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4 Stroke :
Certified
914 F - Certified to FAR33 (EC No. 1592/2002 & 1702/2003)
912 S - Certified to FAR33 (EC No. 1592/2002 & 1702/2003)
912 F - Certified to FAR33 (EC No. 1592/2002 & 1702/2003)
912 A - Certified to JAR 22 (EC No. 1592/2002 & 1702/2003)
 
Non - Certified
914 UL
912 ULS
912 UL

914 F - Certified to FAR33 (EC No. 1592/2002 & 1702/2003)
ENGINE:
Type:  914 F
Performance: 73,5 kW (100 hp) @ 5500 rpm
Torque: Max. 5 min.: 84,5 kW (115 hp) @ 5800 rpm
144 Nm (106 ft.lbf.) @ 4900 rpm
Max. RPM: 5800 rpm
Bore: 79,5 mm (3,13 in.)
Stroke: 61 mm (2,40 in.)
Displacement: 1211,2 cm3 (73,91 cu.in.)
Compression ratio: 9,0 : 1
Ignition unit: double CDI
Ignition timing: 4° up to 1000 rpm
Generator performance: above 26° / 22°
250 W @ 5500 rpm
Voltage: 13,5 V
OPERATING MEDIA:
Fuel: min. RON 95*
Oil: min. AKI 91*
*leaded or unleaded or AVGAS 100 LL
Cooling liquid: API SG or higher
Conventional (mix ratio 50:50) or water-free
WEIGHT-engine:
Standard configuration: 64 kg (141 lb.)
Engine with gearbox i=2,43:
4,0 kg (8,8 lb.)
Exhaust system: 2,0 kg (4,4 lb.)
Engine suspension frame:  
WEIGHT-Options :
Oil radiator:
0,6 kg (1,3 lb.)
Radiator: 1,0 kg (2,2 lb.)
Slipping clutch: 1,7 kg (3,7 lb.)
Air filter: 0,15 kg (0,3 lb.)
Air guide hood: 0,8 kg (1,8 lb.)
Vacuum pump: 0,8 kg (1,8 lb.)
Hydraulic propeller governor:
2,7 kg (5,9 lb.)
External alternator 40A / 12V DC:
3,0 kg (6,6 lb.)
Instrument FLYDAT: 0,5 kg (1,1 lb.)
  Certified per FAR 33 (EC No. 1592/2002 & 1702/2003)
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