AN ATR72 ENG FIRE DEVELOPED DURING START AFTER THE PROP BRAKE APPARENTLY DID NOT RELEASE. THE EXTINGUISHING AGENT PUT OUT THE FIRE AS PAX WERE EVACUATING.

Date: 2007-11 · Aircraft: ATR 72 · Phase: ground

Anomalies: aircraft-equipment-problem-critical|flight-deck-cabin-aircraft-event-smoke-fire-fumes-odor

Synopsis

AN ATR72 ENG FIRE DEVELOPED DURING START AFTER THE PROP BRAKE APPARENTLY DID NOT RELEASE. THE EXTINGUISHING AGENT PUT OUT THE FIRE AS PAX WERE EVACUATING.

Narrative

ACFT WAS CLRED FOR PUSHBACK TAIL N. AFTER PUSH; PARKING BRAKE WAS SET. AUX PUMP WAS DEPRESSED BEFORE PUSH WAS COMPLETED TO INCREASE HYD PRESSURE. RECEIVED PROP BRAKE READY LIGHT. GAVE SIGNAL TO GND CREW TO CLR TO SPIN #2 PROP. AFTER RECEIVING CLRNC TO SPIN PROP; REQUESTED FO TO CLR R. AT THIS TIME; PROP BRAKE SWITCH WAS SET TO UNLOCK. PROP STABILIZED AT 13% NP. AFTER WHICH; R CONDITION LEVER WAS ADVANCED TO MAX RPM. PROP WAS SLOW TO SPIN UP. REQUESTED GND CREW TO STAND BY. APPROX 20 SECONDS LATER; RECEIVED PROP BRAKE WARNING. BROUGHT CONDITION LEVER TO FEATHER AND THEN TO SHUT OFF. DURING THIS TIME; THE CAPT AND FO SMELLED SMOKE. CONTACTED FLT ATTENDANT TO INVESTIGATE POSSIBLE SMOKE FROM #2 ENG; AND THEY RPTED SMELLING SMOKE. APPROX 2 SECONDS AFTER ENG SHUTDOWN; RECEIVED #2 ENG FIRE WARNING. COMMENCED IMMEDIATE ACTION ITEMS AND REFED QRH. FIRE WAS EXTINGUISHED AFTER AGENT #1 WAS DEPRESSED. WHEN READY TO MAKE PA; NOTICED THAT PAX WERE IN THE PROCESS OF EVACING IN AN ORDERLY MANNER. REQUESTED FO TO ENSURE THAT ALL PAX HAVE DEPLANED AND TAKE FIRE EXTINGUISHER. CONTACTED RAMP; OPS; AND FLT CTL OF SITUATION. FO RETURNED TO FLT DECK TO ASSIST IN SECURING ACFT. NO INJURIES WERE RPTED. I BELIEVE THAT THE PROP BRAKE SOMEHOW FAILED TO FULLY DISENGAGE. THIS CAUSED THE ALLEGED SPARKS FROM THE ENG FOLLOWED WITH ENG FIRE. A SLOW TO RISE NP IS NOT NECESSARILY UNIQUE; SO A CHANGE IN RESPONSE FROM THE FLT CREW IS NOT WARRANTED; IN MY OPINION. THE POTENTIAL PROB WITH THE PROP BRAKE MAY HAVE BEEN CAUSED BY ONE OF SEVERAL WAYS. ONE POSSIBILITY IS A MALFUNCTION WITH THE MFC'S (MULTI-FUNCTION COMPUTER). ANOTHER IS WITHIN THE PROP BRAKE.

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Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.