N665UA

Part: INDICATION SYS — FAULTED (FUEL SYS) · airframe 94,764 hrs · 19,779 cycles

FUEL INDICATIONS FLUCUAT ED UP TO 2400LBS BETWEEN TANKS. TOTAL A ND CALC FU EL SPLIT. CONTINUOUS FLUCTUATING FUEL WITH FUEL CONFIG LIGHT ILLUMINATING. PERFORMED FQIS BITE TEST YEILDED IAW AMM 28-41-00. LAST FLIGHT INDICATION WAS CONTAMINATED OR RESISTOR A02 (A ZERO, TWO) FUEL INDICATIONS FLUCUATED UP TO 2400LBS BETWEEN TANKS. TOTAL AND CALCULATED FUEL SPLIT. REMOVED AND REPLACED THE LT MAIN DENSITOMETER IAW AMM 28-41-03. OPS CHECKED GOOD IAW AMM 28-41-00-715-001-002.

Part: SWITCH — OUT OF POSITION · airframe 94,764 hrs · 19,779 cycles

AIRSPEED INDICATION ON BOTH CAPT'S AND FO SIDES LIMITED TO 265 KTS PER CREW REPORT. ON ARRIVAL, INSPECTED E&E COMPARTMENT AND FOUND S591 ALTERNATE VMO/MMO SWITCH IN ALTERNATE POSITION. THIS POSITION LIMITS VMO/MMO BARBER POLES. POSITIONED SWITCH TO NORMAL AND SAFETIED SAME. NO FURTHER DEFECT NOTED.

Part: OVEN — DIRTY (ZONE 700) · airframe 94,718 hrs · 19,769 cycles

FAS REPORTED FUMES IN REAR OF AIRCRAFT 10 MINS INTO FLIGHT. 4 6 PERSONNEL PUT ON O2CREW DEBRIEF CARRIED OUT, FORM 46-6020 ATTACHED AND SENT TO TOM-C. SMOKE/FUMES IN CABIN INSPECTIONS CARRIED OUT AS PER AMM 05-51-56-940-801-C1, STEP 1.A - 1.D.(8). UNABLE TO REPLICATE SMELL/ODOUR TO THIS POINT. CHECKS TO BE CONTINUED FROM STEP 1.D.(9) ONWARDS. ON INITIAL INSPECTION P401 REAR GALLEY PWR PANEL ON RH SIDE HAS BURNT TERMINALS TO GALLEY AC POWER CB C403 ALL AFT GALLEY OVENS EXCESSIVELY DIRTY, CREATING STRONG BURNING SMELL, SEALS ALSO IN POOR CONDITION RELEASING ODOR AND STEAM, IAW AMM 05-51-56. BOTH ENGINES RUN AT GROUND IDLE FOR 7 MINUTES, IAW AMM TASK 71-00-00-802. NO FUMES EVIDENT DURING CABIN WALKTHROUGH. SMOKE / FUMES IN CABIN CONDITIONAL INSPECTION, INITIAL INSPECTIONS AND OPERATIONAL CHECKS CARRIED OUT IAW AMM 05-51-56-940-801-C1 ITEM 1.C TO 1.D(8), DEFECTS NOTED LISTED ABOVE FOR RECTIFICATION. NIL OTHER DEFECTS NOTED. BURNING SMELL NOTED IN AFT GALLEY, CONSISTANT WITH BURNING FOOD, WITH STEAM & SMOKE ESCAPING FROM OVEN DOOR SEALS. FUEL / OIL NOT SMELT AT ANY POINT DURING CHECKS, PACKS ARE NOT CONSIDERED TO BE CONTAMINATED.

Part: OVEN — DIRTY (ZONE 900) · airframe 93,985 hrs · 19,671 cycles

FORWARD GALLEY OVEN 110 SMOKED WITH SPARK FROM WITH INSIDE OVEN. CLOSED DOOR AND PULLED CIRCUIT BREAKER FOR OVEN 110. NO FURTHER SPARKS AND SMOKE DISSIPATED. INSPECTED FWD GALLEY FOUND NO DEFECTS. STEAM OVEN 110 FOUND TO BE DIRTY AND COVERED WITH CARAMEL RESIDUE. . REMOVED AND REPLACED THE OVEN 110 IAW AMM 25-31-00. OPS CHECK GOOD, NO SIGNS OF BURNING, FOUL ODORS OR ARCING. ACFT OK TO CONT.

Part: OVEN — DIRTY (ZONE 900) · airframe 93,985 hrs · 19,671 cycles

ONDITIONAL INSPECTION REQUIRED REF CREW DEBRIEFING REFERENCE: TASK 05-51-56-940-801-C1. C/W CONDITIONAL INSPECTION IAW AMM 05-51-56. FOUND OVEN 110 COVERED IN CARAMEL RESIDUE CAUSING BURNING ODOR AND SMOKE. NO OTHER DEFECTS/FAULTS NOTED. CLEANED OVEN SURROUNDING AREA. FWD GALLEY OVEN 110 SMOKED WITH SPARK FROM WITH INSIDE OVEN. CLOSED DOOR & PULLED OPEN CB FOR OVEN 110. NO FURTHER SPARKS AND SMOKE DISSIPATED. INSPECTED FWD GALLEY FOUND NO DEFECTS. STEAM OVEN 110 FOUND TO BE DIRTY AND COVERED WITH CARAMEL RESIDUE. REF LP 6248151 FOR CONDITIONAL INSPECTION DETAILS AS PER AMM 05-51-56. REMOVED AND REPLACED OVEN 110 AS PER AMM 25-31-00. OPS CHECK GOOD NO SIGNS OF BURNING, FOUL ODORS OR ARCING. A/C OK TO CONT.

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 93,284 hrs · 19,564 cycles

2L AND 2R EXIT DOOR SLIDE PRESSURES OUT OF GREEN BAND. UPON INSPECTION FOUND DOOR 2L AND 2R SLIDE PRESSURE GAUGE IS ONE NEEDLE WIDTH ABOVE GREEN BAND TO BE WITH IN LIMITS PER AMM 25-66-99

Part: IRS — FAULTY (ZONE 100) · airframe 93,250 hrs · 19,558 cycles

AUTOBRAKES DISARMED IN FLIGHT AFTER BEING SET ON 2 FOR LANDING REQUEST MEL 3242Q, AUTOBRAKE SOLENOID CONFIRMED CLOSED. TAPE INSTALLED OVER AUTO BRAKES LIGHT IS TO BE REMOVED UPON CLEARING THIS MEL ITEM. ALL AUTOBRAKE FUNCTIONS, INCLUDING RTO, ARE INOPERATIVE. DEFERRED REF MEL 3242Q APPLIED MEL 3242Q TO AUTOBRAKE SYSTEM. TAPE INSTALLED OVER AUTO BRAKES LIGHT IS TO BE REMOVED UPON CLEARING THIS MEL ITEM. L IRU WAS REPLACED ON 15TH OF JUNE, AS PER FIM 32-42 FAULT TREE 803, PERFORMED BITE TEST ON AACU; FOUND L IRS FAULT. R/R (K511) RELAY. OPS CHECK GOOD. L IRS FAULT MSG ON AACU DOES NOT APPEAR. WORKED AS PER FIM 32-42 FAULT TREE 83. FURTHER TS IS REQ DUE TO FUP LP# 5277384. DURING T/S FOUND MISMATCHED IRS P/N .REMOVED AND REPLACED RH IRS TO MATCHED WIHT CTR AND LH IAW AMM 34-21-01-404-032 IRU TEST GOOD .ACCOMPLISHED TEST 30 GOOD

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 93,130 hrs · 19,542 cycles

2R DOOR PRESURE NOT IN GREEN AFT SERVICE DOOR PRESSURE WITHIN 1 NEEDLE WITH OF GREEN BAND PER AMM TASK 25-66-01-206-001, OK TO CONTINUE.

Part: CONTROL UNIT — FAULTED (ZONE 900) · airframe 92,998 hrs · 19,525 cycles

DURING INSPECTION FOR ODOR IN THE CABIN FOUND AFT GALLEY G6 NOT POWERED. CYCLING AFT RH GALLEY BREAKER ON THE P11 PANEL U34 RESTORED G6 POWER. NOTICED ODOR COMING FROM G6 A FEW MINUTES LATER. INSPECTED WIRING BEHIND COFFEE MAKERS,CIRCUIT BREAKER PANEL AND CHILLERS NO DEFECTS NOTED. PULLED AND CAPPED CIRCUIT BREAKERS U7 AND U34 RH AND LH GALLEY POWER ON THE P11 PANEL. AFT GALLEY IS DISABLED OFF WITH NO POWER, CB U7 AND U34 PULLED. WILL FURHER INVESTIGATE IN ORD. REMOVED OVENS AND COFFEE MAKERS TO FOM. INSPECTED WIRING AND CONNECTORS, NO DEFECTS FOUND. UPON FURTHER INVESTIGATION FOUND ALL 4 OVEN EXHAUST VENTS BLOCKED. CLEANED VENTS AND REINSTALLED OVENS AND COFFEE MAKERS REF AMM 25-31-00 AND 25-31-99. OPS TESTS GOOD UPON TURNING ON AFT GALLEY NO SMELL WAS DETECTED ORDMM WORKING ITEM REPLACED AFT RIGHT GALLEY ELCU, REF LP 5067607, SYSTEM TEST NORMAL.

Part: CONTROL UNIT — FAULTED (ZONE 700) · airframe 92,998 hrs · 19,525 cycles

MULT FA COMPLAINED OF BEING LIGHT HEADE AND NAUSIA AFTER T/O WIT H EXHAUST SMELL IN BACK REF AMM05-51-56. ACCOMPLISHED AMM 05-51-56 INCLUDING HIGHPOWER RUNS WITH LEFT AND RIGHT PACKS ISOLATED. ALSO RAN PACKS WITH APU NO SMELL IN CABIN NOTED. SEE LOG PAGE 5052948 FOR ADDITIONAL FINDINGS. DURING INSPECTION FOR ODOR IN THE CABIN FOUND AFT GALLEY G6 NOT POWERED. CYCLING AFT RH GALLEY BREAKER ON THE P11 PANEL U34 RESTORED G6 POWER. NOTICED ODOR COMING FROM G6 A FEW MINUTES LATER. INSPECTED WIRING BEHIND COFFEE MAKERS,CIRCUIT BREAKER PANEL AND CHILLERS NO DEFECTS NOTED. PULLED AND CAPPED CIRCUIT BREAKERS U7 AND U34 RH AND LH GALLEY POWER ON THE P11 PANEL. AFT GALLEY IS DISABLED OFF WITH NO POWER, CB U7 AND U34 PULLED. WILL FURHER INVESTIGATE IN ORD. ORDMM WORKING ITEM EXHAUST VENTS REMOVED OVENS AND COFFEE MAKERS TO FOM. INSPECTED WIRING AND CONNECTORS, NO DEFECTS FOUND. UPON FURTHER INVESTIGATION FOUND ALL 4 OVEN EXHAUST VENTS BLOCKED. CLEANED VENTS AND REINSTALLED OVENS AND COFFEE MAKERS ADD EMP:U407347 REF AMM 25-31-00 AND 25-31-99. OPS TESTS GOOD UPON TURNING ON AFT GALLEY NO SMELL WAS DETECTED REPLACED AFT RIGHT GALLEY ELCU, REF LP 5067607,. REPLACED AFT RIGHT GALLEY ELECTRICAL LOAD CONTROL UNIT REF AMM 25-31-03-404-009,OP'S CHECK GOOD.

Part: PANEL — CRACKED (LH WING) · airframe 92,757 hrs · 19,491 cycles

FIXED LEADING EDGE PANEL P/N 114T2800-275 DAMAGED DURING SLAT RETRACTION FAILURE. FIXED LEADING EDGE PANEL P/N 114T2800-275 REMOVED FOR REPAIR. SENT TO SHOP IN HOUSTON. DURING REMOVAL FOUND TWO DAMAGED GANG CHANNELS (NUT PLATE STRIPS) IDENTIFIED FROM REF/2/ DRAWING AS P/N 114T2301-66 & P/N 114T2301-69. ACCOMPLISHED NUT PLATE STRIP REPAIR REF. ECRA 5741-01644 THROUGH STEP 5. ITEMS 6 TILL END STILL NEED TO BE ACCOMPLISHED. RECEIVED REPAIRED LEADING EDGE PANEL, REPAIR AND RETURN TAG# R84843. BEGAN INSTALLATION OF PANEL REFERENCING INSTALLATION DRAWINGS FOR PANEL 114T2800-275. ADD EMP:U421245 CONTINUED INSTALLING NEW RIVETS WITH REFERENCE TO BOEING 767 SRM 51-40-02. CONTUNIED INSTALLING FASTENERS OF PANEL REFERENCING INSTALLATION DRAWINGS FOR PANEL 114T2800-275. COMPLETED INSTALLATION OF LEADING EDGE PANEL, REFERENCE INSTALLATION DRAWINGS ASSOCIATED TO PANEL PART NUMBER 114T2800-275. HFEC OF FASTENER HOLES PRIOR TO INSTALLATION REF LOG 4698366. INSPECTION VERIFIED INSTALLATION OF BULL NOSE, OKAY TO APPLY COATING.

Part: GRILL — BROKEN (N/A) · airframe 92,757 hrs · 19,491 cycles

17L DECOMPRESSION GRILL BROKEN REQUIRES REPLACEMENT. REMOVED AND REPLACED LOWER AND UPPER COMPRESSION GRILL.

Part: PANEL — MISSING (ZONE 400) · airframe 92,604 hrs · 19,471 cycles

AIRCRAFT (EXTERNAL) INSPECT (ZONES 100, 200, 300, 500, 600,700,800). {B767-06-3-0217} - ON ARRIVAL, PANEL 436AR FOUND MISSING FROM RIGHT ENGINE PYLON REF IPC 54-53-01-17, PN 311T3065-160 IN TRANSIT FROM LHR HANGAR PANEL 436AR REPLACED, REQUEST EXT TO APPLY COMPANY LIVERY WHEN TIME AVAILABLE. REPLACED PANEL 436AR FROM RIGHT ENGINE PYLON BUT NEEDS TO BE PAINTED TO MATCH LIVERY. PANEL 436AR LIVERY CARRIED

Part: ENGINE — FAILED (NR 2) · airframe 92,581 hrs · 19,468 cycles

ENG FAIL AT 18000 FEET RIGHT ENGINE SEVERE DAMAGE EGT 668 CREW DEBRIEF. THROUGH 16000FT R ENG HIGH EGT 668, HIGH ENG VIBS, NO N2 ROTATION. ENGINE SHUTDOWN INFLIGHT AND FIRE HANDLE PULLED BUT NO BOTTLES FIRED (NO FIRE WARNING). PASSENGER REPORTED FLAMES FROM R ENGINE EXHAUST, AIRFRAME VIB AT POINT OF FAILURE. 7000LBS OF FUEL JETTISONED. ALL OTHER OPS WERE NORMAL DURING EVENT AND ON RETURN TO LHR FOUND METAL FRAGMENTS IN TAILPIPE. NO DMG NOTED TO AILERON, FLAPS OR STAB R ENG SURGE STS. EXEEDANCE. EGT HIGH. EPR, N1, N2, FF, BURNER PRESS ALL DOWN COMPARED TO E1 AND CMD EPR. OIL PX AND QTY GOOD. N1 VIBS-3.2, N2 VIBS-1.3, BB VIBS-1.8. FOUND N2 SEIZED AT G/BOX DRIVE PAD - UNABLE TO TURN N2 MANUALLY.

Part: LAMP — NO TEST (ZONE 200) · airframe 92,302 hrs · 19,430 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - LH AFT FUSELAGE SLIDE EMERGENCY LIGHT INOP RELAMPED AND CLEANED TERMINALS. OPS CHECKED EXTERNAL SLIDE EMERGENCY LIGHTS, ALL GOOD AS PER AMM TASK 33-51-06-902-082.

Part: ACTUATOR — FAULTED (OUTFLOW VALVE) · airframe 91,082 hrs · 19,265 cycles

AIR RETURN DUE CABIN PRESSURE WARNING AT APPROX FL270 CAB ALT 10 000 FT. NEG MASK DROP CREW DEBRIEFING.A/C FLIGHT LEVEL 27K CABIN PRESSURIZATION ONLY READING 10K AND NOT GOING ANY HIGHER CREW RECEIVED CABIN AUTO INOP EICAS MSG AND CABIN PRESSURE WARNING. AT THAT TIME CREW SWITCHED OVER TO MANUAL CABIN PRESSURIZATION AND WERE ABLE TO CONTROL PRESSURIZATION AND BEGAN TO DECREASE A/C ALT. DURING THIS EVENT NO O2 MASK WERE DROPPED. CREW USED CREW O2. PERFORMED WIRING CHECKS PER WDM 21-31-21 FROM AUTO CONTROLLER 1 & 2 TO CABIN PRESURE OUTFLOW VALVE AND OUTFLOW VALVE MOTOR ALL WIRING CHECKS OK. R&R CABIN PRESSURE OUTFLOW VALVE ACTUATOR IN REF AMM 21-31-04 UP TO AND INCLUDING STEPS G(10). OPS CHCK GOOD AND NO OTHER DEFECTS NOTED AT THIS TIME. REQUIRES CLOSE UP.PARTS USED: 75-2133-9-0002,QTY :1 ADD EMP:U346523.ROTABLE PARTS CHANGE WAS INDICATED - TT # 1377604 SN OFF 2574 ACTUATOR, OUTFL OFF 75-2133-9-0002 2574 ON 75-2133-9-0002 2740 REF L/P 9843742 FOR DAMAGED OUTFLOW VALVE DEBRIS CAGE BRACKETS. INSTALL CAGE AFTER SHEET METAL BRACKET REPLACEMENT REF LOGPAGE 9843742. INSTALLED AFT WALL AND LOB BOX REF ALL WORK PERFORMED ON THIS LOGPAGE. AIRCRAFT AWAITS TEST FLIGHT

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 91,080 hrs · 19,263 cycles

LOST CABIN PRESSURE CONTROL ON 1 AND 2. MANUAL CONTROL WORKED. CONTACT TOMC WITH FINDINGS EWRMM WORKING ITEM FOLLOWING FIM 21-31 FAULT TREE 803, PERFORMED BITE OF BOTH AUTO AND REPLACED AUTO CABIN PRESSURE CONTROLLER 1 AND 2 REF AMM CABIN PRESSURE CONTROLLER 1 AND 2. FOUND FAULT LOW INFLOW ON 1 21-31-02. VERIFY TEST PASSED NO FAULTS. NO FURTHER DEFECTS NOTED AND FAULT AC PWR OFF ON 2. AFTER FURTHER TROUBLESHOOTING BOTH AT THIS TIME. PARTS USED: 19-2131-9-0004,QTY :1 BOXES FOUND TO BE OPERATING CORRECTLY. AS PERCAUTIONARY REMOVED 1379294,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1379294 SN OFF 6665 ADDED SECOND PART CHANGED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1374155 SN OFF 7665 CONTROLLER, CAB OFF 19-2131-9-0004 7665 ON 19-2131-9-0004 0080 CONTROLLER, CAB OFF 19-2131-9-0004 6665 ON 19-2131-9-0004 2290

Part: FAIRING — MISSING (ZONE 700) · airframe 91,026 hrs · 19,254 cycles

PDA 2 REF LP 9749794 , R/H MLG SIDE BRACE TRUNNION AFT FARING MISSING OK TO CONTINUE

Part: BULB — INOPERATIVE (ZONE 200) · airframe 90,673 hrs · 19,207 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - RH AFT SLIDE GROUND ILLUMINATION LIGHT INOP. RH AFT DOOR EMERGENCY ESCAPE SLIDE GROUND ILLUMINATION LIGHT REPLACED AS PER AMM 33-51-06-902-082. LIGHT NOW OPERATES CORRECTLY. PARTS USED: 00-0609-3-7622,QTY :1 99-3351-3-0014,QTY :1 40-0676-3-0991,QTY :1

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,767 hrs · 19,081 cycles

FOR IDENTIFICATION REFERENCE SEE SRM 53-80-03-0I-1 FIGURE 1, ITEM 7 (MATERIAL BAC1498-143).REMOVED STRINGER AS PER SRM 51-40-02-0G-0 PARAGRAPH 4 AND 7.INSTALLED THE NEW STRINGER AS PER SRM 51-40-02-0G-0 PARAGRAPH #04, #07, #09 AND SRM 51-10-02-0G-0 PARAGRAPH 09.ESFR NO 1036502.ITEM OK TO SERVICE.

Part: STRINGER — CORRODED (S36R) · corrosion level 2 · airframe 89,767 hrs · 19,081 cycles

REPLACED STRINGER 36RH AS PER SRM 51-40-02-0G-0.PARTS REPAIR AND DETAILS AS PER ESFR#1036501.ITEM OK TO SERVICE.

Part: STRINGER — CORRODED (S36L) · corrosion level 2 · airframe 89,767 hrs · 19,081 cycles

REPLACED STRINGER 36 LH AS PER SRM 51-40-02-0G-0. SRM REFERENCE 53-8--03-0I-1 ITEM 1 FIG1 SECTION 48 - SHEET 3. MATERIAL BAC1498-144 (CLAD 7075-T6) - PO#9284221.FOR PARTS AND DETAILS SEE ESFR#1036499.

Part: FLOORBEAM — CORRODED (BS 325 LBL55) · corrosion level 2 · airframe 89,767 hrs · 19,081 cycles

PERFORMED PERMANENT REPAIR OF THE FLOOR BEAM UPPER CHORD AT STA 325 AND LBL 54.75 CORROSION AS PER ECRA#5310-08344.

Part: SKIN — CRACKED (FUSELAGE) · airframe 89,767 hrs · 19,081 cycles

DURING INSPECTION WAS FOUND INDICATION CRACK AT FWD PASSENGER DOOR (LH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21L. THE LATEST REVISION OF ECRA# 5330-07278 ON OR BEFORE THE AC REACHES 37,500 TOTAL FC. ACCOMPLISH REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 3,000 FC THEREAFTER. PERFORMED INTERIM REPAIR OF THE AFT CORNER SKIN AND BEAR STRAP (DOUBLER) AT 1L FORWARD ENTRY DOOR AS PER ECRA#5330-07278. VERIFIED ACTION TAKEN BY MX AS PER ECRA#5330-07278 WITHOUT DEVIATION, GOOD TO GO. R BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. ACCOMP LISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,000 FLIGHT CYCLES THEREAFTER. PER ECRA 5330-07278: ACCOMPLISH INITIAL INSPECTION REQUIREMENTS TOMC-APPROVAL FROM SC1ELBYC COMMENT PER / PART 2A OF THE LATEST REVISION OF ECRA 5330-07278 ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,000 FLIGHT CYCLES THEREAFTER." 1L FORWARD SERVICE DOOR - AFT CORNER SKIN AND BEAR STRAP AREA WA QC S REPAIRED (DOUBLER) AT GIG. REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH INITIAL INSPECTION REQUIREM ENTS PER PART 2A OF THE LATEST REVISION OF EC/RA 5330-07278 ON O RECORDS UPDATE QC REVIEWED. INIT : 37,500 TAFC INIT WILL ITO TO RIR RIR : 3000 FC......PK/U394517

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 89,767 hrs · 19,081 cycles

DURING INSPECTION WAS FOUND INDICATION CRACK AT FWD SERVICE DOOR (LH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21L. THE CORRECT LOCATION OF THE CRACK IS AT FWD SERVICE DOOR (RH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21R. IS REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. N OF ECRA 5330-07277 ON OR BEFORE THE AC REACHES 37,500 TOTAL FC FC THEREAFTER. ACCOMPLISH INITIAL REQUIREMENTS PER PART 2 OF THE LATEST REVISIO . ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,000 PERFORMED INTERIM REPAIR OF THE CRACKS AT THE 1R FORWARD SERVICE DOOR AFT CORNER SKIN AND BEAR STRAP AS PER ECRA#5330-07277. TH THIS INTERIM REPAIR OF THE CRACKS AT THE 1R FORWARD SERVICE DOOR AFT CORNER SKIN AND BEAR STRAP WAS ACCOMPLISHED WHITOUT DEVIATION AS PER ECRA#5330-07277. THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. ACCOMPLISH REP EAT INSPECTIONS AT INTERVALS NOT TO EXCEED 3,000 FLIGHT CYCLES T HEREAFTER. ?1R FORWARD SERVICE DOOR - AFT CORNER SKIN AND BEAR STRAP AREA W TOMC-APPROVAL FROM SC1ELBYC COMMENT AS REPAIRED AT GIG. REPAIR IS A / PERMANENT SOLUTION WITH INSPECTI ON REQUIREMENTS. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST REVISION OF EC/RA 5330-07277 ON OR BEFORE T HE AIRCRAFT REACHES 37,500 TOTAL / FLIGHT CYCLES. ACCOMPLISH REPEA T INSPECTIONS AT INTERVALS NOT TO EXCEED 3,000 FLIGHT C 1R FORWARD SERVICE DOOR - AFT CORNER SKIN AND BEAR STRAP AREA WA QC S REPAIRED AT GIG. REPAIR IS A / PERMANENT SOLUTION WITH INSP

Part: FLOORBEAM — CORRODED (BS 325 LBL 55) · airframe 89,767 hrs · 19,081 cycles

DURING REMOVAL FLOOR MAT COVERING WAS FOUND A CORROSION AT FLOOR BEAM UPPER CHORD AT STA 325 AND LBL 54.75.(NR002042977).

Part: STRINGER — CORRODED (BS 1810-1833) · airframe 89,767 hrs · 19,081 cycles

THERE ARE CORROSION POINTS ON STR 30R, BETWEEN STA1809.50 AND STA1832.90, FOR REFERENCE SEE SRM 53-80-03-0I-1 FIGURE 1, ITEM 7.

Part: STRINGER — CORRODED (BS 1810 S32R) · airframe 89,767 hrs · 19,081 cycles

THERE ARE CORROSION POINTS ON STR 32R, BETWEEN STA1809.50 AND STA1832.90, FOR REFERENCE SEE SRM 53-80-03-0I-1 FIGURE 1, ITEM 7.

Part: STRINGER — CORRODED (BS 1809-1832) · airframe 89,767 hrs · 19,081 cycles

NR 001978538. CORROSION ON STRINGER S-36L BETWEEN BS 1809 TO BS 1832 .

Part: STRINGER — CORRODED (BS 1810-1833) · airframe 89,767 hrs · 19,081 cycles

CORROSION ON STRINGER S-36 RH BETWEEN BS 1809.5 TO BS 1832.90

Part: RETAINER — MISSING (UNKNOWN) · airframe 88,941 hrs · 18,970 cycles

PANEL 561NB SEAL AND RETAINER STRIP MISSING. QC RECORDS UPDATE..UK WITHIN 5 FLIGHT CYCLES NOT TO EXCEED 25723 FLIGHT CYCLES. ECRA 5751-01495 PART 1 - INTERIM REPAIR C/OUT. PART 2-INSPECTION TO BE C/OUT EACH FLIGHT. PART 3-PERMANENT REPAIR TO BE C/OUT THE PANEL REQUIRES VISUAL INSPECTION PER PART 2 AND REPAIRED PER PART 3 OF ECRA 5751-01495 WITHIN 5 FLIGHT CYCLES. EACH FLT (M METERED) INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. TA: 5 FC, UK.

Part: ACCESS PANEL — MISSING (NR 1 NACELLE) · airframe 88,941 hrs · 18,970 cycles

PANEL 436BL (NO.1 PYLON) IDENTIFIED AS MISSING ON ARRIVAL TO LHR STAND 249. PICTURES ADDED. LOG PAGE 6940113 RAISED FOR MISSING PANEL/ACCESS DOOR. TOMC INFORMED ABOUT PDA. LHR RUNWAY AND TAXI DEPARTMENT ALSO INFORMED. PANEL REPLACED. PARTS USED: 76-5453-3-0002,QTY :1.

Part: WIRE — DAMAGED (SEATS ROW 40-43) · airframe 87,584 hrs · 18,792 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - SEATS ROW 40-43 DEF EMERGENCY AISLE ESCAPE PATH LIGHTS INOP. SDR RAISED. AS PER GMM 04-20-16 EMERGENCY ESCAPE PATH LIGHTING WIRE BETWEEN SEATS 43 AND 44 FOUND DAMAGED. REQUIRES REPLACEMENT. WIRE AT BASE OF SEAT 43 DEF REPLACED. EMERGENCY LIGHTS TESTED OK IAW AMM 33-51-05-402-024.

Part: SPRING — MISSING (RH MLG) · airframe 87,109 hrs · 18,730 cycles

PDA 1. AIRCRAFT WALK AROUND INSPECTION {B767-51-3-6003} - WALKROUND CHECK FOUND R/H LANDING GEAR JURY STRUT SPRING MISSING. INSTALLED 2X R/H LANDING GEAR JURY STRUT SPRINGS. IAW AMM 32-32-05/401.

Part: BATTERY PACK — DISCHARGED (M1559) · airframe 85,824 hrs · 18,557 cycles

INOP EMERGENCY EXIT LIGHT M1559 POWER SUPPLY AT PASSENGER CABIN. REFER TO AEROMAN NON ROUTINE 2023-146216. REMOVED AND REPLACED POWER SUPPLY UNIT (M1559) AND PERFORMED OPERATIONAL TEST AND TEST IS OK. IAW AMM 33-51-07-002-006 AND AMM 33-51-07-402-010 BY V938999

Part: BATTERY — DISCHARGED (M962) · airframe 85,824 hrs · 18,557 cycles

DURING OPERATIONAL ARM/FIRE SWITCH CHECK NO FOUND VOLTAGE IN LATCH ACTUATOR CONNECTOR WHEN THE MECHANISM IS ARMED AT OFF WING RH SIDE.REFER TO NON ROUTINE 2023-146204. REPLACED RIGHT OFF-WING ESCAPE SYSTEM EMERGENCY BATTERY M962 I.A.W AMM-25-65-17-004-001-001 AND AMM-25-65-17-404-008-001.

Part: WIRE HARNESS — SHORTED (FUEL PUMP) · airframe 85,046 hrs · 18,452 cycles

R AFTFUEL PUMP EICAS W ASS. PRESSURE LIGHT IN FLIGHT LOCKED, FOUND WIRE SHORTING TO SHIELD. REQUIRES HIGH RESISTANCE TO GROUND, 24K OHMS, AT D1540 POSITION 6 WITH RPLCMNT. KIT ON ORDER. D4410P DISCONNECTED. W478-402Y-18 AND W478-304Y-18 WIRE SHORTED TO GROUND, REF WDM 28-22-11-4.1. POSITION 4 ON AL1004. COMPLETELY REMOVED BUNDLE W478 FROM A/C. REMOVED WIRE BUNDLE W478 AND W476 FROM THE MAIN FUEL PUMP ROUTED HARNESS W476 & W478 THROUGH BOOST,OVERRIDE,JETTISON CONDUIT. REMOVED BUNDLE W478 FROM THE AUX & JETTISON FUEL PUMPS CONDUIT IAW MM 28-22-15. .

Part: CONTROLLER — FAULTED (FUEL QTY) · airframe 84,635 hrs · 18,397 cycles

RIGHT FUEL GAUGE INTERM QUANITY GOES DOWN 2000 THEN RETURNS TO NORMAL TOTALIZER BLANKS AS WELL UPON ARRIVAL FOUND LEFT AND RIGHT MAIN TANK INDICATION BLANK. REMOVED AND REPLACED THE FQIC. NO FAULTS FOUND. PERFORMED DRY OPERATIONAL TEST IS GOOD AT THIS TIME AND FUEL QUANTITYS ARE NO LONGER ERRATIC.

Part: TIE BOLT — MISSING (NO 7 MAIN WHEEL) · airframe 84,485 hrs · 18,376 cycles

NO 7 MAIN WHEEL FOUND DEFLATED ON WALKAROUND X2 TIE BOLTS FOUND MISSING. NO.7 MAINWHEEL CHANGED IAW AMM 32-45-01/401. PARTS USED: 76-3245-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1368329 SN OFF 3700 WHEEL, TIRE, AS OFF 76-3245-9-9001 3700 ON 76-3245-9-9001 9065

Part: RUB STRIP — DAMAGED (#2 ENG) · airframe 81,405 hrs · 17,934 cycles

NO. 2 ENGINE TR INBOARD WEAR PLATE DAMAGED. PHOTOS ATTACHED WORN AREA AND TAPE DAILY. NEED TO R&R RUBSTRIPS WITHIN 100 HRS. ACCOMPLISHED PART 3 INTERIM TAPE REPAIR OF ECRA 7831-01780. NO DMG NOTED TO UNDERLYING STRUCTURE, JUST TO RUBSRIPS. MUST CHECK INTERIM REPAIR TO ENGINE 2 TR WEAR PLATE REQUIRES RECHECK OF TOMC-APPROVAL FROM SC1ELBYC COMMENT TAPE DAILY AND REPAIR WITHIN 100 HRS. REF ECRA 7831-01780 RECORDS UPDATE Q/C REVIEWED. Q/C REVIEWED. RIR: D-METER (DAILY) (NO M&E) T/A: WITHIN 100 FH...LN/U253409 REPAIR, AREA CLEANED AND INSPECTED. APPLIED ALUMINUM TAPE TO DISCREPANT AREAS. TO BE CHECKED ONCE DAILY. PICTURES ATTATCHED FOR REFERENCE. ON DAILY INPSECTION AT LHR SPEED TAPE NOT FOUND. AS PER ECRA 7831-01780 3. INTERIM TAPE

Part: TURBINE — FAILED (HPT) · airframe 79,450 hrs · 17,626 cycles

METAL DEBRIS FOUND IN #2 ENGINE EXHAUST. REPLACED #2 ENGINE PER TASK CARD 63-7100-1-9800. OPS AND LEAK CHECKED GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1451053 SN OFF 4665 ENGINE, (PW4060 OFF 76-7200-9-0001 4665 ON 76-7200-9-0001 4674 ACP''D RII INSP ON #2 ENG CHANGE IAW TASK CARD 63-7100-1-9800.

Part: ENGINE — STALLED (RIGHT) · airframe 79,450 hrs · 17,626 cycles

RIGHT ENGINE COMP STALL. QUICKLY FOLLOWED BY OVER TEMP OF 712 EG T. ENG SHUTDOWN. ENG FAIL T/O. FURTHER DETAILS AWAITED.

Part: SOLENOID — FAILED (C/P DOOR LOCK) · airframe 76,504 hrs · 17,184 cycles

FLT DECK DOOR -LOCK FAIL - LIGHT CAME ON STEADY I N FLT. DID NOT ICE A STRA NGE ODOR. CKLIST COM SUSPECT SOLONOID HAS BEEN POWERED ALL FLIGHT, PANEL REMOVED AREA INSPECTED AND FOUND DOOR LOCKING SOLONOID EXTREMELY HOT CAUSING A SLIGHT ODOUR AUTOMATIC FLIGHT DECK DOOR DEACTIVATED IAW MEL ADD EMP:U353020 P. NO OTHER SYSTEM IS AFFECTED FROM THIS C/B BEING PULLED REF C/B T5 ON THE P11 PULLED AND COLLARED IAW GMM 05-30-05 SECTION 5251C. FLIGHT DECK ACCESS SWITCH MOVED TO THE OFF POSITION AND WDM 52-51-11. SEE PREVIOUS LOG HISTORY 3952228, 294666, 3932108, 3906034, 3988783 AND 3903210. FORM 46-6920 FILLED OUT BY LHRMM. NOC

Part: LIGHT — LOOSE (CABIN) · airframe 75,082 hrs · 16,997 cycles

EMERGENCY LIGHT STRIP AT MIDDLE ROW OF EMERGENCY EXIT CAME LOOSE. RESECURED EMERGENCY LIGHT STRIP AT X AISLE AND ACP OPS TEST OF LIGHTS PER AMM 31-51-00.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 71,117 hrs · 16,480 cycles

CENTER HYD SYSTEM LOW QTY REMOVED AND REPLACED MAIN WHEEL WELL PRESSURE AND CASE DRAIN FILTER MODULE ,DIFFERENT PRESSURE INDICATOR O-RING REF AMM29-11-19. LEAK CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,867 hrs · 16,443 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK . OP CHECKED NORMAL IAW AMM 33-51-07.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 70,867 hrs · 16,443 cycles

EMERGENCY LIGHTS AT ROWS 34D AND 34F INOPERATIVE. REPAIRED THE CONNECTOR. R & R THE FUSE AT POWER SUPPLY M9047, AND REPLACED THE LIGHT ASSY AT SEAT 34D IAW WDM 33-51-15. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 70,838 hrs · 16,437 cycles

EMERGENCY LANDING DECLARED, DUE TO TRAILING EDGE DISAGREE. PERFORMED FLAP/SLAT ELECTRONIC UNIT BITE PER FIM TASK 27-51-00-815-808, NO CURRENT/PREVIOUS FAULTS NOTED. CYCLED FLAPS/SLATS AND VISUALLY INSPECTED FOR ANY DEFECTS. NO DEFECTS NOTED. OK TO CONTINUE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 70,688 hrs · 16,417 cycles

TE FLAP DISAGREE FLAPS STAYED AT POSITION ONE. PROCEDURE NO HELP WENT TO FLAP ASYMETRY. EMERGENCY DECLARED. TE FLAP DISAGREE SELF RESET ON EICAS. AFTER SWITCHING ADP AND ELEC HYD PUMPS, FLAPS MOVED DOWN TO 5 (LAST POSITION OF FLAP LEVER AFTER LAST FLT). FIM TASK 27-51-00-815-810 PERFORMED, NIL FINDINGS. OVERTORQUE PINS INSPECTED ON ANGLE GEARBOX, FOUND ALL NORMAL, NO OVERTORQUE. SEVERAL FLAPS-SLATS FULL HYD CYCLES PERFORMED, ALL NORMAL. WHEN CYCLING FLAPS-SLATS IN ALTERNATE PWR, TE FLAP DISAGREE DISPLAYED ON EICAS AND FLAPS-SLATS STUCKED IN POS 1. FOUND CB D24 ON P6-4 CB PANEL (ALTERNATE FLAPS POWER) POPPED. CB D24 RESET AND SEVERAL ALT FUNCTIONS PERFORMED, ALL BACK TO NORMAL.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 70,636 hrs · 16,409 cycles

AISLE PATH LIGHTING IS INTERMITTENT AT AISLE CROSSOVER SEGMENT. REPLACED CROSS-AISLE PATH LITE (EEL). OPS CHK GOOD. PER AMM 33-51-10-400.

Part: RECEPTACLE — DIRTY (EMERGENCY LIGHT) · airframe 69,169 hrs · 16,203 cycles

EMERGENCY EXIT GROUND LIGHT, LEFT SIDE, AFT OF WING IS INOPERATIVE. CLEANED RECEPTICLE, OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (COCKPIT DOOR) · airframe 69,169 hrs · 16,203 cycles

EMERGENCY EXIT LIGHT OVER COCKPIT DOOR IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT.

Part: RECEPTACLE — DIRTY (EMERGENCY LIGHT) · airframe 69,169 hrs · 16,203 cycles

EMERGENCY EXIT GROUND LIGHT, RT SIDE AFT OF WING IS INOPERATIVE. CLEANED THE RECEPTICLE, OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 68,362 hrs · 16,093 cycles

2 EA CEILING EMERG LIGHT LENS COVERS MISSING IN AFT PAX COMP. REPLACED LENS COVERS.

Part: LINE — LEAKING (NR 1 ENGINE) · airframe 66,635 hrs · 15,864 cycles

NR 1 ENG AFTER LIFTOFF OIL QUANTITY STARTED TO DECREASE TO ZERO. EVENTUALLY OIL PRESSURE. IFSD PERFORMED. CLEANED OIL RESIDUE. FOUND LINE FROM LOW OIL PRESS SWITCH TO FUEL OIL COOLER LEAKING AT COOLER B NUT. REF IPC 71-00-01-422L ITEM 820. REPLACED LINE. ACCOMPLISHED 5 MIN IDLE RUN LEAK CHECK OF LINE. LEAK CHECKED GOOD AND NO OTHER LEAKS NOTED.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 66,423 hrs · 15,835 cycles

OVERWING EMERGENCY EXIT LIGHTS FOUND INOPERATIVE, DURING 2 SERVICE CHECKS BOTH SIDES OF AIRCRAFT. TROUBLESHOOTING FOUND EMERGENCY BATTERY CHARGER M1209 AT FAULT IAW FIM 33-51-00. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW 33- 51-07 AND TESTED IAW AMM 33-51-00 ALL TESTED OK, LIGHTS WORK.

Part: WIRE — BROKEN (CABIN) · airframe 62,397 hrs · 15,268 cycles

CEILING EMER LIGHT AT SEAT 27 RT HAS BROKEN WIRES & CONNECTOR IS MISSING. CEILING EMER LIGHT AT SEAT 20 RT INOPERATIVE. ALSO ESCAPE PATH AISLE LIGHTING AT SEAT 21, 22 & 23 RT ARE INOPERATIVE. R & R BATTERY PACK AT POWER SUPPLY M1209. REPLACE CONNECTOR AT EMER LIGHT ASSEMBLY POSITION 27 RT. CLEAN CONNECTOR AT POWER SUPPLY M733 & REPLACE LAMPS IN EXIT LIGHT ASSEMBLY. REPLACE RED LIGHT ASSEMBLY AT SEATS 20 LT & RT. EMER LIGHT SYS CHECKED NORMAL IAW AMM 33-51-00.

Part: WIRE — DAMAGED (CABIN) · airframe 60,750 hrs · 15,031 cycles

OPERATIONAL CHECK ON PAX CABIN LIGHTS & SIGNS. REPAIRED WIRE AT SEAT 40 CTR ON EMER LIGHT PATH LT SIDE. SYS CHECKED NORMAL IAW MM 33-51-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,589 hrs · 14,743 cycles

THE CABIN CREW REPORTS AN ODOR IN THE AFT GALLEY, AFT LT LAVATORY AREA. SMELL DISSIPATED APPROX 3 - 5 MINS AFTER SHUTTING OFF GALLEY EQUIPMENT IN AFT GALLEY. ACCOMPLISHED GALLEY, CABIN & LAVATORY INSPECTION & OPERATION IAW AMM 05-51-06-201. OPERATED AFT GALLEY COFFEE MAKERS, WARMERS, OVENS, CHILLERS & LIGHTING FOR 1 HOUR. FOUND NO DISCREPANCIES OR ODORS PRESENT. CHECKED AFT LT LAVATORY LIGHTING NO IRREGULARITIES OR ODORS PRESENT. RAN BOTH PACKS, NO ODORS PRESENT. INBD OVEN INSERTS HAVE BEEN REMOVED.

Part: GROUND WIRE — OUT OF POSITION (FUEL SYSTEM) · airframe 57,556 hrs · 14,614 cycles

AIRCRAFT FAILED FCD 2841-01075 STEP 5, GND WIRING IS NOT IAW FIGURE 4. POSITIONED GND WIRE IAW FCD 2841-01075 FIG 4, BONDING CHECKED GOOD IAW SWPM 20-20-00.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 56,482 hrs · 14,482 cycles

LEFT FWD ENTRY DOOR DIFFICULT TO OPEN FROM OUTSIDE. FOUND SLIDE GIRT BAR DIFFICULT TO ARM & DISARM. ALSO FOUND RAFT STARTING TO UNRAVEL. REPLACED DOOR ESCAPE SLIDE PACK AT DOOR 1L FOR PRECAUTIONARY. UPON REPLACEMENT FOUND OPERATIONS CHECKED NORMAL.

Part: CHINE — MISSING (NR 2 COWLING) · airframe 56,328 hrs · 14,462 cycles

NR 2 ENG INLET COWL CHINE INBD SIDE MISSING, ATTACHING BOLTS ALSO MISSING. INSTALLED NR 2 ENG INLET COWL CHINE INBD SIDE IAW AMM 71-11-02, OKAY.

Part: FUEL CAP — MISSING (FUEL SYSTEM) · airframe 55,473 hrs · 14,352 cycles

ONE OF THE FUEL CAPS IS MISSING. REPLACED & SECURED FUEL CAP.

Part: COUPLING — LEAKING (FUEL SYSTEM) · airframe 55,291 hrs · 14,326 cycles

FUEL LEAKING FROM RT ENGINE STRUT DRAIN. OPENED NR 2 ENG & RAN ENG AT IDLE TO FIND LOCATION OF STRUT DRAIN. ATTACH POINT AT PYLON JUST AFT OF FWD ENGINE MOUNT AT TDC. FUEL LINE COUPLING LEAKING INBD OF FIRE WALL DISCONNECT FITTING INSIDE OF PYLON STRUT CAVITY. REPLACED O-RING SEALS IAW MM. PRESSURIZED LINE NO LEAKS

Part: CIRCUIT CARD — FAULTY (APU) · airframe 55,203 hrs · 14,312 cycles

APU BLEED PRESSURE. ACCOMPLISH ITEMS 1,3 & 4 ON CH8365. REPLACED LT N2 SPEED CARD IAW AMM.

Part: INDICATOR — STICKS (BLEED AIR SYS) · airframe 55,203 hrs · 14,312 cycles

DUCT PRESSURE INDICATOR SLIGHTLY STICKS NEAR ZERO. REPLACED INDICATOR & ALL PRESSURE INDICATIONS SHOW NORMAL.

Part: TUBE — CHAFED (CABIN) · airframe 55,168 hrs · 14,306 cycles

FOUND TUBE CHAFFING ON PROX SENSOR BRACKET BETWEEN NR 2 & NR 3 LATCHES FOR RT OFF WING DOOR SLIDE PCN 160-1065. R & R THE TUBE IN BETWEEN THE NR 2 & NR 3 LATCHES NEXT TO THE PROX SENSOR FOR THE OFF WING DOOR SLIDE IAW AMM 25-65-09.

Part: APU — SHUTDOWN (APU BAY) · airframe 55,153 hrs · 14,304 cycles

APU AUTO SHUT 2 TIMES WITH A FAULT MESSAGE. APU FAULT CLEARED OIL QTY FULL 1 START ATTEMPT SUCCESSFUL. NO FURTHER APU SHUT DOWN AT THIS TIME AC OK CONTINUE.

Part: RELAY — FAILED (RT IDG) · airframe 54,852 hrs · 14,266 cycles

RT IDG VLV STATUS MESSAGE REPEAT WRITE UP. TROUBLE SHOT IAW FIM 24- 20-00 & WDM 24-11-21 PAGE 1 SHEET 2. REPLACED RELAY K971, RAN ENG IAW JRH 2-6-1. TEST PASSED, NO FUTURE MESSAGES APPEAR AFTER ENG RAN.

Part: OXYGEN BOTTLE — LOW PRESSURE (COCKPIT) · airframe 54,852 hrs · 14,266 cycles

CREW OXYGEN BOTTLE PRESS BELOW NR 2 SVC LIMITS. REPLACED OXYGEN BOTTLE IAW AMM, CHECKED OKAY.

Part: FIRE LOOP — INTERMITTENT (NR 1 NACELLE) · airframe 54,709 hrs · 14,247 cycles

NR 1 ENG FIRE LOOP 2 EICAS MESSAGE DISPLAYED. LT ENG FIRE LOOP 2 STATUS MESSAGE INTERMITTENT. ANNUNCIATES FOR A FEW SECONDS. REMOVED AND REPLACED TS681 AND TS683 IAW AMM 26-11-99, & FIM 26-11-00. OPS CHECKED GOOD.

Part: RELAY — FAILED (IDG VALVE) · airframe 54,709 hrs · 14,247 cycles

EICAS STATUS MESSAGE RT IDG VALVE. R & R RT IDG VALVE FAILURE RELAY K1032. CHECKED GOOD.

Part: VALVE — FAULTY (APU) · airframe 54,680 hrs · 14,242 cycles

APU SHUTDOWN DURING ENGINE START ACCOMPANIED BY FAULT LIGHT. REPLACED APU SURGE VALVE IAW AMM, APU OPERATIONS NORMAL.

Part: SENSOR — FAULTY (APU) · airframe 54,656 hrs · 14,239 cycles

APU AUTO SHUT DOWN, CAUSING GATE RETURN. TROUBLE SHOT IAW FIM 49-1 1-00, FOUND REVERSE FLOW ON BITE. R & R INLET TEMPERATURE SENSOR IAW AMM. R & R FLOW SENSING MODULE IAW AMM. ALL OPERATIONS & LEAKS CHECK GOOD AT THIS TIME. APU OK TO CONTINUE.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 54,605 hrs · 14,232 cycles

LT ENG FIRE LOOP 2 STATUS MSG INTERMITTENTLY COMES ON & GOES OFF. R & R NR 2 LOOP ENG 1 CARD FILE M682 IAW AMM 26-10-01-401, IAW FIM 26-11-00 & OPERATIONS CHECKED AMM 26-11-00.OPERATIONS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 54,602 hrs · 14,231 cycles

ON LANDING DECELERATING THRU 120KTS AURAL GEAR WARNING & CONFIG LITE WITH SPEED BRAKE LITE. ACCOMPLISHED PSEU BITE NO EXISTING FAULTS, LANDING CONFIG WARNING TEST TAKE OFF & LANDING PASSED, RA-NO FAULTS, SPOILER CONTROL MODULES NO FAULTS, INSPECTED WW & GEAR SENSORS NO DISCREPANCIES, REPLACED LANDING CONFIG MODULE M983 PRECAUTIONARY.

Part: CONTROL VALVE — FAILED (AC BAY) · airframe 54,468 hrs · 14,213 cycles

LT PACK NOT COOLING. FOUND LT PACK TEMPERATURE VALVE FAILED OPEN. RESET, NO HELP. DEFERRED LT PACK TEMPERATURE VALVE INOPERATIVE IAW MEL 2151S. COMPLIED WITH DEACTIVATION PROCEDURE. REPLACED LT PACK TEMPERATURE CONTROL VALVE IAW AMM, OPERATIONS CHECKED OK.

Part: FASTENER — MISSING (RT WING) · airframe 54,449 hrs · 14,211 cycles

FASTENER MISSING RT WING TE THIRD PANEL IN FROM WING TIP. REPLACED FASTNER.

Part: CASE — CRACKED (COMPRESSOR) · airframe 53,889 hrs · 14,145 cycles

NR 2 COMPRESSOR INTERMEDIATE CASE CRACKED. FOUND TO BE AIRWORTHY FOR FERRY FLIGHT. NR 2 ENGINE COMPRESSOR INTERMEDIATE CASE CRACKED AT NR 3 SUPPORT STRUT CLAMP-UP PLATES.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 53,889 hrs · 14,145 cycles

L2 DOOR SLIDE DEPLOYED AT GATE AFTER PARKING.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 53,816 hrs · 14,134 cycles

EMERGENCY LIGHT REMAINED EXTINGUISHED DURING SLIDE SQUIB TEST. TROUBLESHOT IAW SSM 25-65-01 FOUND FUSE F1 IN BATTERY PACK M962 BLOWN. REPLACED FUSE, OPS GOOD.

Part: ACTUATOR — CRACKED (LT MLG) · airframe 53,757 hrs · 14,127 cycles

LEFT MAIN GEAR TRUCK POSITIONER, LEAKING FROM HOUSING MIDWAY BETWEEN ATTACH FITTINGS. HOUSING CRACKED. REPLACED LT MAIN GEAR TRUCK POSITIONER ACTUATOR IAW AMM 32-32-18. NO LEAKS NOTED.

Part: MONITOR — FAILED (FAN VIBRATION) · airframe 53,696 hrs · 14,119 cycles

FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE ILLUMINATED IN FLIGHT. R & R FWD FAN VIBRATION MONITOR IAW AMM, OPS CHECKED GOOD.

Part: COMPUTER — INOPERATIVE (LT AUTOPILOT) · airframe 53,696 hrs · 14,119 cycles

LEFT AUTOPILOT, LEFT FCC INOPERATIVE. R & R LEFT FCC COMPUTER IAW MM, OPS GOOD. PERFORMED MCDP TEST 30 AND 40 IAW MM, OPS GOOD. ACFT FULL CAPABLE, NO FAULTS AT THIS TIME.

Part: COMPUTER — FAULTY (AUTO THROTTLE) · airframe 53,573 hrs · 14,105 cycles

AUTO THROTTLE FAILED DURING TAKEOFF. TARGET EPR AND SPEED TAPE CYCLE INTERMITTENTLY ALSO. TMC FAILED FLT FAULT AND FAILS MCDP TEST 2. R & R TMC, TESTED GOOD. MCDP TEST 2,10& 30 PASS, ACFT REMAINS FULL CAPABILITY.

Part: BLADE — BULGED (NR 2 ENGINE) · airframe 53,286 hrs · 14,069 cycles

DURING ACFT WALK AROUND, FOUND ON RT ENGINE BLADE NR 2 BULGED .5" LONG BY .0937" DEEP ON THE L/E. BULGE IS LOCATED 6 INCHES FROM ROOT OF THE BLADE. PERFORMED BLENDING OF NR 2 BLADE DAMAGE IAW AMM.

Part: CIRCUIT CARD — FAILED (STICK SHAKER) · airframe 52,857 hrs · 14,017 cycles

CONTINUOUS STICK SHAKER ON GROUND AT GATE. REMOVED AND REPLACED A STALL WARNING PRINTED CIRCUIT CARD, OPS CHECKED OK.

Part: MODULE — MALFUNCTIONED (STALL WARNING) · airframe 52,734 hrs · 14,002 cycles

MIN MANUEVERING AMBER SPEED BAR STILL FLUCTUATES FROM BOTTOM TO TOP CONSTANTLY ON BOTH HSI. REPLACED LEFT AND RIGHT STALL WARNING MODULE PER MM, IN CONJUCTION WITH ECRA 34 22-01040. TESTED SWC SYSTEM. NO FAULTS NOTED, OPS NORMAL.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NR 4 SLAT) · airframe 52,728 hrs · 14,000 cycles

LEADING EDGE SLAT FAULT, RETUNED TO FIELD. TROUBLESHOT. ACCOMPLISHED HEALTH CHECKK OF LE PROXIMITY SENSORS. FOUND S285 OUT OF TOLERANCE PER AMM. 27-88-99. ACCOMPLISHED LEADING EDGE SENSOR SYSTEM HEALTH CHECK PER AMM 27-88-99. FOUND SLAT NR 4 INBD PROXIMITY SENSOR OUT OF LIMITS. ADJUSTED TARGET AND SENSOR S-285, NOW WITHIN LIMITS.

Part: INDICATOR — FAULTED (SLAT SYSTEM) · airframe 52,670 hrs · 13,993 cycles

"L/E SLAT ASSY" EICAS, RETURNED TO FIELD. REMOVED AND REPLACED FLAP INDICATOR. OK FOR SERVICE, NO FAULTS NOTED.

Part: COMPUTER — FAULTED (LT EICAS) · airframe 52,540 hrs · 13,976 cycles

RIGHT ENGINE START EGT STATUS MESSAGE CAME ON DURING CRUISE. REPLACED LEFT EICAS COMPUTER, OPS CHECKED GOOD.

Part: CIRCUIT CARD — MALFUNCTIONED (LT ENG FIRE LOOP) · airframe 52,478 hrs · 13,969 cycles

STATUS MESSAGE LT ENG FIRE LOOP 2. INSPECTED LT ENG LOOP 2. NO FAULTS NOTED. PERFORMED FIRE LOOP TEST. UNABLE TO DUPLICATE. PROBLEM REOCCURED. REMOVED AND REPLACED M682 CARD PER AMM 26-11- 02 AND TROUBLESHOT PER FIM 26-11-00 FIG 104. NO EICAS M

Part: POWER SUPPLY — INTERMITTENT (CABIN) · airframe 52,222 hrs · 13,934 cycles

DOOR 2R EMERGENCY LIGHT LEVEL 1. DUE TO CHRONIC HISTORY OF DOOR 2R EMERGENCY EXIT SIGN LOWER LIGHT INTERMITTENTLY BLINKING. FOUND GROUND GD4618DC FROM D13244 LOOSE. REPLACED GROUND TERM GD4618DC REF WDM 33-51-14 N SWP 20-20-10. REPLACE MS1556 EMERGENCY PWR SUPPLY, OPS CHECK NORMAL.

Part: AMU — FAULTY (NR 1) · airframe 51,971 hrs · 13,901 cycles

OFF THE GATE ACARS INOP, BLANK SCREEN, PER CREW. CREW CYCLED G6 (MU UNIT) AND G13 (CMU-ACRAS DC CBS.ACARS BACK ON AND OPS NORMAL.

Part: CDU — FAULTY (COCKPIT) · airframe 51,971 hrs · 13,901 cycles

OFF THE GATE ACARS INOP, BLANK SCREEN, PER CREW. CREW CYCLED G6 (MU UNIT) AND G13 (CMU-ACRAS DC CBS.ACARS BACK ON AND OPS NORMAL. REMOVED AND REPLACED REF AMM 23-22-02. OPS CHECK NORMAL.

Part: BATTERY — FAILED (CABIN) · airframe 51,967 hrs · 13,900 cycles

DOOR 2R EMERGENCY LIGHT BLINKS. DUE TO THE CHRONIC HISTORY OF DOOR 2R EMERGENCY EXIT IDENTIFIER SIGN LOWER LIGHT INTERMITTENTLY BLINKING. PLEASE REPLACE BATTERY ASSEMBLY M1556 REF AMM. (PCN 585-4495). REMOVED AND REPLACED M1556, OPS CHECKED SATISFACTORY.

Part: OXYGEN BOTTLE — LOW PRESSURE (CABIN) · airframe 51,881 hrs · 13,890 cycles

PSX PORTABLE OXYGEN CYLINDER(S) PRESS IS LOW OR ZERO (AT 01 LOCATIONS). AFT LEFT DOOR REPLACED AFT POB.

Part: LIGHT — INOPERATIVE (COCKPIT DOOR) · airframe 51,783 hrs · 13,876 cycles

COCKPIT DOOR EMERGENCY LIGHT INOPERATIVE. LIGHT ASSY REPLACED PER AMM. OPS CHECKED OKAY.

Part: SKIN — DENTED (BS 434 S38L) · airframe 51,783 hrs · 13,876 cycles

FUSELAGE SKIN DENTED AT BS 434 STRINGER 38 LT. DOUBLER REPAIR INSTALLED PER ECRA 5331-01-680. MAJOR REPAIR.

Part: WEB — DAMAGED (BS 246 RBL 12) · airframe 51,783 hrs · 13,876 cycles

FOUND TWO PUNCH HOLES ON FWD FACE OF BS 246 RBL 12 VERTICAL WEB LOWER AREA. BS 246 FLOORBEAM AT RBL 12 VERTICAL WEB LOWER AREA HOLES REPAIRED PER ECRA 5310-05679 PART 1.

Part: FLOORBEAM — DAMAGED (BS 303) · airframe 51,783 hrs · 13,876 cycles

ELONGATED HOLES FOUND IN UPPER TEE OF FLOORBEAM BS 303 RBL 60. CUT OUT DAMAGE SECTION AND REPAIRED PER SRM 53-00-51 REPAIR 2 FIG 201. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 51,783 hrs · 13,876 cycles

FLOORBEAM UPPER TEE CORRODED BS 347 RBL 28 - 49. CUT OUT DAMAGE FLOORBEAM TEE FROM BL 0 TO RBL 88 AND INSTALLED REPAIR PER SRM 53-00-51 REPAIR 1 FIGURE 201. MAJOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 1518) · airframe 51,783 hrs · 13,876 cycles

FLOORBEAM CRACKED AT BS 1518 RBL 2 UPPER TEE. CUT OUT DAMAGED FLOORBEAM TEE FROM LBL 35 TO RBL 35 AND REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 303) · corrosion level 2 · airframe 51,783 hrs · 13,876 cycles

FOUND CORROSION ON UPPER TEE OF FLOORBEAM BS 303 LBL 4 - 16. CUT OUT CORROSION LBL 4 - 34 AND INSTALLED REPAIR PER SRM 53-00-51 REPAIR 1 FIG 201. MAJOR REPAIR.

Part: FLOORBEAM — DAMAGED (BS 1480) · airframe 51,783 hrs · 13,876 cycles

FLOORBEAM UPPER TEE HAS MISDRILLED HOLES AT BS 1480 RBL 31. CUT OUT DAMAGED AND REPAIRED PER SRM 53-00 -51 REPAIR 2 FIG 20. MAJOR REPAIR

Part: SEAT TRACK — CORRODED (BS 546-658) · airframe 51,783 hrs · 13,876 cycles

SEAT TRACK CORRODED BS 546 TO 549 RBL 88. REPLACED SEAT TRACK SECTION FROM BS 546 TO 658 PER ECRA 5300-01458 AND SRM 53-00-52 REPAIR 3.

Part: SEAT TRACK — CORRODED (BS 1329-1334) · corrosion level 2 · airframe 51,783 hrs · 13,876 cycles

RBL 88, BS 1329 - 1334, SEAT TRACK FOUND CORRODED. SEAT TRACK REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1185-1189) · corrosion level 2 · airframe 51,783 hrs · 13,876 cycles

RBL 88 BS 1185 TO 1189 SEAT TRACK FOUND CORRODED. SEAT TRACK REPLACED IAW SRM 51-40-02.

Part: UNKNOWN — MALFUNCTIONED (VHF COMM) · airframe 51,767 hrs · 13,875 cycles

NR 2 RADIO NOT TRANSMITTING OR RECEIVING. NO AUDIO COMING FROM RT VHF TRANSRECEIVER JACK. TRANSRECEIVER BITE OK. REF :WD-23-12-21 PAGE 2, ANT CABLE IS OPEN. REPLACED NR 2 VHF ANTENNA (PRECAUTIONARY).

Part: SKIN — NICKED (E&E DOOR) · airframe 51,762 hrs · 13,874 cycles

LOWER EXTERNAL FUSELAGE E&E DOOR SKIN NICK ENTIRE SKIN. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED DOUBLER IAW SRM 52-40-01, REPAIR 5.

Part: STIFFENER — CRACKED (NLG WW) · airframe 51,762 hrs · 13,874 cycles

NOSE WHEEL WELL STA 287 VERTICAL STIFFENER CORD HAS CRACK BETWEEN FASTENER 12 AND 13 STARTING FROM TOP. REMOVED DAMAGED AREA, FAB 4 EA RPR PARTS PER SRM51-70-12 AND 51-40-05. INSTALLED RPR REF SRM 51-70-12, FIG 1.

Part: LIGHT — LOOSE (CABIN) · airframe 51,715 hrs · 13,856 cycles

ESCAPE PATH LIGHTS ARE DISLODGED AND HANGING LOOSE IN FIRST CLASS. RE-SECURED EMERGENCY ESCAPE LIGHTS, OPS CHECK OKAY.

Part: CIRCUIT CARD — FAULTY (AC SYSTEM) · airframe 51,664 hrs · 13,847 cycles

'R INOP' & 'PACK OFF 'LIGHTS ON. EICAS MSG 'R PACK OFF' DISPLAYED.' REPLACED RIGHT FLOW CONTROL CARD PER MM. RAN PACK FOR 2 HOURS. NO FAULTS.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 51,664 hrs · 13,847 cycles

WORKING EQ5095 REMOVED SLIDE PACK -779 FROM DOOR 1L WHEN INSTALLING SLIDE -773 SLIDE WAS DAMAGED RIVETS PULLED LOOSE. NEW SLIDE ON ORDER. DO NOT OPEN DOOR 1L FROM EXTERIOR. REMOVED PER MM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 51,645 hrs · 13,843 cycles

CAPTS STAB TRIM IND 5-7-F/O STAB TRIM 2. CAPT INDICATION IN ERROR, COMPLIED WITH MEL2748A, CAPT SIDE INDICATION COVERED. REPLACED CAPTAINS STAB TRIM INDICATOR AND OPS OKAY.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 51,417 hrs · 13,774 cycles

CREW REPORT: L ENGINE HPSOV AND LT ENGINE BLEED LIGHT LIGHT ON IDLE POWER ADVANCING POWER CLEARED LIGHT. INOP'D LEFT ENGINE HI STAGE VALVE PER MEL3611Q PROCEDURES. REPLACED NR 1 ENG HPSOV.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 51,408 hrs · 13,772 cycles

STANDBY ALTIMETER IS 360 FEET HIGH AT FL320. REPLACED STANDBY AIRSPEED INDICATOR AND PERFORMED PITOT STATIC CHECK.

Part: PROBE — FAULTY (PITOT/STATIC SYS) · airframe 51,286 hrs · 13,742 cycles

A-C RETURNED TO BLOCKS FOR :L AUX PITOT EICAS MSG AND ANNUNCIATOR LT FOR SAME. VERIFIED CB NOT POPPED AND L AUX PITOT DOES NOT OPERATE WHEN TEST SW ACTUATED. REPLACED LEFT AUX PITOT PROBE, OP CHECKS NORMAL, LEAK CHECKS WITHIN LIMITS PER MM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 51,206 hrs · 13,723 cycles

EMERGENCY EXIT LIGHT STRIP PULLED OFF SEAT 1B. REPLACED EEL STRIP ON SEAT 1B, LIGHT OPS CHECKS OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 51,178 hrs · 13,715 cycles

CABIN FIRST CLASS SEAT 1B EEL LIGHT ASSY MISSING. REPLACED LIGHT, CHECKS OK.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 51,178 hrs · 13,715 cycles

CABIN EEL LIGHTS INOP FROM ROWS 25H TO 31. SECURED CONNECTOR UNDER SEAT 31HJ, CHECKS OKAY.

Part: BOLT — LOOSE (FUEL ADAPTER) · airframe 50,901 hrs · 13,639 cycles

FUELER REPORTS FUEL ADAPTOR BOLTS LOOSE. REPLACED ALL FASTENERS AND SECURED.

Part: CLAMP — UNSECURE (NR 1 FIRE LOOP) · airframe 50,901 hrs · 13,639 cycles

NR 1 ENGINE LOWER FORWARD FIRE LOOP CLAMP HANGING FROM BRACKET 6 O`CLOCK POSITION. SECURED CLAMP.

Part: APU — SHUTDOWN · airframe 50,686 hrs · 13,594 cycles

APU AUTO SHUT DOWN AT DEPARTURE. ACCOMPLISHED BITE CHECK ON APUC. NO FAULT DATA ON ALL RUNS. "NO DATA" DISPLAYED ON ALL RUNS. TROUBLESHOT IAW MM 49-61-00-101 SECTION G4 OR FCU REF SSM. REPLACED APU PER MM. OPS AND LEAK CHECKED GOOD.

Part: VALVE — FAULTY (RT A/C PACK) · airframe 50,674 hrs · 13,591 cycles

'R PACK INOP' LIGHT ON. EICAS MSG 'R PACK TEMP' DISPLAYED. REPLACED APU SURGE CONTROL VALVE AND AIR SUPPLY SHUTOFF VALVE. APU BLEED PSI NORMAL WITH BOTH PACKS ON AND CTR ADP ON, APU BLEED PSI NORMAL DURING ENGINE DRY MOTOR. APU AIR SUPPLY SHUTOFF VALVE REPLACED, REF DF511, NOW RT PACK OPERATION NORMAL IN AUTO MODE AND R PACK INOP LIGHT NOT ON AND NO STATUS MESSAGES.

Part: VALVE — FAULTY (APU BLEED) · airframe 50,674 hrs · 13,591 cycles

APU BLEED AIR ONLY 8PSI , UNABLE TO START EITHER ENGINE. REPLACED APU SURGE CONTROL VALVE AND AIR SUPPLY SHUTOFF VALVE. APU BLEED PSI NORMAL WITH BOTH PACKS ON AND CTR ADP ON, APU BLEED PSI NORMAL DURING ENGINE DRY MOTOR.

Part: SDU — MALFUNCTIONED (COCKPIT) · airframe 50,629 hrs · 13,579 cycles

SATCOM STATUS ON LINK STATUS PAGE IS NO COMM. REPLACED SATELLITE DATA UNIT. SATCOM SYSTEM CHECKED NORMAL.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 50,323 hrs · 13,511 cycles

LEFT ENGINE HPSOV EICAS WHEN ENGINE REDUCED FOR DESCENT. ACCOMPLISHED QRH. FOUND NR 1 ENGINE HPSOV VALVE WOULD NOT FULLY CLOSE. REPLACED HPSOV PER MM. OP CHECKED GOOD PER SAME MM. PERFORMED 10 MIN IDLE RUN, NO FAULTS.

Part: SHUTOFF VALVE — ACTIVATED (FUEL SYSTEM) · airframe 50,252 hrs · 13,492 cycles

CREW REPORTS INFLIGHT TRANSFER TO CENTER FUEL TANK. SEALED RIB 3 AT 1400, 12 HR CURE. REPLACED LT IB MAIN SHUT OFF VALVE. TANKS CLOSED. TO FUEL 0530 FOR LK & OP CKS. ACP MM28-11-95 ITEM 2.A (4) FOUND SMALL FUEL LEAK AT RIB 3 UPPER AREA BETWEEN STA. L5 AND L6. -SEALED AREA AT RIB 3 UPPER R BETWEEN STR L5 AND L6 WITH 3750-3 AND 3750-5 AT 14:00 NEEDS LEAK CHECK. -REMOVED AND REPLACED LT FUEL TNK INBD FUEL SHUT OFF VLV PER MM. ACP'D NON RII INSP OF AMIS ITEM 2522010 LT FUEL TANK INBD SHUTOFF VLV IAW AMM FOR SAFETY AND SECURITY. INSTALLED FUEL SHUT OFF VLV ACTUATOR PER MM28-21-02. RT MAIN FUEL SELECT INDICATOR GLASS FOGGED UP. REPLACED INDICATOR AND TESTED PER MM, OP CHECKED GOOD

Part: RELAY — FAILED (ENGINE) · airframe 49,838 hrs · 13,398 cycles

LEFT ELECTRICAL DEMAND PUMP IN AUTO DISPLAYS SYS PRESSURE LIGHT AND PRESS LIGHT WITH 90 PSI. REPLACED K680 LT ENGINE START SENSE RELAY AND K681 RT ENGINE START SENSE RELAY PER WDM 29-11-12 PG 2, RAN BOTH ENGINE, OPS CHECKED NORMAL. NO FAULT LIGHTS.

Part: SPEAKER — DISTORTED (PA SYSTEM) · airframe 49,833 hrs · 13,397 cycles

PA SPEAKER ABOVE 3HJ SOUND IS DISTORTED. REPLACED SPEAKER. OPS OK.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 49,828 hrs · 13,396 cycles

WITH LEFT ELECTRIC HYDRAULIC PUMP SELECTED, SYSTEM PRESSURE LIGHT IS ON. REPLACED PUMP, OPS CHECKED OK.

Part: WINDOW — CRACKED (CABIN) · airframe 49,755 hrs · 13,380 cycles

DIVERTED TO DEPARTURE, DUE TO CRACKED EXTERNAL WINDOW. DURING VISUAL INSPECTION OF CABIN WINDOWS. 1J PASSENGER WINDOW HAS A CHIP ON UPPER FWD CORNER. REPLACED WINDOW AT 1J.

Part: VALVE — FAULTY (APU) · airframe 49,499 hrs · 13,325 cycles

APU AIR PRESS CYCLES FOR NO REASON. DEFERRED PNEUMATICS INOP PER MEL. REPLACED APU SURGE VALVE. RAN APU FOR 30 MINUTES WITH DIFFERENT LOADS. NO SURGING NOTED.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 49,432 hrs · 13,310 cycles

APU AUTO SHUTDOWN AT GATE BEFORE PUSHBACK. BITE OF BOX FAULTS LOW OIL PRESS SWITCH. REPLACED APU CONTROLLER, NO HELP.

Part: SLIDING WINDOW — LEAKING (COCKPIT) · airframe 49,341 hrs · 13,291 cycles

CREW REPORT: F/O SIDE FORWARD WINDOW (ONE THAT OPENS) HAS AIR LEAK SQUEAL. REPLACED WINDOW PER MM. MR56604 DASH 105 OFF NEW WINDOW INSTALLED FROM CONTINENTAL SN 799 ON. OPS CHECK NORMAL.

Part: B-NUT — LOOSE (RT ENGINE) · airframe 49,232 hrs · 13,268 cycles

RIGHT ENGINE LEAKING FLUID 60-100 DRIPS PER MINUTE. FOUND PRESSURE LINE ON RT ENG HYDRAULIC PUMP LEAKING, TIGHTENED 'B' NUT AND DRY MOTORED ENGINE. NO LEAKS DETECTED, CHECKS GOOD.

Part: ROTARY ACTUATOR — FAULTY (CARGO DOOR) · airframe 49,097 hrs · 13,238 cycles

RAMP REPORTED THAT FWD CARGO DOOR MAKING NOISE WHEN CLOSING. RAN FWD CARGO DOOR THRU RECYCLE AND FOUND FWD CARGO DOOR MAKING NOISE IN BOTH DIRECTION. NOISE SEEMS TO BE COMING FROM LIFT ACTUATOR OR DOOR LINKS BEARING CYCLE DOOR CLOSE AND CONFIRMED DOOR CLOSED AND LOCK AND STRIPES ARE VISIBLE, AND DOOR LT IS OUT. REPLACED BOTH AFT AND FWD ROTARY ACTUATOR PER MM, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,092 hrs · 13,237 cycles

SEAT MOUNTED EEL LIGHT INOP 3B. ACCOMPLISH NON-RII INSPECTION OF AMIS ITEM 0922011. RPL'D EEL LIGHT AT 3B. OPS CHECK GOOD. ACCOMPLISHED IDT INSPECTION OF EEL LIGHT STRIP INSTALLED AT SEAT 3B.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 48,913 hrs · 13,196 cycles

STATUS MESSAGE 'CABIN ALT 1'. MEL M2131A. FOUND CABIN ALT 1 UNIT NO POWER. RPLC'D UNIT PER MM, BITE CHECK OKAY.

Part: BRAKE ASSY — FAULTY (MLG) · airframe 48,909 hrs · 13,195 cycles

L TRUCK INBD REAR BRAKE TEMP 6. REPLACED NR 6 BRAKE ASSY. ALSO ACP MM05-51-15 BRAKE SEIZURE INSPECTION.

Part: BRAKE — FIRE (NR 2 MLG) · airframe 48,909 hrs · 13,195 cycles

MOMENTARY FIRE OBSERVED BY GROUND CREW COMING FROM NR 2 MLG FWD BRAKE ASSY. RPLC'D NR 2 BRAKE ASSY PER MM. ALSO ACP MM. REPLACED NR 6 BRAKE ASSY PER MM. ALSO ACP MM 05-51-15 BRAKE SEIZURE INSPECTION.

Part: BLADE — DAMAGED (RT ENGINE) · airframe 48,491 hrs · 13,102 cycles

RT ENGINE HAS A SIGNIFICANT NICK IN BLADE 2, BLADE DAMAGE IS AT DIM LEADING EDGE FROM BASE TO DAMAGE IS 20.700. APPROX 750. DEPTH AND LENGTH IS 1.0 INCH. PER MM DOCUMENT BLADE IS NOT REPAIRABLE. REPLACED NR 2 1ST STAGE FAN BLADE AND OPPOSITE FAN BLADE NR 21.

Part: CONTROLLER — FAILED (RT A/C PACK) · airframe 48,484 hrs · 13,100 cycles

'RT PACK INOPERATIVE' LIGHT ON. EICAS MESSAGE 'RT PACK TEMP' DISPLAYED. OPERATED NORM AFTER 'STANBY' SELECTED. RIGHT PACK CONTROLLER 'RAM INLET ACTUATOR', 'LOW LIMIT VALVE' & 'COMPRESSOR SENSOR'. REPLACED RIGHT PACK CONTROLLER. BITE TESTED OKAY.

Part: LIGHT — DISLODGED (SEATS 3AB & 6AB) · airframe 48,465 hrs · 13,092 cycles

SEAT EXIT LIGHTS FALLING OFF AT 3AB AND 6AB. REPLACED EMERGENCY LIGHTS.

Part: ACTUATOR — FAILED (RT A/C PACK) · airframe 48,467 hrs · 13,093 cycles

RIGHT A/C PACK INOPERATIVE LIGHT ON. EICAS MESSAGE 'RT PACK TEMP' DISPLAYED. OPERATED NORM AFTER 'STBY' SELECTED. REF MM 21-51-00 FIG 103 BLOCK 1. BITE SHOWS INOP RT A/C PACK INLET DOOR ACTUATOR. INLET DOOR VERIFIED CLOSED AND OUTLET DOOR FULLY OPEN. PULLED CONNECTOR TO RIGHT PACK OUTLET DOOR ACTUATOR & STOWED. PULLED & SAFTIED RT PACK FLOW CONTROL CIRCUIT BREAKER ON P11 PANEL. SUSPECT INLET DOOR ACTUATOR BAD. REPLACED RAM AIR INLET DOOR ACTUATOR.

Part: VALVE — FAULTY (APU) · airframe 48,331 hrs · 13,060 cycles

APU NO DUCT PRESSURE. CYCLED APU BLEED VALVE SEVERAL TIMES, NO HELP. REPLACED FLOW DIV VALVE PER MM. OPS APU, NO BLEED ISSUE FOUND.

Part: PCU — DAMAGED (CABIN) · airframe 48,336 hrs · 13,061 cycles

CALL LIGHTS AND READING LIGHTS AT 22H AND 22J BLINKING ON AND OFF. FOUND BROKEN WIRE ON PCU. DISCONNECTED WIRE. PCU IS INOP. NEED PCU PART# 581-2249.

Part: RELAY — FAULTY (APU) · airframe 48,255 hrs · 13,042 cycles

APU WILL NOT START. HANGS BETWEEN 0-10% RPM. SHUTSDOWN WITH APU FAULT LIGHT ON. REFER TO MM-49-61-00, CODE B1. NO POWER BEYOND MAIN CONTACTOR, NO POWER TO CONTROL SIDE OF CONTACTOR. REPLACED RELAYS K117 & K197, AND APU CONTROLLER. APU START OKAY.

Part: LIGHT — UNSECURE (SEAT 1B) · airframe 48,240 hrs · 13,038 cycles

EMERGENCY EXIT LIGHT HANGING OFF AT SEAT 1B. REPLACED FWD EMERGENCY LIGHT AT SEAT 1B.

Part: HANDSET — INTERMITTENT (INTERPHONE) · airframe 48,240 hrs · 13,038 cycles

INTERPHONE INTERMITTENT WHEN CALLING COCKPIT FROM L1 DOOR. TAKES UP TO 3 ATTEMPTS TO CONNECT. REPLACED FA HANDSET AND CRADLE OPS CHECKED OKAY.

Part: LIGHT — BROKEN (CABIN) · airframe 48,068 hrs · 13,000 cycles

EEL LIGHT BROKEN OFF SEAT 1B. REPLACED LIGHT ASSY, OPS CHECK GOOD.

Part: DOOR — FALSE ACTIVATION (RT OVERWING) · airframe 48,046 hrs · 12,995 cycles

RT OVERWING SLIDE DOOR BLEW OPEN. SLIDE DID NOT BLOW (SLIDE WAS PINNED). ALL SWITCHES APPEARED TO BE IN PROPER POSITION AND ALL CB'S WERE PULLED. SLIDE BOTTLE AND SLIDE WERE PINNED AT THE TIME. UPON FURTHER INVESTIGATION FOUND RH INBD SPOILER ACTUATOR EXTENDED. REPLACED RT BLOW DOWN ACTUATOR. ON ACCOUNT OF RT OVERWING SLIDE DOOR BLOWN OPEN NR 7 RT SPOILER ACTUATOR SQUIB ALSO BLOWN . REPLACED AS A UNIT WITH THE BLOW DOWN ACTUATOR. REPLACED SLIDE DOOR LATCH ACTUATOR. REPLACED FWD DOOR OPENING ACTUATOR. REPLACE RT OVERWING SLIDE AFT OPENING ACTUATOR. REPLACED RIGHT HAND OVER WING SLIDE.

Part: MODULE — FAULTY (APU) · airframe 48,011 hrs · 12,987 cycles

DUCT PRESSURES FROM APU ZERO WITH APU RUNNING, APU BLEED SWITCH ON, ISOLATION VALVES OPEN, AND ENGINE (BLEED) OFF LIGHTS DISPLAYED ON BOTH ENGINES. VALVE VERIFIED CLOSED. MAY NEED TO REPLACE CLAMP. IPC REF: 49-27-00A-000B ITEM 40 PCN: 651-1454. -INF- :REF ABOVE UPDATE BY SFOEG IT SHOULD READ WILL NEED TO REPLACE CLAMP. REPLACED FLOW SENSE MODULE MR49115 PER MM.

Part: CONTROL VALVE — FAILED (APU) · airframe 47,995 hrs · 12,983 cycles

APU PNEUMATICS FAILED TO PRESSURIZE ON ENGINE START. 4 PSI ONLY. COMPLIED WITH MEL 3611G APU BLEED VALVE LIGHT OPS NORMAL. APU SURGE CONTROL VALVE. LEAK AND OP'S CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 47,980 hrs · 12,980 cycles

ONE EACH FWD SEAT EMERGENCY LIGHT IS MISSING AT SEAT 1B. NEEDS LIGHT STRIP. NO LIGHT STRIP IN STOCK P/N 566-1373. STRIP 566-1373 PLACED ON OSTF S0537. REPLACED LAMP OP CHECK GOOD.

Part: HANDSET — INTERMITTENT (CABIN) · airframe 47,946 hrs · 12,973 cycles

INTERPHONE IS INTERMITTENT AT MID CTR GAL 414. INTERPHONE HANDSET AT MID CTR GALLEY.

Part: BLEED VALVE — FAILED (APU) · airframe 47,854 hrs · 12,950 cycles

NO DUCT PRESSURE WITH APU ON. CYCLED CIRCUIT BREAKER AND SWITCH VARIOUS TIME, NO HELP 3 PSI ONLY. REPLACED APU BLEED VALVE. OPS CHECKED NORMAL.

Part: APU — INOPERATIVE · airframe 47,800 hrs · 12,938 cycles

APU FAILED TO START. SUSPECT APU BATTERY. REPLACED APU BATTERY, REPLACED STARTER AND REPLACED AUX POWER CONTROL UNIT, NO HELP. REMOVED AND REPLACED APU PER AMM, OPS CHECKED OKAY.

Part: SATCOM — FAILED (RIGHT) · airframe 47,791 hrs · 12,936 cycles

SATCOM BITE FAIL STBD BSU. PCN 581-9305. REPLACED STBD BSU. BITE TEST PASSED. SATCOM OPERATIONAL TEST PASSED.

Part: SKIN — PUNCTURED (BS 464) · airframe 47,791 hrs · 12,936 cycles

SKIN PUNCTURED AT BS 464 S22L. REPAIRED SKIN IAW 53-30-01 FIG 1 SHEET 2 ITEM 3 AND EVA-81408A.

Part: SELECTOR PANEL — FAULTY (AUDIO SYSTEM) · airframe 47,781 hrs · 12,934 cycles

VERY LOUD HUM IN CAPT AUDIO ON FLT INPH & SERV INPH. REPEAT WRITE UP. REPLACED CAPT AUDIO SELECT PANEL, OPS NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 47,781 hrs · 12,934 cycles

SEAT 20J ORANGE OVERLAY SEAT MOUNTED IS BROKEN. REPLACED LIGHT ASSY, CHECKS GOOD.

Part: COMPUTER — FAILED · airframe 47,693 hrs · 12,916 cycles

ASA SHOWS NO LAND 3 RESET AND TEST DOES NOT HELP. MCDP SHOW "FCC CENTER FAIL ", RESET CB'S NO HELP. REPLACED FCC-C PER AMM AND ACCOMPLISHED AFDS SYS TEST PER AMM. CHECKS OKAY, ACFT RTN'D TO CAT-III STATUS.

Part: LIGHT — INOPERATIVE (FLAP INDICATOR) · airframe 47,599 hrs · 12,896 cycles

BACKLIGHT IN FLAP INDICATOR INOPERATIVE. REPLACED FLAP TRANSMITTER. OPS NORMAL.

Part: COMPUTER — FAULTY (AUTOPILOT) · airframe 47,599 hrs · 12,896 cycles

AUTOPILOT MOVES YOKE BACK AND FORTH INSIDE THE MARKER APP 1 INCH EACH WAY. REPLACED CENTER FCC AND RESTORED SYSTEM OPERATIONS.

Part: UNKNOWN — DIRTY (CABIN) · airframe 47,283 hrs · 12,830 cycles

AFT CABIN NEAR AFT GALLEY SMELLY ODOR-CHRONIC WRITE UP. AFT CABIN AND GALLEY AREAS CLEANED FOR THRU FLIGHT BY CONTRACT CLEANERS.

Part: FMU — FAULTY (NR 1 ENGINE) · airframe 47,254 hrs · 12,823 cycles

NR 1 ENG START EICAS MSG AND LIGHT L ENG FUEL VLV. REPLACED LEFT FMU PER MM, ACP'D LEAK & OPS CHECK AND IDLE RUN. ALL CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 47,231 hrs · 12,818 cycles

FWD CARGO DET 2 STATUS MSG ON EICAS. SAMC TEXT: CREW COMPLIED MEL CARD. DEFERRED PER SAMC. REPLACED FWD CARGO DET 2 M325 IAW MM & TESTS OKAY.

Part: SELECTOR PANEL — FAULTY (COCKPIT) · airframe 47,208 hrs · 12,813 cycles

CAPTAIN'S AUDIO SELECTOR SWITCH LIGHTS NOT ILLUMINATED WHEN SELECTED ON. PANEL REPLACED PER MM, OPS CHECK'S GOOD.

Part: SELECTOR PANEL — FAULTY (COCKPIT) · airframe 47,198 hrs · 12,811 cycles

CAPT UNABLE TO TRANSMIT USING MINITEL, SPARE MINITEL, NO HELP. TRIED ALL 3 PTT BUTTONS. SAMC TEXT: CAPT REPORTS USING CAPT HANDMIC, TRANSMISSIONS ARE NORMAL. CREW REPORTED: CAPT'S SIDE COMMUNICATIONS CHECKED NORMAL DURING DESCENT. REPLACED AND OP CHECKED CAPT'S AUDIO SELECTOR PANEL AS PRECAUTIONARY. ALSO CHECKED O2 MASK & RESET PA CB'S. MINITEL CHECK'S GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,052 hrs · 12,780 cycles

EMERGENCY FLOOR LIGHTS TURN ON AND OFF THRUOUT FLIGHT BETWEEN SEATS 25-35HJ. SUPPLEMENTAL DATA UPDATE EMERGENCY LIGHTS ARE OFF WITH THE SWITCH IN ARM POSITION. REPLACED BATTERY PACK AND POWER SUPPLY, ALL CHECKED OKAY.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 46,910 hrs · 12,750 cycles

ROW 25-35 H&J EMERGENCY LIGHTS ON & SOMETIMES FLICKERING. REPLACED BATTERY PACK FOR LIGHT GROUP AND OP CHECKED.

Part: RELAY — NO TEST (ESCAPE SLIDE) · airframe 46,804 hrs · 12,728 cycles

EMERGENCY ESCAPE RIGHT NR 1 WILL NOT TEST. REPLACED RELAY K839, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (SEAT 21J) · airframe 46,687 hrs · 12,706 cycles

EMERGENCY LIGHT ON SEAT 21J IS INOPERATIVE. REPLACED LIGHT, CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 46,687 hrs · 12,706 cycles

AFT GALLEY SMALL LEFT EMERGENCY LIGHT MISSING. INSTALLED AFT GALLEY EMERGENCY LIGHT, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,687 hrs · 12,706 cycles

EEL LIGHT ON SEAT 14A IS INOP. REPLACED LIGHT, CHECKS GOOD.

Part: LIGHT — WRONG PART (CABIN) · airframe 46,687 hrs · 12,706 cycles

AFT RIGHT EMERGENCY LIGHT HAS INCORRECT PART INSTALLED. REPLACED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,687 hrs · 12,706 cycles

FWD EEL LIGHT ON SEAT 1A IS INOP. REPLACED LIGHT, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,687 hrs · 12,706 cycles

AFT EEL LIGHT ON SEAT 3A IS INOP. REPLACED LIGHT. CHECKS GOOD.

Part: INDICATOR — FAULTY (ALTIMETER) · airframe 46,631 hrs · 12,694 cycles

VIBRATOR FOR STANDBY ALTIMETER IS WAY TOO LOUD. CAUSES HEADACHES-FATIGUE. INTERFERES WITH ATC COMM. REPLACED INDICATOR CHECKED PER MM.

Part: ACTUATOR — FAULTY (APU) · airframe 46,296 hrs · 12,626 cycles

APU AUTO SHUTDOWN AND THE APU INTAKE DOOR C/B FOUND POPPED. NEED TO REPLACE THE APU AIR INTAKE DOOR ACTUATOR. REPLACED APU DOOR INLET ACTUATOR IAW AMM, OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,144 hrs · 12,595 cycles

EMERGENCY AISLE LIGHT AT SEATS 17AB INOP. RELAMPED, OP CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,144 hrs · 12,595 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 10AB THRU 17AB INOP. REPLACED BATTERY PACK M1558 PER MM, OP CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 46,144 hrs · 12,595 cycles

AFT GALLEY FLOOR STRIP EMERGENCY LIGHT INOP. REPAIRED DAMAGED SPLICE NEAR LIGHT STRIP PER WDM, OP CHECKED GOOD.

Part: LIGHT — MISSING (SEAT 21B) · airframe 46,142 hrs · 12,594 cycles

SEAT 21B APPROX 12'' LONG AND ONE HALF OF LIGHT HAS AN ORANGE STRIPE IS MISSING. REPLACED SEAT MOUNTED LIGHT STRIP. GROUND CHECKED GOOD.

Part: LIGHT — BROKEN (SEAT 1B) · airframe 46,077 hrs · 12,577 cycles

SEAT 1B, FOUND FWD EEL STRIP BROKEN. REPLACED AND OP-CHECK SATISFACTORY.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 46,077 hrs · 12,577 cycles

CAPT AUDIO PANEL VHF L VOLUME TOO LOW AT FULL THROW. REPLACED CAPT AUDIO PANEL AND OPS CHECK SATISFACTORY.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 45,897 hrs · 12,537 cycles

ROWS 25-35 ROW H EMERGENCY LIGHTS ON THE SEATS FLASHES ON AND OFF. REPLACED BATTERY PACK AT ROW 25 HJ PER MM. EEL OPS CHECKS OKAY.

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 45,622 hrs · 12,476 cycles

RT PACK OFF LIGHT ON WITH BOTH PACK ON. LIGHT EXTINQUISHED W L PACK OFF. IND INOP ON ECS-MSG PAGE. RIGHT FLOW CNTRL VALVE WILL OPEN PARTIALLY AND THEN SNAP CLOSED. VALVE & PACK INOP. REPLACED RT FLOW CONTROL AND SHUTOFF VALVE (V17) PER MM. OPS CHECKS AND LEAK CHECK GOOD.

Part: FIRE BOTTLE — DISCHARGED (APU) · airframe 45,553 hrs · 12,458 cycles

APU INOP DUE TO APU BOTTLE DISCHARGE LIGHT ON. REPLACED APU FIRE EXT BOTTLE PER MM.

Part: DUCT — CRACKED (CARGO HEAT) · airframe 45,559 hrs · 12,461 cycles

FWD CARGO HEAT DUCT IN AC BAY CRACKED. REPLACED DUCT.

Part: UNKNOWN — MALFUNCTIONED (CARGO BAY) · airframe 45,551 hrs · 12,457 cycles

PER RAMP BULK CARGO PIT FLOOR INSIDE OF DOOR IS TOO HOT TO TOUCH. VERIFIED BY AIRCRAFT MAINTENANCE. AFT BULK CARGO PIT FLOOR VERY HOT, SHUT APU BLEED VALVE OFF AND FLOOR COOLED. APU BLEED OK. HEAT IN FLOOR CAUSED BY BULK CARGO HEAT. BECOMES HOT WHEN BULK CARGO HEAT AND VENT IS SELECTED ON. CARGO HEAT DEFERRED DF166. AREA BETWEEN STA 1430 TO 1470. BULK CARGO HEAT INOP. FOUND FLOOR WARM FROM BULK CARGO HEAT SYS, CHECKED DUCT FOR CRACKS OR DAMAGE, NONE NOTED. ACP BULK CARGO HEAT CHECK PER MM. NOTE THAT DUCT WAS INSPECTED WITH FLEX BOROSCOPE FROM BOTH END OF DUCT. STARTING AT HOSE ITEM 70 AS IT CONNECTS AT ITEM 120 FIG C PG 2 TO ITEM 100 AS IT CONNECTS TO ITEM 175 FIG F PG 3 OF IPC 21-4 4-01-008.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 45,543 hrs · 12,455 cycles

CTR AUX OVRD PUMP LOW PRESS LIGHT ON, SW ON, EICAS MSG CTR L-R FUEL PUMP. POSITION 7 (7=L CTR,11=R CTR). VERIFIED RIGHT PUMP LO PRESSURE LIGHT NORMAL OPS PER MEL. LEFT CTR PMP INOPED. NEED TO TROUBLESHOOT, LEFT PUMP APPEARS TO BE WORKING, ON RETURN TO BLOCKS. FOUND LEFT FUEL OVRD PRESS SW S423 BAD. REPLACED SW SYSTEM, CHECKED GOOD.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 45,509 hrs · 12,448 cycles

STATUS MESSAGE CABIN ALT AUTO 1 UNABLE TO CLEAR. BITE SHOWING AC MOTOR. ACCMP'D BITE OF NR 1 CABIN PRESSURE CONTROLLER PER MM. FAULT SHOWS "SELECTOR". REPLACED CABIN PRESSURE SELECTOR PANEL M13 PER MM, OPS CKD GOOD. STATUS MSG RETURNED. ITEM HAS SEVERAL HISTORIES WITH AUTO CONTROLLER 1 AND CONTROL PANEL ALREADY REPLACED. RPL CABIN OUTFLOW VLV ACTUATOR. ACT MR21324 = PCN 563-9223. NEED TO HAVE THROAT PRESSURE SENSE LINES CHKD OR HAVE FLOW CONTROL VLV REPLACED PER FIM. LEFT & RIGHT FLOW CONTROL VALVES REPLACED PER AMM. BITE TESTED AUTO CABIN PRESS CONTROLLER SYS AUTO-1 PER A. NOFAULTS.

Part: CAP — OUT OF TOLERANCE (P1-3 PANEL) · airframe 45,061 hrs · 12,353 cycles

A-T DISC LIGHT ON P1-3 PANEL INOP. REPLACED LIGHT SWITCH CAP, OPS CHECKED OKAY.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 44,952 hrs · 12,328 cycles

SEAT 1B HAS LOOSE WIRE AND PLACARD OFF SEAT ON FLOOR NEXT TO SEAT. REPLACED EMERGNECY LIGHT ASSY. OP CHECKED GOOD.

Part: LIGHT — UNSECURE (SEAT 1B) · airframe 44,910 hrs · 12,319 cycles

EXIT SIGN HANGING BY WIRES SEAT 1B. SECURED 1B EMERGENCY STRIP. CKS OK.

Part: SHUTOFF VALVE — FLUCTUATES (RIGHT) · airframe 44,866 hrs · 12,311 cycles

DURING CLIMB & DESCENT RT DUCT PRESSURE FLUCTUATES BETWEEN 15-35 PSI. REPLACED NR 2 ENG PRSOV. RAN ENG AND LEAK CKD. OPS CHECKED NORMAL.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 44,650 hrs · 12,265 cycles

SEAT 1B HAS LOOSE WIRES AT THE BOTTOM THAT LIGHT THE EMERGENCY EXIT PATH FLOOR MARKINGS. REPLACED SEAT EMERGENY LIGHT. OPS OKAY.

Part: CONNECTOR — DIRTY (COOLING FAN) · airframe 44,554 hrs · 12,243 cycles

STATUS MESSAGE "RT IDG VALVE". FOUND 1K OHMS FROM (K1032) PIN 13 TO IDG OIL COOLER FAN AIR S-O VALVE PIN 'B' ON (D11046). CORRECTED BY CLEANING AND INSPECTING FIRE-WALL CONNECTOR (D4216P). NOW WIRING RINGS OK, OPS CHECKED GOOD WITH ENGINE RUN, NO FAULTS.

Part: LIGHT — DISLODGED (SEAT 1B) · airframe 44,344 hrs · 12,189 cycles

EMERGENCY EXIT LIGHT BROKE OFF OF SEAT 1B. INOPERATIVE IAW MEL. RESECURED LIGHT ASSY BUT LIGHT IS INOPERATIVE. REPLACED EMERGENCY LIGHT IAW MM. EMERGENCY LIGHT OPS CHECK OK.

Part: FAN — ODOR (RECIRCULATION) · airframe 44,206 hrs · 12,160 cycles

ELECTRICAL ODOR IN CABIN, FLIGHT DIVERTED. REPLACED RECIRCULATION FAN AND FILTER. RAN ENGINES FOR 5 MIN NO ODORS NOTED. ACFT RETURNED TO SERVICE.

Part: LIGHT — BROKEN (SEAT17B) · airframe 43,902 hrs · 12,086 cycles

EMERGENCY LIGHT ON SIDE OF SEAT 17B BROKEN IN HALF. REPLACED EMERGENCY LIGHT. CHECKS GOOD.

Part: BLOCKER DOOR — OUT OF POSITION (THRUST REVERSER) · airframe 43,764 hrs · 12,049 cycles

NR 1 ENG LT REVERSER OTBD SIDE AT 12 O'CLOCK POSITION BLOCKER DOOR IS HANGING DOWN. INSTALLED BLOCKER DOOR AT POSITION 11:00 PER AMM. REPLACED DAMAGED BLOCKER DOOR PER MM. OPS CHECKS OKAY.

Part: GCU — FAULTY (RIGHT) · airframe 43,654 hrs · 12,020 cycles

CREW REPORTS ON TAXIOUT GOT RT ENG IDG VALVE EICAS MESSAGE. VALVE LOCKED OUT PER MEL 7521D. ACP COMPONENT RESISTANCE CHECK AND OPERATIONAL TEST WITH EXTERNAL AIR USING MIPS PW 4000 IDG AOC TS. VALVE OPERATED WITH NO MSG. ACCOMPLISHED BLOCK 6 POWER RUN. VERIFIED VALVE OPENED AND CLOSED OUT TEMP COOLED. NO STATUS MSG ALSO REPLACED GCU AND RELAY K1031. ALL OPERATIONS CHECKED ON RUN. BPCU CLEAN AFTER RUN. DID NOT REPLACE K1031, BUT REPLACED K971 (R IDG AIR COOLER VLV RELAY).

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 43,518 hrs · 11,989 cycles

SEAT 25A EMERGENCY PATH LIGHT BROKEN OFF. REPLACED LENS. OPS OK.

Part: LIGHT — MISSING (SEAT 1A) · airframe 43,338 hrs · 11,942 cycles

EMERGENCY LIGHT MISSING ON SIDE OF SEAT 1A. INSTALLED EMERGENCY LIGHT.

Part: LIGHT — MISSING (SEAT 2H) · airframe 43,338 hrs · 11,942 cycles

EMERGENCY LIGHT STRIP ON SIDE OF SEAT 2H MISSING. INSTALLED EMERGENCY LIGHT.

Part: MODULE — FAULTY (INSTRUMENT PANEL) · airframe 43,137 hrs · 11,889 cycles

CAPT PITOT HEAT ON OVERHEAD PANEL DIM WITH SWITCH IN BRIGHT. DIM BRIGHT FUNCTION INOP. LIGHT DIM ONLY, PITOT HEATER SYS OPERATES NORMALLY. NEEDS CAP AND BASE ASSY. REPLACED LIGHT CAP MODULE. DIM BRT TEST AND PITOT HEAT TEST NORMAL.

Part: SWITCH — INTERMITTENT (CARGO BAY) · airframe 43,020 hrs · 11,856 cycles

AFT PIT SYS LATERAL RAILS INOP ELECTRICALLY. FOUND FWD LATERAL RAILS ELECTRICALLY INTERMITTENT REPLACED RELAYS K292, K294, K296, NO HELP. SWAPPED TDO RELAYS, NO HELP NEED TO CONTINUE. T-S FOUND EIGHT DIRECTION SELECTOR SWITCH INTERMITTENT. REMOVED AND REPLACED SWITCH AS PER MM.

Part: EXCITER — MALFUNCTIONED (APU) · airframe 42,933 hrs · 11,833 cycles

APU NO START 3 ATTEMPT SWITCH FAULT LIGHT. REPLACED APU IGNITER AND IGNITION EXCITER AS PER MM, OPS CHECKED GOOD.

Part: SENSE LINE — DAMAGED (NR 2 ENGINE) · airframe 42,895 hrs · 11,824 cycles

FOUND AIR SENSE LINE DAMAGED ON LT SIDE OF NR 2 ENG TURBINE CASE AT STARTING AT APPROX 9 O'CLOCK POSITION, LINE IS RIGID AND APPROX 4' IN LENGTH. REPLACED WITH NEW SENSE LINE. SAFTIED AND SECURED.

Part: LIGHT — UNSECURE (SEAT 2H) · airframe 42,608 hrs · 11,759 cycles

EMERGENCY EVAC LIGHT POPPED OUT AND HANGING BY WIRE ON SIDE OF 2H. SECURED EMERGENCY PATH LIGHT ON SEAT 2H & OP CHECKED.

Part: INDICATOR — FAULTY (TE FLAPS) · airframe 42,545 hrs · 11,742 cycles

FLAP INDICATOR SPLIT. FLAPS AT ZERO, VISUALLY VERIFIED, FLAP INDICATOR INDICATES LT AT ZERO, RT AT 1. PROBLEM WITH RIGHT SIDE INDICATOR: STICKS AT 1 DEGREE. OPERATED FLAPS THRU COMPLETE RANGE TO VERIFY OPERATIONS. NORMAL OPS. REPLACED INDICATOR, NO HELP. ACCOMPLISHED BITE CHECK OF FSEU, NO FAULTS. CYCLED FLAPS, INDICATIONS OKAY. INDICATIONS ON FLIGHT 519 OK PER CREW.

Part: ACTUATOR — FAULTY (LT A/C PACK) · airframe 42,516 hrs · 11,736 cycles

LEFT PACK CONTROLLER FAULTS RAM AIR INLET ACTUATOR. REPLACED LEFT RAM AIR INLET ACTUATOR. RAN PACK, OP CHECKS NORMAL.

Part: ACTUATOR — FAULTY (RAM AIR INLET) · airframe 42,516 hrs · 11,736 cycles

'L PACK INOP' LIGHT ON. EICAS MSG 'L PACK TEMP' DISPLAYED. LIGHT DID NOT EXTINGUISH WHEN 'STAND BY' SELECTED. 'RESET' PUSHED, LIGHT EXTINGUISHED THEN WENT ON. CREW COMMENTS: SEEMS TO WORK NORMALLY IN STANDBY. REPAIRED LEFT RAM AIR INLET ACTUATOR. OP CHECK NORMAL.

Part: SKIN — DAMAGED (NR 1 SLAT) · airframe 42,337 hrs · 11,694 cycles

LT WING NR 1 L/E SLAT DAMAGED. REMOVED SLAT AND ROUTED TO SHOP 321. REPLACED NR 1 L/E SLAT IAW MM.

Part: VALVE — FAULTY (RT ENGINE) · airframe 42,318 hrs · 11,689 cycles

RT ENG HPSOV EICAS AND RT ENG BLEED LIGHT AFTER ENG START W-BLEED SWITCH OFF. REPLACED HPSOV AND HP CONTROLLER. HPSOV IS ACTIVATED FOR TEST. ACP'D HIGH PWR RUN IAW JRH, NR 2 BLEED OPS CK GOOD, NO FAULTS NOTED. BLEED LIGHT DID NOT COME ON.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 42,166 hrs · 11,651 cycles

NR 2 ENGINE DRIVEN PUMP IS LEAKING HYDRAULIC FLUID. REMOVED & REPLACED LEAKING ENGINE DRIVEN PUMP. OPS NORMAL.

Part: RECEPTACLE — FAILED (GROUND POWER) · airframe 42,166 hrs · 11,651 cycles

GROUND POWER RECEPTICAL FAILED NO-GO GAUGE TEST. UNABLE TO ACP DURING A-CK VISIT. ORDERED RECEPTACLE. PART NOT STOCKED HNL. REPLACED RECEPTACLE. TASK COMPLETED.

Part: LIGHT — UNSECURE (SEAT 2H) · airframe 42,110 hrs · 11,637 cycles

SEAT 2H LIGHT ON SEAT SIDE OUT. EMERGENCY LIGHT STRIP NOT SECURE ON SEAT. SECURED EMERGENCY LIGHT STRIP.

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHTS) · airframe 42,110 hrs · 11,637 cycles

EMERGENCY LIGHTS ON LT SIDE OF FIRST CLASS IS INOP. FOUND SEAT HARNESS AT SEAT 4AB SHORTED. NO SEAT HARNESS AT HNL. REPLACED HARNESS, OPS OK.

Part: LIGHT — MISSING (CABIN) · airframe 42,008 hrs · 11,613 cycles

EMERGENCY LIGHT ASSY MISSING AT:1B FWD, 5H FWD, 2B AFT, AND 2H AFT. REPLACED MISSING EMERGENCY LIGHT ASSY: 1B FWD, 5H FWD, 2B AFT, AND 2H AFT, CKD NORMAL ON GROUND.

Part: LIGHT — DAMAGED (SEAT 1B) · airframe 41,859 hrs · 11,573 cycles

SEAT 1B EMERGENCY LIGHT (1 EA) DAMAGED. REPLACED EMERGENCY LIGHT AT 1B. OPS CKS OK.

Part: UNKNOWN — UNKNOWN (ELEVATOR) · airframe 41,779 hrs · 11,556 cycles

DURING CONTROL CHECK EXPERIENCED A HYD BUMP WHEN RELEASING AFT AND FULL FWD ELEVATOR. BUMP IN CONTROL COLUMNS IS FELT AFTER RELEASING COLUMN FROM FULL NOSE UP OR FULL NOSE DOWN POSITION. ACP'D CK AND INSPECTED PULLYS AND CABLES NO IRREG FOUND. POSSIBLY BUMP FROM SNUBBING RING.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 41,594 hrs · 11,508 cycles

EMERGENCY LIGHT INOP AT SEAT 3HJ AFT LAMP. NEEDS SEAT HARNESS, AFT EMERGENCY LAMP CONNECTOR BROKEN. REPLACED HARNESS, CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERENCY LIGHTS) · airframe 41,594 hrs · 11,508 cycles

EMERGENCY LIGHT INOP AT SEAT 20 HJ. RELAMPED, OP CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,594 hrs · 11,508 cycles

EMERGENCY LIGHT INOP AT SEAT 29 HJ. RELAMPED, OPS CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 41,594 hrs · 11,508 cycles

FLOOR EMERGENCY LIGHT STRIP INOP AT LT LAV, BEHIND SEAT ROW 41AB. 2 EA LAMPS INOP ADJACENT TO EACH OTHER. FOUND EMERGENCY LIGHT WIRING UNDER SEAT 41AB CUT AND ENDS CAPPED AND STOWED. REPAIRED WIRING AND SEAT 41 AB AND LAV EMERGENCY LIGHT, OP CHECK GOOD.

Part: GCU — FAULTY (APU GENERATOR) · airframe 41,048 hrs · 11,376 cycles

ACFT WON'T SWITCH TO APU GENERATOR POWER. NO TIME TS, TRIED RESETS NO HELP. REPLACED APU GCU. RAN APU AND POWER TRANSFERRED NORMALLY. APU GENERATOR VOLTS AND FREQ NORMAL AND ONLINE.

Part: STARTER — FAULTY (RT ENGINE) · airframe 40,995 hrs · 11,365 cycles

CREW REPORTS RT ENG START VALVE OPENED AND LIGHT EXTINGUISHED BUT NO ENGINE ROTATION. ALSO GND CREW STATED SMOKE FROM ENG DURING START ATTEMPT. REPLACED STARTER AND STARTER SHUTOFF VALVE.

Part: TRANSMITTER — FAULTY (ENGINE OIL) · airframe 40,944 hrs · 11,356 cycles

CREW REPORTS L ENG OIL PRESSURE IS AT 400PSI ALL OTHER INDICATIONS NORMAL. FLT CREW NOTED 400 PSI AT CLIMB POWER ONLY. READ NORMAL AND MATCHED NR 2 ENGINE AT ALL OTHER POWER SETTINGS INCLUDING DESCENT AND IDLE. IN PROCESS OF REPLACING OIL PRESS TRANSMTR NR 1 ENG REPLACED NR 1 OIL PSI TRANSMTR. RAN BOTH ENGINES AND OPS CKS GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 40,940 hrs · 11,355 cycles

EMERGENCY LIGHT STRIP MISSING ON SEATS 1AB, 2AB, 4AB AND 6AB. (1EA PER SEAT). REPLACED MISSING EMERGENCY LIGHT STRIPS, CHECKS OK.

Part: TRANSMITTER — FAULTY (FLAPS) · airframe 40,630 hrs · 11,278 cycles

FLAP-SLAT ELEC LIGHT INTERMITTENT ON TAXI IN. UNABLE TO VERIFY THE PROBLEMS, REPLACED FSEU AS PRECAUTION AND SYS CHECKED NORMAL. PROBLEM RECURRED. ACCOMPLISHED BITE ON FSEU AND HAD M489 FAULT. RPLC'D NR 8 FLAP POSITION TRANSMITTER. SYS CHECKS OK AT THE PRESENT TIME.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 40,584 hrs · 11,266 cycles

EMERGENCY LIGHTS INOP LT SEAT ROWS 1-6, FWD GALLEY FLOOR TRACKS 2EA AND DR 1L LWR EXIT SIGN. REPLACED BATTERY PACK. BATTERY PACK NO HELP. FOUND L901 SHORTED, DISCONNECTED EMERGENCY LIGHT STRIP AT DR 1L LAV. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED NORMAL.

Part: ACTUATOR — FAULTY (TE FLAPS) · airframe 40,584 hrs · 11,266 cycles

FLAP DISAGREE MSG. FOUND "ALT FLAP PWR" CB POPPED. RE-SET AND SYS OP NORMAL. FOUND FLAP ROT ACT OVERLOAD IND ON ACT NR 1, NR 3 AND NR 8 POPPED. REPLACING ALL 3 ACT. NR 8 REPLACED. STARTING NR 1. REPLACED NR1 T-E ROTARY ACTUATOR. REPLACED NR 3 ROTARY ACTUATOR.

Part: SWITCH — OUT OF POSITION (TE FLAPS) · airframe 40,316 hrs · 11,203 cycles

T/E FLAP DISAGREE. FLAP OVERRIDE SWITCH IN OVERRIDE. REPOSITIONED SWITCH. PERFORMED FSEU BIT. NO FAULTS. RAN FLAPS ON GROUND, NO FAULTS. LUBED TRAILING FLAPS. SYS GROUND CKS OKAY. NO PREVIOUS HISTORY.

Part: PCA — MALFUNCTIONED (FLT CONTROLS) · airframe 40,297 hrs · 11,198 cycles

WHEN ACCOMPLISHING FLIGHT CONTROL CHECK, ELEVATOR CHATTERS. DOES NOT FEEL LIKE CONTROL COLUMN PROBLEM, POSSIBLY HYDRAULIC OR FLT CONTROL PROBLEM, PER CREW. REPLACED LT ELEVATOR CENTER SYSTEM PCA. LEAK CHECK AND OPS CHECK GOOD.

Part: GCU — MALFUNCTIONED (NR 2) · airframe 40,048 hrs · 11,134 cycles

RT GEN FIELD MAN RESET LIGHT IS ON. REPLACED GCU, OPS CHECKS GOOD.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 40,039 hrs · 11,132 cycles

FIRST OBSERVERS O2 MASK MIC DOES NOT TEST. THE 1ST OBSERVERS SEAT INOPERATIVE. REPLACED O2 MASK ASSY.

Part: STOWAGE BOX — FAULTY (COCKPIT) · airframe 40,039 hrs · 11,132 cycles

CAPT O2 MASK MIC NOT WORKING. REPLACED AUDIO ACC UNIT, NO HELP. MASK STORAGE BOX BAD FROM STOCK, SWAPPED OBSERVERS WITH CAPT'S MASK BOX UNIT, ALL CHECKS OK.

Part: ENGINE — SEPARATED (NR 1) · airframe 40,029 hrs · 11,130 cycles

CREW REPORT: LEFT ENGINE WOULD NOT SHUTDOWN WITH FUEL CONTROL SWITCH, PULLED FIRE HANDLE TO SHUT DOWN. FOUND NR 1 ENG, INTERMEDIATE PRS CHECK VLV SEPARATED FWD SIDE. LOW STAGE HOT AIR DAMAGED MULTIPLE WIRES UNDER VLV ON WIRE BUNDLES "W3506"AND "W3538" BELONGING TO FMU AND IDG. WILL REPLACE ENGINE WITH SN-724465. NEED TO CONVERT ENGINE.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 39,962 hrs · 11,115 cycles

SECOND OBSERVER O2 MASK BROKEN. SWAPPED WITH CAPTAIN'S, NEED MASK AND BOX ASSY. REPLACED MASK AND STOWAGE BOX.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,952 hrs · 11,113 cycles

AFT LAV LT SIDE EMERGENCY LIGHT INOPERATIVE. REF PTT SEQ 9522015. REPLACED BATTERY, OPS CHECKED, OKAY.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 39,952 hrs · 11,113 cycles

SEAT 35AB -41AB EMERGENCY LIGHT INOP. REPLACED BATTERY LOC SEAT 39AB. OPS CHECKED OKAY.

Part: WIRE HARNESS — CHAFED (RT IDG) · airframe 39,563 hrs · 11,016 cycles

RT IDG DRIVE LIGHT ILLUMINATING. SERVICED RT IDG. FOUND CHAFED AND SHORTING WIRES IN HARNESS W3538 ABOUT 8 INCHES FROM IDG CONNECTOR D10964. MADE SPLICE REPAIR OF RT GEN WIRES W3538-203B (R)-18. SPLICES LOCATED IN HORIZONTAL RUN BETWEEN TWO CLAMPS APPROX 16 INCHES FROM IDG CONNECTOR D10964. SERVICED RT IDG. WIRES NEED TO BE REPLACED WITHIN 500 HOURS. WHILE REPAIRING RT IDG WIRING FOUND WIRES TO START VALVE CHAFED. DAMAGE WAS TO INSULATION ONLY. RE-INSULATED WIRES.

Part: LIGHT — MISSING (CABIN) · airframe 39,522 hrs · 11,004 cycles

SEAT 14HJ SIDE SEAT EEL STRIP IS MISSING. REPLACED MISSING EEL STRIP AT SEAT 14HJ. OPS CHECKS NORMAL.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 39,426 hrs · 10,976 cycles

EMERGENCY EXIT LIGHTS FLICKERING ROWS 20-24 HJ. REPLACED POWER SUPPLY, EMERGENCY LIGHTS 20-24HJ CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 39,403 hrs · 10,969 cycles

SPOILERS EICAS MESSAGE WITH SPOILERS LIGHT ON OVERHEAD PANEL. REPLACED NR 3R SCM, OPERATIONAL CHECK GOOD. NO EICAS MESSAGE DISPLAYED OR SPOILER LIGHT ON OVERHEAD PANEL.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 39,310 hrs · 10,942 cycles

DOORS L1 AND R1 EXIT SIGNS INOP. REPLACED FUSE AND CHECKED OPERATION OF LIGHT CHECKS GOOD PER MM 33-51-00.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 39,310 hrs · 10,942 cycles

A-ZONE AISLE LIGHTS ON SEATS ARE INOP. REPAIRED UNDER SEAT CABLE INTERFACE ASSY FOR SEAT MOUNTED EMERGENCY LIGHTS AND TESTED GOOD.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 39,310 hrs · 10,942 cycles

EXT FUSELAGE STA 1685 BETWEEN STR 34L AND 35L HAS SKIN PUNCTURE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR. NO CRACKS NOTED AFTER DAMAGE REMOVED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,310 hrs · 10,942 cycles

EXTERIOR EMERGENCY LIGHTS L396, L645, AND L391 ARE INOP. RELAMPED LIGHTS L645 AND L391, OPS CHECKS GOOD. LIGHT L396 OPS CHECKS NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 39,310 hrs · 10,942 cycles

SEAT 32 AB EMERGENCY BAR MISSING. SEAT OVERHAULED AT REGENT, RECEIVED WITH 8130-9 WITH LIGHT BAR INSTALLED.

Part: SPLASH GUARD — CORRODED (R1 DOOR) · airframe 39,310 hrs · 10,942 cycles

R-1 DOOR SPLASH GUARD CORRODED. INSTALLED NEW SPLASH GUARD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,310 hrs · 10,942 cycles

ROW 2 LEFT CEILING EMERGENCY LIGHT INOP. RELAMPED AISLE LIGHT AT ROW 2L, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,310 hrs · 10,942 cycles

CEILING EMERGENCY LIGHT AT ROW 25-26 RT IS INOP. RELAMPED AISLE LIGHT AT ROW 25-25. OPS CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,310 hrs · 10,942 cycles

MAIN CABIN FLOORBEAM STA 325, LBL 30 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT UPPER T-CAP FROM RBL 30 TO RBL 70, STA 325. INSTALLED REPAIR T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,310 hrs · 10,942 cycles

MAIN CABIN FLOORBEAM CORRODED AT STA 287, BL 0 TO LBL 10. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW UPPER T-CAP FROM ZERO BL TO RBL 70, STA 287.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,310 hrs · 10,942 cycles

MAIN CABIN FLOOR SUPPORT AT BS 347-350, RBL 89 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW FLOOR SUPPORT STA 347 TO 368, RBL 89.

Part: SLIDE — DAMAGED (RT OVERWING) · airframe 39,310 hrs · 10,942 cycles

RIGHT OVERWING SLIDE FOUND UNLACED. REMOVED AND REPLACED RIGHT OVERWING SLIDE ASSY.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,310 hrs · 10,942 cycles

MAIN SEAT TRACK STA 325 LBL 11 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION OF SEAT TRACK STA 325 TO 425, LBL 11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,310 hrs · 10,942 cycles

MAIN CABIN SEAT TRACK STA 325 RBL 11 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED SEAT TRACK SECTION STA 325 TO 425, RBL 11.

Part: FLOORBEAM — CORRODED (BS 347 RBL 30) · airframe 39,310 hrs · 10,942 cycles

MAIN CABIN FLOORBEAM STA 347 APPROX RBL 30 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED TEE CAP RBL ZERO TO 70. FABRICATED SPLICE ANGLES AND NEW 'T' CAP AND INSTALLED.

Part: CABLE — FRAYED (ENTRY DOOR) · airframe 39,310 hrs · 10,942 cycles

LEFT AFT ENTRY DOOR COUNTERBALANCE PRIMARY CABLE IS FRAYING, BS 1461-1480, STR 1L-2L. REMOVED AND REPLACED LEFT AFT ENTRY DOOR COUNTERBALANCE PRIMARY CABLE. SYSTEM TESTED GOOD.

Part: PULLEY — WORN (ENTRY DOOR) · airframe 39,310 hrs · 10,942 cycles

LEFT AFT ENTRY DOOR COUNTERBALANCE PRIMARY SWIVEL CABLE PULLEY WORN, BS 1461- BS 1480, STR 1L - 2L. REPLACED COUNTERBALANCE PULLEY AT BS 1461-1480, STR 1L-2L. DOOR OPS CHECK NORMAL.

Part: BATTERY — NO TEST (ESCAPE SLIDE) · airframe 39,185 hrs · 10,911 cycles

RIGHT EMERGENCY ESCAPE SLIDE WON'T TEST. REPLACED OFF WING ESCAPE EMERGENCY BATTERY M962 RIGHT SIDE, OPS CHECKS NORMAL.

Part: CONTROL PANEL — UNSECURE (SLIDE) · airframe 39,181 hrs · 10,910 cycles

RT SLIDE SQUIB DOES NOT TEST. RESEATED TEST PANEL. SYSTEM OPS CHECK OKAY.

Part: LIGHT — SHORTED (SEAT 41AB) · airframe 38,981 hrs · 10,857 cycles

FOUND EEL INOP FROM SEAT 35AB TO 41AB. TRIED BATTERY PACK AND CHARGER, NO HELP. LIGHTS ON VERY DIM. LOWER SIDEWALL AT SEAT 40AB REMOVED AND PART OF CARPET UP AT SEAT 41AB. FOUND LIGHT ASSY AT 39AB SHORTED, REPLACED IT, SYSTEM CHECKS GOOD. CLOSED AND SECURED PANELS AND CARPETING.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 38,880 hrs · 10,835 cycles

EMERGENYC LIGHTS AT ROW 23AB 31AB AND 17HJ INOP LT ASSY. REPLACED EMERGENCY LIGHT AT SEAT 23AB. STILL NEED TO REPLACE LIGHTS AT ROW 31AB AND 17HJ. AT SEAT 31AB AND 17HJ EMERGENCY LIGHT HAS BROKEN WIRES AT CONNECTOR GOING TO EMERGENCY LIGHT ON SEAT HARNESS SIDE. REPLACED LIGHT ASSY AND CABLES. LIGHT CHECKS GOOD.

Part: BYPASS VALVE — FAILED (NR 1 ENGINE) · airframe 38,622 hrs · 10,775 cycles

LEFT ENGINE FUEL OIL COOLER BYPASS VALVE ASSY HAS A RUNNING OIL LEAK AROUND ASSY. RE-CLEANED AREA WITH CONTACT CLEANER AND RE-RUN ENGINE AND BYPASS ASSY IS DRIPPING AFTER ENGINE SHUTDOWN. OIL IS VISIBLE RUNNING DOWN FWD CONNECTORS OF BYPASS VLV.

Part: BATTERY — DEFECTIVE (MAIN) · airframe 37,823 hrs · 10,572 cycles

MAIN BATTERY CHARGER STATUS MESSAGE CAME ON IN DESCENT. REPLACED SHIPS MAIN BATTERY. BATTERY AND CHARGER OPS CHECK OKAY.

Part: CABLE — DAMAGED (CABIN) · airframe 37,759 hrs · 10,556 cycles

SEAT 1B EEL INOP. REPAIRED EEL CABLE. OP CHECKED OK.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 37,759 hrs · 10,556 cycles

EEL INOP BETWEEN DOOR 1L AND 1R, (CROSSAISLE) FLOOR LIGHT. REPAIRED LIGHT CONNECTION AT SIDEWALL, OPS NORMAL.

Part: CABLE — DEFECTIVE (CABIN) · airframe 37,759 hrs · 10,556 cycles

SEATS 1B, 17H, 37H, 38H, 39H, 41H EEL INOP. REPLACED EEL CABLE AT SEATS 41HF FEEDER, EMERGENCY LIGHTS CHECK OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 37,759 hrs · 10,556 cycles

AFT GALLEY RT FLOOR STRIP EEL INOP. SECURED EEL CONNECTOR AT SEATS 41HJ, EMERGENCY LIGHTS CHECK OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 37,759 hrs · 10,556 cycles

SEAT 39A MISSING EEL LIGHT. REPLACED EEL STRIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,759 hrs · 10,556 cycles

LT AND RT AFT MID SLIDE GROUND ILLUMINATION EMERGENCY LIGHT INOP. SECURED LAMPS, OPS CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,759 hrs · 10,556 cycles

LOWER CEILING EMERGENCY LIGHTS AT 8A AND 40A INOP. RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — LOOSE (CABIN) · airframe 37,759 hrs · 10,556 cycles

LT AND RT AFT LAV FLOOR STRIP EEL INOP. SECURED EEL CABLE CONNECTORS, EMERGENCY LIGHTS CHECK OK.

Part: LIGHT — MISSING (CABIN) · airframe 37,553 hrs · 10,507 cycles

ONE EEL STRIP LIGHT ON SIDE OF SEAT 3H IS MISSING. REPLACED EEL LIGHT ASSEMBLY.

Part: RVDT — FAULTY (LE SLAT) · airframe 37,553 hrs · 10,507 cycles

NR 7 L/E SLAT SHUTDOWN STATUS MESSAGE. TRBLSTG 27-81-00 FIG 112A. BITE SHOWS M603 FLAP LEVER RVDT MISRIG (SECT 1). SUSPECT INTERMITTENT RVDT. WILL REPLACE ONCE IN HAND. REPLACED M603 RVDT.

Part: WARNING SYSTEM — ACTIVATED (LE SLAT) · airframe 37,553 hrs · 10,507 cycles

NR 7 L/E SLAT SHUTDOWN STATUS MESSAGE.

Part: ROTARY ACTUATOR — TRIPPED (TE FLAP) · airframe 37,553 hrs · 10,507 cycles

TRAILING EDGE FLAP DISAGREE INDICATION WHEN WE WENT TO FLAPS 5. LOWERED FLAPS WITH ALT SWITCH PER CL FOUND LT WING INBOARD FLAP OUTBOARD ROTARY ACT TRIPPED; RESET. ALSO FOUND RT WING OUTBOARD FLAP OUTBOARD FLAP ROTARY ACT TRIPPED; RESET. OPERATED FLAPS ONE CYCLE ALL INDICATIONS NORMAL.

Part: ROTARY ACTUATOR — TRIPPED (TE FLAP) · airframe 37,553 hrs · 10,507 cycles

T/E FLAP DISAGREE INDICATION, WHEN CREW WENT TO FLAPS 5. LOWERED FLAPS WITH ALT SWITCH PER CL. FOUND LT WING INBOARD FLAP OUTBOARD ROTARY ACT TRIPPED; RESET. ALSO FOUND RT WING OUTBOARD FLAP OUTBOARD FLAP ROTARY ACT TRIPPED; RESET. OPERATED FLAPS ONE CYCLE, ALL INDICATIONS NORMAL.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 37,193 hrs · 10,418 cycles

NR 2 ENG EDP DRIVE PAD LEAKING OIL AT 30 DROPS A MIN DURING ENG RUN AND AFTER SHUTDOWN. REMOVED AND REPLACED HYDRAULIC PUMP DRIVE OIL SEAL. REPLACED EDP CARBON SEAL & REPLACED EDP. NO LEAKS NOTED.

Part: LIGHT — MISSING (CABIN) · airframe 37,193 hrs · 10,418 cycles

EXIT STRIP LIGHTING MISSING FROM 31B, PART AT DOOR 1L. REPLACED EEL STRIP. TESTS OKAY.

Part: CHARGER — FAULTY (MAIN BATTERY) · airframe 36,983 hrs · 10,372 cycles

EICAS MSG MAIN BATTERY CHARGER. REPLACED MAIN BATTERY CHARGER.

Part: PUMP — LEAKING (LT ENGINE) · airframe 36,894 hrs · 10,352 cycles

EDP HYD OVERHEAT LGT ILLUM. EICAS MSG (L, R) PRIM HYD OVERHEAT DISPLAYED. PUMP WAS DEACTIVATED, POS 1 (01=L,02=R). FOUND L ENG HYD PUMP LEAKING. REPLACED PUMP. ACP'D SYSTEM FLUSH, REPLACED CASE DRAIN AND PRESSURE FILTERS 3 TIMES. SERVICED L HYD SYS TO FULL.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 36,707 hrs · 10,309 cycles

THE 'T-E FLAP DISAGREE' EICAS MSG DISPLAYED WITH FLAPS AT 20 UNITS. ACCOMPLISHED BITE TEST OF FSEU AT GATE IN SFO WITH FLAPS STILL AT 20 UNITS. FSEU IS THE OLD NON-DIGITAL TYPE. SHOWED FAULTS FOR M548 AND M603. PERFORMED BITE TEST PER MM 27-51-00-FIG 104, FLAPS AT RETRACTED POSITION ENDED AT BLOCK 4 THE FSEU COMPONENTS AND WIRING ARE OK. CREW REPORTED MSG APPEARED WHEN FLAP HANDLE WAS MOVED FROM 1 UNIT POS TO THE 5 UNIT POS. FLAPS WERE LOWERED TO 20 UNITS IN ALTERNATE. NOTHING UNUSUAL FELT OR NOTICED BY CREW. PERFORMED BITE TEST. TEST OK. ALSO RAN SLATS FLAPS IN EACH POSITION FROM 1 TO 25 UNITS, NO FAULTS OR EICAS MESSAGE, ALSO PERFORMED THE BITE TEST AGAIN ON FSEU NO FAULTS INDICATED. NO RECURRENCE AS OF 12/24/08.

Part: VALVE — FAILED (LT ENGINE) · airframe 36,606 hrs · 10,283 cycles

LEFT ENG HPSOV ON MOMENTARILY DURING DESCENT. PER FLT CREW, CAME ON WHEN PWR PULLED TO IDLE FOR DESCENT AND EXTINGUISHED AFTER APPROX 1 MIN. FOUND HPSOV BAD ON HEALTH CHECK. REPLACED HPSOV. OPS AND LEAK CHECK OKAY. NO FAULTS OR MESSAGES.

Part: PANEL — DELAMINATED (EVAC SLIDE) · airframe 36,134 hrs · 10,166 cycles

RIGHT OVERWING SLIDE PANEL HAS A FOOTBALL SIZE DELAMINATION. DELAMINATED PANEL REMOVED & ROUTED TO SHOP. DOOR ASSY 416T2009-7 ON ORDER FROM BOEING. REPLACED RT OVERWING SLIDE DOOR. RIGGED AND ADJUSTED. REPLACED KEEPERS. EG EVALUATED THE FLUSHNESS CONDITION AND FOUND THAT THE FLUSHNESS OF 0.156 IN LIEU OF THE 0.20 PER MM, IS ACCEPTABLE ALONG THE TRAILING EDGE OF THE PANEL AS IT WILL NOT AFFECT AERODYNAMIC FLOW.

Part: PUMP — MALFUNCTIONED (LT ENGINE) · airframe 36,130 hrs · 10,165 cycles

EDP HYD OVERHEAT LIGHT ILLUM EICAS MSG (L, R) PRIM HYD OVERHEAT DISPLAYED. PUMP WAS DEACTIVATED. POS 1 (01=L,02=R). SAMC TEXT: AFTER EDP SECURED SEVERAL MINUTES LATER LT QTY DROPPED TO ZERO AND EMDP WAS TURNED OFF. REPLACED LT ENG HYD PUMP AND CASE DRAIN FILTER. GROUND RUN ENGINE, LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,134 hrs · 10,166 cycles

THE 29HJ EEL LIGHT INOP. REPLACED LAMP. TEST OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,134 hrs · 10,166 cycles

THE 15AB EEL LIGHT INOP. REPLACED LAMP. TEST OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,134 hrs · 10,166 cycles

LT MID LAV EEL LIGHT INOP. SECURED CONNECTOR TEST OK.

Part: UNKNOWN — CONTAMINATED (AC SYSTEM) · airframe 35,665 hrs · 10,051 cycles

HEAVY ODOR (BURNING SMELL) IN CABIN. RTFL. AC SYSTEM OIL CONTAMINATION REMOVAL. ENGINE RUN TO REMOVE OIL ODORS. SIX QUARTS OIL REMOVED FROM OIL TANK. ALL OIL SMELL HAS DISSIPATED FROM NR 1 ENG BLEED SYSTEM. NO ODORS PRESENT AT END OF PACK BURN.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,665 hrs · 10,051 cycles

HEAVY ODOR (BURNING SMELL) IN CABIN. RTFL.

Part: TURBINE BLADES — FAILED (LT ENGINE) · airframe 35,664 hrs · 10,050 cycles

LEFT ENGINE SURGE DET STATUS MSG. FOUND METAL IN THE TAILPIPE. THE ENGINE WAS REPLACED AT PRIOR TO FURTHER FLIGHT. SHOP TEARDOWN REVEALED THAT THE ENGINE HAD SUFFERED AN HP TURBINE STAGE-2 BLADE UNDER PLATFORM STRESS CORROSION (SCC) FAILURE. ONE BLADE FRACTURED AT THE PLATFORM, WITH A PORTION OF THE PLATFORM MISSING. THIS CAUSED FAILURE OF THREE ADJACENT BLADES. MANUFACTURER HAS INTRODUCED A NEW MATERIAL BLADE WITH AN IMPROVED UNDER PLATFORM COATING TO PRECLUDE SCC FAILURES.

Part: FILTER — UNKNOWN (ENGINE OIL) · airframe 35,561 hrs · 10,022 cycles

R ENG OIL FILTER EICAS LIGHT ILLUM APPROX 1 MIN, WENT AWAY. R OIL FILTER STATUS MSG REMAIN. *S/D* REPLACED MAIN OIL FILTER.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 35,314 hrs · 9,959 cycles

NR 1 ENGINE VIBRATION/POSSIBLE BIRD STRIKE. RTFL. ENGINE NOT SHUT DOWN. AFTER RTF, BIRD STRIKE CONFIRMED. MM FOUND 2 DAMAGED FAN BLADES. REPLACED DAMAGED BLADES AND OPPOSITE BLADES. HP COMPRESSOR BORESCOPE OK. AIRCRAFT RETURNED TO SERVICE.

Part: IDG — MALFUNCTIONED (RIGHT) · airframe 35,314 hrs · 9,959 cycles

EICAS MSG ON RIGHT ENGINE GEN DRIVE DISPLAYED. LIGHT ILLUM GEN DRIVE DISCONNECTED. REPLACED RIGHT IDG.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 35,256 hrs · 9,945 cycles

ENG 1 HUNG START AT 43 PERCENT N2, EGT STABLE, START VALVE MESSAGE & START VALVE LIGHT DISAGREE ON OVERHEAD PANEL. ENGINE SHUT DOWN. GROUND CREW REPORTED LOUD BANG. FOUND STARTER SOAKED WITH OIL. OPENED START VALVE AND THERE WAS A STEADY STREAM OF OIL OUT THE AIR EXIT VANES OF THE STARTER WITH NO ENG ROTATION. REPLACED STARTER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,717 hrs · 9,802 cycles

BAG CART HIT AIRCRAFT BELLY JUST AFT OF MAIN LANDING GEAR. MAJOR REPAIR ACCOMPLISHED: ROUTED OUT DAMAGED SKIN AT BS 1171-1175 AND 1197+22-1197+29 BETWEEN STR 36L-38R. FABRICATED & INSTALLED DOUBLERS, TRIPLERS AND FILLERS.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 34,390 hrs · 9,712 cycles

EMERGENCY LIGHTS AT RIGHT SIDE FROM ROW 26 BACK ON WITH SWITCH ARMED, WENT OFF WITH SWITCH OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY FOR EEL LIGHTING PRECAUTIONARY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,381 hrs · 9,708 cycles

CREW REPORTED A T/E FLAP DISAGREE.

Part: FLAP SYSTEM — STUCK (TE FLAPS) · airframe 33,965 hrs · 9,600 cycles

FLAP HANDLE AT 5, FLAPS LOCKED UP AT 1 EICAS, T/E FLAP DISAGREE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,424 hrs · 9,477 cycles

LEFT EMERGENCY LIGHTS L1 AND L3 OVERWING LIGHTS ARE INOP. REPLACED BATTERY PACK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,424 hrs · 9,477 cycles

RIGHT AFT DOOR UPPER EMERGENCY EXIT LIGHT, DOOR HANDLE ILLUMINATION PORTION IS INOP. RELAMPED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 33,424 hrs · 9,477 cycles

BS 246 AT BL 0, PULLEY SUPPORT CRACKED.

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 33,424 hrs · 9,477 cycles

AFT MANUAL CARGO DOOR HAS DENT APPROX 3 INCHES FROM AFT EDGE AND THREE FEET FROM BOTTOM. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER REPAIR. A/C OK FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 33,424 hrs · 9,477 cycles

L-1 DOOR EMERGENCY EXIT LIGHT IS INOP. RESEATED CONNECTOR.

Part: HOUSING — CRACKED (EVAC SLIDE) · airframe 33,424 hrs · 9,477 cycles

LEFT OVERWING EMERGENCY SLIDE DISCONNECT HOUSING IS CRACKED.

Part: LAMP — FAULTY (EMERGENCY LIGHTS) · airframe 33,424 hrs · 9,477 cycles

EMERGENCY AISLE LIGHT ABOVE SEAT 12HJ IS DIM. REMOVED AND REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,424 hrs · 9,477 cycles

IN SEAT EMERGENCY LIGHTS AT SEATS 3HJ, 24HJ AND 35HJ ARE INOP. REMOVED AND REPLACED LIGHTS.

Part: CYLINDER — DEFECTIVE (EVAC SLIDE) · airframe 33,424 hrs · 9,477 cycles

LEFT OVERWING SLIDE CABLE BALL IS BELOW RETAINER SPRING ON INFLATION CYLINDER.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 33,424 hrs · 9,477 cycles

EXTERIOR LIGHTS, OVERWING EMERGENCY SLIDE AND DOOR LIGHTS ARE INOP (LEFT SIDE). RESEATED CONNECTOR.

Part: SUPPORT BRACKET — CRACKED (BS 246) · airframe 33,424 hrs · 9,477 cycles

BS 246, RBL 13.96 PULLEY SUPPORT BRACKET IS CRACKED.

Part: LIGHT — UNSECURE (L1 DOOR) · airframe 33,424 hrs · 9,477 cycles

EMERGENCY EXIT LIGHT AT L-1 DOOR-UPPER SIGN IS NOT PROPERLY SECURED, CAUSES LENSE TO BE LOOSE.

Part: SUPPORT — CRACKED (BS 246 RBL 15) · airframe 33,424 hrs · 9,477 cycles

BS 246 AT RBL 15.78 PULLEY SUPPORT CRACKED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 33,424 hrs · 9,477 cycles

FOUND EMERGENCY LIGHT AT SEAT 17HJ IS INOP. RESECURED LOOSE CONNECTION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,424 hrs · 9,477 cycles

AFT ENTRY DOOR LEFT AND RIGHT EMERGENCY EXIT LIGHT IS INOP. INSTALLED NEW BATTERY.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 33,424 hrs · 9,477 cycles

BS 246 AT LBL 26.39 STIFFENER IS CRACKED.

Part: LIGHT — FAULTY (COCKPIT) · airframe 33,424 hrs · 9,477 cycles

WITH FLIGHT DECK EMERGENCY LIGHT SWITCH IN ARM, INTERIOR EMERGENCY EXIT LIGHTS TURN ON. AFTER FURTHER TROUBLESHOOTING FOUND EMERGENCY C/B TO BE COLLARED. RESET C/B`S AND CHECKED GOOD IAW MM 33-51-00.

Part: LENS — CRACKED (CABIN) · airframe 33,424 hrs · 9,477 cycles

SEVERAL LOWER EMERGENCY EXIT LIGHT IDENTIFIER LENSES ARE CRACKED OR EXCESSIVELY DIRTY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,378 hrs · 9,466 cycles

SEAT 31B EEL INOP. REPLACED LIGHT STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,378 hrs · 9,466 cycles

SEAT 17H EEL INOPERATIVE. REPLACED LIGHT STRIP.

Part: APU — FLAMED OUT · airframe 33,018 hrs · 9,386 cycles

APU FLAMED OUT AND WOULD NOT RESTART.

Part: LIGHT — MISSING (SEAT 26HJ) · airframe 32,447 hrs · 9,256 cycles

EEL STRIP AT 26HJ MISSING. REPLACED LIGHT STRIP.

Part: CONNECTOR — LOOSE (TE FLAPS) · airframe 32,288 hrs · 9,221 cycles

FLAP - SLAT ELEC EICAS MSG DISPLAYED. REPLACED FLAP POSITION TRANSMITTER. SECURED CONNECTOR ON FLAP POSITION TRANSMITTER 1L ON LEFT WING. OPERATED FLAPS, NO MESSAGES, BITE TEST OF FSEU SHOWED NO FAULTS.

Part: SKIN — DAMAGED (BS 1360 S27R) · airframe 32,224 hrs · 9,206 cycles

RT FUSELAGE APPROX 20 INCHES AFT OF AFT CARGO DOOR STA 1360 STR 27 HAS DAMAGE. ACCOMPLISHED REPAIR PER EVA-70734A AND SRM 53-00-01 FIG201. ACFT OK FOR SERVICE.

Part: SPOILER — MALFUNCTIONED (NR 6) · airframe 31,972 hrs · 9,144 cycles

BINDING IN NR 6 SPOILER. BINDING OCCURRED ONLY WITH LEFT HYD SYSTEM AND LEFT WING DOWN - SPOILER NR 6 UP. SPOILER WAS CHATTERING WITH ASSOCIATED NOISE. WITH ONLY CENTER OR RIGHT HYD, NO BINDING OR NOISE NOTED. NR 6 SPOILER FAILED TO LIFT WITH LEFT HYD POWER AT ONE POINT DURING TROUBLESHOOTING. 10-19-07 REMOVED NR 6 SPOILER ACTUATOR PER MM 27-61-02. INSTALLED NR 6 SPOILER ACTUATOR PER MM 27-61-00. OP CHECKS AND LEAK CHECKS GOOD.

Part: AILERON — STICKS · airframe 31,972 hrs · 9,144 cycles

AILERON STICKS WHILE INFLIGHT AND HESITATES WHEN CHECKED ON GROUND AFTER LAG. 10-19-07 REPLACED LEFT LATERAL CONTROL ACTUATOR TORQUE TUBE REF MM 27-11-16. AILERON OPS CHECKS GOOD.

Part: STRUCTURE — SCRATCHED (FUSELAGE) · airframe 30,750 hrs · 8,838 cycles

ALT STATIC PORT, RIGHT SIDE FUSELAGE, JUST FWD OF FWD CARGO DOOR HAS 5 IN LONG SCRATCH THRU WHITE CIRCLE, JUST UNDER STATIC PORT. [08-08-07] DAMAGE DEPTH IS .0021 OK PER 53-00-01 ALSO PER 51-10-03 ITEM F. BURNISHED SCRATCH PER SRM 51-10-02. TOUCHED UP WHITE BORDER PAINT AS NEEDED.

Part: AUTOPILOT SYS — FAILED (COCKPIT) · airframe 30,742 hrs · 8,836 cycles

CENTER & RIGHT AUTOPILOTS FAILED CAUSING A DIVERSION. [07-31-07] RE-ALIGNED RT FCC. STILL HAD PROBLEM. REPLACED LEFT ELEVATOR SERVO VALVE ASSY. RELOADED NAV DATABASE. TESTS OK.

Part: ASPIRATOR — LEAKING (EVAC SLIDE)

ASPIRATOR LEAKING. CAUSE UNKNOWN DUE TO INTERNAL LEAKING. REPLACED ASPIRATOR.

Part: BOTTLE — LOW (EVAC SLIDE) · airframe 27,655 hrs · 8,090 cycles

FOUND LOW BOTTLE PRESSURE. REPLACED SLIDE. AIRCRAFT RETURNED TO SERVICE.

Part: SUPPORT BEAM — CRACKED (LT MLG DOOR) · airframe 27,655 hrs · 8,090 cycles

LT MLG TRUNNION WING DOOR ATTACH SUPPORT BEAM CRACKED. STRUT ASSY FOUND GOUGED & CRACKED. ACCOMPLISHED MAJOR REPAIR PER REO G1 1788. HFEC INSP FOR HIDDEN CRACKING AFTER REPAIR PER NDT 51-00-00-19, PT 6. OK FOR SERVICE.

Part: STIFFENER — CRACKED (BS 246) · airframe 27,655 hrs · 8,090 cycles

CRACKED VERTICAL STIFFENER ON FLOORBEAM BS 246, LBL 40, AFT SIDE. FABRICATED STIFFENER 141T5171-64 PER BACO DWG 141T5171 AND REPLACED PER SRM 53-10-51 AND 51-40-2. SUSPECT FORWARD GALLEY SERVICE EQUIPMENT LOADS.

Part: BEARING — UNSERVICEABLE (TENSION ROD) · airframe 26,398 hrs · 7,794 cycles

FOUND THREE (3) DAMAGED BEARINGS. EXCESSIVE TENSION ON THE TENSION ROD. REPLACED DAMAGED BEARINGS. AIRCRAFT RETURNED TO SERVICE. ROOT CAUSE WAS EXCESSIVE TENSION BUILT IN DURING SLIDE ASSEMBLY.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 26,626 hrs · 7,853 cycles

DIVERTED DUE TO CENTER HYDRAULIC PUMP FAILURE. NR 3 SPOILER ACTUATOR LEAKING HYDRAULIC FLUID. REPLACED NR 3 SPOILER ACTUATOR LAST CHANCE FILTER PLUG O-RING. LEAK CHECKED SPOILER ACTUATORS. LEAK CHECKED OK.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,132 hrs · 7,728 cycles

EEL STRIP INOP AT 1H, 22A AND FROM 14HJ TO MID GALLEY RIGHT LAV. REPLACED EEL STRIP AT SEAT 1H. REPLACED FEEDER CABLE TO EEL STRIP AT SEAT 22A. REATTACHED FEEDER CABLE CONNECTOR AT SEAT 14HJ TO MID-GALLEY-RIGHT LAV EEL STRIP. ALL EEL LIGHTS, OP CHECK OK.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 25,787 hrs · 7,651 cycles

ON APPROACH, WHEN FLAPS WERE SELECTED TO 1, HAD EICAS MSG TE FLAPS DISAGREE DISPLAYED AND TRAILING EDGE LIGHT ILLUMINATED. REPLACED FLAP/STAB POSITION MODULE (FSPM), MR27011, P/N 285T0099-17, MOD A.

Part: SLAT — MALFUNCTIONED · airframe 24,854 hrs · 7,426 cycles

DIVERTED TO HNL DUE TO LEADING EDGE SLAT ASYMMETRY PROBLEM. FAILURE DUE TO A CRACKED 90 DEGREE CONDUIT.

Part: WIRE — BROKEN (SLATS) · airframe 24,854 hrs · 7,426 cycles

DIVERTED DUE TO LEADING EDGE SLAT ASYMMETRY EICAS. FOUND SLAT SKEW SWITCH WIRING FAILED AT RT WING TIP, STA 1107. CAUSE OF WIRING FAILURE WAS BROKEN 90 DEG CONDUIT ELBOW.

Part: STIFFENER — CRACKED (E&E BAY) · airframe 22,300 hrs · 6,806 cycles

E & E BAY, BS 246 FLOORBEAM, STIFFENER FLANGE CRACKED AT RBL 16.38 INCHES. CRACKS ON STATION 246 FLOORBEAM STIFFENERS ARE A KNOWN PROBLEM. THIS CRACKED STIFFENER WAS REPLACED WITH NEW.

Part: FITTING — CRACKED (LT WING SPAR) · airframe 22,300 hrs · 6,806 cycles

LEFT WING REAR SPAR, OUTBOARD FLAP OUTBOARD DEFLECTION FITTING CRACKED. THE SUBJECT FITTING CRACKED TO CYCLICAL FATIGUE LOAD DURING EXTENSION AND RETRACTION OF THE OUTBOARD FLAP. CORRECTIVE ACTION IS REPLACEMENT OF THE FITTING WITH NEW AND IMPROVED FITTING PER COA 616463.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 22,300 hrs · 6,806 cycles

FUSELAGE LEFT SIDE STA 500 PUNCTURED SKIN AT STR 24L. UNDETERMINED CAUSE OF DAMAGE. SKIN REPAIRED PER STANDARD BOEING SRM.

Part: ATTACH ANGLE — CRACKED (TE FLAP HINGE) · airframe 22,300 hrs · 6,806 cycles

RT WING INBOARD FLAP, INBOARD HINGE SUPPORT ATTACH ANGLE CRACKED OUTBOARD SIDE. THE SUBJECT HINGE SUPPORT FITTING CRACKED DUE TO FATIGUE LOAD. THE CRACKED AREA WAS REPAIRED PER 767-300 SRM 57-53-02.

Part: STIFFENER — CRACKED (E&E BAY) · airframe 22,300 hrs · 6,806 cycles

E+E COMPT, BS 246 FLOORBEAM VERTICAL STIFFENER FLANGE CRACKED RBL 11.53 INCHES. STIFFENERS ON THIS FLOORBEAM ARE KNOWN TO CRACK. DISCREPANCY FOUND ON ROUTINE INSPECTION. CRACKED PART WAS REPLACED WITH NEW.

Part: LATCH — FAILED (CABIN)

RT O/W DOOR LATCH INTEGRATOR FAILS TORQUE CHECK. REPLACE LATCHES IAW 767, MM-25-65-98.

Part: LATCH — FAILED (CABIN)

LT OVERWING SLIDE NR 3 DOOR LATCH FAILED INSP CHECK. REPLACE LATCH IAW 767 25-65-98.

Part: ROD — CHAFED (CABIN)

LT OVERWING SLIDE CENTER LATCH ROD ASSEMBLY CHAFFED. REPLACE ROD IAW 767, MM-25-65-98.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 21,385 hrs · 6,587 cycles

AIRCRAFT DAMAGE AT DOOR 4 LEFT AT APPROX STA 1582 BELOW DOOR SILL. PUNCTURE THROUGH SKIN. UNDETERMINED CAUSE OF DAMAGE TO SKIN. REPAIRED PER SRM.

Part: LIGHT — INOPERATIVE (SEAT 36HJ) · airframe 19,747 hrs · 6,178 cycles

EMERGENCY EEL LIGHT AT SEAT 36HJ IS INOPERATIVE. REPLACED SEAT HARNESS.

Part: APU — MALFUNCTIONED · airframe 22,313 hrs · 6,811 cycles

RETURNED TO SFO DUE TO AN AUXILIARY POWER UNIT PROBLEM. P2 SENSOR REPLACED. P2 SENSOR CONFIRMED SHIFTED. SHIFT IN FUEL FLOW SCHEDULE CAUSED APU NO START.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,853 hrs · 5,445 cycles

AFT PIT STA 1439 LT SIDE AT LBL 23, FLOORBEAM IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND FILLER REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 16,853 hrs · 5,445 cycles

AFT PIT STA 1540 LT SIDE FLOORBEAM, STIFFENER IS CRACKED BELOW L-2 DOOR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW STIFFENER.

Part: SKIN — DENTED (CARGO DOOR) · airframe 16,853 hrs · 5,445 cycles

AFT BULK CARGO DOOR SKIN BETWEEN STR 26L AND 27L DOOR SKIN DENTED 3 INCHES FROM EDGE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR DOUBLER.

Part: FIRE DETECTOR — INOPERATIVE (WHEEL WELL) · airframe 10,145 hrs · 3,566 cycles

WHEEL WELL FIRE DETECTION WILL NOT TEST.

Part: CIRCUIT BREAKER — FAILED (BATTERY BUSS) · airframe 7,831 hrs · 2,861 cycles

APPROXIMATELY 200 NM FROM HNL, AIRCRAFT LOST DC STANDBY BUS AND BATTERY BUSS DISTRIBUTION CB ON RIGHT PANEL NEXT TO F/O SEAT. LOST LEFT EEC, YAW DAMPER, REVERSER, TMC, VHF COMM.1, STANDBY ADI. FLAPS INDICATED 1 DEG. CREW RESET TWO CB'S AND MOST OF PROBLEM CORRECTED. EMERGENCY DECLARED. UNEVENTFUL LANDING. SUPPLEMENTAL DATA UPDATE REPLACED DC STBY & BAT DISTR BUS CIRCUIT BREAKERS AS PRECAUTONARY. (C872 & C829 PER WD24-33-11)

Part: SWITCH — INTERMITTENT (BOOST PUMP) · airframe 7,810 hrs · 2,855 cycles

LEFT FORWARD BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED DURING CLIMB. RTF. RTF AGAIN FOR SAME PROBLEM. *S/D* THE PRESSURE LIGHT ILLUMINATION WAS DUE TO FAILURE OF S70 PRESSURE SWITCH. THE SWITCH WAS REPLACED AND OPERATION OF THE LOW PRESSURE INDICATING CIRCUIT HAS BEEN NORMAL.

Part: ROD END BEARING — WORN (ELEVATOR) · airframe 7,254 hrs · 2,675 cycles

GOT SEVERE NOSE STRUT VIBRATION AS SOON AS NOSE WHEEL LOWERED TO RUNWAY. NO NOSE WHEEL STEERING. CAUSE APPEARS TO BE THE LEFT ELEVATOR POWER CONTROL UNIT REACTION LINK ROD END BEARINGS. RADIAL FREEPLAY ON TWO OF THE THREE BEARINGS MEASURED AT .030 AND .012 INCH. ALL THREE LT ELEVATOR ROD ENDS WERE REPLACED.

Part: LINK — DISCONNECTED (NLG) · airframe 7,253 hrs · 2,673 cycles

ON RETRACTING FLAPS, AS THEY PASS FROM POS 1 TO UP: GET CONFIG WARNING ON EICAS, MASTER WARNING AND SIREN, STATUS MSGS. NOSE A-G DISAGREE AND GND PROX BITE DID NOT GET RADIO ALTIMETER CALLOUTS ON LANDING. RTF. NOSE LINK FOUND DISCONNECTED ON LANDING. LINKAGE AND DISCONNECT PINS OPERATION NORMAL. APPEARS PINS WERE INCORRECTLY ENGAGED AT DISPATCH .NOSE GEAR CHECKED PER MM FOR HARD LANDING.

Part: WARNING SYSTEM — ACTIVATED (CARGO DOOR)

FWD CARGO DOOR CAUTION MESSAGE ON EICAS CLIMBING OUT AFTER T/O FROM OGG, ABOUT 11K. FOLLOWED PROC, DIVERTED TO HNL. OVERWEIGHT LANDING. LANDING WEIGHT 316.0.