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 : 1091
AD NO.
2024-15-07
SUBJECT
Air Transport Association (ATA) of America Code 28, Fuel.
APPLICABILITY
This AD applies to The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 777-47A0007 RB, dated November 21, 2023.
ISSUED BY
FAA
AD NO.
2024-15-03
SUBJECT
Air Transport Association (ATA) of America Code 25, Equipment/Furnishings.
APPLICABILITY
This AD applies to all The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, certificated in any category.
ISSUED BY
FAA
AD NO.
2024-0175
SUBJECT
ATA 72 – Engine – Fuel Nozzle – Replacement
APPLICABILITY
LEAP-1A32 engines installed on Airbus S.A.S. A321-251NX aeroplanes having any of the following aeroplane manufacturing serial number (MSN) 11200, 11420, 11473, 11609, 11698, 11791, 11815, 12136, 12314 or MSN 12370.
ISSUED BY
EASA
AD NO.
2020-0104R1-CN
SUBJECT
ATA 35 – CANCELLED: Oxygen – Oxygen Supply Solenoid Valve – Inspection / 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, A320-211, A320-212, A320-214, 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.
ISSUED BY
EASA
AD NO.
2024-0172-E
SUBJECT
ATA 72 – Engine – Piston – Inspection / Replacement
APPLICABILITY
E4 and E4P engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Diamond Aircraft Industries DA 40 NG, DA 42 NG, DA 42 M-NG and DA 62 aeroplanes.
ISSUED BY
EASA
AD NO.
2024-0171
SUBJECT
ATA 55 – Stabilizers – Vertical Stabilizer to Horizontal Stabilizer Junction Fittings – Inspection / Replacement
APPLICABILITY
ATR 42-500 and ATR 72-212A aeroplanes, manufacturer serial numbers (MSN) as listed in the AOM, as defined in this AD.
ISSUED BY
EASA
AD NO.
2024-0167
SUBJECT
ATA 72 – Engine – Intermediate Pressure Compressor Rotor 1 Blades – Inspection
APPLICABILITY
Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes.
ISSUED BY
EASA
AD NO.
2024-16-14
SUBJECT
Air Transport Association (ATA) of America Code 25, Equipment/furnishings.
APPLICABILITY
This AD applies to The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in anycategory, identified in paragraphs (c)(1) and (2) of this AD. (1) Airplanes with a Captain's seat having Ipeco part number P/N 3A380-0007-XX-X or First Officer'sseat having Ipeco P/N 3A380-0008-XX-X. (2) Airplanes that do not have a seat identified in paragraph (c)(1) of this AD.
ISSUED BY
FAA
AD NO.
2024-0165
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 1 / Safe Life Airworthiness Limitation Items – Amendment
APPLICABILITY
Airbus A310-203, A310-204, A310-221, A310-222, A310-203C, A310-304, A310-308, A310-322, A310-324 and A310-325 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-16-01
SUBJECT
Joint Aircraft System Component (JASC) Code: 5300, Fuselage structure.
APPLICABILITY
This AD applies to Bell Textron Inc. (type certificate previously held by Bell Helicopter Textron, Inc.),Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP helicopters, certificated in any category,identified in paragraphs (c)(1) and (2) of this AD. (1) Model 205A, 205A-1, and 205B helicopters, with an upper left-hand cap angle (cap angle) partnumber (P/N) 205-030-207-005 installed. (2) Model 212, 412, 412CF, and 412EP helicopters, with a cap angle P/N 212-030-191-001 installed.
ISSUED BY
FAA
AD NO.
2024-13-05
SUBJECT
Air Transport Association (ATA) of America Code 54, Nacelles/pylons.
APPLICABILITY
This AD applies to all The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated inany category.
ISSUED BY
FAA
AD NO.
2024-0163
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items – Amendment
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-15-07 | Air Transport Association (ATA) of America Code 28, Fuel. | This AD applies to The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 777-47A0007 RB, dated November 21, 2023. |
FAA
|
| 2024-15-03 | Air Transport Association (ATA) of America Code 25, Equipment/Furnishings. | This AD applies to all The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series airplanes, certificated in any category. |
FAA
|
| 2024-0175 | ATA 72 – Engine – Fuel Nozzle – Replacement | LEAP-1A32 engines installed on Airbus S.A.S. A321-251NX aeroplanes having any of the following aeroplane manufacturing serial number (MSN) 11200, 11420, 11473, 11609, 11698, 11791, 11815, 12136, 12314 or MSN 12370. |
EASA
|
| 2020-0104R1-CN | ATA 35 – CANCELLED: Oxygen – Oxygen Supply Solenoid Valve – Inspection / 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, A320-211, A320-212, A320-214, 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. |
EASA
|
| 2024-0172-E | ATA 72 – Engine – Piston – Inspection / Replacement | E4 and E4P engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Diamond Aircraft Industries DA 40 NG, DA 42 NG, DA 42 M-NG and DA 62 aeroplanes. |
EASA
|
| 2024-0171 | ATA 55 – Stabilizers – Vertical Stabilizer to Horizontal Stabilizer Junction Fittings – Inspection / Replacement | ATR 42-500 and ATR 72-212A aeroplanes, manufacturer serial numbers (MSN) as listed in the AOM, as defined in this AD. |
EASA
|
| 2024-0167 | ATA 72 – Engine – Intermediate Pressure Compressor Rotor 1 Blades – Inspection | Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes. |
EASA
|
| 2024-16-14 | Air Transport Association (ATA) of America Code 25, Equipment/furnishings. | This AD applies to The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in anycategory, identified in paragraphs (c)(1) and (2) of this AD. (1) Airplanes with a Captain's seat having Ipeco part number P/N 3A380-0007-XX-X or First Officer'sseat having Ipeco P/N 3A380-0008-XX-X. (2) Airplanes that do not have a seat identified in paragraph (c)(1) of this AD. |
FAA
|
| 2024-0165 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 1 / Safe Life Airworthiness Limitation Items – Amendment | Airbus A310-203, A310-204, A310-221, A310-222, A310-203C, A310-304, A310-308, A310-322, A310-324 and A310-325 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-16-01 | Joint Aircraft System Component (JASC) Code: 5300, Fuselage structure. | This AD applies to Bell Textron Inc. (type certificate previously held by Bell Helicopter Textron, Inc.),Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP helicopters, certificated in any category,identified in paragraphs (c)(1) and (2) of this AD. (1) Model 205A, 205A-1, and 205B helicopters, with an upper left-hand cap angle (cap angle) partnumber (P/N) 205-030-207-005 installed. (2) Model 212, 412, 412CF, and 412EP helicopters, with a cap angle P/N 212-030-191-001 installed. |
FAA
|
| 2024-13-05 | Air Transport Association (ATA) of America Code 54, Nacelles/pylons. | This AD applies to all The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated inany category. |
FAA
|
| 2024-0163 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 1, Safe Life Airworthiness Limitations Items – Amendment | Airbus A380-841, A380-842 and A380-861 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] |