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.
2025-0167R1
SUBJECT
ATA 32 – Landing Gear – Main Landing Gear Aft Pintle Pin – Replacement
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, A319-173N, 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, A321-271NY, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2025-0189
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, A319-173N, 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, and 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.
AD ISR I-05-2025-09-1
SUBJECT
G200 Airworthiness Limitations Section (ALS) revision
APPLICABILITY
All G200 / Galaxy Model Aircrafts
ISSUED BY
CAA Israel
AD NO.
2025-0188
SUBJECT
ATA 25 – Equipment / Furnishings – Large Hook Damper Assembly – Modification
APPLICABILITY
MBB-BK117 C-2 and MBB-BK117 D-2 helicopters, all variants, all serial numbers.
ISSUED BY
EASA
AD NO.
2025-17-15
SUBJECT
Air Transport Association (ATA) of America Code 29, Hydraulic Power.
APPLICABILITY
This AD applies to ATR—GIE Avions de Transport Régional Model ATR42-500 and ATR72-212A airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0103, dated May 5, 2025 (EASA AD 2025-0103).
ISSUED BY
FAA
AD NO.
2025-17-07
SUBJECT
Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks.
APPLICABILITY
This AD applies to Airbus SAS airplanes, in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before August 7, 2024. (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, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -253NY, -271NX, and -272NX airplanes.
ISSUED BY
FAA
AD NO.
2025-17-06
SUBJECT
Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks.
APPLICABILITY
This AD applies to Airbus SAS Model airplanes, identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 1, 2024. (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.
2025-17-05
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
This AD applies to all Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes, certificated in any category.
ISSUED BY
FAA
AD NO.
2025-17-04
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
This AD applies to Airbus SAS Airplanes identified in paragraph (c)(1) through (5) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0200, dated October 21, 2024 (EASA AD 2024-0200). (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.
2025-17-09
SUBJECT
Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks.
APPLICABILITY
This AD applies to ATR—GIE Avions de Transport Régional Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0159, dated August 16, 2024 (EASA AD 2024-0159).
ISSUED BY
FAA
AD NO.
2025-0185
SUBJECT
ATA 57 – Wings – Pylon Spigot Fitting – 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, A319-173N, 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, A321-271NY, A321-272N, and A321-272NX, aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2025-0183
SUBJECT
ATA 73 – Engine Fuel and Control – Hydro-Mechanical Unit – Replacement / Life Limitation
APPLICABILITY
Airbus A350-941 aeroplanes, all manufacturer serial numbers equipped with Rolls-Royce Trent XWB-84 engines, Trent XWB-84EP engines or Trent XWB-75 engines.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2025-0167R1 | ATA 32 – Landing Gear – Main Landing Gear Aft Pintle Pin – Replacement | 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, A319-173N, 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, A321-271NY, A321-272N and A321-272NX aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2025-0189 | 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, A319-173N, 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, and A321-272NX, aeroplanes, all manufacturer serial numbers except those aeroplanes on which Airbus modification (mod) 165315 has been embodied in production. |
EASA
|
| AD ISR I-05-2025-09-1 | G200 Airworthiness Limitations Section (ALS) revision | All G200 / Galaxy Model Aircrafts |
CAA Israel
|
| 2025-0188 | ATA 25 – Equipment / Furnishings – Large Hook Damper Assembly – Modification | MBB-BK117 C-2 and MBB-BK117 D-2 helicopters, all variants, all serial numbers. |
EASA
|
| 2025-17-15 | Air Transport Association (ATA) of America Code 29, Hydraulic Power. | This AD applies to ATR—GIE Avions de Transport Régional Model ATR42-500 and ATR72-212A airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0103, dated May 5, 2025 (EASA AD 2025-0103). |
FAA
|
| 2025-17-07 | Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. | This AD applies to Airbus SAS airplanes, in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before August 7, 2024. (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, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -253NY, -271NX, and -272NX airplanes. |
FAA
|
| 2025-17-06 | Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. | This AD applies to Airbus SAS Model airplanes, identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 1, 2024. (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
|
| 2025-17-05 | Air Transport Association (ATA) of America Code 53, Fuselage. | This AD applies to all Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes, certificated in any category. |
FAA
|
| 2025-17-04 | Air Transport Association (ATA) of America Code 53, Fuselage. | This AD applies to Airbus SAS Airplanes identified in paragraph (c)(1) through (5) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0200, dated October 21, 2024 (EASA AD 2024-0200). (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
|
| 2025-17-09 | Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. | This AD applies to ATR—GIE Avions de Transport Régional Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2024-0159, dated August 16, 2024 (EASA AD 2024-0159). |
FAA
|
| 2025-0185 | ATA 57 – Wings – Pylon Spigot Fitting – 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, A319-173N, 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, A321-271NY, A321-272N, and A321-272NX, aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2025-0183 | ATA 73 – Engine Fuel and Control – Hydro-Mechanical Unit – Replacement / Life Limitation | Airbus A350-941 aeroplanes, all manufacturer serial numbers equipped with Rolls-Royce Trent XWB-84 engines, Trent XWB-84EP engines or Trent XWB-75 engines. |
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] |