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TB 200 Tobago GT

The SOCATA TB 200 TOBAGO GT is a fixedgear, 45 seat, single engine aircraft with constantspeed propeller.

GENERAL INFORMATION
The Socata TB200 Tobago GT is the GT version of Tobago XL. The Socata TB 200 GT is powered by a 200 HP Lycoming IO360 A1B6 fuelinjected engine that eliminates carburetor icing risk. With such a combination of power and its Hartzell constant speed propeller the TB 200 GT offers more performance : climb is 937 ft/min at sea level and cruise speed 130 kt at 75% power. Due to its exceptional maneuvering qualities even at low speeds the TB 200 GT has been selected by many flight schools for basic and advanced training

TECHNICAL SPECIFICATIONS

Configuration

• Low wing, semimonocoque metal construction, certified to FAR Part 23 with amendments 1 through 16

Seating

• Front : 2
• Rear : 23

Power Plant

• Manufacturer : Lycoming
• Type : IO360A1B6 4 cylinders fuel injected
• Power rating : 200 HP at 2,700 RPM
• Recommanded TBO : 2,000 hours

Propeller

• Manufacturer : Hartzell
• Diameter : 74 in (1.88 m)
• Blades : 2
• Type : constant speed

Fuel

• Type : 100 LL
• Total tank capacity : 55.5 US gal (210 l)
• Usable fuel : 53.9 US gal (204 l)

Oil

• Tank capacity : 8.45 US quart (8 l)

Dimensions

DIMENSIONS Wing span: 32.84 ft (10.01 m) Length: 25.43 ft (7.75 m) Wing area : 128.1 sq ft (11.9 m2) Height : 9.91 ft (3,02 m) Wing airfoil: RA 16 3C3 Dihedral : 4°30'
Cabin length : 8.30 ft (2,53 m) Cabin width: 4.20 ft (1.28 m) Cabin height: 3.94 ft (1.20 m) Wheel track : 7.55 ft (2,30 m)
Maximum wing loading: 19.8 lbs/sq.ft (96.6 kg/m²)

Loading

• Operating empty weight : 1,642 lbs (745 kg)
• Maximum takeoff weight : 2,535 lbs (1,150 kg)
• Maximum landing weight : 2,535 lbs (1,150 kg)
• Maximum useful load : 893 lbs (405 kg)
• Maximum weight in luggage compartments : 143 lbs (65 kg)

Performance (ISA at maximum takeoff weight)

• Rate of climb (sea levelmax weight) : 937 ft/mn
• Climb to 8,500 ft : 12 mn 30 s
• Maximum cruising speed : (8,500 ft at 75% W) 130 KTAS (241 km/h)
• Best economy cruising speed : (8,500 ft at 60% W) 115 KTAS (213 km/h)
• Demonstrated crosswind : 25 kt
• Operating ceiling : 16,000 ft

Distance {ISA at maximum takeoff weight)

• Takeoff (50 ft obstacle clearance) : 1,560 ft (475 m)
• Landing (50 ft obstacle clearance) : 1,474 ft (449 m)
• Maximum range (without reserves at 8,500 ft at 60% w): 637 NM (1,179 km)

Systems

Flight controls :

• Dual yoke controls
• Electrically actuated flaps
• Push/pull rods
• Manual elevator trim actuated by cables

Landing gear :

• Steering nosewheel
• Tricycle fixed landing gear with fairings
• Main landing gear of the oleo landing gear shock struts

Fuel system :

• On structural fuel tank per wing
• Electric auxiliary fuel pump
• Enginedriven fuel pump
• Capacitive fuel gauge system

Electrical system :

• Battery : 24 V / 10 A.h
• Circuitbreakers
• Alternator : 28 V / 70 A
• Centralized advisory panel
• Regulator with overvoltage relay
• Integrated instrument panel lighting

Additional benefits

• Machined single wing spar
• Tilt out panel for easy access to avionics
• Triple anticorrosion protection
• Two access doors and two emergency exits

*None of the information included in this document is contractually binding