Airworthiness Directive 50-36-01
one-timeAirworthiness Directives; the machined radius just below the scissors lug boss. Clean and remove paint from this area. Any evidence of cracks will require r
Which aircraft AD 50-36-01 applies to
Inspect main landing gear strut machined radius just below the scissors lug boss for cracks (strip paint for inspection); replace or repair per approved data if cracked.
Whether AD 50-36-01 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:
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.