Airworthiness Directive 68-19-05
one-timeAD 68-19-05 · 1968-01-01 · reciprocating engine
Airworthiness Directives; CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 68-19-05 CESSNA: Amendment 39-652. Applies to Types 172B, 172C, 172D, 172E, 1
Which aircraft AD 68-19-05 applies to
MakesContact Supplementary Information Regulatory Text 68-19-05 Cessna Amendment 39-652 Applies To Types 172B 172C 172D 172E 172F And 172G
Models6A-335-B, 172G
Whether AD 68-19-05 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD 68-19-05 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.
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.