Airworthiness Directive

AD 98-24-18 63 FR 64609 Active

Federal Aviation Administration · 14 CFR part 39

Requires a one-time inspection to detect disbonding of the upper and lower skin panels of the horizontal stabilizer, and repair, if necessary.

FR document
98-31178
Amendment
39-10903
Published
1998-11-23
Effective
1998-12-08
Models covered
1

Last live check: 2026-08-19

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AD

98-24-18

FR doc 98-31178 · 63 FR 64609

AD 98-24-18Published 1998-11-23Effective 1998-12-08

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 a one-time inspection to detect disbonding of the upper and lower skin panels of the horizontal stabilizer, and repair, if necessary.

Supersedes an earlier directive. See the official text.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102 and -103 series airplanes, that currently requires a one-time inspection to detect disbonding of the upper and lower skin panels of the horizontal stabilizer, and repair, if necessary. This amendment establishes repetitive intervals for the inspection to detect disbonding of the upper and lower skin panels of the horizontal stabilizer. This amendment also revises the applicability of the existing AD to include certain additional airplanes, and to exclude certain other airplanes. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by 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