AD 2010-23-04

final rule
Data completeness: 70%

Airworthiness Directives; Bombardier, Inc. Model DHC-8-400 Series Airplanes

AD Number
2010-23-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2010-1041
FR Citation
75 FR 68174

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier, Inc. Model DHC-8-400 Series Airplanes
aircraft Aviat Various Airworthiness Directives; Bombardier, Inc. Model DHC-8-400 Series Airplanes

Unsafe Condition

Cracked nacelle attachment fittings due to stress corrosion, which could compromise structural integrity and affect safe landing.

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

Required Actions

Inspect nacelle attachment fittings for cracking and conduct conductivity checks. Replace fittings if cracking is found. Conduct repetitive detailed inspections if certain conductivity results are detected.

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, Inc. Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serial numbers 4001 and subsequent.

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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