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Airworthiness Directives (ADs)

CAA-2021-05-003(已被CAA-2025-04-005取代)

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
2021/05/10
Applicability
Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category. and Installation of Supplemental Type Certificate ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a “change in product” alternative method of compliance approval request is not necessary to comply with the requirements of 14 CFR 39.17.
Model Number
Boeing 737-600, -700, -700C, -800, -900, and -900ER series airplanes.
CAA AD Number
CAA-2021-05-003(已被CAA-2025-04-005取代)
Aeronautics Authority of Original AD
FAA
Original AD Number
2021-09-06
Effective Date
2021/06/08
Subject
This AD reduces the compliance time of initial inspection and repetitive interval of inspection for cracking of the left- and right-hand side outboard chords of frame fittings and failsafe straps at a certain station around eight fasteners.
Reference Publications (Revision/ATA/SB)
This AD replaces AD 2019-22-10(CAA-2019-11-006)
Remarks
Download
CAA-2021-05-003.pdf
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