Airworthiness Directive 70-26-06
one-timeAirworthiness Directives; that the airplane may be flown in accordance with FAR 21.197 to a base where the repair can be made. (c) Upon the incorporation of
Which aircraft AD 70-26-06 applies to
Compliance is gated to installation of the specific Piper elevator/rudder hinge kit part number noted in the teaser — confirm applicable model from the full AD text before use.
Whether AD 70-26-06 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Superseded by AD 2001-06-01 — comply with the superseding directive.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.