N1602

Part: LIGHT — DAMAGED (ZONE 200) · airframe 115,117 hrs · 16,441 cycles

EMERGENCY PATH LIGHTING SEATS 38B & 44B ARE DAMAGED. REMOVED AND REPLACED EMERG LIGHT ASSY AT SEAT 38B PER B767 AMM 33-52, REPAIRED WIRING AT SEAT 44B PER SWPM CH20. BOTH LIGHTS OPS NML. (7377996)

Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 113,293 hrs · 16,145 cycles

SHIP 1602 1L DOOR SLIDE ARMED INDICATING LIGHT ON 1L FLT ATT PANEL INOP. CORRECTIVE ACTION: REPLACED 1L SLIDE RELAY AND FLASHER REPEAT RELAY IAW B767-300 FIM 52-73-00-815-803. (1033086).

Part: RELAY — FAULTED (ZONE 800) · airframe 113,091 hrs · 16,118 cycles

SHIP 1602 L1 SLIDE LIGHT. CORRECTIVE ACTION: T/S IAW B767-300 FIM 52-73-00-815-803. PER BLOCK 22, REPLACED 1L SLIDE RELAY (K940) AND FLASHER REPEAT RELAY (K939). OPERATION OF 1L DOOR SLIDE LIGHT OK. (0999676)

Part: INDICATOR — NOT REPORTED (ZONE 800) · airframe 113,017 hrs · 16,105 cycles

SHIP 1602 1L MAIN ENTRY DOOR ARMED INDICATOR ( AT DOOR). RESECURED DOOR 1L MAIN ENTRY DOOR ARMED INDICATOR. OPS CHK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 112,983 hrs · 16,099 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. R/R L1 SLIDE INDICATOR LIGHT ASSY PER B767-300. AMM 52-73. TESTED LIGHT, TEST GOOD. (0975624)

Part: INDICATOR — DAMAGED (ZONE 800) · airframe 112,983 hrs · 16,099 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. SLIDE INDICATOR LIGHT PLATE RE-INSTALLED IAW AMM 52-71 CHECKED SATISFACTORY. (0973761)

Part: LIGHT — DETACHED (ZONE 200) · airframe 111,620 hrs · 15,852 cycles

SHIP 1602 LIGHT FIXTURE UNDER AISLE ARMREST OF SEAT 51B IS LOOSE AND HANGING UNDER SEAT. CORRECTIVE ACTION: RE-SECURRED 51B EMER PATHLIGHT. OK FOR SVC (6551687)

Part: TRANSCEIVER — FAULTED (WX RADAR) · airframe 111,330 hrs · 15,790 cycles

SHIP 1602 -ATB- CREW DECISION TO RETURN TO HND DUE TO WEATHER RADAR ISSUES. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP. R/R WXR XCVR AND ANT DRIVE UNIT.(6551013)

Part: SWITCH — INOPERATIVE (SLIDE LIGHT) · airframe 110,237 hrs · 15,628 cycles

SHIP 1602 DOOR 1 RT SLIDE LIGHT INOP. CORRECTIVE ACTION: REPLACED SWITCH IAW B767-300 WDM 52-73-11 (0520710)

Part: MECHANISM — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 110,220 hrs · 15,626 cycles

SHIP 1602 1R DOOR SLIDE ARMED LT INOP. CORRECTIVE ACTION: DOOR SLIDE LIGHT MECHANISM ADJUSTED INSIDE SATIS (6179078)

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 110,176 hrs · 15,620 cycles

SHIP 1602 FOUND 45B PATHWAY LIGHT INOP. CORRECTIVE ACTION: FOUND CONNECTOR FROM SEAT TO SIDEWALL DISCONNECTED. RECONNECTED. (6179051)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 110,015 hrs · 15,599 cycles

AIRCRAFT 1602, L1 HAS HISTORY OF SLIDE LIGHT FLASHING. CORRECTIVE ACTION: SLIDE INDICATION FUNCTIONED NORMALLY. PER MCC REQUEST REPLACED K940 RELAY. OPS CHECKED L1 SLIDE LIGHT PER B767-300 AMM 52-73. OPS CHECK NORMAL. (LP 0477437)

Part: PSEU — INOPERATIVE (DOOR SLIDE) · airframe 109,775 hrs · 15,569 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: R/R PSEU REF B767 AMM 32-09. R/R CARD 07 OF PSEU REF B767-300 AMM 32-09. ALL CHECKS GOOD. (0442204)

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 109,165 hrs · 15,489 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: PREF OPS CHK OF DOOR 1L SLIDE INDICATOR LT. NTF. OPS CHK GOOD. (0376754)

Part: INDICATION SYS — MALFUNCTIONED (R2 DOOR) · airframe 108,820 hrs · 15,437 cycles

SHIP 1602 DOOR 2R PANEL LIGHT DOESN'T GIVE PROPER ARMED/DISARMED LIGHT. CORRECTIVE ACTION: FOUND 2R PANEL LIGHT FUNCTION NML. REF B767 AMM 52-11. OK FOR SVC. (5639458)

Part: LIGHT — MISSING (SEAT 52 ABC) · airframe 108,649 hrs · 15,407 cycles

SHIP 1602 EMERGENCY LIGHT ON SEAT 52 LEFT ABC MISSING. CORRECTIVE ACTION: REPLACED MISSING EEPL HOUSING AND LIGHT AT SEAT 52C IAW B767 CMM 25-28-94. OPS NORMAL, OK FOR SERVICE. (5471874)

Part: WARNING MESSAGE — ILLUMINATED (PAX DOOR) · airframe 108,233 hrs · 15,334 cycles

SHIP 1602 L FWD ENT DOOR CAUTION MSG ON. CORRECTIVE ACTION: PERFORMED PSEU BITE IAE B767-300 AMM 32-09. NO FAULTS NOTED. MEL AND PLACARD REMOVED. A/C OK FOR SVC. (5480668)

Part: LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 108,233 hrs · 15,334 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: PERFORMED OPS CHK OF INDICATOR IAW B767-300 AMM 52-11. OPS NML. MEL AND PLACARD REMOVED. A/C OK FOR SVC. (0244602)

Part: PSEU — FAULTED (MLG) · airframe 108,174 hrs · 15,322 cycles

SHIP 1602 -GEAR- GEAR DISAGREE ON APPROACH ALT EXTENSION USED. CORRECTIVE ACTION: REPLACED PSEU AND LANDING GEAR CONTROL LEVER MODULE. (5480639)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,485 hrs · 15,200 cycles

SHIP 1602 1R DOOR ARMED LIGHT INTERMITENT. CORRECTIVE ACTION: WAS NOT ABLE TO NOTE INTERMITTENT FAULT, CYCLED TEST SWITCH MULTIPLE TIMES, ALL LIGHTS WORK AS INTENDED. (4368690)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,355 hrs · 15,171 cycles

SHIP 1602 LH AFT EMERGENCY DOOR CABLE NOT INSTALL PROPERLY.NEED DISARM BOTH SIDE TO RESTORE THE DOOR. CORRECTIVE ACTION: DISARM THE OFF-WING ESCAPE SYSTEM AS PER B767-300 AMM25-65-00, REV:139.01-NOV-08-2023.LH AFT EMERGENCY DOOR REMOVED AND REINSTALLED AS PER B767-300 AMM52-21-01 (4368617)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 MEC ACCESS DOOR CUTOUT FWD FRAME FOUND PUNCTURE. CORRECTIVE ACTION: FOR FUTURE INSPECTION CARRY OUT AS PER ERA 613820-14AD (0085099)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 ERA 613820-14 ISSUED FOR REPAIR AT STA 303, LBL 10 FRAME WEB. DT A DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: CORRECTION TO ABOVE, NOT TO EXCEED 22335 CYCLES FROM CURRENT HCK (0084152)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 THS CENTER SECTION UPPER SURFACE FOUND CORROSION AT STA 1746 RBL 11, CORRECTIVE ACTION: THE REWORKED AREA BLEND OUT REPAIRED AS PER PRI:613821-14 (0083569)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 ERA 613820-14AD ISSUED FOR REPAIR TO STA 303 LBL 10 FRAME WEB. A MOC REQUIRED. CORRECTIVE ACTION: AMOC TO AD 2021-10-19 REQUIRED NO LATER THAN 50000 TOTAL FLIGHT CYCLES / 34835 FLIGHT CYCLES FROM CURRENT HCK. (0084157)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 LH APU ACCESS DOOR IB EDGE STA 1894 FOUND DEFORMED. CORRECTIVE ACTION: THE WASTE SERVICE PANEL REMOVED AND REPLACED AS PER B767-300 SRM 52-40-02 (0083722)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 RH NACELLE STRUT FOUND CRACK AROUND PANEL 442AL CUT OUT AT NAC STA231. CORRECTIVE ACTION: REPAIRED AS PER PRI613692-14 (0079189)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 FWD CARGO SHEAR TIE FOUND CORROSION AT STA742 BETWEEN S38R AND S39R, CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (0073687)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1329 BETWEEN S39L AND S39R, CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (0070419)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540 BETWEEN S39L AND S38L, CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (0070431)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 LH WING O/B MAIN FLAP LOWER SURFACE FOUND DENT FROM O /B EDGE 151 INCH, FROM T/E 18 INCH. CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4 (0068888)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 RH VERTICAL FIN FWD TORQUE BOX SKIN PANEL FOUND DELAMINATION AT APPROXIMATE FSS 102. CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4 (0068905)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 AFT CARGO SHEAR TIE FOUND CORROSION AT STA1395 BETWEEN S39L AND S39R, CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (0068759)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 BULK CARGO SHEAR TIE FOUND CORROSION AT STA1540 BETWEEN S39R AND S38R, CORRECITVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 51-40-02 (0068732)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,325 hrs · 15,164 cycles

SHIP 1602 CABIN RH FRAME END FITTING ABOVE CENTER FULE TANK UPPER SURFACE AT STA 927 FOUND CRACK. CORRECTIVE ACTION: THE CRACKED RH FRAME END FITTING AT STA 927 REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 REV 121.00-APR-25-2023. (0067461)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,075 hrs · 15,124 cycles

AIRRAFT 1602, 45 41 38 FG EPATH LT HOUSING BROKEN OFF WITH BAD TAPE REPAIR FAILED. REPLACED LIGHT ASSEMBLIES IAW 767 AMM 33-51. (LP 4467873)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 106,975 hrs · 15,108 cycles

SHIP 1602 DURING LAST C-CHECK (02JAN2020) AT STAG, ER/A 584071-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 1602. ACCOMPLISH ER/A 584071-14AD REV. B SECTION III EXTERNAL HFEC INSPECTION AT AREA 'B' AND AREA 'C' WITHIN 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR (2991400)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 106,927 hrs · 15,101 cycles

SHIP 1602 ER/A 584096-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 1602 (12,986 TFC AND 95,158 TFH) IN THE LH WING LOWER SKIN AT STR L-9.5 AND WSTA 906.2. FOLLOW ON ACTION IS REQUIRED FOR SECT. III INSPECTION. CORRECTIVE ACTION: ACCOMPLISH ER/A 584096-14AD REV. A SECTION III EXTERNAL HFEC INSPECTION AT AREA 'A' AND AREA 'B' WITHIN 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR (12,986 TFC AND 95,158 TFH) DATED 01JAN2020, WHICHEVER OCCURS FIRST. (2988195)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 105,564 hrs · 14,897 cycles

SHIP 1602 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:45F. CORRECTIVE ACTION: EMERGENCY FLOOR LIGHT ASSY RE-SEATED. (2819306)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 105,104 hrs · 14,830 cycles

SHIP 1602 EMERG AISLE LENS COVER MISSING AT R1. CORRECTIVE ACTION: FOUND LENS COVER IN CABIN INSTALLED AT R1 DOOR, OPS NML (5117806)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 105,104 hrs · 14,830 cycles

SHIP 1602 EMERGENCY AISLE LENS COVER NEAR L4 DOOR MISSING. CORRECTIVE ACTION: FOUND LENS COVER IN CABIN, INSTALLED AS REQD, OPS NML, MEL + PLAC RMVD OK FOR SVC (5117804)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 104,501 hrs · 14,723 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: PERFORMED LIGHT TEST AT DOOR 601 PER B767 AMM 33-51 OP CHECK NORMAL OK FOR SERVICE NO FAULTS NOTED (2680568)

Part: BUTTON — STICKING (R1 DOOR) · airframe 103,697 hrs · 14,591 cycles

R1 ENTRY DOOR GREEN ARMING BUTTON STICKS, OPERATIONAL CHECK ACCOMPLISHED AS PER AMM 52-11-00 WORKS SATISF.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 103,020 hrs · 14,491 cycles

SHIP 1602 EMERGENCY LIGHTS ROW 45-53 L INOP. CORRECTIVE ACTION: FOUND POWER PACK M9010 INOP R&R POWER PACK PER B767-300 AMM 33- 51 LIGHTS OPS CK. OK. (9409569)

Part: SHROUD — BROKEN (EMERGENCY LIGHTS) · airframe 102,901 hrs · 14,470 cycles

SHIP 1602 EMERGENCY LIGHT SHROUD ASSY BROKEN AT SEATS 46F AND 50B. CORRECTIVE ACTION: R/R EMERGENCY LIGHT SHROUD ASSY PER B767 AMM 25-60 (9409501).

Part: NONE — NONE · airframe 101,935 hrs · 14,327 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:101, CORRECTIVE ACTION: R+R SLIDE INDICATOR LIGHT PER B767-300 AMM 32-28 OPS CHKS GOOD (2362322)

Part: NONE — NONE · airframe 101,881 hrs · 14,321 cycles

SHIP 1602 INDICATOR LIGHT FOR THE ARM/DISARM DOOR IS INOP , CORRECTIVE ACTION: CHECKED INDICATOR LIGHTS FOR ARM/DISARM AT ALL DOORS--NO TROUBLE FOUND. (9016243)

Part: INDICATOR — DAMAGED · airframe 100,947 hrs · 14,191 cycles

SHIP 1602 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:101. CORRECTIVE ACTION: LOCATION 101 SLIDE INDICTOR LIGHTS INSPECTED AND CHKS GOOD. (2262629)

Part: INDICATION SYS — UNSERVICEABLE · airframe 100,786 hrs · 14,161 cycles

SHIP 1602 FAINT POP NOISE FROM RADAR SCREEN FOLLOWED BY DARK RADAR SCREEN ALONG WITH BURNING ELECTRICAL SMELL, CORRECTIVE ACTION: R/R WEATHER RADAR INDICATOR UNIT PER B767 AMM 34-43 OPS TEST GOOD. INSPECTED NEARBY COMPONENTS AND WINDOW HEAT FOR ELECTRICAL SMELLS. NO ODORS PRESENT IN FLIGHT DECK. (8651404)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,412 hrs · 14,083 cycles

SHIP 1602 DURING SVC CHECK FOUND LOWER CREW REST EMERGENCY LIGHT AT AFT BUNK INOP, CORRECTIVE ACTION: T/S AND NTF WITH THE WIRES. SUSPECTING THE CREW REST EXIT SIGN PN BR9795-001. FWD TO MEL & PLACARDED (8793416)

Part: NONE — NONE · airframe 99,820 hrs · 13,992 cycles

SHIP 1602 -ATB- DUE TO F/O AIRSPEED INDICATOR INOP AND UNABLE TO CONTINUE RSVM FLIGHT. CORRECTIVE ACTION: REPLACED F/O AIRSPEED INDICATOR. (8487558)

Part: NONE — NONE · airframe 99,736 hrs · 13,980 cycles

SHIP 1602 -PRES- CABIN AUTO INOP EICAS MESSAGE AND ASSOCIATED LIGHT ILLUMINATED IN CRUISE. MAN PRESSURIZATION MODE SELECTED. DURING DECENT UNABLE TO CONTROL CABIN PRESSURE. MASKS DEPLOYED AND EMERGENCY DESCENT COMPLETED. CORRECTIVE ACTION: FOUND WATER SUPPLY LINE TO AFT GALLEY LEAKING CAUSING ICE AROUND OUTFLOW VALVE. REMOVED ICE, OUTFLOW VALVE OPS CHK GOOD. MTC FOR OTHER SYS IN PROGRESS. (7989999)

Part: NONE — NONE · airframe 99,671 hrs · 13,964 cycles

SHIP 1602 CABIN COMPARTMENT LH "T" FITTING FOUND CRACK AT BS 927.5 AND S-21L. CORRECTIVE ACTION: THE FITTING REPLACED AT CABIN COMPARTMENT BS927.5 AND S-21L AS PER B767-300 SRM 51-40 (2083530)

Part: NONE — NONE · airframe 99,671 hrs · 13,964 cycles

SHIP 1602 THE L/H VERT-STAB HONEYCOMB PNL DELAMINATION BETWEEN AUX SPAR AND FRONT SPAR AND FSS220.521 TO FSS 245.653, CORRECTIVE ACTION: REPAIRED OER PRI 596254-14 (2080997)

Part: SMOKE DETECTOR — DETACHED (LAVATORY) · airframe 98,342 hrs · 13,690 cycles

SHIP 1602 LAV SMOKE DETECTOR RIPPED FROM BASE. CORRECTIVE ACTION: REPLACED SMOKE DETECTOR. (LP 7359164)

Part: BUTTON — NOT SEATED (L1 DOOR SLIDE) · airframe 98,034 hrs · 13,627 cycles

SHIP 1602 L1 DOOR SLIDE LIGHT FLICKERS ON/OFF INTERMITTENTLY AFTER LANDING. CORRECTIVE ACTION: FOUND L1 DOOR SLIDE LIGHT PUSH BUTTON ASSEMBLY NOT SEATED CORRECTLY AND RESEATED. SYSTEM OPERATION IS NORMAL. (LP 7366036)

Part: CYLINDER — DAMAGED (SLIDE) · airframe 97,688 hrs · 13,543 cycles

SHIP 1602 WHILE WORKING AMDS 2561-4697 MAINTENANCE FOUND R/H INFLATION CYLINDER BALL NOT BEHIND RETAINER SPRING AND REPLACED INFLATION CYLINDER. SYSTEM OPERATION IS NORMAL. (LP 7592365)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 106,927 hrs · 15,101 cycles

SHIP 1602 THIS ER/A 584071-14 INCORPORATES FAA FORM 8100-9. ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. THE SUBJECT ER/A IS NOW AT REV. A. CORRECTIVE ACTION: AT OR PRIOR TO 12,000 FLIGHT CYCLES OR 36,000 FLIGHT HOURS AFTER REPAIR ACCOMPLISHMENT (WHICHEVER OCCURS FIRST), AND REPETITIVELY THEREAFTER EVERY 12,000 FLIGHT CYCLES OR 36,000 FLIGHT HOURS (WHICHEVER OCCURS FIRST) ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. (1670515)

Part: PANEL — MISSING (RT WING) · airframe 95,984 hrs · 13,128 cycles

ON PRE-FLIGHT WALK AROUND FOUND PANEL 621AKB MISSING AT RIGHT WING LOWER OUTBOARD SURFACE. CORRECTIVE ACTION: REINSTALLED PANEL.

Part: NUT — DAMAGED (EMERGENCY LIGHT) · airframe 95,970 hrs · 13,117 cycles

DURING INSPECTION FOUND DAMAGED ANCHOR NUT ON LT EXTERNAL EMERGENCY LIGHT STA 1097. CORRECTIVE ACTION: REPLACED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (WING) · airframe 95,158 hrs · 12,986 cycles

WHILE IN C-CHECK MTC DISCOVERED CRACK INDICATION AT FASTENER HOLE #1, #2, #3 AND #4 C/W ERA 584096-14. (LP 1430047)

Part: SKIN — CRACKED (RT WING) · airframe 95,158 hrs · 12,986 cycles

WHILE IN ATL FOR C-CHECK VISIT MTC FOUND RH WING LOWER SKIN WSTA 962.2 TO 990.2, STR L-9.5 / HOLE #66 CRACKED, C/W ERA 584071-14 (LP 1430117)

Part: SKIN — CRACKED (RT WING) · airframe 95,158 hrs · 12,986 cycles

RH WING LOWER SKIN WSTA 906.2 TO 962.2, STR L-9.5 HOLE #22 & #49 - CRACKED. C/W ERA 584095-1 (LP 1430095)

Part: NONE — NONE (NONE) · airframe 103,768 hrs · 14,601 cycles

TRACKING FOR SECTION II: REPETITIVE INSPECTION - ERA 584135-14AD. ER/A 584135-14AD REVISED TO REV. A. ACCOMPLISH ER/A 584135-14AD REV A SECTION II INSPECTIONS.

Part: SKIN — CRACKED (RT WING) · airframe 95,158 hrs · 12,986 cycles

RH WING LOWER SKIN WSTA 962.2 TO 990.2, STR L- 9.5 HOLE #66 HAS CRACK INDICATION C/W ERA 584095-14 (LP 1422879)

Part: SKIN — CRACKED (RT WING) · airframe 95,158 hrs · 12,986 cycles

RH WING LOWER SKIN WSTA 906.2 TO 962.2, STR L- 9.5 HOLE #22 & #49 CRACK REPAIRED PER ERA 584095-00. (LP 1420363)

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 95,028 hrs · 12,963 cycles

EMERGENCY ESCAPE PATH LIGHTS AT ROWS 27FG, 32FG AND 28AB ARE INOPERATIVE. FOUND EMERGENCY EXIT LIGHTING SEAT TO SIDEWALL HARNESS DAMAGED AT THE SIDEWALL FOR SEATS 28AB AND 32FG. REPAIRED LIGHTS MCO/PLAC REMOVED. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,788 hrs · 12,932 cycles

AFTER EMERGENCY LIGHT BATTERY REPLACEMENT , L/H SEATS 21-31 WOULD NOT ILLUMINATE. REPLACED BATTERY CHARGER ASSY AT M9009. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — DAMAGED (ROW 16F) · airframe 94,572 hrs · 12,904 cycles

DAMAGED SEAT PATH LIGHT SHROUD AT 16F. REPLACED SHROUD. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — DAMAGED (ROWS 28F-30F) · airframe 94,572 hrs · 12,904 cycles

DAMAGED SEAT PATH LIGHT SHROUD AT POSITION 28F AND 30F. REPLACED 2 EACH SHROUD. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,151 hrs · 12,724 cycles

LLCR EMERGENCY LIGHTS ALL BURNT. REPLACED ALL EMERGENCY LIGHTS BULBS IN LLCR. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,538 hrs · 12,646 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE. REFITTED LIGHT ASSSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: BUSTLE — DAMAGED (EVAC SLIDE) · airframe 91,253 hrs · 12,478 cycles

UPPER FWD LATCH ON R1 SLIDE BUSTLE DAMAGED. REPLACED R1 SLIDE BUSTLE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 90,750 hrs · 12,416 cycles

ON SERVICE CHECK FOUND EMERGENCY OVERHEAD LIGHTING INOPERATIVE AT ROWS 19 & 31 LEFT SIDE. REPLACED POWER SUPPLY AT SEAT 23A. MCO/PLACARD REMOVED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 90,592 hrs · 12,395 cycles

LEFT EMERGENCY LIGHTS ARE INOPERATIVE. FOUND DISCONNECTED CONNECTOR AND RE-SECURED. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 89,492 hrs · 12,243 cycles

EMERGENCY LIGHTS AT 16G ARE INOPERATIVE. FOUND WIRES DISCONNECTED AT SEAT LEG AND RECONNECTED. SYSTEM OPERATION IS NORMAL.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 88,975 hrs · 12,175 cycles

WHITE EMERGENCY LIGHTS AT SEAT 28B ARE INOPERATIVE. FOUND A WIRE PULLED OUT AT CONNECTOR AND RESEATED. SYSTEM OPS NORMAL.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 87,621 hrs · 11,996 cycles

FLOOR EMERGENCY LIGHT LENS AT SEAT 27B WAS FOUND DAMAGED. REPLACED THE LENS.

Part: LIGHT — OUT OF POSITION (SEAT 27B) · airframe 87,621 hrs · 11,996 cycles

FLOOR EMERGENCY LIGHT AT SEAT 27B WAS FOUND OUT OF POSITION. REPOSITIONED THE LIGHT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 86,904 hrs · 11,896 cycles

EMERGENCY LIGHTS AT SEATS 22-30 ARE INOPERATIVE. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CORRODED (BS 1400) · airframe 86,831 hrs · 11,886 cycles

DURING A WALKAROUND, FOUND THE SKIN, STRINGER 36R LAP JOINT AT BS 1400 TAPERED SHIM CORRORDED. COMPLIED WITH ERA 566202-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,373 hrs · 11,823 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROWS 21 - 30 LEFT AISLE. REPLACED THE POWER SUPPLY. THE SYSTEM OPS NORMAL

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 85,776 hrs · 11,739 cycles

CABIN FLOORBEAM AT STA 1439 LBL24 FOUND CRACKED. C/W ERA 563089-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 85,776 hrs · 11,739 cycles

FWD CABIN FLOORBEAM AT STA 347 BETWEEN RBL 20 AND RBL 55 FOUND CORROSION. C/W ERA 563377-14.

Part: FAILSAFE — CRACKED (BS 955) · airframe 85,776 hrs · 11,739 cycles

DURING AN ULTRASONIC INSPECTION OF THE LT BS 955 FAILSAFE STRAP IAW W/C 5312-01170-05, FIG 1, STEP 4, FOUND THE FAILSAFE STRAP CRACKED. REPAIRED.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 85,776 hrs · 11,739 cycles

LEFT WING OTBD FLAP UPPER SURFACE AT WS 675 AND 5.7 INCH FROM TRAILING EDGE FOUND DENTED. REPAIRED THE SKIN IAW SRM 57-53-01.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 85,776 hrs · 11,739 cycles

LEFT WING OTBD FLAP UPPER SURFACE AT WS 670 AND 8.75 INCH FROM TRAILING EDGE FOUND DENTED. REPAIRED THE SKIN IAW 57-53-01.

Part: SHEAR TIE — CORRODED (BS 1087) · airframe 85,776 hrs · 11,739 cycles

AFT CARGO SHEAR TIE AT BS 1087 STRINGERS 39L & 39R FOUND CORRODED AND WAS REPLACED.

Part: SEAT TRACK — CORRODED (BS 929-998) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

SEAT TRACK AT RBL 11 BETWEEN BS 929 AND 998 FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 347) · corrosion level 2 · airframe 90,064 hrs · 12,319 cycles

DURING AN H CHECK, CORROSION WAS FOUND ON THE BS 347 FLOORBEAM. REPAIRED IAW SRM 53-00-51-2R-1, AND ER/A 563377-14.

Part: SEAT TRACK — CORRODED (BS 929-998) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

SEAT TRACK AT LBL 11 BETWEEN BS 929 AND 998 FOUND CORRODED OUT OF LIMITS. REPLACED THE SEAT TRACK.

Part: FLOORBEAM — CORRODED (BS 888.5) · airframe 85,776 hrs · 11,739 cycles

MID LAVATORIES FLOORBEAM AT BS 888.5, RBL 11, FOUND CORRODED. THE CORROSION REMOVED, ON THE FLOORBEAM UPPER FLANGE AND REPAIRED.

Part: SHEAR TIE — CORRODED (BS 1373) · airframe 85,776 hrs · 11,739 cycles

BULK CARGO SHEAR TIE AT BS 1373, STRINGER 39L FOUND CORRODED AND WAS REPLACED.

Part: FLOORBEAM — CORRODED (BS 911) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

MID LAVATORIES FLOORBEAM AT BS 911, LBL 11 FOUND CORRODED. OUT OF LIMITS. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 1428-1445) · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT LBL 88.5 BETWEEN BS 1428 AND 1445 FOUND CORRODED AND OUT OF LIMITS.

Part: SEAT TRACK — CORRODED (BS 998-1071) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT RBL 11 BETWEEN BS 998 AND 1071 FOUND CORRODED AND OUT OF LIMITS. THE SEAT TRACK WAS REMOVED AND REPLACED. (LP 0294598)

Part: SEAT TRACK — CORRODED (BS 998-1071) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT LBL 88.5 BETWEEN BS 998 AND 1071 FOUND CORRODED AND OUT OF LIMITS. THE SEAT TRACK WAS REPLACED.

Part: FRAME — CRACKED (BS 903) · airframe 85,776 hrs · 11,739 cycles

INSPECTION FOUND ONE CRACK ON THE LT BS 903.5 FRAME. REPAIRED THE FRAME.

Part: SEAT TRACK — CORRODED (BS 1230-1362) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

SEAT TRACK AT LBL 88.5 BETWEEN BS 1230 AND 1362 FOUND CORRODED AND OUT OF LIMITS. THE SEAT TRACK WAS REPLACED.

Part: BUSHING — CHAFED (PYLON LINK) · airframe 85,776 hrs · 11,739 cycles

NR 1 PYLON FWD UPPER LINK FITTING BUSHINGS FOUND CHAFED. NEW BUSHINGS INSTALLED IAW SRM 54-52-90.

Part: SEAT TRACK — CORRODED (BS 1362-1428) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT LBL 88.5 BETWEEN BS 1362 AND 1428 FOUND CORRODED AND OUT OF LIMITS. THE SEAT TRACK WAS REPLACED.

Part: SEAT TRACK — CORRODED (BS 1241-1285) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT RBL 88.5 BETWEEN BS 1241 AND 1285 FOUND CORRODED AND OUT OF LIMITS. THE SEAT TRACK WAS REPLACED.

Part: SEAT TRACK — CORRODED (BS 1428-1450) · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT RBL 88.5 BETWEEN BS 1428 AND 1450 FOUND CORRODED AND IS OUT OF LIMITS IAW SRM 53-00-52. REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1098-1197) · airframe 85,776 hrs · 11,739 cycles

SEAT TRACK AT RBL 88.5, BS 1098 TO 1197+33 CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS. REPAIRED THE SEAT TRACK

Part: SEAT TRACK — CORRODED (BS 1197-1208) · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK, RBL 88.5 BETWEEN BS 1197+33 AND 1208 FOUND CORRODED. FOUND OUT OF LIMITS. REPAIRED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1098-1197) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT LBL 88.5 BETWEEN BS 1098 AND 1197+33 FOUND CORRODED. REMOVED IAW SRM 51-10-02, REV 105. REWORKED AREA WAS FOUND OUT OF LIMITS. A REPAIR SPLICE WAS INSTALLED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 966-1098) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT LBL 88.5 BETWEEN BS 966 AND 1098 FOUND CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02, REV 105. THE REWORKED AREA WAS FOUND OUT OF LIMITS. REPAIRED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 965-1098) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

CABIN SEAT TRACK AT RBL 88 BETWEEN BS 965 AND 1098 FOUND CORRODED. THE CORROSION WAS REMOVED AND THE AREA WAS FOUND OUT OF LIMITS. REPAIRED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 836-965) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

SEAT TRACK AT RBL 88.5 BETWEEN BS 836 AND 965 FOUND CORRODED AND WAS OUT OF LIMITS. REPAIRED THE SEAT TRACK.

Part: FRAME — CRACKED (BS 883) · airframe 85,776 hrs · 11,739 cycles

INSPECTION FOUND ONE CRACK ON THE BS 883.5 FRAME. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 1197-1230) · corrosion level 2 · airframe 85,776 hrs · 11,739 cycles

SEAT TRACK AT LBL 88.5 BETWEEN BS 1197+33 AND 1230 FOUND CORRODED. FABRICATED A REPAIR SPLICE, AND INSTALLED IAW SRM 51-40-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,279 hrs · 11,673 cycles

CEILING EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,279 hrs · 11,673 cycles

LOWER CREW REST HORIZONTAL EXIT SIGN IS INOPERATIVE. REPLACED ALL EIGHT BULBS. OPS CHECKED NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,279 hrs · 11,673 cycles

LOWER CREW REST VERTICAL EXIT SIGN IS INOPERATIVE. REPLACED THE BULBS, OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,491 hrs · 11,447 cycles

DURING CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT MID LAVATORY, CROSS AISLE, LEFT SIDE. REPLACED THE POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,824 hrs · 11,237 cycles

L2 EMERGENCY DOOR LIGHT. REPLACED LIGHT FILAMENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,271 hrs · 11,166 cycles

INTERIOR CEILING EMERGENCY LIGHT ABOVE SEAT 1A IS INOPERATIVE. RELAMPED SYSTEM OPERATION IS NORMAL.

Part: LENS — MISSING (CABIN) · airframe 81,271 hrs · 11,166 cycles

SEAT 5E EMERGENCY LIGHT LENS IS MISSING. REPLACED LENS SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 81,271 hrs · 11,166 cycles

POWER SUPPLY M739 AT SEAT 39A DOES NOT HOLD BATTERY IN POSITION. REPLACED POWER SUPPLY SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,271 hrs · 11,166 cycles

LEFT AFT WING, FORWARD SIDE EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,271 hrs · 11,166 cycles

INTERIOR CEILING EMERGENCY LIGHT ABOVE SEAT 7D IS INOPERATIVE. RELAMPED SYSTEM OPERATION IS NORMAL.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 73,859 hrs · 10,247 cycles

LEFT WING: STR 9, HOLE NR 2, UNINSPECTABLE HOLE, POSSIBLE TOOLING DAMAGE, HOLE MARKED. COMPLIED WITH ER/A 534193-14, REV ORIGINAL.

Part: SKIN — CRACKED · airframe 73,859 hrs · 10,247 cycles

FOUND 2 FASTENER HOLES WITH CRACKS AT INBD END OF STR L6.5, MARKED, LT WING. COMPLIED WITH ER/A 534105-14AD, REV ORIGINAL AND NON-ROUTINE CARD 152 DURING C2 MAINTENANCE VISIT.

Part: SKIN — CRACKED (RT WING) · airframe 73,859 hrs · 10,247 cycles

ACFT 1602, RT WING, STR 10 FASTENER HOLE NR 5 CRACK INDICATION-MARKED, COMPLIED WITH ER/A 534194-14, REV 0, 1878134.

Part: SKIN — CRACKED (RT WING) · airframe 73,859 hrs · 10,247 cycles

RT WING STR 9 HOLE NR 8-MARKED, UNINSPECTABLE HOLE, POSSIBLE TOOLING DAMAGE. COMPLIED WITH ERA 534194-14, REV 0, 1878141.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 69,119 hrs · 9,665 cycles

SEATS 37F AND 39F EMERGENCY LIGHTS INOPERATIVE. CONNECTED LIGHTS. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,883 hrs · 9,510 cycles

FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSY IAW AMM 33-51. OPS CHECKED OK.

Part: WIRE — DAMAGED (CABIN)

SEAT 17B EMERGENCY ESCAPE PATH MARKING LIGHT INOP. FOUND WIRE DAMAGED ON OUTBOARD SEAT LEG. REPAIRED AND RE-TERMINATED CONNECTOR PER BOEING SPWM 20-42-01. OPS CK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

FLOOR PATH EMERGENCY LIGHTS INOP FROM ROWS 6 TO 21 LEFT AND RIGHT SIDES. REPLACED POWER SUPPLY AND BATTERY PACK M9011IAW AMM 33-51-07. OPS CHECKS NORMAL.

Part: WIRE HARNESS — FAILED (MONITOR) · airframe 61,754 hrs · 8,694 cycles

3D SEAT MONITOR STARTED TO SMOKE, TURNED OFF MONITOR AT SEAT ONLY SMOKE STOPPED AND MONITOR COOLED DOWN. PAX SEAT 3G MONITOR REMOVED AND REPLACED MONITOR AND SDU HARNESS AT PAX SEAT 03G IAW AMM 23-32-00 AND DRAWING RD-KM6265 REV B OPS CHECKED NORMAL MONITOR.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 61,277 hrs · 8,636 cycles

ON DRC FOUND ROW 21AB THRU 30AB EMERGENCY LIGHTS INOPERATIVE. THE CHARGER WAS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CHAFED (LE SLAT) · airframe 59,816 hrs · 8,442 cycles

LT WING NR 4 SLAT O/B EDGE RIB O/B SURFACE WAS FOUND CHAFED.

Part: SLAT — CRACKED (RT WING) · airframe 59,816 hrs · 8,442 cycles

RT WING NR 7 SLAT FROM I/B 61 INCHES AND FROM T/E 4 INCHES FOUND A 0.375 INCH CRACK. METAL HOT BOND REPAIR PERFORMED AS PER B767-300 SRM 51-70-10 REPAIR 2 FIG 203.

Part: FLAP — DELAMINATED (RT WING) · airframe 59,816 hrs · 8,442 cycles

RIGHT WING - O/B AFT FLAP T/E FOUND DAMAGE AT APPROXIMATELY 30" FROM I/B EDGE. RIGHT WING O/B AFT FLAP T/E AT APPROX 30" FROM I/B EDGE AREA COMPOSITE REPAIR CARRIED OUT AS PER B767-300 SRM 51-70-06 PAR 5D FIG 7 AND REF HX PROCESS CARD SEQ NO.GJX512057-1 FOR DETAIL.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 59,428 hrs · 8,393 cycles

ON DRC MAINTENANCE FOUND ROWS 31-41AB EMERGENCY LIGHTS INOPERATIVE THE FUSE IN THE BATTERY CHARGER WAS REPLACED. SYSTEM OPERATION IS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,965 hrs · 8,338 cycles

EMERGENCY LIGHTS ROWS 1 THROUGH 6 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: ENGINE — FAILED (NR 1) · airframe 58,524 hrs · 8,283 cycles

ATB, SHIP 1602 FLT 56 EWR-AMS RETURNED TO EWR DUE TO LEFT ENGINE FAILURE ON CLIMB. ENGINE REPLACEMENT. ETOPS CATEGORY 'A': ANY IN-FLIGHT SHUTDOWN.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,791 hrs · 8,052 cycles

EMERGENCY LIGHTS AT SEATS 31AB-41AB ARE INOPERATIVE. MX REPLACED THE PACK FUSE LIGHTS AT 31AB-41AB. SYS OPS IS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 56,791 hrs · 8,052 cycles

EMERGENCY LIGHTS AT 14AB-20AB ARE INOPERATIVE. MX FOUND A DAMAGED SEAT HARNESS AT 17AB AND REPLACED. SYS OPERATION IS NORMAL.

Part: DECODER — FAULTY (ENTERTAIN SYS) · airframe 56,421 hrs · 8,004 cycles

FLIGHT RETURNED TO DEPARTURE DUE TO UNIDENTIFIED FUMES IN THE CABIN, BURNED RUBBER SMELL. ONCE ON THE GROUND MX FOUND AN ELECTRICAL SMELL COMING FROM TRANSFORMER T182 LOCATED IN THE P25 PANEL. THE TRANSFORMER WAS REPLACED. ALSO A DEFECTIVE SEAT DECODER AT 24 CDE WAS FOUND AND REPLACED. AN IDLE AND HIGH POWER ENGINE RUN WAS PERFORMED ALONG WITH INSPECTIONS BY PANASONIC FOR IFE ISSUES. ALL GALLEY EQUIPMENT WAS CHECKED OUT WITH NO FINDINGS.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 55,433 hrs · 7,874 cycles

THE EMERGENCY LIGHTS AT ROW 22AB ARE INOPERATIVE. MAINTENANCE RE-SEATED A LOOSE CONNECTOR AND THE SYSTEM WAS OPERATIONAL AGAIN. (2010-D1338) (DL76G103061)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,433 hrs · 7,874 cycles

THE EMERGENCY LIGHT AT L2 LAVATORY IS INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY PER AMM 33-51-10. SYSTEM OPERATION RETURNED TO NORMAL. (2010-D1337) (DL76G103060)

Part: APU — FAILED · airframe 51,357 hrs · 7,350 cycles

APU FAILED ON PUSHBACK WITH A FAULT LIGHT ILLUMAINATED. AFTER SYS RESET TEST PERFORMED WITH PNEUMATIC LOAD APPLIED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: UNKNOWN — ODOR (EQUIP COOLING) · airframe 50,726 hrs · 7,257 cycles

DURING PREFLIGHT HAD STRONG ELEC SMOKE ODOR IN COCKPIT, GOT STRONGER FOR ABOUT 2 MIN THEN DISSIPATED. NO C/BS WERE FOUND TO BE POPPED. SMELLED ALL RACKS IN E AND E COMP, NO ODORS. PULLED C/B PANELS, OP IN COCKPIT NO ODORSS. PULLED FWD INSTRUMENT PANEL AND CRT. SMELLS FROM EQUIPMENT OR EQUIPMENT COOLING. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,312 hrs · 7,202 cycles

EMERGENCY LIGHT ON FUSELAGE NEAR R-2 DOOR INOP. RELAMPED, LIGHT CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,302 hrs · 7,201 cycles

EMERGENCY LIGHT ON FUSELAGE NEAR R2 DOOR INOP. RELAMPED, CHECKS GOOD.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 50,171 hrs · 7,186 cycles

EMERGENCY PATH LIGHTING INOP AT SEATS 22B AND 23B. REPLACED CONNECTORS AT SEAT JUNCTIONS, OPS CHECK NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: APU — UNSERVICEABLE (APU BAY) · airframe 49,619 hrs · 7,118 cycles

REPLACED APU DUE TO HISTORY OF NOT STARTING.

Part: MODULE — MALFUNCTIONED (THRUST REVERSER) · airframe 47,520 hrs · 6,858 cycles

LT REV ISLN VALVE EICAS MSG AT 10 TO 20 KTS DURING T/O MUC FWD LT T/R TO MCO/PLAC PER MEL 78-31-01. M PROCEDURE C/W, T/S PER FIM. NO TROUBLE FND. NO MSGS ON T/R RELAY MODULE. OPERATED T/R SEVERAL TIMES UNDER ENG PWR. OPS CKS NML. MCO/PLACARD REMOVED.

Part: RELAY — MALFUNCTIONED (THRUST REVERSER) · airframe 47,520 hrs · 6,858 cycles

LEFT REVERSER ISOLATION VALVE MESSAGE CAME ON DURING START OF T/O ROLL. FWD LEFT THRUST REVERSER TO MCO AND PLACARD PER MEL 78-31-01 M PROC COMPLIED WITH TROUBLE SHOOTING PER FIM. NO TROUBLE FOUND. NO MESSAGES ON THRUST REVERSER RELAY MODULE. OPERATED THRUST REVERSER SEVERAL TIMES UNDER ENGINE POWER. OPS CHECKS NORMAL. MCO/PLACARD REMOVED.

Part: TRUNNION — CORRODED (NLG) · airframe 46,920 hrs · 6,787 cycles

FOUND RT NLG TRUNNION FITTING WITH LOOSE BUSHING AND CORRODED IN BRE. OVERESIZED BORE AND INSTALLED OVERSIZED BUSHING.

Part: PUMP — DEFECTIVE (HYDRAULIC SYS) · airframe 46,910 hrs · 6,786 cycles

C HYD PRIM 1 ANNUNCIATOR ILLUMINATED DURING TAXI. FOUND ELECTRICAL CONNECTOR PITTED ON C1 PUMP. REMOVED AND REPLACED C1 PUMP AND CONNECTOR PIN B BURNT. REPLACED CONNECTOR D482. ALL LEAK AND OPS CHECK GOOD. PUMP MFG P/N 731966.

Part: DOOR — OPEN (APU BAY) · airframe 46,314 hrs · 6,717 cycles

RTB - APU DOOR LIGHT ILLUMINATED ON TAXI OUT. ACFT RELEASED AS PER MEL 49-15-01A APU INTAKE DOOR CLOSED.

Part: APU — UNKNOWN · airframe 46,137 hrs · 6,697 cycles

REPLACED APU DUE START HISTORY. APU REPLACED.

Part: ENGINE — MAKING METAL (NR 2) · airframe 45,553 hrs · 6,631 cycles

FOUND DURING SERVICE CHECK, FOUND METAL ON MCD. SHOP ANALYST REPORTS BEARING MATERIAL. MUST REPLACE ENGINE, E/C IN WORK ATL.

Part: WIRE — DAMAGED (CABIN) · airframe 43,605 hrs · 6,407 cycles

ON ARRIVAL, ELECTRICAL SMELL DETECTED IN MID GALLEY. FOUND DAMAGED WIRING AT FLUORESCENT LIGHT ABOVE SEAT 16FG. SECURED AFT OUTBD INDIRECT LIGHTING C/B AND INSULATED WIRES. FWD TO MCO AND PLACARD PER MEL 33-21-01. REPLACED 1 OF 2 SOCKET FWD SOCKET ABOVE 16GF 504125. REPLACED THE SECOND SOCKET AFT SOCKET AT 16GF AND RESET C/B P33 L4. OP CK OK.

Part: LINE — CRACKED (NR 2 ENGINE OIL) · airframe 43,363 hrs · 6,371 cycles

RT ENG OIL QTY LOSS, FOUND OIL QTY XMITTER LINE MPN 1978M64G01 CRACKED. REPLACED SAME, LEAK CKS OK SERVICED ENG W/MOBIL JET.

Part: PSEU — MALFUNCTIONED (TE FLAPS) · airframe 43,151 hrs · 6,343 cycles

AFTER FLAPS UP AIRBORNE, GOT AN EICAS FLAP MSG AND A CONFIG WARNING LIGHT AND WARNING HORN. HORN AND LIGHT WENT OUT WHEN THROTTLES REDUCED BELOW 85 PERCENT. OPS NORMAL WITH FLAPS OUT OF UP POSITION. REMOVED AND REPLACED RELAY K215 AIR/GND NLG SYS 2. BITE FSEU AND PSEU, NO FAULTS FOUND. CHECKED NOSE GEAR TARGET FOR DAMAGE ALL OK. REMOVED AND REPLACED PSEU PER AMM. NO FAULTS NOTED. ALL GND CHKS NORMAL.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 41,344 hrs · 6,123 cycles

CREW REPORTED ON RT ENG START HAD R EEC CONTROL STATUS MSG AND EEC CHAN "A" CB POPPED. CB WOULD NOT RESET. NO DISPATCH FAULT. REPLACED RT EEC. ALL MESSAGES CLEARED.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 40,886 hrs · 6,070 cycles

AT CRZ RIGHT ENG HAD LOUD BANG A/C YAW AND THEN ENG FAILURE. DIVERTING TO TO MAO FOR REPAIRS. CHANGED ENG ON R/C DECK TRANS 76X1T161 CARD 1 THRU 34.

Part: BRAKE ASSY — DAMAGED (MLG) · airframe 38,438 hrs · 5,774 cycles

NR 8 BRAKE TEMP READ SEVEN AFTER PARKING. REPLACED BRAKE ASSY. LEAK AND OPS CK C/W GOOD. PERFORMED AXLE HI-TEMP INSPECTION. NO DEFECTS FOUND ON AXLE.

Part: CONTROL PANEL — NO TEST (OVERHEAT LIGHT) · airframe 37,888 hrs · 5,709 cycles

FOUND LT ENG OVERHEAT LIGHT WOULD NOT TEST. REPLACED FIRE PANEL W/LIKE FROM A/C 173 PER MCC M. CHECKS GOOD PER MM 26-21-02.

Part: TURBINE — MAKING METAL (APU) · airframe 37,384 hrs · 5,647 cycles

APU AUTO SHUTDOWN AT GATE. FOUND METAL ON CHIP DETECTOR. REPLACED APU.

Part: HMU — MALFUNCTIONED (NR 1 ENG) · airframe 36,804 hrs · 5,575 cycles

APPROX 60 MIN INTO FLT THE R ENG HPSOV EICAS MSG CAME ON FOR APPROX 3 MINS THEN EXTINGUISHED BY ITSELF. DURING THIS TIME THE L ENG INTR WERE AS FOLLOWS N1 AT YEL/EGT 800/N2 103/FF8.0/VIB 1.5. L ENG THROTTLE UNRESPONSIVE. R ENG NORMAL. UPON CONSULT W/ ATL MX AND QRH L ENG EEC PLACED IN ATLN MODE WITH NO EFFECT. L ENG SHUTDOWN AT 20000. UNEVENTFUL LANDING AT JFK. JFK MTC REPLACED L ENG HMU AND EEC, ENG RUN NORMAL.

Part: ANTENNA — INOPERATIVE (ATC) · airframe 35,795 hrs · 5,451 cycles

DURING TAXI OUT, BOTH ATC SHOWED ATC FAIL LIGHT AND EICAS ATC FAULT MSG ALSO LOWER ANTENNA FAULT ON RADAR DISPLAY. REPLACED COCKPIT CONTROL PANEL AND LOWER ANTENNA PER MM BOTH TRANSPONDERS NOW TEST NORMALLY.

Part: FAN — UNSERVICEABLE (CABIN) · airframe 35,212 hrs · 5,385 cycles

VIBRATION AND ELEC SMELL MID GALLEY AREA LEFT SIDE CEILING AREA. STOPPED AFTER TWO-THREE MINS. FOUND GASPER FAN CB POPPED. REPLACED GASPER FAN, OPS OK.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 34,606 hrs · 5,313 cycles

ON TAXI OUT, NR 1 GEN LIGHT ON. SWAPPED A/C TO 183. REPLACED NR 1 IDG.

Part: MOTOR — FAILED (COCKPIT SEAT) · airframe 27,134 hrs · 4,306 cycles

DIVERTED INTO PHX DUE TO F/O SEAT SMOKE AND SPARKS INFLIGHT FOUND F/O SEAT ELECTRIC DRIVE MOTOR FAULTED AND C/B POPPED. REPLACED MOTOR.

Part: CIRCUIT CARD — FAILED (E/E BAY) · airframe 26,855 hrs · 4,258 cycles

ON TAKEOFF SEVERAL LIGHTS FLICKERED AND REMAINED ON FOR UP TO 1 MINUTE, FIRE ON ANNUNCIATOR PANEL ILLUMINATED. REPLACED AFOLTS CARD.

Part: CIRCUIT CARD — INTERMITTENT (FIRE PANEL) · airframe 26,829 hrs · 4,253 cycles

ON DEPARTURECLIMBING THRU 1000 FT DISCRETE FIRE LIGHT ILLUM WITH NO AURAL OR OTHER VISUAL INDICATIONS, LIGHT EXT PASSING THRU 4000 FT. REPLACED AFOLTS CARD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,692 hrs · 4,092 cycles

ER/A 092012-14 REV A: FUSELAGE SKIN STA 698 S-35R REPAIR OF GOUGES. DUE TO SERVICE DAMAGE, THE FUSELAGE SKIN WAS FOUND GOUGED AND SCRATCHED AT FS 698 ADJACENT TO STRINGER 35R. AN APPROX 8.25 INCHES WIDE X 6 INCHES TALL SKIN CUTOUT WAS REQUIRED TO REMOVE THE DAMAGE. ER/A ACCOMPLISHES A REPAIR CONSISTING OF INSTALLATION OF AN EXTERNAL REPAIR DOUBLER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,765 hrs · 3,192 cycles

ON L/O FOUND EMERGENCY EXIT LIGHT INOP AT 37FG OVERHEAD. RELAMPED, CHECKS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,765 hrs · 3,192 cycles

ON L/O, FOUND EMERGENCY EXIT LIGHT INOP. RELAMPED, CHECKS OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,765 hrs · 3,192 cycles

ON L/O FOUND 2L DOOR EXT EMERGENCY LIGHT INOP. RELAMPED, CHECKS OK.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,196 hrs · 3,086 cycles

THREE EACH EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED, ALL CHECK OK.

Part: IDG — FAILED (NR 2 ENGINE) · airframe 18,636 hrs · 2,981 cycles

ON CLIMBOUT, RT GEN OFF LOST RT AC BUSS. BUSS RESET. RT GEN WOULD NOT RESET. FELT VIBRATION AT 310 KTS. FOUND -C- PHASE OPEN ON IDG. REPLACED IDG. OPS CK OK ON RUN-UP. REF VIBRATION, VISUAL INSP OF EXTERIOR OF A/C NO DEFECTS NOTED. PERFORMED FLT CONTROL CHECK AND CHECK OF FLT CONTROLS OK.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 16,917 hrs · 2,678 cycles

WHILE IN CRUISE C/B RIGHT DC BUS AND RAM AIR TURBINE POWER C/B BOTH POPPED, ALL EMERGENCY EXIT LIGHTS IN CABIN ILLUMINATED. ALSO RIGHT REC FAN AFT CABIN TEMP EICAS MSG AFT EQUIP COOLING EXHAUST FAN 1 AND FWD EQUIP EXHAUST FAN MSG. RESET C/B C/W RAT MANUAL EXT. NO DEFECTS NOTED. RAN FANS AND PACKS BOTH C/B STAYED IN. INSPECTED WIRING BEHIND P6 AND P11 PANELS, NO CHAFING OR DAMAGE NOTED.

Part: ODOR — DETECTED (CABIN) · airframe 13,951 hrs · 2,152 cycles

BURNING SMELL IN AFT GALLEY OVERHEAD JUMPSEATS. INSPECTED AFT GALLEY AREA. OVENS COFFEEMAKERS AND EQUIP NORMAL. INSPECTED IN OVERHEAD AREA. ALL LIGHTING AND EQUIP NORMAL. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (SEAT 24) · airframe 8,831 hrs · 1,347 cycles

LEFT SIDE EMERGENCY LIGHTS INOP FROM ROWS 21 TO 31 A/B. FOUND WIRES BROKEN AT SEAT 28 A/B. REPAIRED WIRING. REPLACED BATTERY AND CHARGER AT SEAT 24 A/B. FWD TO MCO AND PLACARD PER MEL 33-51-03.

Part: UNKNOWN — ODOR (CABIN) · airframe 8,465 hrs · 1,291 cycles

A FEW F/A AND PAX NOTICED AN ODOR SIMILAR TO ELECTRICAL /OZONE FOR A FEW MINUTES IN AREA OF ROW 33 F/O SIDE. INSPECTED AREA AROUND ROW 33 F/O SIDE FOR ANY EVIDENCE OF DAMAGE OR CHAFING OF ELECTRICAL HARNESS. CHECKED ELECTRONIC EQUIPMENT, OVERHEAD PSU''S AND LIGHTING. NO TROUBLE FOUND.

Part: FAN — FAILED (CABIN) · airframe 6,926 hrs · 1,045 cycles

STRONG ELECTRICAL ODOR IN COCKPIT. SMOKE AND SMELL APPEARED IN MID COACH CABIN. INITIATED SMOKE CHECKLIST AND SMOKE AND SMELL DISSIPATED VERY QUICKLY WITH UTILITY BUSES SECURED. TURNED ENT. SYSTEM OFF AND PULLED T-8 T-9 AND T34 C/B''S. FOUND LT RECIRC FAN AT FAULT. REPLACED FAN PER M/M 21-25- 01-4. OPS AND LEAK CHECK OK. NO ACRID ODOR NOTED. ETOPS CATEGORY ''F'': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: DISPLAY — FAILED (EICAS)

AT THE BEGINNING OF TAKE-OFF ROLL, BOTH EICAS SCREENS BLINKED THEN WENT BLANK. T/O POWER WAS APPLIED AT 50 AT TIME OF SCREEN GOING BLANK. BOTH SCREENS WERE BLANK FOR 2-3 SECONDS. FOUND LT EICAS COMPUTER AT FAULT. REMOVED AND REPLACED SAME PER M/M AND INSTALLED SOFTWARE. LT/RT EICAS GROUND SYSTEMS CHECKS NORMAL.

Part: LIGHT — INOP (CABIN)

FIRST SECTION OF COACH RT SIDE EMERGENCY TRACK LIGHTS INOP. FOUND WIRE SHORTED AT ROW 30. REPAIRED WIRE, OPS NORMAL.

Part: AIR DIST — ODOR (CABIN)

SMELL LIKE BURNED PAPER AFTER OPENING AND CLOSING L1 DOOR SEEMS TO BE COMING FROM ABOVE DOOR. INSPECTED ALL ZONES AROUND L1 DOOR WITH ALL LIGHTS AND ROCKWELL SYSTEM ON. NO ODORS, NEITHER EVIDENCE OF HEAT DETECTED. AIRCRAFT OK FOR SERVICE.

Part: LIGHT — INOP (ROW 32FG)

SEAT MOUNTED PROXIMITY LIGHTING SYSTEM INOP AT 32 FG. RELAMPED SAME AND REPLACED LUMINATOR SOCKET ASSY (2), NO HELP. FWD TO MCO / PLACARD PER MEL 33-51-03B.

Part: SLIDE — DETACHED (R2 DOOR)

R2 DOOR SLIDE PARTIAL DEPLOYMENT. REATTACHED SLIDE, SYSTEM CHECKS NORMAL.