Airworthiness Directive

AD 2000-01-07 65 FR 1765 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-499
Amendment
39-11504
Published
2000-01-12
Effective
2000-01-27
Models covered
1
Last live check
2026-10-03
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AD

2000-01-07

FR doc 00-499 · 65 FR 1765

AD 2000-01-07Published 2000-01-12Effective 2000-01-27

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 the removal and testing of sections of bonded skin from the upper and lower skin panels of the horizontal stabilizer, repair of those areas, and follow-on corrective actions, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Bombardier Model DHC-8-100, -200, and -300 series airplanes. This action requires the removal and testing of sections of bonded skin from the upper and lower skin panels of the horizontal stabilizer, repair of those areas, and follow-on corrective actions, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to prevent reduced strength capability and consequent failure of the horizontal stabilizer, which could result in loss of controllability of the airplane.

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Applies to 1 model in our index