# Proposed AD 2003-CE-47-AD: Goodrich Avionics Systems, Inc. TAWS8000 Terrain Awareness Warning System

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2004-08-15
- Products: Goodrich Avionics Systems
- Product type: Appliance
- Action: Notice of proposed rulemaking (NPRM).
- Published: December 3, 2003, 68 FR 67611
- Comments due: February 2, 2004
- Became: [AD 2004-08-15](https://openairdocs.org/ad/2004-08-15)
- Docket: 2003-CE-47-AD
- FR document: 03-30074
- Official PDF: https://openairdocs.org/files/sha256/61/c5/61c544be860d4634c533c3a108e1dd80dbe1c96fada7bf49df9398482a47f0f2 (from https://www.govinfo.gov/content/pkg/FR-2003-12-03/pdf/03-30074.pdf)
- Federal Register: https://www.federalregister.gov/documents/2003/12/03/03-30074/airworthiness-directives-goodrich-avionics-systems-inc-taws8000-terrain-awareness-warning-system
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A69D89AB9241835586256DF1005BAC64.0001
- Page: https://openairdocs.org/proposed/2003-CE-47-AD

## Summary

The FAA proposes to supersede airworthiness directive (AD) 2003-13-08, which currently applies to all Goodrich Avionics Systems, Inc. (Goodrich) TAWS8000 terrain awareness warning systems (TAWS) that are installed on airplanes. AD 2003-13-08 currently requires you to inspect the TAWS installation and remove any TAWS where both the TAWS and any other device are connected to the same baro set potentiometer. AD 2003-13-08 also prohibits future installation of any TAWS8000 TAWS that incorporates hardware "Mod None", "Mod A", or "Mod B". This proposed AD is the result of omitting from AD 2003-13-08 a provision that prohibits reconfiguring an installed TAWS8000 TAWS after it passes the inspection unless it incorporates hardware "Mod C". This proposed AD would retain the actions of AD 2003-13-08 and would also prohibit future installation or reconfiguration of any TAWS8000 TAWS that does not incorporate hardware "Mod C". We are issuing this proposed AD to prevent the loading of the baro set potentiometer, which could result in an unacceptable altitude error. That condition could cause the pilot to make flight decisions that put the airplane in unsafe flight conditions.

## Notices in this docket

- Dec 3, 2003: Notice of proposed rulemaking (NPRM). (first notice), FR document 03-30074, comments due Feb 2, 2004 (https://www.federalregister.gov/documents/2003/12/03/03-30074/airworthiness-directives-goodrich-avionics-systems-inc-taws8000-terrain-awareness-warning-system)

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