# Airworthiness Directives; Boeing Model 777-200 Series Airplanes
> **Rule** · Final rule. · Published 1999-06-30 · Effective 1999-08-04 · 64 FR 34979
## Document
- **Document number:** 99-16324
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 777-200 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 64 FR 34979
- **Publication date:** 1999-06-30
- **Effective date:** 1999-08-04
- **FAA docket:** Docket No. 98-NM-243-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 777-200 series airplanes, that requires inspections to verify correct installation of certain fasteners located on the trailing edges of the horizontal and vertical stabilizer; replacement of the existing fasteners with new fasteners installed with wet sealant; and follow-on actions, if necessary. This amendment is prompted by reports indicating that, during manufacture of the horizontal and vertical stabilizers, certain fasteners attaching the aluminum ribs and brackets to the trailing edges on the empennage were not correctly installed with wet sealant. The actions specified by this AD are intended to prevent corrosion and possible cracking of those aluminum parts, which could result in loss of the attachment of the elevator and rudder to the empennage and consequent reduced controllability of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1999/06/30/99-16324/airworthiness-directives-boeing-model-777-200-series-airplanes)
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