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.
2021-23-12
SUBJECT
Air Transport Association (ATA) of America Code 31, Indicating/Recording System; 34, Navigation.
APPLICABILITY
This AD applies to all transport and commuter category airplanes equipped with a radio (also known as radar) altimeter. These radio altimeters are installed on various transport and commuter category airplanes including, but not limited to, the airplanes for which the design approval holder is identified in paragraphs (c)(1) through (19) of this AD. (1) The Boeing Company (2) Airbus SAS (3) Bombardier Inc. (4) Embraer S.A. (5) Gulfstream Aerospace Corporation (6) Gulfstream Aerospace LP (7) Textron Aviation Inc. (8) Pilatus Aircraft Limited (9) Fokker Services B.V. (10) Saab AB, Support and Services (11) DeHavilland Aircraft of Canada Limited (12) Airbus Canada Limited Partnership (13) ATR-GIE Avions de Transport Régional (14) Yaborã Ind[uacute]stria Aeronáutica S.A. (15) MHI RJ Aviation ULC (16) BAE Systems (Operations) Limited (17) Lockheed Martin Corporation/Lockheed Martin Aeronautics Company (18) Viking Air Limited (19) Dassault Aviation
ISSUED BY
FAA
AD NO.
2014-0076R3
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, N and NP helicopters, all serial numbers
ISSUED BY
EASA
AD NO.
2020-0249R1
SUBJECT
ATA 31 – Instruments – Angle of Attack Probe and Multi-Function Computers Electrical Routing – Operational Test / Inspection
APPLICABILITY
ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); and ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN.
ISSUED BY
EASA
AD NO.
G-2021-0015
SUBJECT
ATA 32 – Landing Gear – Main Landing Gear / Pintle to Cylinder Interface – Inspection
APPLICABILITY
Jetstream 3100 & 3200 aeroplanes
ISSUED BY
CAA UK
AD NO.
2021-0267
SUBJECT
ATA 55 – Stabilizers – Rudder Hinges – Inspection
APPLICABILITY
P.68 “Victor”, P.68B “Victor”, P.68R “Victor”, P.68C, P.68C-TC, P.68 “Observer”, P.68 “Observer 2” and P.68TC “Observer” aeroplanes, all serial numbers (s/n).
ISSUED BY
EASA
AD NO.
2021-19-17
SUBJECT
Joint Aircraft System Component (JASC) Code: 2500, Cabin Equipment/Furnishings; and 2520, Passenger Compartment Equipment.
APPLICABILITY
Sikorsky Aircraft Corporation Model S-92A helicopters
ISSUED BY
FAA
AD NO.
2021-24-07
SUBJECT
This AD was prompted by a report of a certain procedure in the aircraft maintenance manual (AMM) that incorrectly described a visual inspection of the fire handle. The FAA is issuing this AD to address snap wires made of incorrect material, which, if not detected and corrected, and combined with an engine fire, could lead to a failure of the engine fire handle to operate, possibly resulting in an uncontrolled engine fire and reduced control of the airplane.
APPLICABILITY
This AD applies to the ATR–GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) Emergency AD 2021-0237-E, dated November 4, 2021 (EASA AD 2021-0237-E). (1) Model ATR42-200, -300, -320, and -500 airplanes. (2) Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes.
ISSUED BY
FAA
AD NO.
2021-0259 C
SUBJECT
ATA 53 – Fuselage – Tail Gearbox Fitting – Inspection / Replacement
APPLICABILITY
AB139 and AW139 helicopters, all serial numbers.
ISSUED BY
EASA
AD NO.
2021-0261
SUBJECT
“ATA 05 – Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – Amendment”
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, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
AD NO.
2021-20-09
SUBJECT
This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address fatigue cracking and damage in principal structural elements, which could result in reduced structural integrity of the airplane.
APPLICABILITY
This AD applies to ATR-GIE Avions de Transport Régional Model ATR72-101, -102, -201, – 202, -211, -212, and -212A airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 9, 2020.
ISSUED BY
FAA
AD NO.
2021-0263
SUBJECT
ATA 25 – Equipment / Furnishings – Aft Lavatory Quick Pin – Replacement
APPLICABILITY
Airbus A321-251N, A321-251NX, A321-252NX, A321-253N, A321-253NX and A321-271NX aeroplanes, manufacturer serial numbers (MSN) 07663, 07697, 07891, 07972, 08051, 08106, 08755, 08796, 08837, 08876, 08910, 08993, 09008, 09147, 09198, 09208, 09226, 09278, 09314 and 09365.
ISSUED BY
EASA
AD NO.
2021-0260
SUBJECT
ATA – Aircraft Flight Manual – Auto Flight System Control Panel ALT Knob Button Use – Amendment ATA 22 – Auto Flight – Flight Control Unit – Modification
APPLICABILITY
Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.
ISSUED BY
EASA
| AD NO. | SUBJECT | APPLICABILITY | ISSUED BY |
|---|---|---|---|
| 2021-23-12 | Air Transport Association (ATA) of America Code 31, Indicating/Recording System; 34, Navigation. | This AD applies to all transport and commuter category airplanes equipped with a radio (also known as radar) altimeter. These radio altimeters are installed on various transport and commuter category airplanes including, but not limited to, the airplanes for which the design approval holder is identified in paragraphs (c)(1) through (19) of this AD. (1) The Boeing Company (2) Airbus SAS (3) Bombardier Inc. (4) Embraer S.A. (5) Gulfstream Aerospace Corporation (6) Gulfstream Aerospace LP (7) Textron Aviation Inc. (8) Pilatus Aircraft Limited (9) Fokker Services B.V. (10) Saab AB, Support and Services (11) DeHavilland Aircraft of Canada Limited (12) Airbus Canada Limited Partnership (13) ATR-GIE Avions de Transport Régional (14) Yaborã Ind[uacute]stria Aeronáutica S.A. (15) MHI RJ Aviation ULC (16) BAE Systems (Operations) Limited (17) Lockheed Martin Corporation/Lockheed Martin Aeronautics Company (18) Viking Air Limited (19) Dassault Aviation |
FAA
|
| 2014-0076R3 | 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, N and NP helicopters, all serial numbers |
EASA
|
| 2020-0249R1 | ATA 31 – Instruments – Angle of Attack Probe and Multi-Function Computers Electrical Routing – Operational Test / Inspection | ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN); and ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN. |
EASA
|
| G-2021-0015 | ATA 32 – Landing Gear – Main Landing Gear / Pintle to Cylinder Interface – Inspection | Jetstream 3100 & 3200 aeroplanes |
CAA UK
|
| 2021-0267 | ATA 55 – Stabilizers – Rudder Hinges – Inspection | P.68 “Victor”, P.68B “Victor”, P.68R “Victor”, P.68C, P.68C-TC, P.68 “Observer”, P.68 “Observer 2” and P.68TC “Observer” aeroplanes, all serial numbers (s/n). |
EASA
|
| 2021-19-17 | Joint Aircraft System Component (JASC) Code: 2500, Cabin Equipment/Furnishings; and 2520, Passenger Compartment Equipment. | Sikorsky Aircraft Corporation Model S-92A helicopters |
FAA
|
| 2021-24-07 | This AD was prompted by a report of a certain procedure in the aircraft maintenance manual (AMM) that incorrectly described a visual inspection of the fire handle. The FAA is issuing this AD to address snap wires made of incorrect material, which, if not detected and corrected, and combined with an engine fire, could lead to a failure of the engine fire handle to operate, possibly resulting in an uncontrolled engine fire and reduced control of the airplane. | This AD applies to the ATR–GIE Avions de Transport Régional airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) Emergency AD 2021-0237-E, dated November 4, 2021 (EASA AD 2021-0237-E). (1) Model ATR42-200, -300, -320, and -500 airplanes. (2) Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes. |
FAA
|
| 2021-0259 C | ATA 53 – Fuselage – Tail Gearbox Fitting – Inspection / Replacement | AB139 and AW139 helicopters, all serial numbers. |
EASA
|
| 2021-0261 | “ATA 05 – Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – Amendment” | 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, A330-841 and A330-941 aeroplanes, all manufacturer serial numbers. |
EASA
|
| 2021-20-09 | This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address fatigue cracking and damage in principal structural elements, which could result in reduced structural integrity of the airplane. | This AD applies to ATR-GIE Avions de Transport Régional Model ATR72-101, -102, -201, – 202, -211, -212, and -212A airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 9, 2020. |
FAA
|
| 2021-0263 | ATA 25 – Equipment / Furnishings – Aft Lavatory Quick Pin – Replacement | Airbus A321-251N, A321-251NX, A321-252NX, A321-253N, A321-253NX and A321-271NX aeroplanes, manufacturer serial numbers (MSN) 07663, 07697, 07891, 07972, 08051, 08106, 08755, 08796, 08837, 08876, 08910, 08993, 09008, 09147, 09198, 09208, 09226, 09278, 09314 and 09365. |
EASA
|
| 2021-0260 | ATA – Aircraft Flight Manual – Auto Flight System Control Panel ALT Knob Button Use – Amendment ATA 22 – Auto Flight – Flight Control Unit – Modification | Airbus A350-941 and A350-1041 aeroplanes, all manufacturer 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] |
