AD 2013-15-06

final rule
Data completeness: 80%

Airworthiness Directives; Bombardier, Inc. Airplanes

AD Number
2013-15-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2013-0298
FR Citation
79 FR 54891

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Various Airworthiness Directives; Bombardier, Inc. Airplanes

Unsafe Condition

Dual alternating current (AC) generator failure during flight, attributed to wire chafing along the wing lower flap shroud due to sagging wiring harnesses, missing teflon tape, and missing grommets.

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

Required Actions

Revise the maintenance program to incorporate tasks for the electrical wiring interconnection system inspection program.

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

Compliance Time

Within 12 months of the effective date (October 20, 2014).

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

Affected Aircraft

Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 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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