Other State of Design

2026-18-07

Air Transport Association (ATA) of America Code 53, Fuselage.

This AD applies to The Boeing Company Model 737-8, 737-9, and 737-8200 airplanes, certificated inany category, as identified in Boeing Alert Requirements Bulletin 737-53A1420 RB, dated February 13,2025.

FAA

2024-0144R1

ATA 65 – Tail Rotor Drive – Shaft-Line – Check / Measurement / Modification

EC 130 T2 helicopters, all serial numbers on which AH modification (MOD) 079809 has been embodied in production.

EASA

2023-0214R1

ATA 53 – Fuselage – Tail Rotor Drive Shaft / Rear Transmission Bearing Support – Inspections / Modification

EC 130 T2 helicopters, all serial numbers on which AH modification (mod) 074581 has been embodied in production; except those having AH MOD 0720245, mod 0790004 and mod 0790006 embodied.

EASA

2026-0177

ATA 31 – Indicating / Recording Systems – Integrated Control Panels – Inspection

Airbus A350-941 and A350-1041 aeroplanes, all manufacturer serial numbers.

EASA

2026-0176

ATA 92 – Electrical Systems Installation – Battery Retaining Rods – Identification / Replacement

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, 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, A321-253N, A321-271N, A321-272N, A321-251NX and A321-271NX aeroplanes, all manufacturer serial numbers (MSN).

EASA

2026-17-03 (Correction)

Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section.

This AD applies to International Aero Engines AG (IAE AG) Model V2522-A5, V2524-A5, V2525-D5,V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines with a3rd stage high-pressure compressor (HPC) rotor blade having part number (P/N) 6A8353 or P/N6A8688 installed.

FAA

2026-0174

ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

CFM56-7B20, CFM56-7B22, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/B1, CFM56-7B26, CFM56- 7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B27A, CFM56- 7B27A/3, CFM56-7B20/2, CFM56-7B22/2, CFM56-7B24/2, CFM56-7B26/2, CFM56-7B27/2, CFM56- 7B20/3, CFM56-7B22/3, CFM56-7B22/3B1, CFM56-7B24/3, CFM56-7B24/3B1, CFM56-7B26/3, CFM56-7B26/3F, CFM56-7B26/3B1, CFM56-7B26/3B2, CFM56-7B26/3B2F, CFM56-7B27/3, CFM56- 7B27/3F, CFM56-7B27/3B1, CFM56-7B27/3B1F and CFM56-7B27/3B3 engines, all serial numbers. These engines are known to be installed on, but not limited to, Boeing 737-600, 737-700, 737-800, 737-900 and 737-900ER series aeroplanes.

EASA

2026-0172-E

ATA 79 – Engine Oil – Oil Pump – De-Pairing

RB211 Trent 768-60, 772-60, 772B-60 and Trent 772C-60 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Airbus A330 aeroplanes.

EASA

2026-17-10

Joint Aircraft System Component (JASC) Code 8530, Reciprocating Engine Cylinder Section.

This AD applies to Lycoming Engines Model O-235, -A, -AP, -B, -BP, -C, -C1, -C1A, -C1B, -C1C, -C2A, -C2B, -C2C, -E1, -E1B, -E2A, -E2B, -F1, -F1B, -F2A, -F2B, -G1, -G1B, O-235-G2A, O-235-G2B, O-235-H2C, O-235-J2A, O-235-J2B, O-235-K2A, O-235-K2B, -K2C, -L2A, -L2C, -M1, -M2C, -M3C, -N2A, -N2C, -P1, -P2A, -P2C, and -P3C; O-540-A1A, -A1A5, -A1B5, -A1C5, -A1D, -A1D5, -A2B, -A3D5, -A4A5, -A4B5, -A4C5, -A4D5, -A4E5, -B1A5, -B1B5, -B1D5, -B2A5, -B2B5, -B2C5, -B4A5, -B4B5, -D1A5, -E4A5,-E4B5, -E4C5, -F1A5, -F1B5, -G1A5, -G2A5, -H1A5, -H1A5D, -H1B5D, -H2A5, -H2A5D, -H2B5D, -J1A5D, -J1B5D, -J1C5D, -J1D5D, -J2A5D, -J2B5D, -J2C5D, -J2D5D, -J3A5, -J3A5D, -J3C5D, and -L3C5D; IO-540-A1A5, -AA1A5, -AA1B5, -AB1A5, -AE1A5, -AC1A5, -AF1A5, -B1B5, -AG1A5, -B1A5, -B1C5, -C1B5, -C1C5, -C2C, -C4B5, -C4B5D, -C4C5, -C4D5, -C4D5D, -D4A5, -D4B5, -D4C5, -E1A5, -E1B5, -E1C5, -G1A5, -G1B5, -G1C5, -G1D5, -G1E5, -G1F5, -J4A5, -K1A5, -K1A5D, -K1B5, -K1B5D, -K1C5, -K1D5, -K1E5, -K1E5D, -K1F5, -K1F5D, -K1G5, -K1G5D, -K1H5, -K1J5, -K1J5D, -K1K5, -K2A5, -L1A5, -L1A5D, -L1B5D, -L1C5, -M1A5, -M1A5D, -M1B5D, -M1C5, -M2A5D, -N1A5, -P1A5, -R1A5, -S1A5, -T4A5D, -T4B5, -T4B5D, -T4C5D, -U1A5D, -U1B5D, -V4A5, -V4A5D, -W1A5, -W1A5D, and -W3A5D engines with a serial number listed in Table 2 or Table 3 of Lycoming Mandatory ServiceBulletin No. (MSB) 667A, dated March 12, 2026 (Lycoming MSB 667A), and an installed piston pinhaving part number (P/N) LW-13445 with an FAA Form 8130-3 from the original equipmentmanufacturer for production dated between January 7, 2021 to December 15, 2025. If the productiondate on the FAA Form 8130-3 cannot be determined, or if the FAA Form 8130-3 is not available, thisAD is applicable.

FAA

2026-17-02

Air Transport Association (ATA) of America Code 57, Wings.

This AD applies to The Boeing Company Model 787-8, 787-9, and 787-10 airplanes, certificated in anycategory, as identified in Boeing Alert Requirements Bulletin B787-81205-SB570048-00 RB, Issue001, dated August 11, 2025.

FAA

2025-0094R2

ATA 24 – Electrical Power – Overhead Panel Wires Interference – Inspection / Modification

AB139 and AW139 helicopters, all serial numbers (s/n) from s/n 31201 to 32999 inclusive, and from s/n 41201 to 41999 inclusive.

EASA

2026-17-03

Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section.

This AD applies to International Aero Engines AG (IAE AG) Model V2522-A5, V2524-A5, V2525-D5,V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines with a3rd stage high-pressure compressor (HPC) rotor blade having part number (P/N) 6A8353 or P/N6A8688 installed.

FAA