Airworthiness Directive 95-4371
recurringAirworthiness Directives; Beech Aircraft Corporation Models 1900, 1900C, and 1900D Airplanes; Correction
What this AD requires
This action makes a correction to Airworthiness Directive (AD) 95-02-18 concerning Beech Aircraft Corporation Models 1900, 1900C, and 1900D airplanes, which was published in the Federal Register on February 3, 1995 (60 FR 6652). That publication inadvertently referenced an incorrect repetitive inspection interval for Models 1900 and 1900C airplanes with a part number 129-910032-79 engine truss installed. The inspection interval in sections B and C of the engine truss should be 3,000 hours time-in-service (TIS) instead of 100 hours TIS. This action corrects the AD to reflect this repetitive inspection interval.
Which aircraft AD 95-4371 applies to
with a part number 129-910032-79 engine truss installed
Whether AD 95-4371 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
Supersession
Supersedes AD 92-06-09.
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 →Read the full directive (Federal Register)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.