NOTE
The above mentioned circuit breakers are accessible from bag-
gage compartment through an inspection door.
Baggage door : Secured.
Lower avionic bay access door : Secured.
Tail rotor middle drive shaft bearings : Check condition verifying no
mark slippage. Door secured.
Engine area : Check for fuel and/or oil leaks.
Engine oil : Check gauge for oil presence
(sight glass dark).
Engine oil filter impending bypass in-
dicator : Check for correct indication.
Engine-transmission drive shaft : Condition.
Engine supports (visible area) : Condition.
Engine cowling : Condition, secured.
Engine air intake screen and chamber : Cover removed; free of damage
and/or obstructions.
Cooler system belt : Condition and security.
Main rotor hub and blades : Condition and security.
Main rotor dampers : Check for correct charge indi-
cation.
Main rotor pitch change links : Condition and security.
RFM A109E
R.A.I. Approved 2-9