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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 : 1315
AD NO.
2022-0100
SUBJECT
ATA 53 – Fuselage – Belly Fairing Torsion Box – Modification
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 0006 to 0017 inclusive, MSN 0019 to 0023 inclusive, MSN 0025 to 0031 inclusive, MSN 0033 to 0036 inclusive, MSN 0038 to 0052 inclusive, MSN 0054 to 0059 inclusive, MSN 0061 to 0090 inclusive, MSN 0092 to 0096 inclusive, MSN 0098 to 0101 inclusive, MSN 0103, MSN 0105 to 0117 inclusive, MSN 0119 to 0128 inclusive, MSN 0130 to 0184 inclusive, MSN 0186 to 0195 inclusive, MSN 0197 to 0211 inclusive, MSN 0213 to 0244 inclusive, MSN 0247 to 0249 inclusive, MSN 0251, and MSN 0253 to 0255 inclusive.
ISSUED BY
EASA
AD NO.
2022-11-19
SUBJECT
Joint Aircraft System Component (JASC) Code: 2800 Aircraft Fuel System and 7900 Engine Oil System (Airframe).
APPLICABILITY
This AD applies to Bell Textron Inc. Model 212, 412, 412CF, and 412EP helicopters, certificated in any category, with an engine oil check valve part number (P/N) 209-062-520-001 or fuel check valve P/N 209-062-607-001 manufactured by Circor Aerospace that: (1) Is marked “Circle Seal” and “CORONA CA,” except not a check valve marked with “TQL,” and (2) Has a manufacturing date code of, or prior to, “9/11” (September 2011), or does not have a manufacturing date code, installed.
ISSUED BY
FAA
AD NO.
2022-0098
SUBJECT
ATA – Aircraft Flight Manual – Section Limitations / Normal Procedures – Amendment ATA 27 – Flight Controls – Master Minimum Equipment List – Amendment / Primary Flight Control Computers – Modification (Software Update)
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers, on which Airbus modification (mod) 115496 has been embodied in production, or Airbus Service Bulletin (SB) A350-42-P017 at original issue, Revision 01 or Revision 02 has been embodied in service, except those on which Airbus mod 117819 has been embodied in production.
ISSUED BY
EASA
AD NO.
2022-0097
SUBJECT
ATA 25 – Equipment / Furnishings – Instrument Flight Rules Screens – Removal
APPLICABILITY
EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 P3, EC635 T1, EC635 T2+ and EC635 T3 helicopters, all variants, all serial numbers;
ISSUED BY
EASA
AD NO.
2022-0096
SUBJECT
ATA – Aircraft Flight Manual / Section Limitations – Amendment ATA 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.
CF-2022-29
SUBJECT
Landing Gear – Main Landing Gear (MLG) and Doors – Forward Door Linkage Sleeves Missing Greasing Grooves
APPLICABILITY
De Havilland Aircraft of Canada Limited (formerly Bombardier Inc.) model DHC-8-401 and -402 aeroplanes, serial numbers 4001, 4003 and subsequent.
ISSUED BY
Transport Canada
AD NO.
2022-0094
SUBJECT
ATA 36 – Pneumatic – Air Conditioning / Engine Bleed Air System – Software Update ATA – Airplane Flight Manual / Master Minimum Equipment List – Air Conditioning / Engine Bleed Air System – Amendment ATA 36 – Pneumatic – Engine Bleed Air Supply Over-pressure Valve – Replacement ATA 30 – Ice and Rain Protection – Anti-ice Control Unit – Replacement
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).
ISSUED BY
EASA
AD NO.
2021-0129R1
SUBJECT
ATA 73 – Engine Fuel & Control – Low Pressure Compressor Case Static P30 Air System – Modification
APPLICABILITY
RB211 Trent 970-84, Trent 972-84 and Trent 972E-84 engines, all serial numbers (ESN). These engines are known to be installed on, but not limited to, Airbus A380 aeroplanes.
ISSUED BY
EASA
AD NO.
2022-0093
SUBJECT
ATA 53 – Fuselage – Fasteners at Frame 96 Stringer 6 and 7 on Right Hand Side – Inspection
APPLICABILITY
Airbus A350-941, manufacturer serial numbers 0216, 0217, 0218, 0219, 0220, 0221, 0223, 0224, 0226, 0227, 0228, 0230, 0231, 0232, 0234, 0235, 0236, 0237, 0238, 0239, 0240, 0243, 0244, 0245, 0246, 0247, 0248, 0249, 0250, 0251, 0254, 0255, 0256, 0257, 0259, 0260, 0261, 0263, 0264, 0265, 0267, 0268, 0269, 0271, 0272, 0273, 0276, 0277, 0278, 0279, 0280, 0281, 0282, 0284, 0287, 0289, 0291, 0292, 0293, 0294, 0295, 0297, 0299, 0300, 0301, 0302, 0303 and 0305.
ISSUED BY
EASA
AD NO.
2022-09-09 CORRECTION
SUBJECT
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, and JASC Code 7250, Turbine Section.
APPLICABILITY
This AD applies to CFM International, S.A. (CFM) LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines.
ISSUED BY
FAA
AD NO.
2022-11-04
SUBJECT
Joint Aircraft System Component (JASC) Code: 5510, Horizontal Stabilizer Structure.
APPLICABILITY
This AD applies to Sikorsky Aircraft Corporation Model S-92A helicopters, certificated in any category, with the following installed: Horizontal stabilizer root fitting FWD (forward root fitting) part number (P/N) 92209-07111-101 or 92070-20125-101; or stabilizer strut fitting P/N 92209- 07403-041 or 92070-20117-041 installed on horizontal stabilizer assembly (stabilizer assembly) P/N 92070-20117-045, 92070-20117-046, 92070-20125-041, 92070-20125-042, 92070-20125-043, 92070-20125-044, 92205-07400-043, 92205-07400-045, or 92205-07400-047.
ISSUED BY
FAA
AD NO.
2022-10-51
SUBJECT
Joint Aircraft System Component (JASC) Code: 2700, Flight Control System.
APPLICABILITY
This AD applies to the helicopters identified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. Note 1 to paragraph (c)(1): Helicopters with an AS350B3e designation are Model AS350B3 helicopters. (2) Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, MBB-BK 117 C-2, MBB-BK 117 D-2, and MBB-BK 117 D-3 helicopters. Note 2 to paragraph (c)(2): Helicopters with an EC135P3H designation are Model EC135P3 helicopters. Helicopters with an EC135T3H designation are Model EC135T3 helicopters. Helicopters with an MBB-BK117 C-2e designation are Model MBB-BK117 C-2 helicopters.
ISSUED BY
FAA
AD NO. SUBJECT APPLICABILITY ISSUED BY
2022-0100 ATA 53 – Fuselage – Belly Fairing Torsion Box – Modification Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 0006 to 0017 inclusive, MSN 0019 to 0023 inclusive, MSN 0025 to 0031 inclusive, MSN 0033 to 0036 inclusive, MSN 0038 to 0052 inclusive, MSN 0054 to 0059 inclusive, MSN 0061 to 0090 inclusive, MSN 0092 to 0096 inclusive, MSN 0098 to 0101 inclusive, MSN 0103, MSN 0105 to 0117 inclusive, MSN 0119 to 0128 inclusive, MSN 0130 to 0184 inclusive, MSN 0186 to 0195 inclusive, MSN 0197 to 0211 inclusive, MSN 0213 to 0244 inclusive, MSN 0247 to 0249 inclusive, MSN 0251, and MSN 0253 to 0255 inclusive.
EASA
2022-11-19 Joint Aircraft System Component (JASC) Code: 2800 Aircraft Fuel System and 7900 Engine Oil System (Airframe). This AD applies to Bell Textron Inc. Model 212, 412, 412CF, and 412EP helicopters, certificated in any category, with an engine oil check valve part number (P/N) 209-062-520-001 or fuel check valve P/N 209-062-607-001 manufactured by Circor Aerospace that: (1) Is marked “Circle Seal” and “CORONA CA,” except not a check valve marked with “TQL,” and (2) Has a manufacturing date code of, or prior to, “9/11” (September 2011), or does not have a manufacturing date code, installed.
FAA
2022-0098 ATA – Aircraft Flight Manual – Section Limitations / Normal Procedures – Amendment ATA 27 – Flight Controls – Master Minimum Equipment List – Amendment / Primary Flight Control Computers – Modification (Software Update) Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers, on which Airbus modification (mod) 115496 has been embodied in production, or Airbus Service Bulletin (SB) A350-42-P017 at original issue, Revision 01 or Revision 02 has been embodied in service, except those on which Airbus mod 117819 has been embodied in production.
EASA
2022-0097 ATA 25 – Equipment / Furnishings – Instrument Flight Rules Screens – Removal EC135 P1, EC135 P2, EC135 P2+, EC135 P3, EC135 T1, EC135 T2, EC135 T2+, EC135 T3, EC635 P2+, EC635 P3, EC635 T1, EC635 T2+ and EC635 T3 helicopters, all variants, all serial numbers;
EASA
2022-0096 ATA – Aircraft Flight Manual / Section Limitations – Amendment ATA 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
CF-2022-29 Landing Gear – Main Landing Gear (MLG) and Doors – Forward Door Linkage Sleeves Missing Greasing Grooves De Havilland Aircraft of Canada Limited (formerly Bombardier Inc.) model DHC-8-401 and -402 aeroplanes, serial numbers 4001, 4003 and subsequent.
Transport Canada
2022-0094 ATA 36 – Pneumatic – Air Conditioning / Engine Bleed Air System – Software Update ATA – Airplane Flight Manual / Master Minimum Equipment List – Air Conditioning / Engine Bleed Air System – Amendment ATA 36 – Pneumatic – Engine Bleed Air Supply Over-pressure Valve – Replacement ATA 30 – Ice and Rain Protection – Anti-ice Control Unit – Replacement Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN).
EASA
2021-0129R1 ATA 73 – Engine Fuel & Control – Low Pressure Compressor Case Static P30 Air System – Modification RB211 Trent 970-84, Trent 972-84 and Trent 972E-84 engines, all serial numbers (ESN). These engines are known to be installed on, but not limited to, Airbus A380 aeroplanes.
EASA
2022-0093 ATA 53 – Fuselage – Fasteners at Frame 96 Stringer 6 and 7 on Right Hand Side – Inspection Airbus A350-941, manufacturer serial numbers 0216, 0217, 0218, 0219, 0220, 0221, 0223, 0224, 0226, 0227, 0228, 0230, 0231, 0232, 0234, 0235, 0236, 0237, 0238, 0239, 0240, 0243, 0244, 0245, 0246, 0247, 0248, 0249, 0250, 0251, 0254, 0255, 0256, 0257, 0259, 0260, 0261, 0263, 0264, 0265, 0267, 0268, 0269, 0271, 0272, 0273, 0276, 0277, 0278, 0279, 0280, 0281, 0282, 0284, 0287, 0289, 0291, 0292, 0293, 0294, 0295, 0297, 0299, 0300, 0301, 0302, 0303 and 0305.
EASA
2022-09-09 CORRECTION Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section, and JASC Code 7250, Turbine Section. This AD applies to CFM International, S.A. (CFM) LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A model turbofan engines.
FAA
2022-11-04 Joint Aircraft System Component (JASC) Code: 5510, Horizontal Stabilizer Structure. This AD applies to Sikorsky Aircraft Corporation Model S-92A helicopters, certificated in any category, with the following installed: Horizontal stabilizer root fitting FWD (forward root fitting) part number (P/N) 92209-07111-101 or 92070-20125-101; or stabilizer strut fitting P/N 92209- 07403-041 or 92070-20117-041 installed on horizontal stabilizer assembly (stabilizer assembly) P/N 92070-20117-045, 92070-20117-046, 92070-20125-041, 92070-20125-042, 92070-20125-043, 92070-20125-044, 92205-07400-043, 92205-07400-045, or 92205-07400-047.
FAA
2022-10-51 Joint Aircraft System Component (JASC) Code: 2700, Flight Control System. This AD applies to the helicopters identified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. Note 1 to paragraph (c)(1): Helicopters with an AS350B3e designation are Model AS350B3 helicopters. (2) Airbus Helicopters Deutschland GmbH (AHD) Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, EC135T3, MBB-BK 117 C-2, MBB-BK 117 D-2, and MBB-BK 117 D-3 helicopters. Note 2 to paragraph (c)(2): Helicopters with an EC135P3H designation are Model EC135P3 helicopters. Helicopters with an EC135T3H designation are Model EC135T3 helicopters. Helicopters with an MBB-BK117 C-2e designation are Model MBB-BK117 C-2 helicopters.
FAA

Contact

NoEnquiry TopicEmail Point of Contact
1Aircraft Registration and De-Registration[email protected]
2Certification 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]
3Certification of Airworthiness for Air Operator Certificate (AOC) Holders[email protected]
4Certification of Airworthiness for Non-Air Operator Certificate (Non-AOC) Holders (I.E. GA Aircraft)[email protected]
5Certification of Approved Maintenance Organisation (AMO)[email protected]
6Any Other Matters Not Covered Above[email protected]