John Joseph Bianco

Document ID: FAA-2013-0197-0002
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: April 11 2013, at 12:00 AM Eastern Daylight Time
Date Posted: April 15 2013, at 12:00 AM Eastern Standard Time
Comment Start Date: April 5 2013, at 12:00 AM Eastern Standard Time
Comment Due Date: June 4 2013, at 11:59 PM Eastern Standard Time
Tracking Number: 1jx-84py-ntfz
View Document:  View as format xml

View Comment

Gentlemen, I am the Principal Maintenance Inspector for Empire Airlines based in Hayden Idaho. On 11/15/2012, Empire Airlines, Inc. reported that one of their ATR 42's experienced what they believed to be an engine fire on the #1 engine.(PW121) The engine was shutdown and the aircraft landed safely. An engine tear down report recently received from Pratt & Whitney Canada revealed that a fracture of one LPT blade near the platform was by fatigue propagation from the trailing edge until final fracture by overload. The fatigue fracture most likely originated at the trailing edge tip from a casting anomaly that also resulted in the formation of numerous cracks. Summary: Pratt & Whitney report number: 13GS00001 high pressure turbine vane ring segment (HPT)---Heat eroded Low Pressure Turbine (LPT)---Fractured Based on the engineering analysis contained in this report I have to ask why this particular engine model was omitted from the affectivity list for the proposed AD?

Related Comments

   
Total: 1
John Joseph Bianco
Public Submission    Posted: 04/15/2013     ID: FAA-2013-0197-0002

Jun 04,2013 11:59 PM ET