Performance - Specications
Sinus 912 LSA 80 hp Rotax 912
stall speed (aps extended) 34 kts (64 km/h)
stall speed (aps zero) 40 kts (74 km/h)
cruise speed (5300 RPM) 110 kts (205 km/h)
maximum speed at sea level 118 kts (218 km/h)
VNE 120 kts (222 km/h)
usable fuel capacity standard tanks 14.5 US gal/55 L, endurance 4.6 hours
usable fuel capacity long-range tanks 24.5 US gal/93 L endurance 7.7 hours
fuel ow at cruise speed 2.9 gph (11.2 l/h )
range at cruise speed (excl reserve, standard tanks) 505 NM
range at cruise speed (excl reserve, long range tanks) 850 NM
takeo - ground roll - at MTOM 430 ft (132 m)
takeo total distance over 50 ft obst. at MTOM 760 ft (232 m)
landing distance over 50 ft obst. (airbrakes) 885 ft (270 m)
absolute ceiling at MTOM (with engine running) 23,600 ft (7200 m)
NOTE Airbrakes are standard equipment and recommended for operations on runways short-
er than 2500 ft. The above performance gures are based on airplane weight at 1210 lbs (550 kg),
standard atmospheric conditions, level hard-surfaced dry runways and no wind. They are calcu-
lated valued derived from ight test conducted by Pipistrel LSA s.r.l. under carefully documented
conditions and will vary with individual airplanes and numerous factors (surface condition, tem-
perature, water on wing, etc).
Sinus 912 LSA 80 hp Rotax 912
maximum weight takeo 1210 lbs (550 kg)
maximum weight landing 1210 lbs (550 kg)
standard empty weight 643 lbs (292 kg)
maximum useful load 568 lbs (258 kg)
baggage allowance 55 lbs (25 kg)
fuel capacity, usable 14.5/24.5 US gal
fuel capacity, usable 55 L/93 L
oil capacity (oil bottle) 3.1 quarts
engine Rotax 912 80 hp
propeller
xed pitch* dia. 63’’
1620 mm
*Propeller is a ground adjustable, two-blade composite propeller with metal hub, see chapter
Airplane and Systems Description for more details. Optional is Vario feathering propeller.
Noise levels
According to independent testing performed by German LBA-LTF noise regulations the aeroplanes,
the equivalent exhibited noise measures less than 60 dBa.
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