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Titan T-51 Mustang

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The Titan Aircraft T-51 Mustang is a two-seat, dual control, tandem seat aircraft. It can be built as an N-numbered amateur built experimental aircraft or as a Light Sport Aircraft.

The kit has an estimated build time of 1600 hours and includes all required material, components and fasteners. The kit does not include the engine, propeller and instruments. When equipped with the Rotax 912S engine, controllable propeller, and a full compliment of necessary flight instruments, the finished T-51 should cost well under US$55,000.00.

The T-51 Mustang is rated at a +6g / -4g load limit capability at a gross weight of 1450 pounds. When operating with the 912S engine and landing gear retracted the cruise speed is 150mph. The stall speed in landing configuration is 39mph. 2009 Kit price: 37500 US$

The centre of the spinner is 7 ft from the ground, and its length is 23.5 ft. It is equipped with 2 seats, dual control, and retractable gear.

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With a Suzuki Vitara 2.5 lt fuel injected V-6 developing around 170 hp and driving an Aerotek 2000 four blade prop, takeoff speed is 65-70 mph at 4800 rpm, and cruise is 150 mph at 4200-4500 rpm, 25 in manifold pressure.

 

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T-51 Mustang
Engines: ROTAX 912S, 914, Jabiru 332a, Suzuki V6, Honda V6
Power: 100 -270 HP
Length: 23’ 6” / 7.16 m
Height: 9’ 2” / 2.80 m
Wing span: 24 ft / 7.32 m
Wing area: 118 sq ft / 10.96 sq m
Empty weight: 850-1180 lb / 385-536.4 kg
Gross weight: 1320-1800 lb / 545.5-743.8 kg
Fuel capacity: 25 US GAL / 94.5 lt
Vne: 197 mph / 316.97 kph
Cruise speed: 150-185 mph / 241.35-299.7 kph
Stall speed: 42-52 mph / 62.75-84.24 kph
Range: 720 mi / 1158.5 km
Climb rate: 1200-3000 f/m / 6.1-15.2 m/s
Take off run: 250-400 ft / 91.44-121.95 m
Landing roll: 300-400 ft / 91.44-121.95 m
Ceiling: 16000-18000 ft  /4876.8-5487.8 m
Cabin width: 26 in / 66.04 cm
Cabin head room: 48 in / 121.96 cm
Cabin leg room: 46 in / 116.84 cm
Kit price 2009: $54,900 U.S.

Engine: Suzuki Vitara 2.5 lt fuel injected V-6, 170 hp
Prop: Aerotek 2000 four blade
Takeoff speed: 65-70 mph at 4800 rpm
Cruise: 150 mph at 4200-4500 rpm, 25 in mp
MTOW: 1750 lb
Empty weight: 1150 lb
Stall: 48 mph
Climb rate; 2200 fpm
Takeoff run: 350 ft
Landing soll: 350 ft
Seats: 2
Length: 23.5 ft

Engine: Rotax 912S, 100 hp
HP range: 100-170
Length: 24 ft
Wing span: 24 ft
Wing area: 118 sq.ft
Empty Weight: 386 kg / 850 lbs
MTOW Weight: 658 kg / 1450 lbs
Fuel capacity: 23 USG
Stall: 34 kt / 39 mph / 63 kmh
Cruise: 130 kt / 150 mph / 241 kmh
VNE: 171 kt / 197 mph / 317 kmh
Climb Ratio: 1200 ft/min / 6 m/s
Take-off distance: 300 ft / 91 m
Landing distance: 300 ft / 91 m
Range: 625nm
Seats: 2
Landing gear: tail wheel / retractable

 

 


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