AD 2008-17-06

final rule
Data completeness: 80%

Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes

AD Number
2008-17-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2008-0864
FR Citation
73 FR 47818

Applicability

TypeManufacturerModelDetails
aircraft Bombardier DHC-8-400 Airworthiness Directives; Bombardier Model DHC-8-400 Series Airplanes

Unsafe Condition

Loss of No. 2 hydraulic system fluid causing the power transfer unit (PTU) to overspeed and increasing fluid flow in the No. 1 hydraulic system, potentially leading to loss of both hydraulic systems and essential functions for safe flight and landing.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Revise the Normal and Abnormal Procedures section of the AFM to include procedures ensuring the 'PTU CNTRL' switch is Normal, the 'PTU CNTRL ON' advisory light is out, and the 'HYD PWR XFER' circuit breaker is pulled in the event of the '2 HYD ISO VALVE' caution light illumination.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Bombardier Model DHC-8-400, DHC-8-401, and DHC-8-402 series airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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