Narrative:

After takeoff from mci and climbing through about 12000 ft in clean confign, noticed #1 engine hydraulic low pressure light and then system 'a' quantity at '0'. #2 light then came on. We had lost all system 'a' hydraulic pressure. We ran the checklist and visually inspected the leading edge flaps on left and right side because we also had leading edge flap amber light on forward instrument panel and #2 and #6 kruger flap indicator lights on the flight engineer indicator panel on. We then conferred with maintenance in iah and dispatch for extra fuel burn at FL290 and determined it was safe to continue to ewr. Declared an emergency with ZNY and accomplished all appropriate checklists. We also discussed a go around for this situation and asked for emergency trucks and ground handling. We landed without further incident and were towed into gate at ewr. The 3-MAN crew coordination worked very well. It was the first officer who brought up a possible go around which was an excellent idea. One never knows. The only other unusual aspect of this incident was a thumping noise for the first maybe 10-15 mins back at mid-cabin. Possibly the #1 hydraulic drive motor (it was the cause of the problem) cavitating. This went away. Supplemental information from acn 250896: problem: mechanical failure of pump.

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Original NASA ASRS Text

Title: FLC OF LGT ACR ACFT EXPERIENCED MAIN SYS HYD FAILURE DURING CLBOUT AND CONTINUED ON TO DEST WHERE AN EMER WAS DECLARED FOR ATC HANDLING AND FIRE RESCUE EQUIP STANDBY.

Narrative: AFTER TKOF FROM MCI AND CLBING THROUGH ABOUT 12000 FT IN CLEAN CONFIGN, NOTICED #1 ENG HYD LOW PRESSURE LIGHT AND THEN SYS 'A' QUANTITY AT '0'. #2 LIGHT THEN CAME ON. WE HAD LOST ALL SYS 'A' HYD PRESSURE. WE RAN THE CHKLIST AND VISUALLY INSPECTED THE LEADING EDGE FLAPS ON L AND R SIDE BECAUSE WE ALSO HAD LEADING EDGE FLAP AMBER LIGHT ON FORWARD INST PANEL AND #2 AND #6 KRUGER FLAP INDICATOR LIGHTS ON THE FE INDICATOR PANEL ON. WE THEN CONFERRED WITH MAINT IN IAH AND DISPATCH FOR EXTRA FUEL BURN AT FL290 AND DETERMINED IT WAS SAFE TO CONTINUE TO EWR. DECLARED AN EMER WITH ZNY AND ACCOMPLISHED ALL APPROPRIATE CHKLISTS. WE ALSO DISCUSSED A GAR FOR THIS SIT AND ASKED FOR EMER TRUCKS AND GND HANDLING. WE LANDED WITHOUT FURTHER INCIDENT AND WERE TOWED INTO GATE AT EWR. THE 3-MAN CREW COORD WORKED VERY WELL. IT WAS THE FO WHO BROUGHT UP A POSSIBLE GAR WHICH WAS AN EXCELLENT IDEA. ONE NEVER KNOWS. THE ONLY OTHER UNUSUAL ASPECT OF THIS INCIDENT WAS A THUMPING NOISE FOR THE FIRST MAYBE 10-15 MINS BACK AT MID-CABIN. POSSIBLY THE #1 HYD DRIVE MOTOR (IT WAS THE CAUSE OF THE PROB) CAVITATING. THIS WENT AWAY. SUPPLEMENTAL INFO FROM ACN 250896: PROB: MECHANICAL FAILURE OF PUMP.

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.