# Proposed AD 98-ANE-41-AD: General Electric Company CF6-6, CF6-45, and CF6-50 Series Turbofan Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2000-08-11
- Products: General Electric
- Product type: Engine
- Action: Notice of proposed rulemaking (NPRM).
- Published: October 5, 2001, 66 FR 50912
- Comments due: December 4, 2001
- Became: [AD 2000-08-11](https://openairdocs.org/ad/2000-08-11)
- Docket: 98-ANE-41-AD
- FR document: 01-25077
- Official PDF: https://openairdocs.org/files/sha256/86/69/8669db2b60b936535ddff3dcc3356d002eb8d9d8d58b1e92a912dbc9a832a84a (from https://www.govinfo.gov/content/pkg/FR-2001-10-05/pdf/01-25077.pdf)
- Federal Register: https://www.federalregister.gov/documents/2001/10/05/01-25077/airworthiness-directives-general-electric-company-cf6-6-cf6-45-and-cf6-50-series-turbofan-engines
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6A7B9361DC8B991086256AE0005F17E4.0001
- Page: https://openairdocs.org/proposed/98-ANE-41-AD

## Summary

The Federal Aviation Administration (FAA) proposes to supersede an existing airworthiness directive (AD), applicable to General Electric Company (GE) CF6-6, CF6-45, and CF6-50 series turbofan engines, that currently requires revisions to the Time Limits Section of the manufacturer's Instructions for Continued Airworthiness (ICA) to include required inspection of selected critical life-limited parts at each piece-part exposure. This proposal would modify the airworthiness limitations section of the manufacturer's manual and an air carrier's approved continuous airworthiness maintenance program to incorporate additional inspection requirements. A Federal Aviation Administration (FAA) study of in-service events involving uncontained failures of critical rotating engine parts has indicated the need for mandatory inspections. The mandatory inspections are needed to identify those critical rotating parts with conditions, which if allowed to continue in service, could result in uncontained failures. The actions specified by this proposed AD are intended to prevent critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.

## Notices in this docket

- Jul 28, 1998: Notice of proposed rulemaking (NPRM). (first notice), FR document 98-19628, comments due Oct 26, 1998 (https://www.federalregister.gov/documents/1998/07/28/98-19628/airworthiness-directives-general-electric-company-cf6-6-cf6-45-and-cf6-50-series-turbofan-engines)
- Oct 7, 1999: Notice of proposed rulemaking (NPRM)., FR document 99-26209, comments due Dec 6, 1999 (https://www.federalregister.gov/documents/1999/10/07/99-26209/airworthiness-directives-general-electric-company-cf6-6-cf6-45-and-cf6-50-series-turbofan-engines)
- Oct 5, 2001: Notice of proposed rulemaking (NPRM)., FR document 01-25077, comments due Dec 4, 2001 (https://www.federalregister.gov/documents/2001/10/05/01-25077/airworthiness-directives-general-electric-company-cf6-6-cf6-45-and-cf6-50-series-turbofan-engines)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.