AD 99-13-04

final rule
Data completeness: 70%

Airworthiness Directives; Cessna Models 206H and T206H Airplanes

AD Number
99-13-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
99-CE-23-AD
FR Citation
Federal Register: June 18, 1999 (Volume 64, Number 117)

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 206H Airworthiness Directives; Cessna Models 206H and T206H Airplanes
aircraft Cessna Aircraft Company T206H Airworthiness Directives; Cessna Models 206H and T206H Airplanes

Unsafe Condition

Loose aileron control bellcrank stop bolts could result in restricted movement of the ailerons with possible partial or complete loss of aileron control.

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

Required Actions

Inspect the left and right wing aileron control bellcrank stop bolts and lock nuts for flush and tight contact with the threaded boss on each end of the yoke assemblies. Accomplish follow-on and corrective actions as specified in Cessna Special Service Project SSP99-27-02.

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

Compliance Time

Within the next 10 hours time-in-service after the effective date or within 60 calendar days after the effective date, whichever occurs first.

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

Affected Aircraft

Cessna Models 206H (serials 20608002-20608026) and T206H (serials T20608002-T20608015, T20608017-T20608023, T20608025-T20608028).

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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