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.
2022-0131
SUBJECT
ATA 11 – Placards & Markings – Fuel Shut-off Valve Placards – Replacement ATA – Aircraft Flight Manual – Fuel Handling Procedure – Amendment
APPLICABILITY
P92-J and P92-JS aeroplanes, all serial numbers (s/n) up to s/n 151 inclusive.
ISSUED BY
EASA
AD NO.
2022-0132
SUBJECT
ATA 27 – Flight Controls – Aileron Control Rod / Cover Panel Screws – Inspection
APPLICABILITY
P2006T aeroplanes, all serial numbers (s/n) up to s/n 345 inclusive.
ISSUED BY
EASA
AD NO.
2022-14-02
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section; 7250, Turbine Section.
APPLICABILITY
This AD applies to CFM International, S.A. LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines with an installed: (1) High-pressure turbine (HPT) rotor stage 1 disk (HPT stage 1 disk) with part number (P/N) and serial number (S/N) identified in Table 1 to paragraph (g)(1) of this AD; or, (2) Stages 6-10 compressor rotor spool with P/N 2468M20G03 and S/N GWN1141P
ISSUED BY
FAA
AD NO.
2022-0129
SUBJECT
ATA 72 – Engine – Front Engine Mount Support Structure – Inspection
APPLICABILITY
Trent XWB-75, Trent XWB-79, Trent XWB-79B, Trent XWB-84 and Trent XWB-97 engines, all engine serial numbers. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes.
ISSUED BY
EASA
AD NO.
2022-0120R1
SUBJECT
ATA 25 – Equipment / Furnishings – 80VU Rack Attachments – Inspection / Repair
APPLICABILITY
Airbus A318-111, A318-112, 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 and A321-232 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0128
SUBJECT
ATA 53 – Fuselage – Main Gearbox Bracket Bolts – Inspection
APPLICABILITY
AS 350 B, AS 350 D, AS 350 B1, AS 350 B2, AS 350 BA, AS 350 BB, AS 350 B3, EC 130 B4, EC 130 T2, AS 355 E, AS355 F, AS355 F1, AS355 F2, AS355 N and AS355 NP helicopters, all serial numbers.
ISSUED BY
EASA
AD NO.
2020-0261R1
SUBJECT
ATA 72 – Engine – Accessory Gearbox – Modification
APPLICABILITY
CFM56-3 engines, all models, all serial numbers (s/n). CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/2, CFM56-7B26/3, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B26/3B2F, CFM56-7B26/3F, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27/2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B1F, CFM56-7B27/3B3, CFM56-7B27/3F, CFM56-7B27/B1 and CFM56-7B27/B3 engines, all s/n. These engines are known to be installed on, but not limited to, Boeing 737 aeroplanes.
ISSUED BY
EASA
AD NO.
2022-11-13
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
(1) This AD applies to The Boeing Company Model 737-700, -800, and -900ER series airplanes, certificated in any category, and identified in Boeing Alert Requirements Bulletin 737-53A1384 RB, dated September 10, 2020. (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.
2022-0127
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – System Equipment Maintenance Requirements – ALS Part 4 – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0126
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Certification Maintenance Requirements – ALS Part 3 – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0125
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0124
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2022-0131 | ATA 11 – Placards & Markings – Fuel Shut-off Valve Placards – Replacement ATA – Aircraft Flight Manual – Fuel Handling Procedure – Amendment | P92-J and P92-JS aeroplanes, all serial numbers (s/n) up to s/n 151 inclusive. |
EASA
|
| 2022-0132 | ATA 27 – Flight Controls – Aileron Control Rod / Cover Panel Screws – Inspection | P2006T aeroplanes, all serial numbers (s/n) up to s/n 345 inclusive. |
EASA
|
| 2022-14-02 | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section; 7250, Turbine Section. | This AD applies to CFM International, S.A. LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines with an installed: (1) High-pressure turbine (HPT) rotor stage 1 disk (HPT stage 1 disk) with part number (P/N) and serial number (S/N) identified in Table 1 to paragraph (g)(1) of this AD; or, (2) Stages 6-10 compressor rotor spool with P/N 2468M20G03 and S/N GWN1141P |
FAA
|
| 2022-0129 | ATA 72 – Engine – Front Engine Mount Support Structure – Inspection | Trent XWB-75, Trent XWB-79, Trent XWB-79B, Trent XWB-84 and Trent XWB-97 engines, all engine serial numbers. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes. |
EASA
|
| 2022-0120R1 | ATA 25 – Equipment / Furnishings – 80VU Rack Attachments – Inspection / Repair | Airbus A318-111, A318-112, 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 and A321-232 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0128 | ATA 53 – Fuselage – Main Gearbox Bracket Bolts – Inspection | AS 350 B, AS 350 D, AS 350 B1, AS 350 B2, AS 350 BA, AS 350 BB, AS 350 B3, EC 130 B4, EC 130 T2, AS 355 E, AS355 F, AS355 F1, AS355 F2, AS355 N and AS355 NP helicopters, all serial numbers. |
EASA
|
| 2020-0261R1 | ATA 72 – Engine – Accessory Gearbox – Modification | CFM56-3 engines, all models, all serial numbers (s/n). CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/2, CFM56-7B26/3, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B26/3B2F, CFM56-7B26/3F, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27/2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B1F, CFM56-7B27/3B3, CFM56-7B27/3F, CFM56-7B27/B1 and CFM56-7B27/B3 engines, all s/n. These engines are known to be installed on, but not limited to, Boeing 737 aeroplanes. |
EASA
|
| 2022-11-13 | Air Transport Association (ATA) of America Code 53, Fuselage. | (1) This AD applies to The Boeing Company Model 737-700, -800, and -900ER series airplanes, certificated in any category, and identified in Boeing Alert Requirements Bulletin 737-53A1384 RB, dated September 10, 2020. (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
|
| 2022-0127 | ATA 05 – Time Limits / Maintenance Checks – System Equipment Maintenance Requirements – ALS Part 4 – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0126 | ATA 05 – Time Limits / Maintenance Checks – Certification Maintenance Requirements – ALS Part 3 – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0125 | ATA 05 – Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0124 | ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – Amendment | Airbus A350-941 and A350-1041 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] |