Airworthiness Directive 48-50-01

one-time
AD 48-50-01 · 1948-01-01 · reciprocating engine

Airworthiness Directives; required after each 25 hours of operation. To prevent possible cylinder base flange failure, visual inspection for cracks just abo

Which aircraft AD 48-50-01 applies to

Models6A4-150-B3, 6A4-150-B31, 6A4-150

Visually inspect cylinder base flange for cracks every 25 hours of operation on early-type cylinders until replaced by later cylinders.

Whether AD 48-50-01 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 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 48-50-01 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.

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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.