# Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes
> **Rule** · Final rule. · Published 2000-09-01 · Effective 2000-10-06 · 65 FR 53157
## Document
- **Document number:** 00-22122
- **Category:** airworthiness
- **Manufacturer:** Lockheed Model L-1011-385 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 53157
- **Publication date:** 2000-09-01
- **Effective date:** 2000-10-06
- **FAA docket:** Docket No. 98-NM-314-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Lockheed Model L-1011-385 series airplanes, that requires modifications of the engine turbine cooling air panel at the flight engineer/second officer's console, pilot's caution and warning light panel on the main instrument panel, and monitoring system for the engine turbine air temperature. This amendment is prompted by reports of an undetected fire breaching the high speed gearbox (HSGB) case on certain Rolls Royce engines installed on in-service airplanes due to lack of an internal fire detection system within the HSGB. The actions specified by this AD are intended to prevent undetected fires originating within the HSGB from breaching the HSGB case, which could result in engine damage and increased difficulty in extinguishing a fire.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/09/01/00-22122/airworthiness-directives-lockheed-model-l-1011-385-series-airplanes)
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