Is AD 46-44-01 a recurring Airworthiness Directive?

No — AD 46-44-01 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 46-44-01 apply to?

AD 46-44-01 applies to Cessna — models 120, 140. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 46-44-01

one-time

AD 46-44-01 · 1946-01-01 · airframe

Airworthiness Directives; the cockpit just forward of the rudder pedals. Removal of the fairing which forms a tunnel along the floor from the seat to the pe

Which aircraft AD 46-44-01 applies to

MakesCessna

Models120, 140

Inspect/reinforce bolts mounting rudder pedal assembly at cockpit floor center, just forward of the rudder pedals; requires removing floor fairing/tunnel for access.

Whether AD 46-44-01 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 46-44-01 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.