AD 99-18-14

final rule
Data completeness: 70%

Airworthiness Directives; Cessna Model 172R Airplanes

AD Number
99-18-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
99-CE-55-AD
FR Citation
Federal Register: September 1, 1999 (Volume 64, Number 169)

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 172R Airworthiness Directives; Cessna Model 172R Airplanes

Unsafe Condition

Incorrect length control yoke pivot bolts may come in contact with or rub on adjacent aileron control cables, which could result in loss of aileron control with loss of directional control of the airplane.

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

Required Actions

Inspect the control yoke pivot bolt to ensure positive clearance between the threaded end and aileron direct cable within 25 hours time-in-service after the effective date. If clearance is not found, replace the pivot bolt, inspect adjacent aileron control cables for damage, and replace any damaged cables before further flight.

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

Compliance Time

Within 25 hours time-in-service after the effective date

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

Affected Aircraft

Cessna Model 172R airplanes with serial numbers 17280003 through 17280016, 17280018 through 17280060, 17280062, 17280063, 17280065 through 17280071, 17280073 through 17280083, 17280085 through 17280088, 17280090, 17280091, and 17280093 through 17280096, equipped with Cessna Modification Kit MK 172-27-01 shipped between September 21, 1998, and April 18, 1999.

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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