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.
2024-24-11
SUBJECT
Joint Aircraft System Component (JASC) Code 7603, Power Lever.
APPLICABILITY
This AD applies to Cirrus Design Corporation Model SR20, SR22, and SR22T airplanes, certificatedin any category, that are equipped with upper power lever part number (P/N) 19181-001, 19181-002, or 46505-001.
ISSUED BY
FAA
AD NO.
2024-0235
SUBJECT
ATA 52 – Doors – Rear Passenger Door Latching Mechanism – Inspection / Modification Airplane Flight Manual – Amendment
APPLICABILITY
DA 42, DA 42 M, DA 42 NG, DA 42 M-NG aeroplanes, all serial numbers.
ISSUED BY
EASA
AD NO.
2024-0234
SUBJECT
ATA 54 – Nacelles / Pylons – Pylons Rib 9 – Inspection
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, manufacturer serial numbers as listed in the SB, as defined in this AD.
ISSUED BY
EASA
AD NO.
2024-0232
SUBJECT
ATA 52 – Doors – Door Star Support – Modification
APPLICABILITY
EC 130 B4 helicopters, all serial numbers.
ISSUED BY
EASA
AD NO.
2024-0231
SUBJECT
ATA 25 – Equipment/Furnishings – Cargo Bulkhead Frame 24A Vertical Members – 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, A319-151N, A319-153N, A319-171N, A319-173N, 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, A321-253NY, A321-271N, A321-271NX, A321-272N, and A321-272NX aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-23-01
SUBJECT
Joint Aircraft System Component (JASC) Code: 6300, Main rotor drive system and 6700,Rotorcraft flight control.
APPLICABILITY
This AD applies to Robinson Helicopter Company Model R44 helicopters serial numbers (S/Ns) upto 2480 inclusive and 30001 through 30022 inclusive, and Model R44 II helicopters S/Ns up to14089 inclusive, certificated in any category, with riveted belt tension clutch actuator brackets partnumber A185-1, A185-2, or A185-5 (bracket(s)), installed. Note 1 to paragraph (c): Helicopters with an R44 Cadet designation are Model R44 helicopters. Note 2 to paragraph (c): Brackets attached to the fan scroll housing with screws are notapplicable to this AD.
ISSUED BY
FAA
AD NO.
2024-23-11
SUBJECT
Air Transport Association (ATA) of America Code 27, Flight controls.
APPLICABILITY
This AD applies to The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes, certificatedin any category, as identified in Boeing Alert Requirements Bulletin 737-27A1325 RB, dated July 14,2023.
ISSUED BY
FAA
AD NO.
2024-23-03
SUBJECT
Air Transport Association (ATA) of America Code 27, Flight controls.
APPLICABILITY
This AD applies to The Boeing Company Model 737-300 and -400 series airplanes, certificated inany category, as identified in Boeing Alert Requirements Bulletin 737-22A1399 RB, dated April 13,2023.
ISSUED BY
FAA
AD NO.
2024-0230
SUBJECT
ATA 57 – Wings – Bottom Wing Skin Panel 2 – Inspection
APPLICABILITY
Airbus 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, A321-211, 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.
2024-0201R1
SUBJECT
ATA 57 – Wings – Outer Wing Bottom Buttstrap – Inspections
APPLICABILITY
Airbus 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, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2024-0228
SUBJECT
ATA 25 – Equipment / Furnishings – Hoist – Inspection
APPLICABILITY
AB412, AB412EP, A109E, A109K2, A109S, AB139 and AW139 helicopters, all serial numbers (s/n).
ISSUED BY
EASA
AD NO.
2024-0175 Issued: 06 Sep 2024 [Correction: 28 Nov 2024]
SUBJECT
ATA 72 – Engine – Fuel Nozzle – Replacement
APPLICABILITY
LEAP-1A32 engines installed on Airbus S.A.S. A321-251NX aeroplanes having any of the following aeroplane manufacturing serial number (MSN) 11200, 11420, 11473, 11609, 11698, 11791, 11815, 12136, 12314 or MSN 12370.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2024-24-11 | Joint Aircraft System Component (JASC) Code 7603, Power Lever. | This AD applies to Cirrus Design Corporation Model SR20, SR22, and SR22T airplanes, certificatedin any category, that are equipped with upper power lever part number (P/N) 19181-001, 19181-002, or 46505-001. |
FAA
|
| 2024-0235 | ATA 52 – Doors – Rear Passenger Door Latching Mechanism – Inspection / Modification Airplane Flight Manual – Amendment | DA 42, DA 42 M, DA 42 NG, DA 42 M-NG aeroplanes, all serial numbers. |
EASA
|
| 2024-0234 | ATA 54 – Nacelles / Pylons – Pylons Rib 9 – Inspection | Airbus A350-941 and A350-1041 aeroplanes, manufacturer serial numbers as listed in the SB, as defined in this AD. |
EASA
|
| 2024-0232 | ATA 52 – Doors – Door Star Support – Modification | EC 130 B4 helicopters, all serial numbers. |
EASA
|
| 2024-0231 | ATA 25 – Equipment/Furnishings – Cargo Bulkhead Frame 24A Vertical Members – 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, A319-151N, A319-153N, A319-171N, A319-173N, 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, A321-253NY, A321-271N, A321-271NX, A321-272N, and A321-272NX aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-23-01 | Joint Aircraft System Component (JASC) Code: 6300, Main rotor drive system and 6700,Rotorcraft flight control. | This AD applies to Robinson Helicopter Company Model R44 helicopters serial numbers (S/Ns) upto 2480 inclusive and 30001 through 30022 inclusive, and Model R44 II helicopters S/Ns up to14089 inclusive, certificated in any category, with riveted belt tension clutch actuator brackets partnumber A185-1, A185-2, or A185-5 (bracket(s)), installed. Note 1 to paragraph (c): Helicopters with an R44 Cadet designation are Model R44 helicopters. Note 2 to paragraph (c): Brackets attached to the fan scroll housing with screws are notapplicable to this AD. |
FAA
|
| 2024-23-11 | Air Transport Association (ATA) of America Code 27, Flight controls. | This AD applies to The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes, certificatedin any category, as identified in Boeing Alert Requirements Bulletin 737-27A1325 RB, dated July 14,2023. |
FAA
|
| 2024-23-03 | Air Transport Association (ATA) of America Code 27, Flight controls. | This AD applies to The Boeing Company Model 737-300 and -400 series airplanes, certificated inany category, as identified in Boeing Alert Requirements Bulletin 737-22A1399 RB, dated April 13,2023. |
FAA
|
| 2024-0230 | ATA 57 – Wings – Bottom Wing Skin Panel 2 – Inspection | Airbus 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, A321-211, 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
|
| 2024-0201R1 | ATA 57 – Wings – Outer Wing Bottom Buttstrap – Inspections | Airbus 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, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2024-0228 | ATA 25 – Equipment / Furnishings – Hoist – Inspection | AB412, AB412EP, A109E, A109K2, A109S, AB139 and AW139 helicopters, all serial numbers (s/n). |
EASA
|
| 2024-0175 Issued: 06 Sep 2024 [Correction: 28 Nov 2024] | ATA 72 – Engine – Fuel Nozzle – Replacement | LEAP-1A32 engines installed on Airbus S.A.S. A321-251NX aeroplanes having any of the following aeroplane manufacturing serial number (MSN) 11200, 11420, 11473, 11609, 11698, 11791, 11815, 12136, 12314 or MSN 12370. |
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] |