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Airworthiness Directives (ADs)

CAA-2006-10-008

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
2006/10/18
Applicability
ATR42-500 and ATR72-212A aircraft, fitted with modification n°4440 (composite vertical fin) and on which the modification n°5426 (Service Bulletin ATR42-55-0012 or ATR72-55-1004) has not been embodied, except the following serial numbers : - 618 to 623 inclusive for ATR42-500 model. - 682, 683, 684, 687 and from 694 to 708 inclusive for ATR72-212A model. This Airworthiness Directive (AD) does not affect aircraft modified by SB ATR42-55-0012 original issue or by SB ATR72-55-1004 original issue.
Model Number
ATR42 and ATR72 Aircraft
CAA AD Number
CAA-2006-10-008
Aeronautics Authority of Original AD
EASA
Original AD Number
2006-0303
Effective Date
2006/10/25
Subject
Stabilizers – Vertical Stabilizer Fin Tip – Inspection / Repair / Modification
Reference Publications (Revision/ATA/SB)
ATA 55 Supersedure: DGAC AD 2002-506(B)R1(2002-09-013A) and F-2005-059(CAA-2005-04-009) Ref. ATR SB ATR42-55-0011 and SB ATR42-55-0012 Rev.1; or SB ATR72-55-1003 Rev.1 and SB ATR72-55-1004 Rev.1, as applicable, or later approved revisions.
Remarks
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