Airworthiness Directive

AD 2014-15-20 79 FR 48030 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2014-18306
Amendment
39-17923
Published
2014-08-15
Effective
2014-09-19
Models covered
1
Last live check
2026-10-03
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AD

2014-15-20

FR doc 2014-18306 · 79 FR 48030

AD 2014-15-20Published 2014-08-15Effective 2014-09-19

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 wiring modification to segregate the HPSOV power supply from the TMU.

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 failure of the high pressure shutoff valves (HPSOVs) causing the timer and monitor unit (TMU) to become inoperative since the HPSOV and the TMU are on the same circuit breaker. This AD requires a wiring modification to segregate the HPSOV power supply from the TMU. We are issuing this AD to prevent an inoperative TMU, which could result in the loss of the automatic de-icing mode, and lead to an increased workload for the flight crew and loss of control of the airplane.

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Applies to 1 model in our index