Airworthiness Directive

AD 2012-05-07 77 FR 16145 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2012-6439
Amendment
39-16979
Published
2012-03-20
Effective
2012-04-04
Models covered
1
Last live check
2026-10-03
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AD

2012-05-07

FR doc 2012-6439 · 77 FR 16145

AD 2012-05-07Published 2012-03-20Effective 2012-04-04

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 general visual inspection for chamfer of the upper edge of each leaf spring, and rework if necessary.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes. This AD requires a general visual inspection for chamfer of the upper edge of each leaf spring, and rework if necessary. This AD also requires installing a new friction brake nut. This AD was prompted by reports that it was possible to inadvertently move the power levers through the flight idle gate into the beta range due to an un-chamfered leaf spring in the friction brake that may contact the power lever latch when the friction adjusting knob is fully loosened. We are issuing this AD to detect and correct an unsafe condition where both engines can inadvertently be operated in beta mode during flight and consequently reduce controllability of the airplane.

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Applies to 1 model in our index