Other State of Design

2021-0280R1

ATA 36 – Pneumatic – Pylon / Wing Interface Bleed Duct and Fuel Pipe – Inspection

Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers.

EASA

2024-0211-E

ATA 32 – Main Landing Gear – Main Landing Gear Shock Absorber – Inspection

AB139 and AW139 helicopters, all serial numbers.

EASA

2024-19-15

Air Transport Association (ATA) of America Code 35, Oxygen.

This AD applies to Safran Aerosystems (formerly AVOX Systems Inc.; Scott Aviation) oxygen cylinderand valve assemblies having part number (P/N) 89794050, 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 aircraftidentified 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 -212Aairplanes. (12) The Boeing Company Model 747-8 series airplanes.

FAA

2024-20-07

Joint Aircraft System Component (JASC) Code: 2560, Emergency Equipment; and 3212, Emergency Flotation Section.

This AD applies to the helicopters identified in paragraphs (c)(1) through (8) of this AD, certificated in any category. (1) Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters modified by Supplemental Type Certificate (STC) SR00831LA; Model EC120B helicopters modified by STC SR00780LA; and Model EC130B4 helicopters modified by STC SR01687LA. Note 1 to paragraph (c)(1): Helicopters with an AS350B3e designation are Model AS350B3 helicopters. (2) Airbus Helicopters Deutschland GmbH (AHD) Model BO-105A, BO-105C, BO-105S, and BO-105LS A-3 helicopters modified by STC SR00856LA; Model EC135P1, EC135P2, EC135P2+, EC135P3, EC135T1, EC135T2, EC135T2+, and EC135T3 helicopters modified by STC SR01855LA; and Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters modified by STC SR02244LA. Note 2 to paragraph (c)(2): Helicopters with an EC135P3H designation are Model EC135P3 helicopters; helicopters with an EC135T3H designation are Model EC135T3 helicopters, and helicopters with an MBB-BK117 C-2e designation are Model MBB-BK117 C-2 helicopters. (3) Bell Textron Inc., Model 210, 212, 412, 412CF, and 412EP helicopters modified by STC SR01779LA; and Model 412, 412CF, and 412EP helicopters modified by STC SR01459LA. (4) Bell Textron Canada Limited Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, and 407 helicopters modified by STC SR01535LA. Note 3 to paragraph (c)(4): Helicopters with a 206B3 designation are Model 206B helicopters; helicopters with a 206L-1+ designation are Model 206L-1 helicopters; and helicopters with a 206L-3+ designation are Model 206L-3 helicopters. (5) Leonardo S.p.a. Model AB412 and AB412 EP helicopters modified by STC SR01779LA. (6) MD Helicopters, LLC, Model 369D, 369E, 369F, 369FF, 369HE, 369HM, 369HS, and 500N helicopters modified by STC SR00932LA. (7) Robinson Helicopter Company Model R44 and R44 II helicopters modified by STC SR02049LA; and Model R66 helicopters modified by STC SR02484LA. (8) Sikorsky Aircraft Corporation Model S-76A, S-76B, and S-76C helicopters modified by STC SR01902LA.

FAA

2024-21-02

Joint Aircraft System Component (JASC) Code 8500, Engine (Reciprocating).

This AD applies to Lycoming Engines (Lycoming) model engines that have an affected part and part number (P/N) installed and are assembled within the ship date range, as specified in Table 1 to paragraph (c) of this AD. P/N Affected part Ship date range LW-13923 Connecting Rod Bushing 01/30/2009-11/17/2015 LW-11750 Connecting Rod Assembly 01/30/2009-11/19/2015 78030 Connecting Rod Assembly 01/30/2009-03/31/2016 LW-19332 Connecting Rod Assembly 01/30/2009-01/03/2016 LW-13865 Connecting Rod Assembly 01/30/2009-02/14/2017 77450 Connecting Rod Assembly 01/30/2009-02/14/2017 LW-13422 Connecting Rod Assembly 01/30/2009-02/14/2017 LW-13937 Connecting Rod Assembly 01/30/2009-02/14/2017 LW-15288 Connecting Rod Assembly 01/30/2009-02/14/2017 Note 1 to paragraph (c): The affected parts are known to be installed on Lycoming Model AEIO-320 series, AEIO-360 series, AEIO-390 series, AEIO-540 series, AEIO-580-B1A, AIO-320 series, AIO-360 series, HIO-360 series, HIO-390-A1A, HIO-540-A1A, HO-360 series, IO-320 series, IO-360 series, IO-390 series, IO-540 series, IVO-360-A1A, IVO-540-A1A, LHIO-360 series, LIO-320 series, LIO-360 series, LO-360 series, LTIO-540 series, LTO-360 series, O-233-A1, O-235 series, O-320 series, O-340 series, O-360 series, O-435 series, O-540 series, SO-580 series, TEO-540 series, TIGO-541 series, TIO-360 series, TIO-540 series, TIO-541 series, TIVO-540-A2A, TO-360 series, TVO-435 series, TVO-540-A1A, VO-360 series, VO-435 series, VO-540 series, and VSO-580-A1A engines.

FAA

2022-0047-CN

ATA 53 – CANCELLED: 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

2024-0210

ATA 53 – Fuselage – Inner Cap and Frame Flange at Frame 68 Stringer 22 – Inspections

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: – A319 aeroplanes on which Airbus modification (mod) 28238, mod 28162 and mod 28342 have been embodied in production; and – A318 aeroplanes on which mod 39195 has been embodied in production, or Airbus Service Bulletin (SB) A320-00-1219 has been embodied in service.

EASA

2024-20-04

Joint Aircraft System Component (JASC) Code: 2500, Cabin Equipment/Furnishing; and 2510, Flight Compartment Equipment.

This AD applies to all helicopters, certificated in any category, with a restraint system with a Pacific Scientific Company rotary buckle assembly (buckle) part number (P/N) 1111475 (all dash numbers) or P/N 1111548-01 having a date of manufacture (DOM) between January 2012 and April 2013 inclusive, or an unknown DOM. These buckles may be installed on, but not limited to, Airbus Helicopters model helicopters. Note 1 to paragraph (c): The buckle may be included as a component of a different part-numbered restraint system assembly. Note 2 to paragraph (c): These buckles may also be installed on airplanes; however, the FAA determined that a longer compliance time to accomplish the required actions is allowable for buckles installed on airplanes. Accordingly, the FAA plans to publish a separate AD rulemaking to address all airplanes with an affected buckle installed.

FAA

2024-0208

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, A321-272NX, A321-253NY aeroplanes, all manufacturer serial numbers.

EASA

2024-20-03

Joint Aircraft System Component (JASC) Code: 2700, Flight Control System.

This AD applies to all Robinson Helicopter Company Model R22 Beta, R22 Mariner, R44, and R44 IIhelicopters, certificated in any category, with a governor controller part number (P/N) D270-1,Revision A through E inclusive, installed.

FAA

2024-19-06

Air Transport Association (ATA) of America Code 30, Ice/Rain Protection System.

This AD applies to The Boeing Company Model 737-8 and 737-9 airplanes, certificated in any category,having a line number identified in paragraph 1.A., “Effectivity,” of Boeing Alert Requirements Bulletin 737-30A1083 RB, dated November 18, 2022.

FAA

2024-0195R1

ATA 73 – Engine Fuel & Control – Electronic Engine Control Unit – Software Update ATA 73 – Engine Fuel & Control – Preference Injector – Non-extinguishing Test / Replacement

ARRIUS 2B2, all serial numbers. These engines are known to be installed on, but not limited to, Airbus Helicopters Deutschland (AHD) EC135 twin-engine helicopters.

EASA