# Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
> **Rule** · Final rule; request for comments. · Published 2000-08-25 · Effective 2000-09-11 · 65 FR 51754
## Document
- **Document number:** 00-21616
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 65 FR 51754
- **Publication date:** 2000-08-25
- **Effective date:** 2000-09-11
- **FAA docket:** Docket No. 2000-NM-289-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Boeing Model 767-200, -300, and -300F series airplanes. This action requires a functional check of the shear rivets in all six elevator power control actuator (PCA) bellcrank assemblies to determine the condition of the shear rivets, and replacement or rework of the bellcrank assemblies, if necessary. This action is necessary to detect and correct any failed or partially yielded shear rivets of the elevator PCA bellcrank assemblies. Failure of two bellcrank assemblies on one side can result in that single elevator surface moving to a hardover position independent of pilot command resulting in a significant pitch upset recoverable by the crew. Failure of three bellcrank assemblies on one side may result in loss of controllability of the airplane. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/08/25/00-21616/airworthiness-directives-boeing-model-767-200--300-and--300f-series-airplanes)
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