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.
2023–13–11
SUBJECT
Air Transport Association (ATA) of America Code 35, Oxygen.
APPLICABILITY
This AD applies to AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblies having part number (P/N) 89794077, 89794015, 891511–14, 806835–01, 807982–01, 808433–01, or 891311–14; and oxygen valve assemblies (body and gage assemblies) having P/N 807206–01. These assemblies might be installed on, but not limited to, the aircraft identified in paragraphs (c)(1) through (12) of this AD, certificated in any category. (1) Airbus SAS Model A300 B2–1A, B2–1C, B2K–3C, B2–203, B4–2C, B4–103, and B4–203 airplanes. (2) Airbus SAS Model A300 B4–601, B4–603, B4–620, B4–622, B4–605R, B4–622R, F4–605R, F4– 622R, and C4–605R Variant F airplanes. (3) Airbus SAS Model A310–203, –204, –221, –222, –304, –322, –324, and –325 airplanes. (4) Airbus SAS Model A318–111, –112, –121, and –122 airplanes. (5) Airbus SAS Model A319–111, –112, –113, –114, –115, –131, –132, –133, and –151N airplanes. (6) Airbus SAS Model A320–211, –212, –214, –216, –231, –232, –233, –251N, –252N, –253N, –271N, –272N, and –273N airplanes. (7) Airbus SAS Model A321–111, –112, –131, –211, –212, –213, –231, –232, –251N, –252N, –253N, – 271N, –272N, –251NX, –252NX, –253NX, –271NX, and –272NX airplanes. (8) Airbus SAS Model A330–201, –202, –203, –223, –243, –301, –302, –303, –321, –322, –323, – 341, –342, –343, and –941 airplanes. (9) Airbus Model A340–211, –212, –213, –311, –312, –313, –541, and –642 airplanes. (10) ATR—GIE Avions de Transport Régional Model ATR42–200, –300, –320, and –500 airplanes. (11) ATR—GIE Avions de Transport Régional Model ATR72–101, –102, –201, –202, –211, –212, and – 212A airplanes. (12) The Boeing Company Model 747–8 series airplanes.
ISSUED BY
FAA
AD NO.
2023–13–12
SUBJECT
Air Transport Association (ATA) of America Code 35, Oxygen
APPLICABILITY
This AD applies to all The Boeing Company Model 737–100, 737–200, 737–200C, 737–300, 737–400, 737–500, 737–600, 737–700, 737–700C, 737–800, 737–900, 737–900ER, 757–200, 757–200PF, 757–200CB, 757–300, 767–200, 767–300, 767–300F, and 767–400ER series airplanes, certificated in any category.
ISSUED BY
FAA
AD NO.
2023-0157
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 – System Equipment Maintenance Requirements – Amendment
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers
ISSUED BY
EASA
AD NO.
G-2023-0005-E
SUBJECT
ATA 28 – Fuel – Fuel Cylinders (for balloons) – Withdrawal from Service
APPLICABILITY
All balloons equipped with fuel cylinders Part Number CB2990 Issue A (Alugas) having serial numbers: OC25001 to OC25202 QI14001 to QI14496 Note: This serial number range covers all CB2990 Issue A (Alugas) cylinders. CB2990 Issue B (Alugas) cylinders are not affected by this Airworthiness Directive. These fuel cylinders are known to be installed on, but not limited to, hot-air balloons and airships manufactured by Cameron Balloons Ltd, Colt Balloons, Lindstrand Balloons Ltd (LBL), Lindstrand Hot Air Balloons Ltd, Sky Balloons, Thunder Balloons, and Thunder & Colt.
ISSUED BY
Transport Canada
AD NO.
2022-0120R2
SUBJECT
ATA 25 – Equiment / 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.
2022-0111R1
SUBJECT
ATA 57 – Wings – Overwing Panel / Lug Attachment – Inspection
APPLICABILITY
Airbus A319-115, A320-214, A320-216, A320-232, A320-251N, A320-271N, A321-211, A321-213, A321-231, A321-251N, A321-251NX, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX and A321-272N aeroplanes, manufacturer serial numbers (MSN) as listed in Appendix 1 of this AD.
ISSUED BY
EASA
AD NO.
2023-0153
SUBJECT
ATA 53 – Fuselage – Cargo Door Frame Attachment Drillings – Inspection
APPLICABILITY
Airbus A320-214, A320-216, A320-251N, A320-271N and A321-253NX aeroplanes, manufacturer serial numbers 8781, 8998, 9015, 9036, 9049, 9068, 9077, 9130, 9175, 9197, 9200, 9211, 9216, 9246, 9252, 9253, 9254, 9264, 9273, 9287, 9300, 9306, 9313, 9316, 9317, 9328, 9329, 9331, 9332, 9341, 9343, 9354, 9358, 9363, 9373, 9378, 9384, 9391, 9394, 9428, 9431, 9439, 9446, 9453, 9454, 9457, 9465, 9473, 9482, 9526, 9559, 9574, 9590, 9595, 10019 and 10044.
ISSUED BY
EASA
AD NO.
2023-0151
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – 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 and A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2023-0150
SUBJECT
ATA 53 – Fuselage – Crossbeam Splicing at Frames 16 and 20 – Inspection
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, 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, except: – aeroplanes on which Airbus modification (mod) 161255 was embodied in production; – A318 aeroplanes on which Airbus mod 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; and – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production.
ISSUED BY
EASA
AD NO.
2023-0106R1
SUBJECT
ATA 28 – Fuel – Fuel Pump – Inspection / Replacement
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 and A321-232 aeroplanes, all manufacturer serial numbers. Note 1: The applicability of the AD and the applicability of service documents issued by the type certificate holder may vary, while the applicability of the AD is the binding one.
ISSUED BY
EASA
AD NO.
2023-0138
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 / Certification Maintenance Requirements – 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 and A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2023-0136
SUBJECT
ATA 36 – Pneumatic – Overheat Detection System Sensing Elements – 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 and A340-313 aeroplanes, all MSN.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2023–13–11 | Air Transport Association (ATA) of America Code 35, Oxygen. | This AD applies to AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblies having part number (P/N) 89794077, 89794015, 891511–14, 806835–01, 807982–01, 808433–01, or 891311–14; and oxygen valve assemblies (body and gage assemblies) having P/N 807206–01. These assemblies might be installed on, but not limited to, the aircraft identified in paragraphs (c)(1) through (12) of this AD, certificated in any category. (1) Airbus SAS Model A300 B2–1A, B2–1C, B2K–3C, B2–203, B4–2C, B4–103, and B4–203 airplanes. (2) Airbus SAS Model A300 B4–601, B4–603, B4–620, B4–622, B4–605R, B4–622R, F4–605R, F4– 622R, and C4–605R Variant F airplanes. (3) Airbus SAS Model A310–203, –204, –221, –222, –304, –322, –324, and –325 airplanes. (4) Airbus SAS Model A318–111, –112, –121, and –122 airplanes. (5) Airbus SAS Model A319–111, –112, –113, –114, –115, –131, –132, –133, and –151N airplanes. (6) Airbus SAS Model A320–211, –212, –214, –216, –231, –232, –233, –251N, –252N, –253N, –271N, –272N, and –273N airplanes. (7) Airbus SAS Model A321–111, –112, –131, –211, –212, –213, –231, –232, –251N, –252N, –253N, – 271N, –272N, –251NX, –252NX, –253NX, –271NX, and –272NX airplanes. (8) Airbus SAS Model A330–201, –202, –203, –223, –243, –301, –302, –303, –321, –322, –323, – 341, –342, –343, and –941 airplanes. (9) Airbus Model A340–211, –212, –213, –311, –312, –313, –541, and –642 airplanes. (10) ATR—GIE Avions de Transport Régional Model ATR42–200, –300, –320, and –500 airplanes. (11) ATR—GIE Avions de Transport Régional Model ATR72–101, –102, –201, –202, –211, –212, and – 212A airplanes. (12) The Boeing Company Model 747–8 series airplanes. |
FAA
|
| 2023–13–12 | Air Transport Association (ATA) of America Code 35, Oxygen | This AD applies to all The Boeing Company Model 737–100, 737–200, 737–200C, 737–300, 737–400, 737–500, 737–600, 737–700, 737–700C, 737–800, 737–900, 737–900ER, 757–200, 757–200PF, 757–200CB, 757–300, 767–200, 767–300, 767–300F, and 767–400ER series airplanes, certificated in any category. |
FAA
|
| 2023-0157 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 – System Equipment Maintenance Requirements – Amendment | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers |
EASA
|
| G-2023-0005-E | ATA 28 – Fuel – Fuel Cylinders (for balloons) – Withdrawal from Service | All balloons equipped with fuel cylinders Part Number CB2990 Issue A (Alugas) having serial numbers: OC25001 to OC25202 QI14001 to QI14496 Note: This serial number range covers all CB2990 Issue A (Alugas) cylinders. CB2990 Issue B (Alugas) cylinders are not affected by this Airworthiness Directive. These fuel cylinders are known to be installed on, but not limited to, hot-air balloons and airships manufactured by Cameron Balloons Ltd, Colt Balloons, Lindstrand Balloons Ltd (LBL), Lindstrand Hot Air Balloons Ltd, Sky Balloons, Thunder Balloons, and Thunder & Colt. |
Transport Canada
|
| 2022-0120R2 | ATA 25 – Equiment / 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
|
| 2022-0111R1 | ATA 57 – Wings – Overwing Panel / Lug Attachment – Inspection | Airbus A319-115, A320-214, A320-216, A320-232, A320-251N, A320-271N, A321-211, A321-213, A321-231, A321-251N, A321-251NX, A321-252NX, A321-253N, A321-253NX, A321-271N, A321-271NX and A321-272N aeroplanes, manufacturer serial numbers (MSN) as listed in Appendix 1 of this AD. |
EASA
|
| 2023-0153 | ATA 53 – Fuselage – Cargo Door Frame Attachment Drillings – Inspection | Airbus A320-214, A320-216, A320-251N, A320-271N and A321-253NX aeroplanes, manufacturer serial numbers 8781, 8998, 9015, 9036, 9049, 9068, 9077, 9130, 9175, 9197, 9200, 9211, 9216, 9246, 9252, 9253, 9254, 9264, 9273, 9287, 9300, 9306, 9313, 9316, 9317, 9328, 9329, 9331, 9332, 9341, 9343, 9354, 9358, 9363, 9373, 9378, 9384, 9391, 9394, 9428, 9431, 9439, 9446, 9453, 9454, 9457, 9465, 9473, 9482, 9526, 9559, 9574, 9590, 9595, 10019 and 10044. |
EASA
|
| 2023-0151 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – 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 and A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2023-0150 | ATA 53 – Fuselage – Crossbeam Splicing at Frames 16 and 20 – Inspection | 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, 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, except: – aeroplanes on which Airbus modification (mod) 161255 was embodied in production; – A318 aeroplanes on which Airbus mod 39195 was embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 was embodied in service; and – A319 aeroplanes on which Airbus mod 28238, mod 28162 and mod 28342 were embodied in production. |
EASA
|
| 2023-0106R1 | ATA 28 – Fuel – Fuel Pump – Inspection / Replacement | 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 and A321-232 aeroplanes, all manufacturer serial numbers. Note 1: The applicability of the AD and the applicability of service documents issued by the type certificate holder may vary, while the applicability of the AD is the binding one. |
EASA
|
| 2023-0138 | ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 / Certification Maintenance Requirements – 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 and A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2023-0136 | ATA 36 – Pneumatic – Overheat Detection System Sensing Elements – 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 and A340-313 aeroplanes, all MSN. |
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] |