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|
Attributes | |
ACN | 225592 |
Time | |
Date | 199210 |
Day | Mon |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : mem |
State Reference | TN |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | Large Transport, Low Wing, 3 Turbojet Eng |
Flight Phase | ground other : taxi |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : commercial pilot : flight engineer pilot : instrument pilot : atp |
Experience | flight time last 90 days : 185 flight time total : 11600 flight time type : 3300 |
ASRS Report | 225592 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : declared emergency other |
Consequence | other Other |
Supplementary | |
Primary Problem | Aircraft |
Narrative:
On taxi out for takeoff from mem, the #3 engine was being started as the aircraft was turning the corner up to the hold short line. As the turn was initiated, nosewheel steering was lost. The aircraft was stopped, parking brake set and the engine start was completed. At this time, the a system hydraulic annunciator lights on the first officer panel were illuminated, as well as both of the so panel a system low pressure lights, with a system hydraulic quantity 0 and pressure 0. At this time, we noticed smoke blowing from the right portion of the aircraft forward past the nose. We called ground control who confirmed that there was a substantial amount of smoke coming off the right wing. We requested crash crew assistance and told ground we might have to evacuate/evacuation the aircraft. I notified the flight attendant in charge to have the other flight attendants prepare for possible emergency evacuate/evacuation. The passenger were informed that we were aware of a problem and were investigating it. The so was sent back to the cabin to visually check the smoke's origin. The captain and first officer completed the emergency evacuate/evacuation checklist up to the point of initiating the evacuate/evacuation. When the APU fire handle was pulled as part of the evacuate/evacuation checklist, the smoke stopped almost immediately. An evacuate/evacuation was not initiated. The crash crew arrived within 3 mins of notification, company maintenance came out, pinned the gear and towed the aircraft back to the gate. The problem was caused by a cracked fitting on the landing gear control valve that dumped a system hydraulic fluid almost directly into the APU cooling air intake, causing the smoke. We came as close to an evacuate/evacuation as you can without actually doing it. As captain I was torn between a fear of ordering a possibly unnecessary evacuate/evacuation with potential injuries to passenger and the fear of hesitating too long with possible disastrous consequences. Good coordination with ground control, flight attendants but particularly among the 3 cockpit crewmembers, along with use of checklists and established procedures resulted in a satisfactory resolution to the problem with no injuries.
Original NASA ASRS Text
Title: LEAK OF HYD FLUID ONTO APU COOLING INTAKE CAUSES SMOKE, NEAR EVAC.
Narrative: ON TAXI OUT FOR TKOF FROM MEM, THE #3 ENG WAS BEING STARTED AS THE ACFT WAS TURNING THE CORNER UP TO THE HOLD SHORT LINE. AS THE TURN WAS INITIATED, NOSEWHEEL STEERING WAS LOST. THE ACFT WAS STOPPED, PARKING BRAKE SET AND THE ENG START WAS COMPLETED. AT THIS TIME, THE A SYS HYD ANNUNCIATOR LIGHTS ON THE FO PANEL WERE ILLUMINATED, AS WELL AS BOTH OF THE SO PANEL A SYS LOW PRESSURE LIGHTS, WITH A SYS HYD QUANTITY 0 AND PRESSURE 0. AT THIS TIME, WE NOTICED SMOKE BLOWING FROM THE R PORTION OF THE ACFT FORWARD PAST THE NOSE. WE CALLED GND CTL WHO CONFIRMED THAT THERE WAS A SUBSTANTIAL AMOUNT OF SMOKE COMING OFF THE R WING. WE REQUESTED CRASH CREW ASSISTANCE AND TOLD GND WE MIGHT HAVE TO EVAC THE ACFT. I NOTIFIED THE FLT ATTENDANT IN CHARGE TO HAVE THE OTHER FLT ATTENDANTS PREPARE FOR POSSIBLE EMER EVAC. THE PAX WERE INFORMED THAT WE WERE AWARE OF A PROBLEM AND WERE INVESTIGATING IT. THE SO WAS SENT BACK TO THE CABIN TO VISUALLY CHK THE SMOKE'S ORIGIN. THE CAPT AND FO COMPLETED THE EMER EVAC CHKLIST UP TO THE POINT OF INITIATING THE EVAC. WHEN THE APU FIRE HANDLE WAS PULLED AS PART OF THE EVAC CHKLIST, THE SMOKE STOPPED ALMOST IMMEDIATELY. AN EVAC WAS NOT INITIATED. THE CRASH CREW ARRIVED WITHIN 3 MINS OF NOTIFICATION, COMPANY MAINT CAME OUT, PINNED THE GEAR AND TOWED THE ACFT BACK TO THE GATE. THE PROBLEM WAS CAUSED BY A CRACKED FITTING ON THE LNDG GEAR CTL VALVE THAT DUMPED A SYS HYD FLUID ALMOST DIRECTLY INTO THE APU COOLING AIR INTAKE, CAUSING THE SMOKE. WE CAME AS CLOSE TO AN EVAC AS YOU CAN WITHOUT ACTUALLY DOING IT. AS CAPT I WAS TORN BTWN A FEAR OF ORDERING A POSSIBLY UNNECESSARY EVAC WITH POTENTIAL INJURIES TO PAX AND THE FEAR OF HESITATING TOO LONG WITH POSSIBLE DISASTROUS CONSEQUENCES. GOOD COORD WITH GND CTL, FLT ATTENDANTS BUT PARTICULARLY AMONG THE 3 COCKPIT CREWMEMBERS, ALONG WITH USE OF CHKLISTS AND ESTABLISHED PROCS RESULTED IN A SATISFACTORY RESOLUTION TO THE PROBLEM WITH NO INJURIES.
Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.