AD 47-25-05

final rule
Data completeness: 60%

Airworthiness Directives; Culver Models V and V2 and V2 Aircraft

AD Number
47-25-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Superior Aircraft Company V Airworthiness Directives; Culver Models V and V2 and V2 Aircraft
aircraft Superior Aircraft Company V-2 Airworthiness Directives; Culver Models V and V2 and V2 Aircraft

Unsafe Condition

Corrosion and pitting on the nose-main gear interconnection tube's unpainted aft end, which slides through a trunnion, may cause binding and failure of the landing gear retracting system.

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

Required Actions

Inspect the nose-main gear interconnection tube for corrosion every 50 hours of operation. Apply ANG-3a grease to the unpainted aft end. Replace the tube if pitting or scaling is found.

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

Compliance Time

every 50 hours of operation

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

Affected Aircraft

Superior Aircraft Company Models V, V2, and V2 Aircraft

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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