EASA AD ISR-I-32-24-10-01R1
Nose Landing Gear Actuator to Strut Attachment Pin Inspection / Life Limit AMM Revision
Summary
Airworthiness Directive AD ISR I-32-24-10-01R1 issued by the Civil Aviation Authority of Israel addresses the inspection and life limit revision for the nose landing gear actuator to strut attachment pin on all Gulfstream G150 model aircraft. This directive mandates updates to the Aircraft Maintenance Manual (AMM) to include a life limit for the affected pin part number 2247-0500-008. The directive aims to enhance safety by preventing failures related to this critical landing gear component.
What Changed
This revision updates the part number from 3-2247-0500-008 to 2247-0500-008 and requires G150 operators to incorporate AMM Revision 29 or later, which includes the new pin life limit in section 05-10-10 of the G150 AMM. It introduces a mandatory inspection and life limit for the nose landing gear actuator to strut attachment pin to prevent potential failures.
Why It Matters
The directive is crucial for aviation professionals as it directly impacts the airworthiness and safety of Gulfstream G150 aircraft by addressing a known failure issue with the nose landing gear attachment pin. Operators, maintenance organizations, and compliance teams must ensure the updated AMM procedures are followed to avoid unsafe conditions and regulatory non-compliance. Timely adherence reduces the risk of landing gear malfunctions that could compromise flight safety.
What To Do
Operators of Gulfstream G150 aircraft must update their maintenance procedures by incorporating AMM Revision 29 or later approved by the Civil Aviation Authority of Israel. They must comply with the inspection and life limit requirements for the nose landing gear actuator to strut attachment pin within three months from the effective date of October 15, 2024. Failure to comply prohibits operation of the affected aircraft until the directive is met.
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