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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.
2012-0257-CN
SUBJECT
ATA 64 – CANCELLED: Tail Rotor – Laminated Half-Bearings – Inspection / Replacement
APPLICABILITY
AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2 and AS 350 D helicopters, all serial numbers (s/n). AS 350 B3 helicopters, all s/n, except helicopters that embody modification (MOD) 075601. AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all s/n. Note: MOD 075601 is an integral part of a specific AS 350 B3 model configuration, commercially identified as “AS350B3e” and is not fitted on AS 350 B3 model helicopters of other configurations.
ISSUED BY
EASA
AD NO.
2024-14-03
SUBJECT
Joint Aircraft System Component (JASC) Code 2210, Autopilot System.
APPLICABILITY
Commander Aircraft Corporation: 112B, 112TC, 112TCA, 114, 114A, 114B, 114TC DAHER AEROSPACE: TB20, TB21 Mooney International Corporation: M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20M, M20R, M20S Piper Aircraft, Inc.: PA-24, PA-24-250, PA-24-260, PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28-201T, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-30, PA-39, PA-32-260, PA-32-300, PA-32-301, PA-32-301FT, PA-32-301T, PA-32-301XTC, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 (HP), PA-32R-301 (SP), PA-32R-301T Textron Aviaiton Inc.: 19A, B19, M19A, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R, C35, D35, E35, F35, G35, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, 36, A36, A36TC, B36TC, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P, 172RG, P172D, R172K, FR172K, 177B, 177RG, F177RG, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, F182P, F182Q, FR182, R182, T182, T182T, TR182, 206H, P206C, P206D, P206E, T206H, TP206C, TP206D, TP206E, TU206C, TU206D, TU206E, TU206F, TU206G, U206C, U206D, U206E, U206F, U206G, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N
ISSUED BY
FAA
AD NO.
2024-0141
SUBJECT
ATA 57 – Wings – Main Landing Gear Attachment – Inspection
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0140
SUBJECT
ATA 27 – Flight Controls – Angle of Attack Probes – Replacement
APPLICABILITY
ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0097R2
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.
2024-0139
SUBJECT
ATA 55 – Stabilizers – Vertical Fin – Inspection / Modification ATA 11 – Placards and Markings – Interior Placards – Installation ATA – Aircraft Flight Manual / Airspeed Limitations – Amendment
APPLICABILITY
AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all serial numbers (s/n); and AS 350 B3 helicopters, all s/n, except those that have embodied modification (MOD) 073148 in production.
ISSUED BY
EASA
AD NO.
2024-0136
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment
APPLICABILITY
BR700-725A1-12 engines, all serial numbers. These engines are known to be installed on, but not limited to, Gulfstream GVI (commercial designation G650) aeroplanes.
ISSUED BY
EASA
AD NO.
2024-13-02
SUBJECT
Air Transport Association (ATA) of America Code 35, Oxygen.
APPLICABILITY
This AD applies to all The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes and Model737-700, -800, and -900ER series airplanes, certificated in any category.
ISSUED BY
FAA
AD NO.
2024-0092R1
SUBJECT
ATA 52 – Doors – Main Deck Cargo Door Actuator Bearing Fittings – Inspection
APPLICABILITY
Airbus A300, A300-600 and A310 aeroplanes, all manufacturer serial numbers (MSN), manufactured in freighter model configuration; or modified in accordance with EASA Supplemental Type Certificate (STC) 10014779 (any revision), or EASA STC 10013945 (any revision), or EASA STC 10013960 (any revision), all MSN.
ISSUED BY
EASA
AD NO.
2024-0135
SUBJECT
ATA 53 – Fuselage – Centre Fuselage – Keel Beam Bottom Panel – Inspection
APPLICABILITY
Airbus A318-111, A318-112, A318-121, A318-122 aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or on which Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; 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, A320-231, A320-232 and A320-233 aeroplanes, all MSN having mod 31067 embodied in production, except aeroplanes having a configuration as below: aeroplanes on which Airbus mod 160001 was embodied in production, or on which Airbus SB A320-57-1193 has been embodied in service; and Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all MSN, except aeroplanes on which Airbus mod 160021 was embodied in production.
ISSUED BY
EASA
AD NO.
2021-0282R1
SUBJECT
ATA 64 – Tail Rotor – Tail Rotor Head Pitch Change Unit Bearing Spacer – Marking / Check
APPLICABILITY
AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3, AS 350 D helicopters, and AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N, AS 355 NP helicopters, all serial numbers.
ISSUED BY
EASA
AD NO.
2022-0150R1
SUBJECT
ATA 64 – Tail Rotor – Blades – Inspection
APPLICABILITY
EC 130 B4 and EC 130 T2 helicopters, all serial numbers (s/n).
ISSUED BY
EASA
AD NO. SUBJECT APPLICABILITY ISSUED BY
2012-0257-CN ATA 64 – CANCELLED: Tail Rotor – Laminated Half-Bearings – Inspection / Replacement AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2 and AS 350 D helicopters, all serial numbers (s/n). AS 350 B3 helicopters, all s/n, except helicopters that embody modification (MOD) 075601. AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all s/n. Note: MOD 075601 is an integral part of a specific AS 350 B3 model configuration, commercially identified as “AS350B3e” and is not fitted on AS 350 B3 model helicopters of other configurations.
EASA
2024-14-03 Joint Aircraft System Component (JASC) Code 2210, Autopilot System. Commander Aircraft Corporation: 112B, 112TC, 112TCA, 114, 114A, 114B, 114TC DAHER AEROSPACE: TB20, TB21 Mooney International Corporation: M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20M, M20R, M20S Piper Aircraft, Inc.: PA-24, PA-24-250, PA-24-260, PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181, PA-28-201T, PA-28-235, PA-28-236, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-30, PA-39, PA-32-260, PA-32-300, PA-32-301, PA-32-301FT, PA-32-301T, PA-32-301XTC, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 (HP), PA-32R-301 (SP), PA-32R-301T Textron Aviaiton Inc.: 19A, B19, M19A, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R, C35, D35, E35, F35, G35, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, 36, A36, A36TC, B36TC, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P, 172RG, P172D, R172K, FR172K, 177B, 177RG, F177RG, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, F182P, F182Q, FR182, R182, T182, T182T, TR182, 206H, P206C, P206D, P206E, T206H, TP206C, TP206D, TP206E, TU206C, TU206D, TU206E, TU206F, TU206G, U206C, U206D, U206E, U206F, U206G, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N
FAA
2024-0141 ATA 57 – Wings – Main Landing Gear Attachment – Inspection Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers.
EASA
2024-0140 ATA 27 – Flight Controls – Angle of Attack Probes – Replacement ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500, ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer serial numbers.
EASA
2024-0097R2 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
2024-0139 ATA 55 – Stabilizers – Vertical Fin – Inspection / Modification ATA 11 – Placards and Markings – Interior Placards – Installation ATA – Aircraft Flight Manual / Airspeed Limitations – Amendment AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all serial numbers (s/n); and AS 350 B3 helicopters, all s/n, except those that have embodied modification (MOD) 073148 in production.
EASA
2024-0136 ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment BR700-725A1-12 engines, all serial numbers. These engines are known to be installed on, but not limited to, Gulfstream GVI (commercial designation G650) aeroplanes.
EASA
2024-13-02 Air Transport Association (ATA) of America Code 35, Oxygen. This AD applies to all The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes and Model737-700, -800, and -900ER series airplanes, certificated in any category.
FAA
2024-0092R1 ATA 52 – Doors – Main Deck Cargo Door Actuator Bearing Fittings – Inspection Airbus A300, A300-600 and A310 aeroplanes, all manufacturer serial numbers (MSN), manufactured in freighter model configuration; or modified in accordance with EASA Supplemental Type Certificate (STC) 10014779 (any revision), or EASA STC 10013945 (any revision), or EASA STC 10013960 (any revision), all MSN.
EASA
2024-0135 ATA 53 – Fuselage – Centre Fuselage – Keel Beam Bottom Panel – Inspection Airbus A318-111, A318-112, A318-121, A318-122 aeroplanes, all manufacturer serial numbers (MSN), except aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or on which Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; 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, A320-231, A320-232 and A320-233 aeroplanes, all MSN having mod 31067 embodied in production, except aeroplanes having a configuration as below: aeroplanes on which Airbus mod 160001 was embodied in production, or on which Airbus SB A320-57-1193 has been embodied in service; and Airbus A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all MSN, except aeroplanes on which Airbus mod 160021 was embodied in production.
EASA
2021-0282R1 ATA 64 – Tail Rotor – Tail Rotor Head Pitch Change Unit Bearing Spacer – Marking / Check AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3, AS 350 D helicopters, and AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N, AS 355 NP helicopters, all serial numbers.
EASA
2022-0150R1 ATA 64 – Tail Rotor – Blades – Inspection EC 130 B4 and EC 130 T2 helicopters, all serial numbers (s/n).
EASA

Contact

NoEnquiry TopicEmail Point of Contact
1Aircraft Registration and De-Registration[email protected]
2Certification 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]
3Certification of Airworthiness for Air Operator Certificate (AOC) Holders[email protected]
4Certification of Airworthiness for Non-Air Operator Certificate (Non-AOC) Holders (I.E. GA Aircraft)[email protected]
5Certification of Approved Maintenance Organisation (AMO)[email protected]
6Any Other Matters Not Covered Above[email protected]