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.
2022-17-04
SUBJECT
Air Transport Association (ATA) of America Code 28, Fuel System; and 05, TimeLimits/Maintenance Checks.
APPLICABILITY
This AD applies to De Havilland Aircraft of Canada Limited (type certificate previously held byBombardier, Inc.) Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serialnumbers (S/Ns) 4001, 4003, and subsequent.
ISSUED BY
FAA
AD NO.
2022-18-13
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, and -900 seriesairplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-53A1403 RB, dated August 26, 2021. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability toaccomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE isinstalled, a “change in product” alternative method of compliance (AMOC) approval request is notnecessary to comply with the requirements of 14 CFR 39.17.
ISSUED BY
FAA
AD NO.
2022-18-11
SUBJECT
Air Transport Association (ATA) of America Code 57, Wings.
APPLICABILITY
This AD applies to all The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777Fairplanes, certificated in any category.
ISSUED BY
FAA
AD NO.
2022-0201
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.
ISSUED BY
EASA
AD NO.
2022-0195
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 / System Equipment Maintenance Requirements – Amendment
APPLICABILITY
Airbus A310-203, A310-203C, A310-204, A310-221, A310-222, A310-304, A310-308, A310-322, A310-324 and A310-325 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0193
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitation Items – Amendment
APPLICABILITY
Airbus A310-203, A310-204, A310-221, A310-222, A310-203C, A310-304, A310-308, A310-322, A310-324 and A310-325 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0197
SUBJECT
ATA 28 – Fuel – Fuel Pump – Inspection / Modification
APPLICABILITY
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, A330-743L, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers (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.
2022-18-06
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, andJASC Code 7250, Turbine Section.
APPLICABILITY
This AD applies to: (1) General Electric Company (GE) GE90-110B1 and GE90-115B model turbofan engines; and (2) GE GE90-76B, GE90-85B, GE90-90B, and GE90-94B model turbofan engines with an installedinterstage high-pressure turbine (HPT) rotor seal with part number (P/N) 2629M47P01 and serialnumber (S/N) NCU5430D.
ISSUED BY
FAA
AD NO.
2022-0196
SUBJECT
ATA 25 – Equipment / Furnishings – AFT Galley Complex Lower Attachment Studs – Inspection / Replacement
APPLICABILITY
Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0044, 0056, 0067, 0086, 0087, 0095, 0129, 0136, 0142, 0146, 0149-0151 inclusive, 0153, 0157, 0159, 0160, 0162-0165 inclusive, 0167, 0168, 0172-0179 inclusive, 0181-0185 inclusive, 0187, 0189-0193 inclusive, 0195, 0197-0199 inclusive, 0201-0204 inclusive, 0207-0214 inclusive, 0217, 0218, 0221, 0224, 0228, 0231, 0234-0237 inclusive, 0239, 0240, 0243, 0246, 0247, 0249, 0251, 0255, 0279 and 0297; and A350-1041 aeroplanes, MSN 0118, 0161, 0169, 0188, 0206, 0215, 0225, 0229, 0233, 0241, 0252, 0262, 0286 and 0296.
ISSUED BY
EASA
AD NO.
2022-0189
SUBJECT
ATA 57 – Wings – Inboard Flap Parts – Identification / Inspection
APPLICABILITY
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 and A330-743L aeroplanes, all manufacturer serial numbers (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.
2022-19-12
SUBJECT
Joint Aircraft System Component (JASC) Code: 6410, Tail Rotor Blades
APPLICABILITY
This AD applies to the following Robinson Helicopter Company (Robinson) helicopters, certificated inany category: (1) Robinson Model R44 and R44 II helicopters with a tail rotor blade (blade) part number (P/N)C029-3 with serial number (S/N) 9410 through 9909 inclusive, installed; (2) Robinson Model R44 and R44 II helicopters with a blade P/N C029-3 with S/N 9910 through10659 inclusive, installed; and (3) Robinson Model R66 helicopters with a blade P/N F029-1 with S/N 2410 through 2589 inclusive,installed.
ISSUED BY
FAA
AD NO.
2022-17-02
SUBJECT
Joint Aircraft System Component (JASC) Code 7260, Turbine Engine Accessory Drive
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) LEAP-1B21, LEAP-1B23, LEAP-1B25, LEAP-1B27,LEAP-1B28, LEAP-1B28B1, LEAP-1B28B2, LEAP-1B28B2C, LEAP-1B28B3, LEAP-1B28BBJ1, andLEAP-1B28BBJ2 model turbofan engines with an installed inner radial drive shaft (RDS) with a serialnumber listed in Additional Information, paragraph 6.A., Table 1, of CFM Service Bulletin (SB) LEAP-1B-72-00-0365-01A-930A-D, Issue 003-00, dated April 26, 2022 (CFM SB LEAP-1B-72-00-0365-01A-930A-D).
ISSUED BY
FAA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2022-17-04 | Air Transport Association (ATA) of America Code 28, Fuel System; and 05, TimeLimits/Maintenance Checks. | This AD applies to De Havilland Aircraft of Canada Limited (type certificate previously held byBombardier, Inc.) Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serialnumbers (S/Ns) 4001, 4003, and subsequent. |
FAA
|
| 2022-18-13 | Air Transport Association (ATA) of America Code 53, Fuselage. | (1) This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, and -900 seriesairplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-53A1403 RB, dated August 26, 2021. (2) Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability toaccomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE isinstalled, a “change in product” alternative method of compliance (AMOC) approval request is notnecessary to comply with the requirements of 14 CFR 39.17. |
FAA
|
| 2022-18-11 | Air Transport Association (ATA) of America Code 57, Wings. | This AD applies to all The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777Fairplanes, certificated in any category. |
FAA
|
| 2022-0201 | 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. |
EASA
|
| 2022-0195 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 / System Equipment Maintenance Requirements – Amendment | Airbus A310-203, A310-203C, A310-204, A310-221, A310-222, A310-304, A310-308, A310-322, A310-324 and A310-325 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0193 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 / Damage Tolerant Airworthiness Limitation Items – Amendment | Airbus A310-203, A310-204, A310-221, A310-222, A310-203C, A310-304, A310-308, A310-322, A310-324 and A310-325 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0197 | ATA 28 – Fuel – Fuel Pump – Inspection / Modification | 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, A330-743L, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers (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
|
| 2022-18-06 | Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, andJASC Code 7250, Turbine Section. | This AD applies to: (1) General Electric Company (GE) GE90-110B1 and GE90-115B model turbofan engines; and (2) GE GE90-76B, GE90-85B, GE90-90B, and GE90-94B model turbofan engines with an installedinterstage high-pressure turbine (HPT) rotor seal with part number (P/N) 2629M47P01 and serialnumber (S/N) NCU5430D. |
FAA
|
| 2022-0196 | ATA 25 – Equipment / Furnishings – AFT Galley Complex Lower Attachment Studs – Inspection / Replacement | Airbus A350-941 aeroplanes, manufacturer serial numbers (MSN) 0044, 0056, 0067, 0086, 0087, 0095, 0129, 0136, 0142, 0146, 0149-0151 inclusive, 0153, 0157, 0159, 0160, 0162-0165 inclusive, 0167, 0168, 0172-0179 inclusive, 0181-0185 inclusive, 0187, 0189-0193 inclusive, 0195, 0197-0199 inclusive, 0201-0204 inclusive, 0207-0214 inclusive, 0217, 0218, 0221, 0224, 0228, 0231, 0234-0237 inclusive, 0239, 0240, 0243, 0246, 0247, 0249, 0251, 0255, 0279 and 0297; and A350-1041 aeroplanes, MSN 0118, 0161, 0169, 0188, 0206, 0215, 0225, 0229, 0233, 0241, 0252, 0262, 0286 and 0296. |
EASA
|
| 2022-0189 | ATA 57 – Wings – Inboard Flap Parts – Identification / Inspection | 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 and A330-743L aeroplanes, all manufacturer serial numbers (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
|
| 2022-19-12 | Joint Aircraft System Component (JASC) Code: 6410, Tail Rotor Blades | This AD applies to the following Robinson Helicopter Company (Robinson) helicopters, certificated inany category: (1) Robinson Model R44 and R44 II helicopters with a tail rotor blade (blade) part number (P/N)C029-3 with serial number (S/N) 9410 through 9909 inclusive, installed; (2) Robinson Model R44 and R44 II helicopters with a blade P/N C029-3 with S/N 9910 through10659 inclusive, installed; and (3) Robinson Model R66 helicopters with a blade P/N F029-1 with S/N 2410 through 2589 inclusive,installed. |
FAA
|
| 2022-17-02 | Joint Aircraft System Component (JASC) Code 7260, Turbine Engine Accessory Drive | This AD applies to CFM International, S.A. (CFM) LEAP-1B21, LEAP-1B23, LEAP-1B25, LEAP-1B27,LEAP-1B28, LEAP-1B28B1, LEAP-1B28B2, LEAP-1B28B2C, LEAP-1B28B3, LEAP-1B28BBJ1, andLEAP-1B28BBJ2 model turbofan engines with an installed inner radial drive shaft (RDS) with a serialnumber listed in Additional Information, paragraph 6.A., Table 1, of CFM Service Bulletin (SB) LEAP-1B-72-00-0365-01A-930A-D, Issue 003-00, dated April 26, 2022 (CFM SB LEAP-1B-72-00-0365-01A-930A-D). |
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] |