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.
2023-0101
SUBJECT
ATA 25 – Equipment/Furnishings – Life Raft Inflation System – Replacement
APPLICABILITY
AB139 and AW139 helicopters, all serial numbers (s/n).
ISSUED BY
EASA
AD NO.
2023-0098R1
SUBJECT
ATA 57 – Wings – Front and Rear Spars – Inspection
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2023-0093R1
SUBJECT
ATA 32 – Landing Gear – Braking and Steering Control Unit – Replacement / Master Minimum Equipment List – Amendment ATA 92 – Electric and Electronic Common Installation – Relays – Replacement
APPLICABILITY
Airbus A319-151N, A319-153N, A319-171N, 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, A321-272NX aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2023-0098
SUBJECT
ATA 57 – Wings – Front and Rear Spars – Inspection
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2021-0234R1
SUBJECT
ATA 46 – Information Systems – Electronic Flight Bag Universal Serial Bus Receptacle – Modification
APPLICABILITY
Fokker F27 Mark 050, F28 Mark 3000, F28 Mark 0070 and F28 Mark 0100 aeroplanes; Airbus A318, A319, A320, A321, A330 and A340 aeroplanes; ATR42 and ATR72 aeroplanes; Boeing 737, 757, 767 and 777 aeroplanes; Bombardier (formerly Canadair) and MHI RJ Aviation ULC (formerly Bombardier) CL-600 aeroplanes; and De Havilland Aircraft of Canada (formerly Bombardier) DHC-8 aeroplanes; models and manufacturer serial numbers (MSN) as identified in Appendix 1 of this AD.
ISSUED BY
EASA
AD NO.
2023–07–11
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section.
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) Model LEAP–1B21, LEAP–1B23, LEAP–1B25, LEAP–1B27, LEAP–1B28, LEAP–1B28B1, LEAP–1B28B2, LEAP–1B28B2C, LEAP–1B28B3, LEAP– 1B28BBJ1, and LEAP–1B28BBJ2 engines with an installed No. 3 bearing spring finger housing, part number 2542M54G01, and serial number identified in Table 1 of CFM Service Bulletin LEAP–1B–72– 00–0369–01A–930A–D, Issue 001–00, dated August 22, 2022 (CFM SB LEAP–1B–72–00–0369– 01A–930A–D).
ISSUED BY
FAA
AD NO.
2023-0094
SUBJECT
ATA 35 – Oxygen – SafeLav Gaseous Oxygen Container – 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, all manufacturer serial numbers (MSN); 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, A330-841 and A330- 941 aeroplanes, all MSN; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340- 642 and A340-643 aeroplanes, all MSN.
ISSUED BY
EASA
AD NO.
2023-0093
SUBJECT
ATA 32 – Landing Gear – Braking and Steering Control Unit – Replacement / Master Minimum Equipment List – Amendment ATA 92 – Electric and Electronic Common Installation – Relays – Replacement
APPLICABILITY
Airbus A319-151N, A319-153N, A319-171N, 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, A321-272NX aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2023-0089
SUBJECT
ATA 55 – Stabilizers – Vertical Fin – Inspection 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.
2023-0088
SUBJECT
ATA 11 – Placards and Markings – Stretcher Unit / Placard – Installation
APPLICABILITY
AB139 and AW139 helicopters, all serial numbers (s/n), if modified by EASA STC 10017231 Revision 1 or Revision 2, or STC EASA.R.S.01403 (installation of 3-stretcher Kit Part Number (P/N) 139084-501).
ISSUED BY
EASA
AD NO.
2023–06–15
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
(1) This AD applies to The Boeing Company Model 737–600, –700, –700C, –800, –900, and –900ER series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737– 53A1402 RB, dated July 2, 2021. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a “change in product” alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.
ISSUED BY
FAA
AD NO.
2023-0078R1
SUBJECT
ATA 24 – Electrical Power – Direct Current Emergency Electrical Network – Tests / Modification ATA – Aircraft Flight Manual / Master Minimum Equipment List – Amendment
APPLICABILITY
ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); 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.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2023-0101 | ATA 25 – Equipment/Furnishings – Life Raft Inflation System – Replacement | AB139 and AW139 helicopters, all serial numbers (s/n). |
EASA
|
| 2023-0098R1 | ATA 57 – Wings – Front and Rear Spars – Inspection | Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2023-0093R1 | ATA 32 – Landing Gear – Braking and Steering Control Unit – Replacement / Master Minimum Equipment List – Amendment ATA 92 – Electric and Electronic Common Installation – Relays – Replacement | Airbus A319-151N, A319-153N, A319-171N, 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, A321-272NX aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2023-0098 | ATA 57 – Wings – Front and Rear Spars – Inspection | Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2021-0234R1 | ATA 46 – Information Systems – Electronic Flight Bag Universal Serial Bus Receptacle – Modification | Fokker F27 Mark 050, F28 Mark 3000, F28 Mark 0070 and F28 Mark 0100 aeroplanes; Airbus A318, A319, A320, A321, A330 and A340 aeroplanes; ATR42 and ATR72 aeroplanes; Boeing 737, 757, 767 and 777 aeroplanes; Bombardier (formerly Canadair) and MHI RJ Aviation ULC (formerly Bombardier) CL-600 aeroplanes; and De Havilland Aircraft of Canada (formerly Bombardier) DHC-8 aeroplanes; models and manufacturer serial numbers (MSN) as identified in Appendix 1 of this AD. |
EASA
|
| 2023–07–11 | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section. | This AD applies to CFM International, S.A. (CFM) Model LEAP–1B21, LEAP–1B23, LEAP–1B25, LEAP–1B27, LEAP–1B28, LEAP–1B28B1, LEAP–1B28B2, LEAP–1B28B2C, LEAP–1B28B3, LEAP– 1B28BBJ1, and LEAP–1B28BBJ2 engines with an installed No. 3 bearing spring finger housing, part number 2542M54G01, and serial number identified in Table 1 of CFM Service Bulletin LEAP–1B–72– 00–0369–01A–930A–D, Issue 001–00, dated August 22, 2022 (CFM SB LEAP–1B–72–00–0369– 01A–930A–D). |
FAA
|
| 2023-0094 | ATA 35 – Oxygen – SafeLav Gaseous Oxygen Container – 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, all manufacturer serial numbers (MSN); 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, A330-841 and A330- 941 aeroplanes, all MSN; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340- 642 and A340-643 aeroplanes, all MSN. |
EASA
|
| 2023-0093 | ATA 32 – Landing Gear – Braking and Steering Control Unit – Replacement / Master Minimum Equipment List – Amendment ATA 92 – Electric and Electronic Common Installation – Relays – Replacement | Airbus A319-151N, A319-153N, A319-171N, 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, A321-272NX aeroplanes, all manufacturer serial numbers (MSN). |
EASA
|
| 2023-0089 | ATA 55 – Stabilizers – Vertical Fin – Inspection 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
|
| 2023-0088 | ATA 11 – Placards and Markings – Stretcher Unit / Placard – Installation | AB139 and AW139 helicopters, all serial numbers (s/n), if modified by EASA STC 10017231 Revision 1 or Revision 2, or STC EASA.R.S.01403 (installation of 3-stretcher Kit Part Number (P/N) 139084-501). |
EASA
|
| 2023–06–15 | Air Transport Association (ATA) of America Code 53, Fuselage. | (1) This AD applies to The Boeing Company Model 737–600, –700, –700C, –800, –900, and –900ER series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737– 53A1402 RB, dated July 2, 2021. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a “change in product” alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17. |
FAA
|
| 2023-0078R1 | ATA 24 – Electrical Power – Direct Current Emergency Electrical Network – Tests / Modification ATA – Aircraft Flight Manual / Master Minimum Equipment List – Amendment | ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); 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. |
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] |