Aircraft characteristics – Flight school Jus

Aircraft characteristics

AIRCRAFT CHARACTERISTICS OF OUR FLEET

This data is not for operational use!

P96 Golf 100
S5-PCO		 C-172 R
S5-DYC		 C-172 S
S5-DYG
General
Crew 1 + 1 1 + 3 1 + 3
Load 160,2 kg / 353 lb 298 kg / 657 lb 321 kg / 708 lb
Length 6,40 m / 21 ft 8,28 m / 27 ft 2 in 8,28 m / 27 ft 2 in
Wingspan 8,41 m / 27 ft 7 in 11,00 m / 36 ft 1 in 11,00 m / 36 ft 1 in
Height 2,29 m / 7 ft 6 in 2,72 m / 8 ft 11 in 2,72 m / 8 ft 11 in
Wings surface 12,2 m2 / 131,3 ft2 16,2 m2 / 174 ft2 16,2 m2 / 174 ft2
Wing internally developed modified NACA 2412 modified NACA 2412
Aspect ratio 6,2:1 7,32:1 7,32:1
Empty weight 312,3 kg / 687 lb 813 kg / 1.792 lb 813 kg / 1.792 lb
MTOW 472,5 kg / 1041 lb 1.111 kg / 2.449 lb 1.134 kg / 2.500 lb
Maximum landing weight 472,5 kg / 1041 lb 1.111 kg / 2.449 lb 1.134 kg / 2.500 lb
Fuel AVGAS 100LL JET A-1, Diesel JET A-1, Diesel
Fuel capacity 70 l / 18,5 US gal 180,2 l / 47,6 US gal 180,2 l / 47,6 US gal
Useful fuel 69 l / 18,2 US gal 168,8 l / 44,6 US gal 168,8 l / 44,6 US gal
Powerplant ROTAX 912 ULS 2
73,5 kW / 100 hp		 Technify Motors TAE 125
99 kW / 135 hp		 Technify Motors TAE 125
99 kW / 135 hp
Performance
VNO 210 km⁄h / 113 kts 239 km⁄h / 129 kts 239 km⁄h / 129 kts
VNE 270 km⁄h / 146 kts 302 km⁄h / 163 kts 302 km⁄h / 163 kts
Cruise speed 185 km⁄h / 100 kts 187 km⁄h / 101 kts 198 km⁄h / 107 kts
Stall speed 72 km⁄h / 39 kts 87 km⁄h / 47 kts 87 km⁄h / 47 kts
Range 740 km / 400 nmi 1.485 km / 802 nmi 1.572 km / 849 nmi
Service ceiling 3.962 m / 13.000 ft 5.334 m / 17.500 ft 5.334 m / 17.500 ft
Climbe rate (MTOW) 4,5 m⁄s / 890 ft⁄min 2,8 m⁄s / 558 ft⁄min 3,3 m⁄s / 655 ft⁄min
Fuel consumption (cruise) 18 l⁄h / 4,8 US gal⁄h
14 l⁄h / 3,7 US gal⁄h (175 kts c.s.)		 18,6 l⁄h / 4,9 US gal⁄h 18,6 l⁄h / 4,9 US gal⁄h
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