The MLG actuator is a life limited item; its limit is listed in AMM Chapter 4 – FAA approved Airworthiness Limitations, based on landings. As a consequence, most of P180 operators take note of landing accrued by the actuator.
For operators with a higher flight hours/landing ratio (more than 1), the AD compliance limit presented in FH would be more stringent than required. On the contrary, for operators with a lower flight hours/landing ratio, the AD compliance limit presented in FH would be relaxed with reference to the referenced Service Bulletin.
I suggest to modify the actuator replacement compliance times as follow:
“before affected MLG actuators reach 3000 landings, replace ….; only if landings data are not available, replace the affected actuator before 3000 FH TIS ….” or similar statement.
Related Comments
Total: 2
Carlo Cardu Public SubmissionPosted: 10/17/2011
ID: FAA-2011-0954-0003
Oct 17,2011 11:59 PM ET
Carlo Cardu Public SubmissionPosted: 10/17/2011
ID: FAA-2011-0954-0004
Carlo Cardu
This is comment on Proposed Rule
Airworthiness Directives: PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes
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Related Comments
Public Submission Posted: 10/17/2011 ID: FAA-2011-0954-0003
Oct 17,2011 11:59 PM ET
Public Submission Posted: 10/17/2011 ID: FAA-2011-0954-0004
Oct 17,2011 11:59 PM ET