SI-0023 Blade Installation Procedure
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SI-0023 Blade Installation Procedure

Revision
Change
Approved
Date

1

Initial

MJE

29/4/2024


This instruction covers the recommended procedure for installing Airmaster blade assemblies into the propeller hub.


The operator must ensure that the propeller hub and blade retention assemblies are lubricated correctly beforehand. The operator must also verify that each blade is seated correctly inside the hub after this process in accordance with the post-installation checks.


APL-SI-0023 Blade Installation Procedure R1.pdf
pdf