| CAA-2026-08-001 |
2026/08/06 |
EASA |
2026-0153 |
ARRIEL 2B, 2B1, 2B1A, 2C, 2C1, 2C2, 2S1, 2S2, 2D, 2E, 2H, 2L2 and 2N engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France and Aerospatiale) AS 350 B3 (H125) and EC 130 T2 (H130) helicopters, on Airbus Helicopters Deutschland MBB-BK117 D-2 (EC 145 T2 or H145) helicopters, on Sikorsky S-76C helicopters, on Korea Aerospace Industries LAH and LCH helicopters and on AVIC Aircraft Industry Group AC312E helicopters.
|
|
| CAA-2026-07-019 |
2026/08/05 |
EASA |
2026-0151 |
MBB-BK117 D-3 and D-3m helicopters, all serial numbers (s/n).
|
|
| CAA-2026-07-018 |
2026/07/31 |
UK CAA |
G-2026-0003 |
This AD applies to the following two higher harness assembly part numbers which are used in emergency rescue operations on multiple aircraft types. Part Number : MRIIGQ2779
and MRIASE2494. Item : Harness Lightweight Assembly Kit.
|
|
| CAA-2026-07-017 |
2026/07/24 |
EASA |
2026-0144 |
Airbus A320-251N, A320-252N, A321-252NX and A320-271N, having manufacturer serial numbers (MSN) 12680, 12729, 12751, 12764, 12776, 12852 and 12912.
|
|
| CAA-2026-07-016 |
2026/07/24 |
EASA |
2026-0142 |
Airbus A318-112, A319-115, A319-132, A319-133, A320-214, A320-216, A320-232, A320-233, A320-251N, A320-271N, A321-211, A321-213, A321-231, A321-251NX, A321-253NX, A321-271N and A321-271NX aeroplanes, having a manufacturer serial number (MSN) listed in the Appendix 1 of this AD.
|
|
| CAA-2026-07-015 |
2026/07/24 |
EASA |
2026-0143 |
Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3,
Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3 and Trent 1000-R3 engines, all serial numbers (s/n); and
Trent 7000-68, Trent 7000-70, Trent 7000-72, Trent 7000-72 C and Trent 7000 72-D engines, all s/n.
These engines are known to be installed on, but not limited to, Boeing 787 and Airbus A330 aeroplanes, as applicable.
|
|
| CAA-2026-07-014 |
2026/07/24 |
FAA |
2026-14-03 |
This AD applies to all General Electric Company (GE) engines listed in paragraphs (c)(1) and (2) ofthis AD with a fuel tube hose installed having a part number (P/N) identified in table 1 to paragraph(c) of this AD.
(1) GEnx-1B engines: Model GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2, GEnx-1B67, GEnx-1B67/P1, GEnx-1B67/P2, GEnx-1B70, GEnx-1B70/75/P1, GEnx-1B70/75/P2, GEnx-1B70/P1,GEnx-1B70/P2, GEnx-1B70C/P1, GEnx-1B70C/P2, GEnx-1B74/75/P1, GEnx-1B74/75/P2, GEnx-1B76/P2, and GEnx-1B76A/P2.
(2) GEnx-2B engines: Model GEnx-2B67, GEnx-2B67B, and GEnx-2B67/P.
|
|
| CAA-2026-07-013 |
2026/07/24 |
EASA |
2026-0141 |
Trent 7000-68, Trent 7000-70, Trent 7000-72, Trent 7000-72C and Trent 7000-72D engines, all
engine serial numbers.
These engines are known to be installed on, but not limited to, Airbus A330 (NEO) aeroplanes.
|
|
| CAA-2026-07-011 |
2026/07/21 |
FAA |
2026-14-06 |
This AD applies to CFM International, S.A. 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 high-pressure turbine (HPT) rotorstage 1 blade, having part number (P/N) 2747M92P01, P/N 2553M91G03, P/N 2553M91G05, P/N2553M91G06, P/N 2553M91G07, or P/N 2553M91G08 that has accumulated more than 1,100South Asia takeoffs, and has accumulated 2,500 part cycles since new (PCSN) for Group 1 engines,or 5,100 PCSN for Group 2 engines.
|
|
| CAA-2026-07-012緊急 |
2026/07/16 |
Transport Canada Civil Aviation |
CF-2026-35 |
Pratt & Whitney Canada (P&WC) Models PW210A, PW210A1, and PW210S engines, all serial numbers.
|
|