Donald Neuhaus

Document ID: FAA-2008-1079-0005
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: November 17 2008, at 03:48 PM Eastern Standard Time
Date Posted: November 24 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: October 16 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: November 17 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 807ae7c6
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The FCU is subject to Fuel System Limitations (FSL) as defined in FAA AC 25.981-1B. FSLs are a means of identifying certain design configuration items related to fuel tank ignition source prevention features and Lightning /HIRF protection that require periodic inspection. An Equivalent Level of Safety (ELS) for Continued Airworthiness of the FCUs has previously been developed. The ELS requires a 10,000 FH interval “Safe-Life” test which includes a physical inspection of the FCU electrical components identified as having latent failure modes, and discovery of any overheating, charring, debris, or other suspicious conditions on the interior or exterior of the FCU. While returned units are routinely subjected to normal functional tests, the “Safe- Life” test and inspection contains additional electrical testing (i.e. tank short circuit protection testing) and physical inspections above and beyond the normal functional tests performed on returned units. Only if an FCU was (1) returned under a previous agreement to perform this 10,000 FH Safe Life Test, or (2) with an explicit request to perform this specific testing, can we be sure that both the additional testing and inspection have been performed and the FCU marked IAW the Service Bulletin.

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