# Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes
> **Rule** · Final rule. · Published 1999-03-26 · Effective 1999-04-30 · 64 FR 14580
## Document
- **Document number:** 99-7116
- **Category:** airworthiness
- **Manufacturer:** Lockheed Model L-1011-385 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 64 FR 14580
- **Publication date:** 1999-03-26
- **Effective date:** 1999-04-30
- **FAA docket:** Docket No. 96-NM-256-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Lockheed Model L-1011-385 series airplanes, that requires repetitive external visual inspections and internal borescope inspections to detect discrepancies of the elevator assembly; and either repair or repair/modification of certain identified discrepancies. This amendment is prompted by a report of fretting at the diagonal truss to web joint of the elevator and cracking in the cap fillet radius adjacent to the joint, apparently due to loose fasteners as a result of local vibration. The actions specified by this AD are intended to detect and correct such fretting and cracking, which could result in reduced structural integrity of the elevator and consequent flutter instability if coupled with other structural failures.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1999/03/26/99-7116/airworthiness-directives-lockheed-model-l-1011-385-series-airplanes)
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