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.
2025-17-02
SUBJECT
Joint Aircraft System Component (JASC) Code 3212, Emergency Flotation Section.
APPLICABILITY
This AD applies to Airbus Helicopters Model EC120B, EC 130 B4, and EC 130 T2 helicopters, certificated in any category.
ISSUED BY
FAA
AD NO.
2025-16-12
SUBJECT
Air Transport Association (ATA) of America Code 36, Pneumatic.
APPLICABILITY
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this AD, certificated in any category. (1) Model A319-151N, -153N, -171N, and -173N airplanes. (2) Model A320-251N, -252N, -253N, -271N, -272N, and -273N airplanes. (3) Model A321-251N, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -271NX, -272NX, -253NY, and -271NY airplanes.
ISSUED BY
FAA
AD NO.
2025-0181
SUBJECT
ATA 42 – Integrated Modular Avionics – Core Processing Input and Output Module – Replacement
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0058R2-CN
SUBJECT
ATA 36 – CANCELLED: Pneumatic – Precooler Exchanger – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2025-16-10
SUBJECT
Air Transport Association (ATA) of America Code 27, Flight controls.
APPLICABILITY
This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -272N, and -272NX airplanes.
ISSUED BY
FAA
AD NO.
2025-16-09
SUBJECT
Air Transport Association (ATA) of America Code: 25, Equipment/Furnishings, or Joint Aircraft System Component (JASC) Code 2500, Cabin Equipment/Furnishings; and 2510, Flight Compartment Equipment.
APPLICABILITY
This AD applies to all airplanes, certificated in any category, with a restraint system with a Pacific Scientific Company rotary buckle assembly (buckle) part number (P/N) 1111475 (all dash numbers) or P/N 1111548-01 installed having a date of manufacture (DOM) between January 2012 and April 2013 inclusive, or an unknown DOM. These buckles may be installed on, but not limited to, The Boeing Company model airplanes.
ISSUED BY
FAA
AD NO.
2025-16-08
SUBJECT
Joint Aircraft Service Component (JASC) Code: 6410, Tail Rotor Blades.
APPLICABILITY
This AD applies to Airbus Helicopters Model EC 130 B4 and EC 130 T2 helicopters, certificated in any category.
ISSUED BY
FAA
AD NO.
2025-16-06
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0204, dated October 22, 2024 (EASA AD 2024-0204). (1) Model A319-112 and -132 airplanes. (2) Model A320-214, -232, -233, -251N, and -271N airplanes.
ISSUED BY
FAA
AD NO.
2025-0171R1
SUBJECT
ATA 72 – Engine – High Pressure Turbine Rotor Stage 1 Blade – Inspection
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.
2025-0180
SUBJECT
ATA 25 – Equipment / Furnishings – Slide Upper Latches – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2025-16-04
SUBJECT
Air Transport Association (ATA) of America Code 25, Equipment/furnishings.
APPLICABILITY
This AD applies to all Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, -171N, and -173N airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -271NY, -272N, and -272NX airplanes.
ISSUED BY
FAA
AD NO.
2025-0175
SUBJECT
ATA – Aircraft Flight Manual – Sections Limitations and Normal Procedures – Amendment ATA – Master Minimum Equipment List – Amendment
APPLICABILITY
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 and A330-343 aeroplanes, all manufacturer serial numbers; and 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. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2025-17-02 | Joint Aircraft System Component (JASC) Code 3212, Emergency Flotation Section. | This AD applies to Airbus Helicopters Model EC120B, EC 130 B4, and EC 130 T2 helicopters, certificated in any category. |
FAA
|
| 2025-16-12 | Air Transport Association (ATA) of America Code 36, Pneumatic. | This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (3) of this AD, certificated in any category. (1) Model A319-151N, -153N, -171N, and -173N airplanes. (2) Model A320-251N, -252N, -253N, -271N, -272N, and -273N airplanes. (3) Model A321-251N, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -271NX, -272NX, -253NY, and -271NY airplanes. |
FAA
|
| 2025-0181 | ATA 42 – Integrated Modular Avionics – Core Processing Input and Output Module – Replacement | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0058R2-CN | ATA 36 – CANCELLED: Pneumatic – Precooler Exchanger – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2025-16-10 | Air Transport Association (ATA) of America Code 27, Flight controls. | This AD applies to all Airbus SAS airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -272N, and -272NX airplanes. |
FAA
|
| 2025-16-09 | Air Transport Association (ATA) of America Code: 25, Equipment/Furnishings, or Joint Aircraft System Component (JASC) Code 2500, Cabin Equipment/Furnishings; and 2510, Flight Compartment Equipment. | This AD applies to all airplanes, certificated in any category, with a restraint system with a Pacific Scientific Company rotary buckle assembly (buckle) part number (P/N) 1111475 (all dash numbers) or P/N 1111548-01 installed having a date of manufacture (DOM) between January 2012 and April 2013 inclusive, or an unknown DOM. These buckles may be installed on, but not limited to, The Boeing Company model airplanes. |
FAA
|
| 2025-16-08 | Joint Aircraft Service Component (JASC) Code: 6410, Tail Rotor Blades. | This AD applies to Airbus Helicopters Model EC 130 B4 and EC 130 T2 helicopters, certificated in any category. |
FAA
|
| 2025-16-06 | Air Transport Association (ATA) of America Code 53, Fuselage. | This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0204, dated October 22, 2024 (EASA AD 2024-0204). (1) Model A319-112 and -132 airplanes. (2) Model A320-214, -232, -233, -251N, and -271N airplanes. |
FAA
|
| 2025-0171R1 | ATA 72 – Engine – High Pressure Turbine Rotor Stage 1 Blade – Inspection | 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
|
| 2025-0180 | ATA 25 – Equipment / Furnishings – Slide Upper Latches – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2025-16-04 | Air Transport Association (ATA) of America Code 25, Equipment/furnishings. | This AD applies to all Airbus SAS Model airplanes specified in paragraphs (c)(1) through (4) of this AD, certificated in any category. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, -171N, and -173N airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) Model A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -271NY, -272N, and -272NX airplanes. |
FAA
|
| 2025-0175 | ATA – Aircraft Flight Manual – Sections Limitations and Normal Procedures – Amendment ATA – Master Minimum Equipment List – Amendment | 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 and A330-343 aeroplanes, all manufacturer serial numbers; and 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
|
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] |