# Proposed AD FAA-2006-24951: Gulfstream Model GV and GV-SP Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2006-18-13
- Products: Gulfstream Aerospace
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: June 6, 2006, 71 FR 32487
- Comments due: July 21, 2006
- Became: [AD 2006-18-13](https://openairdocs.org/ad/2006-18-13)
- Docket: FAA-2006-24951 (https://www.regulations.gov/docket/FAA-2006-24951, where comments are filed)
- Project: 2005-NM-184-AD
- FR document: E6-8711
- Official PDF: https://openairdocs.org/files/sha256/d9/ad/d9ada4b88cde7f8f549df0db98ded306d8be8c227baffd8761dd067d71212548 (from https://www.govinfo.gov/content/pkg/FR-2006-06-06/pdf/E6-8711.pdf)
- Federal Register: https://www.federalregister.gov/documents/2006/06/06/E6-8711/airworthiness-directives-gulfstream-model-gv-and-gv-sp-series-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5EB2E62480AA2B69862571850069C070.0001
- Page: https://openairdocs.org/proposed/FAA-2006-24951

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Gulfstream Model GV and GV-SP series airplanes. This proposed AD would require repairing the force link assembly wire harness. This proposed AD results from a report indicating that the wiring harness outer shield and insulation on the primary conductors may have been inadvertently cut due to an improper method used to remove the wiring outer jacket. We are proposing this AD to prevent the loss of the hardover prevention system (HOPS) in the roll axis due to a short circuit in the wiring harness, which could result in reduced controllability of the airplane.

## Notices in this docket

- Jun 6, 2006: Notice of proposed rulemaking (NPRM). (first notice), FR document E6-8711, comments due Jul 21, 2006 (https://www.federalregister.gov/documents/2006/06/06/E6-8711/airworthiness-directives-gulfstream-model-gv-and-gv-sp-series-airplanes)

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