Airworthiness Directive

AD 2007-01-08 72 FR 3352 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E7-911
Amendment
39-14880
Published
2007-01-25
Effective
2007-03-01
Models covered
1
Last live check
2026-10-03
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AD

2007-01-08

FR doc E7-911 · 72 FR 3352

AD 2007-01-08Published 2007-01-25Effective 2007-03-01

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 inspecting for fouling and chafing damage of the outboard brake control cable of the main landing gear, replacing the control cable if necessary, reworking the control cable cover, and, if applicable…

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-400 series airplanes. This AD requires inspecting for fouling and chafing damage of the outboard brake control cable of the main landing gear, replacing the control cable if necessary, reworking the control cable cover, and, if applicable, manufacturing/installing an offset plate on the control cable cover. This AD results from a review of brake control cable operation conducted by the manufacturer. We are issuing this AD to prevent abrasion and wear of the outboard brake control cable, which could lead to cable separation and reduced control of airplane braking.

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Applies to 1 model in our index