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.
2024–01–06
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
This AD applies to The Boeing Company Model 737–600, 737–700, and 737–800 series airplanes, certificated in any category, as identifiedin Boeing Alert Service Bulletin 737–53A1217, Revision 1, dated September 8, 2022.
ISSUED BY
FAA
AD NO.
2024-0031 [Correction: 01 February 2024]
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment
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 and A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0031
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment
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 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.
2024-0030
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 – Certification Maintenance Requirements – Amendment
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 and A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0029
SUBJECT
ATA 79 – Engine Oil – Lubrication / Scavenge Oil Pumps – Installation Criteria
APPLICABILITY
Trent 7000-72 and Trent 7000-72C engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A330 (NEO) aeroplanes.
ISSUED BY
EASA
AD NO.
2024-0028-E
SUBJECT
ATA 64 – Tail Rotor – Tail Rotor Blades – Inspection
APPLICABILITY
EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 P3, EC635 T1, EC635 T2+ and EC635 T3 helicopters, all variants, all serial numbers (s/n).
ISSUED BY
EASA
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 – Implementation ATA – 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.
2023–26–07
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section; 7250, Turbine Section.
APPLICABILITY
This AD applies to General Electric Company (GE) Model GE90–90B and GE90–94B engines with interstage HPT seals listed in Table 1 to Paragraph (c) of this AD and GE90–110B1 and GE90–115B engines with an installed high-pressure turbine (HPT) stage 1 disk, HPT stage 2 disk, forward HPT rotor seal, or stages 7–9 compressor rotor spool part number (P/N) and serial number (S/N) identified in Table 1 to Paragraph (c) of this AD, or identified in Paragraph 4. APPENDIX—A, Tables 1, 2, or 3, of GE GE90–100 Service Bulletin (SB) 72–0914, dated January 25, 2023 (GE90–100 SB 72–0914).
ISSUED BY
FAA
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. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024–01–06 | Air Transport Association (ATA) of America Code 53, Fuselage. | This AD applies to The Boeing Company Model 737–600, 737–700, and 737–800 series airplanes, certificated in any category, as identifiedin Boeing Alert Service Bulletin 737–53A1217, Revision 1, dated September 8, 2022. |
FAA
|
| 2024-0031 [Correction: 01 February 2024] | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment | 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 and A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0031 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment | 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 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
|
| 2024-0030 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 – Certification Maintenance Requirements – Amendment | 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 and A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0029 | ATA 79 – Engine Oil – Lubrication / Scavenge Oil Pumps – Installation Criteria | Trent 7000-72 and Trent 7000-72C engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A330 (NEO) aeroplanes. |
EASA
|
| 2024-0028-E | ATA 64 – Tail Rotor – Tail Rotor Blades – Inspection | EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 P3, EC635 T1, EC635 T2+ and EC635 T3 helicopters, all variants, all serial numbers (s/n). |
EASA
|
| 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 – Implementation ATA – 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
|
| 2023–26–07 | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section; 7250, Turbine Section. | This AD applies to General Electric Company (GE) Model GE90–90B and GE90–94B engines with interstage HPT seals listed in Table 1 to Paragraph (c) of this AD and GE90–110B1 and GE90–115B engines with an installed high-pressure turbine (HPT) stage 1 disk, HPT stage 2 disk, forward HPT rotor seal, or stages 7–9 compressor rotor spool part number (P/N) and serial number (S/N) identified in Table 1 to Paragraph (c) of this AD, or identified in Paragraph 4. APPENDIX—A, Tables 1, 2, or 3, of GE GE90–100 Service Bulletin (SB) 72–0914, dated January 25, 2023 (GE90–100 SB 72–0914). |
FAA
|
| 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
|
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] |