| CAA-2024-05-007 |
2024/05/17 |
FAA |
2024-06-14 |
This AD applies to International Aero Engines, LLC Model PW1124G1-JM, PW1127G-JM, PW1127GA-JM,PW1129G-JM, PW1130G-JM, PW1133G-JM, and PW1133GA-JM engines having a high-pressurecompressor （HPC） 2nd stage rotor or HPC 4th stage rotor having a part number and serial numberidentified in the Applicability, Table 2, of Pratt & Whitney （PW） Alert Service Bulletin （ASB） PW1000G-C-72-00-0208-00A-930A-D, Issue 002, dated January 18, 2024 （PW ASB PW1000G-C-72-00-0208-00A-930A-D, Issue 002）.
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| CAA-2024-05-006 |
2024/05/17 |
EASA |
2024-0097 |
Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N, A321-272NX aeroplanes, all manufacturer serial numbers, except those aeroplanes on which Airbus modification （mod） 165315 has been embodied in production.
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| CAA-2024-04-010修訂 |
2024/05/15 |
FAA |
2024-06-15Correction |
This AD applies to General Electric Company （GE） Model GE90-110B1 and GE90-115B engines with aninstalled interstage high-pressure turbine （HPT） rotor seal having a part number and serial numberlisted in Table 1 or Table 2 of GE GE90-100 Service Bulletin （SB） 72-0908 R00, dated July 7, 2023 （GESB 72-0908）.
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| CAA-2024-05-005 |
2024/05/10 |
EASA |
2024-0096 |
ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers （MSN）; and
ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN.
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| CAA-2024-05-003 |
2024/05/09 |
FAA |
2024-07-02 |
This AD applies to CFM International, S.A. Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines.
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| CAA-2024-05-002(已被CAA-2024-07-003取代) |
2024/05/06 |
EASA |
2024-0098 |
Airbus A350-941 aeroplanes manufacturer serial numbers （MSN） 0001 through 0645 （inclusive）, except aeroplanes having Airbus modification （mod） 113979 embodied in production; and
A350-1041 aeroplanes, MSN 00059 through 00584 inclusive.
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| CAA-2024-05-001 |
2024/05/03 |
EASA |
2024-0095 |
Airbus A330-202, A330-203 and A330-243 aeroplanes modified in accordance with EASA STC 10029272 （previously STC EASA.A.S.02790） （RAAF, RSAF and UAE） or 10063084 （GOS） or 10064192 （FAF） or 10034690 （FSTA STC 1） or 10035945 （FSTA STC 2）, all manufacturer serial numbers （MSN） up to MSN 1779 inclusive, on which Airbus Service Bulletin （SB） A330-53-3275-00 （original issue） or SB A330-53-3275-01 （Revision 01） has been embodied in service, except those on which, during this SB embodiment, the specified roto test was accomplished （no defects found, or defects were corrected, as applicable） in accordance with the instructions of the above referenced SB.
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| CAA-2024-04-011 |
2024/05/03 |
FAA |
2024-07-06 |
This AD applies to CFM International, S.A. （CFM） Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines with an installed No. 3 bearing spring finger housing having part number （P/N） 2629M62G01 and aserial number identified in Table 1 or Table 2 of CFM Service Bulletin （SB） LEAP-1A-72-00-0504-01A-930A-D, Issue002, dated October 17, 2023 （CFM SB LEAP-1A-72-00-0504-01A-930A-D, Issue 002）.
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| CAA-2024-04-010(已被CAA-2024-04-010修訂取代) |
2024/05/01 |
FAA |
2024-06-15 |
This AD applies to General Electric Company （GE） Model GE90-110B1 and GE90-115B engines with an installed interstage high-pressure turbine （HPT） rotor seal having a part number and serial number listed in Table 1 or Table 2 of GE GE90-100 Service Bulletin （SB） 72-A0908 R00, dated July 7, 2023 （GE SB 72-A0908）.
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| CAA-2024-04-009 |
2024/04/30 |
EASA |
2024-0094 |
Occupant restraint harnesses Part Number （P/N） CI-C-1302.
The affected （Ultramagic） occupant restraint harnesses are known to be installed on, but not limited to, certain Ultramagic hot air balloons. Affected occupant restraint harnesses may however be eligible for installation on any （hot air） balloon and may therefore have been installed during the balloon manufacturing process （production line）, or during an in-service modification, either through using Type Certificate holder approved modification instructions, or a Supplemental Type Certificate （STC）, or through a minor modification approval.
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