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Jabiru Aircraft
Pty Ptd
Installation Manual
Jabiru 2200 Aircraft Engine
REVISION
0 1 2
Dated : March 2006
Page:
26
\\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
15
Propeller Selection
•
The hub of the propeller must be drilled with holes to match the flange.
•
The propeller must be carefully selected to match the airframe and the engine: Propellers
up to 1727mm (68”) in diameter and between 762mm (30”) and 1219mm (48”) in pitch
may be used. The propeller flange is drilled with 6 holes at both 4” PCD and 100mm PCD
(total of 12 holes).
•
All Propellers must be able to obtain 2800rpm static and 3150rpm to 3300rpm wide open
throttle straight and level.
•
Do not cruise or climb in the range 2100rpm – 2400rpm.
•
Maximum moment of inertia 0.25 kgm2
Applications outside this range should be referred to Jabiru.
Engine MUST NEVER BE RUN WITHOUT THE PROPELLER. Damage
will occur in this state.