AD 94-10-07

final rule
Data completeness: 70%

Airworthiness Directives; De Havilland Model DHC-8-301 Airplanes

AD Number
94-10-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
93-NM-203-AD
FR Citation
Federal Register: May 18, 1994 (Volume 59, Number 95)

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Inc. DHC-8-301 Airworthiness Directives; De Havilland Model DHC-8-301 Airplanes

Unsafe Condition

Inadequate venting between the cabin and compartments beneath the floor during rapid fuselage decompression could cause floor collapse and subsequent passenger injury.

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Required Actions

Modify the passenger cabin sidewall panels in accordance with de Havilland Service Bulletin No. 8-25-53 within 6 months after the effective date. Alternative methods of compliance may be approved by the FAA.

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Compliance Time

Within 6 months after the effective date of this AD

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Affected Aircraft

De Havilland Model DHC-8-301 airplanes; serial numbers 116 through 185 inclusive, 187, and 188; certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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