Airworthiness Directive 88-03-07
one-timeAirworthiness Directives; compliance with this AD may be used if approved by the Manager, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Roo
Which aircraft AD 88-03-07 applies to
Amendment 39-5841, effective February 10, 1988; relates to Amendment 39-5782 published November 30, 1987 (52 FR 45451). Documents available from Cessna Aircraft Company Customer Service, Wichita, KS; alternative compliance approved by FAA Wichita ACO.
Whether AD 88-03-07 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.