# Proposed AD FAA-2006-25554: Lockheed Model L-1011 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2006-25-11
- Products: Lockheed
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: August 9, 2006, 71 FR 45447
- Comments due: September 25, 2006
- Became: [AD 2006-25-11](https://openairdocs.org/ad/2006-25-11)
- Docket: FAA-2006-25554 (https://www.regulations.gov/docket/FAA-2006-25554, where comments are filed)
- Project: 2006-NM-123-AD
- FR document: E6-12948
- Official PDF: https://openairdocs.org/files/sha256/75/a3/75a378a2025c3ac95e0cd23aac424f89e25b71437e093291d30fc12ceb6dcc75 (from https://www.govinfo.gov/content/pkg/FR-2006-08-09/pdf/E6-12948.pdf)
- Federal Register: https://www.federalregister.gov/documents/2006/08/09/E6-12948/airworthiness-directives-lockheed-model-l-1011-series-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/108E0ACBEC76F89A862571C500551CD7.0001
- Page: https://openairdocs.org/proposed/FAA-2006-25554

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Lockheed Model L-1011 series airplanes. This proposed AD would require a one-time detailed inspection of the C112 harness clamp assembly for proper installation, a one-time detailed inspection of the C112 and C162 harness assemblies for damage, and corrective actions if necessary. This proposed AD results from a report of electrical arcing of the essential bus feeder cables behind hinged circuit breaker panel CB3 P-K. We are proposing this AD to prevent arcing of essential bus feeder cables due to improper installation of the harness C112 clamp assembly, which could result in loss of electrical systems and smoke and/or fire behind the CB3 P-K hinged circuit breaker panel in the flight compartment.

## Notices in this docket

- Aug 9, 2006: Notice of proposed rulemaking (NPRM). (first notice), FR document E6-12948, comments due Sep 25, 2006 (https://www.federalregister.gov/documents/2006/08/09/E6-12948/airworthiness-directives-lockheed-model-l-1011-series-airplanes)

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