AD 2002-01-25

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Bombardier Model DHC-8-100, -200, and -300 Series Airplanes

AD Number
2002-01-25
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-112-AD
FR Citation
67 FR 4342

Applicability

TypeManufacturerModelDetails
aircraft Bombardier DHC-8-100 Airworthiness Directives; Bombardier Model DHC-8-100, -200, and -300 Series Airplanes

Unsafe Condition

Cracking of the rudder pedal adjustment fittings, which could lead to deformation of the fittings, resulting in jammed rudder pedals and loss of rudder control.

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

Required Actions

Inspect the rudder pedal adjustment fittings for cracks. Replace any cracked fittings with new fittings. An optional terminating action is also provided.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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

Affected Aircraft

Bombardier Model DHC-8-100, -200, and -300 series airplanes.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗ Find More ADs for Bombardier DHC-8-100

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