EASA AD 2024-0097R2
SUPERSEDED BY EASA AD 2025-0189
Summary
EASA Airworthiness Directive 2024-0097R2 is a regulatory update addressing inspection and maintenance requirements for Airbus A318, A319, A320, and A321 aircraft. It focuses on the main landing gear (MLG) door hinge and actuator fittings on the keel beam to detect and prevent cracks that could lead to in-flight detachment of MLG doors. The directive applies to both Current Engine Option (CEO) and New Engine Option (NEO) variants, specifying inspection methods and intervals.
What Changed
EASA AD 2024-0097R2 revises the previous AD 2024-0097R1 by allowing compliance using earlier revisions of the Airbus Service Bulletins for inspections. It retains the requirements for repetitive inspections with updated thresholds and intervals and clarifies credit for prior inspections and repairs. The revision also addresses comments received during consultation that were not previously incorporated.
Why It Matters
This directive is critical for aviation professionals to ensure the structural integrity of the MLG door fittings, preventing potential in-flight detachment and consequent damage. Operators and maintenance organizations must adhere to the updated inspection intervals and methods to maintain airworthiness and regulatory compliance. The AD also provides clear guidance on terminating actions through approved modifications, aiding in long-term fleet maintenance planning.
What To Do
Operators of affected Airbus A318, A319, A320, and A321 aircraft must perform detailed visual, high frequency eddy current, and ultrasonic inspections of the MLG door actuator and hinge fittings within specified flight cycle thresholds and continue at intervals not exceeding 2,250 or 3,000 flight cycles as applicable. Any discrepancies found must be corrected before the next flight following Airbus-approved repair instructions. Incorporation of Airbus modification SB A320-53-1502 or SB A320-53-1503 terminates the repetitive inspection requirements.