4
. Advanced Training
. IFR Training
. Surveillance
. Travel
. High-speed long distance liaison
Overview
The Socata TB 20 Trinidad GT is a metal semi-monocoque, single-engine aircraft with a constant-speed propeller and retractable landing gear.
It combines the proven airframe of the Trinidad with the latest aviation technology, driven by Socata's major role as an aerostructure supplier on the Airbus A330/A340. For example, the upper fuselage panels are made of a carbon-fiber/honeycomb sandwich, a light, extremely robust material that can be used to make complex forms.
Windows are flush-mounted for maximum streamlining.
With the Trinidad GT, we have made a nearly perfect blend of comfort and performance even better. We rounded the fuselage to give you more cabin space, while also improving aerodynamics.
The wingtips are derived from those on the TBM700, the fastest single-engine turboprop aircraft in the world. As a final touch, the footsteps retract automatically along with the landing gear.
Configuration
Single engine
Low-wing monoplane with semi-monocoque metal construction
Certified to FAR 23, amendments 1 to 16 for VFR or IFR operations
subject to equipment
Additional benefits to include
Single wing spar
Tilt out panel for easy access to avionics
Triple anti-corrosion protection
Seats : 2 forward, bech for 2 or 3 aft
Powerplant
Manufacturer :
Lycoming
Type :
IO-540-C4 D5D 6 cyl.
Power rating :
250 HP at 2,575 RPM
Recommended TBO :
2,000 hours
Propeller
Manufacturer :
Hartzell
Diameter :
80 in
2.03 m
Type :
Constant speed
Blades :
2
Fuel
Fuel type :
100 LL
Total tank capacity :
88.8 US gal
336 l
Usable fuel capacity :
86.2 US gal
326 l
Oil
Total oil capacity :
13.3 US quarts
12,6 l
Weights
Operating empty weight :
1,911 lbs
867 kg
Max. take off weight (MTOW) :
3,086 lbs
1,400 kg
Max. landing weigh :
3,086 lbs
1,400 kg
Max. useful load :
1,270 lbs
577 kg
Max. luggage capacity in storage :
143 lbs
65 kg
Max. wing loading :
24.1 lbs/sq.ft
117.6 kg/m2
Performances
Rate of climb (sea level - max weight) : 1,200 ft/mn
Climb to 8,500 ft :
9 mn 30 s
Max. cruis. speed 6,500 ft at 75% :
163 KTAS
301 km/h
Best eco.cruis.spd 6,500 ft at 65% :
156 KTAS
272 km/h
Demonstrated crosswind :
25 kt
Maximum range :
1,110 Nm
Certified ceiling :
20,000 ft
Dimensions
Wing span :
32.71 ft
9.97 m
Length :
25.43 ft
7.75 m
Height :
9.35 ft
2,85 m
Wing area :
128.1 sq.ft
11.9 m2
Dihedral :
6°30
Wing airfoil :
RA16 C3
Cabin length :
8.30 ft
2,53 m
Cabin width :
4.20 ft
1.28 m
Cabin height :
3.94 ft
1.20 m
Wheel track :
7.12 ft
2,17 m
Socata TB-20 Trinidad - Performance Data
Horsepower: 250 Gross Weight: 3083 lbs
Top Speed: 167 kts Empty Weight: 1744 lbs
Cruise Speed: 160 kts Fuel Capacity: 86 gal
Stall Speed (dirty): 54 kts Range: 1100 nm
Takeoff Landing
Ground Roll: 1193 ft Ground Roll 755 ft
Over 50 ft obstacle: 1953 ft Over 50 ft obstacle: 1750 ft
Rate Of Climb: 1260 fpm
Ceiling: 20000 ft
. Advanced Training
. IFR Training
. Surveillance
. Travel
. High-speed long distance liaison
Overview
The Socata TB 20 Trinidad GT is a metal semi-monocoque, single-engine aircraft with a constant-speed propeller and retractable landing gear.
It combines the proven airframe of the Trinidad with the latest aviation technology, driven by Socata's major role as an aerostructure supplier on the Airbus A330/A340. For example, the upper fuselage panels are made of a carbon-fiber/honeycomb sandwich, a light, extremely robust material that can be used to make complex forms.
Windows are flush-mounted for maximum streamlining.
With the Trinidad GT, we have made a nearly perfect blend of comfort and performance even better. We rounded the fuselage to give you more cabin space, while also improving aerodynamics.
The wingtips are derived from those on the TBM700, the fastest single-engine turboprop aircraft in the world. As a final touch, the footsteps retract automatically along with the landing gear.
Configuration
Single engine
Low-wing monoplane with semi-monocoque metal construction
Certified to FAR 23, amendments 1 to 16 for VFR or IFR operations
subject to equipment
Additional benefits to include
Single wing spar
Tilt out panel for easy access to avionics
Triple anti-corrosion protection
Seats : 2 forward, bech for 2 or 3 aft
Powerplant
Manufacturer :
Lycoming
Type :
IO-540-C4 D5D 6 cyl.
Power rating :
250 HP at 2,575 RPM
Recommended TBO :
2,000 hours
Propeller
Manufacturer :
Hartzell
Diameter :
80 in
2.03 m
Type :
Constant speed
Blades :
2
Fuel
Fuel type :
100 LL
Total tank capacity :
88.8 US gal
336 l
Usable fuel capacity :
86.2 US gal
326 l
Oil
Total oil capacity :
13.3 US quarts
12,6 l
Weights
Operating empty weight :
1,911 lbs
867 kg
Max. take off weight (MTOW) :
3,086 lbs
1,400 kg
Max. landing weigh :
3,086 lbs
1,400 kg
Max. useful load :
1,270 lbs
577 kg
Max. luggage capacity in storage :
143 lbs
65 kg
Max. wing loading :
24.1 lbs/sq.ft
117.6 kg/m2
Performances
Rate of climb (sea level - max weight) : 1,200 ft/mn
Climb to 8,500 ft :
9 mn 30 s
Max. cruis. speed 6,500 ft at 75% :
163 KTAS
301 km/h
Best eco.cruis.spd 6,500 ft at 65% :
156 KTAS
272 km/h
Demonstrated crosswind :
25 kt
Maximum range :
1,110 Nm
Certified ceiling :
20,000 ft
Dimensions
Wing span :
32.71 ft
9.97 m
Length :
25.43 ft
7.75 m
Height :
9.35 ft
2,85 m
Wing area :
128.1 sq.ft
11.9 m2
Dihedral :
6°30
Wing airfoil :
RA16 C3
Cabin length :
8.30 ft
2,53 m
Cabin width :
4.20 ft
1.28 m
Cabin height :
3.94 ft
1.20 m
Wheel track :
7.12 ft
2,17 m
Socata TB-20 Trinidad - Performance Data
Horsepower: 250 Gross Weight: 3083 lbs
Top Speed: 167 kts Empty Weight: 1744 lbs
Cruise Speed: 160 kts Fuel Capacity: 86 gal
Stall Speed (dirty): 54 kts Range: 1100 nm
Takeoff Landing
Ground Roll: 1193 ft Ground Roll 755 ft
Over 50 ft obstacle: 1953 ft Over 50 ft obstacle: 1750 ft
Rate Of Climb: 1260 fpm
Ceiling: 20000 ft
No comments:
Post a Comment