Airworthiness Directive

AD 2002-25-07 67 FR 78153 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-31752
Amendment
39-12983
Published
2002-12-23
Effective
2003-01-27
Models covered
1
Last live check
2026-10-03
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AD

2002-25-07

FR doc 02-31752 · 67 FR 78153

AD 2002-25-07Published 2002-12-23Effective 2003-01-27

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.

Requires removing the horizontal stabilizer supports and inspecting the edges of the tailboom skins around the horizontal stabilizer openings for a crack.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada Limited (BHTCL) model helicopters that currently requires removing the horizontal stabilizer supports and inspecting the edges of the tailboom skins around the horizontal stabilizer openings for a crack. This amendment requires checking and inspecting the tailboom for a crack and modifying or replacing the tailboom as necessary. This amendment also provides a terminating action, incorporates a more recent alert service bulletin (ASB), and increases the compliance time for performing the inspections. This amendment is prompted by several reports of cracks found during mandatory inspections. The actions specified by this AD are intended to detect a crack in the tailboom skin and to prevent separation of the tailboom and subsequent loss of control of the helicopter.

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All Bell 206 JetRanger / LongRanger directives

Applies to 1 model in our index