose jet trainer
  • Max Speed
  • 460 kt / 530 mph
  • Max Range
  • 1,722 km / 1,070 miles
  • Dimensions
  • span 11.62 m / 38 ft 1.5 in length 11.67 m / 38 ft 3.5 in height 4.51 m / 14 ft 9.5 in
  • Weight
  • empty 3,681 kg / l8,115 lb maximum take-off 9,133 kg / 13,190 lb
  • Powerplant
  • two 1,338 kg / 2,950 lb dry thrust General Electric J85-GE-4 turbojets
  • Armament
  • provision for 1588 kg (3,500 Ibl of disposable stores, including light bombs, rocket-launcher pads and gun pads, carried on four external hardpoints
  • Operators: Venezuela
 

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SAAB 105

SAAB 105  .jpg


  • Origin
  • Sweden
  • Type
  • training/liaison aircraft with secondary attack capability
  • Max Speed
  • 415 kt / 478 mph
  • Max Range
  • 1,400 km / 870 miles
  • Dimensions
  • span 9.50 m / 31 ft 2 in
  • length 10.50 m / 34 ft 5.4 in
  • height 2.70 m / 8 ft 10.3 in
  • Weight
  • empty 2,510 kg / 5,534 lb
  • maximum take-off 4,050 kg / 8,929 lb
  • Powerplant
  • two 744-kg (1,640-lb) dry thrust Turbomeca Aubisque turbofans
  • Armament
  • provision for 700 kg (1,543 lb) of disposable stores, including two Saab Rb05 ASMs, or two 30-mm cannon pods, or 12 135-mm (5.31-in) rockets, or bombs, cluster bombs and rocket-launcher pods, on six external hardpoints
  • Operators: Austria (105OE), Sweden
 

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SIAI-Marchetti SF.260



SIAI-Marchetti SF.260  .jpg

  • Origin
  • Italy
  • Type
  • light trainer/tactical support aircraft
  • Max Speed
  • 165 kt / 190 mph
  • Max Range
  • 278 km / 173 miles
  • Dimensions
  • span 8.35 m / 27 ft 4.7 in
  • length 7.10 m / 23 ft 3.5 in
  • height 2.41 m / 7 ft 10.9 in
  • Weight
  • empty 770 kg / 1,698 lb
  • maximum take-off 1,300 kg / 2,866 lb
  • Powerplant
  • one194-kW (260-hp) Avco Lycoming 0-540-F4A5 flat-six piston engine
  • Armament
  • can include gun pods to provide two or four 7.62-mm (0.3-in) machine guns, fragmentation, general-purpose and practice bombs, flares, and one or two photo-reconnaissance pods or auxiliary drop tanks
  • Operators: Belgium, Brunei (Warrior), Burundi, Burundi (Warrior), Chad (Warrior), Ireland (Warrior), Ethiopia (SF.260TP), Haiti, Italy, Libya (Warrior), Philippines, Philippines, Singapore, Singapore (Warrior), United Arab Emirates, Tunisia, Tunisia (Warrior), Turkey, Uruguay, Venezuela, Zambia, Zimbabwe, Zimbabwe, Zimbabwe (Warrior)
 

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Soko G-2 Galeb

Soko G-2 Galeb  .jpg


  • Origin
  • Yugoslavia
  • Type
  • basic trainer
  • Max Speed
  • 439 kt / 505 mph
  • Max Range
  • 1,240 km / 771 miles
  • Dimensions
  • span 9.73 m / 31 ft 11.1 in
  • length 10.34 m / 33 ft 11.1 in
  • height 3.28 m / 10 ft 9.1 in
  • Weight
  • empty 2,620 kg / 5,776 lb
  • maximum take-off 4,300 kg / 19,480 lb
  • Powerplant
  • one 1134-kg (2,500-lb) dry thrust Rolls Royce Viper 11 Mk 226 turbojet
  • Armament
  • two 12.7-mm (0.5-in) machine gun with 80 rounds per gun; provision for 150-kg (331-Ib) bomblet containers, 100-kg (220-lb) bombs, 127-mm (5-in) rockets, and 55-mm (2,17-in) rocket-launcher pods carried on underwing racks
  • Operators: Libya, Serbia, Zambia
 

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Soko G-4 Super Galeb


Soko G-4 Super Galeb  .jpg


  • Origin
  • Yugoslavia
  • Type
  • basic trainer/light attack aircraft
  • Max Speed
  • 491 kt / 665 mph
  • Max Range
  • range 1900 km / 1,180 miles
  • Dimensions
  • span 9.88 m / 32 ft 5 in length including probe 12.25 m / 40 ft 2.25 in height 4.30 m / 14 ft 1.25 in
  • Weight
  • empty 3172 kg / 6,993 Ib maximum take-off 6300 kg / 13,889 Ib
  • Powerplant
  • one 1814-kg (4,000-lb) dry thrust Rolls Royce Viper Mk 632 turbojet
  • Armament
  • provision for one 23-mm GSh-23L two-barrel cannon with 200 rounds;provision for 2053 kg (4,526 Ib) of disposable stores, including AAMs, bombs, cluster bombs, dispenser weapons, napalm tanks, large-calibre rockets, rocket-launcher pods, drop tanks and ECM pods, carried on four external hardpoints
  • Operators: Bosnia and Herzegovina, Myanmar, Montenegro, Serbia
 

NightWolf

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Yak-130 (Mitten)

The Yakovlev Yak-130 is a subsonic two-seat afvanced jet trainer and light fighter orriginally developed by Yakovlev and Aermacchi.
1024px-Yakovlev_Yak-_130_%28modify%29.jpg


DIMENSIONS


Length, m
11.493
Height, m
4.76
Wing span, m
9.84
Wing area, m2
23.5
Wheel base, m
3.945
Wheel track, m
2.53
POWER PLANT: TURBOFAN ENGINE АI-222-25
Maximum thrust, kgf:
2 x 2,500
WEIGHT
Take-off weight of fully fuelled aircraft (w/o external stores), kg
7,250
Maximum take-off weight, kg
10,290
Fuel capacity:
• in internal tanks, kg
• in drop fuel tanks, kg

1,700
2 х 450
Maximum weight of combat load, kg
3,000
FLIGHT PERFORMANCE
Maximum true airspeed (w/o external stores), km/h
1,060
Maximum Mach Number, М
0.93
Maximum climb speed, m/s
65
Maximum angle of attack, deg.
35
Limit loads range (w/o external stores), g
+8 / -3
Service ceiling, m
12,500
Practical range (w/o drop fuel tanks), km
1,600
Maximum range (with 2 drop fuel tanks, Н=12,000 m), km
2,100
Maximum flight endurance (with two drop fuel tanks), h
3.0
Take-off run, m
550
Landing roll, m
750
Service life
10,000 flight hours /
30 years
 

NightWolf

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Aero L-59 Super Albatros

1200px-Aero.L159a.arp.jpg


General characteristics:

Crew: 2 (stud and instr.)
Length: 12.2 m
Wingspan: 9.54 m
Height: 4.77 m
Wing area: 18.8 sq. m
Empty weight: 4,030 kg
Max. takeoff weight: 7,000 kg
Powerplant: 1xLotarev DV-2 Turbofan

Performance:

Max. speed: 865 km/h (at 5000 m)
Stall speed: 185 km/h
Range: 2000 km (max internal and external fuel tanks)
Service сeiling: 11.800 m
Rate of climb: 28 m/s

Armament:

Guns: 1x GSh-23L (cannon in underfuselage pod)
Hardpoints: 4 underwing hardpoints with a capacity of inner hardpoints - 500 kg, outer hardpoints - 250 kg.
 

NightWolf

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SP-10

%D0%A1%D0%90%D0%A2_%D0%A1%D0%A0-10%2C_%D0%9C%D0%BE%D1%81%D0%BA%D0%B2%D0%B0_-_%D0%96%D1%83%D0%BA%D0%BE%D0%B2%D1%81%D0%BA%D0%B8%D0%B9_%28%D0%A0%D0%B0%D0%BC%D0%B5%D0%BD%D1%81%D0%BA%D0%BE%D0%B5%29_RP13960.jpg


General characteristics:


Origin: Russia
Crew: 2
Length: 9,59 m
Wingspan: 8,40 m
Height: 3,55 m
Gross weight: 2,400 kg
Max takeoff weight: 2,700 kg
Powerplant: 1 x Ivchenko AI-25V turbofan, thrust

Performance:

Maximum speed: 900 km/h
Cruise speed: 520 km/h
Range: 1,500 m
Service ceiling: 6000 m
g limits: +10/-8
Rate of climb: 60 m/s
 

NightWolf

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Yak-152

450px-%D0%A3%D1%87%D0%B5%D0%B1%D0%BD%D0%BE-%D1%82%D1%80%D0%B5%D0%BD%D0%B8%D1%80%D0%BE%D0%B2%D0%BE%D1%87%D0%BD%D1%8B%D0%B9_%D1%81%D0%B0%D0%BC%D0%BE%D0%BB%D1%91%D1%82_%D0%AF%D0%BA-152.jpg


General Characteristics:

Origin: Russia
Crew: 1
Capacity: 1 passanger
Length: 7,72 m
Wingspan: 8,82 m
Height: 2,47 m
Cross weight: 1,320 kg
Max takeoff weight: 1,490 kg
Fuel capacity: 200 kg
Powerplant: 1 x RED Aircraft A03 V-12 four-stroke diesel engine, 370 kW (500 hp)

Performance:

Maximum speed: 500 km/h
Stall speed: 100 km/h
Range: 1,500 km
Service ceiling: 4000 m
g limits: +9/-7
Rate of climb: 10 m/s

Armament:

Hardpoints: 4 with a capacity of 550 kg
 
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