# Proposed AD 99-NE-17-AD: Honeywell International Inc. Models LTS101-600A-2 and LTS101-600A-3 Turboshaft Engines; and LTP101-600A-1A and LTP101-700A-1A Turboprop Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2001-25-04
- Action: Notice of proposed rulemaking (NPRM).
- Published: March 12, 2001, 66 FR 14345
- Comments due: May 11, 2001
- Became: [AD 2001-25-04](https://openairdocs.org/ad/2001-25-04)
- Docket: 99-NE-17-AD
- FR document: 01-5738
- Official PDF: https://openairdocs.org/files/sha256/c1/db/c1db5cfed7cbbce24ecf37c9e59e797dd5ccab1a0a504f208e81aa1a2613fe67 (from https://www.govinfo.gov/content/pkg/FR-2001-03-12/pdf/01-5738.pdf)
- Federal Register: https://www.federalregister.gov/documents/2001/03/12/01-5738/airworthiness-directives-honeywell-international-inc-models-lts101-600a-2-and-lts101-600a-3
- Page: https://openairdocs.org/proposed/99-NE-17-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to Honeywell International Inc. (formerly AlliedSignal Inc. and Textron Lycoming) Models LTS101-600A-2 and LTS101-600A-3 turboshaft engines; and LTP101-600A-1A and LTP101- 700A-1A turboprop engines. This proposal would require replacing certain fuel controls that have beryllium-copper bellows with improved fuel controls that incorporate Inconel 718 stainless steel welded bellows. This proposal is prompted by a report of an uncommanded power loss on a Textron Lycoming LTS101 engine due to a corrosion damaged fuel control bellows. The actions specified by the proposed AD are intended to prevent the engine from reducing the fuel flow to minimum flow resulting in an uncommanded power loss.

## Notices in this docket

- Mar 12, 2001: Notice of proposed rulemaking (NPRM). (first notice), FR document 01-5738, comments due May 11, 2001 (https://www.federalregister.gov/documents/2001/03/12/01-5738/airworthiness-directives-honeywell-international-inc-models-lts101-600a-2-and-lts101-600a-3)

---
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.