N1604R

Part: LIGHT — INOPERATIVE (INDICATOR) · airframe 114,931 hrs · 16,556 cycles

ON FA PANEL ONE LEFT ARMED LIGHT INOPERATIVE. LEFT ARMED LIGHT REPLACED IAW AMM 33-16. (8134008)

Part: LENS — LOOSE (ZONE 200) · airframe 113,695 hrs · 16,351 cycles

33F EMERGENCY LIGHT LOOSE. SECURED LOOSE LENS. CKS GOOD. OK FOR SVC IAW B767-300 AMM 33-51- 10 (7547618)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 113,695 hrs · 16,351 cycles

SEAT 42B WHITE EMERGENCY LIGHT INOP. REPLACED BUMPER AND LIGHT ASSY. (7547622)

Part: SIGN — FAULTED (ZONE 200) · airframe 113,478 hrs · 16,318 cycles

EMERGENCY EXIT SIGN IN FLIGHT DECK OBSRV ENTRY DOOR STAYS ON IN ARMED POSITION. ROBBED EMERGENCY EXIT SIGN ASSY FROM A/C 1817. REPLACED SIGN REF B767 AMM 33-57. OK FOR SVC (7547054)

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 113,174 hrs · 16,264 cycles

SHIP 1604 DURING SERVICE CHECK FOUND SECTION OF PATHWAY EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R EMERGENCY LIGHT POWER SUPPLY PER B767 AMM 33-51. OPS CHECK NORMAL. OK FOR SERVICE. (7071701)

Part: WIRE — DAMAGED (SLAT SYS) · airframe 112,575 hrs · 16,182 cycles

SHIP 1604 -DE/MISC- DUE TO LE ASYM INDICATION IN FLIGHT. CORRECTIVE ACTION: REPLACED SWITCH S286 AND REPAIRED WIRE ON CONNECTER D4434J. ALL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 112,449 hrs · 16,166 cycles

SHIP 1604 EMERGENCY EXIT PATH LIGHTS INOP - ROWS 44FG-54FG. CONNECTIVE ACTION: R/R EMERGENCY LIGHTS PWR SUPPLY M9010 PER B767-300ER AMM 33-51. CHECKS OK. (7553882)

Part: PSEU — FAULTED (SLAT SYS) · airframe 112,575 hrs · 16,182 cycles

SHIP 1604 -MISC/DE- CREW ELECTED DE DURING APPROACH INTO NAP DUE TO INTERMITTENT LE ASSYM INDICATION IN FLIGHT. CORRECTIVE ACTION: R/R PSEU AND S284 FOR HIGH INDUCTANCE.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 111,317 hrs · 15,959 cycles

SHIP 1604 DURING SVC FOUND SEAT 56 G/F EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED PROXIMITY LIGHT BULB, NO HELP, FURTHER DOWN, FOUND QUICK DISCONNECT LINE FOR LIGHT DISCONNECTED, CONNECTED BACK AND OPS CHK EMERGENCY LIGHT PER B767 AMM 33-51 OPS CHK GOOD . (6631340)

Part: SIGN — DETACHED (ZONE 200) · airframe 109,533 hrs · 15,672 cycles

SHIP 1604 EMERGENCY EXIT SIGN IS DETACHED ON THE FLIGHT DECK. CORRECTIVE ACTION: EXIT SIGN REFITTED AND OPS OK. (5261892)

Part: INDICATOR — NOT REPORTED (R2 DOOR) · airframe 107,197 hrs · 15,334 cycles

SHIP 1604 R2 DOOR ARMED INDICATORS. INSTALLED SLIDE WARNING LIGHT PER B767-300 AMM 52-73. OPS CKS GOOD. MEL & PLACARD REMOVED. (0240796)

Part: LIGHT — UNKNOWN (CABIN) · airframe 107,012 hrs · 15,295 cycles

SHIP 1604 FLT ATTENDAT REPORT EMERGENCY EXIT ROW LIGHTS NOT WORKING ON LANDING. CORRECTIVE ACTION: PERFORMED EMERGENCY LIGHTS CK PER B767-300 AMM 33-51, AND NO TROUBLE FOUND. A/C OK FOR SVC. (5551188)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 106,979 hrs · 15,287 cycles

SHIP 1604 FOUND EXIT SIGN'S TRANSPARENT LENS MISSING AT DOOR 2R AND 2L. CORRECTIVE ACTION: INSTALLED 2L EMERGENCY EXIT SIGNS LENS AS PER B767-300 AMM 33-51 -01 (0192297)

Part: DOUBLER — DAMAGED (BS 434-456) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 FWD CARGO COMPARTMENT FOUND 01EA FUSELAGE REPAIRED DOUBLE FASTENER IN POOR CONDITION AT STA434 TO STA456. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 615309-14 (0187820)

Part: SEAT TRACK — CORRODED (BS 1420 RBL 88.5) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 CABIN SEAT TRACKS FOUND UPPER SURFACE MINOR CORROSION AT STA1208 TO STA1428 RBL88.5. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI615136-14 (0187447)

Part: FITTING — CRACKED (BS 927) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 CABIN WING CENTER SECTION AREA FOUND FRAME END FITTING CRACKED AT STA927 LH. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER PRI 615135-14 REV 0 (0187696)

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 R/H WING I/B AFT FLAP FOUND DENT 9.5INCH FROM T/E 23INCH FROM I/B. DAMAGED AREA REPAIRED PER PER B767-300 SRM 57 -53-01-2R-1 & 51-70-10-2R-4 & SRM 51-70-10 (0187471)

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 CABIN RH AFT LAVATORY FLOOR BEAM FOUND CORROSION AT STA 1480, RBL 70.5 TO RBL 75. CORRECTIVE ACTION: CORROSION REPAIRED AS PER B767-300 SRM53-00-51-2R-5 FIG201 REV124.00-JAN-08-2024 AND PRI615168-14 REV.0. (0183581)

Part: FLOORBEAM — PUNCTURED (BS 1307) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 AFT CARGO COMPARTMENT FOUND CABIN FLOOR BEAM WEB PUNCHED AT STA 1307; LBL17. CORRECTIVE ACTION: REPAIRED THE CABIN FLOOR STRUCTURE PUNCHED FLOOR BEAM WEB AT STA 1307; LBL 17 AS PER PRI 615112-14 REV 0 (0183155)

Part: DOOR SILL — CORRODED (BS 588-610) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL FOUND 01EA OUTER CHORD CORROSION AT STA588 TO STA610, RH, OB. CORRECTIVE ACTION: CORROSION REPAIRED AS PER PRI 615203-14 REV 0. (0183593)

Part: SHEAR TIE — CORRODED (BS 742 S35-36R) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA742, BETWEEN S-36R AND S-35R, CORRECTIVE ACTION: R/R THE NEW SHEAR TIE AS PER B767-300 SRM 51-40-02 (0178329)

Part: WINDOW — ARCED (COCKPIT L1) · airframe 107,022 hrs · 15,298 cycles

SHIP 1604 COCKPIT LH NO.1 WINDOWS FOUND ARCING. CORRECTIVE ACTION: REMOVED AND REPLACED COCKPIT LH NO.1 WINDOW AS PER B767-300ER AMM 56-11-01 (0178657)

Part: SEAT TRACK — CORRODED (BS 1417-1480) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 CABIN SEAT TRACKS FOUND UPPER SURFACE MINOR CORROSION AT STA1417 TO STA1480, RBL88.5. CORRECTIVE ACTION: R/R THE NEW SEAT TRACK AS PER B767-300 SRM 51-40-02 (0176814)

Part: SHEAR TIE — CORRODED (BS 742 S38-39R) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA742, BETWEEN S-39R AND S-38R, CORRECTIVE ACTION: R/R THE NEW SHEAR TIE AS PER B767-300 SRM 51-40-02 (0173793)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39L) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 AFT CARGO STRINGER SHEAR TIE FOUND CORROSION AT STA 1197+66, S-38 TO S-39L. CORRECTIVE ACTION: R/R THE NEW SHEAR TIE AS PER B767-300 SRM 51-40-02 (0173827)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38L) · corrosion level 2 · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 AFT CARGO STRINGER SHEAR TIE FOUND CORROSION AT STA 1197+110, S-37L TO S-38L. CORRECTIVE ACTION: R/R THE NEW SHEAR TIE AS PER B767-300 SRM 51-40-02 (0173803)

Part: END PLUG — CRACKED (BS 927 FRAME) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 CABIN WING CENTER SECTION AREA FOUND FRAME END FITTING CRACKED AT STA927 RH. CORRECTIVE ACTION: CRACKED FRAME END FITTING AT STA927 RH, THE CRACK LENGTH IS 1.8" , REMOVED AND REPLACED THE CRACKED FRAME END FITTING AS PER B767 -300 SRM51-40-02 (0172409)

Part: END PLUG — CRACKED (BS 927 FRAME) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 CABIN WING CENTER SECTION AREA FOUND FRAME END FITTING CRACKED AT STA852 RH. CORRECTIVE ACTION: CRACKED FRAME END FITTING AT STA927 RH, THE CRACK LENGTH IS 1.8" , REMOVED AND REPLACED THE CRACKED FRAME END FITTING AS PER B767 -300 SRM51-40-02. (0172371)

Part: END PLUG — CRACKED (BS 852 FRAME) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 CABIN WING CENTER SECTION AREA FOUND FRAME END FITTING CRACKED AT STA852 LH. CORRECTIVE ACTION: CRACKED FRAME END FITTING AT STA852 LH, THE CRACK LENGTH IS 1.9" , REMOVED AND REPLACED THE CRACKED FRAME END FITTING AS PER B767 -300 SRM51-40-02. (0172387)

Part: SKIN — DENTED (LT ELEVATOR) · airframe 106,961 hrs · 15,283 cycles

SHIP 1604 LH I/B ELEVATOR UPPER SURFACE FOUND 1EA DENT. CORRECTIVE ACTION: LH I/B ELEVATOR UPPER SURFACE REPAIRED AS PER B767-300 SRM 55-20 -01 (0161471)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 106,634 hrs · 15,218 cycles

-RVSM- SHIP 1604 EICAS DISAGREE AT FL360, INDICATED ALT CA 357, FO 360 STBY 264. PERFORMED QRH 10.4. CORRECTIVE ACTION: REPLACED CAP AOA PROBE AND PITOT PROBE, OPS NORMAL. (5004366)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 104,653 hrs · 14,922 cycles

SHIP 1604 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: COULD NOT DUPLICATE FAULT. REF B767-300 AMM 52-73 (2839299)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 103,596 hrs · 14,766 cycles

SHIP 1604 EXIT LIGHT IDENTIFIER INOP IN CREW REST. CORRECTIVE ACTION: REPLACED EXIT LIGHT ASSY'. CKS GOOD PER B767 IPC 33-51. MEL/PLAC REMOVED (4822017)

Part: NONE — NONE · airframe 103,189 hrs · 14,701 cycles

SHIP 1604 SMALL RUNNING MAN EMERGENCY EXIT SIGN INOP IN CREW REST. CORRECITVE ACTION: R/R SMALL RUNNING MAN EMERGENCY EXIT CREW REST SIGN. OPS CKS NORMAL. PLACARD REMOVED (9915322)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,754 hrs · 14,639 cycles

SHIP 1604 AT CREW REST. SMALL EXIT SIGN INOP. CORRECTIVE ACTION: R/R EXIT SIGN LIGHT. REF B767 AMM 33-51. (9933831)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 102,655 hrs · 14,619 cycles

COCKPIT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REPLACED BATTERIES IAW MM 33-51. OPS NORMAL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,655 hrs · 14,619 cycles

CREW REST SMALL RUNNING MAN EMERGENCY EXIT SIGN INOP. REPLACED EMERGENCY EXIT SIGN PER B767 MM 33-51. OPS NML.

Part: NONE — NONE · airframe 101,392 hrs · 14,414 cycles

SHIP 1604 LT & RT OVERWING SLIDE LIGHT ON P61 NOT COME ON DURING SQUIB TEST, CORRECTIVE ACTION: RE-CONNECT THE ELECTRICAL CONNECTOR AT THE RT OVERWING BATTERY PACK. OPS CHECK GOOD PER B767 AMDS 2565-7492-01 RII C/W. (9678717)

Part: NONE — NONE · airframe 101,250 hrs · 14,396 cycles

SHIP 1604 - MISC/DE - DUE TO LE DISAGREE MSG. CORRECTIVE ACTION: CHECKED RIGGING OF THE INBOARD SLAT PDU. CHECKED WIRING. VERIFIED RVDT RIGGING. CYCLED SLATS AND FLAPS MULTIPLE TIMES. ON FOLLOW UP LOG REPLACED INBD SLAT PDU AND CHECKED ALL TORQUE TUBE CONNECTIONS. (9034152)

Part: EEC — FAILED · airframe 100,096 hrs · 14,198 cycles

SHIP 1604 - ATO - ABORTED TAKE OFF AT 75 KNOTS DUE TO RIGHT ENGINE UNABLE TO MAKE TAKEOFF POWER. TARGET N1 108.1 MAX OBTAINED 96.5. CORRECTIVE ACTION: EEC UNIT FAIL FADEC FAULT 354-18B. REPLACED EEC AND HMU PER B767 AMM 73-21. OPS CHECK NORMAL. (9282962)

Part: NONE — NONE · corrosion level 2 · airframe 99,544 hrs · 14,088 cycles

SHIP 1604 RH WING CENTER SECTION REAR SPAR WEB NEAR REAR SPAR BULKHEAD FITTING (PICKLE FORK) LH UPPER CORNER SUSPECT CORROSION, CORRECTIVE ACTION: THE CORROSION AREA REPAIRED AS PER PRI 597729-14 (2185418)

Part: NONE — NONE · corrosion level 2 · airframe 99,544 hrs · 14,088 cycles

SHIP 1604 FOUND CORROSION ON CABIN SRAT TRACK AT STA917 RBL88.5, CORRECTIVE ACTION: REPAIR PARTS MADE FROM BAC1520-2193(DA) AND NEW SPLICE AT STA 843 MADE FROM BAC1505-100322 AND 7075T6-0.100" CLAD SHEET AS PER B767-300 SRM53-00 (2176258)

Part: NONE — NONE · airframe 99,544 hrs · 14,088 cycles

SHIP 1604 INTERNAL SECTION 48 FWD DEGE OF HORT STAB 313CLX CUTOUT BETWEEN STA1725-STA1746 FOUND SKIN WORN. CORRECTIVE ACTION: THE DAMAGED SKIN REMOVED AND REPLACED AS PER B767-300 SRM 53-80 (2176273)

Part: NONE — NONE · airframe 99,544 hrs · 14,088 cycles

SHIP 1604 INTERNAL SECTION 48 FWD DEGE OF HORT STAB 314CRX CUTOUT BETWEEN STA1725-STA1746 FOUND SKIN WORN, CORRECTIVE ACTION: THE DAMAGED SKIN REMOVED AND REPLACED AS PER B767-300 SRM 53-80 (2176267)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 99,544 hrs · 14,088 cycles

SHIP 1604 RIGHT SIDE VERT STAB SKIN BETWEEN FSS 92.25 AND FSS 145.12 FOUND DELAMINATION. CORRECTIVE ACTION: RIGHT SIDE VERT STAB INNER SKIN REPAIRED BETWEEN FSS 92.25 AND FSS 145.12 AS PER B767-300 SRM 51-70 & SRM 51-70 (2173732)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE HAS BENT SHEAR TIE AT BS 1480 BETWEEN STRINGERS 37L AND 38L, CORRECITVE ACTION: REMOVED FABRICATED NEW AND INSTALLED SHEAR TIE @ STA 1480 BTWN STR 37L AND 38L IAW B767 SRM 51-40-02 AND DWG# 146T1219 REV C (2053475)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 PERMANENT REPAIR DUE PER ERA 595699-14 REV A. CORRECITVE ACTION: REMOVED TEMPORARY REPAIR FROM LOWER FUSE SKIN STA 1417-1502 STR37R TO STR37L AND APPLIED NEW REPAIR IAW ERA#59579614AD REVA (7636169)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE HAS BENT SHEAR TIE AT BS 1502 BETWEEN STRINGERS 38R AND 39R. CORRECITVE ACTION: BULK CARGO BILGE HAS BENT SHEAR TIE AT BS 1502 BETWEEN STRINGERS 38R AND 39R (2053463)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE HAS BENT SHEAR TIE AT BS 1480 BETWEEN STRINGERS 37R AND 38R, CORRECITVE ACTION: REMOVED AND REPLACED SHEAR TIE @ STA 1480 BTWN STR 37R AND 38R IAW B767 SRM 51-40-02 AND DWG# 146T1219 REV C (2053468)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE HAS BENT SHEAR TIE AT BS 1461 BETWEEN STRINGERS 37R AND 3RL , CORRECITVE ACTION: REMOVED , FABRICATED NEW AND INSTALLED SHEAR TIE @ STA 1461 BTWN 37R - 38R IAW B767 SRM 51-40-02 AND DWG # 146T1218 REV B . (2053456)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 AMOC MONITOR INSPECTION LOG REF ERA 595796-14AD REV.B PENDING AMOC APPROVAL TO AD 2014-14-04 PRIOR TO 50,000 TOTAL FLIGHT CYCLES. CORRECITVE ACTION: DISCONTINUE REVENUE SERVICE ON OR BEFORE 50,000 TOTAL FLIGHT CYCLES PENDING AMOC APPROVAL TO AD 2014-14-04 ASSOCIATED ER/A 13-595796 (2053320)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 DTA MONITOR INSPECTION LOG REF ERA 595796-14 REV. B PENDING DTE APPROVAL DUE PRIOR TO 15 DEC 2022. CORRECITVE ACTION: DISCONTINUE REVENUE SERVICE ON OR BEFORE 15 DEC 2022 PENDING DTE APPROVAL FROM ENABLING TECHNOLOGIES ASSOCIATED ER/A 13-595796 (2053317)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE HAS BENT SHEAR TIE AT BS 1439 BETWEEN STRINGERS 38R AND 39R, CORRECITVE ACTION: REMOVED AND REPLACED SHEAR TIE @ STA 1439 BTWN STR 38R AND 39R IAW B767 SRM 51-40-02 AND DWG# 146T1219 REV C (2053471)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 REMOVE TEMPORARY REPAIRS AS REQ, CORRECITVE ACTION: REMOVED TEMPORARY REPAIR FROM LOWER FUSE SKIN STA 1417 TO 1502 STR 37R TO 37L AND APPLIED NEW REPAIR IAW ERA 595796-14AD REV A AND REV B. (2053421)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE HAS TEMPORARY SHEAR TIE INSTALLED AT BS 1502 BETWEEN STRINGERS 38L AND 39L. CORRECITVE ACTION: REMOVED TEMPORARY SHEAR TIE FROM STA 1502 BETWEEN 38L TO 39L FABRICATED NEW AND INSTALLED SHEAR TIE IAW B767 SRM 51-40-02 AND DWG # 146T1220 REV B. (2053452)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE STRINGER 39L IS BULKLED AT BS1439. CORRECITVE ACTION: REPAIRED BULK CARGO STRINGER IAW B767 SRM 53-00- 03 REPAIR 2 ,SRM 51-40-05 , SRM 51- 20-01 (2049744)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE STRINGER 39R IS BUCKLED AT BS 1502. CORRECITVE ACTION: REPAIRED BULK CARGO STRINGER 39R AT STA 1502 IAW B767 SRM 53-00- 03 REPAIR 2 , SRM 51-40-05 , SRM 51-20-01 (2049755)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 BULK CARGO BILGE STRINGER 39L IS BUCKLED AT BS 1502. CORRECITVE ACTION: REPAIRED BULK CARGO STRINGER IAW B767 SRM 53-00- 03 REPAIR 2 ,SRM 51-40-05 , SRM 51-20-01. (2049752)

Part: NONE — NONE · airframe 98,979 hrs · 13,957 cycles

SHIP 1604 ULK CARGO BILGE STRINGER 39R IS BUCKLED AT BS 1439. CORRECITVE ACTION: REPAIRED BULK CARGO STRINGER IAW B767 SRM 53-00- 03 REPAIR 2 ,SRM 51-40-05 , SRM 51- 20-01 (2049733)

Part: NONE — NONE · airframe 98,845 hrs · 13,928 cycles

SHIP 1604 WHILE WORKING J/C # 3300-4220, FOUND EMERGENCY BATT. CHARGER ON M737 CORRECTIIVE ACTION: R/R EMERGENCY BATT CHARGER @988LT ITEM M737 AS PER B767-300 AMM 33-51. OPS CHK NML.(8325982)

Part: NONE — NONE · airframe 98,825 hrs · 13,924 cycles

SHIP 1604 ON MEET AND GREET FOUND 0.40 INCH HOLE ON LT WING LOWER PANEL 511FB, CORRECTIVE ACTION: HOLE IS 0.40 INCHES IN DIAMETER . FWD TO MON PER B767-300 SRM 57 -20*-01-1A PROCEDURE 1. FIGURE 101 SHEET 3 H & J. INSPECT EVERY A CK AND REPAIR NO LATER THAN 1200 FLT CYCLES. (8325972)

Part: CHARGER — FAULTED (EMERGENCY LIGHT) · airframe 97,886 hrs · 13,715 cycles

SHIP 1604 EMERGENCY ESCAPE LIGHTS AT SEATS 21-31AB ARE INOPERATIVE. CORRECTIVE ACTION: FOUND FUSE BATTERY CHARGER. CHARGER REPLACED. SYSTEM OPERATION IS NORMAL. (LP 7324744)

Part: HMU — POWER LOSS (LEFT ENGINE) · airframe 95,838 hrs · 13,208 cycles

ETOPS EVENT SLC-JFK. PERFORMED A REJECTED TAKE OFF AT 100 KTS DUE TO LEFT ENGINE LACK OF ACCELERATION. ENGINE WOULD NOT GO HIGHER THAN 87%. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FUEL FILTER AND INSTALLED HMU. SYSTEM OPERATION IS NORMAL.

Part: RELAY — MALFUNCTIONED (ENGINE STARTER) · airframe 95,587 hrs · 13,136 cycles

ATO, AT THROTTLE UP DUE TO A RIGHT STARTER CUT OUT EICAS MESSAGE. CORRECTIVE ACTION: PERFORMED IDLE RUN AT 52% N2 THE FAULT RETURNED. REPLACED K666 RELAY AND NR 2 ENGINE SPEED CARD, CLEANED RELATED CONNECTORS AND RAN ENGINE AT POWER WITH NO FAULTS.

Part: LIGHT — INOPERATIVE (DOOR SLIDE) · airframe 95,410 hrs · 13,096 cycles

AFT LEFT DOOR SLIDE LIGHT INOPERATIVE. INSTALLED NEW SLIDE LIGHT ASSEMBLY. MCO/PLAC REMOVED. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,748 hrs · 12,983 cycles

EMERGENCY FLOOR PATH LIGHT FOUND 2, 3, 4B ARE INOPERATIVE. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,639 hrs · 12,964 cycles

DURING SERVICE FOUND SEATS 2B, 3B AND 4B EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY M90018. SYSTEM OPERATION IS NORMAL.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 94,068 hrs · 12,884 cycles

FOUND EMERGENCY LIGHTS AT ROW 21-31 FG INOPERATIVE. FOUND SHORT IN SEAT AND BLOWN FUSE ON CHARGER AND REPAIRED. SYSTEM OPERATION IS NORMAL.

Part: HOLDER — UNKNOWN (BATTERY PACK) · airframe 93,732 hrs · 12,835 cycles

EMERGENCY LIGHTS AT SEATS 1-3A ARE INOPERATIVE. REPLACED EMERGENCY BATTERY HOLDER. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — LOOSE (SEAT 35B) · airframe 91,784 hrs · 12,595 cycles

EMERGECNY SEAT 35B AISLE LIGHT LOOSE. FOUND LIGHT INSTALLED WITH TAPE. RE-INSTALLED AISLE LIGHT. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 91,698 hrs · 12,584 cycles

EMERGENCY LIGHTS INOP IN AFT GALLEY AREA. REPLACED BATTERY PACK UNDER RIGHT AFT FLIGHT ATTENDANT SEAT. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,612 hrs · 12,574 cycles

BOTH AFT SERVICE DOOR UPPER EXIT LIGHTS ARE INOPERATIVE. FOUND DEAD BATTERY PACK, REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 90,279 hrs · 12,393 cycles

EMERGENCY EXIT LIGHTS AT DOOR R2 AND L2 ARE INOPERATIVE. REPLACED BATTERY AT M121 R2 JUMP SEAT. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 90,028 hrs · 12,358 cycles

AFT EMERGENCY BATTERY CHARGER BAD. LEFT AND RIGHT EXIT/THRESHOLD LIGHT IS INOPERATIVE. FOUND POWER SUPPLY CHARGER M1210 PARTIALLY INOPERATIVE, FUSE 9-10 BAD. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL. (LP 5247410)

Part: CIRCUIT BREAKER — FAILED · airframe 87,324 hrs · 12,012 cycles

RETURNED TO DEPARTURE, DUE TO THE FIRST OFFICER MACH AIRSPEED INDICATOR FAILURE. REPLACED THE C581 CIRCUIT BREAKER, RIGHT ADC AND RIGHT MASI. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,513 hrs · 11,906 cycles

DURING ETOPS SERVICE CHECK FOUND ALL EMERGENCY LIGHTS IN LLCR INOPERATIVE. ALL LIGHTS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: COUPLER — FAILED (HF COMMS) · airframe 85,609 hrs · 11,780 cycles

RIGHT HF DOES NOT TRANSMIT, BUT DOES RECEIVE CELL CALLS. BURNING ODOR WHEN KEYING THE MICROPHONE. COULD NOT DUPLICATE ODOR. REPLACED THE RIGHT HF COUPLER.

Part: SKIN — DELAMINATED (LT AILERON) · airframe 85,491 hrs · 11,763 cycles

LEFT WING INBD AILERON LOWER SURFACE INBD AFT AREA, FOUND DELAMINATED. REPAIRED IAW SRM 57-60-01.

Part: SKIN — PUNCTURED (LT WING TE FLAP) · airframe 85,471 hrs · 11,758 cycles

LEFT WING INBD AFT T/E FLAP UPPER SURFACE INBD AREA FOUND PUNCTURED. REPAIRED IAW SRM 57-53-01.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 85,471 hrs · 11,758 cycles

NR 2 ENGINE NACELLE STRUT ACCESS PANEL 442AL, CUTOUT FOUND CRACKED. REPAIRED IAW ERA 564319-14.

Part: FRAME — CHAFED (NR 2 NACELLE) · airframe 85,471 hrs · 11,758 cycles

NR 2 ENG O/B CORE COWL FRAME AS NAC STA 293.74 FOUND CHAFING. REPAIRED COWL AS PER ERA 564415-14 A REPAIR ANGLE DOUBLER REPAIR -2 AND -3 REPAIR FILLERS MADE AND INSTALL AT NR 2 ENG O/B CORE COWL FRAME.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 85,471 hrs · 11,758 cycles

LT CABIN SEAT TRACK AT LBL 11, STA 836-857 FOUND CORROSION AND OUT LIMITS REPLACED PER SRM 51-40-02.

Part: FRAME — CRACKED (BS 903) · airframe 85,471 hrs · 11,758 cycles

INSPECTION FOUND ONE CRACK ON THE RT BS 903.5 FRAME INNER SURFACE AND TRANSITION RADIUS. REPAIRED THE FRAME.

Part: TEE FITTING — CORRODED · corrosion level 2 · airframe 85,471 hrs · 11,758 cycles

INSPECTION FOUND CORROSION ON THE TEE FITTING AROUND ONE HOLE FOR THE THREE FASTERENS CONNECTING THE TEE FITTING TO THE FAILSAFE STRAP. REPLACED THE TEE FITTING.

Part: SEAT TRACK — CORRODED (BS 1428-1443) · corrosion level 2 · airframe 85,471 hrs · 11,758 cycles

LEFT CABIN SEAT TRACK AT LBL 88, BS 1428 - 1443 FOUND CORRODED OUT OF LIMITS. REPAIRED IAW ERA 564248.

Part: SEAT TRACK — CORRODED (BS 1197-1208) · airframe 85,471 hrs · 11,758 cycles

CORROSION LEVEL: 2 SEAT TRACK-RH CABIN SEAT TRACK AT RBL 88 STA 1197-1208 FOUND WITH CORROSION OUT OF LIMITS REPAIRED PER SRM 53-00-52

Part: SEAT TRACK — CORRODED (BS 1098-1197) · airframe 85,471 hrs · 11,758 cycles

CORROSION LEVEL: 2 RH CABIN SEAT TRACK AT RBL 88 STA 1098-1197 FOUND WITH CORROSION OUT OF LIMITS AND REPAIRED PER SRM 53-00-52

Part: SEAT TRACK — CORRODED (BS 933-1098) · airframe 85,471 hrs · 11,758 cycles

CORROSION LEVEL: 2 SEAT TRACK -RH CABIN SEAT TRACK AT RBL 88 STA 933-1098 FOUND WITH CORROSION OUT OF LIMITS REPAIRED PER SRM 53-00-52

Part: LIGHT — DETACHED (CABIN) · airframe 84,387 hrs · 11,622 cycles

EVACUATION LIGHT HANGING LOOSE AT LOCATION 41B. SECURED THE LIGHT, OK FOR SERVICE.

Part: MONITOR — ODOR (SEAT 17C) · airframe 80,273 hrs · 11,116 cycles

BURNING ODOR AT SEAT 17C. MONITOR DISCONNECTED AND THE SEAT 17D ENTERTAINMENT SYSTEM. RESTARTED AND ALL MONITORS AND ELECTRICAL ITEMS IN VICINITY CHECK WITH NO FURTHER FAULTS/ELECTRICAL ODOR PRESENT. RECONNECTED MONITOR AT SEAT 17CD. SYSTEM OPERATION IS NORMAL.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 80,067 hrs · 11,088 cycles

EMERGENCY LIGHT ASSEMBLY FORWARD RIGHT DOOR DAMAGED AND LENS WILL NOT STAY ATTACHED. MAINTENANCE REPLACED LIGHT ASSEMBLY. SYSTEM OPS NORMAL.

Part: SKIN — CRACKED (WING) · airframe 71,811 hrs · 10,092 cycles

CRACKING FOUND IN STEP 2C, FASTENER 1. REPAIRED IAW AMDS 5724-01010-04B.

Part: SKIN — CRACKED (WING) · airframe 71,811 hrs · 10,092 cycles

CRACKING FOUND IN STEP 2C AT FASTENER 1, 2 AND 5. REPAIRED IAW AMDS 5724-01010-03B.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,016 hrs · 9,245 cycles

LARGE EXIT LIGHTS AT 4R AND 3L ARE INOPERATIVE. REPLACED BATTERY AND POWER CHARGER IAW 300 AMM 33-51.

Part: SEAT TRACK — INOPERATIVE (BS 654) · airframe 62,581 hrs · 8,914 cycles

CABIN SEAT TRACK AT FS 654 + 110 UPPER FLANGE WAS REPLACED IAW SRM 53-00-51, FIG 201.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,755 hrs · 8,796 cycles

EMERGENCY EXIT PATH LIGHTS INOPERATIVE FROM ROW 6 TO ROW 20 LH. REPLACED BATTERY PACK IAW AMM 33-51-07. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (SEATS 32AB) · airframe 61,621 hrs · 8,778 cycles

EMERGENCY PATH LIGHTS AT SEAT 32AB INOPERATIVE. MX REPLACED THE LIGHT ASSY. SYSTEM OPS NORMAL.

Part: SOCKET — BROKEN (CABIN) · airframe 59,008 hrs · 8,445 cycles

DURING DRC FOUND EMERGENCY LIGHTS AT ROW 36-40 GF INOPERATIVE. MMTC REPLACED THE BATTERY PACK AND FOUND LENS BROKEN AT SEAT 38GF AND REPLACED LIGHT SOCKET ASSY SYSTEM OPERATION IS NORMAL.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 58,451 hrs · 8,362 cycles

NR 3 SLAT WEDGE UPPER SURFACE DELAMINATED AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND 51-70-10 REPAIR FIG 201.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 58,451 hrs · 8,362 cycles

LEFT WING I/B AFT FLAP UPPER SURFACE IS DELAMINATED. REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND 51-70-10 REPAIR 4 FIG 203.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 58,451 hrs · 8,362 cycles

NR 10 SLAT UPPER SKIN IS DELAMINATED. REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND 51-70-10 REPAIR 4 FIG 202.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 58,451 hrs · 8,362 cycles

NR 6 SLAT WEDGE UPPER SURFACE IS DELAMINATED. REPAIRED PER B767-+300 SRM 57-43-02 REPAIR 1 AND 51-70-10 REPAIR 4 FIG 202.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,451 hrs · 8,362 cycles

FS 654+110 MAIN CABIN FLOORBEAM WAS CORRODED AT RBL 55 AND REPAIRED PER B767-300 SRM 53-00-51 REPAIR 1 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,451 hrs · 8,362 cycles

FS 654 +88 CABIN FLOORBEAM UPPER CHORD IS CORRODED AT RBL 50 AND REPAIRED PER B767-300 SRM 53-00-51 REPAIR 1 FIG 201.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,451 hrs · 8,362 cycles

M/D STA 903 STR 20L-STR 21L FRAME INNER CHORD CRACKED. REPAIRED PER ERA 497674-14 REV ORIG.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 57,693 hrs · 8,260 cycles

EMERGENCY LIGHTS AT SEAT 39AB ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR UNPLUGGED AND RECONNECTED. SYSTEM OPERATIONS NORMAL.

Part: LIGHT — SHORTED (CABIN) · airframe 56,555 hrs · 8,111 cycles

DURING DRC MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT SEATS 16FG-20FG AND 32FG-41FG. THE POWER SUPPLY M9010, AT SEAT 39G, WAS REPLACED AND SEVERAL SHORTED BULBS WERE RE-LAMPED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 55,991 hrs · 8,041 cycles

FOUND ON DRC EMERGENCY LIGHT AT SEAT 20 INOPERATIVE. MAINTENANCE FOUND A PLUG DISCONNECTED AT SEAT 18E AND SHORTED TO SEAT ASSEMBLY. THE PLUG WAS RE-SECURED, THE BATTERY PACK AND POWER SUPPLY WERE REPLACED, AND THE SYSTEM OPERATIONAL CHECK WAS NORMAL.

Part: CLAMP — LOOSE (APU AREA) · airframe 54,470 hrs · 7,828 cycles

ON TAXI OUT STRONG SMOKE/ODOR AROUND ROWS 4-6 NOTICED BY CREW AND PASSENGERS AFTER BOTH APU AND ENGINES WERE STARTED. MX INSPECTED APU AREA FOR OIL LEAKS AND FOUND LOSE BOOT CLAMPS AND TIGHTENED. PERFORMED HIGH ENGINE POWER RUN WITH BOTH PACKS NO ODOR NOTED. SYS OPS IS NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 54,011 hrs · 7,765 cycles

EMERGENCY FLOOR LIGHTS AT MID GALLEY ARE INOPERATIVE. MAINTENANCE FOUND A WIRE BROKEN AND SPLICED. SYSTEM OPERATION IS NORMAL. (2010-D1387) (DL76G103223)

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 52,004 hrs · 7,520 cycles

EMERGENCY PATH LIGHT AT SEAT 30F IS INOPERATIVE. MAINTENANCE FOUND HARNESS PLUG DISCONNECTED FROM SIDEWALL AND RECONNECTED HARNESS. SYSTEM OPERATION IS NORMAL.

Part: BLADES — BENT (NR 1 ENGING FAN) · airframe 50,103 hrs · 7,255 cycles

L ENG BIRDSTRIKE ON APPROACH - DEFLECTED OFF OF RADOME. MX IN PROGRESS- 2 FAN BLADES BENT AND OUT OF LIMITS. REPLACED NR 1 ENG FAN BLADE SET IAW MM ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: SHUTOFF VALVE — MALFUNCTIONED (1 ENGINE) · airframe 49,830 hrs · 7,222 cycles

DURING INTITIAL T/O ROLL LT ENG BLEED AND MESSAGE ILLUMINATED FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-02. DISP GRANTED. FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-04 AND LT ENGINE THRUST REVERSER DEACTIVATED IAW MEL 36-11-02 DISP DISP GRANTED. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 49,822 hrs · 7,221 cycles

DURING INITIAL T/O ROLL L ENG BLEED AND MSG ILLUM FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-04 AND LT ENG THRUST REVERSER DEACTIVATED IAW MEL 36-11-02 DISP GRANTED. R & R LT ENG PRV IAW AMM PERFORMED HIGH PWR ENG RUN DUCT PRESS FOR LT ENG LOW. NO MESSAGES NOTED SUSPECT PRSOV--603133. REMOVED PRSOV IAW AMM 36-11-09-002-033-2 INSTALLED PRSOV IAW AMM STILL NEEDS ENG RUN CHECK 493775. PERFORMED POWER ASSURANCE CHECK IAW AMM ALL NML. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: OVEN — FAILED (GALLEY) · airframe 49,527 hrs · 7,180 cycles

NUMBER 1 OVEN HAS STRONG ELECTRICAL SMELL WHEN USED. BREAKER PULLED AND COLLARED FWD TO NEF 253.30. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,378 hrs · 7,159 cycles

OVERHEAD EMERGENCY EXIT LIGHTS INOP FROM ROWS 32AB TO 41AB CORRECTIVE ACTION REMOVED M739 CHARGER AND BATTERY PACK. REPLACED BATTERY PACK AND CHARGER AND 3 EACH ISLE LIGHT OPS CK OK

Part: CONTROL VALVE — MALFUNCTIONED (APU) · airframe 47,386 hrs · 6,910 cycles

APU AUTO SHUTDOWN WITH FAULT LIGHT WHEN 2 PACK WAS TURNED OFF FOR ENG START. HAPPENED TWICE ONLY FAULT FLAG FOR APU THERMOCOUPLE. STARTED APU AND RAN 15 MINS FULLY LOADED. TEMP WAS WITHIN LIMITS. TRIED SHUTTING DOWN PACKS AND GOT AUTO SHUTDOWN REV FLOW. REPLACED SURGE CONTROL VALVE PER AMM. LK CK GOOD RAN ENG. APU OPS NORMAL AND RT/LT PACK OFF WITH NO SURGE.

Part: ECU — FAILED (APU) · airframe 47,105 hrs · 6,874 cycles

DURING ENGINE START AFTER BOTH PACKS TURNED OFF THE APU SHUTDOWN WITH A FAULT LIGHT. ECU MINI FLAGS WERE 12-37-43. FWD APU PNEUMATICS FUNCTION TO MEL 49-11-01C. MCO/PLAC INSTALLED. OPS CHKD APU ON ARRIVAL OPERATES OK DID BITE CHK SHOWS REPLACED ECU. ECU BITE CHKS GOOD PER AMM 49-61-06. MCO PLACARD REMOVED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 46,865 hrs · 6,841 cycles

CABIN ALT CONTROL FAILURE BOTH AUTO 1 AND 2. TROUBLE SHOOT IAW FIM 21-31-00-101. ALL INDICATIONS OK.

Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 45,481 hrs · 6,667 cycles

RTB - R FWD FUEL BOOST PUMP LOW PRESSURE LIGHT ON. FLT CREW PLACARD WAS ISSUED BUT A/C NEEDED FUEL ADDED DUE 120 RTE PER MEL.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 44,271 hrs · 6,524 cycles

RTB - ON TAXI OUT, HAD CABIN ALT AUTO PRESS 1 AND 2 INOP. RESET PRESS CONTROLLERS.

Part: APU — UNSERVICEABLE (APU BAY) · airframe 44,201 hrs · 6,516 cycles

REPLACED APU DUE TO -NO START- HISTORY. LOADED APU INFLT START INTO FLT PLAN S/N INSTALLED P2563.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 41,753 hrs · 6,223 cycles

L1 DOOR SLIDE HAS BACK BOARD CABLE NOT ATTACHED. FOUND SLIDE PACK NOT SECURED ALONG ONE SIDE AND LOOSE ON THE OTHER SIDE. FOUND DUCT TAPE COVERING RETAINING CABLE HOLE AT TOP OF SLIDE. SLIDE REPLACED ON NR 00175 AND DL JIC 7809 SLIDE PART NBR 251004926 (DL) 101651-303 (MFG).

Part: VANE — WORN (NR 1 ENGINE) · airframe 41,453 hrs · 6,189 cycles

NR 1 ENGINE REPLACED DUE TO VSV WEAR.

Part: CPU — FAILED (NR 1 EEC) · airframe 38,222 hrs · 5,796 cycles

RTB - ON TAXI, LT EEC CONTROL MSG, EEC CH A CB POPPED. REMOVED AND REPLACED LT EEC, OPS CK OK.

Part: VALVE — UNSERVICEABLE (RIGHT) · airframe 38,034 hrs · 5,772 cycles

RIGHT PRV MESSAGE ON TAKEOFF ROLL. RIGHT PRV FOUND AT FAULT - R/R SAME. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 37,241 hrs · 5,673 cycles

ENGINE REPLACED DUE TO HOC NR 2. REPLACED NR 2 ENG PER TRANS 1T161.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 36,369 hrs · 5,567 cycles

RT PACK INOP LIGHT ON AND WOULD NOT RESET. PACK BITE PROCEDURE FIM 21-51-00 ACCOMPLISHED. NO FAULTS PAC RESET, OPS CHK NML.

Part: INDICATOR — FAILED (COCKPIT) · airframe 36,208 hrs · 5,548 cycles

RTB DUE ON TAXI F/O ALT FLAG IN VIEW. REPLACED F/O ALT IND.

Part: HMU — MALFUNCTIONED (NR 1 ENGINE) · airframe 35,920 hrs · 5,512 cycles

AFTER LEAVING GATE ON ENGINE START, GOT EICAS MSG LT ENG CONTROL. MTC IN PROGRESS. FOUND LT ENG PIMU MSG 155-23. TRIED RESET NO HELP. REPLACING HMU REPLACED HMU IAW MM LK CK GOOD A/C OK FOR SVC. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: ENGINE — FAILED (APU) · airframe 35,134 hrs · 5,417 cycles

APU TO START ON VERIFICATION FLT AFTER 3 ATTEMPTS FLT RETURNING TO ATL FOR REPAIRS. REPLACED APU PER M/M. RAN APU LK CKS GOOD MADE 4 SUCCESSFUL STAR VOLTS/FREQ CK GOOD. LOADED APU AIR AND ELEC RAN GOOD. OK FOR SVC.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT ENGINE) · airframe 33,364 hrs · 5,194 cycles

LEFT HPSOV EICAS MSG ON. DIVERTED TO LGW. AIR SUPPLY BITE FAULTS HPSOV MCO PER MEL 36-11-02 . REPLACED LT ENG HP VALVE PER MM. UNLOCKED HP VLV AND UNLOCKED T/R ON LEFT ENG. RAN ENG AND VERIFIED HP VLV OPS NML. NO MSGS NOTED. MCO AND PLACARD REMOVED.

Part: FAUCET — STUCK (LAVATORY) · airframe 33,216 hrs · 5,175 cycles

ON TAXI OUT ACFT BEHIND OURS REPORTED FLUID LEAKING FROM LOWER CENTER FUSELAGE AREA BY DRAIN MAST. FOUND SINK FAUCET STUCK OPEN IN FWD MID ECONOMY LAV. FAUCET NOW OPERATING NORMALLY. ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: FSEU — FAILED (TE FLAPS) · airframe 31,189 hrs · 4,908 cycles

ON APPROACH T/E FLAP DISAGREE WHEN FLAPS 25 SELECTED RIGHT SIDE STAYED AT 20 LEFT WENT TO 25. LANDED WITH T/E FLAPS 20. REPLACED FSEU AND POSITION INDICATOR.

Part: WIRE — DAMAGED (CABIN) · airframe 26,807 hrs · 4,314 cycles

SEAT 4G HANDSET INOP. SPARKING AND SMOKE IN AREA. REPLACED UPCU. PN D250708651 SN 1299026427

Part: ACTUATOR — LEAKING (NR 2 SPOILER) · airframe 25,151 hrs · 4,057 cycles

AT CRUISE FLIGHT RECEIVED EIVCAS MSG RT HYD QTY AND RSVR LIGHT ON HYD PANEL. RT HYD QTY WAS .48 AT THIS TIME AND SUBSEQUENTLY DECREASED TO .32. AS PER ATL MCC TURNED OFF THE RT ENG HYD PUMP AND RT HYD ELECT DEMAND PUMP. QUANTITY STABILIZED. REPLACED O-RING ON NR 2 SPOILER FILTER PLUG LEAK CHECK OK.

Part: ENGINE — FAILED (NR 1)

DIVERSION INTO PHX, NR 1 ENGINE COMPRESSOR STALL AT CRUISE. PHX MAINTENANCE FOUND METAL IN TAIL PIPE. REPLACED ENGINE.

Part: LINE — CHAFED (LEFT PYLON) · airframe 20,890 hrs · 3,410 cycles

FLIGHT DIVERTED TO LGW WITH LOSS OF LEFT HYDRAULIC FLUID. FOUND HYD PIPE IN LEFT PYLON CHAFED THROUGH DUE TO PYLON LATCH OPENING IN FLIGHT AND CHAFING ON PIPE. THE LINE IS DETAILED IN IPC 29-11-27-02 ITEM 116 RESERVOIR RETURN LINE FROM HEAT EXCHANGER. TIME LIMITED REPAIR WITH FLEX LINE. ALSO FOUND LEFT EDP LEAKING AT BLEED POINT. EDP REPLACED.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 19,933 hrs · 3,258 cycles

AFT RT LAV HAS ACRID SMELL BUT NO VISABLE SMOKE OR HAZE. INSPECTED TRASH CAN, ALL OK. HOT WATER HEATER PWR SWITCH AND LAV LIGHTS TURNED OFF. REPLACED LIGHT BULBS. SUSPECT BAD BALLAST IN RT AFT LAV. WD TO MCO AND PLAC 38-30-01B. PULLED FUSE IN BALLAST ASSY. TURNED ON WATER HEATER-NO ACRID SMELL NOTED FROM AREA. REPLACED OVERHEAD FOUR LIGHT BALLST. INSPECTED WIRING IN OVERHEAD AREA, NO SMELL OR SIGNS OF ARCING/BURNING NOTED. LEFT LIGHTS AND WATER HEATER ON FOR EXTENDED PERIOD OF TIME, ALL CKS OK. MCO AND PLAC RMVD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 19,478 hrs · 3,192 cycles

ON LAYOVER FOUND RIGHT AFT 3 WING SLIDE EMERGENCY LIGHTS INOP. FOUND ALL 3 BULBS BAD ALONG WITH PWR SUPPLY M733. REPLACED BULBS AND PWR SUPPLY WITH BATTERY PACK.

Part: MODULE — FAULTY (CABIN) · airframe 17,848 hrs · 2,905 cycles

ELECTRICAL ODOR FWD CABIN VICINITY ENT SYSTEM EQUIPMENT. SECURED BOTH UTILITY BUSSES FOR REMAINDER OF FLT. FOUND VCC/VMOD B AD, SHUTDOWN IFE SYS PULLED AND COLLARD VCC C/B 1.2 3.4 5 ON C/B PNL 101 LOWER E/E BAY. NDS VCC P/N 250008689 MFG P/N 1301394-001. PDX FWD TO MCO/PLAC AS PER MEL 25-20-02J.

Part: ENTERTAIN SYS — CONTAMINATED (CABIN) · airframe 17,631 hrs · 2,866 cycles

ELECTRICAL PLASTIC SMELL REPORTED BY FLIGHT ATTENDANT JUST BEHIND COCKPIT DOOR IN VIDEO CLOSET. DEACTIVATE IFE SYSTEM PER MEL 25-25-02J. REMOVED LOADS OF DUST AND DEBRIS FROM BEHIND IFE COMPONENTS. FOUND DUTY FREE BROCHURES AND SEVERAL SEALS FROM TAPE BOX VMOD LOADED WITH DUST AND LINT. REMOVED ALL. SYSTEM OPS NORMAL AND HAD NO ODORS FROM AREA. MCO AND PLACARD REMOVED.

Part: ODOR — DETECTED (CABIN) · airframe 15,365 hrs · 2,481 cycles

FLIGHT ATTENDANTS REPORTED SMELLING BURNING RUBBER IN THE AREA OF ROW 27 WHILE AT CRUISE ALTITUDE. NO SMOKE WAS VISIBLE. LEFT AND RIGHT RECIRC FANS WERE TURNED OFF AND THE SMELL DISAPPEARED. INSPECTED FLOOR DUCTING AND CEILING IN AREA OF ROW 27. INSPECTED RECIR FANS AND FILTERS IN CARGO COMP. RECIR FANS AND AIRFLOW NORMAL. NO ODORS PRESENT.

Part: ODOR — DETECTED (GALLEY) · airframe 11,102 hrs · 1,762 cycles

ATB FOR ELECTRICAL SMELL IN AFT GALLEY...CREW TURNED OFF OVENS AND RECIRC FANS AND UTILITY BUSSES AND SMELL DISSIPATED. MAD MTC INVESTIGATING.

Part: FMC — MALFUNCTIONED (COCKPIT) · airframe 10,791 hrs · 1,711 cycles

DUAL FMC FAIL. LEG PAGES BLANK ON BOTH CALLS. UNABLE TO ENTER ANY FIX LEGS ON BOTH CDU'S. RESET C/BS. BITE HISTORY ON BOTH CDU'S SHOW NO FAULTS. NO FMC FAILURES / LIGHTS. AS PRECAUTION REMOVED BOTH CDU, CLEAN FILTERS INSPECT CONNECTORS AND REINSTALL. CDU'S OPERATIONAL NORMAL.

Part: WARNING LIGHT — FALSE INDICATION (HYD SYSTEM) · airframe 7,610 hrs · 1,203 cycles

ABORTED TAKEOFF AT 90 KNOTS DUE TO C-HYD EICAS MSG. CUTOUT INSP FOR HI/ENERGY STOP IAW AMM 05-51-14-2. DID NOT FIND DAMAGE OR LEAKS FROM WHEELS OR BRAKES. CTR HYDRAULIC SYSTEM CHECKED FOR LEAKS, PRESSURE AND QUANTITY. ALL OK.

Part: LIGHT — SHORTED (COCKPIT) · airframe 4,980 hrs · 800 cycles

STRONG ELECTRICAL BURNING SMELL IN COCKPIT UPON SHUTDOWN. FOUND SHORTED AND BURNT DIODE CAPSULE IN RT MLG INDICATOR LIGHT. ALSO, LENS WAS PUSHED IN AND STUCK. REPLACED LIGHT ASSY, CHECKS OK.

Part: AIR DIST — ODOR (ROW 10)

ELECTRICAL SMELL COMING FROM MID CABIN JUST AFT OF MID GALLEY. FUMES ONLY DEPOWERED UTILITY BUSSES AND AIRSHOW PASSENGER NOTED CRACKLING IN HEADSET ALONG WITH FUMES ROW 10. DROPPED CEILING PANEL AND CHECKED AREA, FREEZER, OVEN AND CHILLER OPERATING, UNABLE TO DETECT ANY FUMES. REF CMI C/N 101490364 AND 101290324 FOR POSSIBLE CAUSE.

Part: AIR DIST — ODOR (CABIN)

F/A IN FWD CABIN REPORTED SMELL OF BURNED PLASTIC AFTER LANDING. ODOR WAS CONCENTRATED IN CTR OF AREA BETWEEN AISLES AND OCCURED SHORTLY AFTER TOUCHDOWN FOR ABOUT 2 MINS. UNABLE TO TRACE EVIDENTS.