AD Amdt-39-9886

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Aircraft, Inc. SA26, SA226, and SA227 Series Airplanes

AD Number
Amdt-39-9886
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-CE-64-AD
FR Citation
62 FR 2552

Applicability

TypeManufacturerModelDetails
aircraft Fairchild Various Airworthiness Directives; Fairchild Aircraft, Inc. SA26, SA226, and SA227 Series Airplanes

Unsafe Condition

Looseness or movement of the control column pitch bearing attaching nuts and creasing of the elevator control rod end bearing retainer/dust seals could lead to loss of pitch control.

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

Required Actions

Apply torque to the control column pitch bearing attaching nuts, inspect for looseness or movement of the bearing assembly, and inspect elevator control rod end bearing retainer/dust seals for creasing. Replace parts if issues are found, install new bolt and washer at the walking beam connection.

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

Fairchild Aircraft, Inc. SA26, SA226, and SA227 series 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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