AD 2007-04-22

final rule
Data completeness: 80%

Airworthiness Directives; Bombardier Model DHC-8-102, -103, and -106 Airplanes; and Model DHC-8-200 and DHC-8-300 Series Airplanes

AD Number
2007-04-22
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. FAA-2006-26558
FR Citation
72 FR 8619

Applicability

TypeManufacturerModelDetails
aircraft Bombardier DHC-8-102 Airworthiness Directives; Bombardier Model DHC-8-102, -103, and -106 Airplanes; and Model DHC-8-200 and DHC-8-300 Series Airplanes

Unsafe Condition

Damage to the electrical cable harness assembly located on the left and right wing root-to-fuselage aft seal could lead to chafing or grounding of the wiring against the aft seal assemblies, potentially interrupting the operation of various systems, including the propeller feather control, AC electrical power, and standby hydraulic power.

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

Required Actions

Inspect the electrical cable harness assembly for damage on the left and right wing root-to-fuselage aft seal, and repair if necessary. Rework the fuselage aft seal assembly (left and right) to create a clearance between the electrical cable assemblies and the edge of the fairing panel.

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-8-102, -103, and -106 airplanes, as well as Model DHC-8-200 and DHC-8-300 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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