Airworthiness Directive 70-23-04
one-timeAirworthiness Directives; Engineering and Manufacturing Branch, Southwest Region, FAA, Fort Worth, Texas. (2) Inspect flap tracks in accordance with Aerosta
Which aircraft AD 70-23-04 applies to
Concerns inspection of flap tracks per Aerostar Service Bulletin 600-22A (or FAA-approved equivalent); repair required if cracks found; further action required within 100 hours or next annual after effective date. Model family '600' inferred from the service bulletin number prefix; specific variant not confirmed in this excerpt.
Whether AD 70-23-04 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.