AD 53-11-02

final rule
Data completeness: 60%

Airworthiness Directives; de Havilland Model DHC-2 (Beaver) Aircraft

AD Number
53-11-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Viking Air Limited DHC-2 Mk.I Airworthiness Directives; de Havilland Model DHC-2 (Beaver) Aircraft
aircraft Viking Air Limited DHC-2 Mk.II Airworthiness Directives; de Havilland Model DHC-2 (Beaver) Aircraft
aircraft Viking Air Limited DHC-2 Mk.III Airworthiness Directives; de Havilland Model DHC-2 (Beaver) Aircraft

Unsafe Condition

Chafing of the engine oil sump by section assemblies (P/N C2-E-105ND and C2-E-107ND) of the accessory firewall.

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

Required Actions

Incorporate an enlarged flange clearance as soon as possible but not later than the next 100 hours.

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

Compliance Time

not later than the next 100 hours

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

Affected Aircraft

de Havilland Model DHC-2 (Beaver) Aircraft, Serial Numbers 1 to 445 Inclusive.

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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