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Airworthiness Directives (ADs)

88-AS350-005

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date
1999/04/12
Applicability
AS 350 B,BA,B1,B2,B3,BB,D
Model Number
AS350
CAA AD Number
88-AS350-005
Aeronautics Authority of Original AD
DGAC
Original AD Number
1999-085-076(A)
Effective Date
Subject
Tail rotor hub pitch-change plate bearing
Reference Publications (Revision/ATA/SB)
SB No. 05.00.29
Remarks
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