Reference
Modification no.
- 0 -
Page
28
Date
1997 02 01
Main
914 F
01476
CARBURETOR:
CARB CALIBRATION:
FUEL PUMP:
STARTER:
PROPELLER GEAR:
REDUCTION RATIO:
DIRECTION OF ROTATION:
MOMENT OF INERTIA OF PRO-
PELLER:
OVERLOAD CLUTCH:
VACUUM PUMP (optional extra):
PROPELLER PITCH GOVER-
NOR (optional extra):
REDUCTION RATIO:
hydraulic governor and vacuum
pump
TURBO CHARGER:
TURBO CONTROL UNIT (TCU):
CERTIFICATION:
CERTIFICATION DATA SHEET:
2x BING-constant depression carburetors 32 mm, Type 64
Main jet..................................... 162
Idle jet....................................... 35
Needle jet ................................. 2,72
Jet needle................................. (part no. 961 215)
Needle position ........................ 2
Pilot jet ..................................... 85
Mixture screw ........................... 1,5 turns open
2 electric fuel pumps
electric starter, engagement via gearbox and sprag clutch,
12V/0,6 kW
integrated, spur gear, with torsional shock absorber
standard 2,4286 (51T. / 21T.)
anti-clockwise, looking at propeller shaft
max. 6000 kgcm
2
multi-disk
AIRBORNE 211 CCW, drive via gearbox
Hydraulic governor WOODWARD A210786, drive via prop
shaft (for F3 only)
1 : 0,758 (total 1,842).
Transmission ratio from crankshaft to hydraulic governor or
vacuum pump is 1,842 e.g. they rev with 0,543 of crankshaft
speed.
Exhaust gas turbo with waste gate, radial-flow compressor
T25
Electronic, proportional plus integral plus derivative
controller with 2 external indicating lamps.
to FAR 33 and JAR-E,
TW 10-ACG
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