N647UA

Part: PANEL — MISSING (ZONE 400) · airframe 130,985 hrs · 20,278 cycles

RIGHT ENGINE PYLON PANEL MISSING, PANEL 446BL, NR 2 ENGINE INBD NACELLE STRUT ACCESS DOOR PANEL, THE PANEL WAS REMOVED DUE TO 2 MISSING FASTENERS.

Part: COMPUTER — FAULTED (THRUST MANAGEMNT) · airframe 130,898 hrs · 20,267 cycles

PILOTS REPORT THAT ON ENGINE DISPLAY NO COMMAND BAR NOR TAKEOFF INDICATION SHOWN, EPR & AUTOTHROTTLE WILL NOT ENGAGE. PERFORMED AUTO FLT BITE IAW FIM 22-02, TASK 801. R & R THRUST MANAGMENT COMPUTER IAW AMM 22-31-01-404-005. OPS CHECKED GOOD , PERFORMED GROUND RECIRTIFICATION TEST IAW AMM 22-00-02. ALL TEST PASSED. AIRCRAFT RETAINS FULL CAT II/III LAND CAPABILITIES

Part: ACCESS PANEL — MISSING (ZONE 400) · airframe 130,344 hrs · 20,202 cycles

LEFT ENGINE INBOARD PYLON PANEL 436AR WAS MISSING ON ARRIVAL. INSTALLED NEW PANEL WITH LANYARD ATTACHED. AFTER INSPECTING AIRCRAFT FOR FURTHER DAMAGE IAW AMM 05-51-59. NO ADDITIONAL DAMAGE WAS FOUND.

Part: ACCESS DOOR — MISSING (ZONE 400) · airframe 130,139 hrs · 20,177 cycles

NACELLE STRUT ACCESS DOOR 436AR MISSING ON #1 ENGINE UPON ARRIVAL TO VCE.

Part: IDG — FAULTED (NR 2) · airframe 130,044 hrs · 20,165 cycles

RIGHT GENERATOR DRIVE LIGHT CAME ON DURING FLIGHT DEBRIEFED CREW. CREW STATED LIGHT CAME ON DURING FLIGHT. ACCOMPANIED BY EICAS STATUS R GEN DRIVE. REF FIM 24-20 FAULT TREE 801. BITE CHECKED BPCU, FOUND FOLLOWING MESSAGES, ATTACHED PIX DRAINED RIGHT IDG OIL AND FOUND IDG TO HAVE 3 QUARTS OF OIL. SUSPECT LOW OIL CAUSED OVERHEAT CONDITION LEADING TO DRIVE LIGHT ILLUMINATION. #2 ENGINE IDG REMOVED AND REPLACED REF AMM 24-11-01. PERFORMED BPCU BITE TEST AND RESET TEST REF AMM 24-11-00-745-001. ALL SYSTEMS SHOW OK. COMPLETED INSTALL OF #2 ENGINE IDG. REF AMM 24-11-01. OPS CHECK GOOD. NO LEAKS FOUND.

Part: CABLE — MISSING (ZONE 800) · airframe 128,853 hrs · 20,020 cycles

DURING VERIFICATION OF L OW SLIDE BEING IN DIARMED STATUS FOUND LEFT INFLATION TRIGGER CABLE NOT INSTALLED BEHIND RETAINING SPRING, INFLATION CYLINDER REQUIRESS REPLACEMENT PER AMM TASK 25-65-00-042-001 RESECURED INFLATION TRIGGERCABLE BALL PER AMM 25-65-02-350-811-C2. INFLATION CYLINDER OK FOR SERVICE

Part: PRESSURE SWITCH — FAULTED (HYD SYSTEM) · airframe 127,201 hrs · 19,812 cycles

HYD C PRESSURE LT ON EICAS CAME ON AFTER T.O WHEN GEAR WAS MOVED TO RETRACT. ON RETURN ASKEDCREW STATED DURING CLIMB OUT THE 3RD PILOT NOTICED THE HYD PRESSURE EICAS, BUT AT PHASE OF FLIGHT WAS UNABLE TO LOOK UP AND SEE IF THE PRESSURE LIGHT ILLUMINATED ON THE OVHD. CREW STATED THAT THEY HAD A GEAR DISAGREE AND NOTICED THE GEAR DOORS WERE SLOW TO COME UP. ALSO NOTICE THAT THE FLAPS WERE SLOW TO RETRACT. CREW STATED THAT HYDRAULIC "C PRESSURE" EICAS MESSAGE POPUALATED. BREIFED CREW IF THEY RAN THROUGH QRH AND STATED ONCE THEY STARTED THE QRH EVERYTHING WAS OPERATING NORMALLY SO THE QRH AS NOT REQUIRED. WE CONTACTED TOMC TO ASK IF THEY COULD SET THE ADP FROM "AUTO " TO "ON." CREW STATED THAT ON APPROACH BACK TO IAH EVERYTHING OERATED NORMALLY. F/O ALSO STATED HE FLEW THIS AIRCRAFT A FEW DAYS AGO AND ON THE GROUND THE FLAPS WERE SLOW TO EXTEND WHEN OPERATING FLIGHT CONTROL CHECKS AND THE ADP WAS IN "AUTO." PERFORMED FIM TASK FIM29-11 FAULT ROYTREE 813. LEFT SYSTEM SHOW HPSOV AND HPC. SEE PHOTO. CONTINUED WITH FIM 29-11 FAULT TREE 813. REMOVED CONNECTOR D466 FROM ADP CONTROL PRESS SWITCH S29 AND FOUND PRESS SWITCH DAMAGED. INSPECTED CONNECTOR D466. NO DAMAGE NOTED. PRESSURE SWITCH S29 REQUIRES REPLACEMENT. REMOVED AND REPLACED THE S29 SWITCH REF AMM 29-11-19-004-001 AS A PRECAUTION, REMOVED AND REPLACED RELAYS, K684 AND K178. ALSO CHECKED RESISTANCE OF TIME DELAY MODULE M305. RESISTANCE CHECKS GOOD. PERFORMED 5 MIN ENGINE RUN NO FAULTS IN FLIGHT DECK, OR BITE BOX.

Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 126,792 hrs · 19,763 cycles

AIR DIVERSION TO EWR WAS IAD - AMSL2 DOOR NOT ARMED PRIOR TO T/O OUT OF IAD TO AMS.F/A UNABLE TO ARM IN FLT.THE TOMC CONTROLLER AND SENIOR MANAGER CONCUR THAT THE AIRCRAFT CAN BE RELEASED BACK TO SERVICE AFTER EXPERIENCING A DIVERSION O R AIR TURN BACK DUE TO A MECHANICAL REASON LOCKED BY SYSTEM. UNLOCKED FOR SIGN OFF SLIDE AT 2L ARMED AND DISARMED SEVERAL TIMES AND INSPECTED FOR CORRECT INSTALLATION AND OPERATION. NO ISSUED DETECTED. REF AMM 25-66-01.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 126,664 hrs · 19,746 cycles

SEAT 30D EPL ( ESCAPE PATH LIGHT)LENS BROKEN SEAT30D EPL (ESCAPE PATH LIGHT)ASSY SUCCESSFULLY REPLACED IAW AMM 33-51-10. INSPECTED AND APPROVED INSTALLATION AND SYSTEM TEST REF AMM 33-51-10.

Part: LENS — BROKEN (ZONE 200) · airframe 126,664 hrs · 19,746 cycles

SEAT 32D EPL ( ESCAPE PATH LIGHT)LENS BROKEN SEAT32D EPL (ESCAPE PATH LIGHT) SUCCESSFULLY REPLACED IAW AMM 33-51-10. INSPECTED AND APPROVED INSTALLATION AND SYSTEM TEST REF AMM 33-51-10

Part: SHROUD — BROKEN (ZONE 200) · airframe 126,664 hrs · 19,746 cycles

SEAT 35D EPL ( ESCAPE PATH LIGHT) SHROUD ASSY UNIT BRONKEN SEAT 35D EPL (ESCAPE PATH LIGHT)ASSY SUCCESSFULLY REPLACED IAW AMM 33-51-10. INSPECTED AND APPROVED INSTALLATION AND SYSTEM TEST REF AMM 33-51-10.

Part: LENS — BROKEN (ZONE 200) · airframe 126,664 hrs · 19,746 cycles

SEAT 31F EPL( ESCAPE PATH LIGHT)LENS BROKEN SEAT 31F EPL (ESCAPE PATH LIGHT) LENS SUCCESSFULLY REPLACED IAW AMM 33-51-10. INSPECTED AND APPROVED INSTALLATION AND SYSTEM TEST REF AMM 33-51-10.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 126,513 hrs · 19,721 cycles

LH FUSELAGE AFT EMERGENCY EXIT LIGHT INOP RELAMPED REF AMM 33-51-06, OPS CHECKS OK

Part: PUMP — FAULTED (NR 2 FUEL) · airframe 125,828 hrs · 19,616 cycles

R COMPRESSOR STALLGOT COMPRESSOR STALL AT 2500 FEET SPEED 200KT ON FINAL APPROACH INTO IAD. USE FIM 71-05 TASK 803 FOR TROUBLESHOOTING. WORKED FIM 71-05 THROUGH TO BLOCK 7 WITH NO DAMAGE NOTED.N1 ROTOR SPINS FREELY IN BOTH DIRECTIONS. NO DAMAGE TO FAN CASE RUB STRIPS. FAN BLADES, INLET, 1ST STAGE LIP STATORS, AND FAN EXIT GUIDE VANES ARE IN GOOD CONDITION. EXHAUST CONE AND 6TH STAGE TURBINE BLADES HAVE NO EVIDENCE OF METAL OR DAMAGE. OPENING OF BLEED VALVE 2.5 AND 2.9 HAD NO UNUSUAL MATERIAL IN THEM. BLOCK 7 REQUIRES BORESCOPE INSPECTION. REF FIM 71-05 ENG #2 S/N P724698. ACCOMPLISHED BOROSCOPE INSPECTION REF FIM 71-05 TASK 803 BLOCK 7 & AMM TASK 72-00-00-206-001-N01, NO LIMITING DEFECTS FOUND. CONTINUED FIM 71-05 FT803 AND COMPLETED BLOCK 8 AND BLOCK 9. NO DEFECTS NOTED. BITE CHECKED PIMU AND FOUND EEC CH-A/B FMU, SVA, AND TCC TR-CK FAIL MESSAGES. PER FIM 71-01 TASK 826, MUST DO SERVO FUEL CONTAMINATION CHECK. DURING SERVO FUEL CONTAMINATION CHECK FOUND BRONZE PARTICLES IN FUEL PUMP FILTER AND FUEL COLLECTED IN REF TO FIM 71-08 FT815 BLOCK 1. REMOVED FUEL PUMP/ FMU IN REFERENCE TO TASK 73-11-01-004-001-N00 UP TO AND INCLUDING PARA G STEP K. ADD EMP:U405565 COMPLETED REMOVAL OF #2 ENG FUEL PUMP AND FMU REF AMM TASK 73-11-01-004-001-N00. ADD EMP:U383471 REQUEST CLEARANCE TO INSTALLED NEW PER AMM. INSPECTED MOUNTING SURFACE AND LINES FOR NEW FUEL PUMP AND FMU IDT APERFORMED TEST #4 REF. AMM 71-00-00-725-004-N00 ENGINE PARAMETERS ARE WITHIN LIMITS AT THIS TIME.

Part: SKIN — CRACKED (L1 DOOR CUTOUT) · airframe 125,774 hrs · 19,608 cycles

EA 5315-01152 OP001 - 1EA FASTENER HOLE FOUND CRACK ON L1 DOOR CUTOUT AFT CORNER AREA , DETAILS REFER TO ATTACHED REPORT TRANSFER REF HXWO 3270748. L1 DOOR CUTOUT AFT LOWER CORNER LH FUSELAGE SKIN INTERIM REPAIRED AS PER ECRA 5310-08353 REV - PART 1 INTERIM REPAIR ATTACHED FORM 44.0008 ITEM 1 TO ITEM 52.

Part: FRAME — CORRODED (ZONE 100) · airframe 125,774 hrs · 19,608 cycles

B767-53-3-7036 CAB - STA977 BELOW FLOOR RH S/W O/B FRAME CHORD LWR EDGE (NEAR PRESSURE DECK AREA) FOUND CORROSION . CABIN RH STA977 FRAME OUTER CHORD AT WL186 INTERIM REPAIRED AS PER ECRA5311-03241 REV - PART 1 - INTERIM REPAIR WORK DETAIL ATTACHED FORM 44.0008 ITEM 1 TO 48 ACCOMPLISHED.

Part: SKIN — CRACKED (R1 DOOR CUTOUT) · airframe 125,774 hrs · 19,608 cycles

EA 5315-01152 OP.002 - 2EA FASTENERS HOLES FOUND CRACK ON R1 DOOR CUTOUT AFT CORNER AREA , DETAIL REF TO ATTACHED REPORT , R1 DOOR CUTOUT AFT LOWER CORNER RH FUSELAGE SKIN INTERIM REPAIRED AS PER ECRA 5310-08354 REV - PART 1 INTERIM REPAIR ATTACHED FORM 44.0008 ITEM 1 TO ITEM 49 ACCOMPLISHED .

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 125,774 hrs · 19,608 cycles

B767-54-3-0008 #1 PYL PNL 436BL CUTOUT SKIN FOUND CRACKED. TRANSFER REF. NON-ROUTINE WO.3277610 NR 1 PYLON LH SKIN NO.436BL ACCESS PANEL CUTOUT PERMANENT REPAIRED AS PER EC/RA 5450-02947 REV.- ATTACHED FORM 44-0008 ITEM 1 TO ITEM 33.

Part: PRESSURE DECK — DEFORMED (BS 955 RBL 35) · airframe 125,774 hrs · 19,608 cycles

B767-53-3-7036 - CABIN STA955 TO 960 RBL35 TO 38 WHEEL WELL PRESSURE DECK WEB UPPER SURFACE FOUND DEFORMED. CABIN STA955 PRESSURE DECK WEB RBL35" DENT AREA INTERIM CREATED LP 8489125 AND 8489205 AND CARRIED REPAIRED AS PER ECRA 5350-02544 REV - ATTACHED FORM 44.0008 ITEM 1 TO ITEM 32 ACCOMPLISHED.

Part: PROBE — FAULTY (NR 1 ENGINE) · airframe 125,309 hrs · 19,546 cycles

L ENG EEC MODE EICAS ILLUMINATED AFTER ENG START ENG1 EPR INDICATION INOP IN BOTH EICAS AND STBY TRIED CYCLING OF ACCOMPLISHED TROUBLESHOOTING PER FIM 73-21 FAULKT TREE 826, EEC MODE SELECTOR SWITCH, NO HELP. ALSO TRIED ENG 1 RESTART AND FOUND P2/T2 PROBE (T867) AT FAULT PART NIS AT GIG.PN 0154ED2 AFTER ROLL BACK FOR START EEC GOES INTO ALT MODE AND EPR M&P E 76-7323-9-9003. INDICATION REMAINS INOP ADD EMP:U399390 DISCREPANCY OR MSG WERE FOUND. PERFORMED T/S IAW FIM 30-34-803 SHEET 2 BLOCK 2. FOUND CONECTOR D11434 PIN 3 OUT OF POSITION. REF WDM 30-34-11-1.1 . IT WAS REINSERTED PIN 3 IN CORRECT POSITION. ( REF SWPM 20-60 AND 20-63). PERFORMED SYSTEM TEST IAW AMM 30-34-00-715-016, START LH ENG TWICE AND RUN-UP FOR 15 MINUTES IAW AMM 71-00-00. EPR ENG INICATION OK AT EICAS & SEI, NO DISCREPANCIES AND NO MESSAGES NOTED. AIRCRAFT GOOD SERVICE.

Part: FUEL CAP — MISSING (REFUEL COUPLING) · airframe 125,361 hrs · 19,554 cycles

LEFT AND RIGHT FUEL RECEPTACLE CAPS MISSING. MEL 2821L APPROVAL REQUIRED. LEFT AND RIGHT FUEL RECEPTACLE CAPS PLACED ON MEL 2821L DDP C/W. MEL 2841L APPROVED INSTALL LEFT AND RIGHT FUEL CAPS AT REFUELING PANEL DOOR SECURE CLOSE. MEL CLOSE.

Part: TRANSDUCER — DISENGAGED (WHEEL SPEED) · airframe 124,000 hrs · 19,347 cycles

ANTISKID/AUTOBRK EICAS M THE ANTISKID/AUTOBRAKE SYSTEM BITE FOUND A FAILURE. ANTISKID INOP PER FLT CREW. ANTI SKID, NORMAL ANTISKID AND ALTERNATE ANTISKID FLAGGED SDR.. EICAS MESSAGES DISPLAYED TROUBLESHOT IAW FIM 32-42 FAULT TREE 811. FOUND #5 WHEEL SPEED TRANSDUCER CONNECTOR (D2016) NOT FULLY ENGAGED. RESECURED IAW AMM 32-42-06/401. PERFORMED WIRING CHECKS BETWEEN CONNECTORS D2016 AND D5022. ALL WIRING CHECKS AND OPS CHECKS GOOD.

Part: CEILING PANEL — DETACHED (31AB, 33AB) · airframe 123,090 hrs · 19,217 cycles

31AB CEILING FELL OFF PANEL FOUND CEILING PANEL 33AB LOOSE, REPOSITIONED CEILING PANEL REF AMM 25-22-01. ADD EMP:U395709.

Part: LAMP — DIM (L396) · airframe 122,588 hrs · 19,146 cycles

L/H WING SLIDE LIGHT L396 DIM REF HAECO NON-ROUTINE NO.9459249, ORIGINATED BY EMP V905488, SPEC NO.B767-33-3-7004 PERFORMED BY EMP V905488, IDT BY EMP V905449, REPLACED L396 L/H WING SLIDE LIGHT LAMP AND LIGHT TEST FOUND PASS AS PER AMM 33-51 -06-902-082 REV.139

Part: LIGHT — DAMAGED (L645) · airframe 122,588 hrs · 19,146 cycles

L/H WING SLIDE LIGHT L645 DIM REF HAECO NON-ROUTINE NO.9459250, ORIGINATED BY EMP V905488, SPEC NO.B767-33-3-7004 PERFORMED BY EMP V905488, IDT BY EMP V905449, PERFORMED T/S FOUN GMM 09-05-10 REV.165, SWPM 20-10-11 REV.81, AMM 33-51-06-902-082 D L645 LAMP DIM AND TW NUT DAMAGED REPLACED L645 LIGHT ASSY AND REV.139 LAMP,L645 LIGHT INSTALLATION TEST FOUND PASS AS PER FIM 33-51 FA ULT TREE 804 REV.139,SRM 51-40-02 SRM 51-40-05 REV.122

Part: LIGHT — INOPERATIVE (LH WING L645) · airframe 122,588 hrs · 19,146 cycles

L/H WING SLIDE LIGHT L645 DIM REF HAECO NON-ROUTINE NO.9459250, ORIGINATED BY EMP V905488, SPEC NO.B767-33-3-7004 PERFORMED BY EMP V905488, IDT BY EMP V905449, PERFORMED T/S FOUN GMM 09-05-10 REV.165, SWPM 20-10-11 REV.81, AMM 33-51-06-902-082 D L645 LAMP DIM AND TW NUT DAMAGED REPLACED L645 LIGHT ASSY AND REV.139 LAMP,L645 LIGHT INSTALLATION TEST FOUND PASS AS PER FIM 33-51 FA ULT TREE 804 REV.139,SRM 51-40-02 SRM 51-40-05 REV.122

Part: CONNECTOR — CRACKED (CEILING PANEL) · airframe 122,588 hrs · 19,146 cycles

CEILING EMERGENCY LIGHT CONNECTOR DAMAGE AT 32AB, 35AB, 38AB, 40 AB, 6L, 21LK, 35LK, 38LK, 41LK, 43LK - ORIGINATED BY EMP V905488 ON HAECO NR 9459198, EA 4420-03294 REV D OP001. PERFORMED BY EMP V905488, IDT BY EMP V905449, REPLACED CEILING E MERGENCY LIGHT CONNECTORS AT 32AB, 35AB, 38AB, 40AB, 6L, 21LK, 3 5LK, 38LK, 41LK, 43LK AND NEW LIGHT INSTALLATION TEST FOUND PASS , PER SWPM 20-61-28 REV 81. AMM 33-51-05-402-024 REV 139.

Part: LIGHT — DAMAGED (2A, 4A, 6A, 8 A,) · airframe 122,588 hrs · 19,146 cycles

CEILING PANEL EMERGENCY LIGHT CONNECTORS DAMAGE AT 2A, 4A, 6A, 8 A, 2L, 4L, 6L, 8L - ORIGINATED BY EMP V905488 ON HAECO NR 945919 7, EA 4420-03294 REV D OP001. PERFORMED BY EMP V905488, IDT BY TA408 V905449, REPLACED CEILING PANEL EMERGENCY LIGHT CONNECTORS AT 2A 4A 6A 8A 2L 4L 6L 8L AND THE CEILING PANEL EMERGENCY LIGHT INSTALLATION TEST FOUND PASS, PER SWPM 20-61-28 REV 81. AMM 33-51-05-402-024 REV 139.

Part: FLOOR SUPPORT — CORRODED (STA325 LBL55) · airframe 122,588 hrs · 19,146 cycles

CABIN STA325 LBL55 FLOOR BEAM SURFACE FOUND CORROSION - ORIGINAT ED BY EMP V902596 ON HAECO NR 9456640, SPEC NO.B767-06-3-7098. PERFORMED BY EMP V926739, RII BY TA447 V905036. CABIN STA 325 LB L55 FLOOR BEAM CORROSION REPAIRED AS PER SRM 53-00-51-2R-4 REV 1 22. THIS REPAIR APPROVED AS CAT A REPAIR. RII BY TA447, V905036.

Part: FLOOR SUPPORT — CORRODED (STA303 LBL20-55) · airframe 122,588 hrs · 19,146 cycles

CABIN STA303 LBL20-55 FLOOR BEAM UPPER SURFACE FOUND CORROSION - ORIGINATED BY EMP V902596 ON HAECO NR 9456655, SPEC NO.B767-06- 3-7098. PERFORMED BY EMP V926739, RII BY TA447 V905036, CABIN STA303 LBL 20-55 FLOOR BEAM UPPER SURFACE CORROSION REPAIRED AS PER SRM 53-00-51-2R-1 REV 122 & ECRA 5315-01198 REV -, THIS REPAIR APPRO VED AS PER A CAT A REPAIR. RII BY TA447, V905036.

Part: NONE — NONE (FLAP/SLAT SHUTOF) · airframe 120,299 hrs · 18,804 cycles

EVIDENCE OF HYDRAULIC LEAKAGE COMING FROM RIGHT MLG DOOR. FOUND FLAP/SLAT SHUTOFF VALVE MODULE LEAKING, THEN REMOVED FLOW REGULATOR AND ACCOMPLISHED RINGS AND PACKINGS REPLACEMENT IAW AMM 27-51-48. PERFORMED TEST ON THE FLAP/SLAT SHUTOFF VALVE MODULE IAW AMM 27-51-48-712-074.ALL CHECKS GOOD, NO LEAKAGE NOTED.

Part: PACKING — DAMAGED (GIG) · airframe 119,582 hrs · 18,716 cycles

LH MAIN LANDIG GEAR STRUT CYILINDER HYDRAULIC LEAKING. CONFIRMED. LH M.L.G SHOCK STRUT COLLAPSED ACCOMPLISHED ACTIVE SEAL REPLACEMENT WITH SPARE SEALS I.A.W AMM 32-11-25-962-342. NO LEAK NOTED.

Part: PUMP — INOPERATIVE (RT AFT FUEL PMP) · airframe 119,366 hrs · 18,689 cycles

AFTER RT ENGINE START RT AFT FUEL PUMP EICAS MESSAGE AND SWITCH LT INDICATIONS PRV RTUP REQUIRED MEL APPROVAL REF 2822N RIGHT AFTER FUEL PUMP PLACED ON MEL.REMOVED AND REPLACED RIGHT AFT FUEL BOOST PUMP. OPS TEST NORMAL.VERIFIED RIGHT AFT FUEL BOOST PUMP INSTALLED.

Part: SKIN — MISSING (ENG2 NOSE COWL) · airframe 117,796 hrs · 18,449 cycles

PDA 1 ENGINE 2 NOSE COWL HAS A 19"X12" (228 SQUARE INCHES) PIECE OF THE EXTERNAL HONEYCOMB SKIN MISSING AT APPROXIMATELY THE 2 O''CLOCK POSITION. A/C ARRIVED IN IAH FROM ORD, FLIGHT 2675 IN THIS CONDITION. PERFORMED A VISUAL CHECK AND COULD NOT LOCATE MISSING PIECE. PERFORMED VISUAL INSPECTION OF AFFECTED AREA AND LOWER WING AREA AND FLIGHT CONTROLS. REFERENCE LOGPAGE 7898070 FOR CORRECTIVE ACTION ON ENG.#2 NOSE COWLING. OK TO CONTINUE.

Part: MODULE — FAILED (HYD SYSTEM) · airframe 116,250 hrs · 18,134 cycles

C HYD QTY LIGHT CAME ON. QTY AT .47 ACFT ARRIVED AT GATE WITH CENTER HYDRAULIC QUANTITY READING 0.36. NOTICED HYDRAULIC FLUID DRIPPING FROM R/H WHEEL WELL DOOR WEEP HOLE. PICTURES ATTACHED FOUND FLAP AND SLAT HYDRAULIC S/O VALVE MODULE FLOW REGULATOR LEAKING AND BUSTED OUT. PER AMM 27-51-48-022-001 AND 27-51-48-422-036 WILL REQUIRE REMOVED AND REPLACED FLAP AND SLAT HYDRAULIC S/O VALVE MODULE BONDING CHECK PER INSTALL AMM 27-1-48-422-036 AND OPS CHECK AND LEAK PER AMM 51-48-712-074 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1126132 SN OFF 9022 MODULE, FLAP & OFF 76-2753-9-0003 9022 ON 76-2753-9-0003 9021 ACCOMPLISHED THE BONDING CHECK WITH NO DEFECTS. PERFORMED LEAK AND OPS CHECK NO LEAKS NOTED. OPS CHECKS GOOD. REF AMM 27-51-48-422-036 AND AMM 27-51-48-712-074. ALL CHECKS GOOD CENTER SYS SERVICED TO FULL. ADD EMP:U342887

Part: FUSE — INTERMITTENT (RT MLG) · airframe 115,607 hrs · 18,016 cycles

ON TAKEOFF WHEN THE GEAR HANDLE WAS THE GEAR DOORS EICAS AND GEAR DISAGREE DISPLAYED, THE RIGHT MLG DID NOT INDICATE RETRACTED. CREW RAN CHECKLIST PERFORMED PSEU BITE & FOUND FAULT 264 ''R LATCH LOCKED''. PERFORMED PROXIMITY SENSOR LATCH LOCKED SENSOR TEST. TEST SATISFACTORY. REF AMM 32-61-02-702-018. REQUIRES FURTHER T/S REF FIM TASK 32-30 FAULT TREE 817. WITH LANDING GEAR HANDLE "UP", RIGHT GEAR GREEN LIGHT, AMBER GEAR & DOOR LIGHT REMAINED ILLUMINATED. T/S PER FIM 32-30 FAULT TREE 820, SHEET 4 (BLOCK 6) MANUALLY PULLED ON SIDE BRACE ACTUATOR AND THE ROD END MOVED. SHEET 5 (BLOCK 7) SIDE BRACE ACTUATOR FAILED TO RETRACT. SIDE BRACE ACTUATOR NIS GUM. ADD EMP:U241927,U230826 FOUND R/H MLG SIDE BRACE ACTUATOR INOP. SEE L/P 6303898 FOR R/R AND OPS LEAK CK. FOUND HYD FLOW FUSE FOR THE R/H GEAR RETRACT LINE INOP. R/R FLOW FUSE. SEE L/P 6307394, 6307385 FOR R/R OPS AND LEAK CK. PERFORMED AMM TASK 32-32-00-705-001. OPERATIONAL TEST- MAIN GEAR EXTENSION AND RETRACTION SYSTEM. OPS LEAK CK AND ADD EMP:U192746,U218615,U240002 INDICATION PASSED NO FAULTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 114,165 hrs · 17,730 cycles

GENERATING ITEM: 63-3310-1-7300 /// WHEN DOING THE TEST FOR EMERGENCY LIGHTS FROM F/A PANEL THE FIRST 3 ROWS IN FIRST CLASS, THE LIGHTS UNDER OVERWING EXITS AND THE LIGHT STRIP IN FLOOR ARE INOP REF AMES NR 0033. BATTERY PACKS M1209 AND M9047 WERE REMOVED, REPLACED AND TESTED GOOD IAW B767 AMM 33-51-07. EMERGENCY LIGHT TEST GOOD IAW B767 AMM 33-51-00-705-029-0011. INSPCTED BY AMES INSPECTOR 56.

Part: STIFFENER — CRACKED (RT WING) · airframe 114,165 hrs · 17,730 cycles

GENERATING ITEM: 63-0600-1-2338 /// B767-06-3-7171: R/W L/E SPAR WEB VERTICAL STIFFENER IS CRACKED AT WS. 524, #8 SLAT AREA[M] REF AMES NR 0356. FABRICATED AND REPLACED STIFFNER PN 112T2252-1 UAL ON RW LE SPAR WS 524 IAW UNITED ECRA # 5720-03176 AND AMES R EA 47402FAB01. LEAK CHECK FOR WORKED AREA TO BE ACCOMPLISHED ON NR 0721.

Part: PANEL — MISSING (LT WING) · airframe 113,573 hrs · 17,640 cycles

PDA 1 WHEN A/C ARRIVED EWR FOUND DOOR 521ABB ON LEFT WING DEPARTED FROM A/C. REF IPC 57-41-10-10 IT 372. REF T64-0620-1-0067. PERFORMED GMM 02-30-95 TOMC NOTIFIED AS REQUIRED. INSPECTED AREA OF MISSING DOOR/PANEL NO OTHER DEFECTS NOTED AT THIS TIME. DOOR/ PANEL REPLACED PER IPC 57-41-10-10 NEW HARDWARE INSTALLED. OK TO CONTINUE AT THIS TIME.

Part: PANEL — MISSING (LT WING) · airframe 113,573 hrs · 17,640 cycles

PDA 1 WHEN A/C ARRIVED EWR FOUND DOOR 521ABB ON LEFT WING DEPARTED FROM A/C. REF IPC 57-41-10-10 IT 372. REF T64-0620-1-0067. PERFORMED GMM 02-30-95 TOMC NOTIFIED AS REQUIRED. INSPECTED AREA OF MISSING DOOR/PANEL NO OTHER DEFECTS NOTED AT THIS TIME. DOOR/ PANEL REPLACED PER IPC 57-41-10-10 NEW HARDWARE INSTALLED. OK TO CONTINUE AT THIS TIME.

Part: PANEL — MISSING (LT WING) · airframe 113,573 hrs · 17,640 cycles

PDA 1 WHEN A/C ARRIVED EWR FOUND DOOR 521ABB ON LEFT WING DEPARTED FROM A/C. REF IPC 57-41-10-10 IT 372. REF T64-0620-1-0067. PERFORMED GMM 02-30-95 TOMC NOTIFIED AS REQUIRED. INSPECTED AREA OF MISSING DOOR/PANEL NO OTHER DEFECTS NOTED AT THIS TIME. DOOR/ PANEL REPLACED PER IPC 57-41-10-10 NEW HARDWARE INSTALLED. OK TO CONTINUE AT THIS TIME.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 111,002 hrs · 17,293 cycles

AT FL360 NOTICED RIGHT ENGINE INDCATIONS WERE AT REDUCED POWER. EPR 1.03 AND FF 3.3 REF LOG PAGES 3371080 AND 3371024, RIGHT ENG FUEL PUMP, FMU AND EEC REPLACED REF APPLICABLE MM''S REFERENCED IN EACH LOG PAGE. ACP''D POWERPLANT TESTS 2, 3, 4 AND 15. ALL TESTS GOOD. ACCELERATION/DECEL TEST PARAMETERS ALL WITHIN LIMITS AND MATCH LEFT ENGINE. VERIFIED ENGINE WOULD MAKE TAKEOFF POWER. WITHIN LIMITS. CALCULATED MAX EPR 1.52, RAN ENGINE TO 1.48 EPR, ALL PARAMETERS

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 107,329 hrs · 16,627 cycles

AFTER RAISING LDG GEAR FOR TAKEOFF EICAS MSSG GEAR DISAGREE MSG APPEARED. ACCOMPLISHED GEAR PROX SENSOR TEST WRT AMM32-61-99-706-113. ACCOMPLISHED HEALTH CHECK WITH A/C ON GROUND AND FOUND SENSOR S238 FAILED RESISTANCE CHECK. RPLD S238 WRT AMM TASK 32-61-02 AND TESTED NORMAL. ALSO ADJ SENSORS S236 & S258 GAPS (L SIDE BRACE) AND GAPS ON S240 & S262 (R SIDE BRACE). OPERATED GEAR DOORS THROUGH SEVEARL CYCLES AND ALL INDICATIONS APPEARED NORMAL PSEU BITE SHOWED PREVIOUS FAULTS OF S238, S260 AND S258. FAULTS NOW CLEARED AND PSEU TESTED NORMALLY WRT AMM 32-09-03.

Part: SEAT TRACK — CRACKED (BS 756-818) · airframe 108,533 hrs · 16,964 cycles

RBL 11, SEAT TRACK FOUND CRACKED AT BS 756 - 818. REPAIRED IAW SRM 53-00-51, REPAIR 3, FIG 201.

Part: FLOORBEAM — CORRODED (BS 347) · airframe 108,533 hrs · 16,964 cycles

BS 347, RBL 30, FLOORBEAM WAS FOUND CORRODED. THE FLOORBEAM WAS REPAIRED IAWSRM 53 -00-51, REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 1528) · airframe 108,533 hrs · 16,964 cycles

BS 1518, BL 0 FLOORBEAM WAS FOUND CORRODED. THE FLOORBEAM WAS REPAIRED IAW SRM 5 3-00-51, REPAIR 1, FIG 201.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 107,049 hrs · 16,758 cycles

LENS MISSING FOR THE CEILING EMERGENCY LIGHT AT 29B. REPLACED THE LENS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,988 hrs · 16,746 cycles

INTERIOR OVERHEAD EMERGENCY LIGHTS AT SEATS 35J, 6B, AND 6J ARE INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 106,988 hrs · 16,746 cycles

EXTERIOR EMERGENCY EXIT LIGHT AT THE L1 DOOR WAS INOPERATIVE. REPLACED THE BATTERY AND POWER SUPPLY IAW 33-51-07-002-014-002

Part: LIGHT — INOPERATIVE (RT WING) · airframe 103,487 hrs · 16,220 cycles

RIGHT WING TRAILING EDGE OVAL EMERGENCY LIGHT HAS ONE LAMP OF TWO OUT. REMOVED AND REPLACED THE LIGHT ASSY IAW SRM 51-010-02, PARA 7, FIG 12. OPS CHECKED GOOD.

Part: STRINGER — CRACKED (BS 1543) · airframe 103,488 hrs · 16,220 cycles

DURING REMOVAL OF A BRACKET AT BS 1543, STRINGER 33R, FOUND STRINGER 33R CRACKED AT BRACKET. REPAIRED THE STRINGER IAW SRM 53-00-03, PG 201, FIG 201, REPAIR 2.

Part: FLOORBEAM — CORRODED (BS 289) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 289, RBL 68 IN MAIN CABIN. REMOVED THE CORRODED SECTION FROM UPPER SURFACE OF THE FLOORBEAM. FABRICATED A NEW TEE, SPLICES AND SHIMS AND INSTALLED IAW SRM 53-00-51, FIG 201, REPAIR 1.

Part: SHEAR TIE — CORRODED (BS 1329) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON SHEAR TIE AT BS 1329, LBL 33 IN THE AFT CARGO BAY. REMOVED AND REPLACED THE SHEAR TIE IAW 51-40-02, P4, F3.

Part: INTERCOSTAL — CORRODED (BS 1582) · airframe 103,488 hrs · 16,220 cycles

CORROSION AROUND AFT LAVATORY PAN AREA IN AFT CARGO BAY BS 1582, STRINGERS 38L - 38R. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL BS 1562 - 1582 RBL 10 IAW B767-300 SRM 51-40-02 PARA 7D

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 103,488 hrs · 16,220 cycles

CORROSION IN AFT CARGO BELOW FLOOR BOARD FRAME TO SKIN SHEAR TIE AT STA 1395 BL0 REMOVED CORROSION. FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SHEAR TIE BETWEEN STR 39R - 38L BS1395 IAW SRM 51-40- 02 PARA 4 FIG 8 & 3, AND PARA 7D FIG 12, AND SRM 51-10-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 103,488 hrs · 16,220 cycles

BACK SIDE OF FRAME 1540 SHEAR TIE BETWEEN STRINGERS 39L AND 38L HAS CORROSION. REMOVED & REPLACED SHEAR TIE AT STA 1540 BETWEEN STRINGERS 39L AN D 38L IAW SRM 51-40-02 PARA 4 & 7D FIG 3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 103,488 hrs · 16,220 cycles

BACKSIDE OF FRAME 1540 SHEAR TIE BETWEEN 38R AND 39R STRINGERS HAS CORROSION AFT OF BULK CARGO. REMOVED & REPLACED SHEAR TIE AT STA 1540 BETWEEN STRINGERS 38R & 39R IAW SRM 51-40-02 PARA 4 & 7D FIG 3.

Part: SKIN — GOUGED (FUSELAGE) · airframe 103,488 hrs · 16,220 cycles

FUSELAGE EXTERIOR SKIN BS 390 ABOVE STR 33L HAS GOUGE IN SKIN REPAIRED FUSELAGE EXTERNAL SKIN AT BS 390 ABOVE STR33L IAW SRM 53-00-01 REPAIR 29 FIG 201. REPAIR IS A CAT B REPAIR + REQUIRES NDT INSPECTION AT CRITICAL ROW FASTENERS AT 37,500 FLC PER TABLE V.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON BS 955 BL0 AFT CHORD REPAIRED BS 955 BL 0 AFT CHORD ATTACH ANGLE IAW ECRA 5310-07108.

Part: FLOORBEAM — CORRODED (BS 289) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON FLOORBEAM UPPER SURFACE AT BS 289, RBL 16. REMOVED THE CORROSION, AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-51, FIG 201, AND SRM 51-40-02, ORIGINAL.

Part: FRAME — CORRODED (BS 1197) · airframe 103,488 hrs · 16,220 cycles

AFT CARGO BAY FRAME BS 1197+22 HAS DEEP CORROSION. REMOVED CORROSION IAW SRM 51-10-02, REMOVED AND REPLACED THE TEE CAP IAW SRM 51-40-02, PAR 7, FIG 9, PAR 4, FIG 8.4.

Part: FRAME — CORRODED (BS 1351) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON FRAME UNDER TEE CAP AT BS 1351, RBL 31. FOUND TO BE OUT OF LIMITS AND REPLACED IAW SRM 51-40-02, PAR 7 & 4, FIG 4-12-8.

Part: GUARD — CORRODED (BS 289) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON R1 DOOR SPLASH GUARD BS 289, RBL 68. REMOVED & REPLACED THE SPLASH GUARD IAW SRM 51-4 0-02, PAR 7D.

Part: FRAME — CORRODED (BS 1197) · airframe 103,488 hrs · 16,220 cycles

AFT CARGO BAY, BS 1197+88 HAS DEEP CORROSION UNDER TEE CAP. REMOVED CORROSION IAW SRM 51-10-02, REMOVED AND REPLACED THE TEE CAP IAW SRM 51-40-02, PAR 7, & FIG 12 PAR 4 FIG 8+4.

Part: STIFFENER — CORRODED (BS 1260) · airframe 103,488 hrs · 16,220 cycles

AFT CARGO BAY STIFFENER AT BS 1260 HAS CORROSION. REMOVED AND REPLACED THE STIFFENER IAW 51-40-02 (4).

Part: FLOORBEAM — CORRODED (BS 1219) · airframe 103,488 hrs · 16,220 cycles

AFT CARGO BAY FLOORBEAM BS 1219, RBL 26 HAD ONE NUT PLATE CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02, 5, A, 4.

Part: TEE FITTING — CORRODED (BS 1329) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON UNDERSIDE OF THE TEE FITTING AT BS 1329, RBL 26. REPLACED THE TEE FITTING IAW SRM 51-40-02, PAR 7, FIG 12, PARAGRAPH 14.

Part: SHEAR TIE — CORRODED (BS 1540) · airframe 103,488 hrs · 16,220 cycles

BS 1540 SHEAR TIE BETWEEN STRINGERS 39L AND 39R CORRODED. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-40-02, PARA 4 & 7D, FIG 3.

Part: STRINGER — CORRODED (BS 1562) · airframe 103,488 hrs · 16,220 cycles

BS 1562, STRINGER 39R CORRODED, FOUND TO BE OUT OF LIMITS. REPAIRED THE STRINGER IAW SRM 53-00-53, FIG 201, REPAIR 2.

Part: STRINGER — CORRODED (BS 1562) · airframe 103,488 hrs · 16,220 cycles

AFT OF BULK CARGO FORWARD OF BS 1562 ON STRINGER 39L CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED THE STRINGER IAW SRM 53-00-53, FIG 201, REPAIR 2.

Part: SHEAR TIE — CORRODED (BS 1540) · airframe 103,488 hrs · 16,220 cycles

BS 1540 SHEAR TIE BETWEEN STRINGERS 36 AND 37R CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02, PARA 4 & 7D, FIG 3.

Part: ANGLE — CORRODED (BS 1395) · airframe 103,488 hrs · 16,220 cycles

CORROSION ON ANGLE AT BS 1395. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE ANGLE IAW SRM 51-10 -02 PARA 15, SRM 51-40-02 PARA. 4 FIG 3 & 8, AND PARA. 7D FIG 12

Part: ANGLE — CORRODED (BS 1395) · airframe 103,488 hrs · 16,220 cycles

CORROSION IN AFT CARGO BELOW FLOOR BOARD ON STR 39L OUTBD ANGLE AT STA 1395 LBL4 REMOVED CORROSION; FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED ANGLE OTBDSIDE OF STR 39L BS1395 LBL4 IAW B767-300 SRM 51-10- 02 PARA 15, SRM 51-40-02 PARA 4 FIG 3&8, AND PARA 7D FIG 12;

Part: STIFFENER — CRACKED (NLG WW) · airframe 103,488 hrs · 16,220 cycles

NOSE WHEEL WELL VERTICAL STIFFENER CRACKED. REPAIRED IAW SRM 51-70-12.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 103,214 hrs · 16,181 cycles

EMERGENCY EXIT WINDOW LIGHTS ON BOTH SIDES WHERE ON FOR ABOUT 45 AFTER T/O INTERMITTENT NORMAL OPS AFTER POWER SHUTDOWN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 102,588 hrs · 16,091 cycles

FWD GALLEY CROSS AILSE EMERGECY LIGHT IS INOPERATIVE. SECURED THE LAMP AND OP CHECKED OK IAW AMM33-51-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 99,792 hrs · 15,709 cycles

EPL AT SEATS 19 - 22 RT INOPERATIVE. R & R BATTERY PACK & POWER SUPPLY UNIT, POSITION M1209 IAW AMM 33-51-07. PERFORMED EMER LIGHTS TEST, EPL SEATS 19 - 22 RT IAW AMM 33-51-07, FOUND NORMAL.

Part: LUG — UNSECURE (CABIN) · airframe 99,445 hrs · 15,654 cycles

TOP FWD EMER EXIT SIGN INOPERATIVE AT DOOR 2 LT. SECURED CONTACT LUG BEHIND SIGN. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 99,445 hrs · 15,654 cycles

EMERGENCY EXIT FLOOR EMER EXIT LIGHT INOPERATIVE, JUST FWD OF SEAT 1K. SECURED BATTERY CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 99,445 hrs · 15,654 cycles

LOWER FWD EMER EXIT SIGN INOPERATIVE AT DOOR 1 RT. SECURED BATTERY CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 99,445 hrs · 15,654 cycles

SEAT MOUNTED EMER EXIT LIGHTS INOPERATIVE FROM SEAT ROWS 34 LT - 39 LT. REPLACED BATTERY AT M739 IAW SSM 33-51-01. LIGHTS OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 98,341 hrs · 15,501 cycles

EXTERIOR EMER EXIT LIGHT INOPERATIVE AT DOOR 1 RT, RELAMPED. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,341 hrs · 15,501 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT LT CEILING ROW 24, RELAMPED. OPERATIONS CHECKED NORMAL.

Part: SWITCH — DEFECTIVE (CABIN) · airframe 95,279 hrs · 15,081 cycles

GUARDED EMER LIGHT SWITCH ON P22 AFT ATTENDANTS PANEL, WHEN PUSHED TO ON POSITION DOES NOT ILLUMINATE EMER LIGHTS. WITHIN LIMITS IAW SRM 52-30-01 ALLOWABLE DAMAGE 1. ACCOMPLISHED JFEC IAW PART 6 51-00-00 PROCEDURE 23. NO CRACKS NOTED. HFEC INSPECTION REQUIRED EVER 1500 FLIGHT CYCLES. ACCOMPLISH DENT DOT PROCEDURE.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 95,279 hrs · 15,081 cycles

REF A CHECK J C 6-2006-A ITEM 2C 3 GUARDED EMER LIGHT SWITCH ON P22 AFT ATTENDANTS PANEL WHEN PUSHED TO ON POSITION DOES NOT ILLUMINATE EMER LIGHTS. FOUND WIRE W1224-087-22 INSTALLED IN WRONG LOCATION OF CONNECTOR D4290P IAW WDM 33-27-11 PG 2A SHEET 4. WIRE SHOULD BE TERMINATED AT PIN 49, BUT IS CURRENTLY IN POSITION 39. RELOCATE WIRE TO CORRECT POSITION IAW WDM. REMOVED WIRE W1224-087-22 FROM POS 39 & REINSTALLED INTO POSITION 49 OF CONNECTOR D4290 P IAW WDM 33-27-11. OPERATIONS NORMAL IAW MM 33-51-00.

Part: CONTACT — DIRTY (EXIT SIGN) · airframe 94,761 hrs · 15,012 cycles

RIGHT WING OVERWING DOOR CEILING EMER SIGN INOPERATIVE. REPLACED RT OVERHEAD EMER EXIT SIGN POWER SUPPLY IAW IPC 33-57-07 & WDM 33 51-12. AFTER REPLACED SIGN WAS INTERMITTENT, CLEANED TERMINAL CONTACTS ON EMER EXIT SIGN L1050. OPERATIONS CHECKED GOOD.

Part: LENS — DAMAGED (CABIN) · airframe 93,876 hrs · 14,885 cycles

SEAT 6B EMER LIGHT DAMAGED. REPLACED DAMAGED LENS COVER & ACP EMER LIGHT OPERATION TEST IAW MM33-51-00-501.

Part: HYDRAULIC SYSTEM — LEAKING (PYLON) · airframe 93,006 hrs · 14,767 cycles

DIVERT TO LHR DUE TO LOSS ON RT HYD SYS. UPON ARRIVAL MX CONFIRMED LEAK ON ENG PYLON.

Part: PRESSURE SWITCH — LEAKING (HYDRAULIC SYS) · airframe 93,006 hrs · 14,767 cycles

CREW REPORT, RT SYS HYD QTY WENT TO .46. RAN QRH 130.2, RT SYS PUMPS OFF TILL APPROACH. FOUND LEAK FROM EDP PRESS FILTER DELTA P SWITCH. REPLACED SWITCH ASSEMBLY IAW MM 29-11-17 & LEAK CHECKED NORMAL. SYS SERVICED IAW MM 12-12-01. NOTE, AT NO TIME DID LOW PRESS LIGHTS ILLUMINATE & SYS DID NOT RUN DRY.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 92,663 hrs · 14,718 cycles

EMERGENCY EXIT LIGHTS RANDOMLY FLICKERING OVER THREE WINDOW EXITS & SOME SEAT MOUNTED REDS. INTERIOR EMERGENCY LIGHTS VERIFIED IAW FIM TASK 33-51-00, ALL LIGHTS CHECKED OK. NO FLICKERING NOTED ON ALL EXIT WINDOWS LIGHTS DURING ALL GND TRANSIT WITH CONTROL SWITCH ON ARMED POSITION. UNABLE TO DUPLICATE DISCREPANCY ON GND, OPERATIONS OK.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 92,150 hrs · 14,650 cycles

ON ARRIVAL RAMP REPORTED DAMAGE TO FWD CARGO PIT FLOOR BOARD AT APPROXIMATELY STATION 650.

Part: ANTI-ICE VALVE — FAULTY (NR 1 ENGINE) · airframe 92,143 hrs · 14,649 cycles

NR 1 ENG WHEN TAI IS SELECTED ON, VLV OPENS FOLLOWED BY INCREASE IN EGT. WHEN SELECTED OFF, EGT ROLLS BACK EICAS MESSAGE LT ENG ANTI ICE, WITH VLV LIGHT ILLUMINATED IN SWITCH. REPLACED NR 1 ENG ANTI ICE VLV IAW 30-21-03 UP TO PG 405 STEP 11. NEED TO CONT FROM STEP 11 TO END. ACCOMPLISHED ANTI ICE CHECK IAW MM 30-21-03, CHECKED OK.

Part: ANTI-ICE VALVE — FAULTY (NR 1 ENGINE) · airframe 92,143 hrs · 14,649 cycles

WHEN SELECTING RT ENG ANTI ICE EICAS MESSAGE WITH VLV LIGHT ILLUMINATED IN SWITCH. REMOVED RT ENG ANTI ICE VLV & REPLACED NR 1 ENG ANTI ICE VLV IAW 30-21-03 UP TO PG 405 STEP 11. NEED TO CONT FROM STEP 11 TO END.

Part: BRAKE — FAULTY (MLG) · airframe 91,952 hrs · 14,626 cycles

NR 1 FWD BRAKE PIN IS 1-16". CURRENT PTC IS 14625 MUST BE REPLACED ON OR BEFORE PTC 14627. BRAKE PCN 160-9740. R & R NR 1 MLG BRAKE ASSEMBLY.

Part: PRESSURE SWITCH — FAULTY (RT ENGINE) · airframe 91,775 hrs · 14,603 cycles

RT ENG AIV STATUS MESSAGE. REPLACED R ENG THERMAL AIV PSI SWITCH IAW FIM 30-21-00-PG107.

Part: LIGHT — INOPERATIVE (ANTI-ICE VALVE) · airframe 91,775 hrs · 14,603 cycles

NR 2 ENG ANTI ICE VLV LIGHT INOPERATIVE. ANTI ICE VLV LOCKED OPEN, HPSOV LOCKED CLOSED, HMG LOCKED CLOSED IAW MELN 3021H.

Part: ACTUATOR — FAULTY (RT AILERON) · airframe 91,773 hrs · 14,602 cycles

RT INBD AILERON ACTUATOR BAD FOUND DURING TEST FLIGHT. R & R RT INBD ACTUATOR ON NR 36599 IAW AMM 27-11-48 & SRM 51-40-02.

Part: ACTUATOR — FAULTY (NR 6 SPOILER) · airframe 91,773 hrs · 14,602 cycles

NR 6 SPOILER FLOATED DURING TEST FLIGHT. R & R SPOILER ACTUATOR IAW AMM 27-61-02 ON NR 36598.

Part: ACTUATOR — FAULTY (AILERONS) · airframe 91,770 hrs · 14,601 cycles

DURING PREFLIGHT CHECK, AILERON TRIM ASYMMETRIC GOES FROM 6.6 LT TO 4.2 RT, SHOULD BE 5.6 + OR .3 BOTH SIDES. R & R LATERAL TRIM ACTUATOR IAW AMM, AILERON TRIM FUNCTIONS IAW 27-11-00.

Part: SIGN — DISCONNECTED (CABIN) · airframe 91,770 hrs · 14,601 cycles

OVERWING EMERGENCY EXIT SIGNS NOT PROPERLY CONNECTED. RE-CONNECTED OVERWING EXIT SIGNS IAW AMM, OPERATIONS CHECKED GOOD.

Part: WIRE — OUT OF POSITION (COCKPIT) · airframe 91,770 hrs · 14,601 cycles

EMERGENCY LIGHTS ACTIVATED WITH COCKPIT SWITCH IN OFF POSITION. SWAPPED CONNECTOR D4209P, CORRECTED WIRING IAW 767 WDM 33-51-11, OPERATIONS CHECKED GOOD.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,770 hrs · 14,601 cycles

AFT CARGO COMPARTMENT BILGE FRAME T CAP CORRODED TOP SURFACE BS1153, STRINGER 32L -STRINGER 32R. REPLACED UPPER T CAP AT BS 1153, STRINGER 32L-3 2R IAW WITH SRM 53-00-07 & 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,770 hrs · 14,601 cycles

AFT CARGO COMPARTMENT BILGE FRAME T CAP CORRODED TOP SURFACE BS 1175, STRINGER 32L - STRINGER 32R. R & R T CAP AT BS 1175, STRINGER 32L - 32R IAW SRM 53-00-07 & 51-40-02.

Part: STRINGER — DENTED (FUSELAGE) · airframe 91,770 hrs · 14,601 cycles

AFT PIT STRINGER 39L IS DENTED AT BS 1450. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED ONE EACH STRINGER SECTION IAW BAC DRAWING 146T30 03, TWO EACH 6 CHANNELS & TWO EACH 7 ANGLES & INSTALLED IAW SRM 53-00-03, REPAIR 2, DETAIL IV ON NON-ROUTINE 36048.

Part: SPAR — ABNORMAL (NR 1 PYLON) · airframe 91,770 hrs · 14,601 cycles

NR 1 PYLON FWD UPPER SPAR WEB INBD & OTBD DRAIN HOLES HAVE PREVIOUS REPAIRS. THE EXISTING REPAIR WAS REMOVED AT NAC STATION 156, & THE LT DRAIN HOLE WAS FOUND CRACKED PAST THE PREVIOUS STOP DRILLS. A NEW REPAIR WAS INSTALLED IAW REO G16676, REV A & SRM 54-53-01 R10, REPAIR C & ECRA 545-02105.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,770 hrs · 14,601 cycles

MAIN CABIN FLOOR BEAM CORRODED UPPER SURFACE BS 1562, LBL 11- LBL 13. REPAIRED FLOOR BEAM IAW SRM 53-00-51 REPAIR 2 FIG 201.

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 91,770 hrs · 14,601 cycles

NR 2 PYLON UPPER SPAR WEB AT NAC STATION 156, BOTH DRAIN HOLES ARE CRACKED. REPAIRED THE UPPER SPAR WEB IAW REO G16606, REV A & ECRA 5450-02099 INCORPORATING TWO MACHINED DOUBLERS & TWO RADIUS FILLERS IAW NOTE B OF SRM 54-53-01, REPAIR 10.

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 91,770 hrs · 14,601 cycles

MAIN CABIN FLOORBEAM BS 347, RBL 54, HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION. CUTOUT DAMAGED SECTION OF TEE, FABRICATED & INSTALLED A THREE STRAP REPAIR & SHIMS IAW SRM 53-00-51, REPAIR 4.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 91,770 hrs · 14,601 cycles

STATION 246 LOWER FLOOR BEAM WEB CRACKED AT RBL 15. REPAIR AT STATION 246 LOWER FLOOR BEAM WEB PTT SEQ.# 7702072.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 91,770 hrs · 14,601 cycles

STATION 246 FLOORBEAM AT RBL 42 LOWER CHORD & WEB HAS 3/8TH DIAMETER HOLE. TRIMMED OUT HOLE, ACP HFEC IAW PRT 6, 51-00-19, NO CRACKS NOTED. INSTALLED FREEZE PLUG IAW ECRA 5310-05867 & TIMCO REO G16665.

Part: FLOORBEAM — CRACKED (BS 246) · airframe 91,770 hrs · 14,601 cycles

BS 246 LOWER FLOORBEAM WEB CRACKED AT RBL 15. REPAIRED FLOORBEAM IAW ECRA 5310-05868.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,770 hrs · 14,601 cycles

MAIN CABIN FLOORBEAM T-CAP CORRODED AT BS 300 & BETWEEN RBL 45 TO RBL 54.5. REMOVED DAMAGED SECTION OF FLOORBEAM T-CAP, FABRICATED & INSTALLED -1, -2 REPAIR ANGLE S, -3 REPAIR STRAP, 5 EA SHIMS, -13, -14 VERT STIFFENERS, & -63, -64 CLIPS IAW SRM 53-00-51, RPR. 4 & 51-40-2, IAW SRM 53-00-51, RPR 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,770 hrs · 14,601 cycles

MAIN CABIN FLOOR BEAM T-CAP CORRODED APPROXIMATELY BS 325, RBL 45.0-RBL 54.5. REPAIRED FLOOR BEAM IAW SRM 53-00-51, RPR 4, DET I.

Part: A/C PACK — INOPERATIVE (LEFT) · airframe 91,704 hrs · 14,592 cycles

LEFT A/C PACK INOPERATIVE. PERFORMED BITE ON BOTH PACK TEMP CONTROLLERS, NO FAULTS NOTED.

Part: BLADE — BENT (NR 2 ENGINE) · airframe 91,655 hrs · 14,586 cycles

NR 2 ENGINE HAS ONE FAN BLADE WITH L/E TIP BENT. REMOVED .25 CURL FROM FWD L/E TIP AT AREA "A". REMOVED AN ADDITIONAL .020 MATERIAL AFTER EDDY CURRENT INSPECTION.

Part: SWITCH — FAILED (ALTITUDE CONTROL) · airframe 91,586 hrs · 14,577 cycles

EICAS MESSAGE LT PACK AND RT PACK SHOWED IN COCKPIT. BIT ON PACK CONTROLLERS SHOWED ALTITUDE SWITCH. R & R ALTITUDE SWITCH IAW AMM.

Part: CIRCUIT CARD — INTERMITTENT (BLEED CONTROL) · airframe 91,497 hrs · 14,563 cycles

RT BLD DUCT LEAK EICAS AND BLEED DUCT LEAK ON OVERHEAD PANEL. OCCURRED WITH NO AIR AT NR 2 ENGINE. INTERMITTENT INDICATION. REPLACED BLEED AIR CONTROL CARD M860, ACCOMPLISHED DUCT LEAK TEST, TEST NORMAL.

Part: CONTROL UNIT — FAILED (APU) · airframe 91,394 hrs · 14,550 cycles

APU FAILED TWICE AT GATE BEFORE PUSHBACK. R & R ECU IAW AMM, OPS CHECKED GOOD.

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 91,371 hrs · 14,547 cycles

LEFT OVER AISLE EMERGENCY EXIT SIGN LENS DOES NOT HAVE OTBD FACING ARROWS IAW EA 3351-01054, REV "A". REPLACED LENS.

Part: CABLE — DAMAGED (COCKPIT SEAT) · airframe 91,199 hrs · 14,525 cycles

FIRST OBSERVER SEAT DIAG SLIDE LEVER INOPERATIVE. FOUND ACTUATION CABLE DAMAGED, MOVED SEAT TO MOST AFT POSITION. SEAT REPLACED. LUBED AND OPS CHECKED GOOD. POSITIVE LOCK IN ALL POSITIONS AND POSITIVE MOVEMENT WITH ALL CONTROLS.

Part: CONTROL UNIT — FAULTY (HYD SYSTEM) · airframe 91,174 hrs · 14,522 cycles

RIGHT ENGINE HYDRAULIC ELEC DEMAND PUMP LOW PRESSURE & SYS PRESSURE LIGHTS ON WITH SWITCH ON. TROUBLESHOT IAW FIM 29-11, FIG 105 29-11-00-990-806 TO RT ELCU M896. SWAPPED ELCU WITH ELC HYD PUMP C2 POSN VERIFIED FAULT WENT TO C2 PUMP. R & R C2 ELCU WITH NEW ELCU IAW AMM. OPS CHECK OF BOTH THE ACMP RT AND ELC HYD PUMP C2 BOTH OPS OK IAW AMM.

Part: DRIVE UNIT — FAILED (RT GENERATOR) · airframe 91,135 hrs · 14,517 cycles

RT GENERATOR DRIVE LIGHT NOT ILLUMINATED. ALSO, RT GENERATOR FIELD LIGHT NOT ILLUMINATED. REPLACED RT GENERATOR DRIVE AND RT GENERATOR FIELD PUSH BUTTON SWITCHES. OPS CHECKED GOOD.

Part: COVER — DAMAGED (R1 DOOR SLIDE) · airframe 91,048 hrs · 14,505 cycles

R1 DOOR SLIDE RAFT COVER DAMAGED. COMPLIED WITH EC RA 5211-01348 REQUIREMENTS. TAPE APPLIED AS INTERIM.

Part: CABLE — MISINSTALLED (LT OVRWNG SLIDE) · airframe 90,878 hrs · 14,481 cycles

LT OVERWING SLIDE TRIGGER CABLE BALL INSTALLATION INCORRECT. REWORKED LEFT LOW SLIDE TRIGGER CABLE IAW FCD 2560-02526, STEP 6. ALL CHECKED NORMAL.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 90,715 hrs · 14,464 cycles

NR 2 ENG BLADE, NR 29 L/E DAMAGED. DAMAGE IS L/E IN AREA "F", REPAIRED IAW MM 72-31-02.

Part: B-NUT — LEAKING (CREW OXYGEN) · airframe 90,715 hrs · 14,464 cycles

CREW OXYGEN PRESSURE DECREASING, APPARENT LEAK. FOUND LEAK AT B-NUT ON CREW SUPPLY LINE ON SMALL BORE PIPE. LOOSENED AND RETORQUED B-NUT AND NOW NO LEAKS IAW MM 35-11-00 AND MM 12-15-08 AND OXYGEN STILL ABOVE MINIMUM DISPATCH LIMITS AT 1180 PSI. TOTAL LOSS FOR FLT BEFORE REPAIR WAS 20 PSI AFTER BOTTLE TEMP EQUALIZED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 90,562 hrs · 14,444 cycles

SEAT ROW 6A MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT CONNECTOR UNDER SEAT LOOSE. INSTALLED AND SECURED PLASTIC CONNECTOR UNDER SEAT, EMERGENCY LIGHT OP CHECKED GOOD

Part: CONNECTOR — DIRTY (HYD PUMP) · airframe 90,497 hrs · 14,436 cycles

RIGHT HYDRAULIC ELECTRICAL DEMAND PUMP SYSTEM PRESSURE IS ZERO WITH SWITCH IN AUTO OR ON. CLEANED CONNECTOR, OPS CHECKED NORMAL.

Part: CLAMP — LEAKING (LT BLEED DUCT) · airframe 90,353 hrs · 14,417 cycles

LEFT BLEED DUCT LEAK EICAS ON AND LEFT DUCT LEAK LIGHT. FOUND CLAMP LOOSE AT SENSE LINE FROM ACM TO HEAT EXCHANGER. RETORQUED NUMEROUS DUCT CLAMPS IN RIGHT AC BAY AND LEAK WENT AWAY. RAN ENGINE 5 MINUTES. NO FURTHER DUCT LEAK MESSAGES.

Part: DETECTION SYS — INOPERATIVE (WHEEL WELL) · airframe 90,200 hrs · 14,397 cycles

WHEEL WELL FIRE LIGHT FAILED TO ILLUM DURING TEST. WHEEL WELL FIRE TEST OVERHEAT INOP DEFERRED IAW MEL.

Part: CONNECTOR — FAULTED (FIRE DETECTION) · airframe 90,200 hrs · 14,397 cycles

WHEEL WELL FIRE LIGHT FAILED TO ILLUMINATE DURING TEST. RESEATED CONNECTOR M691, GROUND CHECKED OK IAW MM 26-17-00

Part: WARNING LIGHT — FALSE ACTIVATION (LT BLEED) · airframe 90,191 hrs · 14,396 cycles

LEFT BLEED DUCT LEAK ILLUMINATED. EFTL BLEED LIGHT ON MOMENTARILY WITH APU BLEED ON ONLY. ACCOMPLISHED VISUAL INSPECTION ACCESSIBLE DUCTING FOR LEAKS, NO LEAK DETECTED. REPLACED M691 BLEED CARD AS PRECAUTION. NO LIGHT AT THIS TIME, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 90,027 hrs · 14,375 cycles

COCKPIT PORTABLE EMERGENCY LIGHT INOPERATIVE. LIGHT ASSY REPLACED AND OPS CHECKED NORMAL AS PER AMM.

Part: ACTUATOR — INOPERATIVE (SPAR VALVE) · airframe 90,027 hrs · 14,375 cycles

RT WING FUEL ENG SPAR VALVE INOPERATIVE DURING TEST. SPAR VALVE ACTUATOR REPLACED AND OPS CHECKED NORMAL IAW AMM.

Part: CONTROL PANEL — STUCK (BLEED VALVE) · airframe 90,003 hrs · 14,371 cycles

RIGHT ISOLATION VALVE SWITCH STUCK IN OPEN POSITION. REMOVED AND REPLACED BLEED AIR CONTROL PANEL.

Part: SENSOR — FAULTY (AUTO SPEEDBRAKE) · airframe 89,986 hrs · 14,368 cycles

WITH ENGINES OFF, CAPTAIN'S PITOT, RT AUX PITOT, LEFT AOA AND TAT HEATERS OFF LIGHTS ARE OUT. THESE SYSTEM ARE POWERED IN AIR MODE. CIRCUIT BREAKERS K14, K15, K17, K16, L18, L17 HAVE BEEN PULLED ON P6-3, IAW SSM30-31-01, PG101, SHEET 1. RT AUX PIT ON P6 MN POWER DISTRIBUTION, IAW 30-31-01 PG 101, SHEET 2. TAT ON P6 MN POWER DISTRIBUTION, IAW SSM M30-33-01. AOA P6 POWER DISTRIBUTION, SMM30-32-01 PG 101. FOUND AUTO SPEEDBRAKE TILT SENSOR, S10598 AT FAULT. REPLACED SENSOR PER MM. ALL OPS & INDICATIONS NOW OK.

Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 89,868 hrs · 14,353 cycles

CREW REPORTED RIGHT HYD SYSTEM PRESS LIGHT ILLUMINATED, WITH RIGHTT HYD SYS PRESS EICAS MSG. ALSO RIGHTT HYD DEMAND PUMP LOW PRESS LIGHT ILLUMINATED IN AUTO. SWITCHED TO "ON", NO HELP. RIGHT ENGINE HYD PUMP LOW PRESS LIGHT NEVER ILLUMINATED. RIGHT HYD QTY REMAINED NORMAL AT .96. PER QRH, TURNED OFF RIGHT EDP AND ACMP. TURNED RIGHT EDP DURING CONF WITH TOMC, HYD PRESS RESTORED CONTINUED. REPLACED RIGHT SYSTEM ACMP.

Part: GCU — FAULTY (POSIT 2) · airframe 89,399 hrs · 14,288 cycles

FLIGHT ATTENDANT ADVISED COCKPIT INFLIGHT THAT CHATTER HEARD FROM E-E BAY ON TAKEOFF ROLL. NO INFLIGHT RECUR. BEFORE TAKEOFF, THEY LOST BOTH SLIDING WINDOW HEAT AND PITOT TUBE HEAT. EXACT PITOT TUBE UNRECALLED. ACCOMPLISHED BPCU BITE REF MM, RT PWR CHANNEL FAULT: CT LOOP GND. ACCOMPLISHED AMM24-20-00 PG 1 55 CK OF RT GCU FOUND WIRE CKS AT ALL 4 TEST POINTS GOOD. REPLACED RT GCU, SYSTEM CHECKS OKAY.

Part: BATTERY — FAULTY (MAIN) · airframe 89,029 hrs · 14,238 cycles

APU FAULT LIGHT ILLUM WITH APU RUNNING. REPLACED MAIN AC BATTERY, OP CHECKS GOOD.

Part: BRAKE — DRAGGING (RT MLG) · airframe 89,021 hrs · 14,237 cycles

FORWARD INBOARD BRAKE ON RIGHT SIDE DRAGGING. ALL BRAKE TEMPS NORMAL. ACCOMPLISHED BRAKE OPERATION TEST PER FIM CODE 32-41-13 AND ALL BRAKES RELEASE NORMALLY. JACKED RT FWD MAIN GEAR AND ACCOMPLISHED MULTIPLE BRAKE SET-RELEASED CYCLES AND BOTH FWD BRAKES RELEASE NORMALLY AND WHEELS SPIN SMOOTHLY. INSPECTED AREA AND ACCOMPLISHED BRAKE TEMP BITE AND ALL NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,894 hrs · 14,220 cycles

CEILING EMERGENCY LIGHT AT SEAT 10JK IS INOP. RELAMPED, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,894 hrs · 14,220 cycles

EMERGENCY ESCAPE PATH LIGHTS AT 19J, 34J, 35J A ND 38B ARE INOP. RELAMPED, CHECKS OK.

Part: RIVET — DAMAGED (EXHAUST NOZZLE) · airframe 88,509 hrs · 14,169 cycles

FOUND BY FRENCH DGAC ENGINE 2 NOZZLE TRAILING EDGE : ONE BROKEN RIVET (9 O'CLOCK POSITION). MISSING RIVET AT NR 2 ENGINE EXHAUST T-E 9 O'CLOCK POSITION CARRIED FORWARD IAW ECRA 7811-011 73. DETAIL VISUAL INSPECTION ACCOMPLISHED, NO FINDINGS. FOUND FASTENER AT 9 O'CLOCK WITH MISSING HEAD, REPLACED FASTENER.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 88,429 hrs · 14,158 cycles

NR 1 ENGINE HYD EDP LOW PRESSURE LIGHT DOES NOT ILLUMINATE WHEN ENGINE IS SHUT DOWN. REF SM 29-00-02 PG 101 SHEET 1 JUMPED SWITCH S26 AND LIGHT ILLUMINATED AND REF DF231 AUTO FUNCTION THEN OPERATED NORMALLY. CLEANED SWITCH CONTACTS AND REFITTED PLUG AND LIGHT DOES NOT ILLUMINATE. REQUIRES SWITCH S26 PCN (481-0076). COMPLIED WITH MEL TEST REQUIREMENTS. MAINTENANCE TO VERIFY PUMP AND SYSTEM PRESSURE LIGHT OPS BEFORE BEFORE EACH DEPARTURE. REPLACED PRESS SWITCH S26, LIGHT OPS NORMAL.

Part: LINE — LEAKING (BRAKE SYSTEM) · airframe 88,066 hrs · 14,111 cycles

HYDRAULIC LINE LEAKING IN RIGHT MLG WHEEL WELL. LINE REMOVED FOR REPAIR OR REPLACEMENT. REPLACED 1EA CTR SYSTEM HYDRAULIC BRAKE LINE IN RIGHT STRUT-WELL, LEAK CHECKS GOOD.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 88,017 hrs · 14,104 cycles

LEFT FORWARD WINDOW EICAS. LEFT EICAS COMPUTER REPLACED PER AMM. SOFTWARE OPS: 3174-COL-DEO-07,OPC:3100-BCG-006- E7 INSTALLED PER TASK MM. LEFT EICAS COMP, OPS NORMAL. NO FURTHER MESSAGE.

Part: SEAL — LEAKING (LANDING GEAR) · airframe 87,831 hrs · 14,080 cycles

LANDING GEAR SELECTOR HYD LEAK. REMOVED LOWER FWD UNION INCLUDING T-PIECE TO ACCESS UPPER AFT UNION. UPPER AFT UNION REMOVED AND VERIFIED SEAL DAMAGED. NEW SEALS ORDERED FOR BOTH UNION. BOTH UNIONS AND PIPES FITTED HAND TIGHT TO SEAL SYSTEM FROM CONTAMINATED. SEAL 750-5650 AND 750-0683 REQUIRE REPLACEMENT. REPLACED SEALS ON ITEMS 245 & 255. LEAK CHECK ACP. NO LEAKS NOTED.

Part: ACTUATOR — FAULTY (RT ENGINE) · airframe 87,411 hrs · 14,028 cycles

RIGHT ENGINE EEC C1 STATUS MESSAGE DISPLAYED. FOUND ACTUATOR FAULTY.

Part: ACTUATOR — FAULTY (NR 2 ENGINE) · airframe 87,465 hrs · 14,034 cycles

RIGHT ENGINE EEC C1 STATUS MESSAGE DISPLAYED. REPLACED NR 2 ENGINE TCC AIR VALVE ACTUATOR PER MM 75-24-05-401. OPS AND LEAK CHECKED GOOD.

Part: CONNECTOR — FAILED (WINDOW HEAT) · airframe 87,316 hrs · 14,014 cycles

WINDOW NR 2 RT FAILS THE HEAT TEST. REPLACED "WW1156 A-A AND A-B" TERMINAL CONNECTION PLUG AND HARNESS - D1906, REF WD30-41- 11 PG 1. OPERATIONAL TEST OF RIGHT SIDE (R-2) WINDOW HEAT SYS OK.

Part: HOSE — UNSECURE (RADIATOR) · airframe 87,150 hrs · 13,990 cycles

R BLD DUCT LEAK EICAS AND DUCT LEAK ON OVERHEAD. SECURED RADIATOR HOSE IN AREA OF WATER CONDENSOR LEAK CHECKED OK..

Part: COMPENSATOR — INOPERATIVE (FUEL TANK) · airframe 87,149 hrs · 13,989 cycles

RIGHT TANK INDICATOR BLANKING. FOUND FAULT CODE C6 BOTH CHANNELS. ACCOMPLISHED FIM 28-41-00 TABLE 108 (CONFIG 1). REPLACED COMPENSATOR.

Part: SEAL — LEAKING (DUCT) · airframe 86,972 hrs · 13,966 cycles

CREW REPORTS DUCT LEAK LIGHT ILLUMINATED WITH APU BLEED AIR ON. LIGHT EXTINGUISHES WITH APU BLEED OFF. FOUND LEAK AT SLIDING JOINT FWD OF ADP MUFFLER. REPLACED SEALS, LEAK CHECKED AND NO DUCT LEAK LIGHT.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 86,024 hrs · 13,841 cycles

WX RADAR SHOWS GND RETURN AT 60 MILES IN AUTOTILT AT ALL RANGES. WX RADAR RT PER MM. TESTS NORMAL PER MM.

Part: COMPENSATOR — FLUCTUATES (FUEL QTY) · airframe 85,883 hrs · 13,824 cycles

RIGHT FUEL QTY FLUCTUATES 1200 LBS RANDOMLY. REPLACED RT TANK FQIS COMPENSATOR USING MM.

Part: SKIN — DENTED (FUSELAGE) · airframe 85,857 hrs · 13,820 cycles

EXTERNAL FUSELAGE DENTED AT BS 1413 AT STRINGER 34L & 34R. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE & ACP HFEC. NO CRACKS FOUND. ACP INSURANCE CUT. HFEC OPEN HOLES COMMON TO SKIN REPAIR. FABRICATED & INSTALLED EXTERNAL FILLER, DOUBLER & TRIPLER REPAIR REF PEMCO EA PT 67-53-001 & ECRA 5360-01186A.

Part: FLOORBEAM — PUNCTURED (FUSELAGE) · corrosion level 2 · airframe 85,857 hrs · 13,820 cycles

AFT CARGO COMPARTMENT FLOORBEAM WEB PUNCTURED AT BS 1270 RBL 36. MAJOR REPAIR ACCOMPLISHED: RMV'D & RPL PUNCTURED WEB. FABRICATED & INSTALLED NEW WEB SECTION.

Part: FAILSAFE — CORRODED (BS1562 S39L/R) · corrosion level 2 · airframe 85,857 hrs · 13,820 cycles

COMPARTMENT AFT OF BULK CARGO PIT AT BS 1562 BETWEEN STRINGERS S-39L & S-39R FAILSAFE FOUND CORRODED. REMOVED DAMAGE. ACCOMPLISHED NDT & PERFORMED 0.04" INSURANCE CUT. ACCOMPLISHED NDT OF REPAIR FASTENER HOLES. NO CRACKS FOUND. FABRICATED & INSTALLED FILLER & NESTED ANGLE REPAIR REF EA PT67-53-004 & ECRA 5360-01187.

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 85,857 hrs · 13,820 cycles

AFT CARGO BAY FLOORBEAM AT BS 1197+22 AT LBL 38 FOUND CORRODED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. CUT OUT FLOORBEAM SECTION & FABRICATED & INSTALLED FLOORBEAM SPLICE REPAIR, REPAIR 4. THIS IS A CATEGORY 'A' MAJOR REPAIR

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 85,857 hrs · 13,820 cycles

AFT CARGO COMPARTMENT STA 1197+90, LBL 38 FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & REPLACED J-CHORD, STRAP AND CHANNEL PER SRM'S 51-40-02 AND 53-00-07 ON NR 4453N00484.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,857 hrs · 13,820 cycles

AFT CARGO COMP STA 1197+132, LBL 38 FLOORBEAM CORRODED ON LWR SURFACE AROUND NUT PLATE. RMV'D T-CHORD STA 1197+ 132, LBL 38 - RBL 38. FABBED AND INSTALLED NEW T-CHORD PER SRM ON NR 4453N00406.

Part: SHUTOFF VALVE — FAULTY (NR 2 ENGINE) · airframe 85,857 hrs · 13,820 cycles

NR 2 ENGINE HIGH PRES SHUTOFF VALVE FAULTY. NR 2 ENGINE PRESSURE SHUTOFF VALVE REPLACED ON TC 640004012.

Part: SHUTOFF VALVE — FAULTY (NR 1 ENGINE) · airframe 85,857 hrs · 13,820 cycles

NR 1 ENGINE HIGH PRES SHUTOFF VALVE FAULTY. NR 1 ENGINE HIGH PRESSURE SHUTOFF VALVE REPLACED ON TC 640004010.

Part: TRANSCEIVER — DEFECTIVE (WEATHER RADAR) · airframe 85,334 hrs · 13,747 cycles

WXR WEAK MESSAGE INTERMITTENTLY DISPLAYED OI CAP AND F/O HSI. REPLACED WXR XCVR PER MM, CHECKS GOOD.

Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 85,342 hrs · 13,748 cycles

WXR FAIL DSPLYD ON HSI. WXR FAIL WEAK DSPLYD ON HSI IN WXR TEST POS'N. CREW COMMENTS: WXR FAIL WEAK RT DISPLAYS. REPLACED WXR RADAR ANTENNA, ALL OPS CHECKS SATISFACTORY.

Part: DOOR — SATURATED (MLG) · airframe 85,182 hrs · 13,727 cycles

CF968 AND CF967 WATER INGRESS ON MLG DOORS, DOORS REMOVED TALKED TO SHOP WITH EST FOR DOORS RETURN IS 0700-23. LT MLG DOOR IS ON R&R R57058, RT MLG IS ON R57057, SAILTAIL IS ON R57059* SHOP REPORTS SPARE RT MLG DOOR AVAIL BY TOMORROW.

Part: ACTUATOR — LEAKING (YAW DAMPER) · airframe 85,065 hrs · 13,712 cycles

FOUND RT YAW DAMPER ACTUATOR M509 LEAKING DURING OPERATION. INSTALLED NEW ACTUATOR PER MM.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 85,065 hrs · 13,712 cycles

LOWER RUDDER ACTUATOR LEAKING AT PISTON. INSTALLED NEW LOWER RUDDER ACTUATOR. REMOVED MR27250-65 OFF AND -91 ON. NEED TO COMPLETE FROM STEP I-5 ON PAGE 219. COMPLETED INSTALLATION AND OPS CHECK OF RUDDER PCA SYSTEM PER MM.

Part: SHUTOFF VALVE — FAILED (APU) · airframe 84,997 hrs · 13,703 cycles

APU PNEUMATICS NOT OPENING FOR ENGINE START. PACKS OFF. APU BLEED VALVE BAR SHOWS OPEN, YET NO DUCT PRESSURE FOR ENGINE START. REPLACED APU AIR SUPPLY SHUTOFF VALVE PER MM. OPS CHECKED OK.

Part: NUT — MISSING (COCKPIT SEAT) · airframe 84,963 hrs · 13,698 cycles

F-O SEAT IS MISSING FRONT LEFT SEAT TRACK STOP. INSTALLED NUT.

Part: ACTUATOR — MALFUNCTIONED (APU INLET DOOR) · airframe 84,903 hrs · 13,689 cycles

APU DOOR STATUS UPON APU SHUTDOWN. APUC REPLACED . REACTIVATED APU INLET DOOR ACTUATOR REF MEL 4915D. ACCOMPLISHED BITE CHECK ON APUC, NO FAULTS PRESENT. ACCOMPLISHED OPS CHECK OF ACTUATOR. STARTED APU, NO APU OR DOOR FAULTS ON EICAS.

Part: CONTROLLER — FAULTY (APU) · airframe 84,901 hrs · 13,687 cycles

APU NO START. REPLACED APU CONTROLLER PER AMM, OPS CHK OK. SECURED CONNECTOR TO APU DOOR ACTUATOR. STARTED APU. SATISFACTORY OPERATIONS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 84,902 hrs · 13,688 cycles

R ENG FUEL FILT EICAS MSG, RTFL

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM) · airframe 84,416 hrs · 13,613 cycles

NO CTR R FUEL PUMP EICAS W-PUMPS ON AND ENGINE OFF. NO TIME. PERFORMED OPERATIONAL TEST OF ENGINE FUEL FEED SYSTEM. NO FAULTS FOUND. OPS TEST NORMAL.

Part: HOUR METER — INOPERATIVE (APU) · airframe 84,156 hrs · 13,573 cycles

APU OIL CONSUMPTION ABOVE LIMIT. RAN APU FOR 10 MINUTES NO LEAKS NOTED, APU FOUND CLEAN AFTER RAN. PERFORMED T-S PER AMM49-11-00 & RAN APU IAW JRH2-6-15- AFTER RAN NOTED APU HOURMETER INOPERATIVE. APU HOUR METER DEFECTIVE, CLICKS INTERNALLY AT 10TH HOUR BUT DOES NOT MOVE DISPLAY. REPLACED APU HOUR METER IAW AMM 49-72-01, METER CHECKED OK.

Part: ACTUATOR — FAULTY (FUELING PANEL) · airframe 83,721 hrs · 13,513 cycles

NO POWER TO UNDER WING FUELING PANEL. BRACKET FOR PROX SW SWITCH ACTUATOR IS DAMAGED. NEED TO HOLD ACTUATOR FOR PROX SWITCH IN PLACE WHILE FUELING. (PCN 160-5008) IN LOB. ITEM 90 PCN 160-0288 IS NOT AVAIL. ORDERED PART OSTF# X1392. -INF- :PCN 160-0288 ON OSYF Z1446 .*OPB-JSPP*. -INF- :REFUEL DOOR TARGET MISSING WILL NEED A MAGNET TO ACTUATE SW, EACH FUELING OF ACFT. PARTS: 160-0288 114T2454-6 SPRING*Z1446*. REPLACED BRACKET AND ACTUATOR.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 83,454 hrs · 13,474 cycles

APU FAILED TO START. RESTARTED APU. NO FAULTS.

Part: CIRCUIT CARD — FAULTY (WARNING SYSTEM) · airframe 82,623 hrs · 13,342 cycles

WHEN STANDBY PWR SWITCH SELECTED TO OFF POSITION THE CONFIG WARNING SOUNDS AND THE MASTER WARNING LT ILLUMINATES. WHEN STBY PWR BUS DEPOWERED OR WEU B CB P11 B18 PULLED MASTER WARNING LTS ILLUMINATE AND AURAL WARNING SOUNDS. NO EICAS WARNING MSG IS PRESENT WHEN AURAL WARNING AND LTS ILLUMINATED, REQUIRES FURTHER TROUBLESHOOTING (PARTIAL). T/S TO CARD M620 TO CONFIG WARNING MODULE IN P51. REPLACED CARD PER MM. ALL INDICATIONS & OPS NORMAL. NO AURAL WARNING WHEN STBY PWR SWITCHED OFF. CARD IS AA 7 DAY NON-POOL LOAN. PAPERWORK IN LOG. CONTAINER IN LOB.

Part: FITTING — MISSING (RT MLG TRUCK) · airframe 83,426 hrs · 13,468 cycles

LUBRICATION ZERK FITTING MISSING FROM OTBD END OF RIGHT MAIN GEAR TRUCK PIVOT PIN. HOLE IS WORN TOO LARGE TO INSTALL NEW FITTING. INSTALLED OVERSIZED ZERK FITTING. LUBES OKAY.

Part: RELAY — FAILED (COCKPIT) · airframe 83,202 hrs · 13,430 cycles

CAPT SIDE PRIMARY FLIGHT INSTRUMENTS ALL BLANK. REPLACED RELAY K862. CAPT'S EFIS OP CHECKED NORMAL.

Part: PUMP — MALFUNCTIONED (FUEL CELL) · airframe 83,146 hrs · 13,422 cycles

RIGHT CENTER TANK FUEL PUMP INOPERATIVE AND DEACTIVATED. CIRCUIT BREAKER POPPED ON P-6 PANEL. RAN NR 2 ENGINE FOR 5 MIN, OPS CHECKED RIGHT CENTER TANK FUEL PUMP. NO CIRCUIT BREAKER POP, CENTER TANK FUEL PUMP CHECKED NORMAL PER JRH.

Part: CIRCUIT CARD — MALFUNCTIONED (WARNING SYS) · airframe 82,623 hrs · 13,342 cycles

WHEN STANDBY PWR SWITCH SELECTED TO OFF POSITION THE CONFIG WARNING SOUNDS AND THE MASTER WARNING LT ILLUMINATES. WHEN STBY PWR BUS DEPOWERED OR WEU B CB P11 B18 PULLED MASTER WARNING LTS ILLUMINATE AND AURAL WARNING SOUNDS. TRIED SWAPPING WEU A AND B PER MM, NO HELP. REPLACED M618 PER SAME REF AND NO HELP. REFITTED ORIGINAL. NO EICAS WARNING MSG IS PRESENT WHEN AURAL WARNING AND LTS ILLUMINATED, REQUIRES FURTHER TROUBLESHOOTING. T-S TO CARD M620 TO CONFIG WARNING MODULE IN P51. REPLACED CARD PER MM31-51-04. ALL INDICATIONS & OPS NORMAL. NO AURAL WARNING WHEN STBY PWR SWITCHED OFF. CARD IS AA 7 DAY NON-POOL LOAN. PAPERWORK IN LOG. CONTAINER IN LOB.

Part: ADC — FAULTY (COCKPIT) · airframe 82,529 hrs · 13,322 cycles

ADC FAILURE, FLIGHT DIVERTED. MCDP PREV FLT FAULTS: FD BAR FMC L-R CH (110071120081) (110081120071) FD BAR ADC SYST L (110401) FD BAR IRU L (110551) FD BAR ADC L-R CH (122080). REPLACED BOTH LT AND RT ADC PER MM AND PERFORMED LOW RANGE LEAK TEST ON BOTH ADC'S PER MM, OP CHECKED OK. NO LEAKS DETECTED.

Part: FAN BLADE — DAMAGED (NR 1 ENGINE) · airframe 82,406 hrs · 13,304 cycles

ENG NR 1: FAN BLADES NR 34, HAS DAMAGE ON LEADING EDGE ONE NICK. ACCOMPLISHED BLADE REPAIR REF MM.

Part: ACTUATOR — FAULTY (AILERON) · airframe 81,976 hrs · 13,240 cycles

AFTER PUSH AILERON LOCKOUT EICAS MESSAGE. FOUND LEFT SAM HAD LEFT AILERON ACT FAULT. RESET AND DID NOT RETURN. FOLLOWED LM8279 AND REPLACED RIGHT SAM. UPON RETEST LEFT SAM FAULTED LEFT ACTUATOR. INSTALLED NEW SAM IN LEFT SIDE AND ORIGINAL BACK IN RIGHT. RETEST AND LEFT SAM FAULTED LEFT ACTUATOR AGAIN. RPLCD LEFT AIRDATA COMPUTER AND TESTED, THIS TIME THE RIGHT SAM FAULTED THE LEFT ACTUATOR. ACCOMPLISHED FIM. AFTER SEVERAL SWAPS OF LEFT AND RIGHT M524 AND M525 BOTH SIDES TESTED OK PER MM BUT AILERON MSG AND LIGHT WOULD REMAIN AFTER TEST. LT OR RT STAB MOD WOULD ALTERNATELY FAULT THE LT AIL LOCK ACTUATOR. WHEN ACCOMPLISHING LOCKOUT ACT TEST SAM MODULE KEPT FAULTING LT AIL LOCK ACT. REPLACED LT ACT PER MM. RAN TEST AGAIN SEVERAL TIMES AND HAD NO FAU LTS. RESTORED SYSTEM BACK TO NORMAL.

Part: CIRCUIT BOARD — FAILED (EXHAUST FAN) · airframe 81,891 hrs · 13,228 cycles

EICAS MESSAGE FWD EQ EXH FAN DISPLAYED. FWD EQ EXHAUST FAN PLACARD INOP IAW MEL2158F. COMPLIED WITH MEL REQUIREMENTS. CBS H21 AT P6 AND P22 AT P11 PULLED AND COLLARED. STANDBY MODE OPERATIONS VERIFIED WORKING SATISFACTORY. CHANGED ECS FAN CONTROL CAD PER FIM, NO HELP. ACCOMPLISHED FIM 21-58-00. PERFORMED FAN MONITOR REST. OPS CHK NOW OKAY. FAN OPERATED NORMALLY AND NO FURTHER MSG DISPLAYED.

Part: WIRE — ARCED (CARGO BAY) · airframe 81,853 hrs · 13,222 cycles

FWD CARGO PIT AT STA 535 STR 37L ARC WIRING FOUND AND STR 37L PAINT SHOWED HEAT DAMAGE. NEEDS INSPECTION. WHILE WORKING A-CHECK SMELLED SMOKE FROM WIRE BUNDLE IN FWD PIT TO PDUS. FOUND WIRES ARCING. RECOMMENDED HARDNESS TEST. HEAT TREAT VERIFICATION. ACP'D CONDUCTIVITY TEST ON STRINGER 37L STA 535. TESTS WITHIN LIMITS.

Part: SWITCH — FAULTY (IDG) · airframe 81,709 hrs · 13,200 cycles

DURING NR 1 ENG RUN, "L IDG VALVE" MESSAGE APPEARED ON LOWER EICAS, MESSAGE WOULD ERASE, BUT RE-APPEAR ON NEXT ENG RUN. IDG AIR-OIL HEAT EXCHANGER VALVE OVERRIDE SWITCH WAS REPLACED. REMOVED AND PUT NEW COOLER IN PLACE. IDG AIR-OIL HEAT EXCHANGER VALVE OVERRIDE SWITCH WAS REPLACED. NEED TO REPLACE IDG AIR OIL HEAT EXCHANGER. CENTER MOUNT BOLTS NEED TO BE INSTALLED PRIOR TO MAKING CONNECTIONS. COMPLETED INSTALLATION OF AIR OIL HEAT EXCHANGER.

Part: ACTUATOR — BINDING (RT AILERON) · airframe 81,666 hrs · 13,192 cycles

AILERON LOCKOUT DESCENDING OUT OF 10000 240 KNOTS. RT OB AILERON LOCKOUT ACTUATOR PREVIOUSLY REPLACED. STILL FAULTING ACTUATOR. WORKING REPLACEMENT OF ACTUATOR. REPLACED RIGHT OTBD AILERON LOCKOUT ACTUATOR. CHECKED OK. AILERON LOCKOUT FAULT AND HYD PRESSURE SWITCH FAULT BALLS SHOW ON LEFT SAM (R524) RESET AND FAULTS CLEARED DUE TO RECENT HITS REPLACED LT SAM. MECHANISM OPERATES SMOOTHLY, NO BINDING.

Part: ACTUATOR — FAULTY (AILERONS) · airframe 81,657 hrs · 13,191 cycles

AILERON LOCKOUT EICAS WITH ASSOCIATED OVERHEAD LIGHT ILLUMINATED ON ARRIVAL. REPLACED RIGHT OTBD AILERON LOCKOUT ACTUATOR PER MM.

Part: PANEL — PEELING (NR 1 PYLON) · airframe 81,387 hrs · 13,150 cycles

NR 1 AFT OTBD PYLON FAIRING PANEL AT NAC STATION 352.80 HAS METAL OVERLAY PEELING UP. MEASURES 3 INCH BY 4.5 INCH ACP TEMP REPAIR PER EVA UAL 80580, PANEL SECURE. REMOVED NR 1 OUTBOARD PYLON PNL 313T3381-203 AND ROUTED TO SHOP 273. REMOVED AND REPLACED 42995. SHOP RESKINNED INNER SKIN AND REPLACED 4IN STRIP OF CORE PER SRM AND JD. INSTALLED PANEL AFTER SHOP REPAIR.

Part: COMPUTER — FAULTY (EICAS) · airframe 81,307 hrs · 131,377 cycles

RT EICAS COMPUTER DISPLAYED ON STATUS PAGE. ACP FIM R EICAS NO FAULTS NOTED IN TEST MODE, LT EICAS 2 INTERFACE FAULTS, RECEIVER FAULT, EICAS XTALK INTERFACE FAULT LEG 7 AND ON LEG 8 SAME. AT T/O, HARD FAULT. REPLACED LT EICAS COMPUTER.

Part: INDICATOR — FAULTY (RUDDER TRIM) · airframe 81,283 hrs · 13,134 cycles

RUDDER TRIM IND 5 UNITS LT WING- EICAS IND ZERO TRIM. AFTER CLIMB ALL INDICATIONS RETURNED TO NORMAL. VERIFIED WITH CREW THAT TRIM INDICATION WAS THE PROBLEM AND NOT A RUDDER TRIM. IAW FIM AND TEST INDICATIONS ARE NOW NORMAL. DUE TO PREVIOUS HISTORY DEFFERED FOR INDICATOR REPLACEMENT. ACCOMPLISHED MEL TESTS AND INSTALLED STICKER. REPLACED RUDDER TRIM INDICATOR, TESTED OK.

Part: ACTUATOR — INOPERATIVE (RUDDER TRIM) · airframe 81,011 hrs · 13,096 cycles

RUDDER TRIM INOPERATIVE. TRIED NEW RUDDER TRIM CONTROL PANEL, NO HELP. TRIM INDICATOR AND BOTH EICAS INDICATIONS REFLECT SAME.VERIFIED VOLTAGE INTO AND THRU CONTROL PANEL.RUDDER MOVEMENT NORMAL WITH PEDALS. ELECTRIC TRIM TOTALLY INOP. REPLACED TRIM ACTUATOR PER MM. OPS NORMAL.

Part: ACTUATOR — FAULTY (APU DOOR) · airframe 80,218 hrs · 12,987 cycles

APU DOOR EICAS MESSAGE DISPLAYED ON GROUND. NOT RESETABLE. SEVERAL DOOR FUNCTION PERF AND ECU RESET, NO HELP. BITE CHK EICAS FOR MSG'S. REPLACED INLET DOOR ACTUATOR. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (SEAT 37AB) · airframe 79,411 hrs · 12,870 cycles

SEAT 37 AB EMERGENCY EGRESS LIGHT INOPERATIVE. REPLACED LIGHT ASSY.

Part: LIGHT — INOPERATIVE (MID GALLEY) · airframe 79,411 hrs · 12,870 cycles

EMERGENCY LIGHT AT MID GALLEY RT SIDE INOP. AOG- G0839 PN 6025-3. REPLACED EMERGENCY LIGHT ASSY, OP CKS OK.

Part: CONTROLLER — FAULTY (NR 2 BLEED) · airframe 79,000 hrs · 12,815 cycles

RIGHT ENGINE BLEED LGT & RT ENG HPSOV EICAS MSG WITH ENG BLEED SW ON & ENG RUNNING. CONTROLLER FOUND FAULTY. NEW CONTROLLER INSTALLED. OPS CHECK GOOD.

Part: WIRE — CHAFED (FMU) · airframe 78,748 hrs · 12,783 cycles

PER CREW AFTER ENGINE START THE HAVE L ENG EEC C1 STATUS MSG. FOUND WIRE GOING TO FMU CHAFING AND CONTACTING REV COWL. INSULATION WORN REPAIR PER GNMM. RAN ENG AND OPS CHECK NORMAL.

Part: LIGHT — FAULTY (CABIN) · airframe 78,624 hrs · 12,765 cycles

RT EMERGENCY EXIT LIGHT FWD OF DOOR 2L INOP. OPS CHECKED THE EMERGENCY LIGHTS, OPS CHECKED GOOD.

Part: ATTACH FITTING — BROKEN (FLAP TRACK) · airframe 78,624 hrs · 12,765 cycles

RT REAR SPAR, WS 900.2, OTBD FLAP TRACK ATTACH FITTING IS BROKEN AT LWR END. REPLACED FLAP TRACK ATTACHED FITTING AND ACP COA 616464. FUEL LEAK CHECK AT ATTACHED FITTING, NO LEAK, NOT NOTED. OPS CHECK OF FLAP ON C-CK ROUTINE JC. WORK WAS ACP ON NR 2176N00135.

Part: PANEL — CRACKED (RT WING) · airframe 78,624 hrs · 12,765 cycles

RT WING OTBD T/E PANEL AT WS 905, FASTENERS ARE TORN THROUGH PANEL, PANEL IS CRACKED ABOUT 12' LONG. REMOVED T/E PANEL AND REPAIRED AT SHOP. REINSTALLED PANEL IAW MM. WORK WAS ACP ON NR 2176N00126.

Part: FAN — FAULTY (RIGHT) · airframe 78,624 hrs · 12,765 cycles

RT AFT EQUIPMENT FAN DAMAGED BY FAULTY CHECK VALVE FLAPPER AT STA 815. REMOVED AND REPLACED RT RECIRCULATION AIR FAN IAW B767 AMM. REMOVED & REPLACED RT RECIRCULATION AIR CHECK VALVE. OP CHECK RT RECIRCULATION AIR FAN IAW 767 AMM. OP CHECK RT RECIRC AIR CHECK VALVE.

Part: BRAKE ASSY — SMOKE (MLG) · airframe 78,472 hrs · 12,741 cycles

BRAKE SMOKE EVIDENT ON LANDING TEMP OF 3 ON NR 2 BRAKE 300 DEG PER FIRE DEPT LT MAIN FWD INBOARD. REPLACED NR 2 FWD BRAKE.

Part: PROCESSOR — FAILED (FUEL QTY) · airframe 78,380 hrs · 12,725 cycles

FUEL CONFIG LIGHT ILLUMINATED WHEN IT SHOULD BE EXTINGUISHED. NO CORRESPONDING EICAS MSG. REPLACED MFQ PROCESSOR. NEW PART BAD FROM STOCK, FUEL CONFIG LIGHT COMES ON. REMOVED NEW PART AND REINSTALLED PREVIOUS PN WITH ORIGINAL PROBLEM FUEL QTY AND TOTAL ON BOTH CDU'S BLANKED OUT. CONFIRMED BY MX'S 123409 AND 97409.

Part: OVEN — DIRTY (AFT GALLEY) · airframe 78,372 hrs · 12,724 cycles

ON TAXI OUT REAR GALLEY HAD BURNING SMELL. FOUND OVEN DIRTY, NEEDS CLEANING. SMELLS WHEN WARM. AIR SERV TASKED WITH CLEANING OVEN. OVEN HAS BEEN CLEANED.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 78,068 hrs · 12,683 cycles

CREW REPORTED RT ENG EEC C1 STATUS MESSAGE. WITH CREW ASSIST, SHUTDOWN AND RE-STARTED RT ENG, MSG DID NOT CLEAR OK. TO DEFER IAW MEL 7321H. SUGGEST INTERROGATE PIMU FOR MAINT MSGS. MSG 350-14 CH A FOR EEC CHAN FAIL DOWNLINKED BUT THAT IS SOMETIMES ERRONEOUS. POSS PART IS EEC MR73412 480-9191. REPLACED RT ENG EEC. ACCOMPLISHED ALL ASSOCIATED ENG CHECKS SYS OPERATES NORMAL NO STS OR EICAS FAULTS.

Part: CHARGER — MALFUNCTIONED (MASTER BATTERY) · airframe 77,936 hrs · 12,664 cycles

MAIN BATTERY CHARGER STATUS MESSAGE. BATTERY & BATTERY CHARGER FOUND FAULTY. REPLACED MAIN SHIP BATTERY AND BATTERY CHARGER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,722 hrs · 12,634 cycles

3 EA EXTERIOR EMERGENCY LIGHTS INOP. LT AND RT AFT DOORS, AND FWD OF RT AFT DOOR. R & R (3 EA) EXT EMERGENCY LIGHTS LT AND RT AFT DOORS, FWD RT DOOR. OPS CHECK GOOD.

Part: CONTROL VALVE — FAULTY (AC PACK) · airframe 77,482 hrs · 12,598 cycles

OFF THE GATE RT PACK WOULD NOT COME ON WITH ANY ENGS AIR, PER CREW. REPLACED FLOW CONTROL AND SHUTOFF VALVE IAW AMM. OPS CHECK NOW OKAY.

Part: MODULE — FAILED (APU) · airframe 77,367 hrs · 12,582 cycles

APU PNEUMATICS LOW READS APPROX 19 PSI ALONG WITH FLUCTUATING PRESSURE. REPLACED FLOW SENSING MODULE. REPLACED APU SURGE CONTROL VALVE. TESTED APU. OPS CHECKS NORMALLY.

Part: EMITTER — FLUCTUATES (RT FUEL QTY) · airframe 77,210 hrs · 12,550 cycles

RIGHT MAIN FUEL QTY INDICATOR FLUCTUATING +0 TO -1000 LBS OF LT MAIN FUEL QTY INDICATOR. CREW STATES AS MAIN FUEL BURNED DOWN FLUCTUATION HAS DECREASED BUT IS STILL PRESENT. RT TANK READ 3 INCH DIFFERENT ON DRIP READING WITH 7K IN EACH TANK, AFTER FUELING TANKS TO SAME DRIP READING RT TANK READ 1700 NR HIGHER. ACCOMPLISHED FUEL QUANTITY BITE CHECK, HAVE D6 FAULT. ACCOMPLISHED FIM TABLE 119 RESISTANCE VALUES ON RT DENSITOMETER EMITTER FAIL. OUT OF TANK WIRING CHECKED GOOD. REPLACED DENSITOMETER EMITTER.

Part: BEARING — WORN (AILERONS) · airframe 77,065 hrs · 12,523 cycles

CREW REPORTS ON FLT CONTROL CHECK FOR AILERON, THE CONTROL WHEELS (CAPTS AND FO'S) FEEL AN UNUSUAL HARD SPOT AT ABOUT THREE-QUARTERS TRAVEL LT WING DOWN. LT AIL LCCA UPR & LWR TORQUE TUBE SUPPORT BEARINGS (3EA) FOUND WORN & CORRODED AT LWR LINK ARM FOR FEEL, CENTERING & TRIM MECHANISM INPUT ROD ATTACH. REPLACED TORQUE TUBE WITH NEW ASSY. VERIFIED ADJUSTMENT THEN OPS CKD. NO RIGGING DISTURBED AND NO BINDING PRESENT.

Part: SHUTOFF VALVE — FAULTY (RT ENGINE) · airframe 77,054 hrs · 12,521 cycles

RIGHT ENG HPSOV EICAS. HPSOV LOCKED IN CLOSED POSITION. FOUND HPSOV MANUAL LEVER NOT IN THE FULLY CLOSED POSITION. REQUIRED TO WRENCH CLOSED AND INSTALLED LOCK PIN IAW MEL CARD. SUSPECT VALVE MAY BE AT FAULT. REPLACED HPSOV. RAN ENGINE. OPS CHECK OK.

Part: FUEL/OIL COOLER — LEAKING (NR 2 ENGINE) · airframe 77,022 hrs · 12,513 cycles

DURING COURSE OF NR 3 SVC FOUND FUEL LEAKING FROM STRUT DRAIN TUBE BOTTOM OF ENG AT RATE OF 7 DROPS PER MINUTE. FUEL LEAK ON NR 2 ENG. AFTER OPENING COWLING FOUND FUEL LEAKING FROM FUEL/OIL COOLER FWD DRAIN TUBE. STARTED REMOVING FUEL OIL COOLER. STILL NEED LWR HALF OF COOLER TO DISCONNECT.

Part: OIL COOLER — LEAKING (ENGINE) · airframe 77,022 hrs · 12,513 cycles

FUEL IMBALANCE - CONFIG LIGHT. DURING COURSE OF NR 3 SERVICE FOUND FUEL LEAKING FROM STRUT DRAIN TUBE BOTTOM OF ENGINE AT RATE OF 7 DROPS PER MINUTE. AFTER OPENING COWLING FOUND FUEL LEAKING FROM FUEL OIL COOLER DRAIN TUBE. FUEL LEAKING FROM FWD DRAIN TUBE ON FUEL OIL COOLER. COMPLETED INSTALLATION OF FUEL OIL COOLER. OPS CHECK NORMAL. NO LEAKS FOUND.

Part: TRANSMITTER — FAULTY (FUEL FLOW) · airframe 76,915 hrs · 12,490 cycles

NR 2 ENG HIGHER FUEL FLOW. CREW REPORTS RT TANK IS FEEDING RT ENG WITH 17K IN CTR TANK. CTR TANK QTY 40K LT, 36.7K RT POSS CTR BOOST PUMP. TROUBLESHOOTING. REPLACED THE NR 2 ENGINE FUEL FLOW TRANSMITTER. REPLACED RT AUX OVERRIDE PUMP. WITH CTR PUMPS ON FUEL IS STILL BEING USED FROM RT TANK. REPLACED RT AUX TANK OVERRIDE BOOST PUMP WITH NEWER VERSION PUMP AND 4 WINDOW SLEEVE.

Part: PROCESSOR — MALFUNCTIONED (FQIS) · airframe 76,883 hrs · 12,485 cycles

UNWANTED FUEL TRANSFER. PROCESSOR FOUND DEFECTIVE. REPLACED FQIS PROCESSOR. OP CHECKS NORMAL.

Part: SENSE LINE — UNSECURE (HPSOV) · airframe 76,803 hrs · 12,474 cycles

CREW STATES THAT RT PACK OFF LIGHT ON WHEN ENGINE BLEEDS ARE ON. PACK RUNS OK WITH APU BLEED. RT PACK OFF LIGHT ON WHEN ENGINE BLEEDS ARE ON. PRV VALVE REPLACED, NO HELP. CONTINUING TO TEST. FOUND SENSE LINE AT HPRSOV NOT TOTALLY TIGHTENED. ADJUSTED AND RAN ENGINE TWICE, FOUND RT PACKS WORKS OK.

Part: PRESSURE SWITCH — FAILED (GENERATOR) · airframe 76,751 hrs · 12,465 cycles

APU FAULTED AND AUTO SHUTDOWN TWICE. APU IS INOPERATIVE. REPLACED GENERATOR FILTER DIFFERENTIAL PRESSURE SWITCH. OP CHECKS NORMAL.

Part: LENS — FAULTY (EMERGENCY LIGHT) · airframe 76,751 hrs · 12,465 cycles

EMERGENCY EXIT CEILING LIGHT LENS CRACKED RT SIDE IN COACH. TAPED LENS. LENS SECURITY AND INTEGRITY OK FOR SERVICE. REPLACED LIGHT ASSY, ALL LIGHTS CHECK GOOD.

Part: PUMP — MALFUNCTIONED (FUEL TANK) · airframe 76,699 hrs · 12,459 cycles

AFTER LEVEL OFF ALT RIGHT CTR PUMP OUTPUT WEAK RT ENG WAS BURNING FROM RIGHT MAIN. CREW REPORTS LT MAIN FUEL TANK QUANTITY DID INCREASE WHILE ATTEMPTING TO BALANCE FUEL LOAD. REPLACED RT CTR AUX OVERRIDE PUMP. OP TESTS NORMAL.

Part: PUMP — FAILED (FUEL BOOST) · airframe 76,690 hrs · 12,458 cycles

RT ENG FUEL LEAK, FLIGHT DIVERTED. RT WING FUEL QTY DROPPED 3000 LBS IN 10 MINUTES, CONTINUING TO DROP. WHEN A-P IS DISCONNECTED THE ACFT FELT LT WING HEAVY. FUEL CONFIG LIGHT IS ON. RUN UP PERFORMED ON BOTH ENGINES 10 MINUTES IN IDLE POWER NO LEAK OBSERVED. MEASURING STICK PERFORMED NO DISCREPANCY FOUND WITH COCKPIT GAUGES. FQI BITE TEST PERFORMED, NO FAULT RECORDED. IAW CAPTAIN, FUEL ON BOARD AND CALCULATED FUEL ARE THE SAME. DURING NEXT FLIGHT SEGMENT AFTER LEVEL OFF CREW REPORTS LT MAIN FUEL TANK QUANTITY DID INCREASE BY 700LBS WHILE ATTEMPTING TO BALANCE FUEL LOAD. REPLACED RT CTR OVERRIDE BOOST PUMP. ALL CKS NORMAL.

Part: VALVE — MALFUNCTIONED (AC BAY) · airframe 75,909 hrs · 12,340 cycles

RT PACK INOP AFTER ENGINE STARTED. CONTROLLER FAULTED LOW LIMIT VALVE. REPLACED LOW LIMIT VALVE. RAN ENG AND PACK CHECKS OKAY.

Part: WIRE HARNESS — FAILED (FUEL QTY IND) · airframe 75,776 hrs · 12,317 cycles

RIGHT FUEL QTY INDICATION ISSUE. REMOVED HARNESS FROM RIB 30 TO RIB 18. REMOVED HARNESS FROM INBOARD TO PYLON. INSTALLED SUMMING PLUGS AND SEALED AT 1900 WITH B1-2. STARTED TO ROUTE HARNESS FROM PLUGS INBOARD AND OUTBOARD. NEED TO BE SECURED. SECURED WIRE HARNESS FROM WS 226.3 TO WS 798.2. GROMMET INSTALLED AND SEALED AT WS 284.7. VERIFIED INSTALLATION OF WIRE HARNESS FROM ACCESS PNL 632BB THRU 632FB OK. ACCOMPLISHED BITE CHECK. CHECKS GOOD.

Part: PROCESSOR — MALFUNCTIONED (FUEL INDICATOR) · airframe 75,610 hrs · 12,286 cycles

RIGHT FUEL QTY INDICATOR AND TOTALIZER INOP BLANKS OUT. TRIED NEW FUEL PROCESSOR UNIT AND COCKPIT FUEL INDICATOR NO HELP, SUSPECT TANK UNITS. SUGGEST CHECK HI-Z & LO-Z CONN'S FOR CONDITION AND SECURITY FOR RT TANK. REPLACED FUEL QUANTITY PROBE NR 8 IN RT TANK. BITE CHECKED FUEL QUANTITY PROCESSOR AND NO FAULTS INDICATED. LEAK CHECKED FUEL TANK ACCESS PANEL 641EB. NO LEAKS NOTED. REPLACED PROCESSOR DUE TO CODE 88 DISPLAYED WHEN DOING BITE CHECK. SHOULD HAVE DISPLAYED FAULT CODE OR 00. NORMAL OPS NOTED DURING OFF LOAD OF 6000 LBS OF FUEL.

Part: PRESSURE SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 74,984 hrs · 12,190 cycles

CTR AUX OVERRIDE PUMP LOW PRESS LIGHT ON, SWITCH ON, EICAS MSG CTR L-R FUEL PUMP. CREW COMMENTS: APPROX 1 HR INTO FLT RT MAIN TANK FUEL DECREASED RAPIDLY AS IF RIGHT CENTER PUMP OFF. CONFIRMED NO LEAK. NO EXTERNAL LEAKS NOTED. RAN CENTER TANK PUMPS, OPS CK NORMAL ON GROUND. HOWEVER, NEED MORE TROUBLESHOOTING. PUMP CONSIDERED INOP. REPLACED PRESSURE SWITCH S424 FOR RIGHT AUX FUEL TANK. ALSO REPLACED RELAY K330 RIGHT FUEL PUMP CONTROL. OPERATIONS CHECKED NORMAL, FUEL TRANSFERRED INTO AND OUT OF CENTER FUEL TANK NORMALLY WITH NO PRESSURE LIGHTS ON UNTIL TANKS WERE EMPTY.

Part: SWITCH — FAULTY (RT AUX FUEL TANK) · airframe 74,984 hrs · 12,190 cycles

CTR AUX OVERRIDE PUMP LOW PRESS LT-ON-, SW-ON-, EICAS MSG CTR L-R FUEL PUMP. APPROX 1 HR INTO FLT RT MAIN TANK FUEL DECREASED RAPIDLY AS IF RIGHT CENTER PUMP OFF. CONFIRMED NO LEAK. NO EXTERNAL LEAKS NOTED. RAN CENTER TANK PUMPS, OPS CHECK NORMAL ON GROUND, HOWEVER NEEDS MORE TROUBLESHOOTING. PUMP CONSIDERED INOP. REPLACED PRESSURE SWITCH S424 FOR RIGHT AUX FUEL TANK. ALSO REPLACED RELAY K330 RIGHT FUEL PUMP CONTROL. OPERATIONS CHECKED NORMAL, FUEL TRANSFERRED INTO AND OUT OF CENTER FUEL TANK NORMALLY WITH NO PRESSURE LIGHTS ON UNTIL TANKS WERE EMPTY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 74,798 hrs · 12,157 cycles

EMERGENCY LIGHTS NEAR FORWARD LAV CAME ON MOMENTARILY. RESEATED CONNECTOR ON POWER SUPPLIES M735 AND M1557 AND TESTED AND NOW OKAY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 74,798 hrs · 12,157 cycles

EMERGENCY LIGHTS ON FLOOR AT 1L DOOR, CLOSET, GALLEY COME ON FOR 90 SECONDS. RESEATED CONNECTOR ON POWER SUPPLIES M735 AND M1557 AND TESTED OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,610 hrs · 12,128 cycles

FOUND 2 LOWER CEILING EMERGENCY LIGHTS INOP. LIGHTS ARE SITUATED AT AFT GALLEY LEFT SIDE AND LEFT AISLE FWD OF SEAT 1A. RELAMPED AND OPS NORMAL.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 74,567 hrs · 12,121 cycles

FLOOR MOUNTED EMERGENCY LIGHT FWD OF SEAT 1K INOP. WILL NEED 1K SEAT ASSY MOVED 3 FT AFT OF BULKHEAD TO REPAIR OR REPLACE EMERGENCY LIGHT STRIP. THREE SHIFTS REQUIRED TO ACCESS WIRING. FOUND DOOR 1R AISLE FLOOR LIGHT L901 AND DOOR1 RT LOWER EXIT LIGHT L972 INOP. REPLACED POWER SUPPLY M1552 AND OPS CHECKS NORMAL.

Part: IDG — FAILED (RIGHT) · airframe 74,541 hrs · 12,117 cycles

R GEN FAILURE. RTFL. INITIALLY GEN STAYED ON LINE BUT WENT OFF LINE SHORTLY THEREAFTER. IDG WAS THEN DISCONNECTED BY CREW. BPCU HAS MULTIPLE MSGS INCLUDING IDG PMG WIRING, IDG UNDER FREQUENCY, SVC IDG AND IDG HIGH RISE TEMP. REPLACED IDG AND ACCOMPLISHED TEST. REPLACED GCU AND TESTS NORMAL.

Part: FITTING — LEAKING (APU) · airframe 74,531 hrs · 12,115 cycles

APU LEAKING OIL. SERVICED APU WITH 2 QUARTS. LEAK STILL NOT FOUND. RAN APU FOUND T-FITTING 1 O'CLOCK POSITION LEAKING ON FWD SIDE OF GEARBOX. HELICOIL IS STRIPPED OUT. REPLACED APU, RAN APU AND OPS NORMAL.

Part: PROCESSING UNIT — DEFECTIVE (FUEL SYSTEM) · airframe 73,950 hrs · 12,025 cycles

FUEL TANK AND TOTAL FUEL QTY IND INOP, IND BLANK, FUEL QTY IND EICAS MSG DISPLAYED. POSITION 2 (01=L, 02=R, 03=C). SUPPLEMENTAL DATA UPDATE, REPLACED FUEL QUANTITY PROCESSOR UNIT.

Part: ACTUATOR — FAILED (RUDDER TRIM) · airframe 73,903 hrs · 12,013 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. CREW COMMENTS: INTERMITTENT. REPLACED RUDDER TRIM ACTUATOR.

Part: TUBE — LEAKING (RT WING) · airframe 73,365 hrs · 11,936 cycles

FUEL DRAINING FROM RIGHT WING DRY BAY DRAIN AGAIN AFTER ACFT HAS BEEN REFUELED. FOUND RT NR 4 SLAT OUTBOARD TRACK HOUSING CRACKED. DRY BAYS NOT LEAKING. REMOVED NR 9 SLAT O/B HOUSING. REPLACEMENT ON AOG ALONG WITH SELF SEALING NUTS. WELDED DRAIN TUBE ASSY AND LEAK TESTED. NO LEAKS FOUND AT THIS TIME.REINSTALLED ORIGINAL HOUSING AFTER ACCOMPLISHMENT OF WELD REPAIR.

Part: TRANSMITTER — DEFECTIVE (FUEL FLOW) · airframe 72,452 hrs · 11,805 cycles

FUEL FLOW XMTR MAY BE READING A BIT HIGH. ALTHOUGH THIS DOESN'T AFFECT FUEL BURN IT DOES AFFECT FUEL FLOW INDICATION. SUSPECT FUEL FLOW TRANSMITTER IS INACCURATE. REPLACED TRANSMITTER. RAN ENG. OP CHECKS GOOD.

Part: RESOLVER — FAULTY (NR 2 ENGINE) · airframe 72,356 hrs · 11,793 cycles

LT THROTTLE AHEAD. THROTTLES NOT ALIGNED WITHIN 1 INCH AT KNOB AT SAME EPR AT LOW PWR, OK CRUISE AND CLIMB. EEC'S ON. LT THROTTLE FWD OF RT THROTTLE ABOUT ONE INCH IN CRUISE WITH MATCHING EPRS AND N1S. FOUND NR 2 ENG TLA RESOLVER OUT OF RANGE (34.2). ADJUSTED RESOLVER TO 33.7. ACCOMPLISHED ENG RUNS THROTTLES AND EPRS ALIGNED. NO SPLIT.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 72,260 hrs · 11,779 cycles

RT ENG STARTER EICAS MSG, TERMINATED START CYC. INSTALLED NEW START VALVE. ENGINE STARTER OPS NORMAL.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 72,031 hrs · 11,746 cycles

CREW REPORT LEFT GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED AND APU NOW POWERING BUSS. LEFT IDG REPLACED. LEAK CHECK CARRIED OUT OK. TEST CARRIED OUT.

Part: CONNECTOR — DAMAGED · airframe 71,650 hrs · 11,694 cycles

CREW REPORT AIR DEMAND PUMP OVERHEAT LIGHT ILLUMINATED. LIGHT STAYED ON WITH PUMP SWITCHED OFF. CREW REPORT THAT C HYD DEM PUMP EICAS MSG FINALLY APPEARED 5 HOURS AFTER TURNING THE SWITCH ON. ALSO OVHT LIGHT STILL ON. FOUND DAMAGED CONNECTOR (D2216) TO TEMP SWITCH AND DAMAGED CONNECTOR (D464) TO S28. REPLACED D2216 AT S317, SYSTEM CKS OK. ALL INDICATION NORMAL.

Part: ATTACH FITTING — CRACKED (TE FLAP) · airframe 71,467 hrs · 11,668 cycles

LT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING.

Part: FITTING — CRACKED (TE FLAP) · airframe 71,467 hrs · 11,668 cycles

LT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING.

Part: RIB — CRACKED (LT WING) · airframe 71,467 hrs · 11,668 cycles

LT WING O/B LEADING EDGE CAVITY, LWR RIB FWD END CRACKED AT OFSS 688. MAJOR REPAIR ACCOMPLISHED. REMOVED RIB, INSTALLED NEW RIB AND LOWER STRUT.

Part: RIB — CRACKED (LT WING) · airframe 71,467 hrs · 11,668 cycles

LT WING O/B LEADING EDGE CAVITY LWR RIB FWD END CRACKED AT OFSS 547. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED DOUBLER TRIMMED DAMAGE AND INSTALLED DOUBLER.

Part: FLANGE — BROKEN (GEAR BOX) · airframe 71,467 hrs · 11,668 cycles

NR 1 ENG ANGLE GEAR BOX AFT END HAS LOOSE BOLTS AT 12:00 AND FLANGE EAR IS BROKEN AT 1:00.

Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 71,345 hrs · 11,651 cycles

LOST LEFT GEN DUE TO LEFT DRIVE LIGHT. REPLACED LEFT IDG. RAN ENGINE FOR 5 MIN. IDG OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,309 hrs · 11,645 cycles

SEAT EEL SECTION 19L TO 23L INOP. REPLACED BATTERY CHARGER AND BATTERY. OPS CHECKED, OK.

Part: FIRE LOOP — FAULTY (NR 1 NACELLE) · airframe 71,113 hrs · 11,614 cycles

L ENG FIRE LOOP 1 ON STATUS PAGE AND FIRE-OVHT SYS ON EICAS, ABORTED TAKEOFF AT 63 KNOTS. RESISTANCE HIGH AT CARD M681 PINS 19 & 20. CHECKED ENG 1 LOOPS . LOOPS OK. FOUND BAD LUG ON FWD BOTTOM LOOP. REPLACED LUG. RESISTANCE CHECKS NORMAL. SYSTEM TESTED OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,703 hrs · 11,554 cycles

LT AISLE OVERHEAD EXIT SIGN AT FWD ECONOMY CABIN MISSING LENSE. *S/D* REPLACED CALL LIGHT HOUSING. ALL OKAY.

Part: GUIDE VANE — DAMAGED (LT ENGINE) · airframe 70,492 hrs · 11,521 cycles

BIRD STRIKE TO LT ENG. ABORTED TAKEOFF AT 120 KNOTS. *S/D* ACCOMPLISHED ENGINE CORE BORESCOPE INSPECTION, NO DAMAGE. FOUND 3 FAN EXIT GUIDE VANE BASES DAMAGED AT 4 O'CLOCK. REPAIRED PER AMM 72-33-02-801. SUBSEQUENT ENGINE GROUND RUNS OK. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 70,256 hrs · 11,488 cycles

EEL LIGHTS AT LEFT HAND MID CABIN EMERGENCY EXITS INOP. FOUND POWER SUPPLY FAULTY. REPLACED POWER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,840 hrs · 11,430 cycles

EEL LIGHTS ON LT SIDE AT 19 - 22 INOP. *S/D* SUSPECT FAULTY POWER SUPPLY ASSEMBLY. REPLACED POWER SUPPLY, AC OK FOR SERVICE.

Part: FCU — FAULTY (APU) · airframe 69,514 hrs · 11,382 cycles

RTBL WITH A AUXILIARY POWER UNIT DOOR MESSAGE. RECURRED ON FLT 0907-11. REPLACED FUEL CONTROL UNIT. ACCOMPLISHED INSPECTION AS PER MM. ALL OPS AND INDICATIONS NORMAL, LEAK CHECK GOOD. ACCMP VERIFICATION FLIGHT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 69,514 hrs · 11,382 cycles

RTBL WITH A AUXILIARY POWER UNIT DOOR MESSAGE. REOCCURRED ON FLT 0907-11.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 69,488 hrs · 11,377 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. SUSPECT FAULTY ACTUATOR. REPLACED RUDDER TRIM ACTUATOR IAW MM 27-21-11. AC OK FOR SERVICE.

Part: APU — SHUTDOWN · airframe 69,439 hrs · 11,366 cycles

APU AUTO SHUT DOWN.

Part: CONNECTOR — DIRTY (APU) · airframe 69,439 hrs · 11,366 cycles

APU AUTO SHUT DOWN. REMOVED & CLEANED FUEL CONTROL UNIT CONNECTOR. APU STARTS AND RUNS NORMAL.

Part: GCU — FAULTED (NR 1) · airframe 69,007 hrs · 11,304 cycles

EICAS MSG L GEN OFF DISPLAYED. SUSPECT FAULTY BEARING IDG. REPLACED GENERATOR PER AMM24-11-01 AND GCU PRECAUTIONARY OPS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: BOTTLE — READS LOW (ESCAPE SLIDE)

ESCAPE SLIDE BOTTLE LOW .

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,437 hrs · 11,227 cycles

THE 2L EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED PART NUMBER 563-3045. OP CHECKS OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 68,437 hrs · 11,227 cycles

THE 13B SEAT EMERGENCY LIGHT INOP. SECURED UNDER SEAT CONNECTOR. LIGHT OP CHECKS OK.

Part: MONITOR — MALFUNCTIONED (CABIN) · airframe 68,124 hrs · 11,186 cycles

ELECTRICAL ODOR COMING FROM VIDEO MONITOR LOCATED AT SEAT 8J. UNIT THEN SHUT DOWN. THE UNIT WAS CONFIRMED TO BE INOPERABLE BY PACTECHNICIAN. AFTER INSPECTING ALL RELATED WIRING ASSOCIATED WITH THIS CIRCUIT, THE UNIT WAS REPLACED WITH A SERVICABLE UNIT AND OPS CHECKED SATISFACTORY. THE SERVICABLE UNIT HAS BEEN ROUTED TO PAC REPAIR STATION FOR FURTHER INVESTIGATION ON FEB 1. GOOD-IN INSPECTION CONFIRMED THAT THE UNIT HAS A SLIGHT ELECTRICAL ODOR. TEAR DOWN REPORT TO FOLLOW.

Part: ASPIRATOR — LEAKING (EVAC SLIDE)

ASPIRATOR LEAKING. REPLACED ASPIRATOR, CKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,613 hrs · 11,115 cycles

EMERGENCY PATH LIGHTS OUT AT ROW 24-33 AND 38A.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,263 hrs · 11,064 cycles

AT ROW 29AB LEFT OVERHEAD CEILING LIGHT EMERGENCY EXIT IS OUT. REPLACED LIGHT BULB. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (AFT GALLEY) · airframe 66,569 hrs · 10,940 cycles

LARGE AFT GALLEY EEL STRIP IS INOPERATIVE. REPLACED EEL STRIP. CHECKS GOOD.

Part: CAP — LOOSE (EMERGENCY LIGHT) · airframe 66,569 hrs · 10,940 cycles

F/A REPORTS AISLE LIGHT AT SEAT 1B END CAP IS COMING OFF. INSTALLED CAP AND SECURED CONNECTOR AND EEL CHECKS GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 66,569 hrs · 10,940 cycles

FWD LEFT AND MID LEFT LAV FLOOR EEL STRIPS ARE INOPERATIVE. SECURED CONNECTOR. CHECKS GOOD.

Part: LIGHT — MISSING (SEAT 2E) · airframe 66,569 hrs · 10,940 cycles

EEL LIGHT MISSING BY SEAT 2E. INSTALLED LIGHT. CHECKS GOOD.

Part: CAP — OUT OF POSITION (CABIN) · airframe 66,500 hrs · 10,926 cycles

F/A REPORTS AISLE LIGHT AT SEAT 1B END CAP IS COMING OFF. [08-14-07] SHORT EEL STRIP IN FRONT OF END CAP HAS BROKEN END PINS AND DOES NOT ILLUMINATE. REPLACED EEL STRIP. AIRPLANE OK FOR SERVICE.

Part: MODULE — MALFUNCTIONED (CABIN) · airframe 66,255 hrs · 10,884 cycles

SMOKE REPORTED COMING FROM SEAT 5D UPON DEPLANING. COCKPIT CONFIRMED SMELL. FOUND VDB FAILED, SOME INTERNAL COMPONENTS OVERHEATED. NO OTHER DAMAGE TO WIRING OR OTHER COMPONENTS. REPLACED SEAT 5CD VIDEO DISTRIBUTION BOX. SYSTEM OP CHECKED OK.

Part: FAN — FAULTY (CARGO BAY) · airframe 65,635 hrs · 10,781 cycles

RTFL DUE TO 'BULK CARGO VENT STATUS MESSAGE'. *S/D* BULK CARGO FAN STATUS MESSAGE, MSG GONE WITH BULK HEAT SWITCH IN NORM. ANIMALS REMOVED FROM AFFECTED COMPARTMENT. REPLACED BULK CARGO PIT VENT FAN. A/C COMPARTMENT NOW SERVICEABLE.

Part: PLATE — CRACKED (BS 642) · airframe 65,619 hrs · 10,774 cycles

FWD PIT, FWD CARGO DOOR CUTOUT, LOWER MAIN SILL AREA, STA 642, UPPER BEAM CHORD PLATE HAS CRACK INDICATIONS, RBL 60. [SUP 06-01-07] VERIFIED CRACK INDICATIONS PER HFEC INSPECTION. FOUND SILL CRACKED APPROX. 4.5 INCHES LONG. REMOVED LOWER DOOR SILL AND REPLACED WITH PN 451T1604-4 AND INSTALLED PER SRM 51-40-2. A/C OK FOR SERVICE. SUSPECT MULTIPLE IMPACTS FROM CARGO & LOADING EQUIP CAUSED INITIAL CRACK.

Part: DOOR FRAME — PUNCTURED (CARGO DOORWAY) · airframe 65,619 hrs · 10,774 cycles

AFT PIT DOOR CUTOUT FRAME AFT SIDE JUST UNDER THE APU BATTERY DOOR FRAME WEB PUNCTURED. MAJOR REPAIR ACCOMPLISHED: CUTOUT FRAME WEB DAMAGE. FABRICATED & INSTALLED DOUBLER, SHIMS & FILLER REPAIR.

Part: CIRCUIT BREAKER — FAULTY (EVAC SIGNAL) · airframe 65,619 hrs · 10,774 cycles

THE EVAC SIGNAL CIRCUIT BREAKER ON THE P6- 1 (F2) POPS WHEN THE EMERGENCY EVAC SWITCH IS HIT. [SUP 06-01-07] REPLACED EMER. EVAC MODULE AT AFT RT PANEL 22. OP CHECKS NORMALLY.

Part: LIGHT — BROKEN (CABIN) · airframe 65,619 hrs · 10,774 cycles

EEL LIGHT BAR AT THE AFT GALLEY AREA IS BROKEN. REPLACED LIGHT BAR. OPS CHECKS NORMAL.

Part: HOSE — KINKED (O2 MASKS) · airframe 65,619 hrs · 10,774 cycles

MAIN CABIN O2 MASK HOSES KINKED SEAT ROWS 2 CENTER, 1 EA 2 RT 1 EA 35 RT 1 EA 35 CENTER, 2 EA 1 EA AT 18C AND R, 29C AND R, AND 17C AND R. REPLACED MASKS WITH KINKED HOSES PER MM35-21-04. CLOSED PSU'S PER MM35-21-04. A/C READY FOR SERVICE. SUSPECT KINKING CAUSED BY IMPROPER PACKING.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

STA 246 FLOORBEAM UPPER WEB CRACKED OUT OF LWR FASTENER AT LBL 21. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

MAIN CABIN FLOORBEAM INTERCOSTAL UPPER ANGLE CRACKED AT STA 337, LBL 41. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. FABRICATED & INSTALLED NEW ANGLE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

AFT CARGO PIT FRAME UPPER CHORD CORRODED AROUND FASTENER HOLES STA 1197, LBL 42 TO RBL 42. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INSTALLED ANGLE REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

STA 246 FLOORBEAM LBL 11 AFT SIDE MID CHORD CRACKED AT LWR RADIUS NEAR FASTENER. MAJOR REPAIR ACCOMPLISHED: CUT OUT CHORD DAMAGE FROM LBL 59 TO RBL 49. FABRICATED & INSTALLED REPAIR ANGLE, STRAPS & MID CHORD.

Part: CABLE — DISENGAGED (EVAC SLIDE) · airframe 65,619 hrs · 10,774 cycles

LT AFT MED SLIDE RELEASE CABLE DISENGAGED. [SUP 05-18-07] RE-ENGAGED SLIDE RELEASE CABLE PER MM 25-66-00. READY FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT CABLE DISENGAGED BY CONTACT WITH CABIN SERVICE EQUIPMENT DURING LOADING/UNLOADING.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 65,619 hrs · 10,774 cycles

NR 2 ENG PYLON PNL CUT OUT CRACKED AT UPR FWD CORNER LOCATED ON I-B PYLON SKIN ACCESS HOLE CUT OUT JUST FWD OF HYD BAY. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK. FABRICATED & INSTALLED DOUBLER REPAIRS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

LIGHTNING STRIKE AT STA 760, BELOW STR 4L. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. INSTALLED FILLER AND DOUBLER.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

CABIN UNDER FLOORBOARD #P23, INTERCOSTAL UPPER ANGLE IS CRACKED AT STA 293, RBL 36. MAJOR REPAIR ACCOMPLISHED: REMOVED LINE REPAIR. FABRICATED & INSTALLED FILLER & EXTERNAL DOUBLER REPAIR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

CABIN SEAT TRACK AT BS 770 AND LBL 54 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION & DAMAGED SECTION OF SEAT TRACK. FABRICATED & INSTALLED SEAT TRACK SECTION, SPLICE PLATE & SPLICE CHANNEL.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 65,619 hrs · 10,774 cycles

MAIN CABIN FLOOR BEAM INTERCOSTAL SUPPORT BRACKET CRACKED STA 1503, LBL 67. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW BRACKET.

Part: POWER CABLE — OUT OF POSITION (CABIN) · airframe 10,249 hrs · 10,720 cycles

EEL LIGHTING 1EF AND 2EF RIGHT SIDE WIRES STICKING UP AND NOT WORKING. REINSTALLED & RESECURED LIGHT STRIP AND POWER CABLE, BOTH POSITON EEL OP CHECK OK.

Part: ASPIRATOR — LEAKING (ESCAPE SLIDE) · airframe 63,613 hrs · 10,422 cycles

SLIDE ASPIRATOR LEAKING.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 63,747 hrs · 10,450 cycles

NR 2 ENG STRUT SIDE SKIN PANEL AT FWD TORQUE BOX ACCESS HOLE CRACKED THRU EXISTING FASTENER, AND VERIFIED AND END MARKED BY HFEC INSPECTION. REQ STRUCTURAL REPAIR MANUAL REPAIR. STOP DRILLED HOLE, NR 2 ENG PYLON OTBD WEB RPR. DRILLING OUT FASTNERS, HAVE MATERIAL FOR DOUBLER-TRIPLER RPR. DBLR TRPLR MFG'D,TRIMMED & DRILLED. INSTALLED FSTNR. HAVE THRUST REVERSER HINGE FTG BACK FROM SHOP. ACCOMPLISHED INSTALLATION. ACCOMPLISHED RECHECK, OK FOR SERVICED

Part: LATCH — FAILED (CABIN)

RT OVERWING COMPT DOOR LATCHES FAILED TORQUE CHECK. REPLACED LATCHES. IAW B767, MM 25-65-98.

Part: SKIN — LIGHTNING STRIKE (BS 1587) · airframe 59,711 hrs · 9,780 cycles

LIGHTNING STRIKE AT LEFT FUSELAGE STA 1587 JUST AFT OF PRESSURE BULKHEAD. *S/D* LIGHTNING STRIKE DAMAGE CUT OUT AND REPAIRED PER SRM.

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 57,161 hrs · 9,384 cycles

LOSS OF BOTH PACKS CAUSED RESULTANT PRESSURIZATION PROBLEM. ALTHOUGH RT PACK WAS DEFERRED IN STANDBY MODE PER MEL AT THE TIME OF THE EVENT, THERE IS NO RECORD OF ANY DEFECT OR MAINTENANCE ACTIVITY AGAINST THE LT PACK, PRIOR TO OR AFTER THE EVENT. RT PACK COMPRESSOR OUTLET TEMP SENSOR AND RT PACK RAM AIR INLET ACTUATOR WERE BOTH REPLACED. MAINTENANCE ALSO REPLACED LT BLEED ISOLATION VALVE DUE TO DAMAGED BUTTERFLY SEAL. HOWEVER, NONE OF THE AVAILABLE DATA EXPLAINS LOSS OF CABIN PRESSURIZATION.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 56,795 hrs · 9,323 cycles

NR 2 CARGO FIRE SQUIB DOES NOT TEST. FOUND 757 TYPE APU/CARGO FIRE CONTROL PANEL INSTALLED. WITH THAT PANEL INSTALLED, THE NO. 2 CARGO SQUIB TEST LAMP WILL NOT LIGHT DUE TO DIFFERENT INTERNAL CIRCUITRY IN THE PANEL, PANEL WAS REPLACED WITH 767-322 TYPE APU/CARGO FIRE CONTROL PANEL.

Part: ATTACH ANGLE — CRACKED · airframe 47,989 hrs · 7,836 cycles

AFT CARGO PIT AT BS 1087 AND LBL 26, INTERCOSTAL ATTACH ANGLE TO FRAME, IS CRACKED MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE.

Part: FRAME — CRACKED · airframe 47,989 hrs · 7,836 cycles

AFT CARGO PIT AT BS 1087 AND RBL 26, INTERCOSTAL ATTACH ANGLE TO FRAME, IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED ANGLE.

Part: STIFFENER — CRACKED (FLOORBEAM) · airframe 47,989 hrs · 7,836 cycles

RIGHT NOSE TUNNEL AT BS 246, RBL 40, FLOORBEAM INTERCOSTAL ATTACH ANGLE STIFFENER IS CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW STIFFENER.

Part: PUMP — FAILED (RT ENGINE) · airframe 47,217 hrs · 7,723 cycles

RIGHT ENGINE DRIVEN HYDRAULIC PUMP FAILED. DIVERTED TO JFK. NR 2 ENGINE PUMP FAILURE. REPLACED PUMP AND APPLICABLE FILTERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,648 hrs · 6,920 cycles

MAIN CABIN FLOORBEAM STATION 798 LBL 19-15 UPPER CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FLOORBEAM SPLICE PER SRM 53-00-51 FIG 203.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,648 hrs · 6,920 cycles

EXTERNAL FUSELAGE SKIN DENTED AND REPAIRED AT BODY STATION 323 LBL 32. MAJOR REPAIR ACCOMPLISHED AND INSPECTED AT FUSE SKIN BODY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,648 hrs · 6,920 cycles

FUSELAGE SKIN HOLE ELONGATED LOCATED BETWEEN STRINGER 19L-20L BODY STATION 1473. MAJOR REPAIR ACCOMPLISHED PER SRM 51-20-07.

Part: STRINGER (BODY STATION 180) · airframe 42,648 hrs · 6,920 cycles

APPROXIMATELY BODY STATION 180 STRINGER 25R HAS 2 EACH BLIND FASTENERS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPALCED 2 EACH BLIND FASTENERS WITH SOLID FASTENERS.

Part: SHUTOFF VALVE — FAILED (LT ENGINE) · airframe 42,553 hrs · 6,902 cycles

LEFT ENG HPSOV EICAS DURING CLIMB AND CRUISE. REPLACED LT ENG HPSOV. FAULT WAS IN HPC.

Part: BLADE — FRACTURED (NR 1 ENGINE) · airframe 42,436 hrs · 6,880 cycles

VIBRATION ON NR 1 ENGINE, EEC MODE EICAS ILLUMINATED, EGT FLUCTUATED BETWEEN 120 AND 180 AT IDLE, EPR INDICATION LOST, N1 & N2 INDICATIONS NORMAL. CREW ELECTED TO SHUT DOWN ENGINE AND RETURN TO FIELD. *S/D* 1 EA T2 BLADE FAILED AT THE PLATFORM. 2 EA ADJACENT BLADES WERE BROKEN OFF AT MID SPAN. THE RESULTANT HIGH N2 VIBRATION CAUSED THE P4.95 MANIFOLD TO FAIL WHICH CAUSED LOSS OF EPR INDICATION AND REVERSION TO ALTERNATE MODE. ENGINE WAS REMOVED FOR REFURBISHMENT.

Part: OVEN — DIRTY (GALLEY) · airframe 39,032 hrs · 6,317 cycles

AFTER T-O GALLEY PWR TURNED ON AT MID GALLEY AND ELECTRICAL ODOR SMELLED. NO SMOKE NOTED. CIRCUIT BREAKER U-6 PULLED. SUPPLEMENTAL DATA UPDATE AFTER CIRCUIT BREAKER U-6 WAS PULLED, THE ODOR DISSIPATED. CREW REPORTED THE ODOR ONLY DURING THE OPENING OF THE OVENS IN THE AFT-MID GALLEY. THE OVEN INTERIORS FAN SCREEN WAS CLEANED OF FOOD DEBRIS. THE REAR CONNECTORS ON ALL THE OVENS AND COFFEEMAKERS WERE CHECKED AND CLEANED. ALL GALLEY EQUIPMENT WAS RAN FOR OVER TWO HOURS AND NO ABNORMAL ODORS WERE NOTED. NO FURTHER INCIDENCES REPORTED.

Part: BATTERY PACK — INOPERATIVE (OVERWING) · airframe 37,402 hrs · 5,997 cycles

PRIOR TO DEPARTURE OVERWING ESCAPE SYSTEM SQUIB TEST 1 AND 2 INOP BOTH LEFT AND RIGHT SIDES. *S/D* REPLACED LT OVERWING SLIDE BATTERY PACK AND CHARGER.

Part: BRACKET — LOOSE (AC DUCT)

FL 410, CREW REPORTED AT SMOOTH CRUISE A NOTICEABLE POP NOISE HEARD BY CREW AND FA'S. FA'S REPORTED A VIBRATION AT THE FLOOR LEVEL IN THE MID GALLEY AREA. NOTE ALL ENGINE PARAMETERS, BLEEDS, PACK OPERATIONS WERE NORMAL. RETURNED TO IAD, OVERWEIGHT LANDING. *S/D* BRACKET THAT SUPPORTS EXTERNAL AIR CONDITIONING CONNECTOR WAS NOT SECURED. IAD REMOVED BRACKET AND RESECURED BRACKET TO DUCT. JFK INSPECTED THE DUCT AND BRACKET AND FOUND IT TO BE SECURED. BOS COMPLETED EG5268 WHICH CHECK THE CONDITION AND SECURITY OF THE DUCT, BRACKETS, AND RODS. ALL WERE REPORTED TO BE IN GOOD CONDITION.

Part: BRAKES — SMOKING (LANDING GEAR)

DURING TAXI, ANOTHER AIRCRAFT PILOT REPORTED SEEING SMOKE COMING FROM THE RIGHT MAIN LANDING GEAR. *S/D* UPON FURTHER INSPECTION IN THE LT AND RT GEAR AND WHEEL WELLS, FOUND NO EVIDENCE OF SMOKE OR DEFECTS. BRAKE TEMPS WERE WITHIN LIMITS.

Part: SENSOR — DIRTY (CARGO DOOR)

AFTER TAKEOFF, RETURNED TO JFK DUE TO A FORWARD CARGO DOOR WARNING LIGHT. SUPPLEMENTAL DATA UPDATE: SENSORS S214 AND S215 WERE DIRTY AND OUT OF ADJUSTMENT. CLEANED AND ADJUSTED SENSORS AND REPLACED PSEU DRIVER CARD (A3). ALL INDICATIONS NORMAL AFTER BITE CHECK.

Part: IDG — FAILED (RT ENGINE)

DURING TAXI OUT, THE RIGHT INTEGRATED DRIVE GENERATOR FAILED. AIRCRAFT RETURNED TO GATE. SUPPLEMENTAL DATA UPDATE: RIGHT INTEGRATED DRIVE GENERATOR REPLACED FOR FAILED DIODES.