Other State of Design

2020-0249R1-CN

ATA 31 – CANCELLED: 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

2024-0053

ATA 05 – Time Limits / Maintenance Checks – Certification Maintenance Requirements and Airworthiness Limitations – Amendment

ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all manufacturer serial numbers.

EASA

2024–04–09

Air Transport Association (ATA) of America Code 31, Instruments.

This AD applies to The Boeing Company Model 777–200, 777–200LR, 777–300, 777–300ER, and 777F series airplanes, certificated in any category, as identified in Boeing Alert Requirements Bulletin 777–31A0342 RB, dated July 19, 2021.

FAA

2023-0190R1

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

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

EASA

2013-0104R3

ATA 27 – Flight Controls – Flap Actuator – Inspection / Replacement / Modification

TBM 700 aeroplanes, all manufacturer serial numbers, except those on which DAHER modification (MOD) 70-0777-27 has been embodied in production.

EASA

2024-0047

ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 5 – Fuel Airworthiness Limitations – 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 aeroplanes, all manufacturer serial numbers.

EASA

2024-0046

ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 – System Equipment Maintenance Requirements – 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 aeroplanes, all manufacturer serial numbers.

EASA

2024-0048

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

2024-0044-E

ATA 26 – Fire Protection – Engine Fire Extinguishing System – Inspection

ATR ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400 and ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN). ATR 72-101, ATR72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212 and ATR 72-212A aeroplanes, all MSN

EASA

CF-2024-05

Engine – Second-Stage Power Turbine (PT2) Blade Failure

Pratt & Whitney Canada (P&WC) PT6A-64, PT6A-66, PT6A-66A, PT6A-66B, PT6A-66D, PT6A-66T, PT6A-67, PT6A-67A, PT6A-67AF, PT6A-67AG, PT6A-67B, PT6A-67D, PT6A-67F, PT6A-67P, PT6A-67R, PT6A-67RM, PT6A-67T, PT6A-68, PT6A-68B, PT6A-68C, PT6A-68D, PT6A-68T, PT6E-67XP and PT6E-66XT engine models.

TCCA

2024–04–02

Joint Aircraft System Component (JASC) Code 6410, Tail Rotor Blades.

This AD applies to the Robinson Helicopter Company helicopters, certificated in any category,identified in paragraphs (c)(1) through (3) of this AD. (1) Model R22, R22 Alpha, R22 Beta, and R22 Mariner helicopters with tail rotor blade (TRB) partnumber (P/N) A029–2 with TRB serial numbers (S/N) up to 11279 inclusive (P/N A029–2 REV Athrough U inclusive), installed; (2) Model R44 and R44 II helicopters with TRB P/N C029–3 with TRB S/N up to 14329 inclusive (P/NC029–3 REV A through Q inclusive), installed; and (3) Model R66 helicopters with TRB P/N F029–1 with TRB S/N up to 3099 inclusive (P/N F029–1REV A through F inclusive), installed.

FAA

2024-0037R1

ATA 72 – Engine – Main Bearing / Studs – Replacement

E4 and E4P engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Diamond Aircraft Industries DA 40 NG, DA 42 NG, DA 42 M-NG and DA 62 aeroplanes.

EASA