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SOCATA TB 200 TOBAGO XL  

CONFIGURATION
Low wing, semi-monocoque metal construction, certified to FAR
Part 23 with amendments 1 through 16
SEATING
Front: 2 Rear: 2-3
DIMENSIONS
Overall length: 25.26 ft (7.70 m)
Height 9.91 ft (3.02 m)
Wingspan 32.05 ft (9.77 m)
Horizontal tail span 10.50 ft (3.20 m)
Wing area 128.1 ft2 (11.90 m2)
Cabin length 8.30 ft (2.53 m)
Cabin width 4.20 ft (1.28 m)
Maximum cabin height 3.67 ft (1.12 m)
Wheelbase 6.43 ft (1.96 m)
POWERPLANT
Manufacturer: Lycoming
Type IO-360-A1B6
4 cylinders fuel injected
Power rating 200 BHP at 2,700 RPM
Recommended 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 55.4 US gal (210 l)
Usable fuel 53.8 US gal (204 l)
OIL
Tank capacity 8.45 US quarts (8 l)
LOADING
Average empty weight 1,576 lbs (715 kg)
Maximum takeoff weight 2,535 lbs (1,150 kg)
Maximum landing weight 2,535 lbs (1,150 kg)
Maximum useful load 959 lbs (435 kg)
Maximum weight in luggage compartment 143 lbs (65 kg)
PERFORMANCE
Rate of climb
(ISA sea level-max weight)
937 ft/mn
Climb to 8,500 ft 12 mn 30s (ISA)

Maximum cruising speed
(8,500 ft at 75% W)
130 KTAS (241 km/h)
Best economy cruising speed
(10,000 ft at 60% W)
115 KTAS (213 km/h)
Demonstrated crosswind 25 kt
DISTANCE
[ISA - 50 ft - 2,535 lbs (1,150 kg)]
Takeoff 1,560 ft (475 m)
Landing 1,474 ft (449 m)
Maximum range 637 NM (1,179 km)
Certified ceiling 16,000 ft
Reference: SOCATA, Groupe Aerospatiale, France, 1999
Given data is only for information. Please refer to the manufacturer for current data.

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