AD 2009-06-21
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | DHC-8-102 | Airworthiness Directives; Bombardier Model DHC-8-102, -103, and -106 Airplanes, and Model DHC-8-200, -300, and -400 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Bombardier Model DHC-8-102, -103, and -106 Airplanes, and Model DHC-8-200, -300, and -400 Series Airplanes |
Unsafe Condition
An incorrectly assembled fuselage spoiler cable disconnect sensing device, where a pulley and plastic spacer were inadvertently interchanged during production, resulting in the spoiler cable sliding on the spacer rather than the pulley as designed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the fuselage spoiler cable disconnect sensing device for correct assembly. If necessary, inspect components for wear and damage, replace worn or damaged components, and correctly re-assemble the sensing device.
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 for specific aircraft models.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, -315 series airplanes, serial numbers 003 through 644 inclusive, and Model DHC-8-400, -401, and -402 series airplanes, serial numbers 4003, 4004, 4006, and 4008 through 4164 inclusive.
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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