| |
|
| 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. |
|
|