Airworthiness Directives (ADs)
CAA-2019-02-013
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
- 2019/02/22
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Applicability
- This AD applies to General Electric Company (GE) GEnx-1B54, -1B58, -1B64, -1B67, -1B70, -1B54/P1, -1B58/P1, -1B64/P1, -1B67/P1, -1B70/P1, -1B54/P2, -1B58/P2, -1B64/P2, -1B67/P2, -1B70/P2, -1B70C/P1, -1B70/72/P1, -1B70/75/P1, -1B74/75/P1, -1B75/P1, -1B70C/P2, -1B70/72/P2, -1B70/75/P2, -1B74/75/P2, -1B75/P2, -1B76/P2, -1B76A/P2, -1B78/P2, -2B67, -2B67B, and -2B67/P turbofan engines with a high-pressure turbine (HPT) stator case (HPT case), part number (P/N) 2302M90G04 installed, and with any serial number (S/N) listed in Table 1, 2, or 3, in the Planning Information section of GE Service Bulletin (SB) GEnx-2B S/B 72-0360, Revision 04, dated December 4, 2018, or GE SB GEnx-1B S/B 72-0424, Revision 04, dated December 3, 2018, installed.
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Model Number
- General Electric Company (GE) GEnx turbofan engines.
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CAA AD Number
- CAA-2019-02-013
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2019-02-01
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Effective Date
- 2019/02/25
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Subject
- This AD supersedes (AD) 2018-16-07. the main change is that the compliance time for the removal and replacement of certain HPT cases must be reduced.
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Reference Publications (Revision/ATA/SB)
- ATA 72.This AD replaces AD 2018-16-07, Amendment 39-19347 (83 FR 36724, July 31, 2018) (“AD 2018-16-07”).
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Remarks
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