Airworthiness Directive

AD 2016-19-11 81 FR 66516 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2016-22705
Amendment
39-18660
Published
2016-09-28
Effective
2016-11-02
Models covered
1
Last live check
2026-10-03
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AD

2016-19-11

FR doc 2016-22705 · 81 FR 66516

AD 2016-19-11Published 2016-09-28Effective 2016-11-02

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 corrosion of the thermostats' mounting surfaces and fuselage skin surface, corrective actions if necessary, and relocating the existing thermostats.

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 a malfunctioning No. 2 engine intake heater with corrosion on the thermostats and the fuselage skin where the thermostats made contact with the aircraft fuselage skin. This AD requires a general visual inspection for corrosion of the thermostats' mounting surfaces and fuselage skin surface, corrective actions if necessary, and relocating the existing thermostats. We are issuing this AD to prevent corrosion within the thermostats that might cause the switch mechanism to seize in the open position and prevent the activation of the associated engine air intake heater. An inactive engine air intake heater could lead to an engine failure.

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Applies to 1 model in our index