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 : 252
AD NO.
2024-0113
SUBJECT
ATA 64 – Tail Rotor – Tail Rotor Hub Tension-Torsion Bars – Inspection
APPLICABILITY
EC 130 B4 and EC 130 T2 helicopters, all serial numbers.
ISSUED BY
EASA
AD NO.
2024-0111
SUBJECT
ATA 72 – Reciprocating Engine – Inspection
APPLICABILITY
All engine types and models, as specified in the referenced TCDS, all serial numbers, except those manufactured after 18 July 2004, and except those which have been overhauled in accordance with applicable instructions issued by the Type Certificate Holder after 18 July 2004.
ISSUED BY
EASA
AD NO.
2024-0107
SUBJECT
ATA 25 – Equipment / Furnishings – Medical Equipment Support – Inspection
APPLICABILITY
MBB-BK117 D-2 and D-3 helicopters, all serial numbers (s/n), if modified in accordance with EASA STC 10051018 up to revision 4 (inclusive).
ISSUED BY
EASA
AD NO.
2024-11-03
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine.
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.
2024-0106
SUBJECT
ATA 44 – Cabin Systems – Antenna Adapter Plate – Inspection
APPLICABILITY
Airbus 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, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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 A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343, A330-841 and A330-941 aeroplanes; and Airbus A350-941 and A350-1041 aeroplanes; and Airbus A380-841, A380-842 and A380-861 aeroplanes; all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0105
SUBJECT
ATA 53 – Fuselage – Potable and Waste Water Service Panels – Modification
APPLICABILITY
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133 aeroplanes, all manufacturer serial numbers except those on which: – Airbus modification (mod) 160001 was embodied in production or SB A320-57-1193 was embodied in service; and/or – Airbus mod 28238, mod 28162 and mod 28342 were embodied in production.
ISSUED BY
EASA
AD NO.
2024-0091R1
SUBJECT
ATA – Aircraft Flight Manual / Section Limitations – AmendmentATA 22 – Auto Flight – New Flight Guidance Standard – Modification
APPLICABILITY
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-151N, A319-153N, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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.
2024-0097R1
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.
2024-0102
SUBJECT
ATA 72 – Engine – Low Pressure Compressor Blades – Inspection / Replacement
APPLICABILITY
RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A330 aeroplanes.
ISSUED BY
EASA
AD NO.
2024-10-04
SUBJECT
Joint Aircraft System Component (JASC) Code 5740, Wing, Attach Fittings.
APPLICABILITY
This AD applies to Piper Aircraft, Inc. Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes, certificated in any category,serial numbers as identified in Piper Service Bulletin No. 1413, dated April 9, 2024 (Piper Service Bulletin No. 1413).
ISSUED BY
FAA
AD NO.
2024-0098
SUBJECT
ATA 53 – Fuselage – Forward Cargo Door Piano Hinges – Inspection
APPLICABILITY
Airbus A350-941 aeroplanes manufacturer serial numbers (MSN) 0001 through 0645 (inclusive), except aeroplanes having Airbus modification (mod) 113979 embodied in production; and A350-1041 aeroplanes, MSN 00059 through 00584 inclusive.
ISSUED BY
EASA
AD NO.
2024-10-04
SUBJECT
Joint Aircraft System Component (JASC) Code 5740, Wing, Attach Fittings.
APPLICABILITY
This AD applies to Piper Aircraft, Inc. Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180airplanes, certificated in any category, serial numbers as identified in Piper Service Bulletin No. 1413,dated April 9, 2024 (Piper Service Bulletin No. 1413).
ISSUED BY
FAA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-0113 | ATA 64 – Tail Rotor – Tail Rotor Hub Tension-Torsion Bars – Inspection | EC 130 B4 and EC 130 T2 helicopters, all serial numbers. |
EASA
|
| 2024-0111 | ATA 72 – Reciprocating Engine – Inspection | All engine types and models, as specified in the referenced TCDS, all serial numbers, except those manufactured after 18 July 2004, and except those which have been overhauled in accordance with applicable instructions issued by the Type Certificate Holder after 18 July 2004. |
EASA
|
| 2024-0107 | ATA 25 – Equipment / Furnishings – Medical Equipment Support – Inspection | MBB-BK117 D-2 and D-3 helicopters, all serial numbers (s/n), if modified in accordance with EASA STC 10051018 up to revision 4 (inclusive). |
EASA
|
| 2024-11-03 | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine. | 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
|
| 2024-0106 | ATA 44 – Cabin Systems – Antenna Adapter Plate – Inspection | Airbus 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, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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 A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343, A330-841 and A330-941 aeroplanes; and Airbus A350-941 and A350-1041 aeroplanes; and Airbus A380-841, A380-842 and A380-861 aeroplanes; all manufacturer serial numbers. |
EASA
|
| 2024-0105 | ATA 53 – Fuselage – Potable and Waste Water Service Panels – Modification | Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133 aeroplanes, all manufacturer serial numbers except those on which: – Airbus modification (mod) 160001 was embodied in production or SB A320-57-1193 was embodied in service; and/or – Airbus mod 28238, mod 28162 and mod 28342 were embodied in production. |
EASA
|
| 2024-0091R1 | ATA – Aircraft Flight Manual / Section Limitations – AmendmentATA 22 – Auto Flight – New Flight Guidance Standard – Modification | Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-151N, A319-153N, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, 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
|
| 2024-0097R1 | 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
|
| 2024-0102 | ATA 72 – Engine – Low Pressure Compressor Blades – Inspection / Replacement | RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A330 aeroplanes. |
EASA
|
| 2024-10-04 | Joint Aircraft System Component (JASC) Code 5740, Wing, Attach Fittings. | This AD applies to Piper Aircraft, Inc. Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes, certificated in any category,serial numbers as identified in Piper Service Bulletin No. 1413, dated April 9, 2024 (Piper Service Bulletin No. 1413). |
FAA
|
| 2024-0098 | ATA 53 – Fuselage – Forward Cargo Door Piano Hinges – Inspection | Airbus A350-941 aeroplanes manufacturer serial numbers (MSN) 0001 through 0645 (inclusive), except aeroplanes having Airbus modification (mod) 113979 embodied in production; and A350-1041 aeroplanes, MSN 00059 through 00584 inclusive. |
EASA
|
| 2024-10-04 | Joint Aircraft System Component (JASC) Code 5740, Wing, Attach Fittings. | This AD applies to Piper Aircraft, Inc. Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180airplanes, certificated in any category, serial numbers as identified in Piper Service Bulletin No. 1413,dated April 9, 2024 (Piper Service Bulletin No. 1413). |
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] |