Airworthiness Directive

AD 2001-06-13 66 FR 17506 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-7700
Amendment
39-12160
Published
2001-04-02
Effective
2001-05-07
Models covered
1
Last live check
2026-10-03
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AD

2001-06-13

FR doc 01-7700 · 66 FR 17506

AD 2001-06-13Published 2001-04-02Effective 2001-05-07

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 the endcaps of the main landing gear selector valve for leaks of hydraulic oil and, if leaks are detected, replacing the leaking endcaps or the entire selector valve.

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 inspecting the endcaps of the main landing gear selector valve for leaks of hydraulic oil and, if leaks are detected, replacing the leaking endcaps or the entire selector valve. This amendment also requires eventual replacement or rework of certain selector valves, which will terminate the repetitive inspections. This amendment is prompted by a report of the collapse of the main landing gear due to an external leak of hydraulic oil in the landing gear selector valve, resulting from a fracture of the endcap. The actions specified by this AD are intended to prevent leaks of hydraulic oil from the main landing gear selector valve, which could result in the collapse of the main landing gear.

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Applies to 1 model in our index