Piper PA18-135 Super Cup TC-CYC

General features

Year of production: 1956
Crew: 1
Capacity: 1 traveler
Length: 22 ft 7 (6.88 m)
Wingspan : 35 ft 2 ½ (10.73 m)
Height: 6 ft 8 ½ (2.02 m)
Wing area: 178,5 m² (16.58 m²)
Airfoil : ABD 35B
Wing aspect ratio : 07:01
Curb weight : 930 (mass)” lb (422 kg)
Takeoff weight : 1.750 £ (794 kg)
Aircraft engine plant : 1 ×
Lycoming_O-320″ o “Lycoming O-320″ Lycoming O-290 air-cooled flat four cylinder, 135
"Horsepower” hp (100 kW)

Bellenca 7GCBC TC-FCC

General features
Crew: Capacity: 1 traveler
Length: (6.93 m) 22 ft 9 Wingspan: 33 ft 5 (10.19 m)
Height: 6 ft 5 (1.96 m) Wing area: 165 m² (15.3 m  2  ) Boy rate: 6.8:1 Airfoil : NACA 4412
Empty Weight: 1.110 TL (503 kg) Gross weight: 1.650 TL (748 kg)
Engine: 1  Lycoming O-320-A2B  The four-cylinder, four-stroke , Horizontally_opposed “;Aircraft engine, 150 hp (110 kW)
Performance Cruise SPEED: 126 mph (109 kn; 203 km / h) Stall Rate: 51 mil (44 kn; 82 km / h) ”
V SPEEDS” o “VNE”  Do not exceed the speed  : 162 mph (; 261 km / h 141 kn) Range: 500 mil (434 nmi; 805 km)Service Ceiling: 12,000 ft (3,658 m) G limits: +5 / -2
Climbing speed: 1,120 ft / min (5.7 m / s)
Wing loading: 10,0 TL / m² (49 kg / m  2  )

Tecnam P92 Echo Super TC-UAD

General features
Crew: 1 pilot
Capacity: 1 traveler
Length: 6.40 m (20 ft 11 in)
Wingspan : 8.70 m (28 ft 6)
Height: 2.50 m (8 ft 3)
Wing area: 12 m2 (129 ft2)
Empty Weight : 670 £ (304 kg)
Useful load: 650 £ (295 kg)
Max. takeoff weight : 1.212 £ (550 kg)
Central : 1 × Rotax 912 ULS, 100 hp (73,5 kW)
Performance
Do not exceed the speed : 270 km / h (168 mph)
Maximum speed : deniz seviyesinde 235 km / h (124 kts)
Cruise speed : 215 km / h (105 kts)
Stall speed : 63 km / h (33 kts)
Range : 800 km (500 mil)
Service Ceiling : 4500 m (14.760 ft)
Climbing speed : 354 m / min (1161 ft / min)
: Remove Run 100 m (328 ft)
Landing distance: 100 m (328 ft)

T67 Slingsby TC-CBG

General features

Crew: 2
Length: 24 ft 10 (7.55 m)
Wingspan : 34 ft 9 in (10.69 m)
Height: 7 ft 9 (2.36 m)
Wing area: 136 ft ² (12.6 m²)
Airfoil : NACA 23015/23013 (root / ucu)
Empty Weight : 1.750 £ (794 kg)
Max. takeoff weight : 2.550 £ (1.157 kg)
Central : 1 × Textron Lycoming AEIO-540-D 6-silindirli yatay karşı motor, 260 hp (194 kW)
Performance
Do not exceed the speed : 195 knot (224mph, 361 km / h)
Maximum speed : 152 knot (175 mph, 281 km / h)
Cruise speed : 140 knot (161 mph, 259 km / h)
Speed Stall : (flep) with 54 knot (62 mph, 100 km / h)
Range : 407 nm (468 mi, 753 km)
Service Ceiling : 19,000 ft [ 10 ] (5790 m)
Climbing speed : 1.380 ft / min (7 m / s)
Wing loading : 18,8 £ / ft ² (91.8 kg / m²)
Power / mass : 0.10 hp / lb (0.17 kW /kg)