Other State of Design
Airworthiness Directives (ADs) are issued to address unsafe conditions.
Aircraft on the Thai Register are required to comply with applicable ADs in accordance with Requirement of The Civil Aviation Authority of Thailand No.89 attach with TCAR AIR Part-39.
Additionally, Airworthiness Directive (AD) issued by CAAT for products, parts and appliances where Thailand are either state of register or state of design or state of design of modification in accordance with Air Navigation Act (BE 2497) Section 41/82 are required to be complied.
The list of all active ADs is provided in the following Table.
Total : 1090
AD NO.
2024-0097R1
SUBJECT
ATA 53 – Fuselage – Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings – Inspection
APPLICABILITY
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, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N, A321-272NX aeroplanes, all manufacturer serial numbers, except those aeroplanes on which Airbus modification (mod) 165315 has been embodied in production.
ISSUED BY
EASA
AD NO.
2024-10-04
SUBJECT
Joint Aircraft System Component (JASC) Code 5740, Wing, Attach Fittings.
APPLICABILITY
This AD applies to Piper Aircraft, Inc. Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes, certificated in any category,serial numbers as identified in Piper Service Bulletin No. 1413, dated April 9, 2024 (Piper Service Bulletin No. 1413).
ISSUED BY
FAA
AD NO.
2024-09-03
SUBJECT
Air Transport Association (ATA) of America Code 27, Flight Controls.
APPLICABILITY
Air Transport Association (ATA) of America Code 27, Flight Controls.
ISSUED BY
FAA
AD NO.
2024-0102
SUBJECT
ATA 72 – Engine – Low Pressure Compressor Blades – Inspection / Replacement
APPLICABILITY
RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A330 aeroplanes.
ISSUED BY
EASA
AD NO.
2020-0195R1
SUBJECT
ATA 72 – Engine – Low Pressure Turbine Discs – Inspection
APPLICABILITY
Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2 and Trent 1000-L2 engines, all serial numbers.
ISSUED BY
EASA
AD NO.
2024-0088 [Correction: 14 May 2024]
SUBJECT
ATA 11 – Placards and Markings– Rear Facing Seat(s) – Placard Installation
APPLICABILITY
AB139 and AW139 helicopters, serial numbers 31087, 31133, 31269, 31305, 31351, 31502, 31712, 31735, 31757, 31865, 31869, 41582 and 41583, if modified in accordance with EASA STC 10030095 original issue and subsequent revisions, or STC 10017198 original issue and subsequent revisions.
ISSUED BY
EASA
AD NO.
2024-0101
SUBJECT
ATA 28 – Fuel – Engine Low Pressure Shut Off Valve Electrical Harness Routing – Modification
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except those on which Airbus modification (mod) 77076 has been embodied in production.
ISSUED BY
EASA
AD NO.
2024-0087 [Correction: 14 May 2024]
SUBJECT
ATA 57 – Wings – Metallic Wing Rib Feet – Inspection
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 00003 to 00092 inclusive, 00097 to 00099 inclusive, and 00101 to 00109 inclusive.
ISSUED BY
EASA
AD NO.
AD/GA8/3 Amdt 4
SUBJECT
Forward Cargo Door Slide
APPLICABILITY
This AD applies to all GA8 Series Aeroplanes manufactured by Gippsland Aeronautics.
ISSUED BY
CASA
AD NO.
2024-06-15 Correction
SUBJECT
Joint Aircraft System Component (JASC) Code 7250, Turbine Section.
APPLICABILITY
This AD applies to General Electric Company (GE) Model GE90-110B1 and GE90-115B engines with an installed interstage high-pressure turbine (HPT) rotor seal having a part number and serial number listed in Table 1 or Table 2 of GE GE90-100 Service Bulletin (SB) 72-0908 R00, dated July 7, 2023 (GE SB 72-0908).
ISSUED BY
FAA
AD NO.
2024-07-02
SUBJECT
Joint Aircraft System Component (JASC) Code 7250, Turbine Section.
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) 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
ISSUED BY
FAA
AD NO.
2024-0099
SUBJECT
ATA 25 – Equipment / Furnishings – Fuselage / Belly Fairing Mounted Emergency Evacuation Escape Slides – Replacement
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-0097R1 | ATA 53 – Fuselage – Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings – Inspection | 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, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX, A321-272N, A321-272NX aeroplanes, all manufacturer serial numbers, except those aeroplanes on which Airbus modification (mod) 165315 has been embodied in production. |
EASA
|
| 2024-10-04 | Joint Aircraft System Component (JASC) Code 5740, Wing, Attach Fittings. | This AD applies to Piper Aircraft, Inc. Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes, certificated in any category,serial numbers as identified in Piper Service Bulletin No. 1413, dated April 9, 2024 (Piper Service Bulletin No. 1413). |
FAA
|
| 2024-09-03 | Air Transport Association (ATA) of America Code 27, Flight Controls. | Air Transport Association (ATA) of America Code 27, Flight Controls. |
FAA
|
| 2024-0102 | ATA 72 – Engine – Low Pressure Compressor Blades – Inspection / Replacement | RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A330 aeroplanes. |
EASA
|
| 2020-0195R1 | ATA 72 – Engine – Low Pressure Turbine Discs – Inspection | Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2 and Trent 1000-L2 engines, all serial numbers. |
EASA
|
| 2024-0088 [Correction: 14 May 2024] | ATA 11 – Placards and Markings– Rear Facing Seat(s) – Placard Installation | AB139 and AW139 helicopters, serial numbers 31087, 31133, 31269, 31305, 31351, 31502, 31712, 31735, 31757, 31865, 31869, 41582 and 41583, if modified in accordance with EASA STC 10030095 original issue and subsequent revisions, or STC 10017198 original issue and subsequent revisions. |
EASA
|
| 2024-0101 | ATA 28 – Fuel – Engine Low Pressure Shut Off Valve Electrical Harness Routing – Modification | Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except those on which Airbus modification (mod) 77076 has been embodied in production. |
EASA
|
| 2024-0087 [Correction: 14 May 2024] | ATA 57 – Wings – Metallic Wing Rib Feet – Inspection | Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 00003 to 00092 inclusive, 00097 to 00099 inclusive, and 00101 to 00109 inclusive. |
EASA
|
| AD/GA8/3 Amdt 4 | Forward Cargo Door Slide | This AD applies to all GA8 Series Aeroplanes manufactured by Gippsland Aeronautics. |
CASA
|
| 2024-06-15 Correction | Joint Aircraft System Component (JASC) Code 7250, Turbine Section. | This AD applies to General Electric Company (GE) Model GE90-110B1 and GE90-115B engines with an installed interstage high-pressure turbine (HPT) rotor seal having a part number and serial number listed in Table 1 or Table 2 of GE GE90-100 Service Bulletin (SB) 72-0908 R00, dated July 7, 2023 (GE SB 72-0908). |
FAA
|
| 2024-07-02 | Joint Aircraft System Component (JASC) Code 7250, Turbine Section. | This AD applies to CFM International, S.A. (CFM) 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 |
FAA
|
| 2024-0099 | ATA 25 – Equipment / Furnishings – Fuselage / Belly Fairing Mounted Emergency Evacuation Escape Slides – Replacement | Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
Contact
| No | Enquiry Topic | Email Point of Contact |
|---|---|---|
| 1 | Aircraft Registration and De-Registration | [email protected] |
| 2 | Certification of Design and Production of Aircraft (DOA/POA), including: – Aircraft Modification and Repair Approval – Aircraft Type Certificate (TC) / Supplemental Type – Certificate (STC) Validation – Aircraft Noise Certificate | [email protected] |
| 3 | Certification of Airworthiness for Air Operator Certificate (AOC) Holders | [email protected] |
| 4 | Certification of Airworthiness for Non-Air Operator Certificate (Non-AOC) Holders (I.E. GA Aircraft) | [email protected] |
| 5 | Certification of Approved Maintenance Organisation (AMO) | [email protected] |
| 6 | Any Other Matters Not Covered Above | [email protected] |