Narrative:

On climb out, MFDU alert hydraulic system #2 low quantity. Reservoir had approximately 30% for system #2. We completed the procedure shutting off system #2 engine 1/2 pumps. We then took vectors direct dfw and declared an emergency. We got vectors direct runway 17C dfw. Approach and landing were uneventful except 7 units of left wing down trim was required. Callback conversation with reporter of acn 479149 revealed the following information: reporter said that on postflt inspection there appeared to be a leak in the area of the rudder power unit accounting for the loss of hydraulic fluid. With the fluid loss there is loss of one aileron but that should not have accounted for the amount of trim required. He suspects the failure of the rudder out of the faired position may have been the problem with trim.

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Original NASA ASRS Text

Title: F100 HYD LOSS DUE TO LEAK IN RUDDER PWR UNIT.

Narrative: ON CLBOUT, MFDU ALERT HYD SYS #2 LOW QUANTITY. RESERVOIR HAD APPROX 30% FOR SYS #2. WE COMPLETED THE PROC SHUTTING OFF SYS #2 ENG 1/2 PUMPS. WE THEN TOOK VECTORS DIRECT DFW AND DECLARED AN EMER. WE GOT VECTORS DIRECT RWY 17C DFW. APCH AND LNDG WERE UNEVENTFUL EXCEPT 7 UNITS OF L WING DOWN TRIM WAS REQUIRED. CALLBACK CONVERSATION WITH RPTR OF ACN 479149 REVEALED THE FOLLOWING INFO: RPTR SAID THAT ON POSTFLT INSPECTION THERE APPEARED TO BE A LEAK IN THE AREA OF THE RUDDER PWR UNIT ACCOUNTING FOR THE LOSS OF HYD FLUID. WITH THE FLUID LOSS THERE IS LOSS OF ONE AILERON BUT THAT SHOULD NOT HAVE ACCOUNTED FOR THE AMOUNT OF TRIM REQUIRED. HE SUSPECTS THE FAILURE OF THE RUDDER OUT OF THE FAIRED POS MAY HAVE BEEN THE PROB WITH TRIM.

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.