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.
2025-19-13
SUBJECT
Joint Aircraft System Component (JASC) Code 7250, Turbine Section.
APPLICABILITY
This AD applies to International Aero Engines AG (IAE AG) Model V2522-A5, V2524-A5, V2525-D5,V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines
ISSUED BY
FAA
AD NO.
2025-0212
SUBJECT
ATA 57 – Wings – Wing Rear Spars – Inspection
APPLICABILITY
A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 194, 204, 205, 206, 215, 232, 236, 239, 248, 249, 256, 257, 258, 259, 260, 261, 262, 263, 264, 266, 267, 268 and 269.
ISSUED BY
EASA
AD NO.
2025-0210
SUBJECT
ATA 57 – Wings – Centre Wing Box Fasteners – Replacement
APPLICABILITY
Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0005 to 0058 inclusive, 0060 to 0064 inclusive, 0066 to 0070 inclusive, 0072 to 0087 inclusive, 0089 to 0101 inclusive, 0103 to 0107 inclusive, 0109, 0111 to 0117 inclusive and MSN 0119 to 0121 inclusive.
ISSUED BY
EASA
AD NO.
2025-0209
SUBJECT
ATA 57 – Wings – Centre Wing Box and Belly Fairing Fasteners – Modification
APPLICABILITY
Airbus A350-941 aeroplanes, manufacturer serial numbers 0005 through 0047 (inclusive).
ISSUED BY
EASA
AD NO.
2025-0208
SUBJECT
ATA 27 – Flight Controls – Flight Control Primary Computer – Modification
APPLICABILITY
Airbus A330-941 aeroplanes manufacturer serial numbers (MSN) 1819, 1836, 1844, 1850, 1861, 1870, 1876, 1884, 1887, 1890, 1892, 1895, 1897, 1900, 1901, 1903, 1904, 1906, 1908, 1909, 1910, 1913, 1914, 1915, 1918, 1920 through 1927 inclusive, 1929, 1931, 1933, 1934, 1935, 1937, 1938, 1939, 1941, 1943, 1946, 1947, 1948, 1949, 1952, 1953, 1954, 1956, 1957, 1958, 1959, 1961, 1962, 1963, 1966, 1967, 1970, 1971, 1972, 1973, 1975, 1976, 1978, 1981, 1983, 1984, 1986, 1987, 1988, 1990 through 1997 inclusive, 1999 through 2004 inclusive, 2006, 2009, 2010, 2013, 2014, 2017, 2018, 2019, 2021, 2024, 2025, 2026, 2028, 2029, 2031 through 2035 inclusive, 2037, 2038, 2039, 2040, 2042, 2044 through 2059 inclusive, 2061 through 2071, 2073 through 2085 inclusive, 2087 and 2088.
ISSUED BY
EASA
AD NO.
2025-0207
SUBJECT
ATA 53 – Fuselage – Seat Rail Connections Nylon Bushes – 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, A320-215, 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) 152721 and mod 154725 embodied in production.
ISSUED BY
EASA
AD NO.
2025-0174R1
SUBJECT
ATA 53 – Fuselage – Rear Structure / Rear Frame – Inspection
APPLICABILITY
EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 T1 and EC635 T2+ helicopters, all variants, all serial numbers (s/n) up to 1276 inclusive, if equipped with mounting ring frame X9227 Part Number (P/N) L535H2120301, P/N L535H2120303 or P/N L535H2120304, except those having the frame reinforcement installed.
ISSUED BY
EASA
AD NO.
2025-0206
SUBJECT
ATA 72 – Engine – High Pressure Turbine Blades – Inspection
APPLICABILITY
Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3 and Trent 1000-R3 engines, all serial numbers. These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes.
ISSUED BY
EASA
AD NO.
2025-0205
SUBJECT
ATA 53 – Fuselage – Passenger Seat Tracks – Inspection / Replacement
APPLICABILITY
ATR 42-200, ATR 42-300, ATR 42-320, 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.
2025-0204
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2025-0203
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 – System Equipment Maintenance Requirements – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2025-18-05
SUBJECT
Air Transport Association (ATA) of America Code 34, Navigation.
APPLICABILITY
This AD applies to The Boeing Company Model 767-300 series airplanes, certificated in any category,that have been modified to a special freighter configuration, in accordance with FAA SupplementalType Certificate (STC) ST02040SE, and which are listed in paragraph I.A., “Effectivity,” of IsraelAerospace Industries Ltd., Service Bulletin 368-34-106, dated August 2024.
ISSUED BY
FAA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2025-19-13 | Joint Aircraft System Component (JASC) Code 7250, Turbine Section. | This AD applies to International Aero Engines AG (IAE AG) Model V2522-A5, V2524-A5, V2525-D5,V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines |
FAA
|
| 2025-0212 | ATA 57 – Wings – Wing Rear Spars – Inspection | A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 194, 204, 205, 206, 215, 232, 236, 239, 248, 249, 256, 257, 258, 259, 260, 261, 262, 263, 264, 266, 267, 268 and 269. |
EASA
|
| 2025-0210 | ATA 57 – Wings – Centre Wing Box Fasteners – Replacement | Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0005 to 0058 inclusive, 0060 to 0064 inclusive, 0066 to 0070 inclusive, 0072 to 0087 inclusive, 0089 to 0101 inclusive, 0103 to 0107 inclusive, 0109, 0111 to 0117 inclusive and MSN 0119 to 0121 inclusive. |
EASA
|
| 2025-0209 | ATA 57 – Wings – Centre Wing Box and Belly Fairing Fasteners – Modification | Airbus A350-941 aeroplanes, manufacturer serial numbers 0005 through 0047 (inclusive). |
EASA
|
| 2025-0208 | ATA 27 – Flight Controls – Flight Control Primary Computer – Modification | Airbus A330-941 aeroplanes manufacturer serial numbers (MSN) 1819, 1836, 1844, 1850, 1861, 1870, 1876, 1884, 1887, 1890, 1892, 1895, 1897, 1900, 1901, 1903, 1904, 1906, 1908, 1909, 1910, 1913, 1914, 1915, 1918, 1920 through 1927 inclusive, 1929, 1931, 1933, 1934, 1935, 1937, 1938, 1939, 1941, 1943, 1946, 1947, 1948, 1949, 1952, 1953, 1954, 1956, 1957, 1958, 1959, 1961, 1962, 1963, 1966, 1967, 1970, 1971, 1972, 1973, 1975, 1976, 1978, 1981, 1983, 1984, 1986, 1987, 1988, 1990 through 1997 inclusive, 1999 through 2004 inclusive, 2006, 2009, 2010, 2013, 2014, 2017, 2018, 2019, 2021, 2024, 2025, 2026, 2028, 2029, 2031 through 2035 inclusive, 2037, 2038, 2039, 2040, 2042, 2044 through 2059 inclusive, 2061 through 2071, 2073 through 2085 inclusive, 2087 and 2088. |
EASA
|
| 2025-0207 | ATA 53 – Fuselage – Seat Rail Connections Nylon Bushes – 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, A320-215, 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) 152721 and mod 154725 embodied in production. |
EASA
|
| 2025-0174R1 | ATA 53 – Fuselage – Rear Structure / Rear Frame – Inspection | EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 T1 and EC635 T2+ helicopters, all variants, all serial numbers (s/n) up to 1276 inclusive, if equipped with mounting ring frame X9227 Part Number (P/N) L535H2120301, P/N L535H2120303 or P/N L535H2120304, except those having the frame reinforcement installed. |
EASA
|
| 2025-0206 | ATA 72 – Engine – High Pressure Turbine Blades – Inspection | Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3 and Trent 1000-R3 engines, all serial numbers. These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes. |
EASA
|
| 2025-0205 | ATA 53 – Fuselage – Passenger Seat Tracks – Inspection / Replacement | ATR 42-200, ATR 42-300, ATR 42-320, 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
|
| 2025-0204 | ATA 05 – Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2025-0203 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 – System Equipment Maintenance Requirements – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2025-18-05 | Air Transport Association (ATA) of America Code 34, Navigation. | This AD applies to The Boeing Company Model 767-300 series airplanes, certificated in any category,that have been modified to a special freighter configuration, in accordance with FAA SupplementalType Certificate (STC) ST02040SE, and which are listed in paragraph I.A., “Effectivity,” of IsraelAerospace Industries Ltd., Service Bulletin 368-34-106, dated August 2024. |
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] |