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| SOCATA TB 9 TAMPICO SPRINT |
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| CONFIGURATION |
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Low wing, semi-monocoque metal construction, certified to FAR
Part 23 with amendments 1 through 16
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| SEATING |
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| Front: 2 |
Rear: 2-3 |
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| DIMENSIONS |
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| 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) |
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| POWERPLANT |
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| Manufacturer: |
Lycoming |
| Type |
O-320-D2A |
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4 cylinders |
| Power rating |
160 BHP at 2,700 RPM |
| Recommended TBO |
2,000 hours |
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| PROPELLER |
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| Manufacturer |
Sensenich |
| Diameter |
74 in (1.88 m) |
| Blades |
2 |
| Type |
Fixed pitch |
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| FUEL |
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| Type |
100 LL |
| Total tank capacity |
41.7 US gal (158 l) |
| Usable fuel |
40.2 US gal (152 l) |
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| OIL |
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| Tank capacity |
8.45 US quarts (8 l) |
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| LOADING |
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| 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) |
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| PERFORMANCE |
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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 |
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| DISTANCE |
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| [ISA - 50 ft - 2,337 lbs (1,060 kg)] |
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| Takeoff |
1 ,870 ft (570 m) |
| Landing |
1,378 ft (420 m) |
| Maximum range |
591 NM (1,094 km) |
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Reference: SOCATA, Groupe Aerospatiale, France, 1999 |
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Given data is only for information. Please refer to the manufacturer for current
data. |
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