Airworthiness Directive

AD 2002-01-25 67 FR 4342 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-1962
Amendment
39-12620
Published
2002-01-30
Effective
2002-03-06
Models covered
1
Last live check
2026-10-03
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AD

2002-01-25

FR doc 02-1962 · 67 FR 4342

AD 2002-01-25Published 2002-01-30Effective 2002-03-06

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 repetitive inspections of the rudder pedal adjustment fittings for cracks and replacement of cracked fittings with new fittings.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-100, -200, and -300 series airplanes, that requires repetitive inspections of the rudder pedal adjustment fittings for cracks and replacement of cracked fittings with new fittings. This amendment also provides an optional terminating action. This action is necessary to detect and correct cracking of the rudder pedal adjustment fittings, which could lead to deformation of the fittings, resulting in jammed rudder pedals and loss of rudder control, with consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index