SDR 2011F00022

Service difficulty report · Electronic Unit · Gulstm GIV

Difficulty date
January 25, 2011
Submitted
January 28, 2011
Operation
Air carrier
Aircraft
N450JE
Make and model
Gulstm GIV
Aircraft serial
1233
Aircraft time
8,130 hours, 2,759 cycles
Engine
Rroyce TAY6118
Engine time
7,801 hours, 2,650 cycles
Part
Electronic Unit
Part number
1159SCP01113
Part serial
1984
Condition
Intermittent
Location
Zone 500
Part time
8,130 hours, 2,759 cycles
Stage of operation
CL
How discovered
O
Nature of condition
G, R, J
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

IMMEDIATELY AFTER REACHING CRUISING ALTITUDE OF FL410, THE CREW NOTICED THE LT AUTOTHROTTLE ADVANCING FOLLOWED IMMEDIATELY BY A MASTER CAUTION CHIME/LIGHT. CAS MESSAGES OF LT FUEL PRESS LOW (RED CAPTION), LT MAIN FUEL FAIL (AMBER), LT ALT FUEL FAIL (AMBER). THE AUTOTHROTTLE ADVANCING WAS THE ENGINE STARVING FOR FUEL. THE PIC RETARDED THE ENGINE AND RETURNED TO DEPARTURE AIRPORT AND DECLARED AN EMERGENCY AS A PRECAUTION. AS THE ACFT DESCENDED, THE INDICATIONS CLEARED THEMSELVES AND AN UNEVENTFUL LANDING WAS MADE. THE MALFUNCTION OCCURRED ABOUT 21 MINUTES INTO THE FLIGHT UPON REACHING CRUISING ALTITUDE (FL410). TROUBLESHOOTING IN COOPERATION WITH THE MFG TECH DETERMINED THAT POWER WAS LOST TO BOTH LT WING BOOST PUMPS AND THAT THE LIKELY COMPONENT WAS AN INLINE FILTER (ELECTROMAGNETIC INTERFERENCE) AS IT IS THE ONLY PLACE WHERE BOTH SYSTEMS (MAIN AND ALT) ARE IN THE SAME LOCATION. THE SYS IS DESIGNED TO SELF FEED BELOW FL270 WHICH IS WHY THE MESSAGES EXTINGUISHED ON DESCENT. REPLACING THE FILTER PN 1159SCP011-13 AND PERFORMING A TEST FLIGHT PROVED A SUCCESSFUL RECTIFICATION.