Airworthiness Directive 98-25782
one-timeAirworthiness Directives; Rolls-Royce Limited, Aero Division Bristol/S.N.E.C.M.A. Olympus 593 Series Turbojet Engines
What this AD requires
The FAA is withdrawing the final rule; request for comments, which was published on September 16, 1998 (63 FR 49418). The reason for the withdrawal is because it is a duplicate of a final rule; request for comments, published on September 15, 1998 (63 FR 49278). The September 15, 1998, final rule, remains effective September 30, 1998. The September 15, 1998 amendment adopted a new airworthiness directive (AD) that is applicable to Rolls-Royce Limited, Aero Division--Bristol/ S.N.E.C.M.A. Olympus 593 series turbojet engines.
Which aircraft AD 98-25782 applies to
Whether AD 98-25782 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.