Airworthiness Directive

AD 2002-12-11 67 FR 42989 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-15367
Amendment
39-12783
Published
2002-06-26
Effective
2002-07-31
Models covered
1
Last live check
2026-10-03
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AD

2002-12-11

FR doc 02-15367 · 67 FR 42989

AD 2002-12-11Published 2002-06-26Effective 2002-07-31

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 revision of the applicable maintenance program manual, repetitive inspections for corrosion or cracking of the hook roller shafts of the flap carriage, and eventual replacement of the hook roller shafts with new or…

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 revision of the applicable maintenance program manual, repetitive inspections for corrosion or cracking of the hook roller shafts of the flap carriage, and eventual replacement of the hook roller shafts with new or serviceable hook roller shafts. This replacement extends the interval for the repetitive inspections. This action is necessary to prevent cracking of the hook roller shafts of the flap carriage and consequent reduced structural integrity of the flap, which could result in jamming of the flap. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index