AD 72-07-11

final rule
Data completeness: 70%

Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes

AD Number
72-07-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Revo, Incorporated Colonial C-1 Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes
aircraft Revo, Incorporated Colonial C-2 Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes
aircraft Revo, Incorporated Lake LA-4 Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes
aircraft Revo, Incorporated Lake LA-4-200 Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes
aircraft Revo, Incorporated Lake LA-4A Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes
aircraft Revo, Incorporated Lake LA-4P Airworthiness Directives; Consolidated Aeronautics Model Colonial C-1, Colonial C-2, Lake LA-4, LA-4A, LA- 4P and LA-4-200 Airplanes

Unsafe Condition

Failure of the rod-end bearing, P/N HM-5C, connected to the flap pushrod, P/N 2-7811-21, which could result in hazards in flight due to corrosion, cracks, or binding of the ball motion.

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

Required Actions

Within 15 hours in service after the effective date, inspect the rod-end bearing P/N HM-5C for corrosion and ball motion using visual and 10-power glass inspection. Replace corroded, cracked, or binding parts before further flight. Lubricate the ball before reinstallation. Discontinue inspections if P/N HM-5G or equivalent is installed.

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

Compliance Time

within the next 15 hours in service after the effective date of this AD, unless already accomplished within the last 10 hours in service, and at intervals thereafter not to exceed 25 hours in service from the last inspection

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

Affected Aircraft

Consolidated Aeronautics Model Colonial C-1, C-2, and Lake Model LA-4, LA-4A, LA-4P, and LA-4-200 airplanes below serial number 503 with Flap Actuator Pushrod Assembly, Lake Aircraft Corporation P/N 2-7811-7

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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