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AMC 25.1027(b) Propeller Feathering

ED Decision 2003/002/RM

The amount of trapped oil should be sufficient to cover one feathering operation; taking into account the maximum oil leakage in the feathering system due to wear and deterioration in service.

Details
Source-Title: AMC 25.1027(b) Propeller Feathering View latest amendments
Erulesid: ERULES-1963177438-8708 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 17 October, 2003
Entryintoforcedate: 17 October, 2003
Regulatorysource: ED Decision 2003/2/RM Navigate
Regulatorysubject: CS-25
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 25.1027 Propeller feathering system
Origin: EASA
Category: EAR