EASA Regulations for ATR 42

23 airworthiness directives and regulations affecting ATR 42.

EASA SIB 2011-02

ATR Main Landing Gear (MLG) Shock Absorbers — Cross Locking Bolt of the Attachment Pin

EASA Safety Information Bulletin 2011-02 is an informational document addressing the ATR 42 and ATR 72 aeroplanes' main landing gear (MLG) shock absorbers, specifically the cross locking bolt of the attachment pin. It highlights the risk of migration and rupture of the shock absorber attachment pin due to missing locking bolts, referencing previous maintenance manuals and service bulletins.

Mar 18, 2011

Safety Information BulletinMaintenanceSafety MgmtATR 42ATR 72

EASA SIB 2010-29

Thales Angle of Attack (AoA) Sensors

EASA Safety Information Bulletin SIB No. 2010-29 addresses issues with Thales Angle of Attack (AoA) sensors installed on ATR 42 and ATR 72 aircraft. The bulletin highlights that certain AoA sensors, identified by specific part and serial numbers, were repaired using improperly calibrated test equipment, potentially affecting their accuracy. It references Thales Avionics service bulletins that provide instructions for testing and adjustment of the affected units.

Oct 7, 2010

Safety Information BulletinMaintenanceSafety MgmtATR 42ATR 72

EASA SIB 2010-11

Component Configuration Control — Discrepancies between the Manufacturer—s Aircraft Configuration Data and Operators— Spares Management Systems.

EASA Safety Information Bulletin SIB No: 2010-11 addresses discrepancies between manufacturer aircraft configuration data and operators' spares management systems, specifically involving the ATR 72 aircraft. The bulletin highlights an incident where an incorrect Fuel Quantity Indicator part number for the ATR 42 was fitted on an ATR 72, causing erroneous fuel readings. It emphasizes the importance of using approved maintenance data and manufacturer configuration data for component eligibility.

Apr 16, 2010

Safety Information BulletinMaintenanceSafety MgmtATR 42ATR 72