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SOCATA TB 10 TOBAGO  

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 O-360-A1AD
4 cylinders
Power rating 180 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 1,543 lbs (700 kg)
Maximum takeoff weight 2,535 lbs (1,150 kg)
Maximum landing weight 2,535 lbs (1,150 kg)
Maximum useful load 992 lbs (450 kg)
Maximum weight in luggage compartment 143 lbs (65 kg)
PERFORMANCE
Rate of climb
(ISA sea level-max weight)
787 ft/mn
Climb to 8,500 ft 16 mn (ISA)

Maximum cruising speed
(8,500 ft at 75% W)
127 KTAS (235 km/h)
Best economy cruising speed
(10,000 ft at 60% W)
108 KTAS (199 km/h)
Demonstrated crosswind 25 kt
DISTANCE
[ISA - 50 ft - 2,535 lbs (1,150 kg)]
Takeoff 1,657 ft (505 m)
Landing 1,509 ft (460 m)
Maximum range 697 NM (1,291 km)
Certified ceiling 13,000 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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