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 : 249
AD NO.
2024-06-01
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, -900 and -900ERairplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-53A1407 RB, dated December 20, 2022. (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.
2024-0068
SUBJECT
ATA 53 – Fuselage – Lateral Cockpit Window Frame Upper Stiffener – 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 (MSN), except: – A318 aeroplanes on which Airbus modification (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 28162, mod 28238 and mod 28342 were embodied in production.
ISSUED BY
EASA
AD NO.
2024-0067-E
SUBJECT
ATA 72 – Engine – Life Limited Parts – Replacement
APPLICABILITY
CFM56-2, CFM56-2A, CFM56-2B, CFM56-3, CFM56-3B and CFM56-3C engines, serial numbers (s/n); CFM56-5, CFM56-5-A1/F, CFM56-5A3, CFM56-5A4, CFM56-5A4/F, CFM56-5A5 and CFM56-5A5/F engines, all s/n; CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2, CFM56-5B2/2P, CFM56-5B2/3, CFM56-5B2/P, CFM56-5B3/2P, CFM56-5B3/2P1, CFM56-5B3/3, CFM56-5B3/3B1, CFM56-5B3/P, CFM56-5B3/P1, CFM56-5B4, CFM56-5B4/2P, CFM56-5B4/2P1, CFM56-5B4/3, CFM56-5B4/3B1, CFM56-5B4/P, CFM56-5B4/P1, CFM56-5B5, CFM56-5B5/3, CFM56-5B5/P, CFM56-5B6, CFM56-5B6/2P, CFM56-5B6/3, CFM56-5B6/P, CFM56-5B7, CFM56-5B7/3, CFM56-5B7/P, CFM56-5B8/3, CFM56-5B8/P, CFM56-5B9/2P, CFM56-5B9/3 and CFM56-5B9/P engines, all s/n; CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F, CFM56-5C2/F4, CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C2/P, CFM56-5C3/F, CFM56-5C3/F4, CFM56-5C3/G, CFM56-5C3/G4, CFM56-5C3/P, CFM56-5C4, CFM56-5C4/1, CFM56-5C4/P and CFM56-5C4/1P engines, all s/n; and CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3, CFM56-7B20E, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B22/B1, CFM56-7B22E, CFM56-7B22E/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B24/B1, CFM56-7B24E, CFM56-7B24E/B1, CFM56-7B26, CFM56-7B26/2, CFM56-7B26/3, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B26/3B2F, CFM56-7B26/3F, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B26E, CFM56-7B26E/B1, CFM56-7B26E/B2, CFM56-7B26E/B2F, CFM56-7B26E/F, CFM56-7B27, CFM56-7B27/2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B1F, CFM56-7B27/3B3, CFM56-7B27/3F, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B27A, CFM56-7B27A/3, CFM56-7B27AE, CFM56-7B27E, CFM56-7B27E/B1, CFM56-7B27E/B1F, CFM56-7B27E/B3 and CFM56-7B27E/F engines, all s/n.
ISSUED BY
EASA
AD NO.
2024-0066
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – 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.
2021-0217R1
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment
APPLICABILITY
Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes.
ISSUED BY
EASA
AD NO.
2024–05–05
SUBJECT
Air Transport Association (ATA) of America Code 26, Fire Protection.
APPLICABILITY
This AD applies to all ATR–GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Model ATR42–200, –300, –320, and –500 airplanes. (2) Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes.
ISSUED BY
EASA
AD NO.
2024-0062
SUBJECT
ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment
APPLICABILITY
Trent 1000 engines, models Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G and Trent 1000-H engines, all serial numbers.
ISSUED BY
EASA
AD NO.
2024-0060
SUBJECT
ATA 54 – Nacelles / Pylons – Air Intake Cowl – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2013-0038-CN
SUBJECT
ATA 72 – CANCELLED: Engine – Air Guide Tube / Phonic Ring – Inspection
APPLICABILITY
RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, serial number (ESN) 41062, 41065, 41073, 41095, 41117, 41128, 41134, 41146, 41149, 41160, 41170, 41206, 41215, 41216, 41224, 41225, 41237, 41242, 41244, 41250, 41256, 41264 and 41266.
ISSUED BY
EASA
AD NO.
2024-0058
SUBJECT
ATA 36 – Pneumatic – Precooler Exchanger – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0057
SUBJECT
ATA 25 – Equipment/Furnishings – Escape Slide and Offwing Slide Inflation Reservoir Venting Holes – Inspection / Replacement
APPLICABILITY
A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0055-CN
SUBJECT
ATA 73 – CANCELLED: Engine Fuel and Control – Fuel Manifold to Burner Fuel Tube Assembly – Replacement
APPLICABILITY
RB211 Trent 768-60, Trent 772-60, Trent 772B-60 and Trent 772C-60 engines, all serial numbers.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-06-01 | Air Transport Association (ATA) of America Code 53, Fuselage. | (1) This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, -900 and -900ERairplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 737-53A1407 RB, dated December 20, 2022. (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
|
| 2024-0068 | ATA 53 – Fuselage – Lateral Cockpit Window Frame Upper Stiffener – 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 (MSN), except: – A318 aeroplanes on which Airbus modification (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 28162, mod 28238 and mod 28342 were embodied in production. |
EASA
|
| 2024-0067-E | ATA 72 – Engine – Life Limited Parts – Replacement | CFM56-2, CFM56-2A, CFM56-2B, CFM56-3, CFM56-3B and CFM56-3C engines, serial numbers (s/n); CFM56-5, CFM56-5-A1/F, CFM56-5A3, CFM56-5A4, CFM56-5A4/F, CFM56-5A5 and CFM56-5A5/F engines, all s/n; CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2, CFM56-5B2/2P, CFM56-5B2/3, CFM56-5B2/P, CFM56-5B3/2P, CFM56-5B3/2P1, CFM56-5B3/3, CFM56-5B3/3B1, CFM56-5B3/P, CFM56-5B3/P1, CFM56-5B4, CFM56-5B4/2P, CFM56-5B4/2P1, CFM56-5B4/3, CFM56-5B4/3B1, CFM56-5B4/P, CFM56-5B4/P1, CFM56-5B5, CFM56-5B5/3, CFM56-5B5/P, CFM56-5B6, CFM56-5B6/2P, CFM56-5B6/3, CFM56-5B6/P, CFM56-5B7, CFM56-5B7/3, CFM56-5B7/P, CFM56-5B8/3, CFM56-5B8/P, CFM56-5B9/2P, CFM56-5B9/3 and CFM56-5B9/P engines, all s/n; CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F, CFM56-5C2/F4, CFM56-5C2/G, CFM56-5C2/G4, CFM56-5C2/P, CFM56-5C3/F, CFM56-5C3/F4, CFM56-5C3/G, CFM56-5C3/G4, CFM56-5C3/P, CFM56-5C4, CFM56-5C4/1, CFM56-5C4/P and CFM56-5C4/1P engines, all s/n; and CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3, CFM56-7B20E, CFM56-7B22, CFM56-7B22/2, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B22/B1, CFM56-7B22E, CFM56-7B22E/B1, CFM56-7B24, CFM56-7B24/2, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B24/B1, CFM56-7B24E, CFM56-7B24E/B1, CFM56-7B26, CFM56-7B26/2, CFM56-7B26/3, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B26/3B2F, CFM56-7B26/3F, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B26E, CFM56-7B26E/B1, CFM56-7B26E/B2, CFM56-7B26E/B2F, CFM56-7B26E/F, CFM56-7B27, CFM56-7B27/2, CFM56-7B27/3, CFM56-7B27/3B1, CFM56-7B27/3B1F, CFM56-7B27/3B3, CFM56-7B27/3F, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B27A, CFM56-7B27A/3, CFM56-7B27AE, CFM56-7B27E, CFM56-7B27E/B1, CFM56-7B27E/B1F, CFM56-7B27E/B3 and CFM56-7B27E/F engines, all s/n. |
EASA
|
| 2024-0066 | ATA 05 – Time Limits / Maintenance Checks – Safe Life Airworthiness Limitations Items – ALS Part 1 – 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
|
| 2021-0217R1 | ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment | Trent XWB-75, Trent XWB-79, Trent XWB-79B and Trent XWB-84 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A350 aeroplanes. |
EASA
|
| 2024–05–05 | Air Transport Association (ATA) of America Code 26, Fire Protection. | This AD applies to all ATR–GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category. (1) Model ATR42–200, –300, –320, and –500 airplanes. (2) Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes. |
EASA
|
| 2024-0062 | ATA 05 – Time Limits / Maintenance Checks – Time Limits Manual / Maintenance Programme – Amendment | Trent 1000 engines, models Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G and Trent 1000-H engines, all serial numbers. |
EASA
|
| 2024-0060 | ATA 54 – Nacelles / Pylons – Air Intake Cowl – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2013-0038-CN | ATA 72 – CANCELLED: Engine – Air Guide Tube / Phonic Ring – Inspection | RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, serial number (ESN) 41062, 41065, 41073, 41095, 41117, 41128, 41134, 41146, 41149, 41160, 41170, 41206, 41215, 41216, 41224, 41225, 41237, 41242, 41244, 41250, 41256, 41264 and 41266. |
EASA
|
| 2024-0058 | ATA 36 – Pneumatic – Precooler Exchanger – Inspection | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0057 | ATA 25 – Equipment/Furnishings – Escape Slide and Offwing Slide Inflation Reservoir Venting Holes – Inspection / Replacement | A321-251NX, A321-252NX, A321-253NX, A321-271NX and A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0055-CN | ATA 73 – CANCELLED: Engine Fuel and Control – Fuel Manifold to Burner Fuel Tube Assembly – Replacement | RB211 Trent 768-60, Trent 772-60, Trent 772B-60 and Trent 772C-60 engines, all serial numbers. |
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] |