| CAA-2019-05-003修訂 |
2019/07/08 |
ANAC |
Brazilian 2019-05-02Correction |
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 with manufacturer serial numbers 19000002, 19000004,
19000006 through 19000213, 19000215 through 19000276, 19000278 through 19000466, 19000468
through 19000525, 19000527 through 19000758, inclusive, in operation.
Note (1): Airplanes with an original airworthiness certificate or original export certificate
of airworthiness issued on or after September 27, 2018 must comply with the airworthiness limitations
specified as part of the airworthiness certification of those airplanes, or in accordance with operations
specifications approved under “Regulamento Brasileiro da Aviação Civil” (RBAC) 121 or 135, or an
inspection program approved under paragraph 91.409(e) of “Regulamento Brasileiro de Homologação
Aeronáutica” (RBHA) 91.
Note (2): This AD requires revisions to certain operator maintenance documents to include
new inspections or modification to the existing ones and its respective thresholds and intervals.
Compliance with these inspections is required by RBHA 91.403(c). For airplanes that have been
previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not
be able to accomplish the inspections described in the revisions. In this situation, to comply with RBHA
91.403(c), the operator must request approval for an alternative method of compliance according to
paragraph (c) of this AD. The request should include a description of changes to the required inspections
that will ensure the continued damage tolerance of the affected structure.
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| CAA-2019-07-001緊急 |
2019/07/01 |
EASA |
2019-0151-E |
Airbus A319-111, A319-112, A319-115, A319-131, A320-214 and A320-232 aeroplanes, manufacturer serial numbers (MSN) 0921, 2007, 2015, 2172, 2202, 2205, 2237, 2238, 2269, 2285, 2293, 2298, 2454, 2499, 2525, 2545, 2551, 2561 and 2638.
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| CAA-2019-05-012A(已被CAA-2019-08-001取代) |
2019/07/01 |
EASA |
2019-0121R1 |
AW169 helicopters, all serial numbers (s/n); and AW189 helicopters, all s/n.
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| CAA-2019-06-013(已被CAA-2019-07-001緊急取代) |
2019/06/27 |
EASA |
2019-0147 |
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 and A320-233, aeroplanes, all manufacturer serial numbers.
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| CAA-2019-06-012 |
2019/06/27 |
EASA |
2019-0146 |
CFM56-5B1, CFM56-5B2, CFM56-5B4, CFM56-5B5, CFM56-5B6, CFM56-5B7, CFM56-5B1/P, CFM56-5B2/P, CFM56-5B3/P, CFM56-5B4/P, CFM56-5B5/P, CFM56-5B6/P, CFM56-5B7/P, CFM56-5B8/P, CFM56-5B9/P, CFM56-5B3/P1, CFM56-5B4/P1, CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P, CFM56-5B4/2P, CFM56-5B6/2P, CFM56-5B9/2P, CFM56-5B3/2P1 and CFM56-5B4/2P1 engines, all serial numbers (s/n);
CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F, CFM56-5C2/F4, CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C2/P, CFM56-5C3/F, CFM56-5C3/F4, CFM56-5C3/G, CFM56-5C3/G4, CFM56-5C3/P, CFM56-5C4, CFM56-5C4/1, CFM56-5C4/P and CFM56-5C4/1P engines, all s/n; and
CFM56-7B20, CFM56-7B22, CFM56-7B24, CFM56-7B26, CFM56-7B27, CFM56-7B22/B1, CFM56-7B24/B1, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B20/2, CFM56-7B22/2, CFM56-7B24/2, CFM56-7B26/2, CFM56-7B27/2 and CFM56-7B27A engines, all s/n.
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| CAA-2019-06-011 |
2019/06/25 |
FAA |
2019-11-02 |
This AD applies to The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 777-53A0081, Revision 2, dated March 29, 2019.
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| 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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