Airworthiness Directive

AD 2007-12-03 72 FR 30968 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E7-10678
Amendment
39-15081
Published
2007-06-05
Effective
2007-07-10
Models covered
1
Last live check
2026-10-03
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AD

2007-12-03

FR doc E7-10678 · 72 FR 30968

AD 2007-12-03Published 2007-06-05Effective 2007-07-10

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 revising the Limitations section of the airplane flight manual to include procedures for pulling the "HYD PWR XFER" circuit breaker in the event of the loss of all hydraulic fluid in the No.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-400 series airplanes. This AD requires revising the Limitations section of the airplane flight manual to include procedures for pulling the "HYD PWR XFER" circuit breaker in the event of the loss of all hydraulic fluid in the No. 1 or No. 2 hydraulic system. This AD results from reports of fluid loss in the No. 2 hydraulic system, causing the power transfer unit to overspeed, increasing the fluid flow within the No. 1 hydraulic system. We are issuing this AD to prevent possible loss of both the No. 1 and No. 2 hydraulic systems, resulting in the potential loss of several functions essential for safe flight and landing of the airplane.

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Applies to 1 model in our index