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 : 252
AD NO.
2024-0087 [Correction: 14 May 2024]
SUBJECT
ATA 57 – Wings – Metallic Wing Rib Feet – Inspection
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 00003 to 00092 inclusive, 00097 to 00099 inclusive, and 00101 to 00109 inclusive.
ISSUED BY
EASA
AD NO.
2024-0090
SUBJECT
ATA 52 – Doors – Cockpit Emergency Escape Hatch Drain Hose – Inspection
APPLICABILITY
ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, and ATR 72-212A aeroplanes, manufacturer serial numbers as listed in the Appendix 1 of the AOM, as defined in this AD.
ISSUED BY
EASA
AD NO.
2024-0060R1
SUBJECT
ATA 54 – Nacelles / Pylons – Air Intake Cowl – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0058R1
SUBJECT
ATA 36 – Pneumatic – Precooler Exchanger – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0087
SUBJECT
ATA 57 – Wings – Metallic Wing Rib Feet – Inspection
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 00003 to 00092 inclusive, 00097 to 00099 inclusive, and 00101 to 00109 inclusive.
ISSUED BY
EASA
AD NO.
2024-0028R1
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.
2024-0089
SUBJECT
ATA 53 – Fuselage – Main Landing Gear Bay Rear Panel – Inspections
APPLICABILITY
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers, except those having any of the following configurations: A319 aeroplanes on which Airbus modification (mod) 160001 was embodied in production; A319 aeroplanes on which Airbus Service Bulletin (SB) A320-57-1193 was embodied in service; A319 aeroplanes on which Airbus mod 28162, mod 28238 and mod 28342 were embodied in production; A320 aeroplanes on which Airbus mod 160001 was embodied in production; A320 aeroplanes on which Airbus SB A320-57-1193 was embodied in service; A321 aeroplanes on which Airbus mod 160021 was embodied in production.
ISSUED BY
EASA
AD NO.
2024-0088
SUBJECT
ATA 11 – Placards and Markings– Rear Facing Seat(s) – Placard Installation
APPLICABILITY
AB139 and AW139 helicopters, serial numbers 31087, 31133, 31269, 31305, 31351, 31502, 31712, 31735, 31757, 31865, 31869, 41582 and 41583, if modified in accordance with EASA STC 10030095 original issue and subsequent revisions or STC 10017198 original issue and subsequent revisions.
ISSUED BY
EASA
AD NO.
2024-08-02
SUBJECT
Air Transport Association (ATA) of America Code 24, Electrical power.
APPLICABILITY
This AD applies to the ATR—GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0181, dated October 13, 2023 (EASA AD 2023-0181). (1) Model ATR42-200, -300, -320, and -500 airplanes. (2) Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes
ISSUED BY
EASA
AD NO.
2022-0096R2
SUBJECT
ATA – Aircraft Flight Manual / Section Limitations – Amendment ATA 22 – Auto Flight – New flight Guidance Standard – Modification
APPLICABILITY
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-151N, A319-153N, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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.
2024-0084-E
SUBJECT
ATA 32 – Main Landing Gear – Main Landing Gear Shock Absorber – Inspection
APPLICABILITY
AB139 and AW139 helicopters, all serial numbers.
ISSUED BY
EASA
AD NO.
2024-0081
SUBJECT
ATA 27 – Flight Controls – Rudder Travel Limiting Unit – Inspection
APPLICABILITY
ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); and ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-0087 [Correction: 14 May 2024] | ATA 57 – Wings – Metallic Wing Rib Feet – Inspection | Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 00003 to 00092 inclusive, 00097 to 00099 inclusive, and 00101 to 00109 inclusive. |
EASA
|
| 2024-0090 | ATA 52 – Doors – Cockpit Emergency Escape Hatch Drain Hose – Inspection | ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, and ATR 72-212A aeroplanes, manufacturer serial numbers as listed in the Appendix 1 of the AOM, as defined in this AD. |
EASA
|
| 2024-0060R1 | ATA 54 – Nacelles / Pylons – Air Intake Cowl – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0058R1 | ATA 36 – Pneumatic – Precooler Exchanger – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0087 | ATA 57 – Wings – Metallic Wing Rib Feet – Inspection | Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 00003 to 00092 inclusive, 00097 to 00099 inclusive, and 00101 to 00109 inclusive. |
EASA
|
| 2024-0028R1 | 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
|
| 2024-0089 | ATA 53 – Fuselage – Main Landing Gear Bay Rear Panel – Inspections | Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers, except those having any of the following configurations: A319 aeroplanes on which Airbus modification (mod) 160001 was embodied in production; A319 aeroplanes on which Airbus Service Bulletin (SB) A320-57-1193 was embodied in service; A319 aeroplanes on which Airbus mod 28162, mod 28238 and mod 28342 were embodied in production; A320 aeroplanes on which Airbus mod 160001 was embodied in production; A320 aeroplanes on which Airbus SB A320-57-1193 was embodied in service; A321 aeroplanes on which Airbus mod 160021 was embodied in production. |
EASA
|
| 2024-0088 | ATA 11 – Placards and Markings– Rear Facing Seat(s) – Placard Installation | AB139 and AW139 helicopters, serial numbers 31087, 31133, 31269, 31305, 31351, 31502, 31712, 31735, 31757, 31865, 31869, 41582 and 41583, if modified in accordance with EASA STC 10030095 original issue and subsequent revisions or STC 10017198 original issue and subsequent revisions. |
EASA
|
| 2024-08-02 | Air Transport Association (ATA) of America Code 24, Electrical power. | This AD applies to the ATR—GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0181, dated October 13, 2023 (EASA AD 2023-0181). (1) Model ATR42-200, -300, -320, and -500 airplanes. (2) Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes |
EASA
|
| 2022-0096R2 | ATA – Aircraft Flight Manual / Section Limitations – Amendment ATA 22 – Auto Flight – New flight Guidance Standard – Modification | Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-151N, A319-153N, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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
|
| 2024-0084-E | ATA 32 – Main Landing Gear – Main Landing Gear Shock Absorber – Inspection | AB139 and AW139 helicopters, all serial numbers. |
EASA
|
| 2024-0081 | ATA 27 – Flight Controls – Rudder Travel Limiting Unit – Inspection | ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); and ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN. |
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] |