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|
Attributes | |
ACN | 643056 |
Time | |
Date | 200412 |
Day | Wed |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | atc facility : zzz.tracon |
Altitude | msl single value : 9000 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | artcc : zzz.artcc |
Operator | common carrier : air carrier |
Make Model Name | EMB ERJ 145 ER&LR |
Operating Under FAR Part | Part 121 |
Flight Phase | climbout : initial |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Experience | flight time last 90 days : 135 flight time total : 3500 flight time type : 1600 |
ASRS Report | 643056 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other anomaly other anomaly other |
Independent Detector | other flight crewa other flight crewb |
Resolutory Action | flight crew : overcame equipment problem flight crew : landed in emergency condition flight crew : declared emergency other |
Consequence | other other |
Supplementary | |
Problem Areas | Aircraft |
Primary Problem | Aircraft |
Narrative:
Passing through about 9000 ft MSL on climb out, we got bleed air leak message for both engines #1 and #2. While we were going through the checklist that dealt with this problem, we heard a loud pop, which was followed by smoke in the cockpit and cabin. We donned our oxygen masks, declared an emergency and turned back. With all bleed valves closed, the smoke did not seem to get worse and by the time we landed, only a strong odor remained. On our descent, we got a message saying the #1 radar altimeter had failed. TCASII, GPWS, and the landing gear warning system also failed since these are connected to the #1 radar altimeter. We later found that the leak had occurred in the ducting from the #1 engine. A large gap in the ducting was created when a clamp that holds together 2 pieces of tubing had broken. The air coming out of the leak from the #1 side was sufficient enough in volume and temperature to set off the leak sensor for the #2 engine bleed system. The leak sensors for the #1 and #2 sides were about 1.5 ft apart. The radar altimeter was located in this area. All of its external wiring connections had been melted. The only other damage found was done to the #1 bleed leak sensor.
Original NASA ASRS Text
Title: AN EMBRAER 145 #1 ENG BLEED AIR DUCT CLAMP FAILED DURING CLBOUT, FILLING THE COCKPIT AND CABIN WITH SMOKE AND FORCING THE CREW TO RETURN TO THE DEP ARPT.
Narrative: PASSING THROUGH ABOUT 9000 FT MSL ON CLBOUT, WE GOT BLEED AIR LEAK MESSAGE FOR BOTH ENGS #1 AND #2. WHILE WE WERE GOING THROUGH THE CHKLIST THAT DEALT WITH THIS PROB, WE HEARD A LOUD POP, WHICH WAS FOLLOWED BY SMOKE IN THE COCKPIT AND CABIN. WE DONNED OUR OXYGEN MASKS, DECLARED AN EMER AND TURNED BACK. WITH ALL BLEED VALVES CLOSED, THE SMOKE DID NOT SEEM TO GET WORSE AND BY THE TIME WE LANDED, ONLY A STRONG ODOR REMAINED. ON OUR DSCNT, WE GOT A MESSAGE SAYING THE #1 RADAR ALTIMETER HAD FAILED. TCASII, GPWS, AND THE LNDG GEAR WARNING SYS ALSO FAILED SINCE THESE ARE CONNECTED TO THE #1 RADAR ALTIMETER. WE LATER FOUND THAT THE LEAK HAD OCCURRED IN THE DUCTING FROM THE #1 ENG. A LARGE GAP IN THE DUCTING WAS CREATED WHEN A CLAMP THAT HOLDS TOGETHER 2 PIECES OF TUBING HAD BROKEN. THE AIR COMING OUT OF THE LEAK FROM THE #1 SIDE WAS SUFFICIENT ENOUGH IN VOLUME AND TEMP TO SET OFF THE LEAK SENSOR FOR THE #2 ENG BLEED SYS. THE LEAK SENSORS FOR THE #1 AND #2 SIDES WERE ABOUT 1.5 FT APART. THE RADAR ALTIMETER WAS LOCATED IN THIS AREA. ALL OF ITS EXTERNAL WIRING CONNECTIONS HAD BEEN MELTED. THE ONLY OTHER DAMAGE FOUND WAS DONE TO THE #1 BLEED LEAK SENSOR.
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.