N851GT

Part: PDU — FAULTED (TE FLAPS) · airframe 54,575 hrs · 8,508 cycles

FLAPS DRIVE CAUTION MSG.(<P>REMOVE &AMP; REPLACE #4 PDU FEEDBACK SWITCH ASSY PER AMM 27-88-01. REMOVED AND REPLACED #4L PDU PER AMM 27-81-03 APC 27-81-03-51. OPS CHECK GOOD. NO MESSAGES OR FAULTS NOTED.</P>)

Part: OUTFLOW VALVE — FAILED (ZONE 100) · airframe 54,027 hrs · 8,415 cycles

DURING CLIMB ON, THE CABIN WOULD NOT PRESSURIZE, STOPPED CLIMB AT 10,000, CAB ALT WAS 10300. DELTA P WAS 0.1 COULD NOT CONTROL THE CABIN PRESSURE IN MANUAL OR AUTO.(<P>REMOVED AND REPLACED R/H OUTFLOW VALVE IAW B747 AMM 21-31-01 UP TO SUBTASK 21-31-01-430-016. OPS CHECK GOOD.</P>)

Part: LINE — LOOSE (HYD SYSTEM) · airframe 53,452 hrs · 8,332 cycles

#1 ADP FAILED, LOSS OF HYDRAULIC FLUID. #1 EDP ON DEFERRAL PRIOR TO FLIGHT.(<P>R/R EDP PER AMM 29-11-05 &AMP; IPC 29-11-05-05, RETURN LINE FOUND LOOSE, LEADING TO FLUID LOSS. SCAVENGE FILTER CHECKED FOR DEBRIS, NONE FOUND. R/R RETURN MOD FILTER PER MCC REQUEST. FILTER FOUND NO CONTAMINATION PER AMM 29-11-29. DMI 221876 CLOSED</P>)

Part: OUTFLOW VALVE — FAULTED (CABIN PRESSURE) · airframe 51,726 hrs · 8,080 cycles

AIR TURN BACK UNABLE CRUISE ALTITUDE DUE TO PRESSURIZATION(<P>MIA MX PERFORMED INSPECTION OF EXTERIOR AND INTERIOR OF THE A/C, DOOR SEALS, A/C MANIFOLD DUCTING, NO ISSUES FOUND. R/R E/E FAN, R/R OVBD SOV, R/R X2 RELAYS FOR FWD CGO OVBD VALVE OPEN &AMP; CLOSE, &AMP; R/R FWD OVBD CGO VALVE</P>)

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 50,782 hrs · 7,950 cycles

RH HORIZONTAL STAB T/E ASSY CHANNEL FOUND CRACK(<P>BONDED NEW CHANNEL AS PER RI-55-10-16833 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: BEAM — CRACKED (RT WING) · airframe 50,782 hrs · 7,950 cycles

RHW L/E ILES 560 D BEAM WEB CRACKED(<P>RHW L/E ILES 560 D BEAM WEB REPAIRED AS PER RI-57-41-16827 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: INTERCOSTAL — DEFORMED (BS 1480-1520) · airframe 50,782 hrs · 7,950 cycles

FUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL, P/N: 65B07241-1 BETWEEN STA 1480 +60 TO STA 1520 LBL 45. DEFORMATION DAMAGE - TEMPORARY REPAIR REFER EA-4853A0088(<P>FUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL REPLACED AS PER SRM 51-10-02, SRM 51-40-02 AND RI-53-00-16832 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — WORN (NR 8 FLAP) · airframe 50,782 hrs · 7,950 cycles

#8 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,782 hrs · 7,950 cycles

RH FUS EMER SLIDE LT L6690 FOUND NOT ILLUMINATED(<P>R/H FUS EMER SLIDE LT L6690 LAMP REPLACED AND TEST IS NORMAL AS PER AMM 33-51-00 REV 44 15 MAR 2024.</P>)

Part: SKIN — WORN (NR 18 FLAP) · airframe 50,782 hrs · 7,950 cycles

#18 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPIAR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — WORN (NR 9 FLAP) · airframe 50,782 hrs · 7,950 cycles

#9 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — WORN (NR 19 FLAP) · airframe 50,782 hrs · 7,950 cycles

#19 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — WORN (NR 7 FLAP) · airframe 50,782 hrs · 7,950 cycles

#7 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,782 hrs · 7,950 cycles

EMERGENCY LIGHT ON THE TOP OF STAIRWAY FOUND INOP.(<P>LAMP OF EMERGENCY LIGHT ON THE TOP OF STAIRWAY REPLACED AND OPERATIONAL TEST NORMAL IAW AMM 33-51-07 REV 44, 15 MAR 2024</P>)

Part: NUT — UNKNOWN (FRAME) · airframe 50,782 hrs · 7,950 cycles

REFER JOB CARD SEQ 1.725 #1 CANOE AFT FRAME MOD FIG 6 INSTALLATION AFTER ROW HAS 5EA FASTENER HOLE LOCATION CAN NOT USE BACC30AC6 DUE HOLES TOO CLOSE TO ART INTERFERENCE COLLAR(<P>NUTS REPLACED AS PER RI-57-50-16856 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: CURTAIN — TORN (BS 2160) · airframe 50,782 hrs · 7,950 cycles

AFT CARGO COMPT STA 2160 END WALL CURTAIN FOUND TORN.(<P>AFT CARGO COMPT STA 2160 ENDWALL CURTAIN REPAIRED AS PER RI-25-52-16836 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — WORN (NR 20 FLAP) · airframe 50,782 hrs · 7,950 cycles

#20 V/C FLAP LSA FOUND WORN(<P>PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — ERODED (NR 10 FLAP) · airframe 50,782 hrs · 7,950 cycles

#10 V/C FLAP UPR EDGE FOUND EROSION(<P>PERFORMED REPAIR AT EROSION AREA IAW SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED</P>)

Part: BRACKET — UNKNOWN (UNKNOWN) · airframe 47,482 hrs · 7,507 cycles

FOUND THE GROUND PNEUMATIC DOOR GROUND SERVICE MISSING ON WALKAROUND(<P>FABRICATED THE BRACKET AS PER SERVICE REQUEST 270823140 AND DWG 69B11807 AND INSTALLED BRACKET AT NEW PNEUMATIC DOOR IAW SRM 51-40-02-01</P>)

Part: BRACKET — UNKNOWN (UNKNOWN) · airframe 47,467 hrs · 7,505 cycles

ENGINE START PNEUMATIC GROUND SERVICE DOOR MISSING.(<P>PERFORMED TIME LIMITED REPAIR PER EA-4852A0005 PART 1 (REV 0). FOLLOW UP REPAIR DUE NEXT F/C. PLACARD INSTALLED. TRANSFER TO DMI 188348 NON-MEL DUE DATE 6/30/2023.</P> / <P>LP 1620525 M9: FABRICATED THE BRACKET AS PER SERVICE REQUEST 270823140 AND DWG 69B11807 AND INSTALLED BRACKET AT NEW PNUEMATIC DOOR IAW SRM 51-40-02-01. DMI 188348 CLOSED</P>)

Part: WIRE — BROKEN (APU FIRE LOOP) · airframe 41,676 hrs · 6,670 cycles

APU FIRE DETECTOR LOOP A (W0906) WIRE FOUND BROKEN AT L/H AFT APU COMPT(<P>WIRE REPLACED BUT BEN-HAR SLEEVE TEMPOARY REPAIRED AS PER&NBSP;<SPAN>BOEING RDR NO.HKA-PAO-22-0028-07B</SPAN></P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

BULK CGO STA 2160 ENDWALL FOUND TORN AS MARKED(<P>BULK CGO STA 2160 ENDWALL REPAIRED AS PER RI-25-54-15456 REV.A</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

VERTICAL FIN FWD L/E FAIRING #321B FOUND DENT MARK(<P>DENT AREA REPAIRED AS PER SRM 55-30-01-2R-4 REPAIR 4 FIG.201</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

LHW L/E #7 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(<P><SPAN>LSA DAMAGED AREA PERFORMED REPAIR</SPAN></P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

LHW L/E #9 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(<P><SPAN>LSA DAMAGED AREA PERFORMED REPAIR</SPAN></P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

RH H.STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(<P>RH H.STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U12 WAS REPLACED AS PER RI NO. RI-55-10-15473 REV A AND INSTALL AS PER SRM 51-40-02 REV 36. DATE 20 FEB 2022.</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

#2 V/C FLAP BULLNOSE EDGE FOUND EROSION(<P>PERFORMED REPAIR AT ERODED AREA</P>)

Part: WEB — NONE · airframe 41,676 hrs · 6,670 cycles

R/H H.STAB, STAB BL 421.5 WEB CRACKED(<P>CRACK WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB INSTALLED AS PER SRM 51-40-02</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

LH H.STAB REAR WEB AT STA BL 391.9 ANGLE CRACKED.(<P>CRACK ANGLE LOCAL FABRICATED AS PER RI NO. RI-55-00-15458 REV A AND NEW ANLGE INSTALLED AS PER SRM 51-40-02.</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

R/H H-STAB STA BL 421.5 LOWER CHORD CRACKED(<P>LOWER CHORD CRACK AREA REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12,FIG.201,DETAIL VII</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

LHW L/E #8 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(<P><SPAN>LSA DAMAGED AREA PERFORMED REPAIR</SPAN></P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

LHW I/B T/E LWR PNL AT WS 129.86 TO 228.05 FWD SUPPORT BEAM O/B BRACKET CRACKED(<P>SUPPORT BEAM FITTING P/N : 115U2252-19 FASBRICATED AS PER RI NO.RI-57-00-15477 REV A AND BOEING DRAWING 115U2252-19PL</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

L/H BLG I/B TRUNNION SUPPORT FITTING AND LOWER CAP FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER SRM 53-40-90-2R-1 REPAIR 1 AND HAECO RI NO. RI-53-40-15465 REV.A</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

LHW L/E #6 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(<P>LSA DAMAGED AREA PERFORMED REPAIR</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

L/H STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(<P>LH STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U11 WAS REPLACED AS PER RI NO. RI-55-10-15472 REV A AND INSTALLED AS PER SRM 51-40-02 REV 36, DATE 20 FEB 2022.</P>)

Part: NONE — NONE · airframe 41,676 hrs · 6,670 cycles

R/H H.STAB BL 421.5 UPPER CHORD CRACKED.(<P>R/H H.STAB BL 421.5 UPPER CHORD REPLACED ACCOMPLISHED IAW SRM 51-40-02 AND SRM 51-40-05 REV 36, 20 FEB 2022&NBSP;</P>)

Part: FMC — NONE · airframe 41,063 hrs

RIGHT FMC FAILURE AFTER DEPARTURE, DUAL FMC FAILURE ENROUTE.(<P>REMOVED AND REPLACED RT FMC PERFORMED SOFTWARE CROSSLOAD &AMP; CONFIG CHECK , PERFORMED GROUND TESTS THROUGH CMC ALL TESTS PASSED PER AMM 34-61-01&NBSP; &NBSP;34-61-00-472-105&NBSP; &NBSP;34-61-000-752-101</P>)

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,200 hrs · 5,356 cycles

CRACK DAMAGE ON THE STRINGER S-10L BETWEEN STA 860 AND STA 900. ACCOMPLISHED EI NO T2020A53M-1390 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: ROTARY ACTUATOR — FAILED (LT WLG) · airframe 33,200 hrs · 5,356 cycles

LT WING ALTERNATE EXTEND SYSTEM OPERATIONAL TEST FAIL. IAW AMM 32-36-01-004-001 REV 32 AND AMM 32-36-01-404-009 REV 32 REPLACED LT WING ROTARY ACTUATOR. IAW AMM 32-36-00-705-009 REV 32 PERFORM WLG LT ALTERNATE EXTENSION SYSTEM OPERATIONAL TEST. RESULT WAS NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,200 hrs · 5,356 cycles

CRACK DAMAGES ON THE STRINGER S-9L BETWEEN STA 860 AND STA 900. REPAIRED DAMAGED AREA IAW EI NO T2020A53M-1449 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,200 hrs · 5,356 cycles

CRACK DAMAGES ON THE STRINGER S-8L BETWEEN STA 870 AND STA 890. REPAIRED DAMAGED AREA IAW EI NO T2020A53M-1373 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,200 hrs · 5,356 cycles

CRACK DAMAGES ON THE STRINGERS S-11L BETWEEN STA 860 AND STA 900. REPAIRED DAMAGED AREA IAW EI NO T2020A53M-1458 REV 3. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,200 hrs · 5,356 cycles

CRACK DAMAGES ON THE STRINGER S-9R BETWEEN STA 880 AND STA 900. ACCOMPLISHED STRINGER REPAIR IAW EI NO T2020A53M-1378 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: WEB — CRACKED (LT HORIZ STAB) · airframe 33,200 hrs · 5,356 cycles

CRACK ON UPPER AND LOWER CHORD AND WEB OF LH SIDE HORIZONTAL STABILIZER T/E AT HSB 421.5. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV 30. INSTALLED NEW PARTS IAW SRM 51-40-02 REV 30 AND DWG NR 182U5800, SHEET 1, REV B. REPAIRED DAMAGED AREA IAW EI NO T2020A55M-1383 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,200 hrs · 5,356 cycles

CRACK DAMAGES ON THE STRINGER S-11R BETWEEN STA 850 AND STA 900. ACCOMPLISHED STRINGER REPAIR IAW EI NO T2020A53M-1443 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,200 hrs · 5,356 cycles

CRACK DAMAGES ON THE STRINGER S-10R BETWEEN STA 860 AND STA 880. REPAIRED THE CRACKED AREA IAW EI NO T2020A53M-1459 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: RIB — CRACKED (LT WING) · airframe 33,200 hrs · 5,356 cycles

CRACK ON RIB OF LT WING FIXED TRAILING EDGE AT WBL 448.7. ACCOMPLISHED EI NO T2020A57M-1374 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: ROTARY ACTUATOR — FAILED (RT BLG) · airframe 33,200 hrs · 5,356 cycles

RT BLG ALTERNATE EXTEND SYSTEM OPERATIONAL TEST FAIL. IAW AMM 32-35-01-004-001 REV 32 AND AMM 32-35-01-404-007 REV 32 REPLACE RT BLG ROTARY ACTUATOR. IAW AMM 32-35-00-715-059 REV 32 PERFORM RT BLG ALTERNATE EXTEND SYSTEM OPER TEST. RESULT WAS NORMAL.

Part: FAIRING — DENTED (LT HORIZ STAB) · airframe 29,557 hrs · 4,802 cycles

LT HORIZONTAL STAB L/E FAIRING #331CL FOUND DENT. (<P>LT HORIZONTAL STAB L/E FAIRING #331CL DENT AREAS REPAIRED IAW SRM 55-10-01-2R-2 REPAIR 2.</P>)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 28,548 hrs · 4,653 cycles

GEAR TILT CAUTION MESSAGE DURING CLIMB. FOUND HYDRAULIC LINE TO LEFT BODY GEAR TILT ACTUATOR LEAKING. REMOVED AND REPLACED LINE. LEAK CHECK NORMAL I.A.W. AMM 32-13-14.<BR /></P>)

Part: RELAY — FAULTY (BRAKE SYSTEM) · airframe 25,964 hrs · 4,267 cycles

REJECTED T/O AT LOW SPEED DUE TO "CONFIG PARK BRAKE" T/O WARNING. SHOWED CMC NO REPORTED FOUND AND CHECKED PARKING BRAKE STS THEN FOUND PARKING BRAKE VLV NOT MOVE AND R&R PARKING BRAKE VLV CLOSE RELAY ( R7514) PER FIM 32-04-00-810-802 AND SYS TEST NORMAL PER AMM 32-44-00 ALSO T/O CONFIG WARNING CHECK NORMAL.

Part: CIRCUIT CARD — FAILED (HYD SYSTEM) · airframe 21,108 hrs · 3,542 cycles

DURING CRUISE, HAD A EICAS MESSAGES FOR HYD PRESSURE, SYS 3. PERFORMED QRH PROCED WITH NR 3 DMD ENG PUMPS OFF PRIOR TO PROCEDURE EICAS MESSAGES HYD PRESSURE NR 3 ENG, GPS, ADC CENTER MESSAGES. QRH/ ELC LIST COMPLETE BUT AURAL WARNING CONTINUED. NR 3 HYD SYS TEMP CONTINUNED TO RISE PEAKED AT 118 DEGREES. TEMP START REDUCING DURING DESCENT. HYD OVERHEATT SYS NR 3 EICAS MESSAGE, 1 HOUR AFTER BOTH DMD ENG PUMPS WERE TURNED OFF. TWO PAGES OF STATUS MESSAGES AT BLOCK IN. TESTED OK IAW AMM 34-58-00/501, AND 34-25-00/501. REPLACED WITH NEW HYD IM CARD ON THE NR 3 ENG POSITION IAW AMM 29-11-42 AND SYSTEM OPERATIONAL CHECKED OK.

Part: HINGE — LOOSE (FUSELAGE) · airframe 16,170 hrs · 2,785 cycles

NR 1 RAM AIR OUTLET HINGE FOUND LOOSE. NR 1 RAM AIR OUTLET LOOSED HINGE, REPLACED IAW SRM 51-10-02 AND FASTENERS INSTALLED SRM 51-40-02 AND SHEET 6, REV A.

Part: BRACKET — CRACKED (RT WING) · airframe 16,170 hrs · 2,785 cycles

NR 3 PYLON OTBD WING ACCESS NR 621AB INTERIOR INBD BEAM AFT BRACKET FOUND CRACKED. NR 3 PYLON OTBD WING ACCESS NR 621AB INTERIOR CAVITY AREA VAPOR BARRIER FWD ATTACHED TAG AT ILE 697.48 IS REPAIRED IAW NR:RI-57-41-11433, REV A FOLLOW UP INSPECTION IS REQUIRED IAW RI-57-41-11433, REV A.

Part: PANEL — CRACKED (LT WING) · airframe 16,170 hrs · 2,785 cycles

LEFT WING UPPER, WING T/E FIXED PANEL FOUND CRACKED AT JUST FWD OF NR 6 SPOILER. LT WING UPPER T/E FIXED PANEL AT JUST FWD OF NR 6 SPOILER CRACKED AREA COMPOSITE REPAIRED IAW RI-57-51-11434, REV A.

Part: BRACKET — CRACKED (LT WING) · airframe 16,170 hrs · 2,785 cycles

NR 2 PYLON OTBD WING ACCESS NR 521AB INTERIOR INBD BEAM AFT BRACKET FOUND CRACKED. NR 2 PYLON OTBD WING ACCESS NR 521AB INTERIOR CAVITY AREA VAPOR BARRIER FWD ATTACHED TAG AT ILE 697.48 IS REPAIRED IAW NR :RI-57-41-11433, REV A FOLLOW UP INSPECTION REQUIRED IAW RI-57-41-11433, REV A.

Part: SKIN — DAMAGED (NLG DOOR) · airframe 16,170 hrs · 2,785 cycles

ACFT DAMAGED, LT NOSE GEAR DOOR DENT DAMAGE, BIRD STRIKE, D=0.120", W=4", L=6", W/Y=33.3, SRM 52-80-01-1A, DETAIL V. LT NLG DOOR SMALL EXTERNAL SKIN REPAIRED IAW NR: RI-52-84-11435, REV A.

Part: PLUG — MISSING (GEARBOX) · airframe 12,769 hrs · 2,284 cycles

NR 4 ENGINE SHUTDOWN DUE TO LOW OIL QUANTITY AND PRESSURE. FOUND EDP DEACTIVATION KIT GEARBOX PLUG NOT INSTALLED. INSTALLED PLUG AS REQUIRED IAW AMM 29-11-02. LEAK CHECK NORMAL IAW AMM 71-00-00. ALSO, ACCOMPLISHED WINDMILL INSPECTION IAW AMM 71-00-00-200-806-G00. NO DEFECTS NOTED AT THIS TIME.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 12,769 hrs · 2,284 cycles

NR 4 HYDRAULIC SYSTEM FAILED APPROACHING LEVEL AT 11,000 FT. ACCOMPLISHED CHECKLIST. SHUTDOWN NR 4 ENGINE DRIVEN PUMP. FOUND NR 4 EDP LEAKING FROM PRESSURE SENSOR AND CASE DRAIN. TRANSFER TO MDDR 59865, MEL 29-11-01-02B. PUMP REMOVED AND PLATE INSTALLED IAW AMM 29-11-15 AND DDG PROCEDURES.

Part: FILTER — CONTAMINATED (ENGINE FUEL) · airframe 12,376 hrs · 2,221 cycles

DURING CLIMBOUT, EICAS MESSAGE, ENGINE 3 THRUST. PRELIMINARY INSPECTIONS SHOWED FUEL FILTER CONTAMINATION. NR 3 ENGINE REPLACEMENT IN WORK.

Part: FMU — POWER LOSS (NR 3 ENGINE) · airframe 12,353 hrs · 2,217 cycles

ENGINE NR 3 ROLLED BACK AND FLAMEOUT AT APPROXIMATE 16:42Z OIL PRESSURE STABILIZED AT 14 PSI IN CRUISE. N1 & N2 ROTATION 17.8/ 17.7. FIRE SWITCH NOT PULLED. PULLED AND INSPECTED NR 3 ENGINE FUEL FILTER FOR INSPECTION. FOUND CONTAMINATION. R & R FUEL & METERING UNIT IAW AMM 73-21-04. OPS AND LEAK CHECK GOOD.

Part: PUMP — FAILED (ENGINE FUEL) · airframe 12,353 hrs · 2,217 cycles

NR 3 ENGINE ROLLED BACK AND FLAMEOUT, OIL PRESSURE STABILIZED AT 14 PSI DURING CRUISE. N1 & N2 ROTATION 17.8/ 17.7. FIRE SWITCH NOT PULLED. NR 3 ENGINE FUEL PUMP REPLACED IAW AMM 73-11-01. OPS AND LEAK CHECKED OK.

Part: ENGINE — POWER LOSS (NR 4) · airframe 6,306 hrs · 1,143 cycles

DURING TAKEOFF ROLL AT VERY LOW SPEED, NR 4 ENG ROLLED BACK TO IDLE. DURING TAKEOFF REJECTION THERE WAS A BURNING ODOR FOR APPROXIMATELY 20 SECONDS IN THE AIR CONDITIONING SYS & THEN THE ODOR DISSIPATED COMPLETELY. ACCOMPLISHED INLET & EXHAUST INSPECTION, NO DAMAGE NOTED. ALSO ACCOMPLISHED TASK 72-11-02-700-803 THROTTLE RESOLVER TEST, PASSED. ACCOMPLISHED FMC SERVO TEST, PASSED.. ACCOMPLISHED POWER ASSURANCE HIGH POWER RUN IAW AMM 71-00-00. IAW MCC & POWER PLANT ENGINEERING, PERFORMED SMOKE & FUMES INSPECTION IAW AMM 71-00-00-200-804-600, WITH NO FINDINGS.