Airworthiness Directive

AD 2015-02-12 80 FR 5025 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2015-01180
Amendment
39-18079
Published
2015-01-30
Effective
2015-03-06
Models covered
1
Last live check
2026-10-03
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AD

2015-02-12

FR doc 2015-01180 · 80 FR 5025

AD 2015-02-12Published 2015-01-30Effective 2015-03-06

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 doing a detailed inspection of the apex joints of the stabilizer brace lock link in the MLG for clearance; rectifying and repairing the clearance gap, if necessary; and lubricating the apex joints of the stabilizer brace…

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of two in-service incidents where one side of the main landing gear (MLG) did not achieve down-lock. This AD requires doing a detailed inspection of the apex joints of the stabilizer brace lock link in the MLG for clearance; rectifying and repairing the clearance gap, if necessary; and lubricating the apex joints of the stabilizer brace lock link in the MLG. We are issuing this AD to detect and correct insufficiently greased stabilizer brace lock linkage of the MLG and over-torqued lock linkage attachment bolts, which could lead to the failure to extend and down-lock the MLG, and could affect the safe landing of the airplane.

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Applies to 1 model in our index