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.
2022-0074
SUBJECT
ATA 72 – Engine – Transfer Gearbox Module Scavenge Screens – Inspection / Modification
APPLICABILITY
LEAP-1B21, LEAP-1B23, LEAP-1B25, LEAP-1B27, LEAP-1B28, LEAP-1B28B1, LEAP-1B28B2, LEAP-1B28B2C, LEAP-1B28B3, LEAP-1B28BBJ1 and LEAP-1B28BBJ2 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Boeing 737-8, 737-9 and 737-8200 aeroplanes.
ISSUED BY
EASA
AD NO.
2022-0071
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment
APPLICABILITY
LEAP-1B21, LEAP-1B23, LEAP-1B25, LEAP-1B27, LEAP-1B28, LEAP-1B28B1, LEAP-1B28B2, LEAP-1B28B2C, LEAP-1B28B3, LEAP-1B28BBJ1 and LEAP-1B28BBJ2 engines, all serial numbers (s/n).
ISSUED BY
EASA
AD NO.
2022-06-07
SUBJECT
Air Transport Association (ATA) of America Code 53, Fuselage.
APPLICABILITY
This AD applies to The Boeing Company Model 777-200 and -300 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 777-53A0075, Revision 2, dated February 22, 2021.
ISSUED BY
FAA
AD NO.
2014-0213R1
SUBJECT
ATA 53 – Fuselage – Section 19 Upper Cross Fitting Upper Beam Inner Cap Joints – Inspection
APPLICABILITY
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except those on which Airbus modification (mod) 77140 has been embodied in production.
ISSUED BY
EASA
AD NO.
CF-2022-21
SUBJECT
ATA – 55 Stabilizers – Horizontal Stabilizer to Vertical Stabilizer Joint – Non-Conforming Saddle Washer (Radius Filler)
APPLICABILITY
De Havilland Aircraft of Canada Limited (formerly Bombardier Inc.) model DHC-8-401 and -402 aeroplanes, serial numbers 4001 and 4003 through 4633.
ISSUED BY
Transport Canada
AD NO.
2022-0064
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.
2022-0065
SUBJECT
ATA 26 – Fire Protection – Engine Fire Extinguishing Pipes – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers fitted with an affected engine, as defined in this AD.
ISSUED BY
EASA
AD NO.
2022-0057
SUBJECT
ATA 56 – Windows – Windshields – Inspection
APPLICABILITY
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, A330-941 aeroplanes, all manufacturer serial numbers (MSN); and 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.
2022-0055
SUBJECT
ATA 72 – Engine – Intermediate Pressure Compressor Rotor Shaft – Inspection
APPLICABILITY
RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Airbus A330 series aeroplanes.
ISSUED BY
EASA
AD NO.
2022-0054
SUBJECT
ATA – Aircraft Flight Manual – Performance Database – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0053
SUBJECT
ATA 32 – Landing Gear – Skid-Type Landing Gear – Inspection
APPLICABILITY
EC 130 T2 and EC 130 B4 helicopters, all serial numbers (s/n); and EC 120 B helicopters, all s/n.
ISSUED BY
EASA
AD NO.
2022-0051
SUBJECT
ATA 53 – Fuselage – Rear Structure Junction Frame Reinforcement Angles – Inspection
APPLICABILITY
AS 350 B, BA, BB, B1, B2, B3 and D helicopters, and AS 355 E, F, F1, F2 and N helicopters, all serial numbers (s/n), if an affected part, as defined in this AD, is installed, except helicopters on which AH modification (MOD) 073232 has been embodied in production, or AH AS350 Service Bulletin (SB) No. 53.00.58 and AS355 SB No. 53.00.34, as applicable, have been embodied in service. AS 355 NP helicopters, s/n 5747, and s/n 5749 to 5766 inclusive, except helicopters on which AH AS355 SB No. 53.00.34 has been embodied in service.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2022-0074 | ATA 72 – Engine – Transfer Gearbox Module Scavenge Screens – Inspection / Modification | LEAP-1B21, LEAP-1B23, LEAP-1B25, LEAP-1B27, LEAP-1B28, LEAP-1B28B1, LEAP-1B28B2, LEAP-1B28B2C, LEAP-1B28B3, LEAP-1B28BBJ1 and LEAP-1B28BBJ2 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Boeing 737-8, 737-9 and 737-8200 aeroplanes. |
EASA
|
| 2022-0071 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment | LEAP-1B21, LEAP-1B23, LEAP-1B25, LEAP-1B27, LEAP-1B28, LEAP-1B28B1, LEAP-1B28B2, LEAP-1B28B2C, LEAP-1B28B3, LEAP-1B28BBJ1 and LEAP-1B28BBJ2 engines, all serial numbers (s/n). |
EASA
|
| 2022-06-07 | Air Transport Association (ATA) of America Code 53, Fuselage. | This AD applies to The Boeing Company Model 777-200 and -300 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 777-53A0075, Revision 2, dated February 22, 2021. |
FAA
|
| 2014-0213R1 | ATA 53 – Fuselage – Section 19 Upper Cross Fitting Upper Beam Inner Cap Joints – Inspection | Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers (MSN), except those on which Airbus modification (mod) 77140 has been embodied in production. |
EASA
|
| CF-2022-21 | ATA – 55 Stabilizers – Horizontal Stabilizer to Vertical Stabilizer Joint – Non-Conforming Saddle Washer (Radius Filler) | De Havilland Aircraft of Canada Limited (formerly Bombardier Inc.) model DHC-8-401 and -402 aeroplanes, serial numbers 4001 and 4003 through 4633. |
Transport Canada
|
| 2022-0064 | 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
|
| 2022-0065 | ATA 26 – Fire Protection – Engine Fire Extinguishing Pipes – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers fitted with an affected engine, as defined in this AD. |
EASA
|
| 2022-0057 | ATA 56 – Windows – Windshields – Inspection | 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, A330-941 aeroplanes, all manufacturer serial numbers (MSN); and 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
|
| 2022-0055 | ATA 72 – Engine – Intermediate Pressure Compressor Rotor Shaft – Inspection | RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Airbus A330 series aeroplanes. |
EASA
|
| 2022-0054 | ATA – Aircraft Flight Manual – Performance Database – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0053 | ATA 32 – Landing Gear – Skid-Type Landing Gear – Inspection | EC 130 T2 and EC 130 B4 helicopters, all serial numbers (s/n); and EC 120 B helicopters, all s/n. |
EASA
|
| 2022-0051 | ATA 53 – Fuselage – Rear Structure Junction Frame Reinforcement Angles – Inspection | AS 350 B, BA, BB, B1, B2, B3 and D helicopters, and AS 355 E, F, F1, F2 and N helicopters, all serial numbers (s/n), if an affected part, as defined in this AD, is installed, except helicopters on which AH modification (MOD) 073232 has been embodied in production, or AH AS350 Service Bulletin (SB) No. 53.00.58 and AS355 SB No. 53.00.34, as applicable, have been embodied in service. AS 355 NP helicopters, s/n 5747, and s/n 5749 to 5766 inclusive, except helicopters on which AH AS355 SB No. 53.00.34 has been embodied in service. |
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] |
