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.
2022-0054
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.
2022-0049
SUBJECT
ATA 32 – Landing Gear – Nose and Main Landing Gear Main Fittings and Main Landing Gear Sliding Pistons – Replacement
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 and A340-313 aeroplanes, all MSN.
ISSUED BY
EASA
AD NO.
2022-0045
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.
2022-0039
SUBJECT
ATA 27 – Flight Controls – Trimmable Horizontal Stabilizer Actuator / Electric Load Sensing Device – 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, and A330-941 aeroplanes, all manufacturer serial numbers (MSN) up to MSN 1919 inclusive, except MSN 1915; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN.
ISSUED BY
EASA
AD NO.
2022-0036
SUBJECT
ATA 53 – Fuselage – Tailboom Attachment – Inspection / Replacement
APPLICABILITY
212 helicopters, serial numbers (s/n) 30501 to 30999 inclusive, 31101 to 31311 inclusive, 32101 to 32142 inclusive and 35001 to 35103 inclusive; and 412 and 412EP helicopters, s/n 33001 to 33213 inclusive, 34001 to 34036 inclusive, 36001 to 36687 inclusive, 36689 to 36999 inclusive, 37002 to 37018 inclusive, 37021 to 37051 inclusive, 38001 and 39101 to 39103 inclusive.
ISSUED BY
EASA
AD NO.
2011-0072-CN
SUBJECT
ATA 25 – CANCELLED: Equipment & Furnishings – Emergency Flotation Gear Attachment Brackets – Inspection / Replacement
APPLICABILITY
AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers (s/n), and AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all s/n, if equipped with fixed parts of the emergency flotation gear.
ISSUED BY
EASA
AD NO.
CF-2022-09
SUBJECT
ATA 21 – Air Conditioning – Avionics Cooling – Integrated Flight Cabinet (IFC) Failure Due to High Temperatures
APPLICABILITY
De Havilland Aircraft of Canada Limited (formerly Bombardier Inc.) model DHC-8-401 and -402 aeroplanes
ISSUED BY
TCCA
AD NO.
2022-0032
SUBJECT
ATA 32 – Landing Gear – Braking and Steering Control Unit – Replacement / Master Minimum Equipment List – Amendment
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, A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2022-0033
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment
APPLICABILITY
BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and BR700-710D5-21 engines, all serial numbers. These engines are known to be installed on, but not limited to, Bombardier BD-700-1A10 and BD-700-1A11 aeroplanes, and Gulfstream GV (commercial designation G500) and GV-SP (commercial designation G550) aeroplanes.
ISSUED BY
EASA
AD NO.
2020-0227R1
SUBJECT
ATA 92 – Electrical Routing – Electrical Harness Routes 1M and 1S-1V – Modification
APPLICABILITY
ATR 72-212A aeroplanes, manufacturer serial numbers (MSN) 1165 to 1627 inclusive, except those on which ATR modification (mod) 10052 has been embodied in production, and except MSN 1589, 1591, 1592 and 1595.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 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
|
| 2022-0049 | ATA 32 – Landing Gear – Nose and Main Landing Gear Main Fittings and Main Landing Gear Sliding Pistons – Replacement | 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 and A340-313 aeroplanes, all MSN. |
EASA
|
| 2022-0045 | ATA – Aircraft Flight Manual – Performance Database – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0039 | ATA 27 – Flight Controls – Trimmable Horizontal Stabilizer Actuator / Electric Load Sensing Device – 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, and A330-941 aeroplanes, all manufacturer serial numbers (MSN) up to MSN 1919 inclusive, except MSN 1915; and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN. |
EASA
|
| 2022-0036 | ATA 53 – Fuselage – Tailboom Attachment – Inspection / Replacement | 212 helicopters, serial numbers (s/n) 30501 to 30999 inclusive, 31101 to 31311 inclusive, 32101 to 32142 inclusive and 35001 to 35103 inclusive; and 412 and 412EP helicopters, s/n 33001 to 33213 inclusive, 34001 to 34036 inclusive, 36001 to 36687 inclusive, 36689 to 36999 inclusive, 37002 to 37018 inclusive, 37021 to 37051 inclusive, 38001 and 39101 to 39103 inclusive. |
EASA
|
| 2011-0072-CN | ATA 25 – CANCELLED: Equipment & Furnishings – Emergency Flotation Gear Attachment Brackets – Inspection / Replacement | AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers (s/n), and AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all s/n, if equipped with fixed parts of the emergency flotation gear. |
EASA
|
| CF-2022-09 | ATA 21 – Air Conditioning – Avionics Cooling – Integrated Flight Cabinet (IFC) Failure Due to High Temperatures | De Havilland Aircraft of Canada Limited (formerly Bombardier Inc.) model DHC-8-401 and -402 aeroplanes |
TCCA
|
| 2022-0032 | ATA 32 – Landing Gear – Braking and Steering Control Unit – Replacement / Master Minimum Equipment List – Amendment | 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, A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2022-0033 | ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment | BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and BR700-710D5-21 engines, all serial numbers. These engines are known to be installed on, but not limited to, Bombardier BD-700-1A10 and BD-700-1A11 aeroplanes, and Gulfstream GV (commercial designation G500) and GV-SP (commercial designation G550) aeroplanes. |
EASA
|
| 2020-0227R1 | ATA 92 – Electrical Routing – Electrical Harness Routes 1M and 1S-1V – Modification | ATR 72-212A aeroplanes, manufacturer serial numbers (MSN) 1165 to 1627 inclusive, except those on which ATR modification (mod) 10052 has been embodied in production, and except MSN 1589, 1591, 1592 and 1595. |
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] |
