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Jabiru Aircraft
Pty Ptd
Installation Manual
Jabiru 2200 Aircraft Engine
REVISION
0 1 2
Dated : March 2006
Page:
29
\\Gateway\library\files\engine_manuals\2200_engine_manuals\Hydraulic_Lifters\Working copies\HL_Installation_Manual_2200_Rev_0.doc
Print Date: 3/8/2006 1:56:00 PM
18
Appendix B – Supplemantay Information
18.1 Recommended Propeller Type
•
Fixed pitch wooden propellers.
•
Maximum propeller diameter 1727mm (68").
18.2 Equipment
The following equipment is included in the engine approval:-
•
Carburettor:
1 x Bing constant Pressure carburettor type 94/40
Main jet is Bing 220. Needle jet 276. Idle jet 45.
•
Fuel Pump:
Mechanical, Jabiru P/N PG10332N
•
Ignition System:
Jabiru dual magneto, high voltage transistorised,
contactless
P/N
PI10522N
•
Spark Plugs:
NGK D9EA
•
Alternator:
Integrated Jabiru, permanent magnet single phase
alternator, P/N 4532064/4535064 with regulator rectifier
P/No. PI10652N.
•
Starter:
Jabiru 12V/1.5 kW, engagement via reduction gear and
flywheel. Nippon Denso type, P/No. 4933023.
The following optional equipment may be driven by or fitted to the engine subject to the type
number being included in the approved Jabiru Aircraft Pty Ltd engine specification:-
Vacuum Pump
Tempest 212CW (or equivalent) vacuum pump fitted to the
alternator mounting plate and directly coupled to the
crankshaft. The drive pad is dry & The pad and spline are
SAE
Standard