AD 2012-16-16

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2012-16-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-1093
FR Citation
77 FR 50577

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Extensive corrosion of the ballscrew of the drive mechanism of the horizontal stabilizer trim actuator, which could lead to undetected failure of the primary and secondary load paths for the ballscrew in the horizontal stabilizer, resulting in loss of control of the horizontal stabilizer and consequent loss of control of the airplane.

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

Required Actions

Repetitive detailed inspections for discrepancies of the horizontal stabilizer ballscrew assembly; repetitive lubrication of the horizontal stabilizer trim control system; repetitive measurements for discrepancies of the ballscrew to ballnut freeplay; and corrective actions, if necessary.

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

Compliance Time

Within specified intervals (not detailed in the provided text).

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Affected Aircraft

All The Boeing Company Model 757 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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