Airworthiness Directive 88-03-07

one-time
AD 88-03-07 · 1988-01-01 · airframe

Airworthiness 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

MakesCessna Aircraft Company

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:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 88-03-07 complied with on your aircraft?

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.

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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.