Airworthiness Directive 63-25-01
one-timeAD 63-25-01 · 1963-01-01 · airframe
Airworthiness Directives; the front truss is replaced with a new heavier steel truss (Beech P/N 35- 410030-17), the requirements specified in (a) shall beco
Which aircraft AD 63-25-01 applies to
MakesFront Truss Is Replaced With A New Heavier Steel Truss Requirements Specified In Shall Become Applicable 2 000 Hours' Time In Service After Requirements Specified In Shall Become Applicable 2 000 Hours' Time In Service After Installation Of This Truss Note
Models35
Whether AD 63-25-01 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 63-25-01 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.