N174DN

Part: LENS — MISSING (ZONE 200) · airframe 150,247 hrs · 22,424 cycles

RED EMERGENCY LIGHT LENS LOCATED AT RT AFT LAV EXTERIOR WALL MISSING. INSTALLED RED LENS COVER (7788250)

Part: AUTOTHROTTLE SYS — FAULTED · airframe 149,921 hrs · 22,353 cycles

ATO- A/T DISCONNECT ON T/O ROLL WITH ABORT AT APPROXIMATELY 60 KTS. MEL APPLIED. FOLLOW UP: TMC FAILED DURING RTS TEST. R/R TMC. BOTH A/T DISCONNECT SWITCHES REPLACED PER MCC REQUEST.(4993858)

Part: LENS — MISSING (ZONE 200) · airframe 148,617 hrs · 22,105 cycles

EMERGENCY LIGHT LENS COVER AT ROW 17GF MISSING. INSTALLED EMERGENCY LIGHT LENS REF B767 AMM 33-51.

Part: MODULE — INOPERATIVE (ZONE 800) · airframe 148,171 hrs · 22,023 cycles

SHIP 0174 1R SLIDE ARM LIGHT INOP. CORRECTIVE ACTION: R/R DOOR 1R ALARM SIGNAL MODULE AS PER B767-300 AMM 52-73. (1040051).

Part: SENSOR — FAULTED (ZONE 800) · airframe 147,712 hrs · 21,933 cycles

SHIP 0174 -ATB- FLIGHT RETURNED TO ATL DUE TO FWD CARGO DOOR EICAS MESSAGE AND DISCRETE LIGHT. CREW DID DECLARE AN EMERGENCY WITH ATC. MAINTENANCE DEFERRED THE DOOR INDICATION SYSTEM PER MEL 52-71-01. ON 08MSY25 IN ATL THE PSEU FAULTED SENSOR S215 WAS REPLACED PER THE AMM AND THE DEFERRAL WAS REMOVED. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP #7155132)

Part: LENS — MISSING (ZONE 200) · airframe 146,937 hrs · 21,779 cycles

AT 16AB, THE OVERHEAD EMERGENCY EXIT SIGN IS MISSING THE LENS. MAINTENANCE INSTALLED A LENS AND SECURED AS REQUIRED. (LP #6867620)

Part: ADC — FAULTED (RIGHT) · airframe 146,789 hrs · 21,751 cycles

SHIP 174 -RVSM- DURING FLIGHT ALTITUDE DISAGREE EICAS MESSAGE AND CAUTION. QRH PROCEDURE APPLIED, CA/STBY/FO ALTIMETERS INDICATED 31240/31500/ 31000 WHILE DESCENDING THROUGH FL310. CORRECTIVE ACTION: R/R RT ADC PER B767AMM 3412 OPS TEAT GOOD. (6378263)

Part: DOOR SILL — FOD (ZONE 800) · airframe 146,198 hrs · 21,629 cycles

SHIP 174 UNABLE TO ARM 1L DOOR AT DEPARTURE. CORRECTIVE ACTION: FOUND PALSTIC SEAL IN/ON DOOR SILL. REMOVED IT AND NOW DOOR ARKS /DISARMS NORMALLY PER B767 AMM 52-11. (6638386)

Part: PAWL — BROKEN (R1 DOOR) · airframe 146,146 hrs · 21,619 cycles

SHIP 174 1R DOOR SLIDE WILL NOT ARM. CORRECTIVE ACTION: DURING CATERING SVC 1R SVC DOOR INTERLOCK PAWL WAS BROKEN. R/R 1R INTERLOCK PAWL IAW 767 AMM 52-11-26. OPS CHK GOOD A/C OK FOR SVC. (6638372)

Part: LENS — DAMAGED (ZONE 200) · airframe 145,983 hrs · 21,587 cycles

SHIP 174 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:605. CORRECTIVE ACTION: RE-SECURED LOC 605 EXIT COVER CKS GOOD OK FOR SVC. (0620330)

Part: SIGN — DAMAGED (ZONE 200) · airframe 145,983 hrs · 21,587 cycles

SHIP 174 PASSENGER DAMAGED EXIT SIGN. CORRECTIVE ACTION: RESECURRED EXIT SIGN AS REQUIRED (6487372)

Part: PAWL — WORN (R2 DOOR) · airframe 145,937 hrs · 21,578 cycles

SHIP 174 2R DOOR HARD TO ARM GIRT BAR. CORRECTIVE ACTION: FOUND 2R DOOR INTERLOCK PAWL WORN CAUSING HANDLE TO STICK OUT. R /R INTERLOCK PAWL PER B767 AMM 52-11. ALL OPS NML. (0602392)

Part: SIGN — LOOSE (ZONE 200) · airframe 145,248 hrs · 21,448 cycles

SHIP 174 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:604. CORRECTIVE ACTION: RESECURED 'EMERGENCY EXIT SIGN'. (0511191)

Part: DOOR — FOD (ZONE 800) · airframe 145,197 hrs · 21,438 cycles

SHIP 174 2 RIGHT DOOR LEVER WON'T ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM DOOR. OPS CHECK GOOD PER B767 AMM 52-11 (5703982)

Part: SIGN — DETACHED (CABIN) · airframe 144,248 hrs · 21,267 cycles

SHIP 174 A/C EXIT SIGN FOUND ON GROUND, A/C RIGHT SIDE BY CONFORT PLUS. CORRECTIVE ACTION: INSTALLED EXIT SIGN RT SIDE BY CONFORT PLUS ALL NML. (5330936)

Part: HANDLE — DISLODGED (R1 DOOR) · airframe 144,248 hrs · 21,267 cycles

SHIP 174 DURING IN-FLIGHT R1 DOOR HANDLE BECAME SLIGHTLY UN-SEATED. SLIDE LIGHT EXTINGUISHED. ARMED LIGHT ON FA PANEL STAYED ILLUMINATED . VIA MX SUGGESTION, HANDLE WAS PUSHED AND RE-SECURED. SLIDE LIGHT ILLUMINATED. CORRECTIVE ACTION: COMPLETED INTERNAL AND EXTERNAL MANUAL OPERATION OF DOOR R1 OPEERATIONAL TES IAW B767/200/300 AMM 52-11-715-128 WITH OK RESULTS. (5330920)

Part: DOOR — FOD (R1) · airframe 143,680 hrs · 21,165 cycles

SHIP 174 1R DOOR DOES NOT ARM. CORRECTIVE ACTION: CYCLED 1R DOOR,RMVD FOD. 1R DOOR IS SECURED CLOSED AND ARMED. A/ C OK FOR SVC. (5328502)

Part: SIGN — DETACHED (CABIN) · airframe 143,572 hrs · 21,144 cycles

EXIT SIGN 2R FELL OFF. CORRECTIVE ACTION: RESCURED SIGN CKS OK.

Part: FLAG — INOPERATIVE (R1 DOOR SLIDE) · airframe 143,572 hrs · 21,144 cycles

SHIP 174 1R DOOR SLIDE ARMING FLAG INOP. CORRECTIVE ACTION: R/R 1R DOOR ARMING FLAG PER B767 AMM 52-73. (0285564)

Part: NONE — NONE (NONE) · airframe 143,538 hrs · 21,135 cycles

SHIP 174 UNABLE TO ARM R2 DOOR AT DEPARTURE. CORRECTIVE ACTION: 2R DOOR ARMS NORMAL PER B767 MM 52-11 (5255846)

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 143,366 hrs · 21,103 cycles

SHIP 174 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: R/R THE 1R DOOR SLIDE LIGHT AS PER B767-300 AMM 33-51. (0252735)

Part: NONE — NONE (R1 DOOR) · airframe 143,366 hrs · 21,103 cycles

SHIP 174 R1 MAIN DOOR WILL NOT ARM. CORRECTIVE ACTION: PPERFORMED OPS CHK OF R1 DOOR AS PER B767 AMM 52-11. OPS CHK NML. (5746978)

Part: LENS — UNSECURE (INDICATOR) · airframe 143,340 hrs · 21,098 cycles

SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. SECURED LENS FOR SLIDE DOOR 602 INDICATOR. OPS NORMAL OK FOR SVC (0248513)

Part: DOOR — UNKNOWN (CABIN) · airframe 143,175 hrs · 21,065 cycles

SHIP 174 2R CABIN DOOR JAMMED / WILL NOT ARM. CORRECTIVE ACTION: CYCLED DOOR 2R OPEN/CLOSE. DOOR ARMS OK PER B767-300ER AMM 52-11 . (5746900)

Part: DOOR — BINDING (R1) · airframe 142,955 hrs · 21,014 cycles

SHIP 174 FA REPORTS 1R DOOR DIFFICULT TO ARM. CORRECTIVE ACTION: CYCLED 1R DOOR ARM AND DISARM. CHECKS GOOD. (4405814)

Part: STRUCTURE — CORRODED (WALL MOUNT) · corrosion level 2 · airframe 142,928 hrs · 21,009 cycles

SHIP 174 FOUND THE STRUCTION UNDER THE MOUNT WALL CORRODED. CORRECTIVE ACTION: CORROSION REPAIRED AS PER PRI 615167-14 (0173686)

Part: FRAME — CRACKED (BS 927 RBL 90) · airframe 142,928 hrs · 21,009 cycles

SHIP 174 FOUND FRAME END FITTING CRACK AT STA 927 RBL90. CORRECTIVE ACTION: CRACK LENGTH IS 1.3"; REMOVED AND REPLACED THE CRACKED FRAME END FITTING AT STA 927; RBL 90 AS PER B767-300 SRM 51-40-02 (0170400)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 142,591 hrs · 20,941 cycles

SHIP 174 DURING SVC FOUND EMG LIGHT ON SEAT 40 F INOP. CORRECTIVE ACTION: FOUND GND WIRE CUT BEFORE BATTERY ON SEAT 40F APPLIED SPLICE IAW BOEING SWPM CH 20-30-12 LIGHT TEST OK (5041897)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 142,381 hrs · 20,894 cycles

SHIP 174 MAIN ENTRY/SERVICE DOOR ARMED INDICATORS R1 DOOR. CORRECTIVE ACTION: R/R 1R DOOR SLIDE LIGHT AS PER B767 AMM 52-73. OPS CHK GOOD NO FURTHER DEFECTS. THIS CLEARS MEL PLACARD REMOVED. (0063157)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 142,391 hrs · 20,896 cycles

SHIP 174 FUSELAGE / STR 39L / STA 1307 TO STA 1373 / CORROSION, CRACKS AND HOLE. CORRECTIVE ACTION: THIS IS A DTA MONITOR INSPECTION LOG FOR ER/A 603441-14 REV B. STAGE 3 DTA APPROVAL IS REQUIRED ON OR BEFORE 37,500 TOTAL AIRFRAME CYCLES. A 1,000 CYCLE PRIOR INITIAL CONTACT LIMIT WAS SETUP SO THAT STAGE 3 CAN BE REQUESTED FROM BOEING BEFORE THE THRESHOLD IS REACHED. (2933133)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,534 hrs · 20,589 cycles

SHIP 0174 -ATB- DUE TO LE SLAT ASYM INDICATION DURING CLIMB. CREW C/W QRH AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: REPLACED #10 PSEU CARD PER FIM 32-09-00. NO FAULT NOTED. (9906154)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,534 hrs · 20,589 cycles

SHIP 174 DOOR 2L SLIDE ARMED LIGHT ALWAYS ILLUMINATED. CORRECTIVE ACTION: PER B767-300 FIM 25-66-00-815-802 FOUND CARD IN PROX BOX BAD. REPLACED PROX BOX PER B767 AMM 32-66. TESTS OK. SLIDE LIGHT CHECKS OK. (9906160)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,331 hrs · 20,553 cycles

SHIP 0174 -MISC/DE- CREW ELECTED DE DUE TO TE FLAP DISAGREE MESSAGE WHEN FLAPS WERE SELECTED FROM 1 TO 5 ON APPROACH. FLAPS REMAINED IN 1. CREW C/W QRH, ALTERNATE FLAP EXTENSION SUCCESSFUL, AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: PERFORMED FSEU BITE PER FIM 27-51-00-815-809. NO EXISTING FAULTS. RAN FLAPS WITH PRIMARY POWER MULTIPLE TIMES WITH NO DEFECTS NOTED. REPLACED FLAP DRIVE UNIT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,305 hrs · 20,548 cycles

SHIP 0174 -MISC/DE- CREW ELECTED DE DUE TO TE FLAP DISAGREE INDICATION DURING APPROACH. CREW C/W QRH AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: R/R 3 FLAP POSITION XMTR. (LP 4796798)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,305 hrs · 20,548 cycles

SHIP 0174 -MISC/DE- CREW ELECTED DE DUE TO TE FLAP DISAGREE INDICATION DURING APPROACH. CREW C/W QRH AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: R/R FLAP DRIVE NML HYD AND ALT ELEC DRIVE MOTORS. REPLACING FLAP PDU. MTC IN PROGRESS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 140,293 hrs · 20,545 cycles

SHIP 0174 -MISC/DE- CREW ELECTED DE DUE TO TE FLAP DISAGREE INDICATION DURING APPROACH. CREW C/W QRH AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: LUBED FLAPS. R/R NBR 4 AND 5 FLAP POSITION XMTRS. (4796778)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 139,735 hrs · 20,455 cycles

SHIP 174 FOUND 521FB PANEL MISSING ON ARRIVAL, CORRECTIVE ACTION: INSTALLED 521FB IAW B767-300 IPC 57-41. A/C OK FOR SVC. (5118376)

Part: NONE — NONE · airframe 139,313 hrs · 20,380 cycles

SHIP 174 DURING SVC FOUND EMERG LIGHT OF ON SEAT 18GF INOP. CORRECTIVE ACTION: RECRIMED EMERG LIGHT WIRE ON 18GF PER SWPM CHAPTER 20. (9919668)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 139,103 hrs · 20,340 cycles

SHIP 174 CENTER WING / LH LOWER UNDERWING LONGERON FITTING REPLACEMENT / / SB 767-57A0126 REV 5 / TENSION BOLT HOLE DAMAGE. CORRECTIVE ACTION: ACCOMPLISH 596938-14 REV A SECTION II INSPECTION WITHIN THE FIRST OF EVERY 7000 CYC OR 19000 HRS BEGINNING AFTER SECTION I. (2611969)

Part: SHUTTLE VALVE — FAULTED (ANTI SKID SYS) · airframe 138,947 hrs · 20,310 cycles

CREW ELECTED DE DUE TO RT HYD QTY EICAS MESSAGE AND QUANTITY INDICATION LOW. C/W QRH AND LANDED NORMALLY. R/R LT AND RT ANTISKID SHUTTLE VALVES. A/C RTS.

Part: CABLE — MISINSTALLED (SLIDE BOTTLE) · airframe 138,957 hrs · 20,312 cycles

RIGHT SLIDE INFLATION BOTTLE TRIGGER CABLE BALL NOT INSTALLED BEHIND THE RETAINER SPRING. R & R RT SLIDE INFLATION BOTTLE IAW AMDS W/C #2561-4723-RH.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 138,763 hrs · 20,273 cycles

ROWS 21-30 EMERGENCY LIGHTS INOP ON BOTH SIDES. R & R BATTERY AND CHARGER (M9009) PER B767 AMM 33-51. OPS CHECK NORMAL.

Part: LENS — DAMAGED · airframe 138,645 hrs · 20,250 cycles

SHIP 174 DURING SVC CHECK FOUND OVERHEAD EXIT SIGN LENS AT ROW 16, RT HAND SIDE. CORRECTIVE ACTION: INSTALLED NEW LENS PER B767 AMM 33-20. CKS GOOD OK FOR SVC. (9480580)

Part: STRINGER — CORRODED (BS 1329 S39L) · corrosion level 2 · airframe 138,230 hrs · 20,170 cycles

SHIP 174 STR 39L CORRODED @ STA 1329 ON L/H SIDE UNDER UPPER FLANGE. CORRECTIVE ACION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 000-0001:5300-0780/009 00027 COMPLIED WITH ERA 603441-14 (2488871)

Part: SHEAR TIE — CORRODED (BS 1329 S38R) · corrosion level 2 · airframe 138,230 hrs · 20,170 cycles

SHIP 174 STA 1329 FRAME CLIP CORRODED ON FWD SIDE BETWEEN S38R, CORRECTIVE ACION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 000-0001:5300-0780/008 00026 COMPLIED WITH ERA 603444-14AD (2488856)

Part: NONE — NONE · airframe 138,228 hrs · 20,169 cycles

SHIP 174 PER ERA 603444-14, ACCOMPLISH SECTION 2 INSTRUCTIONS AT 37500 CYCLES, AND EVER 7500 CYCLES AFTER THAT. CORRECTIVE ACTION: AS PER ERA 603444-14AD ACCOMPLISH SECTION 2 REPETITIVE INSPECTIONS AS NOTED (2482492)

Part: NONE — NONE (UNKNOWN) · airframe 138,228 hrs · 20,169 cycles

ER/A 603441-14 NEEDS DTE WITHIN 12 MONTHS. MTC PERFORMED 28" X 5 " CUTOUT IN THE SKIN TO GAIN ACCESS AND REPLACE DAMAGED STR S- 39L BETWEEN STA 1307 AND 1329. CORRECTIVE ACTION: PER ER/A 603441-14 REV B, DTE STAGE 2 ACCOMPLISHED. DTE STAGE 3 IS TRACKED ON NEW LOG PAGE 2933133 AND IS REQUIRED ON OR BEFORE 37,500 TOTAL AIRFRAME CYCLES. PLEASE CLOSE THIS LOG PAGE. (2479295)

Part: NONE — NONE · airframe 138,175 hrs · 20,158 cycles

SHIP 174 CEILING EMERG LIGHT ABOVE 7D INOP. CORRECTIVE ACTION: R/R EMERGENCY LIGHT ASSY IAW B767-300 AMM 33-51. OPS CHK NML. NO FAULTS NOTED. (9391756)

Part: NONE — NONE · airframe 138,123 hrs · 20,148 cycles

SHIP 174 SEATS 22-30 AB EMERITS INOP, CORRECTIVE ACTION: REPLACED DISC FUSE IN M 9009.CKS GOOD PER B767 AMM 33-52 (9391735)

Part: NONE — NONE · airframe 138,007 hrs · 20,124 cycles

SHIP 174 FOUND EIXT EMERGENCY LIGHTS INOP NEXT TO 1L, LR DOORS AND CEILING EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R BATTERY PACK CHARGER AT M1208 PER B767 AMM 33-51. OPS CK NML . OK FOR SVC. (9677950)

Part: NONE — NONE · airframe 137,727 hrs · 20,067 cycles

SHIP 174 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:801, CORRECTIVE ACTION: ATTACHED MISSING SIGN PER B767 AMM 33-50 (2388414)

Part: LIGHT — INOPERATIVE · airframe 137,259 hrs · 19,976 cycles

AIRCRAFT 0174, EMERGENCY EXIT PATH LIGHT AT SEAT 32B INOP. CORRECTIVE ACTION: FOUND WIRE AT 32B DAMAGED. REPAIRED WIRE IAW B767 WDM 33-51-31. (8919116)

Part: NONE — NONE · airframe 137,182 hrs · 19,961 cycles

SHIP 174 1L DOOR ARMED INDICATION INOP OF FWD PANEL, CORRECTIVE ACTION: OPS CK OF MAIN/SVC DOOR ARMED INDICATION B767 AMM 52-00 WITH NTF (2314077)

Part: LIGHT — INOPERATIVE · airframe 136,475 hrs · 19,780 cycles

SHIP 174 EMERGENCY LIGHT SEATS 32-41 RT DO NOT WORK, CORRECTIVE ACTION: FOUND SHORT BEHIMD DOGHOUSE IN FRONT OF LAV 2R. REPATRED WIRE PER BOEING SWPM CHAPTER 20-30. OK FOR SVC. (8805164)

Part: UNKNOWN — UNKNOWN · airframe 136,278 hrs · 19,705 cycles

SHIP 174 PANEL / COVER MISSING, L/E RIGHT WING, JUST OUTBOARD OF RT ENGINE. CORRECTIVE ACTION: OK TO DEF TO CDL 57-41-02 (8791820)

Part: NONE — NONE · airframe 136,240 hrs · 19,684 cycles

SHIP 174 SEAT 23 FG EEPLS LIGHT HANGING. NOT SECURE. CORRECTIVE ACTION: RESECURED EEPLS LT ASSEMBLY. OPS CK GOOD. OK FOR SVC. REF CABIN GENERAL MTC CMM 25-00-66. (8791803)

Part: NONE — NONE · airframe 136,215 hrs · 19,662 cycles

SHIP 174 UPON ARRIVAL FOUND NBR 1 ENG NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: INSTALLED #1 ENG NACELLE STRUT ACCESS DOOR. REF B767-300 AMM 54- 53 (8257766)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 RH OFF WING SLIDE RAFT PACK FOUND CORROSION AT OUTER CARRIER. CORRECTIVE ACTION: REMOVED AND REPLACED RH OFF WING SLIDE REFER TO AMDS W/C 2561- 4697 (2126225)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND BULK CGO LOWER STRUCTURE STRINGER CORROSION AT STA1329-STA1351 S38R, CORRECTIVE ACTION: THE DAMAGED SECTION REPAIRED AS PER B767-300 SRM 53-00-03-2R. (2124391)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE SPLICE PLATE AT STA955 LBL36 WHEN CLEAN THE CANTED PRESSURE DECK DRAIN INLET AREA. CORRECTIVE ACTION: THE CORROSION AREA REPAIRED REFER TO NRC 200-123 (2124575)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND 01EA CRACK ON LH LOWER UNDER-WING LONGERON FITTING REPLACEMENT OF THE LOWER LH UNDER-WING LONGERON FITTING, CORRECTIVE ACTION: THE LOWER UNDER-WING LONGERON FITTING REPLACED PER W/C 5711- 01042-03. (2124824)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CABIN FUEL TANK UPPER SURFACE FOUND CORROSION AT STA954 LBL33, CORRECTIVE ACTION: THE CORROSION AREA REPAIRED REFER TO NRC 200-123 (2124566)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND BULK CGO LOWER STRUCTURE STRINGER RIVET CORROSION AT STA1480-STA1502 S38R, CORRECTIVE ACTION: THE DAMAGED SECTION REPAIRED AS PER B767-300 SRM51-40-02 RELEASE117.00 07JAN22. (2124404)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CABIN FUEL TANK UPPER SURFACE FOUND CORROSION AT STA955 LBL73, CORRECTIVE ACTION: THE CORROSION AREA REPAIRED AS PER PRI596574-14 (2124486)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND 2 DENTS COMMON TO FWD FUSELAGE RH SIDE BETWEEN STA148.75 AND STA164.75 AND 5.7" BELOW THE LAP SPLICE AT STR24, CORRECTIVE ACTION: REPAIRED AS PER PRI592090-14 REV.0. (2124700)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CABIN FUEL TANK UPPER SURFACE FOUND CORROSION AT STA955 BETWEEN LBL11 AND LBL33, CORRECTIVE ACTION: THE CORROSION AREA REPAIRED REFER TO NRC 200-123 (2124495)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 01EA CRACK ON RH LOWER UNDER-WING LONGERON FITTING REPLACMENT OF THE LOWER RH UNDER - WING LONGERON FITTING, CORRECTIVE ACTION: THE LOWER RH UNDER-WING LONGERON FITTING REPLACED PER W/C 5711- 01042-04. (2124816)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE STRINGER CORROSION AT STA1283-STA1305 S36L, CORRECTIVE ACTION: THE DAMAGE AREA REPAIRED AS PER B767-300 SRM53-00-03 (2123606)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE STRINGER CORROSION AT STA1373-STA1395 S39R, CORRECTIVE ACTION: THE CORROSION REPAIRED AS PER B767-300 SRM51-10-08 (2123645)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE STRINGER CORROSION AT STA1197+132-STA1219 S-39L, CORRECTIVE ACTION: THE CORROSION REPAIRED AS PER B767-300 SRM 53-00-03 (2123628)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE STRINGER CORROSION AT STA1329-STA1351 S39R, CORRECTIVE ACTION: THE CORROSION REMOVED AND DVI CARRIED OUT FOUND NO OTHER DAMAGE EVIDENT AS PER B767-300 SRM51-10-08 (2123637)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE STRINGER CORROSION AT STA1351-STA1373 S37L, CORRECTIVE ACTION: THE DAMAGE AREA REPAIRED AS PER B767-300 SRM53-00-03 (2123601)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 DURING C/O HFEC INSPECTION ON TENSION BOLT HOLE ON THE INTERNAL BATHTUB FITTING AT 9 O'CLOCK POSITION FOUND 1EA CRACK. CORRECTIVE ACTION: THE INTERNAL BATHTUB FITTING TENSION BOLT HOLE AT 9 O'CLOCK POSITION CRACK AREA REPAIRED REFER TO NRC NO.100-365 (2122295)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 ERA 592090-14 REV A ISSUED FOR REPAIR TO STA 157, S24R REPAIR DO UBLER. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 592090-14 REV A SECTION IV AT OR BEFORE 37500 TOT AL FLIGHT CYCLES (2123353)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND BULK CGO LOWER STRUCTURE STRINGER CORROSION AT STA1540-STA1562 S37L, CORRECTIVE ACTION: DAMAGE AREA REPAIR AS PER B767-300 SRM53-00-03 (2122188)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND BULK CGO LOWER STRUCTURE STRINGER CORROSION AT STA1439-STA1461 S37L, CORRECTIVE ACTION: THE DAMAGE AREA REPAIRED AS PER B767-300 SRM53-00-03 (2122200)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND BULK CGO LOWER STRUCTURE STRINGER CORROSION AT STA1439-STA1461 S38R, CORRECTIVE ACTION: DAMAGE AREA REPAIR AS PER B767-300 SRM53-00-03 (2122172)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 INTERNAL SECTION 48 STA1725 AT LOWER FWD APU INLET CUTOUT FOUND CRACK. CORRECTIVE ACTION: INTERNAL SECTION 48 STA1725 AT LOWER FWD APU INLET CUTOUT CRACK AREA REPAIRED AS PER PRI596987-14 REV.0. (2121143)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 DURING REMOVE FWD FASTENER FOR THE BLADE ON THE UNDER WING LONGERON FITTING FOUND LOWER DRAG SPLICE ANGLE TOOLING MARK. CORRECTIVE ACTION: THE LOWER DRAG SPLICE ANGLE FWD FASTENER HOLE TOOLING MARK REMOVED AND REPAIRED AS PER PRI596938-14 (2120477)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 THE FUS EXTERNAL SKIN SCRATCH AT BS1417 TO 1395 AND S -36L TO 38L. CORRECTIVE ACTION: REPAIRED AND DOCUMENTED AS PER DAL ER/ A476909-14. (2120408)

Part: NONE — NONE · airframe 136,164 hrs · 19,636 cycles

SHIP 174 ERA 596987-14AD ISSUED FOR REPAIR TO STA 1725.5, STR 7R. FOLLOW ON ACTION IS REQUIRED, CORRECTIVE ACTION: ACCOMPLISH ERA 596987-14AD SECTION II AT 37500 TOTAL FLIGHT CYCL ES, THEN EVERY 6000 FLIGHT CYCLES THEREAFTER (2121066)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 RHW NO.9 SLAT I/B ANTI-ICE DUCT SEAL SUPPORT RIB CRACK. CORRECTIVE ACTION: REPAIRED AS PER PRI596963-14 REV.0. (2120238)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 MTC TASK - FOUND AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA1329 S38R-S39R, CORRECTIVE ACTION: THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM51-40-02 (2118231)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1518 S36R-S37R, CORRECTIVE ACTION: THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM51-40-02 (2118245)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1518 S38R-39R, CORRECTIVE ACTION: THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM51-40-02 (2118226)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 ER/A 596938-14AD SECTION I WAS ACCOMPLISHED. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH REVISION OF ER/A 596938-14AD TO INCLUDE STAGE II OR III (2117309)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1395 S39L-S39R, CORRECTIVE ACTION: THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2117129)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA1329 S38L-S39L, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2115530)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO STRUCTURE STRINGER CLIP CORROSION AT STA1329 S38R, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2115527)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1219 S37L-S38L, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114728)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1373 S39R-S38R, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114707)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA1307 S37L-S38L, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114452)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND DOOR 2 LEFT ARMED LIGHT FLASHES WITH DOOR NOT ARMED. CORRECTIVE ACTION: FOUND PSEU INOP.REMOVED AND REPLACED PSEU AS PER B767-300 AMM 32-09. OPS NML. (2114436)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1395 S38R-S39R, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114462)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO STRUCTURE STRINGER CLIP CORROSION AT STA1329 S39R, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114732)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE SEAT TRACK AT STA347, RBL88.5, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114674)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1351 S38L-S39L, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114712)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1241 S35R-S36R, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114413)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1197+88 S39L-S39R, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114694)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO LOWER STRUCTURE SHEAR TIE CORROSION AT STA1373 S36L-S37L, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114439)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND FWD CGO STRUCTURE SHEAR TIE CORROSION AT STA1480 38L-37L, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114424)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 FOUND AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA1283 S39L-S39R, CORRECTIVE ACTION: DAMAGED AREA REMOVED AND REPLACED AS PER B767-300 SRM51-40 (2114718)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE SEAT TRACK AT STA1186, RBL11, CORRECTIVE ACTION: THE CORROSION SECTION REPAIRED AS PER B767-300 SRM53-00 (2112219)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE SEAT TRACK AT RBL57, FROM STA390 TO STA412, CORRECTIVE ACTION: DAMAGE SECTION REPLACED IT WITH THE FABRICATED PART PER DWG11DL676-036 AND B767 -300 SRM51-40. (2112087)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE SEAT TRACK AT STA1244, RBL88.5, CORRECTIVE ACTION: DAMAGE SECTION REPLACED IT WITH THE FABRICATED PART PER DWG11DL676-036 AND B767 -300 SRM51-40 (2112288)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE CABIN FLOOR BEAM AT STA347, BETWEEN RBL25 AND RBL40. CORRECTIVE ACTION: THE DAMAGED SECTION REPAIRED AS PER B767-300 SRM53-00 (2112303)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE CABIN FLOOR BEAM AT STA917, RBL11 , CORRECTIVE ACTION: THE DAMAGED SECTION REPAIRED AS PER B767-300 SRM53-00 (2112127)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE CABIN FLOOR BEAM AT STA917, LBL11, CORRECTIVE ACTION: THE DAMAGED SECTION REPAIRED AS PER B767-300 SRM53-00 (2112152)

Part: NONE — NONE · corrosion level 2 · airframe 136,147 hrs · 19,632 cycles

SHIP 174 CORROSION FOUND ON THE SEAT TRACK AT STA1065, LBL88.5, CORRECTIVE ACTION: THE DAMAGED SECTION REPAIRED AS PER B767-300 SRM53-00 (2108855)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 SEAT TRACK - WORN SIGN FOUND AROUND THE SEAT TRACK SCREW HOLE AT STA933, LBL88.5. CORRECTIVE ACTION: DAMAGED SECTION REPAIRED MADE FROM BAC1520- 2193[DA] AND NEW SPLICE MADE PER B767-300 SRM53-00. (2108866)

Part: NONE — NONE · airframe 136,147 hrs · 19,632 cycles

SHIP 174 HFEC INSPECTION FOUND 01EA CRACK ON RH EXTERNAL SURFACE OF THE FUSELAGE SKIN AT S-14AR, STA1637. CORRECTIVE ACTION: CRACK AREA REPAIRED AS PER B767-300 SRM53-80 (2108832)

Part: NONE — NONE · airframe 136,086 hrs · 19,609 cycles

SHIP 174 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: REPLACED INTERLOCK PAWL PER B737 AMM 52-11. SYSTEM CKS NRML. (8401976)

Part: NONE — NONE · airframe 136,068 hrs · 19,603 cycles

SHIP 174 FLIGHT ATTENDANT PANEL DOOR 2L ARMED LIGHT FLASHES RAMDIMY. CORRECTIVE ACTION: OPERATED SLIDE ARM/DISARM OPERATION. SLIDE LIGHT OPERATES NORMAL ON THE DOOR AND AT THE FA PANEL. OPS CHECKS GOOD PER B767-300 AMM 25-66. (8401961)

Part: NONE — NONE · airframe 136,068 hrs · 19,603 cycles

SHIP 174 FA REPORT 2L DOOR DIFFICULT TO DISARM. SLIDE LIGHT FLASHES. CORRECTIVE ACTION: OPERATED DOOR 2L ARM/ DISARM AND NO FAULTS NOTED. SLIDE LIGHT OPERATED NORMAL .NO DIFFICULTIES IN ARMING AND DISARMING SLIDE OPS CHECKS GOOD PER B767-300 AMM 25-66. (8401960)

Part: NONE — NONE · airframe 135,976 hrs · 19,572 cycles

SHIP 174 R1 DOOR WOULD NOT ARM. CORRECTIVE ACTION: FOUND OUTSIDE HANDLE NOT FLUSH. RE-CLOSED DOOR. DOOR ARMS NML (8349298)

Part: SEAL — MISSING (LT WING) · airframe 134,537 hrs · 19,154 cycles

REPORTED BY CREW THE LEFT INBD FLAP TO AILERON MATING SEAL 12" SECTION MISSING. C/W ERA 591452-14. (LP 7641270)

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 134,351 hrs · 19,096 cycles

SHIP 174 SEAT 19F RED EMERGENCY LIGHTS AT 19F INOPERATIVE. MAINTENANCE CLEANED AND RE-SECURED ALL WIRE CONNECTIONS. SYSTEM OPERATION IS NORMAL. (LP 6943355)

Part: NONE — NONE · airframe 137,649 hrs · 20,052 cycles

SHIP 174 DURING ACCOMPLISHMENT OF EM 5724-01010 THE LH WING, LOWER SKIN WAS FOUND CRACKED NEAR L-9.5. CORRECTIVE ACTION: POST REPAIR INSPECTIONS ARE REQUIRED TO MAINTAIN COMPLIANCE WITH AD 2018-11-14. HFEC INPSECTION PER ER/A 583039-14AD SECTION II ARE REQUIRED 12,000 FC OR 36,000 FH WHICHEVER OCCURS FIRST AFTER ACCOPLISHMENT OF ER/A 583039-14AD SECTION I REPAIR. (1373367)

Part: NONE — NONE · airframe 137,649 hrs · 20,052 cycles

SHIP 174 DURING ACCOMPLISHMENT OF EM 5724-01010 THE RH WING, LOWER SKIN WAS FOUND CRACKED NEAR L-6.5. CORRECTIVE ACTION: POST REPAIR INSPECTIONS ARE REQUIRED TO MAINTAIN COMPLIANCE WITH AD 2018-11-14. HFEC INPSECTION PER ER/A 583037-14AD SECTION II ARE REQUIRED 12,000 FC OR 32,000 FH WHICHEVER OCCURS FIRST AFTER ACCOPLISHMENT OF ER/A 583037-14AD (1373276)

Part: SKIN — CRACKED (LT WING) · airframe 133,072 hrs · 18,838 cycles

LEFT HAND WING LOWER SKIN WSTA 990 TO 1018 STR L 6.5 /HOLES #1 & #2 CRACKED. C/W ERA 583038-14. (LP 1371888)

Part: SKIN — CRACKED (LT WING) · airframe 138,849 hrs · 20,290 cycles

DURING ACCOMPLISHMENT OF EM 5724-01010, THE LT WING, LOWER SKIN WAS FOUND CRACKED NEAR L-6.5. ER/A 583038-14AD WAS WRITTEN TO ACCOMPLISH THE REPAIR. ER/A 583038-14AD REVISED TO REV. A. ACCOMPLISH ER/A 583038-14AD REV A SECTION II INSPECTIONS.

Part: WEDGE — DAMAGED (NR 1 SLAT) · airframe 133,072 hrs · 18,838 cycles

#1 LE SLAT UPPER IB CORNER OF AFT WEDGE SURFACE FAILED TAP TEST. APPLIED PERMANENT REPAIR TO # 1 L/E SLAT UPPER I/B CORNER OF AFT WEDGE IAW B767-300 SRM 57-43-02 REPAIR. (LP 1366914)

Part: SKIN — DAMAGED (NR 4 SLAT) · airframe 133,072 hrs · 18,838 cycles

#4 L/E SLAT UPPER SKIN T/E WEDGE HAS A CREASE THAT REQUIRES REPAIR LOCATED 72'' FROM I/B END, 9'' FROM T/E , REPAIRED PER SRM 51-70-10. (LP 1367136)

Part: WEDGE — DAMAGED (NR 4 SLAT) · airframe 133,072 hrs · 18,838 cycles

#4 L/E SLAT I/B LWR AFT WEDGE SKIN HAS POSSIBL VOID ACCOMPLISHED PERMANENT REPAIR ON #4 SLAT UPPER SKIN T/E WEDGE. (LP 1367130)

Part: SHEAR TIE — CORRODED (BS 1556) · corrosion level 2 · airframe 133,072 hrs · 18,838 cycles

CORROSION LEVEL: 2 LOWER FUSELAGE SKIN HAS AREA OF CORROSION AT BS 1556 BETWEEN STRINGERS 24L AND 25L. FOUND OUT OF LIMITS. REPLACED SHEAR TIE (LP 1365434)

Part: CHANNEL — CORRODED (BS 1170-1180) · corrosion level 2 · airframe 133,072 hrs · 18,838 cycles

CORROSION LEVEL: 2 MAIN CABIN FLOOR L/H MOP SILL UPPER SURFACE HAS AREAS OF CORROSION BS 1170 TO BS 1180. REPLACED SILL STA 1170 TO 1180. (LP1361567)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 133,035 hrs · 18,833 cycles

EMERGENCY LIGHTS AT SEATS 31AB-41AB ARE INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY M9010. SYSTEM OPERATION IS NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 132,942 hrs · 18,819 cycles

DURING CHECK FOUND ALL BULBS EMERGENCY LIGHT INSIDE THE CREW REST AREA BURNED. REPLACED ALL BULBS OK FOR SERVICE. (LP6339430)

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 132,775 hrs · 18,797 cycles

BOTH CREW REST LADDER COMMON AREA EMERGENCY EXIT SIGNS ARE INOPERATIVE. FOUND 26 BULBS BURNT OUT AND REPLACED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 129,804 hrs · 18,416 cycles

EMERGENCY PATH LIGHTS AT 28F IS INOPERATIVE. REPAIRED CONNECTOR. SYSTEM OPERATION NORMAL.

Part: PANEL — MISSING (RT NACELLE) · airframe 129,804 hrs · 18,416 cycles

PANEL MISSING FROM RIGHT INBOARD PYLON. REPLACED STRUT ACCESS DOOR ON RIGHT ENGINE. (LP 5615353)

Part: ATTACH BRACKET — BROKEN (EMERGENCY LIGHT) · airframe 127,021 hrs · 18,047 cycles

EMERGENCY LIGHT AT SEAT 39F FELL OFF. THE ATTACH BRACKET WAS BROKEN. REPLACED THE BRACKET. SYSTEM OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 125,883 hrs · 17,901 cycles

EMERGENCY LIGHTS ARE BURNED. MAINTENANCE REPLACED THE LIGHTS. SYSTEM OPERATION IS NORMAL.

Part: ACCESS PANEL — CRACKED (NR 1 PYLON) · airframe 125,177 hrs · 17,805 cycles

NR 1 PYLON ACCESS PANEL CRACKED AT UPPER FWD CORNER. COMPLIED WITH ERA 565377-14.

Part: SKIN — DAMAGED (PYLON STRUT) · airframe 132,018 hrs · 18,697 cycles

WHILE ACCOMPLISHING SRM 54-53-01, REPAIR 7 ON THE LH PYLON STRUT SKIN, DAMAGE OCCURRED IN MULTIPLE HOLES COMMON TO THE REPAIR. C/W ERA 565377-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 122,737 hrs · 17,492 cycles

EMERGENCY LIGHT IS INOPERATIVE AT ROWS 6-19 BOTH AB AND FG SEATS. REPLACED THE POWER SUPPLY AND BATTERY. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 122,541 hrs · 17,466 cycles

DURING SERVICE CHECK FOUND ROW 40FG EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE UNDER SEAT. SYSTEM OPERATION IS NORMAL.

Part: CHILLER — ODOR (GALLEY) · airframe 120,870 hrs · 17,257 cycles

RETURNED TO THE GATE DUE TO REPORTED ODOR IN THE CABIN ON TAXI OUT. FOUND THE AFT GALLEY CHILLER NR 1 AS THE SOURCE OF THE ODOR. REPLACED AFT GALLEY NR 1 CHILLER PER AMM 25-33. OPS CHECKS NORMAL.

Part: SKIN — CRACKED (WING) · airframe 129,580 hrs · 18,385 cycles

LEFT LOWER INSPAR SKIN RIB 31 STR L-9.5 / CRACKS. REPAIRED PER ERA 531304-14. (LP 210267)

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 120,125 hrs · 17,166 cycles

REPORTED ODOR OF SMOKE IN FLIGHT DECK AND ELECTED TO DIV INTO LHR. EMERGENCY WAS DECLARED AND SMOKE, FUMES QRH PROCEDURES WAS ACCOMPLISHED. CREW PULLED MASKS OUT BUT DID NOT DON THE OXYGEN MASKS. MTC FOUND HIGH VOLTAGE CONNECTION HARDWARE AT L1 WINDOW LOOSE AND BURNED. REPLACED WINDOW, J5 WIRING, HARDWARE AND WINDOW HEAT CONTROLLER.

Part: WINDOW — ARCED (COCKPIT) · airframe 120,125 hrs · 17,166 cycles

LEFT FWD WINDOW HEATING ELEMENT ARCHED DURING FLIGHT. CREW TURNED LEFT FWD WINDOW HEAT OFF. REPLACED WINDSHIELD AND WINDOW CONTROLLER. PERFORMED BITE. SYSTEM OPERATION IS NORMAL.

Part: OVEN — SMOKE (GALLEY) · airframe 117,683 hrs · 16,853 cycles

LIGHT SMOKE FROM OVEN 2, FWD GALLEY. STOPPED WHEN POWER REMOVED. EVIDENCE OF ELECTRICAL FAULT FOUND AREA UNDER OVEN COMPLETELY DIRTY. REPLACED FWD GALLEY NR 2 OVEN.

Part: FUEL TANK — CORRODED (BS 955) · corrosion level 2 · airframe 115,798 hrs · 16,615 cycles

CABIN DRAIN PATH AT BS 955, LBL 55 CENTER TANK UPPER SKIN CORROSION. REMOVED AND ACCOMPLISHED IAW PRI 534290-14.

Part: FRAME — CRACKED (BS 903) · airframe 115,798 hrs · 16,615 cycles

HFEC INSPECTION FOUND 01 EA CRACK ON RT BS 903.5, FRAME INNER CHORD TRANSITION RADIUS AS MARK IAW W/C 5311-01195- 06 AND THE REPAIR WC 5311-01195-09F.

Part: FRAME — CRACKED (BS 859) · airframe 115,798 hrs · 16,615 cycles

HFEC INSPECTION FOUND 01 EA CRACK ON LT-BS 859.5. FRAME INNER CHORD TRANSITION RADIUS IAW W/C 5311-01195-01 AND THE REPAIR WC 5311-01195-09A MUST BE ACCOMPLISHED. PRIOR TO FURTHER FLIGHT.

Part: STRINGER — CORRODED (BS 1021) · corrosion level 2 · airframe 115,798 hrs · 16,615 cycles

CABIN STRINGER 20R AT BS 1021 CORRODED. C/W ERA 534289-14.

Part: STRINGER — CRACKED (BS 1562) · airframe 115,784 hrs · 16,612 cycles

FUSELAGE STRINGER AT BS 1562 FOUND S-39R CRACKED. REPAIRED IAW SRM 53-00.

Part: BULKHEAD — NOT REPORTED (NLG WW) · airframe 115,784 hrs · 16,612 cycles

LT SIDE NOSE WHEEL WELL BULKHEAD CHORDS IAW W/C 5312-01165-0301 AND TO REPAIRED IAW WC 5312-01165-0701.

Part: SHEAR TIE — CORRODED (BS 1562) · corrosion level 2 · airframe 115,784 hrs · 16,612 cycles

CORROSION FOUND ON SHEAR TIE BULK CARGO BAY AT BS 1562, S39L - 38R. REPLACED.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 112,224 hrs · 16,168 cycles

EMERGENCY LIGHTS ROW 6, 7, 8 AND 9D ARE INOPERATIVE. MAINTENENCE FOUND LIGHT INVERTER FUSE BLOWN AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 111,949 hrs · 16,135 cycles

EMERGENCY LIGHTS COMING ON MOMENTARILY IN FLIGHT . REPLACED BATTERY PACK M00735.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 111,949 hrs · 16,135 cycles

OVERHEAD EMERGENCY LIGHTS ON LT SIDE BETWEEN SEATS 1-9 ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER, M735. SYSTEM OPS NORMAL.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 111,949 hrs · 16,135 cycles

EMERGENCY LIGHTS COME ON IN FLIGHT, LEFT SIDE BUSINESS CLASS. REPLACED BATTERY TRAY M9008, INSPECTED WIRE TO SPLICE SM9002, SM9003, SM9004I. SYS OPS IS NORMAL.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 111,949 hrs · 16,135 cycles

1HR 40 MINUTES INTO FLIGHT, EMERGENCY LIGHTS CAME ON IN CABIN. REPLACED POWER SUPPLY AND BATTERY. SYSTEM OPS IS NORMAL.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 111,780 hrs · 16,116 cycles

DURING CRUISE FL 350, ALL CABIN EMERGENCY LIGHTS ILLUMINATED, LIGHTS OUT WITH COCKPIT EMERGENCY LIGHT SWITCH IN OFF POSITION. FOUND LIGHT ON AS WELL. MAINTENANCE REPLACED BATTERY IN UPPER CEILING. SYS OPS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 111,512 hrs · 16,085 cycles

LT WING LOWER SKIN CRACKED APPROXIMATELY .250 IN BEYOND COUNTERSINK AT GROUP A FASTENER AFT ROW INBD FASTENER. REPAIRED IAW ERA 531304-14.

Part: SKIN — DAMAGED (BS 463) · airframe 109,576 hrs · 15,845 cycles

LIGHTNING STRIKE DAMAGE ON SKIN AT BS 463 ON S4L. REMOVED DAMAGE AND INSTALLED REPAIR IAW ERA 527719-14.

Part: SKIN — DAMAGED (BS 394) · airframe 109,576 hrs · 15,845 cycles

LIGHTNING STRIKE DAMAGE ON SKIN AT BS 394 S3L. REMOVED DAMAGE AND INSTALLED REPAIR IAW ER/A 527763-14.

Part: SKIN — DAMAGED (BS 444) · airframe 109,576 hrs · 15,845 cycles

LIGHTNING DAMAGE FOUND AT BS 444 ON S4R. REMOVED DAMAGED AREA AND INSTALL REPAIR IAW ERA 527729-14.

Part: STRUCTURE — DAMAGED (BS 390) · airframe 109,576 hrs · 15,845 cycles

DURING CHECK, DAMAGE WAS FOUND AT BS 390 S3L. REMOVED DAMAGE AND INSTALLED REPAIR IAW SRM 53-00-03, REPAIR 1.

Part: SKIN — DAMAGED (BS 394) · airframe 109,658 hrs · 15,856 cycles

LIGHTEN STRIKE DAMAGE ON FUSELAGE SKIN BS 394 S3L. REPAIRED IAW SRM 53-00-01.

Part: SKIN — CRACKED (RT WING) · airframe 102,193 hrs · 14,878 cycles

RT WING LWR SKIN AFT PITCH LOAD FITTING OTBD HOLE FOUND CRACKED. REPAIRED IAW ERA 499361-14AD, REV ORIG SECTION 2 PERMANENT REPAIR.

Part: SEAT TRACK — CORRODED (BS 1208.45-1428) · airframe 102,193 hrs · 14,878 cycles

BS 1208.45-1428 RBL 88 SEAT TRACK FOUND CORRODED. REPAIRED IAW ERA 507557-14V REV ORIG.

Part: HOSE — NOT REPORTED (CREW OXYGEN) · airframe 102,193 hrs · 14,878 cycles

CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE IAW EA 01-074935-03.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 101,846 hrs · 14,833 cycles

WIRE PULLED AT WALL FROM EMERGENCY LIGHT AT SEAT 18G. MX REPLACED THE PIN ON CONNECTOR. SYS OPERATION IS NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 101,119 hrs · 14,744 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 20 GH ARE INOPERATIVE. MAINTENANCE REPLACED THE PIN CONNECTION AT SIDEWALL PER SPWM. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 98,980 hrs · 14,457 cycles

EMERGENCY ESCAPE PATH LIGHTS AT 15AB ARE INOPERATIVE. MTC FOUND A CONNECTOR SEPARATED THAT SUPPLYS SEAT POWER AND RECONNECTED. SYSTEM OPERATION IS NORMAL.

Part: FITTING — NOT REPORTED (WING) · airframe 98,565 hrs · 14,397 cycles

WINGS DIAGONAL BRACE AFT PITCH LOAD FITTING, LWR WIN IAW EA 01-451812-03.

Part: BATTERY — DISCHARGED (CABIN) · airframe 97,440 hrs · 14,252 cycles

EMERGENCY CEILING LIGHTS ARE INOPERATIVE IN FIRST CLASS ON RIGHT SIDE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY PER AMM. SYSTEM OPERATION IS NORMAL.

Part: FITTING — CORRODED (LT WING) · airframe 97,292 hrs · 14,232 cycles

LT FS 955 WING REAR SPAR AREA AFT "T" FITTING HAS CORROSION IN AREA OF A FASTENER HOLE. FITTING REPLACED PER ERA 496323-14AD REV ORIG.

Part: STRAP — CRACKED (RT WING) · airframe 97,292 hrs · 14,232 cycles

RT FS 955 WING REAR SPAR B/H FITTING AREA HAS 1 FASTENER HOLE CRACKED AT FAIL SAFE STRAP AND REPAIRED PER ERA 496324-14AD REV ORIG.

Part: STRAP — CRACKED (LT WING) · airframe 97,292 hrs · 14,232 cycles

LT FS 955 REAR SPAR B/H FITTING AREA HAS 1 FASTENER HOLE CRACKED AT FAIL SAFE STRAP AND REPAIRED PER ERA 496323-14AD REV ORIG.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 97,030 hrs · 14,201 cycles

EMERGENCY LIGHTS FROM ROWS 32-41 ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AT 32FG. SYSTEM OPERATION IS NORMAL.

Part: STRUCTURE — NOT REPORTED (BS 1809) · airframe 95,842 hrs · 14,042 cycles

FUSELAGE 1809 BULKHEAD, FWD OUTER CHORD, HORIZONTAL INNER CHANNEL. IAW EA 01-455010-12.

Part: WIRE — BROKEN (CABIN) · airframe 95,703 hrs · 14,026 cycles

EMERGENCY PATH LIGHTS AT SEAT 27B ARE INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT CONNECTED AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 95,693 hrs · 14,024 cycles

EMERGENCY PATH LIGHTS AT SEAT 25 FG ARE INOPERATIVE. MAINTENANCE REPLACED THE SOCKET. SYSTEM OPERATION IS NORMAL.

Part: WIRE — PULLED (CABIN) · airframe 95,141 hrs · 13,954 cycles

EMERGENCY LIGHTS AT SEAT 27AB ARE INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF CONNECTOR AT WALL AND RE-SECURED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — PULLED (CABIN) · airframe 94,628 hrs · 13,884 cycles

EMERGENCY LIGHTS AT SEAT 14AB AND 19FG ARE INOPERATIVE. MAINTENANCE FOUND HARNESS CONNECTOR UNDER THE SEAT PULLED AND RESEATED PINS. SYSTEM OPERATION IS NORMAL. (2011-D0219)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,897 hrs · 13,512 cycles

ON DRC MX FOUND THE FLIGHT DECK EMERGENCY LIGHT INOPERATIVE AND REPLACED THE LIGHT ASSY. SYS OPS IS NORMAL.

Part: DRAIN — LEAKING (GALLEY) · airframe 90,379 hrs · 13,320 cycles

LT/CTR RT A/P CONTROL SLOOPY. CTR A/P DICONNECTED. MAN ELEV CONTROL STIFF. TRIM NML. HYD NML. MALF OCCURRED BELOW 14K. FLEW MANUAL FROM LOC INCPT AT 5K ABOVE GND. ELEV HARD TO MOVE UP/DOWN. AT 10-20 FT FELT LIKE ELEV BROKE FREE. BOUNCED LDG HIGHLY SUSPECTED EXSISTING WATER LEAK FROM AFT GALLEY DRAIN SYS DRIPPING ON FLT CONTROLS. (SEE SIMILAR OCCURANCE BEFORE COMPLIANCE OF EA 01-090573-03 ON SHIP 175) EA C/W ON THIS ACFT 2007. MX REPAIRED WATER LEAK. INSPECT ALL CONTROL CABLES. NON-REV V/F C/W ON FLT 9983/28. ALL OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: REFLECTOR — DAMAGED (SLIDE LIGHT) · airframe 90,295 hrs · 13,308 cycles

AFT GROUND SLIDE LIGHT INOP ON LT SIDE. REPLACED REFLECTOR ASSY, CKS.

Part: FRAME — CRACKED (BS 903 LBL 81) · airframe 90,163 hrs · 13,290 cycles

CABIN-BS 903 LBL 81 FRAME INBD CHORD LWR AREA FOUND CRACKED AND REPAIRED IAW ERA 473040-14 REV 0.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 90,161 hrs · 13,289 cycles

NR 2 PYLON FWD UPPER SPAR WEB FUEL TUBE CUTOUT FOUND CRACKED. REPAIRED IAW ERA 473380-14.

Part: SKIN — CRACKED (BS 1197 S39R) · airframe 90,161 hrs · 13,289 cycles

DURING INSP OF FUSELAGE FOUND CORROSION WITH A CRACK, CRACK APPROX 3/8 IN LENGTH REPAIRED IAW SRM 53-60-01 FIG 201 REPAIR 2.

Part: WARNING SYSTEM — MALFUNCTIONED (HYDRAULIC SYS) · airframe 89,291 hrs · 13,170 cycles

RTO AT 50K DUE TO -L DEM OVHT- EICAS MESSAGE. RETURNED TO GATE. T/S SYSTEM INSPECTED WIRING IN LEFT PYLON. LOOKS OK. PERFORMED ENG RUN, ALL HYD SYSTEMS OPERATE NORMALLY. AS PRECAUTIONARY REPLACED L DEMAND PUMP CONN D916 AND CASE DRAIN AND PRESS FILTERS. LEAK CHECK AND OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (RIGHT LP1) · airframe 88,038 hrs · 13,010 cycles

RT DUCT LEAK LP1 MESSAGE. FWD TO MCO/PLAC 26-18-01A, T/S PER FIM UNABLE TO DUPLICATE FAULT. DUCT LEAK TEST GOOD M AND PLACARD REMOVED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 87,510 hrs · 12,949 cycles

LT PACK OFF AND LT EICAS LT PACK OFF LIGHTS DO NOT ILLUMINATE WITH LT PACK TURNED OFF. RESET CONN ON FLOW CONTROL VALVE CYCLED PACK SEVERAL TIMES, CHECKS OK.

Part: PUMP — FAILED (LT OVERRIDE) · airframe 87,030 hrs · 12,894 cycles

RTB, ON TAXI OUT AFTER ENGINE STAT LEFT CENTER FUEL PRESSURE LIGHT ILLUMINATED, FWD TO MCO PLACARD PER MEL 28-22-02A DISPATCH APPROVED. REMOVED AND REPLACED LEFT CTR OVERRIDE PUMP IAW AMM. OPS AN LEAK CHECK OK. MCO AND PLACARD REMOVED.

Part: VALVE — MALFUNCTIONED (CABIN TEMP) · airframe 84,987 hrs · 12,646 cycles

RTB - DUE FWD CABIN TEMP CONTROL EICAS MSG. TEMP CONTROL FWD CABIN INOP LIGHT ILLUMINATED. NO MEL RELIEF BY FCP/C MTC CLOSED FWD TRIM VALVE AND RELEASED PER MEL 21-61-04A.

Part: TEE FITTING — CRACKED (NR 2 PYLON) · airframe 84,852 hrs · 12,629 cycles

THE CLOSEOUT TEE AT THE MIDSPAR FITTING AT THE NR 2 PYLON WAS FOUND CRACKED. THE PART WAS REPLACED PER ER/A 01-452215-14.

Part: TEE FITTING — CRACKED (NR 1 PYLON) · airframe 84,852 hrs · 12,629 cycles

THE CLOSEOUT TEE AT THE MIDSPAR FITTING OF THE NR 1 PYLON WAS FOUND CRACKED. THE PART WAS REPLACED PER ER/A 01-452214-14AD.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 80,365 hrs · 12,091 cycles

UNUSUAL AIR SURGE SOUND DURING TAXI IN LEFT ENG IS 23 PSI AND RT ENG IS 34. REMOVED AND REPLACED LEFT ENG PRSOV, ENG RUN VALVE OP CHECKS GOOD.

Part: MODULE — FAULTED · airframe 80,101 hrs · 12,058 cycles

DIV DUE AUTOPILOTS WILL NOT ENGAGE-RUDDER RATIO AND AILERON LOCKOUT EICAS MSGS AND LIGHTS ILLUMINATED ON OVERHEAD PNL. MSG CAME ON A 250 KTS GOT STAB TRIM LIGHT FOR 5 SEC MSG DID NOT GO AWAY WHEN WE SLOWED DOWN OR RECONFIGURED /C. FOUND BOTH SAMS FAULTED RESET BOTH REPLACED LT SAM AS PRECAUTIONARY AP NOW EGAGE OK. TEST 30 AND TEST 40 CARRIED OUT OK. LAST FLT FAULTS SAM INFC WITH FCC-L-C-R, NO RUDDER RATIO FAULT BALLS.

Part: PUMP — FAILED (RT FUEL BOOST) · airframe 79,402 hrs · 11,970 cycles

AT PUSHBACK, RT AFT FUEL BOOST PUMP POPPED C/B, RESET NO GOOD. FWD TO MEL 28-22-01A. IT WAS POSSIBLE TO FLT CREW PLACARD TO APPLY THIS MEL. THE AIRCRAFT NEEDED MORE FUEL SO HAD TO RETURN TO GATE. REMOVED AND REPLACED BOOST PUMP W MFG P/N 5006003D PER AMM REMOVED MCO AND PL PER MEL 28-22-01A.

Part: ACTUATOR — LEAKING (YAW DAMPER) · airframe 77,979 hrs · 11,795 cycles

CENTER HYD LOW LEAK TRACED TO LT YAW DAMPER SERVO ACTUATOR P/N REQUIRED 1536600-7, LEAY SERVO S/N 1979. A/C DISP IAW MEL 22-21-01 CAT C. C HYD SYSTEM SERVICED TO FULL WITH 6 GALLONS. REMOVED AND REPLACED LEFT YAW DAMPER SERVO PER AMM 21-21-02 MANF PN 1540500-9. LEAK CHK AND SERVO TEST GOOD. PER TOPP 40-30-05 ITEM NOT RII MCO AND PLACARD REMOVED.

Part: FITTING — DAMAGED (WING TE FLAP) · airframe 77,747 hrs · 11,769 cycles

WING T/E -INBD FLAP -MAIN FLAP -COLLAR FITTING REPLACEMENT IAW EO 01-073591-12 ME12 AND ME13 C/W EO 01-073591-12 ME12 AND ME13.

Part: CONNECTOR — CONTAMINATED (IDG) · airframe 76,907 hrs · 11,664 cycles

L IDG VLV STATUS MSG AFTER ENG START. MX FOUND ELECTRICAL CONNECTOR CONTAMINATED. CLEANED RESEATED CONNECTOR AND MSG CLEARED. RAN ENG AT IDLE NO MSG.

Part: BEARING — BINDING (RUDDER) · airframe 75,208 hrs · 11,442 cycles

RUDDER PEDALS BINDING ON PRE FLT CHECK. FOUND BEARING IN RUDDER FEEL/CENTURING UNIT FROZEN. REPLACED SAME AND CHECKED OUT RUDDER FEEL AND CENTERING PER AMM 27-21-10-712-098 RUDDER AND PEDALS OPERATE NORMAL WITH FULL TRAVEL.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 74,650 hrs · 11,378 cycles

SLIGHT PLASTIC ODOR DESCENDING THRU 6000 IN COCKPIT FWD GALLEY AND BUSINESS CLASS. LASTED JUST A FEW 3 MINUTES. NO ODOR FOUND, SUSPECT PLASTIC FROM CONTENTS IN OVEN, CLEANED OVENS.

Part: BEARING — LEAKING (NR 2 ENGINE) · airframe 74,361 hrs · 11,342 cycles

WORKING NR 2 ENG HOC MSU FOUND NR 3 BEARING WEEP HOLE LEAKING ALONG WITH OIL CONSUMPTION BEYOND ACCEPTABLE LIMITS. REQUIRES ENGINE REPLACEMENT. ENGINE CHANGE IN PROGRESS. REPLACED NR 2 ENG PER TRANS 1T149AD.

Part: ACTUATOR — FAILED (RUDDER) · airframe 73,449 hrs · 11,229 cycles

RUDDER RATIO LIGHT AND EICAS STATUS MSG ILLUMINATED. LIGHT/MSG WOULD NOT RESET. FOUND RUDDER RATIO CHANGER ACTUATOR AT FAULT. REPLACED AND OPS CK OK.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 73,356 hrs · 11,217 cycles

FOUND 3RD EMERGENCY LIGHT ON RT WING BURNED OUT. RELAMPED, OPS CK OK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 73,356 hrs · 11,217 cycles

2ND EMERGENCY LIGHT ON LEFT SIDE AFT OF WING INOP DURING TEST. RELAMPED, OPS CK OK.

Part: COFFEEMAKER — SPARKS (FWD GALLEY) · airframe 69,560 hrs · 10,713 cycles

FWD GALLEY COFFEE MKR INOP/SPARKING, REPLACED SAME.

Part: CIRCUIT CARD — MALFUNCTIONED (E/E BAY) · airframe 69,382 hrs · 10,689 cycles

ON TAKEOFF POWERUP TO 1.20, GOT A TAKEOFF CONFIG WARNING AND FLAPS EICAS MESSAGE. RAN ENGINES UP AGAIN W/ FLAP 5 AND 15 SAME PROBLEM. REPLACED TAKEOFF CONFIG WARNING CARD, OPS OKAY.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 67,056 hrs · 10,359 cycles

RT ENG SHUTDOWN BY CREW DUE TO VIBS/LOW OIL PRESSURE/LOSS OF OIL QTY. A/C DIVERTED TO NCE. REPLACED ENGINE.

Part: CONTROLLER — ODOR (ENTERTAIN SYS) · airframe 65,176 hrs · 10,083 cycles

FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR FROM INFLIGHT ENTERTAINMENT CONTROL BOX. REPLACED CONTROLLER.

Part: DUCT — LOOSE (E/E BAY) · airframe 62,388 hrs · 9,698 cycles

IN CLIMBOUT AT FL270 OVERHEAT LIGHT CAME ON IN STAY-BY MODE AS PER QRH SWITCHED TO OVERRIDE. AFTER 2-3 MIN NO COOLING LIGHT CAME ON. FOUND DUCT SEPARATED FWD OF EQUIP COOLING SUPPLY CHECK VALVE LOCATED IN THE FWD CARGO COMPT LEFT SIDEWALL AREA. RESECURE DUCT OVERRIDE VLV V140 AND SYS INTERCONNECT VLV V90 CK OK I OVERRIDE MODE. STANDBY MODE CKD OK. ATLMA NOTIFIED. SEE ITE 005 THIS SVC FOR AUTO MODE OPS CK.

Part: PSEU — MALFUNCTIONED (E/E BAY) · airframe 60,306 hrs · 9,368 cycles

AFTER TAKEOFF AND GEAR RETRACTION AND PLACING THE GEAR HANDLE TO THE OFF POSITION, GOT SEVERAL MESSAGES. DID NOT PLACE HANDLE TO THE UP POSITION. RETURNED TO JFK DUE TO MSG OF TAIL SKID. MTC IN PROGRESS. PERFORMED T/S FOR LANDING GEAR HANDLE INTLK PER FIM 32-30-00. ALL FIM STEPS CHECK OK. REPLACED PROX SWITCH ELEX UNIT PER MM. PERFORMED VERIFICATION TEST FLT. LANDING GEAR RET AND AIR GROUND SENSOR INFLT CHECK OK.

Part: ODOR — DETECTED (CABIN) · airframe 55,662 hrs · 8,548 cycles

ACRID SMELL INFLIGHT. A/C DIVERTED TO MANCHESTER. MANCHESTER MTC DID NOT FIND ANYTHING OBVIOUS. MTC WILL CONTINUE TO MONITOR AIRCRAFT.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 53,241 hrs · 8,161 cycles

FLT DIVERTED TO BOS WITH BURNING SMELL IN AFT GALLEY. REMOVED ALL AFT COFFEEMAKERS AND CLEANED AREA OF COFFEE RESIDUE. INSPECTED AFT GALLEY FOR OTHER SOURCE OF SMELL. NONE FOUND. REPLACED NR 1 AND NR 3 COFFEEMAKERS PRECAUTIONARY.

Part: WIRE — BROKEN (CABIN) · airframe 50,083 hrs · 7,630 cycles

EMERGENCY LIGHTS AT ROW 10-11-20 F AND G INOP. TERMINATED GROUND WIRE.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,080 hrs · 7,628 cycles

DENT FOUND AT STA 1378 AND STRINGER 29R. DENT BEYOND SRM ALLOWABE LIMITS AND IS CUTOUT AND REPAIRED WITH EXTERNAL DOUBLER. REPAIRED ER/A 396401-14.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 49,736 hrs · 7,568 cycles

HIGH OIL CONSUMPTION HISTORY ON NUMBER 1 ENGINE. NUMEROUS ATTEMPTS TO CORRECT HAVE NOT YIELDED SATISFACTORY RESULTS. REPLACED ENGINE.

Part: LINE — LEAKING (LEFT PYLON) · airframe 47,642 hrs · 7,213 cycles

LEFT HYD QTY LEAK DURING CRUISE, RIGHT DISENGAGED AND CENTER A/P OK. FOUND LEAKING HYD RETURN LINE IN LEFT PYLON. REPLACED SAME WITH AA PURCHASED PART. PRESSURIZED HYD, NO LEAKS. RAN FCC RIGHT TEST, NO FAULTS. OK FOR SERVICE. ETOPS CATEGORY ''B'': DIVERSION OR TURNBACK

Part: CONTROL PANEL — SMOKE (CARGO HEAT) · airframe 47,507 hrs · 7,193 cycles

AT ABOUT 30W THE CARGO HEAT FWD OVERRIDE C/B POPPED. GOT ELECTRIC SMELL AND LT/RT REC FAN EICAS MSG. LOST GALLEY PWR INFLIGHT. PULLED C/B B7 ON P6-1 AND RESET PWR. FOUND CARGO FIRE CONTROL PANEL CAUSING ELECTRICAL SMELL. REPLACED PANEL, SYSTEM CHECKS NORMAL. ETOPS CATEGORY ''E'': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: UNKNOWN — ODOR (CABIN)

F/A REPORTED A STRONG ELECTRICAL ODOR COMING FROM F/C GALLEY 8 MINUTES BEFORE DEPARTURE. REPLACED COFFEEMAKER. NO TROUBLE FOUND. (P/N 251005193) (S/N 427)

Part: UNKNOWN — ODOR (CABIN)

FLT ATTS NOTICED STRANGE ODOR COMING FROM VIDEO EQUIP. TURNED EQUIP OFF THEN ON AND SMELL DISSIPATED. INSPECTED VCC AND PERFORMED OPS CHECK OF SYS. FOUND NO FAULTS OR STRANGE ODORS.

Part: CAM — DAMAGED (MLG)

PARTS WERE RECEIVED AT B. F. GOODRICH AEROSPACE LOCATED IN OPA-LOCKA, FLORIDA. THE INTERNAL PARTS ARE DAMAGED BEYOND REPAIR. SUBMITTER STATED THE DAMAGES TO UPPER AND LOWER CAMS COULD HAVE BEEN A RESULT OF A DISLODGED SUPPORT PIN LOCATED I THE LOWER CAM. (X)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

LEFT AFT EMERGENCY EXIT LIGHT AND AISLE LIGHTS FORWARD AND AFT OF EXIT LIGHT NOT WORKING DURING OPERATIONAL CHECK OF EMERGENCY EXIT LIGHTS. REPLACED BATTERY CHARGER, SYSTEM OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (ROW 6FG)

EMERGENCY TRACK LIGHTS INOP AT SEATS 6 F/G THRU 20 F/G. REPLACED SHORTED LIGHT ASSY AT SEAT 11G AND REPLACED FUSE IN POWER SUPLY M9011. EMERGENCY LIGHTS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (BS 654)

ON L/O, FOUND EMERGENCY LIGHTS INOP SEATS 6, 10, 11 AND 20 FIG. FOUND AFT LIGHT OF SEAT 11FG BLOWING FUSE ON POWER SUPPLY. REPLACED POWER SUPPLY AND FORWARD AFT LIGHT OF 11FG TO MCO AND PLACARD.

Part: MASK — DIRTY (LT COCKPIT)

CAPTS O2 MASK VALVE STICKS. HARD TO EXHALE, NEEDED CLEANING. REPLACED O2 MASK.

Part: WIRE — SHORTED (SEAT 2A/B)

PAX SPILLED DRINK ON ELECT MOTORSEAT 2A/B, SHORTED OUT. BESIDES SEATS 2A/B FOUND CHAFFED/SHORTED WIRES BETWEEN AIR LOUVERS/FLOOR. CUT WIRES, ISOLATED WITH END CONNECTORS/TAPE. MADE PROTACTED INSP OF WIRES BUNDLES BEHIND AIR LOUVERS FOUND SATISFACTORY STORED WIRES BEHIND LOUVER/FIXED. RESET C/B, FOOTREST/CHECKED. FOUND NORMAL. FWD TO MCO FOR MAIN BASE REPAIR OF WIRES BUNDLES. SEATS 2A/B INOP IN ELECT MODE. OK IN MANUAL MODE.

Part: HYD PUMP — FAILED (NR 2 ENGINE)

RT HDY QTY DECREASED TO 0.13 QTY STABLE WITH ENGINE DRIVEN PUMP OFF. OCCURED AT FL310 AT FL 310 STABLIZED IN CRUISE 40 MIN INTO FLT. REPLACED RIGHT ENGINE DRIVEN PUMP, PRESSURE FILTER AND CASE DRAIN FILTER. SYSTEM SERVICED, OPS CHECK GOOD AFTER ENGINE RUN.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

CLASS EMERGENCY LIGHT TRACK INOP. REPLACED EMERGENCY POWER SUPPLY M9008, OPS CHK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHT AT 2 LEFT INOPERATIVE AND LIFTED FROM THE FLOORING. RESECURED EMERGENCY TRACK LIGHT, OPERATION NOW NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON LAYOVER, EMERGENCY PATH LIGHT AT SEAT 24 TO 27 BOTH SIDE INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY OPS CHK NORMAL.

Part: TR UNIT — DAMAGED (NR 1 ENGINE)

ON ARRIVAL, FOUND NR 1 ENG FAN DUCT COWL ASSY DAMAGED. REPLACED NR 1 ENGINE INBD THRUST REVERSER HALF.

Part: FUSE — BLOWN (CABIN)

ON L/O, FOUND E-PATH LIGHT IN AFT B/C AND FORWARD PART OF Y-CLASS INOPERATIVE ON BOTH SIDES. REPLACED FUSE F1 IN POWER SUPPLY. OPS CKS OK.

Part: FCC COMPUTER — FAILED (LEFT)

EN ROUTE, A/C DIV KEF DUE LT FCC COMPUTER FAILED. ELECTRICAL SMELL IN COCKPIT REPORTED BY FLT CREW. MTC REPLACED THE LT FCC COMPUTER.

Part: PROCESSOR — MALFUNCTIONED (FUEL IND SYSTEM)

DIVERTED BDL DUE WEATHER, DURING DIVERSION HAD EICAS STATUS MESSAGE FUEL QUANTITY CHANNEL. PERFORMED BITE, FAULTS PROCESSOR CHANNELS 1 AND 2. COULD NOT DISPATCH. REPLACED PROCESSOR PER M/M. PERFORMED BITE, OPERATION NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: STRINGER — CRACKED (FS 1540)

L/O CHK STRINGER 39L HAS .75 INCH CRACK AT STA 1540, FABRICATED REPAIR PARTS PER 53-00-03. OK TO INSTALL, INSTALLED SPLICE PER SRM. DAMAGE WAS FROM TAIL STRIKE ON LANDING.

Part: STRINGER — DAMAGED (FS 1500)

L/O CHK STRINGER 38R DAMAGED AT STA 1500. REPLACED DAMAGED STRINGER AND SPLICED AT STA 1472 AND STA 1547.

Part: STRINGER — DAMAGED (FS 1461)

STRINGER 39L DAMAGED AT STA 1461. REMOVED DAMAGED STRINGER 39L. SPLICED STRINGER STA 1470, 1509, AND 1530 PER SRM 53-00-03. INSTALLED SPLICED STRINGER AT STA 1450 TO STA 1562 PER SRM 53-00-03. DAMAGE WAS FROM TAIL STRIKE ON LANDING.

Part: STRINGER — DAMAGED (FS 1461)

AT L/O STRINGER 39R DAMAGED AT STA 1461. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER AND SPLICE IN NEW SECTION AT STA 1450 TO STA 1562. DAMAGE WAS FROM TAIL STRIKE ON LANDING.

Part: ENGINE — FAILED (NR 1)

AFTER REVIEW OF ENGINE HISTORY, NR 1 ENGINE WAS REMOVED AND ROUTED TO SHOP FOR REPAIRS, DUE TO HIGH EGT AT ISA RESTRICTION.

Part: ENGINE — DAMAGE (NR 2 ENGINE)

NR 2 ENGINE FAILED BORESCOPE INSPECTION, FOUND FIRST STAGE GUIDE VANE DAMAGE BEYOND LIMITS. REPLACED ENGINE FOR RETURN TO SERVICE.