適航指令資料庫查詢
CAA-2016-09-002(已被CAA-2019-02-008取代)
依據民用航空法規，航空器所有人或使用人除應遵守本國民航局所發布適航指令，亦應遵守航空器設計國之民航主管機關所通告之適航指令。
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發布日期
- 2016/09/13
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適用性說明
- (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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型別
- Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes
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民航局AD編號
- CAA-2016-09-002(已被CAA-2019-02-008取代)
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原發布國
- FAA
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原AD編號
- 2016-18-01
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生效日期
- 2016/10/05
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主旨摘要
- 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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參考資訊（版本/ATA/SB）
- ATA 32. Reference: Boeing Special Attention Service Bulletin 737-32-1448, Revision 1, dated May 29, 2015.
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存檔序號
- 105-09-003
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專業分項
- Systems
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產品類別
- Airplane
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備註
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檔案下載
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1.本局早期(2012年前)所發布AD目前未提供檔案下載服務。如欲查詢，請自行連結原發布國民航主管機關網頁，再依”原AD編號”查詢。
2.我國目前所引進航空產品原發布國民航主管機關網頁聯結如下：
Canada、EASA、FAA、Israel、JapanCAB、UK、Brazil、CAA-CZ