Regulacje i polityka gospodarcza · 2.12.1996

Airworthiness Directives; Textron Lycoming Reciprocating Engines

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 96-23-03 that was sent previously to all known U.S. owners and operators of Textron Lycoming IO-320, LIO- 320, AEIO-320, IO- 360, LIO-360, AEIO-360, HIO-360, TO-360, IO-540, O- 540-L, LIO-540, and AEIO-540 series reciprocating engines by individual letters. This AD requires a maintenance records check to determine if suspect high pressure fuel pumps are installed, and inspection to determine if the high pressure fuel pump has one of the suspect date codes. If the high pressure fuel pump has a suspect date code, this AD requires disassembly and inspection of the high pressure fuel pump, and, if necessary, removal from service and replacement with a serviceable part. In addition, this AD requires reporting findings of unserviceable high pressure fuel pumps. This amendment is prompted by reports of inflight failures of high pressure fuel pumps. The actions specified by this AD are intended to prevent an inflight engine failure due to fuel starvation, which could result in a forced landing.