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.
2024-07-06
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section.
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1,LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32,LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines with an installed No. 3 bearing spring fingerhousing having part number (P/N) 2629M62G01 and a serial number identified in Table 1 or Table 2of CFM Service Bulletin (SB) LEAP-1A-72-00-0504-01A-930A-D, Issue 002, dated October 17, 2023(CFM SB LEAP-1A-72-00-0504-01A-930A-D, Issue 002).
ISSUED BY
FAA
AD NO.
2024-0070
SUBJECT
ATA 79 – Oil – Front Bearing Housing Oil Feed Tube Assembly – Replacement
APPLICABILITY
Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes.
ISSUED BY
EASA
AD NO.
2024-05-05
SUBJECT
Air Transport Association (ATA) of America Code 26, Fire Protection.
APPLICABILITY
This AD applies to all ATR—GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Model ATR42-200, -300, -320, and -500 airplanes. (2) Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes.
ISSUED BY
FAA
AD NO.
2024-07-02
SUBJECT
Joint Aircraft System Component (JASC) Code 7250, Turbine Section.
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines
ISSUED BY
FAA
AD NO.
2024-0079
SUBJECT
ATA 32 – Landing Gear – Body Landing Gear Rear Axle – Replacement
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2024-0079 [Correction: 04 April 2024]
SUBJECT
ATA 32 – Landing Gear – Body Landing Gear Rear Axle – Replacement
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2024-06-15
SUBJECT
Joint Aircraft System Component (JASC) Code 7250, Turbine Section.
APPLICABILITY
This AD applies to General Electric Company (GE) Model GE90-110B1 and GE90-115B engines with aninstalled interstage high-pressure turbine (HPT) rotor seal having a part number and serial numberlisted in Table 1 or Table 2 of GE GE90-100 Service Bulletin (SB) 72-A0908 R00, dated July 7, 2023(GE SB 72-A0908).
ISSUED BY
FAA
AD NO.
2024-06-13
SUBJECT
Joint Aircraft System Component (JASC) Code 2700, Flight Control System.
APPLICABILITY
This AD applies to Diamond Aircraft Industries GmbH (DAI) Model DA 42, DA 42 NG, and DA 42 M-NG airplanes, all serianumbers, certificated in any category.
ISSUED BY
EASA
AD NO.
2023-0132R1
SUBJECT
ATA 57 – Wings – Inboard Flap Trunnion – Inspection / Modification
APPLICABILITY
Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0005 through 0046 inclusive, except MSN 0025 and MSN 0033.
ISSUED BY
EASA
AD NO.
2024-0078
SUBJECT
ATA 25 – Equipment / Furnishings – AFT Galley Complex Lower Attachment Studs – Inspection / Replacement
APPLICABILITY
Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0044, 0049, 0050, 0052, 0055-0057 inclusive, 0060, 0066, 0067, 0073, 0074, 0080, 0082, 0086, 0087, 0091, 0092, 0094, 0095, 0098, 0105, 0111, 0112, 0115, 0117, 0121, 0123, 0124, 0127, 0129, 0130, 0132, 0135, 0136, 0138, 0142, 0143-0146 inclusive, 0149-0151 inclusive, 0153, 0157, 0159, 0160, 0162-0165 inclusive, 0167, 0168, 0172-0179 inclusive, 0181-0185 inclusive, 0187, 0189-0193 inclusive, 0195, 0197-0199 inclusive, 0201-0204 inclusive, 0207-0214 inclusive, 0217, 0218, 0221, 0224, 0228, 0231, 0234-0237 inclusive, 0239, 0240, 0243, 0246, 0247, 0249, 0251, 0255, 0256, 0257, 0260, 0267, 0268, 0270, 0277, 0279, 0280, 0281, 0283-0285 inclusive, 0287, 0292, 0295, 0297 and 0299; and A350-1041 aeroplanes MSN 0065, 0071, 0088, 0102, 0110, 0118, 0125, 0141, 0161, 0169, 0188, 0206, 0215, 0225, 0229, 0233, 0241, 0252, 0258, 0262, 0266, 0274, 0286, 0290, 0296 and 0298.
ISSUED BY
EASA
AD NO.
2024-0077
SUBJECT
ATA 53 – Fuselage – Pressure Panel Longitudinal Beams – Inspection / Repair / Modification
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, A320-215, 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 (MSN), except those having Airbus modification (mod) 151574 embodied in production.
ISSUED BY
EASA
AD NO.
2024-0077 [Correction: 25April2024]
SUBJECT
ATA 53 – Fuselage – Pressure Panel Longitudinal Beams – Inspection / Repair / Modification
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, A320-215, 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 (MSN), except those having Airbus modification (mod) 151574 embodied in production.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-07-06 | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section. | This AD applies to CFM International, S.A. (CFM) Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1,LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32,LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines with an installed No. 3 bearing spring fingerhousing having part number (P/N) 2629M62G01 and a serial number identified in Table 1 or Table 2of CFM Service Bulletin (SB) LEAP-1A-72-00-0504-01A-930A-D, Issue 002, dated October 17, 2023(CFM SB LEAP-1A-72-00-0504-01A-930A-D, Issue 002). |
FAA
|
| 2024-0070 | ATA 79 – Oil – Front Bearing Housing Oil Feed Tube Assembly – Replacement | Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes. |
EASA
|
| 2024-05-05 | Air Transport Association (ATA) of America Code 26, Fire Protection. | This AD applies to all ATR—GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Model ATR42-200, -300, -320, and -500 airplanes. (2) Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes. |
FAA
|
| 2024-07-02 | Joint Aircraft System Component (JASC) Code 7250, Turbine Section. | This AD applies to CFM International, S.A. (CFM) Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines |
FAA
|
| 2024-0079 | ATA 32 – Landing Gear – Body Landing Gear Rear Axle – Replacement | Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2024-0079 [Correction: 04 April 2024] | ATA 32 – Landing Gear – Body Landing Gear Rear Axle – Replacement | Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2024-06-15 | Joint Aircraft System Component (JASC) Code 7250, Turbine Section. | This AD applies to General Electric Company (GE) Model GE90-110B1 and GE90-115B engines with aninstalled interstage high-pressure turbine (HPT) rotor seal having a part number and serial numberlisted in Table 1 or Table 2 of GE GE90-100 Service Bulletin (SB) 72-A0908 R00, dated July 7, 2023(GE SB 72-A0908). |
FAA
|
| 2024-06-13 | Joint Aircraft System Component (JASC) Code 2700, Flight Control System. | This AD applies to Diamond Aircraft Industries GmbH (DAI) Model DA 42, DA 42 NG, and DA 42 M-NG airplanes, all serianumbers, certificated in any category. |
EASA
|
| 2023-0132R1 | ATA 57 – Wings – Inboard Flap Trunnion – Inspection / Modification | Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0005 through 0046 inclusive, except MSN 0025 and MSN 0033. |
EASA
|
| 2024-0078 | ATA 25 – Equipment / Furnishings – AFT Galley Complex Lower Attachment Studs – Inspection / Replacement | Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0044, 0049, 0050, 0052, 0055-0057 inclusive, 0060, 0066, 0067, 0073, 0074, 0080, 0082, 0086, 0087, 0091, 0092, 0094, 0095, 0098, 0105, 0111, 0112, 0115, 0117, 0121, 0123, 0124, 0127, 0129, 0130, 0132, 0135, 0136, 0138, 0142, 0143-0146 inclusive, 0149-0151 inclusive, 0153, 0157, 0159, 0160, 0162-0165 inclusive, 0167, 0168, 0172-0179 inclusive, 0181-0185 inclusive, 0187, 0189-0193 inclusive, 0195, 0197-0199 inclusive, 0201-0204 inclusive, 0207-0214 inclusive, 0217, 0218, 0221, 0224, 0228, 0231, 0234-0237 inclusive, 0239, 0240, 0243, 0246, 0247, 0249, 0251, 0255, 0256, 0257, 0260, 0267, 0268, 0270, 0277, 0279, 0280, 0281, 0283-0285 inclusive, 0287, 0292, 0295, 0297 and 0299; and A350-1041 aeroplanes MSN 0065, 0071, 0088, 0102, 0110, 0118, 0125, 0141, 0161, 0169, 0188, 0206, 0215, 0225, 0229, 0233, 0241, 0252, 0258, 0262, 0266, 0274, 0286, 0290, 0296 and 0298. |
EASA
|
| 2024-0077 | ATA 53 – Fuselage – Pressure Panel Longitudinal Beams – Inspection / Repair / Modification | 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, A320-215, 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 (MSN), except those having Airbus modification (mod) 151574 embodied in production. |
EASA
|
| 2024-0077 [Correction: 25April2024] | ATA 53 – Fuselage – Pressure Panel Longitudinal Beams – Inspection / Repair / Modification | 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, A320-215, 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 (MSN), except those having Airbus modification (mod) 151574 embodied in production. |
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] |