| CAA-2024-05-002 |
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 |
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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| CAA-2024-03-010修訂 |
2024/04/30 |
EASA |
2024-0077Correction |
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, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers （MSN）, except those having Airbus modification （mod） 151574 embodied in production.
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| CAA-2023-01-011A |
2024/04/30 |
EASA |
2023-0013R1 |
DA 42, DA 42 M, DA 42 NG and DA 42 M-NG aeroplanes （including those certified in the Restricted category）, all manufacturer serial numbers （MSN）.
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| CAA-2024-04-008 |
2024/04/25 |
EASA |
2024-0093 |
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, all serial numbers （s/n）. These engines are known to be installed on, but not limited to, certain Airbus A319, A320 and A321 aeroplanes.
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| CAA-2024-04-007 |
2024/04/24 |
Transport Canada Civil Aviation |
CF-2024-12 |
Bombardier Inc. model CL-600-1A11, CL-600-2A12 and CL-600-2B16 aeroplanes, all serial numbers.
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| CAA-2024-04-006 |
2024/04/24 |
FAA |
2024-06-01 |
This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, -900 and -900ER airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-53A1407 RB, dated December 20, 2022.
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