N666UA

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 91,557 hrs · 19,310 cycles

AISLE EMERGENCY PATH MARKING LIGHTS AT 34 D AND 32 F FOUND DAMAGED AND REQUIRE REPLACING. LIGHT STILL OPS AISLE EMERGENCY PATH MARKING LIGHT AT 32F REMOVED & REPLACED IAW AMM TASK 33-51-10-962-105, OP CHECK OKAY. AISLE EMERGENCY PATH MARKING LIGHT AT 34D. REMOVED & REPLACED IAW AMM TASK 33-51-10-962-105, OPS CHECK OKAY.

Part: SYMBOL GENERATOR — FAULTED (ZONE 100) · airframe 91,046 hrs · 19,244 cycles

SG FAIL ON FO SIDE ADI AND HSI IN FLIGHT REMOVAL AND INSTALL THE EFIS SYMBOL GENERATOR IAW TASK 34-22-01-404-006. SOFTWARE LOAD. ELECTRONIC FLIGHT INSTRUMENT SYSTEM. MAINTENANCE PRACTICES REF 34-22-00/201. REMOVED AND REPLACED RT EFIS SYMBOL GENERATOR IAW AMM 34-22-01-404-006, OPS CHECK OK. NO FURTHER DEFECTS NOTED. SOFTWARE CHECK OK,

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 90,602 hrs · 19,185 cycles

DOOR 2L SLIDE GUAGE OUT RANGE 2L SLIDE CYLINDER. PRESSURE WITHIN RANGE PER AMM 25-66-02-200-001

Part: BOTTLE — NO DISCREPANCY (ZONE 800) · airframe 90,602 hrs · 19,185 cycles

SLIDE RAFT AT 2L INDICATES LOW PRESSURE GAUGE INSPECTED AFTER FLIGHT, CURRENTLY READING AT THE TOP OF THE GREEN BAND, GAUGE TO BE RECHECKED AFTER 2 HOURS OF STABLE TEMPERATURE REF TASK AMM 25-66-99-702-001 BOTTLE PRESSURE RECHECKED AFTER 2 HOURS AT A STABLE TEMPERATURE. PESSURE NEEDLE IS WITHIN ONE NEEDLE WIDTH TO THE RIGHT OF THE GREEN BAND (TOWARDS THE HIGHER END), THEREFORE THE BOTTLE IS STILL PROPERLY CHARGED (GO CONDITION) AS PER AMM 25-66-99-702-001.

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 90,231 hrs · 19,137 cycles

2L SLIDE PRESSURE GAUGE INDICATES LOW PRESSURE UPON INSPECTION FOUND TO BE WITHIN LIMITS REF AMM TASK 25-66-02-206-001, OK TO CONTINUE.

Part: STEERING SYS — FAULTY (NLG) · airframe 87,894 hrs · 18,815 cycles

NOSE WHEEL STEERING SYSTEM AIRPLANE PULLS DURING TAXI AC PULLS L ON TAXI. COMPLETION OF A RIGHT TURN UPPER TORTION LINK RETURNS TO THE NEUTRAL POSITION. ON COMPLETION OF A LEFT TURN UPPER TORTION TENSIONS ON CABLES NWS1A, NWS1B, NWS2A, AND NWS2B ARE IN TOLERANCE PARTS USED:1119186,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1119186 SN OFF 6666 IPC REFERENCE #32-51-04 NLG NWS METERING VALVE MODULE INSTALLATION VERIFIED AMM 32-51-04-404-013. AND TILLER HANDLE STEERING TEST SATISFACTORY. ADJUSTMENT OF NWS STEERING SYSTEM CHECKED AMM 32-51-00-835-001. ALL RIG PINS CONFIRMED REMOVED. NLG STEERING METERING MODULE VALVE REPLACED AS PER AMM VERIFIED IPC 32-51-04-01A. 32-51-04/401. LEAK CHECK CARRIED OUT OK. CHECK OF ADJUSTMENT OF THE NOSE WHEEL STEERING SYSTEM ACTIONED AS PER AMM 32-51-00-835-001.ALL RIG PINS FIT IN RIG PIN HOLES AND VALVE, NLG, STE OFF 76-3252-9-0001 0580 ON 0273 UPON FURTHER INVESTIGATION FOUND STEERING COMPENSATOR WORN REQUIRES REPLACEMENT. REF LP 9293396 FOR COMPENSATOR REPLACEMENT. ALSO FOUND CABLE SYSTEM OUT OF ADJUSTMENT REQUIRES ADJUSTMENT. CARREIED OUT ADJUSTMENT OF NOSE WHEEL STEERING SYSTEM. IAW AMM PARTS USED: 00-0583-3-2585,QTY :1 00-0597-3-0941,QTY :1 32-51-00-835-001.FOUND SATISFACTORY ALL RIG PINS REMOVED. CARRIED OUT SYSTEM TEST OF NOSE WHEEL STEERING SYSTEM. IAW AMM 32-51-00-735-072. FOUND SATISFACTORY ALL RIG PINS REMOVED. VERIFIED SYS TEST & ADJUST OF NOSE WHEEL STEERING SYS IAW AMM 32-51-00

Part: SERVO MOTOR — FAULTED (AUTOTHROTTLES) · airframe 86,631 hrs · 18,649 cycles

AUTOTHROTTLES OCCILATE WITH FLCH VNAV V/S ENGAGED. MOMENTARY A/T DISC LIGHT. CARETS NORM FIM TASK 22-03/803 MCDP GROUND TEST 2 TMC CARRIED OUT, TEST MCDP GROUND TEST 10 - SERVO A/T PERFORMED. TEST SHOWS "TACH L SERVO) PULLED & COLLARED & PLACARDS INSTALLED. REQUESTING AUTOLAND DEGRADED TO LAND 2. MEL 2230C APPLIED, AUTOLAND STATUS - LAND 2. SHOWS "NO INFC TMC - TACH L". FIM TASK 22-05/879 FOLLOWED AND FAIL FWD" & "TACH L FAIL AFT" MESSAGES. CB F16 ON P11 (TMC DEFERRAL OF AUTOTHROTTLE SERVO PER MEL 2230C FOR FURTHER T/S. DISPATCH DESK: 67 NAME: IT DATE: 01-JUN-24- OK TO DEFER AUTOTHROTTLE SERVO

Part: CONTROL PANEL — INOPERATIVE (CABIN LIGHTS) · airframe 86,480 hrs · 18,630 cycles

SPARKS COMING FROM FLT DECK DOOR SWTCH AREA. ADDING PICTURES OF SMOKE IN CABIN FORM. SYSTEM CHECKS GOOD ACCOMPLISHED WINDOW HEAT CONTROLLERS SYSTEM CHECK ALL CHECKS GOOD PER 33-13-00, 33-42-01,33-42-03,33-42-00,33-44-02,33-44-01 ,52-51-13 AND 30-41-01PARTS USED: 1301760,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1301760 SN OFF 1503 IPC REFERENCE # 31-12-11 PHOTOS OF PANEL THAT CREATED SPARKING IN THE COCKPIT FOUND OVERHEAD LIGHT ASSY TO NOSE GEAR SWITCH JAMNUT BACKED OUT PERFORMED VISUAL INSPECTION OF WIRING ON OVERHEAD LANDING LIGHT PERFORMED GVI BEHIND THE FOLLOWING PANELS; WIPER, ANTI-ICE, PERFORMED OPERATION CHECK OF ALL THE SWITCHED ON THE FLIGHT DECK CAUSING SWITCH TO MAKE CONTACT REMOVED AND REPLACED ENTIRE ANTICOLLISION LIGHT ASSY AREA NO FAULTS FOUND WINDOW HEAT, FLIGHT DECK DOOR LOCK, AND ANTI-COLLISION LIGHTS. DOOR PANEL AND THE ADJACENT LIGHT PANEL THAT WAS REPLACED. ALL LIGHT ASSY PERFORMED OPS CHECK OF SYSTEM ALL SYSTEMS CHECK GOOD NO WIRING DEFECTS NOTED IAW SWPM 20-10-06 OPERATIONS ARE NORMAL AND AS ATTED IN THE PREVIOUS UPDAYE THE ALSO ACCOMPLISHED FLIGHT DECK DOOR OVERHEAD PANEL OPS CHECK CAUSE WAS THE LIGHT PANEL. A/C. OK TO CONTINUE VARIFIED PREVIOUS UPDATES A/C OK FOR SERVICE, CAUSE OF SPARKING WAS THE OVERHEAAD LIGHT PANEL THAT WAS REPLACED.

Part: AUTOTHROTTLE SYS — FAULTED · airframe 85,989 hrs · 18,565 cycles

AUTO THROTTLES DISENGAGE ON TAKEOFF WHILE SPOOLING ENGINES JUST BEFORE TAKE-OFF A/T DISENGAGED. CREW LEFT RUNWAY TO T/S BUT GOT A/T AND TMC RE-ENGAGED BUT NOW CREW IS LOW ON FUEL PER DISPATCH AND NEEDS UPLIFT AND OPS CHECK OF THE A/T. PERFORMED MCDP GROUND TEST PER FIM 22-03 FAULT TREE 803. NO FAULTS FOUND.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,476 hrs · 18,359 cycles

ON CLIMB OUT LAV C SPILLED MASS AMOUNT OF WATER INTO THE GALLEY AND INTO PASSENGER AREA INFO UDATE ONLY, SEE PICTURE UNCLOGGED GALLEY DRAIN AROUND THE DRAIN MAST AREA, REMOVED ABOUT 10 INCHES OF COFFEE GROUNDS IN THE DRAIN LINE RIGHT ON TOP OF FWD DRAIN MAST, SEE PICTURE,CLEANED AREA AND BLANKET AS REQUIRED AT FWD DRAIN MAST. ALL LAVS AND GALLEY OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (SEAT 2L) · airframe 84,414 hrs · 18,349 cycles

CABIN ZONE A CTR SEAT SOME FLOOR PROXIMITY EMER LT NOT ILLUMINATE. REF HX WO.2519908 AND ORIGINATED BY V920585. CABIN SEAT 2L O/H EMER LT BATTERY PACK REPLACED & TEST OKAY IAW AMM 33-51-07. WORK ACCOMPLISHED BY V920585 AND INSP BY V897802.

Part: SKIN — CRACKED (R1 DOOR) · airframe 84,414 hrs · 18,349 cycles

SUPPORT TASK - EA 5315-01152 OP 002 RH PASSENGER DOOR 1 AFT LOWER CORNER (1EA) FASTENER HOLE FOUND CRACK ON SKIN AND BEAR STRAP LAYER DETAILS REFER RECORD. TRANSFER REFER NON-ROUTINE WO.2416363 ON REPAIR INSTALLED AS PER PART 2 OF LATEST REVISION ECRA CYCLES. REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 3,000 5330-07153 ON OR BEFORE AIRCRAFT REACHES 37,500 TOTAL FLIGHT FLIGHT CYCLES. RH FWD PASSENGER DOOR AFT LOWER CUTOUT SKIN REPAIRED PER ECRA 5330-01753. GENERATING DIP TO ACCOMPLISH INSPECTION REQUIREMENTS PER ECRA 5330-07153: INITIATE A DIP LOGPAGE TO "ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS ON REPAIR INSTALLED ON FUSELAGE SECTION 41 RH FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER AS PER PART 2 OF LATEST REVISION OF EC5330-07153 ON OR BEFORE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTION AT INTERVAL NOT EXCEED 3,000 FLIGHT CYCLES." TOMC APPROVED; QC REVIEWED TOMC APPROVED; QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT UPDATE.

Part: DOUBLER — UNKNOWN (STA 412 TO 434) · airframe 84,414 hrs · 18,349 cycles

SUPPORT TASK - REMOVE FWD CARGO STA 412 TO 434 STR 36L TO 38L EXISTING REPAIR DOUBLER FOR INSPECTION ACCESS.

Part: SKIN — CRACKED (L1 DOOR) · airframe 84,414 hrs · 18,349 cycles

SUPPORT TASK - EA 5315-01152 OP 001 LH PASSENGER DOOR 1 AFT LOWER CORNER (2EA) FASTENER HOLE FOUND CRACK ON SKIN AND BEAR STRAP LAYER DETAILS REFER RECORD. TRANSFER REFER NON-ROUTINE WO.2416366 AND ORIGINATOR V896921 ON REPAIR INSTALLED AS PER PART 2 OF THE LATEST REVISION OF ECRA CYCLES. REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 3,000 5330-07152 ON OR BEFORE AIRCRAFT REACHES 37,500 TOTAL FLIGHT FLIGHT CYCLES LH FWD DOOR CUTOUT AFT LOWER CORNER REPAIRED PER ECRA 5330-07152. GENERATING DIP TO ACCOMPLISH INSPECTION REQUIREMENTS PER ECRA 5330-07152:INITIATE A DIP LOGPAGE TO READ "ACCOMPLISH TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTION REQUIREMENTS ON REPAIR INSTALLED ON FUSELAGE SECTION 41 LH FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER AS PER PART 2 OF LATEST REVISION OF EC5330-07152 ON OR BEFORE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTION AT INTERVAL NOT EXCEED 3,000 FLIGHT CYCLES." TOMC APPROVED; QC REVIEWED TOMC APPROVED; QC REVIEWED INSPECTIONS. AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SHEAR TIE — CORRODED (AFT CARGO COMP) · airframe 84,414 hrs · 18,349 cycles

B767-53-3-7051 AFT CGO COMPT STA 1329 S38L - 39L SHEAR TIE FOUND CORROSION. TRANSFER REFER NON-ROUTINE WO.2458011 AND ORIGINATOR V896921 AFT CGO COMPT STA 1329 S38L-39L SHEAR TIE REPLACED AS PER WORK ACCOMPLISHED BY MECH V920500 AND INSPECTED BY V912779 S.R.M 51-10-02, ATTACH FASTENER INSTALLED AS PER S.R.M 51-40-02 AND REFER BOEING DWG 146T1212 SHEET 1, 146T3240 SHEET 1, ATTACH FORM 44-0008 WORKSHEET ITEM 1-8 ACCOMPLISHED. RII INSPECTED AND OKAY BY HX169509

Part: SHEAR TIE — CORRODED (AFT CARGO COMP) · airframe 84,414 hrs · 18,349 cycles

B767-53-3-7051 AFT CGO COMPT STA 1329 S37L - 38L SHEAR TIE FOUND CORROSION. TRANSFER REFER NON-ROUTINE WO.2457989. AFT CARGO COMPT STA 1329 S37L-38L SHEAR TIE REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER S.R.M 51-40-02 AND REFER BOEING DWG 146T1212 SHEET 1, 146T3240 SHEET 1. ATTACH FORM 44-0008 WORKSHEET ITEM 1 TO 8.

Part: BATTERY — INOPERATIVE (M1552) · airframe 84,373 hrs · 18,344 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - R1 DOOR NEAR TO THE FLOOR EXIT SIGN INOP. PART IS ORDERED M&E :76-3351-3-0031 FLAGGED SDR. EEL POWER SUPPLY BATTERY PACK REPLACED W.R.T AMM 33-51-07-422-012. OPERATIONAL TEST CARRIED OUT. TEST OK.

Part: FITTING — SHEARED (NOSE GEAR) · airframe 83,749 hrs · 18,258 cycles

NOSE GEAR TOW FITTING SHEARED DURING TOWING PLEASE PERFORM CONDITIONAL INSPECTION AMM 05-51-29 AND UPDATE THIS ITEM WITH FINDINGS. NOSEWHEELS REPLACED PRECAUTIONARY IAW AMM 32-45-02/401. CONDITIONAL INSPECTION OF NOSE GEAR CARRIED OUT IAW AMM 05-51-29. PHASE 1 INSPECTION CARRIED OUT AND NO DEFECTS FOUND. OPERATED STEERING TILLER FULLY LEFT AND RIGHT AND OBSERVED NORMAL STEERING ACTION WITH NO DAMAGE OR FLUID LEAKS FOUND.

Part: CONTROL VALVE — FAULTED (STA 785.90) · airframe 83,659 hrs · 18,244 cycles

CENTER PEDESTAL EXTRMLY HOT TO TOUCH. GLARESHIELD TOO HOT TO TOUCH. HOT AIR COMING FR OM UNDER GLARESHIELD. UNABLE TO COOL FLIGHT DECK OBSTRUCTIONS AND OPS NORMAL. REF AMM 21-58-00Z PERFORMED FIM 21-58 FAULT 912, WITH NO INDICATION OF EQUIP COOLING ADVISORY MSG OR STATUS MSG REPORTED BY FLIGHT CREW,ACCOMPLISHED CHECKS OF NOTED ITEMS FOR EQUIPMENT COOLING SYSTEM. AIR INLET AND DISTRIBUTION DUCTS NO DEBRIS OR ADD EMP:U155524, U118140. OBSTRUCTIONS AND OPS NORMAL. REF AMM 21-58-00Z MX PERFORMED ON MULTIPLE LOG PAGES. REF LP 5286702 FOR ECM TEST. OPS CHECK GOOD. REF LP 5286739 WHERE WE PERFORMED EQUIP COOL SYSTEM TEST. R&R OF OVHT SWITCH AND OPS CHECK. LP 5286783 WHERE WE REMOVED ALL DISPLAYS AND INSPECTED FOR DEBRIS AND ADEQUATE AIRFLOW. REF LP 5284077 FOR FAULTED LH PACK TCV FAULTING. TCV R&R & OPS CHECK GOOD. REF LP 5288714 FOR OPS CHECK OF TRIM AIR MODUL ATING VALVE. OPS CHECK GOOD. REF LP 5286466 FOR R&R OF L MCDU. PERFORMED EQUIPMENT COOLIMG MONITOR TEST WITH AND WITHOUT ENGINES RUNNING REF AMM 21-58-37-810-801-C2. NO FAULTS NOTED. TO VERIFY FUNCTION OF OVHT INDICATION. DUE TO NO OPS CHECKS BEING AVAILABLE FOR THE OVHT SWITCH ITSELF, REMOVE AND REPLACE OVHT SWITCH S00041 IAW AMM 21-58-26. INSTALLED NEW OVHT SWITCH S00041 PERFORMED OVERHEAT INDICATION TEST REF AMM 21-58-00-705-122-006. NO FAULTS DETECTED PARTS USED: 64-2158-3-0006,QTY :1. DUE TO DISPLAY INDICATION ISSUES AND OVHT ISSUES PLEASE REMOVE ALL DISPLAYS AND INSPECT SCREENS FOR DEBRIS. ALSO VERIFY ADEQUATE AIRFLOW IS PRESET. REFERENCE AMM 34-22-04 FOR EHSI, 34-22-03 FOR EADI, AND 31-41-01 FOR EICAS. REMOVED ALL SPECIFIED SCREENS AND DISPLAYS, INSPECTED SCREENS. NO DEBRIS FOUND. REF AMM 34-22-04 FOR EHSI, 34-22-03 FOR EADI, AND 31-41-01 FOR EICAS. BITE TEST ON LEFT PACK TEMP CONTROLLER SHOWS LEFT PACK TEMP CONTROL VALVE FAULTING. REPLACED LH PACK TEMP CONTROL VALVE REF 21-51-12. ACCOMPLISHED INSTALLATION & LEAK CHECK OF LH PACK TEMP CONTROL VALVE REF 21-51-12-404-013, NO LEAKS OR OTHER DEFECTS NOTED. PERFORMED OPS CHECK OF THE TRIM AIR MODULATING VALVE IAW AMM 21-61-00-735-033 STEP L. TEST PASSED. WHILE TROUBLESHOOTING TECH'S, "OBSERVED NAV DISPLAY RANDOMLY SHOWING ALIGNMENT. HEADING SWINGS IRRADICALLY. ALSO SEEING GS JUMP UP AND DOWN AT THE SAME TIME. THIS IS OCCUR RING WITH THE IRU ALIGNED AND OFF. TRIED TO ISOLATE CAUSE BY PUL LING BREAKERS ON THE FOLLOWING COMPONENTS: LT CTR RT IRUS, LT AN D RT SIGNAL GENERATORS, LT CTR RT MMRS, LT RT FMC AND LT AND RT EICAS COMPUTERS. REF AMM 34-21-00/201.01 SERVICE TIP." REPLACED LH MCDU PER TECH SUPPORT REQUEST. AMM REF 34-61-02-400-802. PARTS USED: 75-3120-9-0007,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1548527 SN OFF 5505 PANEL, MCDU, FL OFF 75-3120-9-0007 5505 ON 19-3461-9-0006 2557 PANEL, MCDU, FL OFF 75-3120-9-0007 5505 ON 0000 PERFORMED IRU OPS CHECK PER TECH SUPPORT REQ. OPS CHECK GOOD. LH MCDU OPS CHECK GOOD AS WELL IAW AMM 34-61-02-710-802. ORIGINAL SUBMISSION DATE: 7/28/2023

Part: SLIDE — DEPARTED (RT OVERWING) · airframe 83,658 hrs · 18,243 cycles

*THIS IS A SUPPLEMENTAL REPORT TO THE ORIGINAL REPORT, WITH THE SAME CONTROL NUMBER, CIRCULATED ON 07/21/2023* PDA 1 THE AIRCRAFT ARRIVED AT T5 GATE M21 WITH RH OVERWING SLIDE DOOR AND SLIDE PACK MISSING. RH OVERWING SLIDE DOOR IS DIFFICULT TO CLOSE(LP 5217256). REMOVED R/H OFF WING SLIDE COMPARTMENT DOOR REF AMM 25-65-08. PER AVO10998 AND EA 2560-02662D OP 8 REPLACED DOOR LATCH KEEPERS REPLACEMNET DOOR IN ORDER TO COMPLY WITH PART NUMBER CHANGE. KEEPERS STILL REQUIRE SEALANT. BEGAN INSTALLATION OF NEW L/H OFF WING SLIDE DOOR REF AMM 25-65-08. DOOR HAS 1" GAP AT AFT CORNER WHEN FWD CORNER CONTACTS CLOSE STOP UPON CLOSING. AFT OPEN STOP IS STILL DISCONNECTED DUE TO LINKAGE BEING BENT. REMOVED AND REINSTALLED RH OVERWING SLIDE DOOR TO TROUBLESHOOT THE REASON DOOR WASNT CLOSING. REPOSITIONED OUTER DOOR STOP ROD AND REINSTALLED DOOR, REAR EDGE WAS CONTACTING FAIRING STRUCTURE, TRIMMED DOOR EDGES, DOOR FITS IN CUTOUT NOW, AND CONTINUED WITH INSTALL OF RH SLIDE COMPARTMENT DOOR. PERFORMED FIT AND FARE CHECK PER AMM 25-65-08-404-013 STEP 3.C.3. FWD EDGE OF DOOR IS OUT OF LIMITS. PER STEP 3.C.1, MAX LIMIT IS .090. CURRENTLY AT .230 GAP. LOCAL ENGINEERING HAS RECOMMENDED A NEW CONTINUED WITH RH OFF WING SLIDE DOOR INSTALLATION REF TASK 25-65-08-404-013, PARA 3.C.3. FORWARD EDGE OF SLIDE DOOR TO MAINTAIN CORRECT CLEARANCE AFTER INSTALLATION OF NEW FUSELAGE PANEL 196CR ON LOG 5250637 REF AMM TASK 53-52-01-400-806. SEALED EDGES REF. AMM 25-65-08-404-013 UP AND INCLUDING STEP 3C(2). DOOR OPENING CABLES AND INFLATION ACTUATING ROD NEEDS TO BE RECONNECTED. DOOR BE INSTALLED. CONTINUE WITH TASK 25-65-08-404-013 PARA 3.C.4. COMPLETED RII INSPECTION OF RH O/W SLIDE DOOR INSTALL REF AMM 25-65-08-404-013 UP TO STEP 3.C.6, THEN COMPLETED ADJ. OF O/W ESCAPE SYSTEM AMM 25-65-00-825-001 UP TO BUT NOT INCLUDING STEP 2.J. IAW GMM 9-25-05 COMPLETED RII INSPECTION REQUIREMENTS OF RH O/W SLIDE DOOR INSTALLATION AMM 25-65-00-825-001 STEP 2.J IAW GMM 9-25-05 UPDATED TO TAG RII PARTS INFO UPDATE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1616403 SN OFF 1298 CONTINUED THE ADJ OF O/W ESCAPE SYSTEM REF AMM 25-65-00-825-001 UP TO AND INCLUDING STEP J (4) CONTINUED WORKING AMM 25-65-00-825-001 COMPLETED STEP J STARTED RH DOOR INSTALL REF AMM 25-65-08-404-013 UP TO STEP 3.C.6, THEN STARTED ADJUSTMENT OF OFF WING ESCAPE SYSTEM AMM 25-65-00-825-001 UP TO BUT NOT INCLUDING STEP 2.J ADD EMP:U134580 IPC REFERENCE # 25-65-08-01. COMPLETED RII INSPECTION REQUIREMENTS WORKING RH OVERWING SLIDE DOOR REF AMM 25-65-00-825-001, COMPLETED STEP K. , VERIFIED SLIDE PART EFFECTIVITY. IAW GMM 9-25-05 DOOR SLIDE READY TO BE MOUNTED. CONTINUED WORKING RH OVERWING SLIDE DOOR REF AMM 25-65-00-825-001, COMPLETED STEP K. UPDATING TO ADD INSPECTION AND ROTABLE PART INFO PARTS USED: 76-2561-9-0003,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1683401 SN OFF 0138 SLIDE, ASSY, EV OFF 76-2561-9-0003 0138 ON 76-2561-9-0003 0121 ACCOMPLISHED RII INSPECTION OF RH OFFWING SLIDE INSTALLATION PER MM 25-65-01. INSTALLED RH OVERWING SLIDE REF AMM 25-65-01 TO COMPLETION. LP 5207775: REFERENCE AVO10994 STEP 6, RH OVERWING SLIDE INFLATION CYLINDER NEEDS TO BE REPLACED. STARTED TO INSTALL RH OVERWING SLIDE INFLATION CYLINDER REF.AMM 25-65-02-404-010, INSTALLATION COMPLETE THRU STEP 3G(12), CONTINUE FROM STEP 3G(13), NO INSPECTION IDT ITEMS HAVE BEEN ACCOMPLISHED. PARTS USED: 76-2565-9-9002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1778377 SN OFF 8659 CYLINDER, ASSY, OFF 76-2565-9-9002 8659 ON 76-2565-9-9002 5419 FINISHED INSTALLATION OF RH OVERWING SLIDE INFLATION BOTTLE REF AMM 25-65-03. LP 5238584: PER AVO10998 STEP 9, REPLACE THE FWD DOOR OPENING SNUBBER ACTUATOR PER 25-65-11 W/U SHOULD READ PER AMM25-65-10 UPDATE FOR PARTS INFO ROTABLE PARTS CHANGE WAS INDICATED - TT # 1614487 SN OFF 1456 INSTALLED NEW AFT R/H OFFWING DOOR SNUBBER REF TASK 25-65-10-004-001-001. STEPS THROUGH 3,G,3. PROCEED WITH STEPS 4 CORRECTION... FWD SNUBBER CHANGED.IPC REFERENCE # 25-65-61 ACTUATOR, ASSY, OFF 0000 ON 76-2565-9-0002 1462 ACTUATOR, ASSY, OFF 76-2565-9-0002 1456 ON 0000 COMPLETED RII INSPECTION REQUIREMENTS OF R/H OVERWING EXIT ESCAPE SLIDE DOOR, FWD DOOR OPENING ACTUATOR IAW AMM 25-65-10-404-016, AND GMM 9-25-05. R/H OVERWING EXIT ESCAPE SLIDE DOOR, FWD DOOR OPENING ACTUATOR, REINSTALLED AFTER REMOVAL OF SIMULATOR TOOL, REF AMM 25-65-10-404-016-001 UP TO STEP 3(G). STEP H REACTIVATIONTO BE ACCOMPLISHED ON AMM 25-65-00-825-801. OK FOR SERVICE. ORIGINAL SUBMISSION DATE: 07/21/2023

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,681 hrs · 17,839 cycles

EMERGENCY EXIT SIGN AND PROXIMITY LIGHTS INOP AT SEAT ROW 20-23 REMOVED AND REPLACED EMERGENCY BATTERY PACK M1209, PERFORMED OPS CHECK OF THE EMERGENCY EXIT LIGHTS. TEST FOUND NORMAL PER B767 AMM 33-51-07 AND 33-51-00.

Part: FAIRING — MISSING (LT NACELLE) · airframe 80,678 hrs · 17,838 cycles

DURING THE CHECK FOUND PANEL MISSING ON LH ENG 5ÓCLOCK (RHS). INSTALLED PANEL ON L/H 5 OCLOCK ENGINE START POSITON. NO FURTHER ACTION REQUIRED. WORK ACCOMPLISHED.

Part: FUEL CAP — LEAKING (LEFT WING) · airframe 80,428 hrs · 17,804 cycles

CREW REPORTED FUEL LEAKING FROM LEFT WING FUEL CAP ON TOP OF WING. PIC ATTACHED. UPDATE: CREW REPORTED FUEL IMBALANCE 700# LEFT WING LOW.MAINT FILLED LEFT WING AND CONFIRMED FUEL LEAKING FROM OVERWING FILL PORT THRU-FITTING.

Part: DOOR SEAL — DAMAGED (LH OVERWING) · airframe 78,489 hrs · 17,540 cycles

CREW REPORTS THAT THE LEFT OVERWING ESCAPE DOOR MADE LOUD HUMMING/VIBRATION NOISE IN FLIGHT LOCKNG LOG CAPTAIN STATED THAT THERE WAS NO ACTUAL VIBRATION WITH THE SOUND ADDITIONAL INFO - CREW REPORTS THAT THERE WAS NO SQUEAL AT AND THAT IT STARTED IN CRUISE. NO NOISE DURING CLIMB OUT AND THE ANYTIME WHEN THE NOISE WAS PRESENT. SOUND WAS NOT CONSTANT, IT WOULD START AND STOP MOMENTARILY. REPOSITIONED AND SEALED LEADING EDGE SEAL. RECONDITION SEALANT IN ALL GAPS AND JOINTS AN PANEL. UNLOCKED LOG PAGES FOR UPDATES. DURING INSPECTION OF UPPER WING FAIRINGS, FOUND PANEL 191FL FORWARD ATTACH SCREW BOTTOMED OUT AND NOT SECURING PANEL. ALSO LEADING EDGE SEAL ON PANEL 191FL UNSECURE AND OUT OF POSITION. RESECURED FORWARD ATTACH SCREW WITH PROPER LENGTH AND FOUND SMALL LEAK IN LEFT LOWER FORWARD CORNER OF OVERWING ESCAPE DOOR LERT HAND. REPLACED DOOR SEAL PER AMM 25-65-00. INSPECTED INSTALLATION OF L/H OVERWING ESCAPE DOOR. REFERENCE AMM 25-65-00 AND GMM 09-25-05.

Part: SKIN — CRACKED (STR L 6.5) · airframe 76,869 hrs · 17,279 cycles

SUPPORT TASK - EA5725-01003 OP006 AD2018-13-06 RHW STR L-6.5 BETWEEN RIB31 AND 32 1EA CODE ''A'' HOLE FOUND CRACK , DETAILS REFER ATTACHED FIG. TRANSFER REF NR LP9131134 AND ORIGINATED BY EMP V897399 RII INSPECTED BY HX146606 RHW LOWER SKIN AT STRINGER L-6.5 BETWEEN WSTA990.2 AND 1046.2 FASTENER HOLE CODE ''A'' 1EA AND CODE ''B'' 1EA INTERIM REPAIRED AS PER ECRA 5720-03241 REV - PART 1 WORK ACCOMPLSIHED BY MECHANIC V897490 INSPECTED BY V897008 ADD EMP:V897008 RHW LOWER SKIN AT STRINGER L-6.5 BETWEEN WSTA990.2 AND 1046.2 FASTENER HOLE CODE ''A'' 1EA AND CODE ''B'' 1EA INTERIM REPAIRED AS PER ECRA5720-03241 REV PART 1 WORK ACCOMPLISHED BY MECHANIC V897490 INSPECTED BY V896832 ADD EMP:V896832 RII INSPECTED BY HX146606 ADD EMP:V896834

Part: SPAR — CRACKED (STA 175) · airframe 76,869 hrs · 17,279 cycles

B767-06-3-7110 - NO.2 PYLON STA175 RH UPPER SPAR WEB FOUND CRACKED AT HYD TUBE CUTOUT POSITION TRANSFER REF NR LP9131205 AND ORIGINATED BY EMP V896810 RII INSPECTED BY HX126723 ADD EMP:V896826 NO.2 PYLON NAC STA175 RH UPPER SPAR WEB CASE DRAIN TUBE CUTOUT INTERIM REPAIRED AS PER ECRA 5410-01954 REV - PART 1 WORK ACCOMPLISHED BY MECHANIC V897545 INSPECTED BY V896853 ADD EMP:V896853 NO.2 PYLON NAC STA175 RH UPPER SPAR WEB CASE DRAIN TUBE CUTOUT INTERIM REPAIRED AS PER ECRA5410-01954 REV - PART 1 WORK ACCOMPLISHED BY V897545 INSPECTED BY V896853 ADD EMP:V896853 RII INSPECTED BY HX126723 ADD EMP:V896826

Part: SKIN — CRACKED (STR L-9.5) · airframe 76,869 hrs · 17,279 cycles

SUPPORT TASK EA5725-01008 OP.4 AD2018-13-06 RHW STR L-9.5 BETWEEN RIB 28 AND 29 CODE ''ZVQ'' 1EA HOLE FOUND CRACK TRANSFER REF NR 9131133 AND ORIGINATED BY EMP V897399 RII INSPECTED BY HX169509 ADD EMP:V898550 RHW LOWER SKIN AT STRINGER L-9.5 BETWEEN RIB28 AND 29 1EA CODE ''ZVQ'' FASTENER HOLE INTERIM REPAIRED AS PER ECRA 5720-03242 REV - PART 1 WORK ACCOMPLISHED BY MECHANIC V906016 INSPECTED BY V896888 ADD EMP:V896888 RHW LOWER SKIN AT STRINGER L-9.5 BETWEEN RIB28 AND 29 1EA CODE ''ZVQ'' FASTENER HOLE INTERIM REPAIRED AS PER ECRA 5720-03242 REV PART 1 WORK ACCOMPLISHED BY MECHANIC V897490 INSPECTED BY V896832 ADD EMP:V896832 RII INSPECTED BY HX146606 ADD EMP:V896834

Part: SKIN — CRACKED (STR L - 9.5) · airframe 76,869 hrs · 17,279 cycles

SUPPORT TASK - EA 5725-01008 OP.4 AD 2018-13-06 RHW STR L-9.5 BETWEEN RIB27 & 28 CODE ''A'' HOLE FOUND CRACK , TRANSFER REF NR 9131132 AND ORIGINATED BY EMP V897399 RII INSPECTED BY HX146606 ADD EMP:V896834 RHW LOWER SKIN AT STRINGER L-9.5 BETWEEN RIB27 AND 28 1EA CODE ''A'' FASTENER HOLE INTERIM REPAIRED AS PER ECRA5720-03242 REV - PART 1 WORK ACCOMPLISHED BY MECHANIC V920518 INSPECTED BY V896888 ADD EMP:V896888 RHW LOWER SKIN AT STRINGER L-9.5 BETWEEN RIB27 AND 28 1EA CODE ''A'' FASTENER HOLE INTERIM REPAIRED AS PER ECRA5720-03242 REV - PART 1 WORK ACCOMPLISHED BY V897490 INSPECTED BY V896832 ADD EMP:V896832 RII INSPECTED BY 146606 ADD EMP:V896834

Part: SPAR — CRACKED (STA185) · airframe 76,869 hrs · 17,279 cycles

B767-54-3-7013 - NO.2 PYLON STA185 UPPER SPAR WEB FOUND CRACKED AT LH ELECT BUNDLE CUTOUT POSITION TRANSFER REF NR 9130920 AND ORIGINATED BY EMP V896810 NO.1 PYLON NAC STA185 UPPER SPAR WEB LH ELECT BUNDLE CUTOUT PERMANENT REPAIRED (CAT A) AS PER SRM54-53-02-2R-2 REPAIR 2 FIG.201 DETAIL IV WORK ACCOMPLISHED BY MECHANIC V912857 INSPECTED BY V898550 ADD EMP:V898550 RII INSPECTED BY HX135550 ADD EMP:V917657

Part: BEAM — NONE (STA346) · airframe 76,869 hrs · 17,279 cycles

B767-53-3-7062 - CABIN RBL 30-48 STA346 FLOOR SUPPORT FOUND CORRODED AS MARK TRANSFER REF NR LP9131563 AND ORIGINATED BY EMP V926653 CABIN STA346 BTW BL0"-RBL90" FLOOR BEAM UPPER FLANGE PERMANENT REPAIRED (CAT A) AS PER SRM53-00-51-2R-1 REPAIR 1 FIG.201 WORK ACCOMPLISHED BY MECHANIC V920537 INSPECTED BY V896919 ADD EMP:V896919 RII INSPECTED BY HX202044 ADD EMP:V898556

Part: NONE — NONE (STA185) · airframe 76,869 hrs · 17,279 cycles

B767-54-3-7024 - NO.1 PYLON STA185 UPPER SPAR WEB FOUND CRACKED AT LH ELECT BUNDLE CUTOUT POSITION TRANSFER REF NR LP9130922 AND ORIGINATED BY EMP V896810 RII INSPECTED BY HX126723 ADD EMP:V896826 NO.1 PYLON NAC STA185 UPPER SPAR WEB LH ELECT BUNDLE NO.1 PYLON NAC STA185 UPPER SPAR WEB REPAIR IS MAJOR CUTOUT PERMANENT REPAIRED (CAT A) AS PER SRM54-53-02-2R-2 REPAIR REPAIR 2 FIG.201 WORK ACCOMPLISHED BY MECHANIC V897545 ADD EMP:V896853 INSPECTED BY V896853 ADD EMP:V896853 NO.1 PYLON NAC STA185 UPPER SPAR WEB LH ELECT BUNDLE CUTOUT PERMANENT REPAIRED (CAT A) AS PER SRM54-53-02-2R-2 REPAIR 2 FIG.201 WORK ACCOMPLISHED BY MECHANIC V897545 INSPECTED BY V896853 ADD EMP:V896853 RII INSPECTED BY HX126723

Part: BEAM — NONE (STA303LBL27) · airframe 76,869 hrs · 17,279 cycles

B767-53-3-7069, CABIN STA303 FLOOR BEAM LBL27 FOUND CORRODED TRANSFER REF. NR LP 9131455 AND ORIGINATED BY EMP V917689 CABIN STA303 BTW LBL2"-LBL66" FLOOR BEAM UPPER FLANGE PERMANENT REPAIRED (CAT A) AS PER SRM53-00-51-2R-1 REPAIR 1 FIG.201 WORK ACCOMPLISHED BY MECHANIC V926514 INSPECTED BY V896919 ADD EMP:V896919 RII INSPECTED BY HX203084 ADD EMP:V896920

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,850 hrs · 17,275 cycles

REPLACE EMERGENCY BATTERY PACK LOCATION ROW 44BA. BATT. DID NOT HOLD CHARGE REMOVED AND REPLACED EMERGENCY BATTERY PACK LOCATED ROW 44BA REF. B767-322 AMM 33-51-07 REV 133

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 75,988 hrs · 17,156 cycles

GENERATING ITEM: 63-3350-1-9300 /// JOB CARD 63-3350-1-9300 DURING OPS CHECK OF EMER LIGHTS, 5TH FROM THE FRONT ON R/H SIDE OF CABIN CEILING FAILED TO OPERATE. REF AMES NR 0637, WHILE T/SING W/REF TO B767 WDM 33-51-12, FOUND A FUSE BLOWN ON POWER SUPPLY M732. REMOVED AND REPLACED FUSE PER B767 33-51-07. OPS CHECK OF EMERGENCY LIGHT SYSTEM GOOD PER B767 AMM 33-51-00

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,988 hrs · 17,156 cycles

FUSELAGE SKIN 1/2" CRACK F/S 1654 AT LWR SHEAR TIE FASTENER ABOVE STR 8R. REPAIRED FUSELAGE SKIN CRACK AT F/S 1654 AT LOWER SHEAR TIE FASTENER ABOVE STR 8R IAW B767 SRM 53-80-01 REPAIR 4 ADD RII INSP ACCOMPLISHED

Part: SHEAR TIE — CRACKED (BS 1702) · airframe 75,988 hrs · 17,156 cycles

SUPPORT TASK: SHEAR TIE CRACKED BETWEEN S5-6R F.S. 1702. FOUND W HILE WORKING SKIN REPAIR ON NR-0082. REMOVED AND REPLACED SHEAR TIE AT STA 1702 S-5R-S6R IAW B767 SRM 51-40-02 PARA 7. ADD EMP:V929435

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,988 hrs · 17,156 cycles

FUSELAGE SKIN 1" CRACK F/S 17036 AT LWR SHEAR TIE FASTENER ABOVE STR 6R. REF AMES N-R 0082. REMOVED DAMAGE FROM F-S 1703. FABRICATED REPA IR PARTS FROM .040" 7075-T6 CLAD CLAD TAG 1114184, AND 7075-T6 . 080" BARE TAG 2442829, INSTALLED REPAIR PARTS IAW B767-300 SRM 5 3-80-01 REPAIR 4. ADD EMP:V929433

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 74,292 hrs · 16,912 cycles

AFT RIGHT HAND FLOOR LEVEL EMERGENCY EXIT LIGHT INOP. LENS DETACHED LIGHT INOP, EXIT CONSIDERED INOP,

Part: FLOOR SUPPORT — UNKNOWN (BS 784-846) · airframe 73,352 hrs · 16,775 cycles

REF NRC 9130831 & EA 2500-07893 OP.01 - BL20 SEAT TRACK REWORK STA 784-846 FLOOR BEAM RLB11 FLOOR BEAM REPAIR PER SRM 53-00-31 REPAIR 3 CABIN STA 784-836 RBL11 FLOOR BEAM REPAIRED PER ECRA2500-08244A. FLOURESCENT PENETRANT INSPECTION CARRIED OUT PER BOEING SOPM 20- 20-02 TY1 LV3, NO CRACK FOUND. CABIN STA 784-836 RBL11 FLOOR BEAM REPAIR RII INSP APPROVED BY HX203141

Part: STRAP — CRACKED (BS 1725) · airframe 73,352 hrs · 16,775 cycles

BS 1725 STR 7R BULKHEAD OUTER CHORD STRAP HAS CRACKED FASTENER H OLE. REQUIRES DIP AFTER REPAIR. REF ECRA 5300-02348. DURING C-12 HEAVY CHECK IN MACON REPAIRED BULKHEAD OUTER CHORD S TRAP AT BS STA 1725 STR 7R IAW ECRA 5300-02348. REQUIRES RE-INSP ECT PER ECRA 5300-02348. ACCOMPLISH INITIAL INSPECTIONS PER ECRA 5300-02348 PART 2 ON OR BEFORE ACFT REACHES 37,500 TOTAL AIRFRAME CYCLES. PERFORM REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 6000 FLIGHT CYCLES THEREAFTER. TOMC-APPROVAL FROM SC1ELBYC COMMENT EPAIRED INSPECTED BY HAECO, MCN QC.71 QC REVIEWED ACCOMPLISH INITIAL INSPECTIONS PER ECRA 5300-02348 PART 2 ON OR BEFORE ACFT REACHES 37,500 TOTAL AIRFRAME CYCLES. PERFORM REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 6000 FLIGHT CYCLES THEREAFTER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,352 hrs · 16,775 cycles

AFT CARGO COMPARTMENT FUSELAGE SKIN HAS CORROSION LOCATED BETWEEN BS 1197 +110- BS 1197 + 132 STR 37R.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 70,555 hrs · 16,413 cycles

LT WING INBD TRAILING EDGE AFT FLAP UPPER SKIN HAS ONE ELONGATED HOLE. REPAIRED IAW ECRA 5750-05051, REV.

Part: LATCH — OUT OF TOLERANCE (OVERWING EXIT) · airframe 69,447 hrs · 16,261 cycles

RT OFF-WING ESCAPE SLIDE COMPARTMENT DOOR LATCHES REQUIRED MORE THAN 175 INCH POUNDS WHEN TESTED ON STEP 5 OF EA 2560-02662 OP2. OP4 OF EA 2560-0266 MUST BE ACCOMPLISHED TO REPLACE THE LATCHES. REPLACED 4 EA LATCHES PER EA2560-2662 OPS 4.

Part: ARMING LEVER — LOOSE (R2 DOOR) · airframe 69,334 hrs · 16,247 cycles

EXIT 2R EMERGENCY ARMING HANDLE LOOSE. OPERATED R2 DOOR INSIDE AND OUTSIDE OF A/C NO FAULTS NOTED. OK TO CONTINUE.

Part: REFLECTOR — DEFECTIVE (CABIN) · airframe 68,058 hrs · 16,068 cycles

R2 DOOR EMERGENCY SLIDE LIGHT INOP. REPLACED LIGHT ASSY REFLECTOR. OPS CKS GOOD.

Part: ENGINE — SURGES (NR 2) · airframe 68,058 hrs · 16,068 cycles

RT ENGINE SHUT DOWN IN FLIGHT DUE TO ENGINE VALVE EICAS AND ENGINE SURGE. CREW REPORTS ENGINE WINDMILLED FOR APPROX 7-10 MINUTES WITH POS ITIVE OIL PRESSURE. REPLACED THE NR 2 ENGINE IAW AMM 71-00-02.

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 67,950 hrs · 16,054 cycles

EMERGENCY EXIT SIGN ABOVE EXIT THE R2 DOOR IS LOOSE. SECURED THE SIGN. CHECKED GOOD IAW AMM 33-51-03.

Part: ACTUATOR — TRIPPED (TE FLAP) · airframe 66,250 hrs · 15,820 cycles

TE FLAPS DISAGREE EICAS LANDED FLAPS 20. EMERGENCY DECLARED. FSEU READ OUT SHOWS TE FLAPS SEE FIM MAINT MST 27-51104. TE DISAGREE INRMTNT INACTIVE. FIM 27-51 FT 810 APPLIED. NO TE FLAP DISAGREE MSG ON ARRIVAL. ROTARY ACTUATOR 1 AND 8 P/N 256T3250-4 FOUND INSTALLED. OVERLOAD TRIP INDICATOR ON ACTUATOR NO 2 AND 6 FOUND TRIPPED. RESETTED TRIP INDICATORS. FIM BLOCK 45 RECOMMENDS TO MONITOR THE TE FLAP ROTARY ACTUATORS DURING FUTURE FLIGHT LEGS. MCC INFORMED. SYSTEM OK FOR FLIGHT.

Part: SENSOR — FAULTY (LE SLAT) · airframe 65,829 hrs · 15,762 cycles

LE/SLAT DISAGREE AFTER TAKEOFF. EMERGENCY DECLARED. PSEU BITE INDICATED INITIALLY SENSOR S302 SLAT 10 FAR. LATER TESTS OK.AS PRECAUTION REPLACED SENSOR S302 PER AMM 27-88-01. CYCLED FLAPS/SLATS THROUGH FULL RANGE OF TRAVEL, SEVERAL TIMES ALL INDICATIONS NORMAL AND NO DISCREPANCIES OBSERVED DURING SURFACE MOVEMENTS. PSEU SYSTEM TEST ALSO OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 65,702 hrs · 15,747 cycles

TE FLAP DISAGREE DID QRH AND LANDED. FIM PROCEDURE 27 90 30 PERFORMED RELATIVE TO TE FLAP DISAGREE. FSEU BITE TEST PERFORMED IAW AMM 27 51 00 735. NO FAULT FOUND, FLAPS OPERATIONAL CHECK PERFORMED THREE TIMES SATISFACTORY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,807 hrs · 14,749 cycles

EMERGENCY ESCAPE LT & RT GREEN TEST LIGHTS ON P 61 PANEL FAILED TO TEST. R & R BOTH LT & RT OFF WING ESCAPE SYS EMER BATTERY PACKS IAW AMM 25-65-17. OPERATIONS CHECKED GOOD.

Part: SEALANT — MISINSTALLED (FUEL SYSTEM) · airframe 56,778 hrs · 14,485 cycles

AIRCRAFT FAILED FCD 2841-01075 STEP 5. SEALANT ON GND STUD ASSEMBLY NOT APPLIED CORRECTLY IAW FIG 1, CIRCLE 7, SEE PG 6 & 7 OF FCD. APPLIED SEALANT TO GND STUDS IAW FCD 2841-01075.

Part: HYDRAULIC LINE — DAMAGED (HYDRAULIC SYS) · airframe 56,764 hrs · 14,482 cycles

CREW REPORT HYD QTY C EICAS MSG. CTR HYD READING .31 NOW & FALLING. SECURED ALL CTR PUMPS OFF BEFORE ANY LOW PRESS LIGHTS ILLUMINATED. REPLACED HOSE ON RT STAB TRIM MODULE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 56,678 hrs · 14,471 cycles

LEFT OTBD ELEVATOR SN 000739 LOWER SKIN REPAIRED. LOWER SKIN REPAIRED IAW ECRA 5520-01448 & UAL SPEC SM 60-55-20-02-JD REF 8130-3 TRACKING NUMBER 016-A00561331. STATIC BALANCE PERFORMED & BALANCE MOMENT OF +2722.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 56,009 hrs · 14,389 cycles

CABIN ALT AUTO 2 STATUS MSG ON DESCENT.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 55,845 hrs · 14,369 cycles

MOTORING RT ENG CAUSED LT SYS PRESS TO DROP TO 20 PSI, LT ELEC DEMAND PUMP SHEDS OK FOR SERVICE IAW AMM 29 -11-00 PAGE 1 ITEM 2 B ON GROUND. THE LT SYS ACMP IS INHIBITED DURING STARTING OF EITHER ENG TO REDUCE ELEC LOADS ON THE APU GENERATOR.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 55,503 hrs · 14,328 cycles

RT AUXILIARY PITOT WARNING LIGHT ON & EICAS MESSAGE.

Part: INLET BULLET — DAMAGED (NR 2 ENGINE) · airframe 54,620 hrs · 14,206 cycles

NR 2 ENG REAR SEGMENT OF INLET CONE FAILED INSPECTION. HAS NUMEROUS CRACKS & PEELING OF FIBERS. FAILED INSPECTION IAW MM 72-31-01 STEP 2E 2CB NOTE AREA & STEP 2 A, PEELING OF FIBERS. R & R REAR CONE.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 54,620 hrs · 14,206 cycles

EMERGENCY LIGHTS INOPERATIVE ROWS 30 DEF THRU 32 DEF. BAD SEAT CABLE AT ROW 29 DEF. REPLACED HARNESS AT ROW 29 DEF, OPERATIONS CHECKED GOOD.

Part: CAP — DEFECTIVE (COCKPIT) · airframe 54,597 hrs · 14,202 cycles

ON PREFLIGHT NOSE GEAR LIGHT WONT ILLUMINATE OR TEST, IF PRESSED LIGHT WILL COME ON. R & R NOSE GEAR LIGHT CAP ASSEMBLY. CHECKED GOOD IAW AMM.

Part: PAINT — CHIPPED (RADOME) · airframe 54,593 hrs · 14,201 cycles

RADOME LARGE PAINT CHIP MISSING POSSIBLE LIGHTENING DAMAGE. PERFORMED INTERIM REPAIR ON NOSE RADOME IAW ECRA 5350-02074 REV A. NO DAMAGE NOTED. APPLIED TAPE TAP2505-5-0300. PERFORMED TAP TEST, NO DEFECT NOTED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 53,858 hrs · 14,108 cycles

FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY AND SECURED TO STOWAGE HOLDER.

Part: IDG — FAULTY (LT ENGINE) · airframe 53,826 hrs · 14,104 cycles

LT GENERATOR RELAY DID NOT CLOSE AFTER ENGINE START. REMOVED & REPLACED LT ENGINE INTEGRATED DRIVE GENERATOR PER MM, OPS CHECKED NORMAL.

Part: OXYGEN BOTTLE — DEPLETED (CABIN) · airframe 53,805 hrs · 14,102 cycles

INFANT PORTABLE OXYGEN BOTTLE AT 903 DEPLETED. SERVICED O2 BOTTLE LOCATED AT POS 903. ALL OPS OK.

Part: SENSE LINE — LOOSE (RT ENG) · airframe 53,664 hrs · 14,085 cycles

RT ENGINE PRV EICAS APPEARED EARLY IN TAKEOFF ROLL. FOUND PRIORITY VALVE TO PRIORITY VALVE CONTROLLER SENSE LINE LOOSE. TIGHTENED SENSE LINE.

Part: SHUTOFF VALVE — FAILED (FUEL CELL) · airframe 53,215 hrs · 14,030 cycles

FUELER ADVISES CENTER FUELING VALVE NOT CLOSED. R & R LT AUX TANK FUEL SHUTOFF VALVE. ALL OPS NORMAL AT THIS TIME. NO LEAKS NOTED.

Part: RELAY — FAILED (FUEL OVERFIL) · airframe 53,183 hrs · 14,026 cycles

ACFT WILL NOT TAKE FUEL. REPLACED RELAYS 181, 180, 186, 186, 46, 45, 184, 183. OPENED FUELING VALVES BY HAND TO PUT FUEL ON. NOW THE 6 FUELING VALVES WILL NOT OPEN. REPLACED RELAY K180. OPS CHECKED NORMAL.

Part: FUEL/OIL COOLER — LOCKED (NR 2 ENGINE) · airframe 53,183 hrs · 14,026 cycles

NR 2 ENGINE GEARBOX OIL CONTAMINATED WITH FUEL. REMOVED & REPLACED FUEL-OIL COOLER IAW AMM 79-21-01.

Part: ACTUATOR — LEAKING (NR 11 SPOILER) · airframe 53,154 hrs · 14,023 cycles

SPOILER NR 11, SMALL HYD LEAK ON EXTENSION CHECK AND THERMAL RELIEF VALVE, 2 DROPS. REMOVED AND REPLACED NR 11 SPOILER ACTUATOR PER AMM, OPS AND LEAK CHECKED GOOD,

Part: DUCT — LOOSE (GASPER) · airframe 53,093 hrs · 14,015 cycles

LOUD AIR NOISE AT ROW 32 OVER MIDDLE SEATS. FOUND OFF TAKE FROM GASPER DUCT ABOVE ROW 32 DEF LOOSE. INTERIM REPAIR CARRIED OUT. OFF TAKE SECURED WITH TIE WRAPS OK.

Part: SEAT TRACK — CORRODED (BS 1042-1043) · airframe 52,125 hrs · 13,887 cycles

SEAT TRACK CORRODED FOUND AT BS 1042-1043 LBL 88. REPLACED SEAT TRACK SECTION FROM BS 1031 TO 1098 PER SRM 53-00-52 REPAIR 3 FIG 201.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,041 hrs · 13,862 cycles

ACCOMPLISH EMERGENCY LIGHT OPERATIONAL CHECK PER MM AND REPORT INOPERATIVE LIGHTS TO TOMC. ACCOMPLISHED TEST, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOP ON RT SIDE FOR SEAT ROWS 20-25. REPLACED POWER SUPPLY M1554. ACCOMPLISHED EMERGENCY LIGHT OPERATIONAL TEST, OPS CHKS GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 52,036 hrs · 13,860 cycles

REF 'A' CHECK JOB CARD 6-2006-A STEP 2 B 3 A, FLIGHT DECK (OVER DOOR) EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WITH P5 SWITCH IN ON POSITION. REPLACED THE LIGHT ASSEMBLY, SYSTEM CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,036 hrs · 13,860 cycles

REF 'A' CHECK JOB CARD 6-2006-A, STEP 2 B 2 A, DOOR CAVITY EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE AT DOOR 2R. (LIGHT ASSY L309). RELAMPED, CHECKS NORMAL.

Part: WIRE — OPEN (APU) · airframe 51,987 hrs · 13,847 cycles

APU FAULT-BITE EICAS MSG. ACP WIRING CHECKS FOUND OPEN WIRE FROM APU FIREWALL CONN D4024P POS 5 TO THE DE-OILER SOL CON P11 POS 1 WITH DIODE FORWARD AND REVERSED BIASED. CREATED NEW SMC.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 51,966 hrs · 13,841 cycles

APU INOP FAULTED TWICE. PERFORMED VISUAL INSPECTION ON APU COMPARTMENT, CHECKED APU OIL LEVEL FOUND OVERSERVICED DRAINED TO PROPER LEVEL. STARTED APU. OPS CHECK NORMAL. OK TO CONTINUE.

Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 51,860 hrs · 13,808 cycles

FORWARD CARGO DOOR, LOWER AFT DEPRESSOR SEAL IS DAMAGED. REPLACED SEAL DEPRESS P/N 143T8542Y4 REF AMM FOR REMOVAL AND REPLACEMENT.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 51,848 hrs · 13,806 cycles

APU FAILED AFTER EXTERNAL POWER REMOVED, RESTARTED OKAY. REPEAT WRITEUP. RESTARTED APU, NO PROBLEMS AT THIS TIME. NO HISTORY.

Part: LIGHT — UNSECURE (CABIN) · airframe 51,748 hrs · 13,778 cycles

ROW 3B STRIP LIGHT FELL OFF. SECURED STRIP ON SEAT 3B.

Part: FAN — FAULTY (CARGO BAY) · airframe 51,733 hrs · 13,775 cycles

GRINDING NOISE IN CABIN, RTFL. REPLACED BULK CARGO VENTILATION FAN, OPS CHECKED GOOD. PART AVAILABLE. VALVE WAS SHIPPED FROM DENVER.

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 51,586 hrs · 13,742 cycles

AUTOLAND AP PUMPED THE YOKE WHEN FLARE MODE ENGAGED. MCDP TEST 40 SHOW TLA R FAIL. REPLACE TMC. OP CHECK GOOD CAT 3 CHECK REF AMM. AC RETURNED TO CAT 3.

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 51,527 hrs · 13,729 cycles

CREW REPORTED RUDDER RATIO LIGHT AND EICAS MESSAGE. TROUBLESHOT IAW FIM TASK 27-21-00 FIG 104. REPLACED LEFT ELECTRICAL HYD PUMP CONTROL PRESSURE SWITCH S27 IAW AMM. 'HYD SWITCH' FAULT CLEARED ON RIGHT YAW DAMP MODULE. 'RUDDER RATIO' LIGHT AND EICAS MESSAGE CLEARED.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 51,430 hrs · 13,706 cycles

EICAS WINDSHEAR SYSTEM INOPERATIVE. REPLACED AND OP CHECKED WXR TRANSCEIVER PER MM. TEST GOOD. CONFIRM CORRECT TRANSCEIVER PER ON-LINE IPC.

Part: TRANSCEIVER — INOPERATIVE (WEATHER RADAR) · airframe 51,430 hrs · 13,706 cycles

EICAS WINDSHEAR SYSTEM INOP. REPLACED AND OP CHECKED WXR TRANSCEIVER PER MM. TEST GOOD. CONFIRM CORRECT TRANSCEIVER PER ON-LINE IPC.

Part: BONDING STRAP — BROKEN (EXT POWER DOOR) · airframe 51,283 hrs · 13,667 cycles

BROKEN WIRE ON EXTERNAL POWER DOOR THAT ATTACHES DOOR TO AIRCRAFT. INSTALLED SERVICEABLE JUMPER STRAP PER SWP.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 51,271 hrs · 13,665 cycles

LCL MAINT REPORTS: APU AUTO SHUT-DOWN TWICE. AFTER 1ST SHUT-DOWN RESTARTED AND OPERATED FOR APPROX 10 MINUTES, THEN AUTO SHUT-DOWN AGAIN. BITE TEST APU CONTROLLER, OIL PRESSURE FAULT, APU OVERSERVICED, DRAINED TO PROPER LEVEL APU OK FOR SERVICE.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 51,147 hrs · 13,633 cycles

BOTH LT & RT FMC'S INOP, RTFL ASSOCIATED AUTO-PILOT CAUTION LIGHT. SEE AMIS HISTORY FOR INBOARD CREW DEBRIEF. NOTE ON ARRIVAL, MCDP BITE SHOWED A-P CTR MODE ERROR, CODES 112480, 122480, 132480. REPLACED CENTER FCC. ACP'D RELOAD OF FMS NAV DATABASE UA41209001, ACP'D FMCS OPERATIONAL TEST MM. TESTS OKAY. ACP 'D CAT III TEST. TESTS OK. ACFT STATUS CAT III.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 51,081 hrs · 13,617 cycles

FIRST OFFICER'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS. INSPECTED WINDOW AND FOUND DELAMINATION ALONG THE EDGE OF WINDOW. NO CRACKING NOT ICED. DELAMINATION APPX 5.5 IN WIDE AND .75 IN HIGH. COMPLETED WINDOW INSTALLATION.

Part: RFU — FAULTY (SATCOM) · airframe 51,081 hrs · 13,617 cycles

SATVOICE LOST EICAS MSG ON THROUGHOUT MOST OF THE FLT REPLACED RFU. SUCESSFULLY PASSED INSTALLATION.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 51,030 hrs · 13,606 cycles

EMERGNCY EXIT LIGHT WIRING EXPOSED AT SEAT 1B. REPLACED EMERGENCY LIGHT AT 1B.

Part: ENGINE — FAULTY (NR 1) · airframe 51,001 hrs · 13,600 cycles

LEFT ENGINE FIRE LP2 STATUS MESSAGE DISPLAYED AFTER POWER TRANSFER TO GROUND UNABLE TO CLEAR MESSAGE. REPLACED NR 1 ENG PER MM.

Part: LIGHT — UNSECURE (SEAT 1B) · airframe 50,817 hrs · 13,560 cycles

SEAT 1B EMERGENCY LIGHT IS SEPARATED FROM SEAT. SECURED EMERGENCY LIGHT.

Part: DISPLAY — FAILED (COCKPIT) · airframe 50,759 hrs · 13,547 cycles

HSI CIRCUIT BREAKER TRIPPED AND SMOKE CAME FROM BACK OF CAPTAIN'S INSTRUMENT PANEL. CHECKED WIRING AT P1-1, P1 -3 AND P11 C-B PANEL. CHECKED OK. FOUND CAPTAIN`S EHSI HAD BURNING ODOR. ALSO FOUND CAPTAIN`S AND FIRST OFFICER`S EHSI HAD MR41814 INSTALLED. REPLACED LT AND RT EHSI N5 AND N45 REF MM 34-22-04, 34-22-04 AND 31-11- 11-011, CHECKED OK.

Part: CHECK VALVE — DAMAGED (RECIRCULATION) · airframe 50,759 hrs · 13,547 cycles

FOUND LEFT RECIRCULATION FAN PLENUM ASSY DAMAGED. REPAIRED DAMAGED AREAS PER MM, FOUND 1 PLENUM CHECK VALVE FLAP BROKEN FROM HINGE AREA. REPLACED CHECK VALVE PER IPC 21-25-01-004.

Part: SDU — FAILED (SATCOM) · airframe 50,759 hrs · 13,547 cycles

DATALINK LOST AND SATVOICE LOST. REPLACED SDU, OPS CHECKED GOOD.

Part: FILTER — CONTAMINATED (LT ENGINE OIL) · airframe 49,987 hrs · 13,369 cycles

CREW REPORTED THAT SOON AFTER ENGINE START LEFT ENGINE OIL FILTER STATUS MESSAGE APPEARED MASTER CHIP DETECTOR CHS CLEAN. FOUND MAIN OIL FILTER WITH ABNORMAL AMOUNT OF CARBON, NO METAL. CHANGE FILTER AND RAN ENGINE. CHECKED NORMAL.

Part: PUMP — LACK OF LUBE (FUEL SYSTEM) · airframe 49,719 hrs · 13,310 cycles

FUEL PUMP HAS LACK OF LUBRICATION. PUMP REMOVED AND INSTALLED NEW PUMP. LEAK CHECKED AND RUNS GOOD.

Part: LIGHT — MISSING (SEAT 1AB) · airframe 49,719 hrs · 13,310 cycles

SEAT 1AB AFT EMERGENCY LIGHT MISSING. REPLACE MISSING AFT EMERGENCY LIGHT AT SEAT 1AB. OPS CHECKED GOOD.

Part: WIRE HARNESS — WORN (FIRE WARNING SYS) · airframe 49,719 hrs · 13,310 cycles

FIRE WARNING HARNESS HAS TWO WIRES AT 21:00 POSITION HAS WORN INSULATION UNDER CLAMP. REPLACED HARNESS 585-4978 REF WDM 26-11-21. ACCOMPLISHED FIRE DETECTION TEST PER MM. TEST PASSED.

Part: WARNING LIGHT — FALSE ACTIVATION (LT ENGINE) · airframe 49,659 hrs · 13,295 cycles

APPLYING POWER TOWARDS TAKE OFF, HAD LEFT ENGINE CONTROL EICAS. WENT OUT AFTER REDUCING THRUST. CREW REPORTED EICAS MESSAGE WAS IMMEDIATE AND THROTTLE WAS RETARDED IMMEDIATELY.

Part: SMOKE GOGGLES — DAMAGED · airframe 49,654 hrs · 13,294 cycles

SMOKE GOGGLE STRAP STRETCHED DOES NOT SEAL. REPLACED SMOKE GOGGLES.

Part: LIFE VEST — TORN (FLIGHT DECK) · airframe 49,613 hrs · 13,285 cycles

INFANT LIFE VEST TORN IN FLIGHT DECK. REPLACED LIFE VEST.

Part: ECU — FAULTY (APU) · airframe 49,536 hrs · 13,268 cycles

APU BLEED VALVE DID NOT OPEN LIGHT ON SWITCH DOESN'T SHOW THE DISAGREEMENT. PERFORMED BITE TEST OF APU FOUND ECU REPEATED FAULTS, REPLACED ECU PER AMM. OPS CHECK GOOD.

Part: WIRE HARNESS — CHAFED (NR 1 ENGINE) · airframe 49,525 hrs · 13,266 cycles

WORK WITH LA3260, FOUND EEC ALTERNATOR WIRING HARNESS W3P1 CHAFED, DAMAGE 40 PERCENT, AND INTERMITTANT SHORTED TO NR 1 ENGINE CASE. NEED TO REPLACE W3P1 HARNESS. DOUBLE CHECKED W5P6 EEC ALTERNATOR WIRING HARNESS OKAY. REPLACED EEC HARNESS ASSEMBLY W3 (W3P1). (PCN 585-5200).

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 49,482 hrs · 13,257 cycles

CREW REPORTED ON TAKEOFF ROLL HAD A MOMENTARY HPSOV CAUTION MSG. CREW COULD NOT DETERMINE FROM WHICH SIDE. MAX SPEED WAS BELOW 60 KTS. NO EXCESSIVE BRAKING APPLIED. ACFT RE-LOCATED TO RUN AREA. CREW RAN LT & RT ENG TO 1.20 EPR AND 1.3 EPR 2 CONSECUTIVE TIMES. NO CAUTIONS OR MSGS DISPLAYED. ITEM ENTERED INTO HISTORY. NO FURTHER MAINTENANCE ACTION NEEDED PER OPBLM. (NFF)

Part: SENSE LINE — OBSTRUCTED (LT ENGINE) · airframe 49,496 hrs · 13,260 cycles

L ENG CONTROL STATUS MSG APPEARED AFTER L ENG START. PURGED P2 LINE ON ACCOUNT OF PIMU P2 LINE MSG AND ACCOMPLISHED FIM TASK PER 350-22 EEC CH A-B P2 LINE. CREW PERFORMED ENG RUN AND SYSTEM 'C' OPS CHECKED, NO MSG'S.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 49,454 hrs · 13,251 cycles

APU BLEED WILL NOT OPEN MAINT TEXT: VERIFIED BAR LT AND VLV SWITCH LT ARE NOT ILLUMINATED. DEPARTURE TIME. CLEANED AIR SUPPLY SHUTOFF VALVE CONNECTOR. APU PNEUMATIC OPERATION CHECK NORMAL.

Part: IGNITER — FAILED (NR 1 ENGINE) · airframe 49,328 hrs · 13,224 cycles

CREW REPORT: NR 1 ENGINE NO LIGHT OFF. START OK SECOND ATTEMPT WITH START SWITCH IN BOTH. MEL COMPLIED WITH BY FLIGHT CREW. REPLACED NR 1 IGNITER PLUG. RAN MOTOR OPS NORMAL.

Part: CHILLER — FAULTY (LEFT) · airframe 49,310 hrs · 13,219 cycles

LEFT AFT CHILLER BLOWING WARM AIR. REPLACED CHILLER PER AMM, OPS CHECK NORMAL. UNIT OFF MR25349-1500 UNIT ON MR25349-1472.

Part: SCREEN — DIRTY (RUDDER) · airframe 48,930 hrs · 13,139 cycles

CHRONIC RUDDER RATIO ISSUES. REPLACING RUDDER RATIO SCREEN AND FILTER.

Part: LIGHT — LOOSE (CABIN) · airframe 48,891 hrs · 13,131 cycles

CREW REPORT: EMERGENCY EXIT LIGHT AT SEAT 1H LOOSE. SECURED LOOSE EMERGENCY EXIT LIGHT STRIP. OPS NORMAL.

Part: CONVERTER — FAULTY (COCKPIT) · airframe 48,879 hrs · 13,128 cycles

F/O WIPER CONTINUES FOR SEVERAL SECONDS AFTER USE AND PULSES INTERMITTENTLY THROUGHOUT FLIGHT. REPLACED WINDSHIELD WIPER CONVERTER PER MM.

Part: ACTUATOR — FAULTY (RUDDER) · airframe 48,830 hrs · 13,116 cycles

RUDDER RATIO LIGHT ON. PERFORMED RUDDER RATIO CHANGER MODULE TEST PER FIM 27-09-00. PCA FAULT BALL NOTED. REPLACED RUDDER RATIO CHANGER ACTUATOR PER MM, RIGGED PER MM. NO LEAKS NOTED, RIG GOOD.

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 48,810 hrs · 13,112 cycles

RUDDER RATIO EICAS ON WHEN SELECTION OF FLAPS 5 ON APPROACH. LT SYS HYD PRESSURE LIGHT DOES NOT COME ON WITH HYD 'OFF'. SUSPECT SWITCH S27. REF FIM AND FAULT BITE INDICATED LT HYD PRESS SWITCH. REPLACED SWITCH AND NO FAULTS NOTED. REPLACED RUDDER RATIO CHANGER MECHANISM LVDT. REPLACED RRCM LVT PER MM. REPLACED RRCM LVDT. SECURED CONNECTORS ALSO. ALSO REINSTALLED LOWER LT BLUE ROD END BOLT. OPS CHECKED GOOD, NO FAULTS.

Part: OIL SYSTEM — OVERSERVICED (RT ENGINE) · airframe 48,736 hrs · 13,097 cycles

OIL DRIP FROM RIGHT ENGINE. CHECKED FOR VISUAL LEAK, NONE NOTED. OPENED OIL CAP AND FOUND TANK OVERSERVICED. 1 QT OF OIL REMOVED. OIL CAP RESECURED AND COWLS CLOSED & LATCHED. RAN ENGINE FOR LEAK CHECK, NO LEAKS NOTED.

Part: BLADE — DAMAGED (NR 2 COMPRESSOR) · airframe 48,599 hrs · 13,062 cycles

NR 2 ENGINE HAS DAMAGED FAN BLADES. BLENDED NR 7 BLADE PER AMM 72-31-02. ACCOMPLISHED HFEC BLADE NDT PER MM AND NO CRACKS FOUND. ACCOMPLISHED FINAL BLEND BLADE. OK FOR SERVICE.

Part: DOOR — UNSECURE (LT WING ACCESS) · airframe 48,529 hrs · 13,048 cycles

FOUND ON ARRIVAL, LT WING ACCESS PANEL DOOR FOR WING THERMAL ANTI-ICE DUCT FOUND HANGING.

Part: DOOR — DAMAGED (LT WING) · airframe 48,529 hrs · 13,048 cycles

ON WALK AROUND FOUND LEFT LEADING EDGE WING THERMAL ANTI -ICING DUCT SEAL DOOR ASSEMBLY DAMAGED OUTBOARD NR 1 ENGINE. INSTALLED NEW HINGE ASSEMBLIES ON BOTH ENDS OF DOOR ASSY.

Part: LIGHT — BROKEN (CABIN) · airframe 48,509 hrs · 13,044 cycles

SEAT 1B EMERGENCY LIGHT BROKEN. REPLACED LIGHT STRIP.

Part: HOLDER — MISINSTALLED (COCKPIT) · airframe 48,535 hrs · 13,049 cycles

RIGHT VISOR HOLDER ON CAPTAIN SLIDING WINDOW INSTALLED BACKWARDS. VISOR HOLDER INSTALLED CORRECTLY.

Part: HOLDER — MISINSTALLED (COCKPIT) · corrosion level 2 · airframe 48,504 hrs · 13,043 cycles

RIGHT VISOR HOLDER ON CAPTAIN SLIDING WINDOW INSTALLED BACKWARDS. VISOR HOLDER INSTALLED CORRECTLY NEED SLIDER STOP, PCN 160-8969, NIS AT HNL.

Part: MONITOR — FAULTY (CABIN) · airframe 48,295 hrs · 13,001 cycles

REPORTED ELECTRICAL BURNING SMELL COMING FROM MONITOR AT ROW 10. READING LIGHTS INOP. BURNING SMELL COMING FROM MONITOR AT 10AB. INOPED MONITOR. RESET READING LIGHT MASTER SWITCH - READING LIGHTS WORK NORMALLY.

Part: FILTER — POPPED (HYDRAULIC SYS) · airframe 48,276 hrs · 12,997 cycles

NR 1 ENG PYLON HYD SVC BAY, FWD FILTER MODULE CASE DRAIN FILTER'S DPI POPPED. REPLACED LT HYDRAULIC MODULE OIL FILTER.

Part: AMPLIFIER — FAULTY (SATCOM) · airframe 48,104 hrs · 12,960 cycles

SATCOM HI GAIN MSG CANNOT BE ERASED. RESET DID NOT HELP. MESSAGE CAME BACK. SATCOM HIGH. ONLY FAULTS DURING SATCOM VOICE CALL (HGA HPA VSWR FAULT). REPLACED HPA (M1782) FOR HGA. INSTALLATION TEST "OK". MADE CALLS ON BOTH L & R SATCOM.

Part: ACTUATOR — FAILED (CARGO DOOR) · airframe 48,080 hrs · 12,954 cycles

WHEN OPENING FWD CARGO DOOR TO LOAD, SQUEAKY GRINDING NOISE, DOOR ALMOST FULL OPEN. A LOUD POP, THE DOOR SLAMMED CLOSED. NOW DOOR HANGING & SWINGING REPLACED BOTH ROTARY ACTUATORS FOR FWD CARGO DOOR, OPS CHECKED GOOD..

Part: UNKNOWN — ODOR (CABIN) · airframe 47,916 hrs · 12,919 cycles

CREW REPORTED POSSIBLE BURNING ODOR IN THE VICINITY OF ROW 30 THRU 33, TURNED OFF THE OVERHEAD LIGHTS SEEMED TO ALLEVIATE THE PROBLEM. WITH IFE SWITCH OFF, BURNING ODOR STILL PRESENT BUT NOT AS STRONG, WITH GASPER FAN OFF, ODOR WORSE. FOUND BATTERY CHARGER M733 WARMER THAN OTHER CHARGERS. NO BURNED ODOR NOTED. REPLACED AS A PRECAUTION. CHECKED SDU, RF UNIT, APU BATTERY AND CHARGER, ALL OKAY.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 47,666 hrs · 12,865 cycles

FOUND LEFT WINDOW 1 J5 TERMINAL BLOCK LOOSE. REMOVED AND INSTALLED NEW NR 1 LEFT WINDSHIELD IAW AMM.

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 47,478 hrs · 12,823 cycles

OXYGEN MASKS HANGING AT 33HJ. SECURED O2 MASK AT 33HJ.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 47,343 hrs · 12,790 cycles

MIC SELECTOR BUTTONS WILL NOT STAY DOWN AT CAPT'S RADIO PANEL. REPLACED CAPTAINS AUDIO SEL PANEL,TESTED OKAY.

Part: AUDIO PANEL — DEFECTIVE (COCKPIT) · airframe 47,345 hrs · 12,791 cycles

CAPT UNABLE TO TRANSMIT USING ANY MIC SWITCH. REPLACED AUDIO SELECTOR PANEL AND CHECKED GOOD.

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 47,178 hrs · 12,752 cycles

CAPTAIN'S RADIO INOP. CHANNELS BLEED OVER TO FLT PHONE. REPLACED AUDIO SELECT PANEL PER MM. OPS CHECK GOOD.

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 47,167 hrs · 12,750 cycles

ACTIVE HYDRAULIC LEAK FOUND CTR NR 1 ISOLATION VALVE. REPLACED ACMP PRESSURE SHUT-OFF VALVE PER MM.

Part: SWITCH — FAULTY (NR 1 IDG) · airframe 47,047 hrs · 12,724 cycles

DUE TO A PREVIOUS GRIPE OF RT IDG VALVE STATUS MESSAGE, REMOVE CONNECTOR, PULLED RT ENG IDG VALVE CB. REMOVED AND REPLACED NR 1 ENG IDG AIR-OIL HEAT EXCHANGER VALVE OVERRIDE SWITCH PER MM. IDLE RUN FOR 5 MINUTES NO STATUS MESSAGES.

Part: NIPPLE — LEAKING (LT IDG) · airframe 46,958 hrs · 12,707 cycles

L ENG FLUID LEAK. FOUND OIL LEAKING FROM IDG OIL SERVICE NIPPLE. REPLACED NIPPLE, RUN ENG NO LEAKS, SVC IDG TO NORMAL.

Part: SATCOM — FAULTY (NR 1) · airframe 46,792 hrs · 12,671 cycles

SATCOM LOW GAIN STATUS MESSAGE WON'T CLEAR. FOUND LGA HPA BITE FAILED. REPLACED LGA HPA PER MM. AFTER WARM UP WAS THEN FAULTING HGA HPA. REPLACED SDU PER MM. SYSTEM OPS CHECKS NORMAL PER MM.

Part: B-NUT — LOOSE (LT IDG) · airframe 46,787 hrs · 12,670 cycles

L ENG DRIPPING OIL ONE DROP PER 10 SECONDS. FOUND IDG 'B' NUTS LOOSE TIGHTEN LINE AND SERVICED IDG. DRY MOTORED ENG NO ACTIVE LEAK NOTED.

Part: SKIN — DAMAGED (NR 6 SLAT) · airframe 46,561 hrs · 12,621 cycles

LEFT L/E HALF MOON PANEL & SLAT WEDGE PANEL JUST ABOVE ARE DAMAGED WITH HALF MOON PANEL HAVING SECTION MISSING. LEFT NR 6 LEADING EDGE SLAT HAS DAMAGE. ACCOMPLISHED VISUAL INSPECTION OF ADJACENT AREA AND ASSURE NO FURTHER DAMAGE TO SLAT OR WING PANEL. APPLIED 2 LAYERS OF SPEED TAPE TO UNDERWING PANEL WITH 4 INCH OVERLAP TO SECURE. ONE LAYER OF SPEED TAPE TO SLAT WITH 4 INCH EXTENSION BEYOND DAMAGED AREA. ACCOMPLISHED AS STATED ABOVE.

Part: IDG — FAILED (RT GENERATOR) · airframe 46,491 hrs · 12,606 cycles

TAXI IN SHUT DOWN RT ENGINE LEFT GENERATOR TRIP AND BUSS TIE OPEN RESET LT GEN HELD 10SEC TRIP AG. REPLACED LT IDG. LEAK & OPS CHECKED GOOD.

Part: GCU — FAULTY (LT ENGINE) · airframe 46,483 hrs · 12,603 cycles

LEFT GEN TRIPPED OFF START OF TAKEOFF. RAN CHECKLIST AND DID NOT RESET. REPLACED LT ENG GCU. RAN BOTH ENGINES, SYSTEM WORKED NORMAL. REPLACED LT GEN TIE BREAKER. BPCU BITE CHECK HAD LT GEN DP TRIP MAIN BUS-OVERLAP ZONE MSG TWICE. GCU WAS REPLACED ON THE FIRST W-UP.

Part: MODULE — FAULTY (STAB TRIM) · airframe 46,473 hrs · 12,599 cycles

STAB TRIM & LEFT AUTOPILOT EICAS.

Part: PANEL — MISSING (NR 6 SLAT) · airframe 46,414 hrs · 12,584 cycles

NR 6 L/E SLAT LWR TRAILING EDGE FAIRING SECTION MISSING. REPLACED NR 6 L/E SLAT LOWER PANEL.

Part: VALVE — FAULTY (APU) · airframe 46,264 hrs · 12,545 cycles

APU PNEUMATIC AIR WEAK, INDICATES 20 PSI WITH LOAD. SLOW ENGINE STARTS. REPLACED SURGE VALVE IN REF TO MM. GROUND CHECKS GOOD.

Part: CARTRIDGE — FAULTY (APU) · airframe 46,154 hrs · 12,521 cycles

APU AUTO SHUTDOWN WITH APU BTL DISCHARGE LIGHT. REPLACED APU FIRE EXTINGUISHER BOTTLE AND DISCHARGE CARTRIDGE PER MM. UNIT CHECKS OKAY AT THIS TIME.

Part: SELECTOR PANEL — DEFECTIVE (COCKPIT) · airframe 46,144 hrs · 12,518 cycles

CAPTAIN'S AUDIO SELECTOR PANEL INTEGRATED LIGHTING INOP. REPLACED PANEL, OPS OKAY. 2 SEGMENTS LATER THE NR 1 COCKPIT SPKR IS DEFECTIVE. (O1=CAPT, O2=1ST OFF). CREW COMMENTS: SPEAKER HAS RANDOM STATIC. REPLACED CAPTAIN'S AUDIO SELECTOR PANEL (PRECAUTIONARY) AND OPS OKAY.

Part: AUDIO PANEL — FAULTY (POSIT 1) · airframe 46,105 hrs · 12,509 cycles

CAPT'S AUDIO PANEL UNABLE TO HEAR ILS IDENT SWAPPED CAPTS AUDIO SEL PANEL WITH 2ND OBS SEAT, 2ND OBS SEAT CONSIDERED INOP. NO PARTS AVAIL. UPDATED MR DATA TO REFLECT CORRECT POSITIONS OF MR PARTS, DEFECTIVE AUDIO SELECTOR PANEL MR23524 -24 LOCATED AT 2ND OBS SEAT. CHANGE AUDIO PANEL AT 2 OBS.

Part: WIRE — BROKEN (WINDOW HEAT) · airframe 45,978 hrs · 12,479 cycles

NR 3 F/O SLIDING WINDOW HEAT INOPERATIVE. AND FOUND BAD CONNECTOR PLUG. WIRE BROKEN AT F-O'S SLIDING WINDOW TERMINAL D1906 POS. D. WIRE CAPPED. NO PART AT IAD. REPLACED WINDOW TERMINAL PLUG ASSY. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 45,978 hrs · 12,479 cycles

TWO EACH OVERHEAD EMERGENCY LIGHTS ARE INOP AT ROWS 25 AND 28. REPLACED EMERGENCY LIGHT POWER SUPPLY M732 BATTERY PACK PER AMM. FUNCTIONAL TEST GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,978 hrs · 12,479 cycles

EEL LIGHT IS INOP AT SEAT 26B. REPLACED EEL LIGHT AT SEAT 26AB PER MM.

Part: CONTROLLER — FAILED (NR 2) · airframe 45,978 hrs · 12,479 cycles

NR 2 ENG PRC FAILED HEALTH CHECK STEPS 5Q THRU U. REMOVED AND REPLACED PRC VALVE ON THE NR 2 ENG IAW B767-300 AMM. OPS CHECK GOOD. USED OHM METER 13230064 CAL DUE DATE 08-05-2011.

Part: SLIDING WINDOW — DELAMINATED (COCKPIT) · airframe 45,975 hrs · 12,478 cycles

F-O SLIDING WINDOW DELAMINATING. CAPTAIN IS AGREEABLE TO FLY ONE LEG TO TPA DUE TO EXTENSION OF LIMITS IN LEGEND. REMOVED AND REPLACED FO NR 2 SLIDING WINDOW WITH OVERHAULED UNIT & ADJUSTED IAW B767-300MM ON PEMCO NR 2542N00042.

Part: SLIDE — UNWANTED DEPLOY (RT OVERWING) · airframe 45,650 hrs · 12,412 cycles

RT OVERWING SLIDE DEPLOYED BUT NOT INFLATED AND RT OVRD SPOILER ACTUATOR FIRED 2ND TIME. SECURED SLIDE AND REPLACED SQUIBS PER MM. ACP RII OF RT OVERWING SLIDE SQUIBS INSTALLED PER MM. REPLACED ACTUATOR. RETURNED ESCAPE SLIDE SYSTEM TO NORMAL PER MM. ALL PINS REMOVED WITH AN INSPECTOR PRESENT TO WITNESS. BATTERY PACKS RECONNECTED. ACP RII RT OVERWING SLIDE ARMING PER MM.

Part: SLIDE — UNSECURE (LT OVERWING) · airframe 45,650 hrs · 12,412 cycles

LT OVERWING SLIDE HAS LOOSE LACES. REPLACED LT OVERWING SLIDE IAM AMM. ACCOMPLISHED INSPECTION OF SLIDE INSTALLATION MM.

Part: LIGHT — MISSING (CABIN) · airframe 45,611 hrs · 12,404 cycles

AFT EEL LIGHT ON SEAT 5J IS MISSING. REPLACED LIGHT. CHECKS GOOD.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 45,459 hrs · 12,369 cycles

CABIN CREW DEP CHECK, AT START OF BOARDING 2L DOOR ESCAPE SLIDE PRESSURE FOUND LOW. REPLACED 2 LEFT DOOR SLIDE ASSY.

Part: COMPUTER — FAULTY (EICAS) · airframe 45,208 hrs · 12,320 cycles

RT EICAS COMPUTER STATUS MESSAGE RT EICAS COMPUTER INOPERATIVE. REPLACED RT EICAS COMPUTER IAW MM. CHECKED OPS PROGRAM IAW IPC. UNIT CHECKED OK AT THIS TIME.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 45,081 hrs · 12,295 cycles

CEILING MOUNTED EXIT SIGN INOP AT ROW 17 RT AISLE. REPLACED POWER SUPPLY M1209, OP CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 44,959 hrs · 12,269 cycles

SEAT 20AB EMERGENCY LIGHT INOPERATIVE. SECURED UNDER SEAT CONNECTOR, CHECKS GOOD.

Part: FEEDER CABLE — DISCONNECTED (EMERGENCY LIGHT) · airframe 44,959 hrs · 12,269 cycles

IN FRONT OF SEATS 21DEF FLOOR EMERGENCY LIGHT INOPERATIVE. RECONNECTED AT FEEDER CABLE, CHECKS GOOD.

Part: FEEDER CABLE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 44,959 hrs · 12,269 cycles

LEFT MID LAV FLOOR EMERGENCY LIGHT INOPERATIVE. RECONNECTED FEEDER CABLE, CHECKS GOOD.

Part: BATTERY PACK — FAULTY (FWD GALLEY FLOOR) · airframe 44,959 hrs · 12,269 cycles

FWD GALLEY FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED FWD GALLEY EMERGENCY LIGHT ASSY AND BATTERY PACK, CHECKS GOOD.

Part: LIGHT — BROKEN (SEAT 29B) · airframe 44,893 hrs · 12,256 cycles

SEAT 29B SIDE EMERGENCY LIGHT BROKEN. REPLACED ASSY. OPS OK.

Part: LIGHT — MISSING (SEAT 1B) · airframe 44,772 hrs · 12,230 cycles

EMERGENCY LIGHT MISSING AT SEAT 1B. REPLACED LIGHT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,772 hrs · 12,230 cycles

EMERGENCY LIGHTS INOP RT ROWS 1-6. REPLACED BATTERY PACK.

Part: LIGHT — LOOSE (SEAT 5HJ) · airframe 44,749 hrs · 12,224 cycles

EMERGENCY LIGHT STRIP TORN OFF 5HJ. 1 STRIP TORN, 1 IN PLACE. INSTALLED EMERGENCY LIGHT STRIP AT 5 HJ. CKS OK.

Part: PUMP — FAULTY (LEFT) · airframe 44,671 hrs · 12,208 cycles

LEFT CENTER AUX TANK OVERRIDE PUMP. REPLACED LT OVERRIDE & JETTISON PUMPS IAW MM. DID NOT REPLACE SHUTOFF SLEEVES, VERIFIED THAT THEY WERE 4 WINDOW STYLE.

Part: GENERATOR — FAULTY (APU) · airframe 44,309 hrs · 12,119 cycles

APU GENERATOR FAILED AT DEPARTURE. REPLACED GENERATOR AND GCU, OP CHECKS NORMAL.

Part: LIGHT — MISSING (SEAT 1H & 5H) · airframe 44,303 hrs · 12,116 cycles

EMERGENCY LIGHTS MISSING SEATS 1H, 5H. REPLACED EMERGENCY LIGHTS SEATS 1H, 5H, CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 5H) · airframe 44,150 hrs · 12,075 cycles

EMERGENCY LIGHT INOP ON SEAT 5H AFT. REPLACED LIGHT ASSY, CHECKED NORMAL ON GROUND.

Part: PRESSURE SWITCH — FAULTY (HYD SYSTEM) · airframe 44,043 hrs · 12,045 cycles

RUDDER RATIO LIGHT ILLUMINATED IN FLIGHT. EICAS MESSAGE RUDDER RATIO DISPLAYED. REPLACED LEFT ELEC. HYD PRESSURE SWITCH S27 PER MM. ACP OPS CHECKED PER MM. CHECKS OKAY, NO FAULTS & NO MESSAGES.

Part: LIGHT — BROKEN (SEAT 1B) · airframe 43,943 hrs · 12,018 cycles

SEAT 1B EMERGENCY LIGHT BROKEN OFF. REPLACED LIGHT ASSY. OPS OK.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 43,780 hrs · 11,973 cycles

AT SEAT 1H, SEAT MOUNTED EMERGENCY STRIP INOPERATIVE. WIRES HAVE PULLED OUT OF THE CONNECTOR FOR THIS AFT EMERGENCY LIGHT. REPLACED EMERGENCY LIGHT ASSY AT 1H.

Part: PROCESSOR — MALFUNCTIONED (FUEL QTY) · airframe 43,685 hrs · 11,950 cycles

BOTH COCKPIT AND FUELING PANEL GAUGES QUANTITIES FLUCTUATE. FUELERS USED THE STICKS TO VERIFY. REPLACED FQIS IAW MM. OPS NORMAL.

Part: WIRE HARNESS — MISSING (EMERGENCY LIGHT) · airframe 43,590 hrs · 11,929 cycles

SEAT 1AB ONE EMERGENCY LIGHT MISSING. SEAT EMERGENCY LIGHT CABLE END FITTING RECEPTACLE MISSING UNABLE TO ATTACH EMERGENCY LIGHT TO CABLE. REPLACED CONNECTOR AND SEAT EMERGENCY LIGHT LAMP. OPS CHECK OKAY.

Part: LIGHT — UNSECURE (SEAT 1B) · airframe 42,638 hrs · 11,690 cycles

EMERGENCY EXIT LIGHT STRIP AT 1B NEEDS TO BE REATTACHED. SECURED LIGHT ASSY, TESTS NORMAL.

Part: LIGHT — SEPARATED (CABIN) · airframe 42,596 hrs · 11,679 cycles

SEAT 2H EMERGENCY LIGHT IS SEPARATED FROM IT'S MOUNT. SECURED LT STRIP TO SEAT & OP CHECKED.

Part: LIGHT — MISSING (SEAT 2H) · airframe 42,455 hrs · 11,643 cycles

REFLECTIVE STRIP ON SIDE OF SEAT 2H HAS FALLEN OFF PIECE IN COCKPIT. REPLACED MISSING EMERGENCY LIGHT ON SEAT 2H.

Part: LIGHT — MISSING (SEAT 2H) · airframe 42,393 hrs · 11,627 cycles

F-C PAX SEAT 2H AFT EMERGENCY LIGHT ASSY MISSING. REPLACED PAX SEAT AFT EMERGENCY LIGHT ASSY AND OPS CKD GOOD.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 42,388 hrs · 11,626 cycles

CREW REPORTS ON TAXIOUT, GOT FWD EQUIP VALVE EICAS MSG. CYCLED CB B11 AND NO HELP. CYCLED EQUIP COOLING SELECTOR ON OVERHEAD, CONDITION NORMAL. VERIFIED 3-4 TIMES, UNABLE TO FAULT SYS. NO EICAS MSG OR IND LIGHT ILLUMINATED. REPLACED FWD OVERBOARD EXHAUST VALVE AND OPS TESTED. OPS OK NO MESSAGES

Part: LAMP — UNSECURE (EMERGENCY LIGHT) · airframe 42,341 hrs · 11,613 cycles

EMERGENCY LIGHTING STRIP AT SEAT 2H IS COMING OFF. SECURED LAMP AT ROW 2 AND FOUND ROW 1 EMERGENCY LAMP TORN OFF. REPLACED LAMP AT ROW 1, OP CHECKS GOOD.

Part: LIGHT — MISSING (SEAT 2J) · airframe 42,321 hrs · 11,609 cycles

SEAT MOUNTED EMERGENCY LIGHT IS MISSING ON SEAT 2J. REPLACED EMERGENCY STRIP, OPS CHECK OK.

Part: LIGHT — LOOSE (CABIN) · airframe 42,321 hrs · 11,609 cycles

EMERGENCY LIGHT STRIP LOOSE FIRST CLASS 2H. SECURED LIGHT ASSY.

Part: LIGHT — OBSTRUCTED (CABIN) · airframe 42,221 hrs · 11,586 cycles

AFT RT LAV EMERGENCY LIGHT COVERED BY CARPET LT WORKS OK. TRIM CARPET AS NECESSARY. LIGHT NOW CLEARLY SEEN.

Part: BATTERY — DISCHARGED (APU DOOR) · airframe 41,932 hrs · 11,514 cycles

PRE DEPT FOUND APU DOOR STATUS MSG. RESET DOOR NUMEROUS TIMES. DOOR STUCK OPEN. SUSPECT ACTUATOR. DOOR SECURED CLOSED IAW MEL. REPLACED INLET DOOR ACTUATOR, NO HELP. DOOR DOESN'T OPEN, CRANKED OPEN MANUALLY & REMOVED CONNECTOR PLUG APU, STILL NO CRANK. CLOSED INLET DOOR & DISCONNECTED CONNECTOR PLUG. SUSPECT INLET DOOR SWITCH BAD. ALSO, CHK APU START SW P-N & IF ANYTHING OTHER THAN 3600-5929 RPL SWITCH. THX, SFOEPA. REPLACED APU START SWITCH IAW SFOEPA, NO HELP. REPLACED RELAY K176, NO HELP. FOUND APU BATTERY DEAD. REPLACED APU BATTERY AND APU BATTERY CHARGER. OPS ARE NORMAL.

Part: ISOLATION VALVE — FAULTY (BLEED AIR SYS) · airframe 41,837 hrs · 11,487 cycles

RT ISLN VALVE LIGHT ON WITH SWITCH IN OR OUT. VALVE DEEMED DEFECTIVE. REPLACED RIGHT ISOLATION VALVE. OPS ARE GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 41,713 hrs · 11,458 cycles

RIGHT MAIN GEAR DOWN INDICATOR LIGHT INOP. REPLACED LIGHT ASSEMBLY. AS PRECAUTION PERFORMED PSEU LANDING GEAR SYSTEM NR 1 AND NR 2 AND SYSTEM TEST NORMAL.

Part: LIGHT — MISSING (SEAT 1B FWD) · airframe 41,067 hrs · 11,312 cycles

SEAT 1B FWD EMERGENCY LIGHT MISSING. REPLACED SEAT 1B EMERGENCY LIGHT STRIP. CHECKS OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,991 hrs · 11,296 cycles

HEAVY RUBBER ODOR IN AFT CABIN NEAR SEAT 25 & AFT. TURNED OFF BOTH UTILITY ON SHORT FINAL. IAW CAPTAIN THE BURNED ODOR WAS NOTICED ON THE FLIGHT DECK. IAW THE F/A THE ODOR WAS ON THE RT SIDE OF THE CABIN AND DISSIPATED AFTER CAPTAIN TURNED OFF THE UTILITY BUSSES. ACCOMPLISHED CHECKS NO ABNORMALITIES NOTED.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 40,866 hrs · 11,265 cycles

L ENG HPSOV ON AND BLEED LIGHT ON. RETARDED THROTTLES TO IDLE. GOT LT ENG HPSOV EICAS MSG AND OVERHEAD PANEL BLEED LIGHT ILLUMINATED. SECURED LT HPSOV CLOSE POSITION. REPLACED HPSOV. OP CHECKS NORMAL.

Part: CONTROLLER — MALFUNCTIONED (BLEED SYSTEM) · airframe 40,814 hrs · 11,251 cycles

DUCT PRESS APPROX 35L-20R IN CLIMB. REMAINS SPLIT 20L-10R IN CRUISE 350 EPR 1.17. RAN BITE CHECK ON AIR SUPPLY BITE MODULE, FOUND FAULTS ON PRV AND PRV CONTROL. REPLACED PRV AND PRV CONTROL. OP CHECKS NORMAL

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 40,676 hrs · 11,218 cycles

EMERGENCY LIGHT BROKEN AT SEAT 1A. LAMP FOUND DAMAGED. REPLACED LAMP. CHECKS OK.

Part: LIGHT — UNSECURE (SEAT 1B) · airframe 40,588 hrs · 11,194 cycles

SEAT 1B EMERGENCY LIGHT DETACHED SECURED LIGHT STRIP AND OP CHECK LIGHT.

Part: LIGHT — MISSING (CABIN) · airframe 40,489 hrs · 11,167 cycles

SEAT 6H EEL LT MISSING. REPLACED EEL LIGHT STRIP AT 6H. TESTED OKAY.

Part: COMPUTER — FAULTY (RT EICAS) · airframe 40,333 hrs · 11,128 cycles

LOWER EICAS SCREEN WENT TO ALL BLUE COLOR. WORKS NORMAL ON RIGHT COMPUTER. REPLACED RT EICAS COMPUTER. ACP SOFTWARE LOAD. OPS CHECK OKAY.

Part: SHUTOFF VALVE — FAILED · airframe 40,169 hrs · 11,089 cycles

LEFT DUCT PRESSURE FLUCTUATES BETWEEN 25 TO 40 PSI ON DESCENT. FOUND PRSOV FAILED HEALTH CHECK. REPLACED PRSOV, OPS CHECKS GOOD.

Part: OVEN — DIRTY (GALLEY) · airframe 39,834 hrs · 11,003 cycles

AT DEPARTURE CREW REPORTS BURNING SMELL IN 1ST CLASS. FOUND SEVERAL LIGHTS INOP IN NEED OF BALLAST P2511. FOUND FWD GALLEY WARMING OVENS ON & EXTREMELY HOT WITH FOIL BREAD BAG INSIDE. AFTER OVENS OFF FOR 1 HR SMELL DISSIPATED. ODOR WAS STRONGEST AT MED 1L.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN FLOORBEAM CORRODED ON UPPER FLANGE BS 287, LBL 20 TO RBL 15. MAJOR REPAIR ACCOMPLISHED. CORROSION FOUND TO BE OUT OF LIMITS. DAMAGED SECTION OF FLOORBEAM REMOVED BETWEEN LBL 32 TO RBL 88. FABRICATED & INSTALLED A REPAIR T-ANGLE, SPLICE PLATE, AND SPLICE ANGLES.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 39,797 hrs · 10,991 cycles

NR 2 ENG PYLON SIDE SKIN AT PANEL 446BL UPPER FWD CORNER IS CRACKED. MAJOR REPAIR ACCOMPLISHED: STOP DRILL CRACK AND INSTALLED DOUBLER REPAIR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,797 hrs · 10,991 cycles

G1 EMERGENCY AISLE LIGHTS INOP. RELAMPED 1G EMERGENCY AISLE LIGHT, OPS CHECKS GOOD.

Part: TRIGGER — OUT OF POSITION (SLIDE BOTTLE) · airframe 39,797 hrs · 10,991 cycles

LEFT OVERWING SLIDE BOTTLE TRIGGER CABLE BALL IS OUTSIDE SPRING RETAINER. INSTALLED NEW LT OVERWING SLIDE BOTTLE.

Part: LIGHT — INOPERATIVE (AFT GALLEY) · airframe 39,797 hrs · 10,991 cycles

LEFT EMERGENCY LIGHT INOP AT AFT GALLEY AREA. INSTALLED NEW LIGHT AFT GALLEY, OPS CHECKS GOOD.

Part: OXYGEN MASK — FAULTY (SEAT 12) · airframe 39,797 hrs · 10,991 cycles

B-ZONE SEAT 12 CENTER FAILS O2 DROP. REPACK O2 MASK AT SEAT 12 CENTER. OPS CHECKS GOOD.

Part: LIGHT — IMPROPER PART (CABIN) · airframe 39,797 hrs · 10,991 cycles

SEAT 20AB HAS WRONG IN-SEAT EEL LIGHT ASSY INSTALLED. REMOVED & REPLACED THE HALF-RED HALF-GREEN EEL LIGHT & INSTALLED CORRECT LIGHT STRIP & OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,797 hrs · 10,991 cycles

MID CROSS AISLE EEL LIGHT BAR INOP. REMOVED & REPLACED MID CROSS AISLE LIGHT BAR. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,797 hrs · 10,991 cycles

EMERGENCY AISLE LIGHT INOP AT SEAT 4AB. RELAMPED AISLE LIGHT AND OPS CHECKS GOOD.

Part: CYLINDER — DEFECTIVE (EVAC SLIDE) · airframe 39,797 hrs · 10,991 cycles

RIGHT OVERWING SLIDE BOTTLE TRIGGER CABLE BALL IS OUTSIDE SPRING RETAINER. INSTALLED NEW INFLATION CYLINDER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,797 hrs · 10,991 cycles

EMERGENCY AISLE LIGHT AT AFT LEFT LAV INOP. RELAMPED AND OPS CHECKED GOOD.

Part: SLIDE — OUT OF TOLERANCE (R1 DOOR) · airframe 39,797 hrs · 10,991 cycles

DOOR R1 SLIDE OUT OF TOLERANCE. INSTALLED NEW SLIDE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,797 hrs · 10,991 cycles

AFT CARGO COMPARTMENT SHEAR TIE SURFACE CORRODED AT BS 1197+22, BETWEEN STR 37R-38R. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE AND FABRICATED & INSTALLED A NEW SHEAR TIE.

Part: ATTACH ANGLE — CRACKED (NLG WW) · airframe 39,797 hrs · 10,991 cycles

FORWARD E&E COMPARTMENT, RIGHT NOSE GEAR WHEEL WELL, PULLEY BRACKET ATTACH ANGLE CRACKED, LOWER OUTBOARD SIDE OF FLOORBEAM BS 246 AND LBL 15. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED ANGLE AND REPLACED WITH NEW ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN FLOORBEAM CORRODED ON UPPER FLANGE BS 287, RBL 88. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FLOORBEAM BETWEEN LBL 32 TO RBL 88. FABRICATED & INSTALLED A REPAIR T-ANGLE, SPLICE PLATE AND SPLICE ANGLES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN SEAT TRACK CORRODED ON BS 325, LBL 11. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF SEAT TRACK BETWEEN BS 322 TO 423 LBL 11. FABRICATED AND INSTALLED A NEW SPLICE SECTION.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,797 hrs · 10,991 cycles

AFT CARGO COMPARTMENT SHEAR TIE SURFACE CORRODED AT BS 1197+22, BETWEEN STR 39L-39R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SHEAR TIE. FABRICATED & INSTALLED A NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,797 hrs · 10,991 cycles

AFT CARGO COMPARTMENT SHEAR TIE SURFACE CORRODED AT BS 1197, STR 37R-38R. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE AND FABRICATED & INSTALLED A NEW SHEAR TIE.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN FLOORBEAM CORRODED BS 1520, LB L30. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FLOORBEAM AT BS 1518, LBL 26 TO LBL 31. FABRICATED & INSTALLED A REPAIR SECTION OF T-CAP AND SPLICE ANGLES.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN SEAT TRACK CORRODED BS 325, RBL 11. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF SEAT TRACK BETWEEN BS 322 TO 423, RBL 11, FABRICATED AND INSTALLED A REPAIR SECTION.

Part: STIFFENER — CRACKED (NLG WW) · airframe 39,797 hrs · 10,991 cycles

FORWARD E&E COMPARTMENT RIGHT NOSE GEAR WHEEL WELL STIFFENER CRACKED, MIDDLE OF STIFFENER AT FLOORBEAM BS 246, LBL 10. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STIFFENER.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN RT SEAT TRACK IS CORRODED AT R-1 DOOR BS 347, RBL 88. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SEAT TRACK BETWEEN BS 343 TO BS 402 RT SIDE. FABRICATED & INSTALLED A NEW SECTION OF TRACK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,797 hrs · 10,991 cycles

AFT CARGO COMPARTMENT SHEAR TIE SURFACE CORRODED STA 1197 + 66, STR 37R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW SHEAR TIE.

Part: GUARD — CORRODED (BS 325-347) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN RT SPLASH GUARD IS CORRODED AT R-1 DOOR, BS 325-BS 347, RBL 88. REMOVED CORROSION AND FOUND PART TO BE CRACKED AT FASTENER HOLE, NO CRACKS PERMITTED. REMOVED AND REPLACED SPLASH GUARD P/N 141T8310-244 AND RE-INSTALLED REMOVED SCUFF PLATES AND GIRT BAR FITTINGS.

Part: GUARD — CORRODED (BS 303-347) · airframe 39,797 hrs · 10,991 cycles

MAIN CABIN LT SPLASH GUARD IS CORRODED AT L-1 DOOR, BS 303 - BS 347, LBL 88. REMOVED AND REPLACED SPLASH GUARD. RE-INSTALLED SCUFF PLATE AND GIRT BAR FITTINGS RESPECTIVELY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,797 hrs · 10,991 cycles

DOOR 2R EMERGENCY LIGHT INOPERATIVE. RELAMPED R2 DOOR EMERGENCY EXIT LIGHT AND OPS CHECK GOOD.

Part: CABLE — DAMAGED (OVERWING DOOR) · airframe 39,797 hrs · 10,991 cycles

LEFT AFT OVERWING EMERGENCY EXIT STEP AFT CABLE KINKED AND FRAYED. REMOVED AND REPLACED LEFT OVERWING AFT STEP CABLE AND OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,797 hrs · 10,991 cycles

DOOR 2L EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. RELAMPED L2 DOOR EMERGENCY EXIT LIGHT AND OPS CHECK GOOD.

Part: LATCH — GOUGED (EVAC SLIDE) · airframe 39,797 hrs · 10,991 cycles

RIGHT OVERWING SLIDE COMPARTMENT DOOR LATCH NR 4 DAMAGED (GOUGED). INSTALLED NEW NR 4 LATCH, OPS CHECKS GOOD.

Part: LATCH — GOUGED (EVAC SLIDE) · airframe 39,797 hrs · 10,991 cycles

RIGHT OVERWING SLIDE COMPARTMENT DOOR LATCH NR 3 DAMAGED (GOUGED). INSTALLED NEW NR 3 LATCH, OPS CHECKS GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 38,758 hrs · 10,738 cycles

IN SEAT EEL LIGHT AT SEAT 36HJ MISSING. INSTALLED NEW EEL LIGHT, CHECKS GOOD.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 38,748 hrs · 10,736 cycles

BLEED DOES NOT OPEN AT IDLE-INTERMITTENTLY WITH PWR LVL RAISED. REPLACED PRVC CONTROLLER, OP CK'D NORMAL.

Part: IDG — DEFECTIVE (NR 2 ENGINE) · airframe 38,550 hrs · 10,691 cycles

RIGHT GEN "DRIVE" AMBER LOW PRX LIGHT IS NOT ILLUMINATED WITH ENGINE NOT RUNNING. RAN ENG2, DISCONNECTED IDG EICAS INDICATION NORMAL, INDICATION ON SWITCH INOP. JUMPERED PINS FROM PRESSURE SWITCH AT IDG AND LIGHT CAME ON. BAD PRESS SWITCH ON IDG. REPLACED NR 2 ENG IDG.

Part: LIGHT — MISSING (CABIN) · airframe 38,186 hrs · 10,599 cycles

SEAT 6AB MISSING 1 EACH ESCAPE LIGHT. INSTALLED NEW LIGHT, OP NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,186 hrs · 10,599 cycles

EMERGENCY ESCAPE LIGHTS CONNECTED TO POWER SUPPLY M734 ARE INOP. REPLACED BATTERY AT M734, OP NORMAL.

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 37,039 hrs · 10,336 cycles

AFT EMERGENCY LIGHT ON SEAT 6A IS MISSING. REPLACED LIGHT, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,039 hrs · 10,336 cycles

EEL LIGHT ON SEAT 35A IS INOP. REPLACED CABLE ASSY (HARNESS) AND OPS CHECKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,039 hrs · 10,336 cycles

EEL LIGHT ON SEAT 30A IS INOP. NEEDS LIGHT ASSY. NO PARTS AT SFO. PCN 585-5228. RELAMPED, OPS CK OK

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,039 hrs · 10,336 cycles

EMERGENCY LIGHT ON SEAT 30A IS INOP. RELAMPED, OPS CK OK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 37,039 hrs · 10,336 cycles

EEL LIGHT ON SEAT 39J IS INOP. FOUND HARNESS DISCONNECTED AT OUTBOARD END, SECURED CONNECTOR, OPS CHECK OKAY.

Part: LAMP — MISSING (CABIN) · airframe 37,039 hrs · 10,336 cycles

AFT EEL LIGHT ON SEAT 6A IS MISSING. REPLACED LIGHT, CHECKS GOOD.

Part: LIGHT — BROKEN (EXTERIOR) · airframe 37,039 hrs · 10,336 cycles

ALL 6EA RT SIDE EXTERIOR EEL LIGHTS ARE INOP. REPLACED BROKEN BULB AT AFT RT DOOR SLIDE LIGHT, BATTERY AT M733, AND BATTERY AND CHARGER AT M731. CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,039 hrs · 10,336 cycles

LT SIDE 2EA AFT EXTERIOR EEL LIGHTS ARE INOP. RELAMPED AND LIGHTS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 36,468 hrs · 10,209 cycles

EMERGENCY ESCAPE LIGHTING LOOSE IN FLOOR AT SEAT 3B. LIGHT FOUND UNSECURE. REPLACED THE EEL LIGHT AT SEAT 3B AS REQUIRED. OP CHECKS NORMAL.

Part: OIL FILTER — FAULTY (NR 2 ENGINE) · airframe 36,354 hrs · 10,184 cycles

NR 2 ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE DISAPPEARED WHEN THRUST REDUCED. OIL FILTER IS FAULTY. REPLACED NR 2 ENG OIL FILTER. LEAK AND OPS CHECK GOOD.

Part: IDG — LEAKING (LEFT) · airframe 36,227 hrs · 10,152 cycles

EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. CREW COMMENTS: L T ENG DRIVE LIGHT CAME ON AFTER T/O AND WENT OUT AFTER TWO MINUTES WITH NO CREW ACTION. FUEL OIL COOLER LEAKING AND IDG DRY. REPLACED NR 1 ENGINE IDG & NR 1 ENG FUEL OIL COOLER & BYPASS VALVE.

Part: BYPASS VALVE — FAULTY (T/E FLAP) · airframe 35,974 hrs · 10,093 cycles

ALTERNATE T/E FLAP DRIVE ELECTRIC MOTOR RUNS BUT DOES NOT TURN GEARBOX TO EXTEND FLAPS. REPLACED T/E FLAP BYPASS VALVE. OP CHECKS NORMAL.

Part: EEC — FAULTY (NR 1 ENGINE) · airframe 35,920 hrs · 10,078 cycles

L ENG CONT EICAS AND L ENG CONT STATUS. REPLACED NR 1 ELECTRICAL ENGINE CONTROL. ACCOMPLISHED OPS CHECK. CHECKS OKAY.

Part: CONTROL UNIT — FAULTY (APU) · airframe 35,904 hrs · 10,071 cycles

APU FAULT. ECU FOUND FAULTY. REPLACED ECU. OPS CHECKS NORMAL.

Part: ENGINE — HUNG START (LEFT) · airframe 35,443 hrs · 9,958 cycles

LEFT ENGINE HUNG START AT 30 PERCENT N2. LEFT HYD QTY NOW LOW.

Part: CONTROL PANEL — INOPERATIVE (COCKPIT) · airframe 35,398 hrs · 9,947 cycles

UNABLE TO SET ALTITUDE IN CABIN ALTITUDE CONTROL. REMOVED & REPLACED CABIN ALTITUDE CONTROL PANEL.

Part: FILTER — WARNING MESSAGE (ENGINE OIL) · airframe 34,993 hrs · 9,851 cycles

LT ENG OIL FILTER MSG APPEARED AFTER ENG START. MSG CLEARED WITHOUT ANY FLIGHT CREW ACTION. RETURNED TO BLOCKS. MAINTENANCE REPLACED THE MAIN OIL FILTER PER AMM 79-21-05. NO METAL FOUND. FLIGHT TOOK AN 84 MINUTE DELAY. PROBLEM DID NOT RECUR.

Part: BATTERY — DISCHARGED (AFT CARGO BAY) · airframe 34,452 hrs · 9,715 cycles

APU WILL NOT START. SUSPECT FAULTY BATTERY. REPLACED BATTERY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: PUMP — OVERHEATED (RIGHT) · airframe 34,325 hrs · 9,684 cycles

RIGHT HYDRAULIC SYSTEM OVERHEAT PROBLEM CAUSED FLIGHT DIVERSION. REPLACED RT EDP. NO SHOP RECORD FOUND. ROOT CAUSE UNKNOWN.

Part: PANEL — DAMAGED (RT WING) · airframe 34,095 hrs · 9,623 cycles

MOST INBOARD LOWER RT LEADING EDGE PANEL INBD CORNER BROKEN OFF. APPROX. 3 INCH BY 1-2 INCH REINFORCED LEADING EDGE SECTION MISSING. REMOVED FOR REPAIR. REPAIRED BY SHOP. REINSTALLED PANEL. ACFT OK FOR SERVICE.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 33,915 hrs · 9,575 cycles

FA SHOCKED WHEN GRABBING BOTH HANDLES OF THE COFFEE POTS AT 2R. REPLACED M51 & M52 COFFEE MAKER - OP CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — UNSECURE (SEAT 6B) · airframe 33,713 hrs · 9,530 cycles

SEAT 6B EMERGENCY LIGHT ON SIDE NEEDS GLUE, IT'S DANGLING ON WIRE.

Part: APU — UNKNOWN · airframe 33,684 hrs · 9,524 cycles

APU WILL NOT START. AFTER EXTENSIVE TEST, REPLACED APU PER MM 49-11- 01 PG401.PERFORMED APU TEST PER JRH 2-6-15 AND PER UNIMATIC DISPLAY 2450 PERFORMANCE CHECK GOOD. VERIFICATION FLIGHT ACCOMPLISHED. APU STARTED NORMALLY. AC OK FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 33,599 hrs · 9,505 cycles

RT FWD OVERWING CABIN EEL LIGHT INOP. TROUBLESHOOT FOUND UNDER SEAT CONNECTOR LOOSE. SECURED THE CONNECTION OPS CKECKED OK. AC OK FOR SERVICE.

Part: CIRCUIT CARD — OVERHEATED (COCKPIT) · airframe 33,580 hrs · 9,501 cycles

L ENG OH LP 1 STATUS MESSAGE WILL NOT ERASE. FOUND OVERHEAT DETECTION CARD. RESEATED OVERHEAT CARD FOR NR 1 ENGINE MESSAGE CLEARED, FIRE-TEST CHECKS GOOD. AC OK FOR SERVICE.

Part: SHUTOFF VALVE — FAULTY (APU) · airframe 33,499 hrs · 9,482 cycles

APU DOES NOT START. REPLACED APU SHUTOFF VALVE. OPS CHECK GOOD.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 33,290 hrs · 4,539 cycles

SUSPECT BALLAST OVERHEATING IN MID GALLEY. TURNED OFF LIGHTS, STRONG ACRID ODOR PRESENT. REMOVED MID GALLEY CEILING PANEL AND NOTICED ODOR WAS EMANATING FROM SPEAKER DRIVE MODULE. REMOVED CONNECTOR AND ODOR DISSIPATED. REPLACED SPEAKER DRIVE MODULE. NO FURTHER REPORT OF ACRID ODOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,109 hrs · 9,394 cycles

EEL LIGHTS INOP AT SEATS 30HJ & 39HJ. REPLACED EEL STRIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,109 hrs · 9,394 cycles

SEAT 3AB EEL LIGHT INOPERATIVE. RELAMPED.

Part: STARTER — INOPERATIVE (APU) · airframe 33,043 hrs · 9,377 cycles

APU FAILED TO START AFTER TWO ATTEMPTS, FAULT LIGHT ON LAST ATTEMPT. CHK'D MAG CHIP DETECTRS OK, BIT APU CONTROL OK. REPLACED APU STARTER, OPS OK APU START.

Part: ENGINE — LEAKING (NR 1) · airframe 32,293 hrs · 9,204 cycles

(NR 1 ENG HOC): OIL LEAKING FROM FUEL PUMP DRAIN 4 DPM WITH ENG STATIC.

Part: PUMP — MALFUNCTIONED (APU OIL SYSTEM) · airframe 29,771 hrs · 8,565 cycles

APU OIL CONSUMPTION IS EXCESSIVE. [SUP 4-20-07] APU WAS REMOVED FROM AIRCRAFT FOR HIGH OIL CONSUMPTION. OIL CONSUMPTION WAS INVESTIGATED AND CONFIRMED IN THE TEST CELL. THE LRU OIL PUMP WAS REPLACED AND ALL HOC WAS GONE. WITH PROPER TROUBLESHOOTING, THIS APU COULD HAVE BEEN REPAIRED WITH THE APU STILL IN THE AIRCRAFT. THE REMOVAL OF THIS APU WAS UNNECESSARY. THE OIL PUMP IS A LINE REPLACEABLE UNIT.

Part: SWITCH — DEFECTIVE (EMERGENCY LIGHTS) · airframe 29,233 hrs · 8,429 cycles

ALL AIRCRAFT EMERGENCY LIGHTS COME ON WHEN POWER REMOVED FROM AIRCRAFT. FOUND EMERGENCY LIGHT SWITCH S1 DEFECTIVE. REPLACED SWITCH. OP CHECKS NORMALLY.

Part: DETECTION SYS — NO TEST · airframe 28,728 hrs

FIRE-OVERHEAT TEST DID NOT INITIATE WHEN -ENG APU CARGO- TEST SWITCH PUSHED. RETESTED ON GROUND PER AMM 26-15-00, P 501. UNABLE TO DUPLICATE. NO PROBLEM FOUND. CHECKED OK

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,489 hrs · 8,003 cycles

FOUND FWD GALLEY CROSS AISLE EEL LIGHT INOP. REPLACED EEL STRIP, OPS CK OK.

Part: WARNING LIGHT — ILLUMINATED (BLEED OVERHEAT) · airframe 24,811 hrs · 7,371 cycles

RETURNED TO FIELD DUE TO LEFT BLEED OVERHEAT INDICATION. THE WING DUCT LEAK DETECTORS TS211 & TS212 WERE REPLACED. DURING TROUBLESHOOTING THE SENSOR THAT WAS CAUSING THE FAULT COULD NOT BE DETERMINED SO BOTH WERE REPLACED. THE REMOVED PARTS ARE NON-STOCK, NO FURTHER ANALYSIS. AS OF 09FEB06 THIS WAS THE ONLY ABNORMALITY REPORTED IN AMIS FOR CHAPTER 26. AN 8-IN CRACK WAS FOUND IN THE DUCT CAUSING BLEED AIR LEAKAGE AND "BODY DUCT LEAK" EICAS MESSAGE TO APPEAR. THE DUCT WAS REPLACED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 24,712 hrs · 7,344 cycles

FUSELAGE DENTED AND GOUGED FWD OF AFT CARGO PIT CONTROL PANEL DOOR. FUSELAGE SKIN REPAIRED PER SRM. SUPPLEMENTAL INSPECTIONS REQUIRED BY 37,500 CYCLES ARE MONITORED BY AMIS CF9010.

Part: LATCH — FAILED (CABIN)

LT O/W COMPT INTEGRATOR TORQUE CHECK FAILED AND LATCHES MUST BE REPLACED. REMOVE AND REPLACE LATCHES IAW UAL B767 MM-25-65-98.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 17,082 hrs · 5,469 cycles

CABIN FLOORBEAM WEB CRACKED STATION 1439, LBL 25. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE DOUBLER.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 12,868 hrs · 4,333 cycles

FLAME-OUT OF NUMBER 2 ENGINE. INADEQUATE FUEL SUPPLY PROVIDED TO NR 2 ENGINE. CONDUCTED EXTENSIVE ENGINE AND FUEL SYSTEM DIAGNOSTIC TESTING. DISCOVERED NO INDICATION OF MECHANICAL OR ELECTRONIC SYSTEM FAULTS. CAREFULLY TRACKED AIRPLANE OPERATION AFTER INCIDENT WITH NO FURTHER ANOMALIES INDICATED.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 12,452 hrs · 4,219 cycles

R EICAS CMPTR EICAS MSG DISPLAYED. REPLACED EICAS COMPUTER AND LOADED CORRECT OPS AND OPC SOFTWARE. OPS OK. THERE WAS NO FAULT FOUND IN THE REMOVED EICAS COMPUTER.

Part: COMPRESSOR — DETERIORATED (NR 2 ENGINE) · airframe 12,254 hrs · 4,166 cycles

AT APPROX 300 AGL NR 2 ENGINE HAD A COMPRESSOR SURGE, MAX EGT 638F. ENGINE EXPERIENCED A GROUP 3 SURGE. SURGE IS CAUSED BY EXCESSIVE BLADE TIP CLEARANCES IN THE HPC REAR STAGES. PERFORMED TEST-21 AND ENGINE FAILED. ENGINE WAS REMOVED FOR SHOP REWORK. AD 2001-25-11 ALREADY IN EFFECT FOR FLEET DETERIORATION MANAGEMENT. FINAL FIX PENDING.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 9,514 hrs · 3,333 cycles

APU WOULD NOT START IN FLIGHT AFTER 3 ATTEMPTS AT FL 300, FL320, AND FL360, RTF.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 9,512 hrs · 3,332 cycles

LEFT GEN TRIP EN ROUTE TO HNL WOULD NOT RESET. APU WOULD NOT START, RTF.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 9,512 hrs · 3,332 cycles

APU FAILED TO START AT FL340. AFTER TURNBACK, IT DID START AT FL200. NR 1 GEN ALSO INOP, RTF.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 8,904 hrs · 3,115 cycles

ON GEAR RETRACTION DURING T/O FROM OGG, AIR DEMAND PUMP LOW PRESS LIGHT CAME ON. DIVERTED TO HNL. *S/D* REPLACED AIR DRIVEN PUMP.

Part: ENGINE — FLAMED OUT (LT & RT ENGINE) · airframe 8,622 hrs · 3,031 cycles

LEFT AND RIGHT ENGINE FLAMEOUT REPORTED AT FL240. RESTARTS ACCOMPISHED. DIVERTED KOA. EMERGENCY DECLARED. LANDED APPROXIMATELY 24000 LBS OVERWEIGHT.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 8,879 hrs · 3,109 cycles

AFTER T/O DURING FLAP RETRACTION A LOUD METAL ON METAL SOUND WAS HEARD THROUGHOUT THE ACFT. THIS NOISE CONFIRMED BY FLT CREW WHILE FLAPS IN MOTION AND CEASED IMMEDIATELY WHEN FLAPS STOPPED. *S/D* INTERNAL FAILURE OF CENTER HYDRAULIC SYSTEM AIR DRIVEN PUMP (ADP) CAUSED GRINDING SOUND IN PUMP. THIS PUMP IS ON DEMAND FOR T/O WITH BOTH LANDING GEAR AND TRAILING EDGE FLAP SYSTEMS OPERATIVE. REPLACED SUBJECT ADP WITH SERVICEABLE UNIT.