Airworthiness Directives (ADs)
CAA-2016-09-002(已被CAA-2019-02-008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.
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Issue Date
- 2016/09/13
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Applicability
- (1) This AD applies to certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 737-32-1448, Revision 1, dated May 29, 2015.
(2) Installation of Supplemental Type Certificate (STC) ST00830SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/184DE9A71EC3FA5586257EAE00707DA6?OpenDocument&Highlight=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 (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.
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Model Number
- Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes
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CAA AD Number
- CAA-2016-09-002(已被CAA-2019-02-008取代)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2016-18-01
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Effective Date
- 2016/10/05
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Subject
- To detect and correct heavy corrosion and chrome damage of the forward and aft trunnion pin assemblies of the right and left MLGs which could result in cracking of these assemblies and collapse of the MLGs.
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Reference Publications (Revision/ATA/SB)
- ATA 32. Reference: Boeing Special Attention Service Bulletin 737-32-1448, Revision 1, dated May 29, 2015.
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Remarks
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