AD Amdt-39-10524

final rule
Data completeness: 70%

Airworthiness Directives; REVO, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

AD Number
Amdt-39-10524
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-CE-48-AD
FR Citation
63 FR 26964

Applicability

TypeManufacturerModelDetails
aircraft Lake LA-4 Airworthiness Directives; REVO, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 Airplanes

Unsafe Condition

Fatigue cracks to the horizontal and vertical stabilizer attachment fitting could result in loss of control of the airplane.

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

Required Actions

Measure clearances between attachment fitting and horizontal stabilizer rear beam (minimum 5/32 inch) and stabilizer skin (minimum 1/16 inch). Remove affected horizontal tail half if clearances are insufficient, inspect attachment fitting for fretting, cracking, or corrosion. Replace attachment fitting if defects found and trim stabilizer skin to ensure clearance.

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

Compliance Time

Before further flight

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

Affected Aircraft

REVO, Incorporated Models Colonial C-2, Lake LA-4, Lake LA-4A, Lake LA-4P, and Lake LA-4-200 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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