Airworthiness Directive 59-05-06
one-timeAirworthiness Directives; stated in Republic Aviation Service Bulletins 3.45-1, safetying lateral trim cylinder cap nut and 8.10-3 on rework of emergency fu
Which aircraft AD 59-05-06 applies to
Modifications per Republic Aviation Service Bulletins 3.45-1 (safetying lateral trim cylinder cap nut) and 8.10-3 (rework of emergency fuel shutoff lever) must be accomplished immediately. Specific model not present in the retrieved text.
Whether AD 59-05-06 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 →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.