# Airworthiness Directives; Boeing Model 747-200, -300, and -400 Series Airplanes
> **Rule** · Final rule. · Published 1996-11-06 · Effective 1996-12-06 · 61 FR 57291
## Document
- **Document number:** 96-26952
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 61 FR 57291
- **Publication date:** 1996-11-06
- **Effective date:** 1996-12-06
- **FAA docket:** Docket No. 94-NM-226-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747-200, -300, and -400 series airplanes, that requires modification of the left and right inboard elevator servo assemblies and the hydraulic routing of the right inboard elevator power control package (PCP). This amendment is prompted by a report of an uncommanded right elevator deflection after takeoff and reports of elevator/control column bumps during landing gear retraction on these airplanes. The actions specified by this AD are intended to prevent uncommanded elevator deflection, which could result in structural damage and reduced controllability of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1996/11/06/96-26952/airworthiness-directives-boeing-model-747-200--300-and--400-series-airplanes)
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