AD 2008-21-07

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Dowty Propellers R408 Series Propellers

AD Number
2008-21-07
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. FAA-2008-1088
FR Citation
73 FR 61346

Applicability

TypeManufacturerModelDetails
aircraft Aviat Various Airworthiness Directives; Dowty Propellers R408 Series Propellers

Unsafe Condition

Three in-service propellers have been found to have blades which have lost the bonded metallic leading edge guard. If the leading edge guard comes off as the propeller turns, it could cause secondary damage to aircraft or injury to personnel.

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

Required Actions

Inspect all concerned blade assemblies where the bonded metallic L/E guard has accumulated 1,200 flight hours or less since installation, in accordance with Dowty Propellers ASB No. D8400-61-A69. Inspect the concerned blade assembly within 50 flight hours or 1 month after installing a replacement blade.

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

Compliance Time

Within 50 flight hours or within 1 month after the effective date of this AD, whichever occurs first.

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

Affected Aircraft

Dowty Propellers model R408/6-123-F/17 propellers with blades, part numbers 697071200-18, 697071210-18, 697071227-18, 697071240-18, 697071245-18, or 697071257-18, installed on Bombardier, Inc. (formerly de Havilland Canada) models DHC-8-400, DHC-8-401, and DHC-8-402 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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