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| SOCATA TB 20 TRINIDAD |
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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 |
25.29 ft (7.71 m) |
| Height |
9.35 ft (2.85
m) |
| Wing span |
32.05 ft (9.77 m) |
| Horizontal tail span |
12.07 ft (3.68
m) |
| Wing area |
128.1 ft2 (11.90 in2) |
| 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 |
6.27 ft (1 .91
m) |
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| POWERPLANT |
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| Manufacturer: |
Lycoming |
| Type |
IO-540-C4 D5D |
|
6 cylinders fuel injected |
| Power rating |
250 BHP at 2,575 RPM |
| Recommended TBO |
2,000 hours |
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| PROPELLER |
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| Manufacturer |
Hartzell |
| Diameter |
80 in (2.03 m) |
| Blades |
2 |
| Type |
Constant speed |
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| FUEL |
|
| Type |
100 LL |
| Total tank capacity |
88.8 US gal (336 l) |
| Usable fuel |
86.2 US gal (326 l) |
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| OIL |
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| Tank capacity |
13.3 US quarts (12.6 l) |
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| LOADING |
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| Average empty weight |
1,764 lbs (800 kg) |
| Maximum takeoff weight |
3,086 lbs (1,400 kg) |
| Maximum landing weight |
3,086 lbs (1,400 kg) |
| Maximum useful load |
1,323 lbs (600 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) |
1,200 ft/mn |
| Climb |
9 mn (ISA) to 8,000 ft |
| Maximum cruising speed (8,500 ft) |
163 KTAS (301 km/h) |
| Best economy cruising speed (8,500 ft) |
157 KTAS (290 km/h) |
| Demonstrated crosswind |
25 kt |
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| DISTANCE |
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| [ISA - 50 ft - 3,086 lbs (1,400 kg)] |
|
| Takeoff |
2,150 ft (655 m) |
| Landing |
1,750 ft (533 m) |
| Maximum range |
1,108 NM (2,053 km) |
| Certified ceiling |
20,000 ft |
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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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