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SOCATA TB 9 TAMPICO SPRINT  

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: 25.33 ft (7.72 m)
Height 9.91 ft (3.02 m)
Wingspan 32.45 ft (9.89 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 6.30 ft (1.92 m)
POWERPLANT
Manufacturer: Lycoming
Type O-320-D2A
4 cylinders
Power rating 160 BHP at 2,700 RPM
Recommended TBO 2,000 hours
PROPELLER
Manufacturer Sensenich
Diameter 74 in (1.88 m)
Blades 2
Type Fixed pitch
FUEL
Type 100 LL
Total tank capacity 41.7 US gal (158 l)
Usable fuel 40.2 US gal (152 l)
OIL
Tank capacity 8.45 US quarts (8 l)
LOADING
Operating weight 1,426 lbs (647 kg)
Maximum takeoff weight 2,337 lbs (1,060 kg)
Maximum landing weight 2,337 lbs (1,060 kg)
Maximum useful load 911 lbs (413 kg)
Maximum weight in luggage compartment 143 lbs (65 kg)
PERFORMANCE
Rate of climb
(ISA sea level - max weight)
665 ft/mn
Climb to 5,000 ft 9 mn 30 s (ISA)
Maximum cruising speed (6,000 ft) 115 KTAS (213 km/h)
Best economy cruising speed (6,000 ft) 98 KTAS (181 km/h)
Demonstrated crosswind 25 kt
Certified ceiling 11,000 ft
DISTANCE
[ISA - 50 ft - 2,337 lbs (1,060 kg)]
Takeoff 1 ,870 ft (570 m)
Landing 1,378 ft (420 m)
Maximum range 591 NM (1,094 km)

Reference: SOCATA, Groupe Aerospatiale, France, 1999
Given data is only for information. Please refer to the manufacturer for current data.

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