| CAA-2019-06-010(已被CAA-2021-08-007取代) |
2019/06/25 |
FAA |
2019-12-05 |
This AD applies to: (1) CFM International S.A. (CFM) CFM56-5B1, -5B2, -5B4, -5B5, -5B6, -5B7, -5B1/P, -5B2/P, -5B3/P, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P, -5B3/P1, -5B4/P1, -5B1/2P, -5B2/2P, -5B3/2P, -5B4/2P, -5B6/2P, -5B9/2P, -5B3/2P1, -5B4/2P1, -7B20, -7B22, -7B24, -7B26, -7B27, -7B22/B1, -7B24/B1, -7B26/B1, -7B26/B2, -7B27/B1, -7B27/B3, -7B20/2, -7B22/2, -7B24/2, -7B26/2, -7B27/2, -7B27A model turbofan engines with a:
(i) rotating air high-pressure turbine (HPT) front seal:
(A) with part number (P/N) 1795M36P01 or P/N 1795M36P02 and serial numbers (S/Ns) GWNDN949 through GWNSE969 or S/Ns GWN000CE through GWN0990L, not including S/Ns GWN08ND7, GWN0923A, GWN0971E, GWN098A1, GWN098W6, GWN098W8, GWN098WA, and GWN0990G, installed;
(B) that has been removed from the original HPT disk and re-assembled to a different HPT disk; and
(C) that has 6,001 or more cycles since being reconfigured.
(ii) [Reserved]
(2) CFM CFM56-5C2, -5C2/4, -5C2/F, -5C2/F4, -5C2/G, -5C2/G4, -5C2/P, -5C3/F, -5C3/F4, -5C3/G, -5C3/G4, -5C3/P, -5C4, -5C4/1, -5C4/P, -5C4/1P model turbofan engines with a: (i) rotating air HPT front seal: (A) with P/N 1795M36P01 or P/N 1795M36P02 and S/Ns GWNDN949 through GWNSE969 or S/Ns GWN000CE through GWN0990L, not including S/Ns GWN08ND7, GWN0923A, GWN0971E, GWN098A1, GWN098W6, GWN098W8, GWN098WA, and GWN0990G, installed;
(B) that has been removed from the original HPT disk and re-assembled to a different HPT disk; and
(C) that has 3,751 or more cycles since being reconfigured.
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| CAA-2019-06-009 |
2019/06/21 |
ANAC |
Brazilian 2019-06-01 |
This Airworthiness Directive applies to Embraer S.A. ERJ 190-100 STD, ERJ 190-100 LR,
ERJ 190-100 IGW, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR, and ERJ 190-200 IGW
airplanes models, with serial numbers 19000001, 19000003, 19000004, and 19000006 thru 19000077.
ERJ 190-100 IGW, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR, and ERJ 190-200 IGW
airplanes models, with serial numbers 19000001, 19000003, 19000004, and 19000006 thru 19000077.
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| CAA-2019-06-008 |
2019/06/17 |
EASA |
2019-0110 |
ARRIEL 2C, 2C1, 2S1 and 2S2 engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters AS 365 N3, EC 155 B and Sikorsky S-76C helicopters.
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| CAA-2019-06-007 |
2019/06/17 |
FAA |
2019-11-06 |
This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-53A1368, dated February and Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, 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-2019-06-006 |
2019/06/17 |
EASA |
2019-0140 |
Airbus A330-941 aeroplanes, all manufacturer serial numbers.
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| CAA-2019-06-005(已被CAA-2019-06-005A修訂取代) |
2019/06/17 |
EASA |
2019-0138 |
Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.
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| CAA-2015-11-005D(已有後續修訂版) |
2019/06/17 |
EASA |
2015-0226R4 |
This AD applies to the following helicopters, when equipped with a Goodrich hoist having a Part Number (P/N) as listed in Table 1 of this AD: Leonardo AW109SP, AB139, AW139 and AB412 (all Models) helicopters, all serial numbers (s/n); BHTI 212, 214 and 412 helicopters (all Models), all s/n; BHTC 429 and 430 helicopters, all s/n; AH AS 365 N3, AS 332 L2 and EC225 LP helicopters, all s/n; AHD MBB-BK117 C-2, EC135 and EC635 (all Models) helicopters, all s/n; MDHI MD900 helicopters, all s/n; and Sikorsky S-61 (all Models), S-76A, S-76B, S-76C and S-92A helicopters, all s/n.
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| CAA-2019-06-004 |
2019/06/13 |
FAA |
2019-11-03 |
This AD applies to The Boeing Company Model 737-700C, -800, and -900ER series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-27A1312 RB, dated June 4, 2019. and Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, 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-2019-06-003 |
2019/06/11 |
EASA |
2019-0125 |
Embraer ERJ 170-100 STD, ERJ 170-100 LR, ERJ 170-200 STD, ERJ 170-200 LR, ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR and ERJ 190-200 IGW aeroplanes, all serial numbers (s/n), if modified to have an affected stretcher installed in accordance with EASA STC 10030758, formerly STC number EASA.A.S.03712.
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| CAA-2019-06-002 |
2019/06/11 |
EASA |
2019-0126 |
Airbus A350-941 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 111207 or mod 111445 has been embodied in production.
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