| 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
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| 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.
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| 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.
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| 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.
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| CAA-2021-07-018取消 |
2023/09/11 |
EASA |
2021-0180-CN |
Airbus A300, A300-600 and A310 aeroplanes, all certified models, all manufacturer serial numbers (MSN);
Airbus A300F4-608ST aeroplanes, all MSN;
Airbus A318, A319, A320 and A321 aeroplanes, all certified models, all MSN;
Airbus A330 aeroplanes, all certified models except A330-223F and A330-243F, all MSN, and
Airbus A340 aeroplanes, all certified models, all MSN.
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| CAA-2023-09-004 |
2023/09/08 |
FAA |
2023-13-11 |
This AD applies to AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblieshaving part number (P/N) 89794077, 89794015, 891511–14, 806835–01, 807982–01, 808433–01, or891311–14; and oxygen valve assemblies (body and gage assemblies) having P/N 807206–01. Theseassemblies might be installed on, but not limited to, the aircraft identified in paragraphs (c)(1) through(12) of this AD, certificated in any category.
(1) Airbus SAS Model A300 B2–1A, B2–1C, B2K–3C, B2–203, B4–2C, B4–103, and B4–203 airplanes.
(2) Airbus SAS Model A300 B4–601, B4–603, B4–620, B4–622, B4–605R, B4–622R, F4–605R, F4–622R, and C4–605R Variant F airplanes.
(3) Airbus SAS Model A310–203, –204, –221, –222, –304, –322, –324, and –325 airplanes.
(4) Airbus SAS Model A318–111, –112, –121, and –122 airplanes.
(5) Airbus SAS Model A319–111, –112, –113, –114, –115, –131, –132, –133, and –151N airplanes.
(6) Airbus SAS Model A320–211, –212, –214, –216, –231, –232, –233, –251N, –252N, –253N, –271N,–272N, and –273N airplanes.
(7) Airbus SAS Model A321–111, –112, –131, –211, –212, –213, –231, –232, –251N, –252N, –253N, –271N, –272N, –251NX, –252NX, –253NX, –271NX, and –272NX airplanes.
(8) Airbus SAS Model A330–201, –202, –203, –223, –243, –301, –302, –303, –321, –322, –323, –341, –342, –343, and –941 airplanes.
(9) Airbus Model A340–211, –212, –213, –311, –312, –313, –541, and –642 airplanes.
(10) ATR—GIE Avions de Transport Régional Model ATR42–200, –300, –320, and –500 airplanes.
(11) ATR—GIE Avions de Transport Régional Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes.
(12) The Boeing Company Model 747–8 series airplanes.
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| CAA-2021-09-013取消 |
2023/09/08 |
EASA |
2021-0218-CN |
ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer serial numbers.
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| CAA-2023-09-002 |
2023/09/06 |
EASA |
2023-0169 |
Airbus A330-841 and A330-941 aeroplanes, manufacturer serial numbers (MSN) 1819, 1836, 1850, 1870, 1876, 1884, 1887, 1890, 1892, 1895, 1897, 1900, 1901, 1903, 1904, 1906, 1908, 1909, 1910, 1913, 1914, 1915, 1918, 1920, 1921, 1922, 1923, 1924, 1925, 1926, 1927, 1929, 1931, 1933, 1934, 1935, 1937, 1938, 1939, 1941, 1943, 1946, 1947, 1948, 1949, 1953, 1954, 1956, 1957, 1962, 1963, 1964, 1969, 1977, 1978 and 1979.
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| CAA-2023-09-001 |
2023/09/05 |
FAA |
2023-17-14 |
This AD applies to all The Boeing Company Model 777–200, –200LR, –300, –300ER, and 777Fseries airplanes, certificated in any category, excluding the airplanes identified in paragraphs (c)(1)and (2) of this AD. (1) Boeing Model 777–200 series airplanes having a maximum taxi weight equal to or less than547,000 pounds.
(2) Boeing Model 777F series airplanes with manufacturer line numbers of 1743 and subsequent.
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| CAA-2023-08-013 |
2023/09/04 |
EASA |
2023-0167 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-323, A330-342, A330-343, A330-743L, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers (MSN).
Airbus A340-312 and A340-313 aeroplanes, all MSN.
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