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.
2024-0159
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Certification Maintenance Requirements and Airworthiness Limitations – Amendment
APPLICABILITY
ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer serial numbers which are in post-MOD 2510 configuration.
ISSUED BY
EASA
AD NO.
2024-0157
SUBJECT
ATA 27 – Flight Controls – Outer Aileron – Master Minimum Equipment List Restriction ATA 32 – Landing Gear – Remote Brake Control Unit / Main Wheel Tie Bolt / Steering Control – Master Minimum Equipment List Restriction
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2024-0156
SUBJECT
ATA 32 – Landing Gear – Main Landing Gear Bogie Beam Axle – Replacement
APPLICABILITY
Airbus A350-941 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0155
SUBJECT
ATA 57 – Wings – RIB 1 Corner Fitting and Upper / Lower Wing Skin Cover Edge Glow Sealant – Inspection / Modification
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, manufacturer serial numbers (MSN) as listed in the inspection SB1, and/or the modification SB1, and/or the modification SB2, and/or the inspection SB2, as defined in this AD.
ISSUED BY
EASA
AD NO.
2024-0147R1
SUBJECT
ATA 53 – Fuselage – Centre Fuselage Forward Pressure Bulkhead – 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, 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, A321-232, aeroplanes, all manufacturer serial numbers (MSN), except: – A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service, and – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production, and – all aeroplanes on which mod 157159 was embodied in production.
ISSUED BY
EASA
AD NO.
2019-0069R2
SUBJECT
ATA 25 – Equipment / Furnishings – Overhead Stowage Compartments – Modification
APPLICABILITY
Airbus A318-112, A318-121, A318-122, A319-111, A319-112, A319-115, A319-131, A319-132, A319-133, A320-214, A320-216, A320-232, A320-233, A320-251N, A320-271N, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-253N, A321-271N and A321-272N aeroplanes, manufacturer serial numbers as listed in the applicable SB.
ISSUED BY
EASA
AD NO.
2024-0151
SUBJECT
ATA – Aircraft Flight Manual / Complementary Performance Data File – Amendment
APPLICABILITY
Airbus 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.
2024-0148
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment
APPLICABILITY
ARRIUS 1A engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aérospatiale) AS 355 N twin-engine helicopters.
ISSUED BY
EASA
AD NO.
2024-0147
SUBJECT
ATA 53 – Fuselage – Centre Fuselage Forward Pressure Bulkhead – 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, 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, A321-232, aeroplanes, all manufacturer serial numbers (MSN), except: – A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service, and – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production, and – all aeroplanes on which mod 157159 was embodied in production.
ISSUED BY
EASA
AD NO.
2024-0118R1
SUBJECT
ATA 72 – Engine – High Pressure Turbine Blades – Inspection / Limitation
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.
2024-0144
SUBJECT
ATA 65 – Tail Rotor Drive – Shaft-Line – Check / Measurement / Modification
APPLICABILITY
EC 130 T2 helicopters, all serial numbers on which AH modification 079809 has been embodied in production.
ISSUED BY
EASA
AD NO.
2024-0143
SUBJECT
ATA 55 – Stabilizers – Maintenance Instructions – Amendment
APPLICABILITY
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, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers; and A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-0159 | ATA 05 – Time Limits / Maintenance Checks – Certification Maintenance Requirements and Airworthiness Limitations – Amendment | ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer serial numbers which are in post-MOD 2510 configuration. |
EASA
|
| 2024-0157 | ATA 27 – Flight Controls – Outer Aileron – Master Minimum Equipment List Restriction ATA 32 – Landing Gear – Remote Brake Control Unit / Main Wheel Tie Bolt / Steering Control – Master Minimum Equipment List Restriction | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2024-0156 | ATA 32 – Landing Gear – Main Landing Gear Bogie Beam Axle – Replacement | Airbus A350-941 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0155 | ATA 57 – Wings – RIB 1 Corner Fitting and Upper / Lower Wing Skin Cover Edge Glow Sealant – Inspection / Modification | Airbus A350-941 and A350-1041 aeroplanes, manufacturer serial numbers (MSN) as listed in the inspection SB1, and/or the modification SB1, and/or the modification SB2, and/or the inspection SB2, as defined in this AD. |
EASA
|
| 2024-0147R1 | ATA 53 – Fuselage – Centre Fuselage Forward Pressure Bulkhead – 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, 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, A321-232, aeroplanes, all manufacturer serial numbers (MSN), except: – A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service, and – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production, and – all aeroplanes on which mod 157159 was embodied in production. |
EASA
|
| 2019-0069R2 | ATA 25 – Equipment / Furnishings – Overhead Stowage Compartments – Modification | Airbus A318-112, A318-121, A318-122, A319-111, A319-112, A319-115, A319-131, A319-132, A319-133, A320-214, A320-216, A320-232, A320-233, A320-251N, A320-271N, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-253N, A321-271N and A321-272N aeroplanes, manufacturer serial numbers as listed in the applicable SB. |
EASA
|
| 2024-0151 | ATA – Aircraft Flight Manual / Complementary Performance Data File – Amendment | Airbus 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
|
| 2024-0148 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment | ARRIUS 1A engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aérospatiale) AS 355 N twin-engine helicopters. |
EASA
|
| 2024-0147 | ATA 53 – Fuselage – Centre Fuselage Forward Pressure Bulkhead – 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, 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, A321-232, aeroplanes, all manufacturer serial numbers (MSN), except: – A318 aeroplanes on which Airbus modification (mod) 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service, and – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production, and – all aeroplanes on which mod 157159 was embodied in production. |
EASA
|
| 2024-0118R1 | ATA 72 – Engine – High Pressure Turbine Blades – Inspection / Limitation | 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
|
| 2024-0144 | ATA 65 – Tail Rotor Drive – Shaft-Line – Check / Measurement / Modification | EC 130 T2 helicopters, all serial numbers on which AH modification 079809 has been embodied in production. |
EASA
|
| 2024-0143 | ATA 55 – Stabilizers – Maintenance Instructions – Amendment | 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, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers; and A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 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] |