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.
2024-08-02
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
FAA
AD NO.
2024-0097
SUBJECT
ATA 53 – Fuselage – Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings – Inspection
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, A321-272NX aeroplanes, all manufacturer serial numbers, except those aeroplanes on which Airbus modification (mod) 165315 has been embodied in production.
ISSUED BY
EASA
AD NO.
2024-0098
SUBJECT
ATA 53 – Fuselage – Forward Cargo Door Piano Hinges – Inspection
APPLICABILITY
Airbus A350-941 aeroplanes manufacturer serial numbers (MSN) 0001 through 0645 (inclusive), except aeroplanes having Airbus modification (mod) 113979 embodied in production; and A350-1041 aeroplanes, MSN 00059 through 00584 inclusive.
ISSUED BY
EASA
AD NO.
2024-0096
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, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN
ISSUED BY
EASA
AD NO.
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.
2024-06-15
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.
2023-0013R1
SUBJECT
ATA 27 – Flight Controls – Rudder Steering Bracket – Inspections / Modification
APPLICABILITY
DA 42, DA 42 M, DA 42 NG and DA 42 M-NG aeroplanes (including those certified in the Restricted category), all manufacturer serial numbers (MSN).
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.
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 serial numbers, certificated in any category.
ISSUED BY
FAA
AD NO.
2024-0093
SUBJECT
ATA 72 – Engine – Non-Synchronous Vibration During Engine Operation – Monitoring
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 and 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.
2023-0136R1
SUBJECT
ATA 36 – Pneumatic – Overheat Detection System Sensing Elements – Inspection
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 A330-743L aeroplanes, all manufacturer serial numbers (MSN); and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.
ISSUED BY
EASA
AD NO.
2024-06-03
SUBJECT
Air Transport Association (ATA) of America Code 24, Electrical Power.
APPLICABILITY
This AD applies to The Boeing Company Model 737-8 and 737-9 airplanes, certificated in any category,as identified in Boeing Alert Requirements Bulletin 737-24A1248 RB, dated May 16, 2022.
ISSUED BY
FAA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 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 |
FAA
|
| 2024-0097 | ATA 53 – Fuselage – Centre Fuselage / Main Landing Gear Door Keel Beam Hinge and Actuator Fittings – Inspection | 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, A321-272NX aeroplanes, all manufacturer serial numbers, except those aeroplanes on which Airbus modification (mod) 165315 has been embodied in production. |
EASA
|
| 2024-0098 | ATA 53 – Fuselage – Forward Cargo Door Piano Hinges – Inspection | Airbus A350-941 aeroplanes manufacturer serial numbers (MSN) 0001 through 0645 (inclusive), except aeroplanes having Airbus modification (mod) 113979 embodied in production; and A350-1041 aeroplanes, MSN 00059 through 00584 inclusive. |
EASA
|
| 2024-0096 | 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, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN |
EASA
|
| 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
|
| 2024-06-15 | 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
|
| 2023-0013R1 | ATA 27 – Flight Controls – Rudder Steering Bracket – Inspections / Modification | DA 42, DA 42 M, DA 42 NG and DA 42 M-NG aeroplanes (including those certified in the Restricted category), all manufacturer serial numbers (MSN). |
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
|
| 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 serial numbers, certificated in any category. |
FAA
|
| 2024-0093 | ATA 72 – Engine – Non-Synchronous Vibration During Engine Operation – Monitoring | 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, 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
|
| 2023-0136R1 | ATA 36 – Pneumatic – Overheat Detection System Sensing Elements – Inspection | 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 A330-743L aeroplanes, all manufacturer serial numbers (MSN); and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN. |
EASA
|
| 2024-06-03 | Air Transport Association (ATA) of America Code 24, Electrical Power. | This AD applies to The Boeing Company Model 737-8 and 737-9 airplanes, certificated in any category,as identified in Boeing Alert Requirements Bulletin 737-24A1248 RB, dated May 16, 2022. |
FAA
|
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] |