| CAA-2023-10-006 |
2023/10/18 |
EASA |
2023-0181 |
ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers （MSN）, except those on which ATR modification （mod） 05948 has been embodied in production; 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, except those on which ATR mod 05948 has been embodied in production.
|
|
| CAA-2023-10-005 |
2023/10/16 |
EASA |
2023-0179 |
Airbus A320-214, A320-216, A320-251N, A320-271N ａｎｄ A321-253NX aeroplanes, manufacturer serial numbers 8781, 8998, 9015, 9036, 9049, 9068, 9077, 9130, 9175, 9197, 9200, 9211, 9216, 9246, 9252, 9253, 9254, 9264, 9273, 9287, 9300, 9306, 9313, 9316, 9317, 9328, 9329, 9331, 9332, 9341, 9343, 9354, 9358, 9363, 9373, 9378, 9384, 9391, 9394, 9428, 9431, 9439, 9446, 9453, 9454, 9457, 9465, 9473, 9482, 9526, 9559, 9574, 9590, 9595, 10019 ａｎｄ 10044.
|
|
| CAA-2023-10-004 |
2023/10/13 |
EASA |
2023-0176 |
Airbus A350-941 ａｎｄ A350-1041 aeroplanes, all manufacturer serial numbers.
|
|
| CAA-2023-10-003 |
2023/10/11 |
FAA |
2023-20-08 |
General Electric Company （GE） Model CF6–80C2B1F, CF6–80C2B2F, CF6–80C2B4F, CF6–80C2B5F, CF6–80C2B6F, CF6–80C2B7F, CF6–80C2K1F engines, having engine serial numbers （S/Ns） 630–136 through 630–156 inclusive, engine S/Ns 707–510 through 707–645 inclusive, which have accumulated less than 400 engine cycles since new （CSN） on the effective date of this AD.
|
|
| CAA-2023-10-002 |
2023/10/11 |
FAA |
2023-18-06 |
The Boeing Company Model 747–100, 747–100B, 747–100B SUD, 747–200B, 747–200C, 747–200F, 747–300, 747–400, 747–400D, 747–400F, 747SR series airplanes, certificated in any categy, as identified in Boeing Alert Requirements Bulletin 747–57A2367 RB, Revision 1, dated March 20, 2023.
|
|
| CAA-2023-10-001 |
2023/10/06 |
Transport Canada Civil Aviation |
CF-2023-65 |
Bombardier Inc. model BD-700-1A10 BD-700-1A11 aeroplanes, serial numbers 9001 through 9879, 9998 60001 through 60065.
|
|
| CAA-2023-09-008 |
2023/09/27 |
FAA |
2023-13-05 |
（1） This AD applies to all The Boeing Company Model 737–600, –700, –700C, –800, –900,
–900ER series airplanes, certificated in any categy.
（2） Installation of Supplemental Type Certificate （STC） ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefe, 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
|
|
| CAA-2023-09-007 |
2023/09/23 |
FAA |
2023-17-08 |
This AD applies to General Electric Company （GE） Model GEnx–1B64/P2, GEnx–1B67/P2, GEnx–1B70/75/P2, GEnx–1B70/P2, GEnx–1B70C/P2, GEnx–1B74/75/P2, GEnx–1B76/P2, GEnx–1B76A/P2, GEnx–2B67/P engines with an installed: （1） Stages 6–10 compress rot spool having a part number （P/N） serial number （S/N） listed in paragraph 4, Appendix—A, Table 1 of GE GEnx–1B Service Bulletin 72–0515, R00, dated January 31, 2023 （GEnx–1B 72–0515 R00）; （2） Fward seal having a P/N S/N listed in paragraph 4, Appendix—A, Table 2 of GEnx–1B 72–0515 R00;
（3） Stages 6–10 compress rot spool having a P/N S/N listed in paragraph 4, Appendix—A,
Table 1 of GE GEnx–2B Service Bulletin 72–0452, R00, dated January 31, 2023. （GEnx–2B 72–0452 R00）; （4） Fward seal having a P/N S/N listed in paragraph 4, Appendix—A, Table 2 of GEnx–2B 72–0452 R00.
|
|
| CAA-2023-09-006 |
2023/09/19 |
FAA |
2023-18-04 |
This AD applies to General Electric Company Model CF6–80E1A2, CF6–80E1A3, CF6–80E1A4, CF6–80E1A4/B engines with an installed fward outer seal, high-pressure turbine rot （HPTR） stage 1 disk, rotating seal having a part number （P/N） serial number （S/N） identified in Table 1 to paragraph （c） of this AD.
|
|
| CAA-2023-09-003 |
2023/09/12 |
FAA |
2023-16-07 |
This AD applies to International Aero Engines, LLC (IAE LLC) Model PW1122G–JM, PW1124G1–JM, PW1124G–JM, PW1127G–JM, PW1127G1–JM, PW1127GA–JM, PW1129G–JM, PW1130G–JM, PW1133G–JM, PW1133GA–JM, PW1428G–JM, PW1428GA–JM, PW1428GH–JM,PW1431G–JM, PW1431GA–JM, and PW1431GH–JM engines with an installed:
(1) High-pressure turbine (HPT) 1st-stage hub, part number (P/N) 30G6201 or 30G7301, with aserial number (S/N) listed in Tables 1, 2, 3, or 4 of Pratt & Whitney (PW) Special Instruction No.149F–23, dated August 4, 2023; or
(2) HPT 2nd-stage hub, P/N 30G5502 or 30G6602, with an S/N listed in Tables 1, 2, 3, or 4 of PWSpecial Instruction No. 149F–23, dated August 4, 2023.
|
|