AD 2010-19-02

final rule
Data completeness: 70%

Airworthiness Directives; Bombardier, Inc. Model DHC-8-200 and DHC-8-300 Series Airplanes

AD Number
2010-19-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-0432
FR Citation
75 FR 55461

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier, Inc. Model DHC-8-200 and DHC-8-300 Series Airplanes
aircraft Aviat Various Airworthiness Directives; Bombardier, Inc. Model DHC-8-200 and DHC-8-300 Series Airplanes

Unsafe Condition

All three flapper valves located in each collector tank do not conform to design requirements due to the installation of a valve spring on the flapper hinge pin, which should have been removed prior to installation. This valve spring holds the flapper valve closed, preventing gravity feed and potentially leading to an in-flight engine shutdown in the event of scavenge system failure.

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

Required Actions

Perform a detailed inspection of each collector tank flapper valve for the presence of a valve spring. If the valve spring is present, remove it and apply an identification mark. If the valve spring is not present, apply an identification mark. All actions must be completed before further flight.

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

Compliance Time

Within 1,000 flight hours after the effective date of this AD.

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Affected Aircraft

Bombardier, Inc. Model DHC-8-201, -202, -301, -311, and -315 airplanes, certificated in any category, having serial numbers 644 through 664 inclusive.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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