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.
2024-22-05
SUBJECT
Air Transport Association (ATA) of America Code 32, Landing gear.
APPLICABILITY
This AD applies to all The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in any category.
ISSUED BY
FAA
AD NO.
2024-22-08
SUBJECT
Air Transport Association (ATA) of America Code 25, Equipment/furnishings.
APPLICABILITY
This AD applies to Airbus SAS Model Airbus A350-941 and -1041 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0073, dated March 18, 2024 (EASA AD 2024-0073).
ISSUED BY
FAA
AD NO.
2024-0225
SUBJECT
ATA 72 – Engine – Forward Outer Seal, High-Pressure Compressor Stages 6-10 Compressor Rotor Spools and High-Pressure Turbine Rotor Stage 1 Disks – Replacement
APPLICABILITY
LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, LEAP-1A35A engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, certain Airbus A319, A320 and A321 aeroplanes.
ISSUED BY
EASA
AD NO.
2023-0189R1
SUBJECT
ATA 36 – Pneumatic – Trent XWB Engine Bleed Air Supply System T-Duct – Replacement
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN). Note: While the applicability of the SB, as defined in this AD, is limited to aeroplanes having installed Trent XWB-84 and Trent XWB-97 engines, this AD is also applicable to aeroplanes having installed any Trent XWB engine.
ISSUED BY
EASA
AD NO.
2024-0222
SUBJECT
ATA 25 – Equipment / Furnishings – Equipment Rack Extension Support Rails – Modification
APPLICABILITY
MBB-BK117 C-2, all variants, all serial numbers (s/n), if modified by EASA STC EASA.R.S.01506, EASA STC 10016765 Rev. 3 (formerly STC EASA.IM.R.S.01096), EASA STC 10016793 Rev. 2 (formerly STC EASA.IM.R.S.01143), EASA STC 10017157 Rev. 1 (formerly STC EASA.R.S.01265), EASA STC 10030992 Rev. 3, EASA STC 10039944 Rev. 1 (formerly STC FOCA.21J.004-SADD-2005-001 or STC LBA STC RC 1240), or EASA STC 10075050 (previously STC FOCA 25-20-95 or LBA STC RC 1231), or any previous revision.
ISSUED BY
EASA
AD NO.
2024-0220
SUBJECT
ATA 35 – Oxygen – Cabin Oxygen Containers – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, manufacturer serial numbers (MSN) as listed in the AOT1 and AOT2.
ISSUED BY
EASA
AD NO.
2024-0217
SUBJECT
ATA 53 – Fuselage – Double Joggle Area at Frame 16 and Frame 20 – 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, A320-216, 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 and A321-272NX aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes in any of the configurations below: – Aeroplanes on which Airbus modification (mod) 160917 has been embodied in production; – A318 aeroplanes on which Airbus mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service; – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 have been embodied in production; – A319 aeroplanes on which Airbus mod 162338 has been embodied in production; – A320 aeroplanes on which Airbus mod 162339 has been embodied in production; – CEO aeroplanes on which Airbus SB A320-53-1378, SB A320-53-1379, SB A320-53-1380 and SB A320-53-1381 have been embodied in service; – NEO aeroplanes on which Airbus SB A320-53-1422, SB A320-53-1423, SB A320-53-1424, and SB A320-53-1425 have been embodied in service.
ISSUED BY
EASA
AD NO.
2024-0216
SUBJECT
ATA 32 – Landing Gear – Main Landing Gear Door Actuators – Inspections
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, A321-253NY, A321-271N, A321-271NX, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2024-0214
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – Amendment
APPLICABILITY
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0213
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – Amendment
APPLICABILITY
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-22-02
SUBJECT
Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks.
APPLICABILITY
This AD applies to Airbus SAS airplanes, identified in paragraphs (c)(1) through (5) of this AD,certificated in any category, with an original airworthiness certificate or original export certificate ofairworthiness issued on or before October 20, 2023. (1) Model A330-201, -202, -203, -223, and -243 airplanes. (2) Model A330-223F and -243F airplanes. (3) Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes. (4) Model A330-841 airplanes. (5) Model A330-941 airplanes.
ISSUED BY
FAA
AD NO.
2024-0207
SUBJECT
ATA 72 – Engine – Gas Generator First Stage High Pressure Turbine Blades – Replacement
APPLICABILITY
ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K, 1K1, 1S and 1S1 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aérospatiale, Sud Aviation) AS 350 B, BA, BB, B1 and B2, AS 365 and SA 365 (all models, except AS 365 N3) helicopters; Airbus Helicopters Deutschland (formerly Eurocopter Deutschland, Messerschmitt-Bölkow-Blohm) MBB-BK117-C1 and -C2, Leonardo (formerly AgustaWestland, Agusta) A 109 K2, and Sikorsky S-76A helicopters.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-22-05 | Air Transport Association (ATA) of America Code 32, Landing gear. | This AD applies to all The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in any category. |
FAA
|
| 2024-22-08 | Air Transport Association (ATA) of America Code 25, Equipment/furnishings. | This AD applies to Airbus SAS Model Airbus A350-941 and -1041 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0073, dated March 18, 2024 (EASA AD 2024-0073). |
FAA
|
| 2024-0225 | ATA 72 – Engine – Forward Outer Seal, High-Pressure Compressor Stages 6-10 Compressor Rotor Spools and High-Pressure Turbine Rotor Stage 1 Disks – Replacement | LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, LEAP-1A35A engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, certain Airbus A319, A320 and A321 aeroplanes. |
EASA
|
| 2023-0189R1 | ATA 36 – Pneumatic – Trent XWB Engine Bleed Air Supply System T-Duct – Replacement | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN). Note: While the applicability of the SB, as defined in this AD, is limited to aeroplanes having installed Trent XWB-84 and Trent XWB-97 engines, this AD is also applicable to aeroplanes having installed any Trent XWB engine. |
EASA
|
| 2024-0222 | ATA 25 – Equipment / Furnishings – Equipment Rack Extension Support Rails – Modification | MBB-BK117 C-2, all variants, all serial numbers (s/n), if modified by EASA STC EASA.R.S.01506, EASA STC 10016765 Rev. 3 (formerly STC EASA.IM.R.S.01096), EASA STC 10016793 Rev. 2 (formerly STC EASA.IM.R.S.01143), EASA STC 10017157 Rev. 1 (formerly STC EASA.R.S.01265), EASA STC 10030992 Rev. 3, EASA STC 10039944 Rev. 1 (formerly STC FOCA.21J.004-SADD-2005-001 or STC LBA STC RC 1240), or EASA STC 10075050 (previously STC FOCA 25-20-95 or LBA STC RC 1231), or any previous revision. |
EASA
|
| 2024-0220 | ATA 35 – Oxygen – Cabin Oxygen Containers – Inspection | Airbus A350-941 and A350-1041 aeroplanes, manufacturer serial numbers (MSN) as listed in the AOT1 and AOT2. |
EASA
|
| 2024-0217 | ATA 53 – Fuselage – Double Joggle Area at Frame 16 and Frame 20 – 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, A320-216, 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 and A321-272NX aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes in any of the configurations below: – Aeroplanes on which Airbus modification (mod) 160917 has been embodied in production; – A318 aeroplanes on which Airbus mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service; – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 have been embodied in production; – A319 aeroplanes on which Airbus mod 162338 has been embodied in production; – A320 aeroplanes on which Airbus mod 162339 has been embodied in production; – CEO aeroplanes on which Airbus SB A320-53-1378, SB A320-53-1379, SB A320-53-1380 and SB A320-53-1381 have been embodied in service; – NEO aeroplanes on which Airbus SB A320-53-1422, SB A320-53-1423, SB A320-53-1424, and SB A320-53-1425 have been embodied in service. |
EASA
|
| 2024-0216 | ATA 32 – Landing Gear – Main Landing Gear Door Actuators – Inspections | 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, A321-253NY, A321-271N, A321-271NX, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2024-0214 | ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – Amendment | Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0213 | ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – Amendment | Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-22-02 | Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. | This AD applies to Airbus SAS airplanes, identified in paragraphs (c)(1) through (5) of this AD,certificated in any category, with an original airworthiness certificate or original export certificate ofairworthiness issued on or before October 20, 2023. (1) Model A330-201, -202, -203, -223, and -243 airplanes. (2) Model A330-223F and -243F airplanes. (3) Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes. (4) Model A330-841 airplanes. (5) Model A330-941 airplanes. |
FAA
|
| 2024-0207 | ATA 72 – Engine – Gas Generator First Stage High Pressure Turbine Blades – Replacement | ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K, 1K1, 1S and 1S1 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aérospatiale, Sud Aviation) AS 350 B, BA, BB, B1 and B2, AS 365 and SA 365 (all models, except AS 365 N3) helicopters; Airbus Helicopters Deutschland (formerly Eurocopter Deutschland, Messerschmitt-Bölkow-Blohm) MBB-BK117-C1 and -C2, Leonardo (formerly AgustaWestland, Agusta) A 109 K2, and Sikorsky S-76A helicopters. |
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] |