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.
2023–21–09
SUBJECT
Air Transport Association (ATA) of America Code 27, Flight controls.
APPLICABILITY
This AD applies to all The Boeing Company Model 777–200, 777–200LR, 777–300, 777–300ER, and777F series airplanes, certificated in any category.
ISSUED BY
FAA
AD NO.
2023-0197
SUBJECT
ATA 65 – Tail Rotor Drive – Flexible Couplings and Tail Rotor Shafts – Inspection
APPLICABILITY
EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 P3, EC635 T1, EC635 T2+ and EC635 T3 helicopters, all variants, all serial numbers (s/n).
ISSUED BY
EASA
AD NO.
2023-0196
SUBJECT
ATA 24 – Electrical Power – Nickel-Cadmium Rechargeable Batteries – 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, 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 and A321-272NX aeroplanes; and Airbus A300 B4-2C, A300 B4-102, A300 B4-103, A300 B4-120, A300 B4-203, A300 B4-220, A300 C4-203, A300 F4-203, A310-203, A310-221, A310-222, A310-204, A310-203C, A310-322, A310-304, A310-324, A310-308, A310-325, A300 B4-620, A300 B4-601, A300 B4-603, A300 B4-622, A300 C4-620, A300 B4-605R, A300 B4-622R, A300 F4-605R, A300 F4-622R and A300 C4-605R variant F aeroplanes; and Airbus A300 F4-608ST aeroplanes; and 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, A330-743L, A330-841 and A330-941, aeroplanes; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313 and A340-541, A340-542, A340-642 and A340-643 aeroplanes; and Airbus A350-941 and A350-1041 aeroplanes; and Airbus A380-841, A380-842 and A380-861 aeroplanes.
ISSUED BY
EASA
AD NO.
2023-0190-E
SUBJECT
ATA 65 – Tail Rotor Drive – Shaft-Line – Check / Measurement
APPLICABILITY
EC 130 T2 helicopters, all serial numbers on which AH modification 079809 has been embodied in production.
ISSUED BY
EASA
AD NO.
2023-0189
SUBJECT
ATA 36 – Pneumatic – TRENT XWB Engine Bleed Air Supply System T-Duct – Replacement
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN). Note: While the applicability of the SB, as defined in this AD, is limited to aeroplanes installing Trent XWB-84 and Trent XWB-97 engines, this AD is also applicable to aeroplanes installing Trent XWB-75 engines.
ISSUED BY
EASA
AD NO.
2023-0187
SUBJECT
ATA 76 – Engine Controls – Microswitches – Inspection / Modification
APPLICABILITY
AS 350 B3 helicopters, all serial numbers (s/n). EC 130 B4 helicopters, all s/n. EC 130 T2 helicopters, all s/n.
ISSUED BY
EASA
AD NO.
2023-0186
SUBJECT
ATA 75 – Air – Intermediate / High Pressure Air Tubes – Inspection
APPLICABILITY
Trent 7000-72 and Trent 7000-72C engines, all serial numbers.
ISSUED BY
EASA
AD NO.
2023-0185
SUBJECT
ATA 72 – Engine – Low Pressure Compressor Blades – Inspection / Replacement
APPLICABILITY
Trent 1000 engines, models Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G and Trent 1000-H engines, all engine serial numbers (ESN); and Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2 and Trent 1000-L2 engines, all ESN. These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes.
ISSUED BY
EASA
AD NO.
2020-0262R1
SUBJECT
ATA 27 – Flight Controls – Stabilator Trim Control Cable – Inspection / Replacement
APPLICABILITY
P.68R “Victor”, P.68C, P.68C-TC, P.68 “Observer”, P.68 “Observer 2” and P.68TC “Observer” aeroplanes, serial number (s/n) 333, 337 to 339 inclusive, 378, 379, and 383 to 524 inclusive, except s/n 387, 398, 410, 418, 426, 508, 514 and 522.
ISSUED BY
EASA
AD NO.
2023-0181
SUBJECT
ATA 24 – Electrical Power – Direct Current Emergency Electrical Network Contactor 1PA – Operational Test
APPLICABILITY
ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN), except those on which ATR modification (mod) 05948 has been embodied in production; 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, except those on which ATR mod 05948 has been embodied in production.
ISSUED BY
EASA
AD NO.
2023-0179
SUBJECT
ATA 53 – Fuselage – Cargo Door Frame Attachment Drillings – Inspection
APPLICABILITY
Airbus A320-214, A320-216, A320-251N, A320-271N and A321-253NX aeroplanes, manufacturer serial numbers 8781, 8998, 9015, 9036, 9049, 9068, 9077, 9130, 9175, 9197, 9200, 9211, 9216, 9246, 9252, 9253, 9254, 9264, 9273, 9287, 9300, 9306, 9313, 9316, 9317, 9328, 9329, 9331, 9332, 9341, 9343, 9354, 9358, 9363, 9373, 9378, 9384, 9391, 9394, 9428, 9431, 9439, 9446, 9453, 9454, 9457, 9465, 9473, 9482, 9526, 9559, 9574, 9590, 9595, 10019 and 10044.
ISSUED BY
EASA
AD NO.
2023-0176
SUBJECT
ATA 53 – Fuselage – Cargo Compartment Panels Sealing Tape – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2023–21–09 | Air Transport Association (ATA) of America Code 27, Flight controls. | This AD applies to all The Boeing Company Model 777–200, 777–200LR, 777–300, 777–300ER, and777F series airplanes, certificated in any category. |
FAA
|
| 2023-0197 | ATA 65 – Tail Rotor Drive – Flexible Couplings and Tail Rotor Shafts – Inspection | EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 P3, EC635 T1, EC635 T2+ and EC635 T3 helicopters, all variants, all serial numbers (s/n). |
EASA
|
| 2023-0196 | ATA 24 – Electrical Power – Nickel-Cadmium Rechargeable Batteries – 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, 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 and A321-272NX aeroplanes; and Airbus A300 B4-2C, A300 B4-102, A300 B4-103, A300 B4-120, A300 B4-203, A300 B4-220, A300 C4-203, A300 F4-203, A310-203, A310-221, A310-222, A310-204, A310-203C, A310-322, A310-304, A310-324, A310-308, A310-325, A300 B4-620, A300 B4-601, A300 B4-603, A300 B4-622, A300 C4-620, A300 B4-605R, A300 B4-622R, A300 F4-605R, A300 F4-622R and A300 C4-605R variant F aeroplanes; and Airbus A300 F4-608ST aeroplanes; and 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, A330-743L, A330-841 and A330-941, aeroplanes; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313 and A340-541, A340-542, A340-642 and A340-643 aeroplanes; and Airbus A350-941 and A350-1041 aeroplanes; and Airbus A380-841, A380-842 and A380-861 aeroplanes. |
EASA
|
| 2023-0190-E | ATA 65 – Tail Rotor Drive – Shaft-Line – Check / Measurement | EC 130 T2 helicopters, all serial numbers on which AH modification 079809 has been embodied in production. |
EASA
|
| 2023-0189 | ATA 36 – Pneumatic – TRENT XWB Engine Bleed Air Supply System T-Duct – Replacement | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN). Note: While the applicability of the SB, as defined in this AD, is limited to aeroplanes installing Trent XWB-84 and Trent XWB-97 engines, this AD is also applicable to aeroplanes installing Trent XWB-75 engines. |
EASA
|
| 2023-0187 | ATA 76 – Engine Controls – Microswitches – Inspection / Modification | AS 350 B3 helicopters, all serial numbers (s/n). EC 130 B4 helicopters, all s/n. EC 130 T2 helicopters, all s/n. |
EASA
|
| 2023-0186 | ATA 75 – Air – Intermediate / High Pressure Air Tubes – Inspection | Trent 7000-72 and Trent 7000-72C engines, all serial numbers. |
EASA
|
| 2023-0185 | ATA 72 – Engine – Low Pressure Compressor Blades – Inspection / Replacement | Trent 1000 engines, models Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G and Trent 1000-H engines, all engine serial numbers (ESN); and Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2 and Trent 1000-L2 engines, all ESN. These engines are known to be installed on, but not limited to, Boeing 787 aeroplanes. |
EASA
|
| 2020-0262R1 | ATA 27 – Flight Controls – Stabilator Trim Control Cable – Inspection / Replacement | P.68R “Victor”, P.68C, P.68C-TC, P.68 “Observer”, P.68 “Observer 2” and P.68TC “Observer” aeroplanes, serial number (s/n) 333, 337 to 339 inclusive, 378, 379, and 383 to 524 inclusive, except s/n 387, 398, 410, 418, 426, 508, 514 and 522. |
EASA
|
| 2023-0181 | ATA 24 – Electrical Power – Direct Current Emergency Electrical Network Contactor 1PA – Operational Test | ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN), except those on which ATR modification (mod) 05948 has been embodied in production; 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, except those on which ATR mod 05948 has been embodied in production. |
EASA
|
| 2023-0179 | ATA 53 – Fuselage – Cargo Door Frame Attachment Drillings – Inspection | Airbus A320-214, A320-216, A320-251N, A320-271N and A321-253NX aeroplanes, manufacturer serial numbers 8781, 8998, 9015, 9036, 9049, 9068, 9077, 9130, 9175, 9197, 9200, 9211, 9216, 9246, 9252, 9253, 9254, 9264, 9273, 9287, 9300, 9306, 9313, 9316, 9317, 9328, 9329, 9331, 9332, 9341, 9343, 9354, 9358, 9363, 9373, 9378, 9384, 9391, 9394, 9428, 9431, 9439, 9446, 9453, 9454, 9457, 9465, 9473, 9482, 9526, 9559, 9574, 9590, 9595, 10019 and 10044. |
EASA
|
| 2023-0176 | ATA 53 – Fuselage – Cargo Compartment Panels Sealing Tape – Inspection | Airbus A350-941 and A350-1041 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] |