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 : 240
AD NO.
2024-0027
SUBJECT
ATA 57 – Wings – Bottom Wing Skin Panel 2 – Inspection
APPLICABILITY
Airbus 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, A321-211, 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.
ISSUED BY
EASA
AD NO.
2024-0026
SUBJECT
ATA 72 – Engine – High Pressure Turbine – Rotor Interstage Seal – 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.
2024-0025
SUBJECT
ATA 11 – Placards and Markings – Cargo Height Limitation – ImplementationATA – Cargo Loading Procedure – Amendment
APPLICABILITY
ATR 42 and ATR 72, all certified models, all manufacturer serial numbers (MSN), on which EASA STC 10069551 Rev. 1 or EASA STC 2004-2872 has been embodied.
ISSUED BY
EASA
AD NO.
2024-0023
SUBJECT
ATA 25 – Equipment/Furnishings – Galley 4 Aft Bulkhead Cover Panel – Replacement
APPLICABILITY
A330-243, A330-302, A330-343 and A330-941 aeroplanes, manufacturer serial numbers (MSN) 1627, 1628, 1637, 1679, 1691, 1692, 1701, 1716, 1720, 1721, 1745, 1754, 1757, 1769, 1779, 1783, 1792, 1872, 1878, 1915, 1920, 1931, 1935, 1949, 1953, 1957, 1962, 1983, 1990, 1991, 1994, 1999, 2000 and 2010.
ISSUED BY
EASA
AD NO.
2024-0022
SUBJECT
ATA 32 – Landing Gear – Nose Landing Gear – Repair Assessment
APPLICABILITY
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, 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, A321-211, 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.
ISSUED BY
EASA
AD NO.
2024–01–11
SUBJECT
Joint Aircraft System Component (JASC) Code: 2500, Cabin Equipment/Furnishings.
APPLICABILITY
This AD applies to all helicopters, certified 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 between January 2012 andSeptember 2012 inclusive or an unknown date of manufacture. These buckles may be installed on, but not limited to, Airbus Helicoptersmodel helicopters, certificated in any category.
ISSUED BY
FAA
AD NO.
2024-0020
SUBJECT
ATA 31 – Indicating and Recording Systems – Flight Warning Computer Software – Modification
APPLICABILITY
Airbus A340-541, A340-542, A340-642 and A340-643 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024–02–51
SUBJECT
Air Transport Association (ATA) of America Code 52, Doors.
APPLICABILITY
This AD applies to The Boeing Company Model 737–9 airplanes, certificated in any category, with a mid cabin door plug installed.
ISSUED BY
FAA
AD NO.
CF-2024-02
SUBJECT
Stabilizers – Horizontal Stabilizer – Incorrect Torque Specified for Attachment Bolts
APPLICABILITY
Diamond Aircraft Industries Inc. model DA 62 aeroplanes, serial numbers 62.C001 through 62.C044 and 62.008 through 62.203.
ISSUED BY
TCCA
AD NO.
2024-0016
SUBJECT
ATA 27 – Flight Controls – Trimmable Horizontal Stabilizer Actuator / Electric Load Sensing Device – Modification
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, and A330-941 aeroplanes, all manufacturer serial numbers (MSN) up to MSN 1919 inclusive, except MSN 1915; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.
ISSUED BY
EASA
AD NO.
2024-0014
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – System Equipment Maintenance Requirements – ALS Part 4 – 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.
2024-0013
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. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-0027 | ATA 57 – Wings – Bottom Wing Skin Panel 2 – Inspection | Airbus 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, A321-211, 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. |
EASA
|
| 2024-0026 | ATA 72 – Engine – High Pressure Turbine – Rotor Interstage Seal – 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
|
| 2024-0025 | ATA 11 – Placards and Markings – Cargo Height Limitation – ImplementationATA – Cargo Loading Procedure – Amendment | ATR 42 and ATR 72, all certified models, all manufacturer serial numbers (MSN), on which EASA STC 10069551 Rev. 1 or EASA STC 2004-2872 has been embodied. |
EASA
|
| 2024-0023 | ATA 25 – Equipment/Furnishings – Galley 4 Aft Bulkhead Cover Panel – Replacement | A330-243, A330-302, A330-343 and A330-941 aeroplanes, manufacturer serial numbers (MSN) 1627, 1628, 1637, 1679, 1691, 1692, 1701, 1716, 1720, 1721, 1745, 1754, 1757, 1769, 1779, 1783, 1792, 1872, 1878, 1915, 1920, 1931, 1935, 1949, 1953, 1957, 1962, 1983, 1990, 1991, 1994, 1999, 2000 and 2010. |
EASA
|
| 2024-0022 | ATA 32 – Landing Gear – Nose Landing Gear – Repair Assessment | Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, 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, A321-211, 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. |
EASA
|
| 2024–01–11 | Joint Aircraft System Component (JASC) Code: 2500, Cabin Equipment/Furnishings. | This AD applies to all helicopters, certified 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 between January 2012 andSeptember 2012 inclusive or an unknown date of manufacture. These buckles may be installed on, but not limited to, Airbus Helicoptersmodel helicopters, certificated in any category. |
FAA
|
| 2024-0020 | ATA 31 – Indicating and Recording Systems – Flight Warning Computer Software – Modification | Airbus A340-541, A340-542, A340-642 and A340-643 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024–02–51 | Air Transport Association (ATA) of America Code 52, Doors. | This AD applies to The Boeing Company Model 737–9 airplanes, certificated in any category, with a mid cabin door plug installed. |
FAA
|
| CF-2024-02 | Stabilizers – Horizontal Stabilizer – Incorrect Torque Specified for Attachment Bolts | Diamond Aircraft Industries Inc. model DA 62 aeroplanes, serial numbers 62.C001 through 62.C044 and 62.008 through 62.203. |
TCCA
|
| 2024-0016 | ATA 27 – Flight Controls – Trimmable Horizontal Stabilizer Actuator / Electric Load Sensing Device – Modification | 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, and A330-941 aeroplanes, all manufacturer serial numbers (MSN) up to MSN 1919 inclusive, except MSN 1915; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN. |
EASA
|
| 2024-0014 | ATA 05 – Time Limits / Maintenance Checks – System Equipment Maintenance Requirements – ALS Part 4 – 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
|
| 2024-0013 | 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
|
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] |