2012-SW-047-AD MD Helicopters, Inc., Model 369A, 369D, 369E, 369H, 369HE, 369HM, 369HS, 369F and 369FF helicopters, to require inspecting the tail rotor blade pitch control arm and revising the retirement life of certain tail rotor blades.
🏛 Federal Aviation Administration (FAA)FAA-2013-0401
Documents
0
Total comments
0
all analyzed
Comment status
Closed
Last activity
—
In this docket
Documents
Rules, notices, and supporting material — the primary rule pinned first.
No documents mirrored for this docket yet.