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.
2022-09-09 CORRECTION
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, and JASC Code 7250, Turbine Section.
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines.
ISSUED BY
FAA
AD NO.
2022-11-04
SUBJECT
Joint Aircraft System Component (JASC) Code: 5510, Horizontal Stabilizer Structure.
APPLICABILITY
This AD applies to Sikorsky Aircraft Corporation Model S-92A helicopters, certificated in any category, with the following installed: Horizontal stabilizer root fitting FWD (forward root fitting) part number (P/N) 92209-07111-101 or 92070-20125-101; or stabilizer strut fitting P/N 92209- 07403-041 or 92070-20117-041 installed on horizontal stabilizer assembly (stabilizer assembly) P/N 92070-20117-045, 92070-20117-046, 92070-20125-041, 92070-20125-042, 92070-20125-043, 92070-20125-044, 92205-07400-043, 92205-07400-045, or 92205-07400-047.
ISSUED BY
FAA
AD NO.
2022-10-51
SUBJECT
Joint Aircraft System Component (JASC) Code: 2700, Flight Control System.
APPLICABILITY
This AD applies to the helicopters identified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. Note 1 to paragraph (c)(1): Helicopters with an AS350B3e designation are Model AS350B3 helicopters. (2) Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, MBB-BK 117 C-2, MBB-BK 117 D-2, and MBB-BK 117 D-3 helicopters. Note 2 to paragraph (c)(2): Helicopters with an EC135P3H designation are Model EC135P3 helicopters. Helicopters with an EC135T3H designation are Model EC135T3 helicopters. Helicopters with an MBB-BK117 C-2e designation are Model MBB-BK117 C-2 helicopters.
ISSUED BY
FAA
AD NO.
2021-0107R2
SUBJECT
ATA 57 – Wings – Lower Main Wing Spar Caps – Inspection
APPLICABILITY
PA-28-151 (Warrior) All //PA-28-161 (Warrior II) All //PA-28-161 (Warrior III) All, except s/n 2842006 PA-28-161 (Cadet) All //PA-28-181 (Archer II and Archer III) All //PA-28-235 (Cherokee Pathfinder) All// PA-28R-180 (Arrow) All //PA-28R-200 (Arrow) All //PA-28R-200 (Arrow II) All, except s/n 28R-7235151 //PA-28R-201 (Arrow III) All, except s/n 2844029, 2844030, 2844081, 2844125, 2844136, 2844147 to 2844151 inclusive, 28R-7737078, 28R-7737142, 28R-7837108, 28R-7837125 and 28R-7837257 //PA-28R-201T (Turbo Arrow III) All //PA-28RT-201 (Arrow IV) All //PA-28RT-201T (Turbo Arrow IV) All// PA-32-260 (Cherokee Six 260) All //PA-32-300 (Cherokee Six 300) All //PA-32R-300 (Lance) All //PA-32RT-300 (Lance II) All, except s/n 32R-7985004 //PA-32RT-300T (Turbo Lance II) All
ISSUED BY
EASA
AD NO.
2015-0226R7
SUBJECT
ATA 25 – Equipment / Furnishings – Hoist – Test / Replacement
APPLICABILITY
This AD applies to the following helicopters, when equipped with a Goodrich hoist having a Part Number (P/N) as listed in Table 1 of this AD: Leonardo AW109SP, AB139, AW139 and AB412 (all Models) helicopters, all serial numbers (s/n); BTI 212, 214 and 412 helicopters (all Models), all s/n; BTCL 429 and 430 helicopters, all s/n; AH AS 365 N3, AS 332 L2 and EC225 LP helicopters, all s/n; AHD MBB-BK117 C-2, EC135 and EC635 (all Models) helicopters, all s/n; MDHI MD900 helicopters, all s/n; and Sikorsky S-61 (all Models), S-76A, S-76B, S-76C and S-92A helicopters, all s/n.
ISSUED BY
EASA
AD NO.
2022-0091
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 / Certification Maintenance Requirements – Amendment
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, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0090
SUBJECT
ATA 52 – Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism – Inspection
APPLICABILITY
Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX aeroplanes, manufacturer serial numbers as listed in the AOT
ISSUED BY
EASA
AD NO.
2019-0207R1
SUBJECT
ATA 52 – Doors – Passenger / Crew Door Girt Bar Fitting Assemblies – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 115327 has been embodied in production.
ISSUED BY
EASA
AD NO.
2022-0088
SUBJECT
ATA 29 – Hydraulic Power – Yellow Fire Shut Off Valve Grounding Wiring – Modification
APPLICABILITY
Airbus A350-941 aeroplanes, manufacturer serial numbers from 0006 up to 0044 inclusive
ISSUED BY
EASA
AD NO.
2020-0236-CN
SUBJECT
ATA 25 – CANCELLED: Equipment / Furnishings – Emergency Escape Slide / Raft Inflation Reservoir – Pressure Check
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, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-09-09
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, and JASC Code 7250, Turbine Section.
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines.
ISSUED BY
FAA
AD NO.
2022-0086
SUBJECT
ATA 67 – Rotors Flight Control – Tail Rotor Actuator – Inspection
APPLICABILITY
MBB-BK117 C-2 helicopters, all serial numbers.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2022-09-09 CORRECTION | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, and JASC Code 7250, Turbine Section. | This AD applies to CFM International, S.A. (CFM) LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines. |
FAA
|
| 2022-11-04 | Joint Aircraft System Component (JASC) Code: 5510, Horizontal Stabilizer Structure. | This AD applies to Sikorsky Aircraft Corporation Model S-92A helicopters, certificated in any category, with the following installed: Horizontal stabilizer root fitting FWD (forward root fitting) part number (P/N) 92209-07111-101 or 92070-20125-101; or stabilizer strut fitting P/N 92209- 07403-041 or 92070-20117-041 installed on horizontal stabilizer assembly (stabilizer assembly) P/N 92070-20117-045, 92070-20117-046, 92070-20125-041, 92070-20125-042, 92070-20125-043, 92070-20125-044, 92205-07400-043, 92205-07400-045, or 92205-07400-047. |
FAA
|
| 2022-10-51 | Joint Aircraft System Component (JASC) Code: 2700, Flight Control System. | This AD applies to the helicopters identified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. Note 1 to paragraph (c)(1): Helicopters with an AS350B3e designation are Model AS350B3 helicopters. (2) Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, MBB-BK 117 C-2, MBB-BK 117 D-2, and MBB-BK 117 D-3 helicopters. Note 2 to paragraph (c)(2): Helicopters with an EC135P3H designation are Model EC135P3 helicopters. Helicopters with an EC135T3H designation are Model EC135T3 helicopters. Helicopters with an MBB-BK117 C-2e designation are Model MBB-BK117 C-2 helicopters. |
FAA
|
| 2021-0107R2 | ATA 57 – Wings – Lower Main Wing Spar Caps – Inspection | PA-28-151 (Warrior) All //PA-28-161 (Warrior II) All //PA-28-161 (Warrior III) All, except s/n 2842006 PA-28-161 (Cadet) All //PA-28-181 (Archer II and Archer III) All //PA-28-235 (Cherokee Pathfinder) All// PA-28R-180 (Arrow) All //PA-28R-200 (Arrow) All //PA-28R-200 (Arrow II) All, except s/n 28R-7235151 //PA-28R-201 (Arrow III) All, except s/n 2844029, 2844030, 2844081, 2844125, 2844136, 2844147 to 2844151 inclusive, 28R-7737078, 28R-7737142, 28R-7837108, 28R-7837125 and 28R-7837257 //PA-28R-201T (Turbo Arrow III) All //PA-28RT-201 (Arrow IV) All //PA-28RT-201T (Turbo Arrow IV) All// PA-32-260 (Cherokee Six 260) All //PA-32-300 (Cherokee Six 300) All //PA-32R-300 (Lance) All //PA-32RT-300 (Lance II) All, except s/n 32R-7985004 //PA-32RT-300T (Turbo Lance II) All |
EASA
|
| 2015-0226R7 | ATA 25 – Equipment / Furnishings – Hoist – Test / Replacement | This AD applies to the following helicopters, when equipped with a Goodrich hoist having a Part Number (P/N) as listed in Table 1 of this AD: Leonardo AW109SP, AB139, AW139 and AB412 (all Models) helicopters, all serial numbers (s/n); BTI 212, 214 and 412 helicopters (all Models), all s/n; BTCL 429 and 430 helicopters, all s/n; AH AS 365 N3, AS 332 L2 and EC225 LP helicopters, all s/n; AHD MBB-BK117 C-2, EC135 and EC635 (all Models) helicopters, all s/n; MDHI MD900 helicopters, all s/n; and Sikorsky S-61 (all Models), S-76A, S-76B, S-76C and S-92A helicopters, all s/n. |
EASA
|
| 2022-0091 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 / Certification Maintenance Requirements – Amendment | 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, all manufacturer serial numbers. |
EASA
|
| 2022-0090 | ATA 52 – Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism – Inspection | Airbus A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX aeroplanes, manufacturer serial numbers as listed in the AOT |
EASA
|
| 2019-0207R1 | ATA 52 – Doors – Passenger / Crew Door Girt Bar Fitting Assemblies – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification (mod) 115327 has been embodied in production. |
EASA
|
| 2022-0088 | ATA 29 – Hydraulic Power – Yellow Fire Shut Off Valve Grounding Wiring – Modification | Airbus A350-941 aeroplanes, manufacturer serial numbers from 0006 up to 0044 inclusive |
EASA
|
| 2020-0236-CN | ATA 25 – CANCELLED: Equipment / Furnishings – Emergency Escape Slide / Raft Inflation Reservoir – Pressure Check | 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, all manufacturer serial numbers. |
EASA
|
| 2022-09-09 | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, and JASC Code 7250, Turbine Section. | This AD applies to CFM International, S.A. (CFM) LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines. |
FAA
|
| 2022-0086 | ATA 67 – Rotors Flight Control – Tail Rotor Actuator – Inspection | MBB-BK117 C-2 helicopters, all 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] |