# SAIB NE-06-02: 

- Type: Special airworthiness information bulletin (advisory, not mandatory)
- Status: Current
- Revision: 0
- Issued: October 18, 2005
- Products: CFM International CFM56-2, CFM56-3 and CFM56 -5
- Product type: Engine
- PDF: https://openairdocs.org/files/sha256/f7/c9/f7c9bf356cb40b25c2d1055a679b01cbd529fc3173f23f8a062606f27dd90442
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/38A8DF13723708A18625721F0052EB0B.0001
- Page: https://openairdocs.org/saib/NE-06-02

## Text

**SPECIAL AIRWORTHINESS**

**INFORMATION BULLETIN**

Aircraft Certification Service Washington, DC

U.S. Department of Transportation Federal Aviation Administration

NE-06-02 October 18, 2005 http://www.faa.gov/aircraft/safety/alerts/SAIB This is information only. Recommendations aren’t mandatory.

Introduction

This Special Airworthiness Information Bulletin alerts you, owners, operators, and certificated repair facilities of CFM International, S.A. Model CFM56-2, -3, & -5 engines of issues regarding in-flight turnbacks resulting from the failure of variable bleed valve actuation shafts. These shafts transmit power from the hydraulic gear motor to the master ballscrew actuator to operate the variable bleed valve.

Background

In April 2004, a flexshaft manufacturer was notified of possible failure of two flexshafts at one airline at 3500 cycles-since-new (CSN) and 3600 CSN. We have received reports of at least seven additional failures. Analysis at the airline determined that the failure might have been caused by either mis-alignment or overtorqueing of the flexshaft during installation.

Either or both of these installation conditions can add additional loads, which can lead to failure of the flexshaft.

Recommendations

We recommend that when installing any flexshaft (either a new replacement flexshaft or re-installing the flexshaft during a maintenance activity), you ensure the proper alignment of the flexshaft and that you use the correct torque values when tightening all fasteners and connections.

Following proper alignment and torqueing procedures will minimize additional loads on the flexshaft, thus reducing the risk of flexshaft failure and the potential for an in-flight turnback.

For Further Information Contact

Frank Stadmeyer, Aerospace Engineer, FAA Engine and Propeller Directorate, Engine Certification Office, ANE-141, 12 New England Executive Park, Burlington, MA 01803-5213; phone: (781) 238-7763; email:

francis.stadmeyer@faa.gov

## Registered aircraft it may concern (OpenAirDocs)

Registry models matched by make and model, the same way as ADs, most registered aircraft first.

- [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series): 708 registered aircraft (engine model)
- [CFM International CFM56-3 series](https://openairdocs.org/engine/cfm-international-cfm56-3-series): 1 registered aircraft (engine model)
- [CFM International CFM56-2 series](https://openairdocs.org/engine/cfm-international-cfm56-2-series): 0 registered aircraft (engine model)
- [CFM International CFM56-5 series](https://openairdocs.org/engine/cfm-international-cfm56-5-series): 0 registered aircraft (engine model)

---
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.