AD 2002-12-11

Recurring final rule
Data completeness: 70%

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

AD Number
2002-12-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-69-AD
FR Citation
67 FR 42989

Applicability

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

Unsafe Condition

Cracking of the hook roller shafts of the flap carriage, which could result in reduced structural integrity of the flap and jamming.

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

Required Actions

Revise the applicable maintenance program manual. Perform repetitive inspections for corrosion or cracking of the hook roller shafts of the flap carriage. Replace the hook roller shafts with new or serviceable ones.

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

Compliance Time

Within 12 months of the effective date of the 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

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

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