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.
2025-0080 [Correction: 23 April 2025]
SUBJECT
ATA 26 – Fire Protection – Aft Cargo Compartment Fire Extinguisher Distribution Piping – Functional Check
APPLICABILITY
ATR 42-300, ATR 42-320 and ATR 72-201 all manufacturer serial numbers (MSN) to which ATR modification (MOD) 00639 has been applied; and ATR 42-400, ATR 42-500 aeroplanes, all MSN, except MSN 1617 and subsequent; and ATR72-102, ATR 72-202, ATR 72-211, ATR 72-212 aeroplanes, all MSN; and ATR 72-212A aeroplanes, to which ATR MOD 07900 has not been applied, except MSN 1627, 1677, 1678, 1703 to 1716 inclusive, 1718 to 1721 inclusive, 1723 to 1726 inclusive, 1728 and subsequent.
ISSUED BY
EASA
AD NO.
2025-0088
SUBJECT
ATA 34 – Navigation – Satellite Based Augmentation Systems / Global Positioning System Receiver – Replacement
APPLICABILITY
Rockwell Collins GPS-4000S, GLU-2100, GLUS-2100 and GLUS-2100A receivers, having a Part Number (P/N) as listed in Appendix 1 of this AD, all serial numbers. These receivers may be installed on, but not limited to, aeroplanes listed in Appendix 2 of this AD.
ISSUED BY
EASA
AD NO.
2025-07-10
SUBJECT
Joint Aircraft System Component (JASC) Code 7320, Fuel Controlling System.
APPLICABILITY
This AD applies to General Electric Company (GE) Model GE90-110B1 and GE90-115B engines.
ISSUED BY
FAA
AD NO.
2017-0098R1
SUBJECT
ATA 53 – Fuselage – Potable Water and Wastewater Service Panels – Reinforcement
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 on which Airbus modification (mod) 160055 or mod 160056 has been embodied in production, and except A319 aeroplanes on which mod 28162, 28238 and 28342 have been embodied (“Corporate Jet”).
ISSUED BY
EASA
AD NO.
2025-0083
SUBJECT
ATA 25 – Equipment/Furnishings – Cargo Bulkhead Frame 24A Vertical Members – 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, A319-173N, 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, A321-253NY, A321-271N, A321-271NX, A321-271NY, A321-272N, and A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
G-2025-0001R1-E
SUBJECT
Hot Air Balloons – Cylinders fitted with PRV adaptor CB8426– Inspect for Cracking
APPLICABILITY
Cylinders fitted with PRV adaptor CB8426 including, but not limited to the below cylinder models: Thunder & Colt: V20-100-00/CB8420, 830922-1, V30-100-00/CB8430, V40-100-00/CB8440 Sky: A0/V30, A0/V40 Lindstrand: V20/CY-020-A-001, V30/CY-030-A-001, V40/CY-040-A-001, T30/CY-050-A-001
ISSUED BY
UK CAA
AD NO.
2025-0082
SUBJECT
ATA 72 – Engine – Intermediate Pressure Compressor Rotor 1 Blades – Inspection / Modification
APPLICABILITY
Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers, except those having embodied Rolls-Royce modification (MOD) 72-AL099. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes.
ISSUED BY
EASA
AD NO.
2025-0080
SUBJECT
ATA 26 – Fire Protection – Aft Cargo Compartment Fire Extinguisher Distribution Piping – Functional Check
APPLICABILITY
ATR 42-300, ATR 42-320 and ATR 72-201 all manufacturer serial numbers (MSN) to which ATR modification (MOD) 00639 has been applied; and ATR 42-400, ATR 42-500 aeroplanes, all MSN, except MSN 1617 and subsequent; and ATR72-102, ATR 72-202, ATR 72-211, ATR 72-212 aeroplanes, all MSN; and ATR 72-212A aeroplanes, to which ATR MOD 07900 has not been applied, except MSN 1627, 1677, 1678, 1703 to 1716 inclusive, 1718 to 1721 inclusive, 1723 to 1726 inclusive, 1728 and subsequent.
ISSUED BY
EASA
AD NO.
2025-0079
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment
APPLICABILITY
ARRIEL 2D, 2E, 2H, 2L2 and 2N engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale) AS 350 B3 (H125) and EC 130 T2 (H130) helicopters; Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 (EC 145 T2 or H145) helicopters; Korea Aerospace Industries LAH and LCH helicopters; and AVIC Aircraft Industry Group AC312E helicopters.
ISSUED BY
EASA
AD NO.
2025-0078
SUBJECT
ATA 53 – Fuselage – Centre Fuselage Skin and Forward Pressure Bulkhead – Inspection
APPLICABILITY
Airbus A318-111, A318-112 and A318-122 aeroplanes, all manufacturer serial numbers (MSN); and 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, A320-232, 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 MSN up to MSN 09287 inclusive, on which Airbus modification (mod) 157159 is embodied in production; except aeroplanes in any of the following configuration: – Airbus A318 aeroplanes on which Airbus mod 39195 was embodied in production or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; – Airbus A319 CEO aeroplanes, on which Airbus mod 28162 and mod 28238 and mod 28342 were embodied in production; – Airbus A320 NEO aeroplanes on which Airbus mod 162339 was embodied in production.
ISSUED BY
EASA
AD NO.
2025-07-05
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
This AD applies to Airbus SAS Model A350-941 and -1041 airplanes, certificated in any category, asidentified in European Union Aviation Safety Agency (EASA) AD 2024-0129, dated July 5, 2024(EASA AD 2024-0129).
ISSUED BY
FAA
AD NO.
2025-07-03
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
(1) This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ERseries airplanes, certificated in any category. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability toaccomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE isinstalled, a “change in product” alternative method of compliance (AMOC) approval request is notnecessary to comply with the requirements of 14 CFR 39.17.
ISSUED BY
FAA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2025-0080 [Correction: 23 April 2025] | ATA 26 – Fire Protection – Aft Cargo Compartment Fire Extinguisher Distribution Piping – Functional Check | ATR 42-300, ATR 42-320 and ATR 72-201 all manufacturer serial numbers (MSN) to which ATR modification (MOD) 00639 has been applied; and ATR 42-400, ATR 42-500 aeroplanes, all MSN, except MSN 1617 and subsequent; and ATR72-102, ATR 72-202, ATR 72-211, ATR 72-212 aeroplanes, all MSN; and ATR 72-212A aeroplanes, to which ATR MOD 07900 has not been applied, except MSN 1627, 1677, 1678, 1703 to 1716 inclusive, 1718 to 1721 inclusive, 1723 to 1726 inclusive, 1728 and subsequent. |
EASA
|
| 2025-0088 | ATA 34 – Navigation – Satellite Based Augmentation Systems / Global Positioning System Receiver – Replacement | Rockwell Collins GPS-4000S, GLU-2100, GLUS-2100 and GLUS-2100A receivers, having a Part Number (P/N) as listed in Appendix 1 of this AD, all serial numbers. These receivers may be installed on, but not limited to, aeroplanes listed in Appendix 2 of this AD. |
EASA
|
| 2025-07-10 | Joint Aircraft System Component (JASC) Code 7320, Fuel Controlling System. | This AD applies to General Electric Company (GE) Model GE90-110B1 and GE90-115B engines. |
FAA
|
| 2017-0098R1 | ATA 53 – Fuselage – Potable Water and Wastewater Service Panels – Reinforcement | 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 on which Airbus modification (mod) 160055 or mod 160056 has been embodied in production, and except A319 aeroplanes on which mod 28162, 28238 and 28342 have been embodied (“Corporate Jet”). |
EASA
|
| 2025-0083 | ATA 25 – Equipment/Furnishings – Cargo Bulkhead Frame 24A Vertical Members – 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, A319-173N, 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, A321-253NY, A321-271N, A321-271NX, A321-271NY, A321-272N, and A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| G-2025-0001R1-E | Hot Air Balloons – Cylinders fitted with PRV adaptor CB8426– Inspect for Cracking | Cylinders fitted with PRV adaptor CB8426 including, but not limited to the below cylinder models: Thunder & Colt: V20-100-00/CB8420, 830922-1, V30-100-00/CB8430, V40-100-00/CB8440 Sky: A0/V30, A0/V40 Lindstrand: V20/CY-020-A-001, V30/CY-030-A-001, V40/CY-040-A-001, T30/CY-050-A-001 |
UK CAA
|
| 2025-0082 | ATA 72 – Engine – Intermediate Pressure Compressor Rotor 1 Blades – Inspection / Modification | Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers, except those having embodied Rolls-Royce modification (MOD) 72-AL099. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes. |
EASA
|
| 2025-0080 | ATA 26 – Fire Protection – Aft Cargo Compartment Fire Extinguisher Distribution Piping – Functional Check | ATR 42-300, ATR 42-320 and ATR 72-201 all manufacturer serial numbers (MSN) to which ATR modification (MOD) 00639 has been applied; and ATR 42-400, ATR 42-500 aeroplanes, all MSN, except MSN 1617 and subsequent; and ATR72-102, ATR 72-202, ATR 72-211, ATR 72-212 aeroplanes, all MSN; and ATR 72-212A aeroplanes, to which ATR MOD 07900 has not been applied, except MSN 1627, 1677, 1678, 1703 to 1716 inclusive, 1718 to 1721 inclusive, 1723 to 1726 inclusive, 1728 and subsequent. |
EASA
|
| 2025-0079 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment | ARRIEL 2D, 2E, 2H, 2L2 and 2N engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale) AS 350 B3 (H125) and EC 130 T2 (H130) helicopters; Airbus Helicopters Deutschland GmbH MBB-BK117 D-2 (EC 145 T2 or H145) helicopters; Korea Aerospace Industries LAH and LCH helicopters; and AVIC Aircraft Industry Group AC312E helicopters. |
EASA
|
| 2025-0078 | ATA 53 – Fuselage – Centre Fuselage Skin and Forward Pressure Bulkhead – Inspection | Airbus A318-111, A318-112 and A318-122 aeroplanes, all manufacturer serial numbers (MSN); and 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, A320-232, 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 MSN up to MSN 09287 inclusive, on which Airbus modification (mod) 157159 is embodied in production; except aeroplanes in any of the following configuration: – Airbus A318 aeroplanes on which Airbus mod 39195 was embodied in production or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; – Airbus A319 CEO aeroplanes, on which Airbus mod 28162 and mod 28238 and mod 28342 were embodied in production; – Airbus A320 NEO aeroplanes on which Airbus mod 162339 was embodied in production. |
EASA
|
| 2025-07-05 | Air Transport Association (ATA) of America Code 53, Fuselage. | This AD applies to Airbus SAS Model A350-941 and -1041 airplanes, certificated in any category, asidentified in European Union Aviation Safety Agency (EASA) AD 2024-0129, dated July 5, 2024(EASA AD 2024-0129). |
FAA
|
| 2025-07-03 | Air Transport Association (ATA) of America Code 53, Fuselage. | (1) This AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ERseries airplanes, certificated in any category. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability toaccomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE isinstalled, a “change in product” alternative method of compliance (AMOC) approval request is notnecessary to comply with the requirements of 14 CFR 39.17. |
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] |