Airworthiness Directive 2013-02-01

one-time
Official AD 2013-02-01 · FR doc 2013-01008 · 2013-01-23 · airframe

Airworthiness Directives; Bell Helicopter Textron Canada Limited (Bell) Helicopters

What this AD requires

We are adopting a new airworthiness directive (AD) for Bell Model 206L, 206L-1, 206L-3, and 206L-4 helicopters. This AD requires inspecting certain hydraulic servo actuator assemblies (servo) for a loose nut, shaft, and clevis assembly, modifying or replacing the servo as necessary, and reidentifying the servo. This AD is prompted by an investigation after an accident and the determination that there was a loose connection due to improper lock washer installation. These actions are intended to detect loose or misaligned parts of the servo to prevent failure of the servo and subsequent loss of control of the helicopter.

Which aircraft AD 2013-02-01 applies to

MakesBell
Models206L, 206L-1, 206L-3, 206L-4
Serial-conditional — narrows to serials 52001–52430.
Part-conditional206-076-062-103.

Applies only when hydraulic servo actuator assembly (servo) P/N 206-076-062-103 is installed. Model 206L, 206L-1, and 206L-3: all serial numbers. Model 206L-4: S/N 52001 through 52430 only.

Whether AD 2013-02-01 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 2013-02-01 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.

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.