Beech 65 Queen Air Airworthiness Directives

Q: What is the newest Airworthiness Directive for the Beech 65 Queen Air?

AD 95-20-01 R1, published 1995-10-24: Airworthiness Directives; Beech Aircraft Corporation Models 65 and L-23F Airplanes.

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Also known as: L-23F

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What Airworthiness Directives apply to the Beech 65 Queen Air

The FAA has published one Airworthiness Directive that names the Beech 65 Queen Air, published on 1995-10-24.

Newest

AD 95-20-01 R1 Airworthiness Directives; Beech Aircraft Corporation Models 65 and L-23F Airplanes 1995-10-24

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Airworthiness Directives

1 record

ADAD 95-20-01 R1Beech Aircraft Corporation Models 65 and L-23F Airplanes1995-11-03Active

95-20-01 R1

FR doc 95-26107 · 60 FR 54415

AD 95-20-01 R1Published 1995-10-24Effective 1995-11-03

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Beech Aircraft Corporation Models 65 and L-23F Airplanes

Requires fabricating and installing a placard that specifies not to operate the airplane with the cabin door removed, and incorporating a copy of the AD into the Limitations Section of the Airplane Flight Manual (AFM).

Full official abstract

Airworthiness Directives; Beech Aircraft Corporation Models 65 and L-23F Airplanes

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-20-01 R1, which was sent previously to all known U.S. owners and operators of certain Beech Aircraft Corporation (Beech) Models 65 and L-23F (military conversion) airplanes. This AD requires fabricating and installing a placard that specifies not to operate the airplane with the cabin door removed, and incorporating a copy of the AD into the Limitations Section of the Airplane Flight Manual (AFM). A recent accident of one of the affected airplanes that was operating with the cabin door removed prompted the existing AD. The actions specified by this AD are intended to prevent the possibility of a reduction in stability, controllability, or airplane climb performance during operation, particularly in single- engine operations at high gross weights.

Source: Federal Register document 95-26107, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

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Service Bulletins

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This page indexes 1 AD and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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