Airworthiness Directive 74-06-01
one-timeAirworthiness Directives; accordance with AiResearch Aviation Company Service Bulletin No. 14.1.10, dated February 6, 1974 or later FAA-approved revision, f
Which aircraft AD 74-06-01 applies to
AiResearch Aviation Company turbocharger modification per AiResearch SB No. 14.1.10 (dated Feb 6, 1974) and SB No. 14.1.11 (dated Feb 6, 1974), or later FAA-approved revisions, for serial numbers 27-2505 and subsequent; equivalent modification may be approved by the Chief, Aircraft Engineering Division, FAA Western Region; aircraft may be flown to a base for compliance.
Whether AD 74-06-01 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
Supersession
Superseded by AD 2005-01-10 — comply with the superseding directive.
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 →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.