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<blockquote data-quote="wuriburu" data-source="post: 257090" data-attributes="member: 322"><p>Se han cambiado ciertas partes de este motor que impulsa el I.A.63 ? </p><p></p><p>airworthiness Directives; Honeywell International Inc. (Formerly </p><p>AlliedSignal Inc. and Garrett Turbine Engine Co.). TFE731-2 and -3 </p><p>Series Turbofan Engines </p><p></p><p>AGENCY: Federal Aviation Administration (FAA), DOT. </p><p></p><p>ACTION: Notice of proposed rulemaking (NPRM). </p><p></p><p>----------------------------------------------------------------------- </p><p></p><p>SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) </p><p>for Honeywell International Inc. (formerly AlliedSignal Inc. and </p><p>Garrett Turbine Engine Co.) TFE731-2 and -3 series turbofan engines </p><p>with certain part numbers (P/Ns) and serial numbers (SNs) of low </p><p>pressure (LP) 1st and 2nd stage turbine rotor discs initially installed </p><p>as new parts before April 1, 1991. This proposed AD would require </p><p>replacement of those LP 1st and 2nd stage turbine rotor discs. This </p><p>proposed AD results from a report of an uncontained failure of an LP </p><p>2nd stage turbine rotor disc that caused an in-flight engine shutdown. </p><p>We are proposing this AD to prevent LP turbine rotor disk separation, </p><p>which could result in an uncontained engine failure and damage to the </p><p>airplane. </p><p></p><p>DATES: We must receive any comments on this proposed AD by August 30, </p><p>2004.</p></blockquote><p></p>
[QUOTE="wuriburu, post: 257090, member: 322"] Se han cambiado ciertas partes de este motor que impulsa el I.A.63 ? airworthiness Directives; Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Co.). TFE731-2 and -3 Series Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) for Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 series turbofan engines with certain part numbers (P/Ns) and serial numbers (SNs) of low pressure (LP) 1st and 2nd stage turbine rotor discs initially installed as new parts before April 1, 1991. This proposed AD would require replacement of those LP 1st and 2nd stage turbine rotor discs. This proposed AD results from a report of an uncontained failure of an LP 2nd stage turbine rotor disc that caused an in-flight engine shutdown. We are proposing this AD to prevent LP turbine rotor disk separation, which could result in an uncontained engine failure and damage to the airplane. DATES: We must receive any comments on this proposed AD by August 30, 2004. [/QUOTE]
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