AD 2011-10-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna | Aircraft Company Models 150 | Airworthiness Directives; Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 Airplanes |
Unsafe Condition
Excessive wear on seat rail and seat rail holes, seat pin engagement, seat rollers, washers, axle bolts or bushings, wall thickness of roller housing and the tang, and lock pin springs may lead to seat slippage or the seat roller housing departing the seat rail, potentially causing the pilot/copilot to lose control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and replace parts as necessary, including the seat rail and seat rail holes; seat pin engagement; seat rollers, washers, and axle bolts or bushings; wall thickness of roller housing and the tang; and lock pin springs. Add steps to the inspection procedures, including inspections of the tang thickness and length on the seat roller housing. Revise figures for clearer inspection guidance.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 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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