AD NO.
AD/GA8/12
SUBJECT
ATA 72 – Engine – Combustion Rear Inner Case Bolt – Replacement / Modification
APPLICABILITY
All GA8 aircraft as identified in Table 1 of GippsAero Service Bulletin SB-GA8-2024-218 Issue 1, dated 11 July 2024, as in force on the date of commencement of this Airworthiness Directive (AD).
ISSUED BY
EASA