# Airworthiness Directives; Airbus Model A310 Series Airplanes
> **Rule** · Final rule. · Published 2000-06-23 · Effective 2000-07-28 · 65 FR 39077
## Document
- **Document number:** 00-15307
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A310 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 39077
- **Publication date:** 2000-06-23
- **Effective date:** 2000-07-28
- **FAA docket:** Docket No. 2000-NM-77-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A310 series airplanes, that requires modification of the position 1 flap screw jack. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent fracture of the lead screw of the position 1 flap screw jack, which could result in failure of the tie bar and possible disconnection of the flap structure from the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/06/23/00-15307/airworthiness-directives-airbus-model-a310-series-airplanes)
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