# Proposed AD FAA-2011-0945: Honeywell International Inc. Turbofan Engines

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2012-16-14
- Products: Honeywell International
- Product type: Engine
- Action: Notice of proposed rulemaking (NPRM).
- Published: January 9, 2012, 77 FR 1043
- Comments due: March 9, 2012
- Became: [AD 2012-16-14](https://openairdocs.org/ad/2012-16-14)
- Docket: FAA-2011-0945 (https://www.regulations.gov/docket/FAA-2011-0945, where comments are filed)
- Project: 2011-NE-18-AD
- FR document: 2012-80
- Official PDF: https://openairdocs.org/files/sha256/07/0a/070a9b8f7cff68197938d0907d6e16fc843b3ba3e9af81408a0af64a9acee52f (from https://www.govinfo.gov/content/pkg/FR-2012-01-09/pdf/2012-80.pdf)
- Federal Register: https://www.federalregister.gov/documents/2012/01/09/2012-80/airworthiness-directives-honeywell-international-inc-turbofan-engines
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/86EA52B401A7972586257982004DCD75.0001
- Page: https://openairdocs.org/proposed/FAA-2011-0945

## Summary

We propose to adopt a new airworthiness directive (AD) for the products identified above. This proposed AD was prompted by a report of a quality escape of about 8,000 2nd stage low pressure turbine (LPT2) rotor blades, manufactured by Honeywell Chihuahua Manufacturing Operation since 2009. This proposed AD would require removing and inspecting certain LPT2 rotor blades. During LPT rotor acceleration, these blades may contact and damage the 3rd stage LPT (LPT3) nozzle seal carrier, which may subsequently fatigue and contact the adjacent rotor and damage the rotor. Also, these blades could deform the blade retainers, which could lead to blade movement that may cause rotor damage. We are proposing this AD to correct an unsafe condition caused by these blades installed on these engines.

## Notices in this docket

- Jan 9, 2012: Notice of proposed rulemaking (NPRM). (first notice), FR document 2012-80, comments due Mar 9, 2012 (https://www.federalregister.gov/documents/2012/01/09/2012-80/airworthiness-directives-honeywell-international-inc-turbofan-engines)

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