N189DN

Part: FAIRING — MISSING (RT NR 12 SLAT) · airframe 123,146 hrs · 18,266 cycles

ON ARRIVAL, W/A CHK FOUND RT WING OTBD MOST LEADING EDGE SLAT LINKAGE FAIRING PANEL (SLAT #12) MISSING. DAMAGED AREA REPAIRED, THE NR 12 SLAT OTBD FAIRING PANEL WAS INSTALLED & PAINTED IAW AMM 51-21-10. (8130946)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 121,954 hrs · 18,058 cycles

ATB TO BOS DUE TO LEFT ENGINE OIL FILTER EICAS MESSAGE. QRH STATES NOT TO INITIATE AN OVER WATER CROSSING. INSPECTED LEFT ENGINE MAGNETIC CHIP DETECTORS IAW FIM, NO TROUBLE FOUND. REMOVED, INSPECTED AND REPLACED LEFT ENGINE OIL FILTER IAW AMM, NO TROUBLE FOUND. REMOVED AND REPLACED OIL FILTER DP SWITCH IAW AMM. OPERATIONAL CHECK OK, NO FAULTS.(7605892)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 119,210 hrs · 17,616 cycles

SHIP 189 FOUND LEFT/RIGHT OFF-WING ESCAPE SYSTEM EMERGENCY BATTERY INOP. CORRECTIVE ACTION: R/R L/R OFF-WING ESCAPE SYSTEM EMERGENCY BATTERY PER B767-300 AMM 25-65. OPS CHECK GOOD. (6948016)

Part: DOOR — MISSING (#04 SLAT LUBRICA) · airframe 118,628 hrs · 17,517 cycles

SHIP 189 #04 SLAT LUBRICATION ACCESS DOOR MISSING. CORRECTIVE ACTION: INSTALLED MISSING #04 SLAT LUBE ACCESS DOOR PANEL. CDL AND PLACARD REMOVED, NO M PROCEDURES. (6645632)

Part: LIGHT — DAMAGED (ZONE 200) · airframe 118,470 hrs · 17,489 cycles

SHIP 189 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:52B. CORRECTIVE ACTION: RESECURED SEAT 52B EMERGENCY LIGHT PER CMM 25-28-89. OK FOR SVC (0664743)

Part: BOTTLE — INOPERATIVE (ZONE 800) · airframe 118,308 hrs · 17,460 cycles

SHIP 189 LEFT OVERWING EMERGENCY BOTTLE LIGHT ON P61 PANEL NOT WORKING. CORRECTIVE ACTION: R/R L/H OVERWING POWER SUPPLY BATTERY PER B767 AMM 25-26. FOUND L/H OVERWING SPOILET SQUIB BLOWN. R/R L/H SPOILET OVERRIDE ACTUATOR SQUIB REF B767-300 AMM 25-65.RE-ARMED OVERWING ESCAPE SYSTEM REF B767-300 AMM 25-65. (9739118)

Part: SQUIB — NO TEST (ZONE 200) · airframe 117,856 hrs · 17,390 cycles

SHIP 189 DURING PDC FOUND EMER ESCAPE SQUIB WONT TEST IN TEST 1 OR 2. CORRECTIVE ACTION: R/R O/W ESCAPE SYS LT & RT BATTERY PACKS PER B767 AMM 25- 65. SYS TEST GOOD. (4071987)

Part: SENSOR — DIRTY (SLIDE INDICATOR) · airframe 117,807 hrs · 17,383 cycles

SHIP 189 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:608. CORRECTIVE ACTION: CLEANED SENSORS CKS OK (0563774)

Part: SWITCH — MALFUNCTIONED (DOOR SLIDE) · airframe 117,783 hrs · 17,379 cycles

SHIP 189 2R DOOR SLIDE LT + FWD PANEL SHOW ARMED W/DOOR IN DISRAMED POSITION. CORRECTIVE ACTION: R/R 'SLIDE' LIGHT SWITCH PER B767-300 AMM 52-73. OPS CK NML. (4071945)

Part: GIRT BAR — DIRTY (ZONE 200) · airframe 117,767 hrs · 17,377 cycles

SHIP 189 2R DOOR SLIDE LIGHT AND FWD FA PANEL SHOW ARMED WITH LEVER IN DISARMED POSITION. CORRECTIVE ACTION: DEBRIS REMOVED, 2R DOOR SLIDE ARMED WARNING SYSTEM OP. TEST C/W OK IAW B767-300 AMM 52-73-00 (4071940)

Part: CONTROL PANEL — ODOR (WX RADAR) · airframe 117,767 hrs · 17,377 cycles

SHIP 189 WXR PANEL BURNING SMELL. CORRECTIVE ACTION: R/R PANEL PER B767-300 AMM 34-43. TEST OK. OK FOR SVC (4071931)

Part: DOOR — FOD (ZONE 800) · airframe 117,419 hrs · 17,329 cycles

SHIP 189 UNABLE TO ARM L1 DOOR. CORRECTIVE ACTION: REMOVED DEBRIS (5262010)

Part: FLEX HOSE — DETERIORATED (RT OVRWG SLIDE) · airframe 115,775 hrs · 17,104 cycles

SHIP 189 RIGHT OFFWING SLIDE DEPLOYMENT FLEX HOSE FROM SLIDE BOTTLE IN LOWER RIGHT FUSELAGE IS SEVERELY DETERIORATED FROM SKYDROL IMPINGEMENT, APPEARS TO BE TOTALLY COLLAPSED INSIDE BRAIDING. CORRECTIVE ACTION: REPLACED HOSE PER B767-300 AMM 25-65-22 (0302820)

Part: BATTERY PACK — NO TEST (OVERWING SLIDE) · airframe 115,242 hrs · 17,018 cycles

SHIP 189 ON PDC FOUND BOTH OVERWING SLIDE SQUIBS NO TESTING. CORRECTIVE ACTION: REPLACED BATT PACKS ON EMER POWER SUPPLIES M961 & M962 REF B767 MM 25-65 NO TEST NML (5728047)

Part: LIGHT — OUT OF ADJUST (R2 DOOR) · airframe 115,164 hrs · 17,001 cycles

SHIP 189 2R DOOR LIGHT NOT CONTROLLING W/ ACTUAL DISARMED POSITION. CORRECTIVE ACTION: ADJUSTED INDICATION LIGHT OF DISARMED POSITION SW, CKS OK. (5081589)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,758 hrs · 16,761 cycles

SHIP 0189 -MISC/DE- CREW ELECTED DE AFTER QRH COMPLETION FOR LE SLAT DISAGREE INDICATION. CORRECTIVE ACTION: VERIFIED RIGGING IS GOOD. REPLACED RIGHT INBD PDU PER B767 AMM 27-81. OPS CHECK NORMAL. (4557330)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,717 hrs · 16,755 cycles

SHIP 0189 -FCNT/DE- CREW DECLARED EMERGENCY DUE TO LE SLAT DISAGREE ON APPROACH. CORRECTIVE ACTION: FOUND TORQUE TUBE DAMAGED. REPLACED SCREWS RECONNECTED TORQUE TUBE AND REPAIRED DAMAGE SECTION. (4557306)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,631 hrs · 16,743 cycles

SHIP 189 DEPLOYMENT BAR GAS SPRING WEAK ON L1 DOOR, CORRECTIVE ACTION: R/R GAS SPRING IAW B767-300 AMM 25-66 OPS CHECK GOOD. (4977638)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,562 hrs · 16,730 cycles

SHIP 189 RIGHT WING LEADING EDGE LOWER PANEL 611KB HAS HAIL DAMAGE. CORRECTIVE ACTION: REMOVED PNL FOR REPAIR. REPAIRED PER B767 SRM 51-70-08 FIBERGLASS 350 DEGREE REPAIR. INSTALLED PANEL PER B767 AMM 57-41. (2900054)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,562 hrs · 16,730 cycles

DIVERTED TO FCO DUE TO ENCOUNTERED HAIL STORM ON DEPARTURE. FIRST OFFICER'S WINDSHIELD OUTER PANE SHATTERED, RADOME DAMAGED AND WEATHER RADAR FAIL. CORRECTIVE ACTION: REPLACED R1 WINDOW AND RADOME. (2887127)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,562 hrs · 16,730 cycles

SHIP 189 -DE/DIV- DIVERTED TO FCO DUE TO ENCOUNTERED HAIL STORM ON DEPARTURE. FIRST OFFICER'S WINDSHIELD OUTER PANE SHATTERED, RADOME DAMAGED AND WEATHER RADAR FAIL. CORRECTIVE ACTION: MAINTENANCE IN PROGRESS. (A008377)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,258 hrs · 16,683 cycles

SHIP 189 ON SVC CHECK FOUND EMERGENCY FLOOR LIGHTING FROM ROW 6 TO 20 INOP ON THE RH SIDE. CORRECTIVE ACTION: REPLACED POWER SUPPLY AND BATTERY AT M9011 IAW B767 AMM 33-51-07 . OPS CHECK GOOD. (2825479)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,201 hrs · 16,676 cycles

SHIP 0189 - DIV - TO SLC DUE TO FO'S PITOT HEAT INOP. CORRECTIVE ACTION: REPLACED FAULTING PITOT PROBE. OPS CHECKS GOOD.(4117326)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,682 hrs · 16,600 cycles

SHIP 189 AFT DOOR ARMING LEVER COVER DAMAGED / POOR CONDITION LOCATIONS:601 CORRECTIVE ACTION: INSPECTED 1L DOOR SEAL NO CUTS OR DEFECTS NOTED. CLEANED AND LUBED DOOR SEAL. ALSO INSPECTED DOOR FRAME AIR NO DEFECTS NOTED. ALL PER B767-300 AMM 52-09 (2751375)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,073 hrs · 16,518 cycles

SHIP 189 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 1L. CORRECTIVE ACTION: COULD MOT DUPLICATE FAULT. (2678565)

Part: NONE — NONE · airframe 111,811 hrs · 16,470 cycles

SHIP 189 CREW REST SMALL RUNNING MAN EMERGENCY EXIT SIGN INOP. CORRECTIVE ACTION: NEEDS BR9795-001 NIS DELTA DEFERRED CREW REST TO MEL + PLAC PER B767 MEL 33-51-01D CREW REST INOP (4134515)

Part: NONE — NONE · airframe 109,531 hrs · 16,102 cycles

SHIP 189 LLCR EXIT SIGN INOP, CORRECTIVE ACTION: REMOVED AND REPLACED LLCR EXIT SIGN IAW B767-300 AMM 33-51-01. OPS CHK GOOD OK FOR SVC (9023510)

Part: LIGHT — FALSE INDICATION · airframe 109,429 hrs · 16,079 cycles

SHIP 189 2R DOOR INDICATING ARMED AFTER DISARMING ON ARRIVAL. CORRECTIVE ACTION: OPERATIONAL TEST OF DOOR 2R PERFORMED ON GROUND AND TEST OK. AMM B767-52-73 (9261560)

Part: NONE — NONE · airframe 109,312 hrs · 16,062 cycles

SHIP 0189 -DIV- TO DTW DUE TO WEATHER RADAR FAILURE ENROUTE. CORRECTIVE ACTION: REPLACED WEATHER RADAR ANTENNA DRIVE UNIT. (9261512)

Part: NONE — NONE · airframe 109,037 hrs · 16,024 cycles

SHIP 189 ODOR REPORTED BY FA'S FROM TO THRU APPROX 1 HR OF FLIGHT, SMOKE AND FUMES QUESTIONNAIRE ATTACHED PER MTC REQUEST, CORRECTIVE ACTION: INSP BOTH ENG COMPRESSOR AND SPINNERCONE, ALL GALLEYS, OVENS, LAVS AND CABIN NIL FINDING. RAN BOTH PACKS AND ENG, NO SMELL NOTED. (8931480)

Part: STRINGER — CRACKED · airframe 108,412 hrs · 15,918 cycles

SHIP 189 RHW LOWER SKIN FASTENER HOLE CRACK AT STRINGER L-9.5 AND WS 980. CORRECTIVE ACTION: REPAIRED AS PER PRI598626-14 REV.0 AND PRI598626-14 REV.1. (2213136)

Part: FRAME — CRACKED · airframe 108,412 hrs · 15,918 cycles

SHIP 189 THE END FITTING OF THE FUSELAGE FRAME WHICH IS ATTACHED ON THE FUEL TANK UPPER SURFACE AT STA 825 ,RBL 90 FOUND CRACK. CORRECTIVE ACTION: THE END FITTING REMOVED AND REPLACED AS PER PRI598682-14 REV.0. THE PRI598682-14 (2212884)

Part: FRAME — CRACKED · airframe 108,412 hrs · 15,918 cycles

SHIP 189 THE END FITTING OF THE FUSELAGE FRAME WHICH IS ATTACHED ON THE FUEL TANK UPPER SURFACE AT STA 852 ,LBL 90 FOUND CRACK. CORRECTIVE ACTION: THE END FITTING REMOVED AND REPLACED AS PER PRI598682-14 REV.0. THE PRI598682-14 REV.0 COMPARED AND COMPLIED WITH ER/A598682-14 (2212885)

Part: NONE — NONE · airframe 108,398 hrs · 15,915 cycles

SHIP 189 ERA 598626-14AD ISSUED FOR REPAIR TO RH LOWER WING SKIN EXTERNAL SURFACE AT STRINGER 9.5L BETWEEN STATIONS 962.2 AND 990.2. FOLL ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 598626-14 SECTION II WITHIN 12000 FLIGHT CYCLES O R 36000 FLIGHT HOURS, FIRST TO OCCUR, AFTER SECTION I. (2212423)

Part: NONE — NONE · airframe 108,398 hrs · 15,915 cycles

SHIP 189 ERA 598626-14AD ISSUED FOR REPAIR TO RH LOWER WING SKIN EXTERNAL SURFACE AT STRINGER 9.5L BETWEEN STATIONS 962.2 AND 990.2. FOLL ON ACTION IS REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 598626-14AD SECTION III EVERY 10,000 FLIGHT CYCLE S (2212426)

Part: NONE — NONE · airframe 108,398 hrs · 15,915 cycles

SHIP 189 RHW I/B FLAP MAIN FLAP UPPER SURFACE DELAMINATION FROM I/B EDGE 32 INCH AND AFT EDGE 6 INCH. CORRECTIVE ACTION: RHW I/B FLAP MAIN FLAP UPPER SURFACE REPAIRED FROM I/B EDGE 32 INCH AND AFT EDGE 6 INCH AS PER B767-300 SRM 57-53-01-2R-01 & SRM 51-70-05. (2198435)

Part: NONE — NONE · airframe 108,398 hrs · 15,915 cycles

SHIP 189 RHW I/B FLAP MAIN FLAP UPPER SURFACE DENT FROM I/B EDGE 24 INCH AND AFT EDGE 9 INCH. CORRECTIVE ACTION: RHW I/B FLAP MAIN FLAP UPPER SURFACE REPAIRED FROM I/B EDGE 24 INCH AND AFT EDGE 9 INCH AS PER B767-300 SRM 57-53-01-2R-1 & SRM 51-70-05. (2198365)

Part: NONE — NONE · airframe 108,176 hrs · 15,864 cycles

SHIP 189 ON WALK AROUND FOUND #1 ENG RT HAND SIDE NACELLE STRUT ACCESS PANEL MISSING 436BR. CORRECTIVE ACTION: ON WALK AROUND FOUND #1 ENG RT HAND SIDE NACELLE STRUT ACCESS PANEL MISSING 436BR. (8151814)

Part: NONE — NONE · airframe 108,094 hrs · 15,846 cycles

SHIP 189 FOUND ON WALK AROUND 2 DENTS RT AFT INBD T/E FLAP, CORRECTIVE ACTION: PERMANENT REPAIR COMPLETE PER B767 SRM 57-53-01 (8843888)

Part: NONE — NONE · airframe 106,938 hrs · 15,579 cycles

SHIP 189 CAUTION FLAP DOESN'T SHOW WHEN DOOR IS ARMED AT L1. CORRECTIVE ACTION: REPLACED ARMING LEVER FLAP. SYSTEM OPERATION IS NORMAL. (LP 7367566)

Part: ACCESS DOOR — MISSING (NR 1 NAC STRUT) · airframe 106,799 hrs · 15,552 cycles

SHIP 189 #1 ENGINE O/B NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: FORWARD TO CDL 54-53-02 PLACARD INSTALLED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 106,027 hrs · 15,408 cycles

SHIP 189 EMERGENCY EXIT SIGN AT L4 DOOR MISSING LENS. CORRECTIVE ACTION: REPLACED L4 DOOR EMERGENCY EXIT DOOR THRESHOLD LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL. (LP 7369662)

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 105,118 hrs · 15,191 cycles

SHIP 189 R2 DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED FUSE ON M733. SYSTEM OPERATION IS NORMAL. (LP 9858413)

Part: SKIN — DEFECTIVE (RT WING) · airframe 105,075 hrs · 15,180 cycles

DURING AIRCRAFT H-CHECK FOUND RIGHT WING LOWER SKIN STR L-6.5 WSTA 990.2 - 1018.2 HOLE REPORTED DEFECT IS A COUNTERSUNK FREEZE PLUG. REPAIRED PER ERA 585233-14. (LP 1514884)

Part: STRINGER — CRACKED (WING) · airframe 111,404 hrs · 16,402 cycles

SHIP 189 DURING INSPECTION PER WC 5724-01010-41B, EM 5724-01010, AD 2018- 11-14, A CRACK WAS FOUND IN A HOLE AT THE END OF STRINGER L-6.5. CORRECTIVE ACTION: ER/A 585233-14AD REVISED TO REV. A. ACCOMPLISH ER/A 585233-14AD REV A SECTION II INSPECTIONS.

Part: FRAME ANGLE — CORRODED (BS 1043) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 STA 1043 STRINGER 17 R FOUND ANGLE STRAP. CORRODED REPAIRED FRAME OUTER CHORD. C/W ERA 585301-14. (LP 1504638)

Part: LATCH — DAMAGED (SERVICE PANEL) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 WASTE WATER SERVICE PANEL 163AL LATCHES DAMAGED CORROSION FOUND IN AREAS AROUND LATCHES, REMOVED CORROSION 0.020 REMAINING OF 0.140 FOUND TO BE OUT OF LIMITS. REPLACED LATCHES. (LP 1506309)

Part: SKIN — CRACKED (BS 998) · airframe 105,075 hrs · 15,180 cycles

L/W LOWER EXTERIOR SKIN IS CRACKED THROUGH FASTNER HEAD I/B OF RIB 31 W.S. 998 LONGERON 6.5. REPAIRED PER ERA 585070-14. (LP 1499219)

Part: STRINGER — DAMAGED (WING) · airframe 111,404 hrs · 16,402 cycles

DURING INSPECTION PER WC 5724-01010-41A, EM 5724-01010, AD 2018- 11-14, A CRACK WAS FOUND IN A HOLE AT THE END OF STRINGER L-6.5. CORRECTIVE ACTION: ER/A 585070-14AD REVISED TO REV. A. ACCOMPLISH ER/A 585070-14AD REV A SECTION II INSPECTIONS.

Part: STRINGER SPLICE — CORRODED (BS 1307) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 WHILE CLEANING ALC FOUND CORROSION ON SPLICE PLATE BETWEEN FASTENERS AT STA 1307 S39R FWD SIDE OF WEB. REPLACED STRINGER SPLICE. (LP 1496376)

Part: FLOORBEAM — CORRODED (BS 1175) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 CORROSION UNDER NUTPLATES ON FLOORBEAMS UPPER CHORD AT STA 1175 RBL 8 AND 17 FOUND OUT OF LIMITS. REPLACED CHORD. (LP 1496367)

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 CORROSION UNDER NUTPLATES ON LOWER FLOOR BEAM UPPER CHORD AT 1197 RBL 3,8,17,34 AND 36. REPLACED PLATE. (LP 1496373)

Part: STRINGER SPLICE — CORRODED (BS 1307) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 WHILE CLEANING ALC FOUND CORROSION ON SPLICE PLATE BETWEEN FASTENERS AT STA 1307 S39R, FWD SIDE OF WEB. REPLACED STRINGER PLATE. (LP 1495272)

Part: SUPPORT BRACKET — CORRODED (BS 1087) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 STA 1087 STRINGER 28R WIRE CLAMP SUPPORT BRACKET CORRODED AND FOUND TO BE OUT OF LIMITS. REPLACED BRACKET. (LP 1493598)

Part: FLOORBEAM — CORRODED (BS 1175) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 CORROSION UNDER NUTPLATES ON LOWER FLOOR BEAM UPPER CHORD AT STA.1175 RBL 8 AND 17. REPLACED UPPER CHORD. (LP 1493977)

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 CORROSION UNDER NUTPLATES ON LOWER FLOOR BEAM UPPER CHORD AT STA.1197 RBL 3 , 8 , 17 , 34 AND 36. REPLACED CHORD. (LP 1493970)

Part: CLOSEOUT PANEL — CRACKED (NR 6 SLAT) · airframe 105,075 hrs · 15,180 cycles

#6 SLAT CLOSE OUT PANEL CRACKED. REPAIRED PER SRM 51-70-17. (LP 1489784)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 STA 1197+110 SHEAR TIE BETWEEN S38R-37R OUT OF LIMITS AND REPLACED. (LP 1486331)

Part: FRAME — CORRODED (BS 1241) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 UPPER CABIN STATION 1241 19 RIGHT CORRODED FRAME BLENDED AND REMOVED CORROSION FOUND OUT OF LIMITS, TRIMMED FRAME AT UPPER CABIN STA 1241 STR 19 R/H, LOCATED, DRILLED, DEBURND, ALODINE, AND PRIMED AND INSTALLED REPAIR ANGLE (LP 1486987)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1219 BETWEEN S39L-S38L CORRODED OUT OF LIMITS AND REPLACED. (LP 1486341)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 STA 1197+110 SHEAR TIE BETWEEN S38L-39L OUT OF LIMITS AND REPLACED. (LP 1486336)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2SHEAR TIE AT STA. 1197+132 CORRODED OUT OF LIMITS BETWEEN S- 39L-S39R. REPLACED SHEAR TIE. (LP 1486344)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 STA 1197+110 SHEAR TIE BETWEEN S39L-39R OUT OF LIMITS AND REPLACED. (LP 1486333)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1219 BETWEEN S39R-S38R CORRODED OUT OF LIMITS AND REPLACED. (LP 1486339)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1219 BETWEEN S37L-S38L CORRODED OUT OF LIMITS AND REPLACED (LP 1486342)

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1285 BETWEEN S38L-S37L CORRODED FOUND OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1485797)

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEARTIE AT STA 1307 BETWEEN S38L-S37L CORRODED FOUND OUT OF LIMITS. REPLACED SHEARTIE. (LP 1485817)

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1285 BETWEEN S39L-S39R CORRODED FOUND OUT OF LIMITS, REPLACED SHEAR TIE. (LP 1485805)

Part: SHEAR TIE — CORRODED (BS 1241) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1241 BETWEEN S39L-S39R CORRODED OUT OF LIMITS AND REPLACED. (LP 1486024)

Part: SHEAR TIE — CORRODED (BS 1263) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1263 BETWEEN S39R-S39L CORRODED FOUND OUT OF LIMITS AND REPLACED SHEAR TIE (LP 1485810)

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 105,075 hrs · 15,180 cycles

CORROSION LEVEL: 2 SHEAR TIE AT STA 1307 BETWEEN S39R-S39L CORRODED OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1484836)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 105,075 hrs · 15,180 cycles

R/H SIDE OF VERTICAL STAB BETWEEN AUX SPAR AND FWD SPAR THERE IS AN AREA OF DELAMINATION AT APROX FSS 92.25. REMOVED DAMAGE, PREPPED AND INSTALLED REPAIR UNDER VACUUM PER SRM 51-70-10. (LP 1477173)

Part: FAN — FAILED (RECIRCULATION) · airframe 103,762 hrs · 14,989 cycles

CREW REPORTED AN ELECTRICAL ODOR IN THE FLIGHT DECK AND ASSOCIATED LT RECIRCULATION FAN MESSAGE. DECISION WAS MADE TO DIVERT TO THE NEAREST SUITABLE AIRPORT. REPLACED THE LT RECIRCULATION FAN, FAN VIBE MONITOR AND FAN FILTER. ALL SYSTEMS CHECKED NORMAL.

Part: SLIDE — UNWANTED DEPLOY (RT WING) · airframe 99,787 hrs · 14,456 cycles

RIGHT WING SLIDE DEPLOYED. REPLACED ACTUATOR.

Part: CONNECTOR — LOOSE (CABIN) · airframe 98,287 hrs · 14,248 cycles

ON SERVICE CHECK FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT 40AB. FOUND LOOSE CONNECTOR OUTSIDE OF SEAT AND RECONNECTED. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (BS 1660) · airframe 97,196 hrs · 14,091 cycles

HFEC INSPECTION SHOWED A CRACK INDICATION ON THE SKIN AT STRINGER 13AR, BS 1660, THE CRACK INDICATION IS APPROXIMATELY. 2.5 INCHES LONG. REMOVED THE DAMAGE IAW SRM 53-80-01.

Part: SKIN — CRACKED (BS 1660) · airframe 97,196 hrs · 14,091 cycles

HFEC INSPECTION SHOWED A CRACK INDICATION IN THE SKIN AT STRINGER 13AL, BS 1660. THE CRACK WAS APPROXIMATELY. 2 INCHES LONG. REMOVED THE DAMAGE AND REPAIRED IAW SRM 53-80-01.

Part: FAILSAFE — CRACKED (BS 955) · airframe 96,519 hrs · 13,991 cycles

DURING UT INSPECTION, FOUND A CRACK INDICATION ON THE RT BS 955 FAILSAFE STRAP. THE FAILSAFE WAS REPAIRED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 96,519 hrs · 13,991 cycles

DURING A HFEC OPEN HOLE INSPECTION, FOUND A CRACK AT BS 955, ON THE FAIL SAFE STRAP. THE FAIL SAFE WAS REPAIRED IAW AD 2012-09-04.

Part: TEE FITTING — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 96,519 hrs · 13,991 cycles

DURING INSPECTION, FOUND CORROSION ON THE TEE FITTING TO THE FAIL-SAFE STRAP. REPLACED IAW AD 2012-09-04.

Part: BLADE — CRACKED (HPT) · airframe 96,343 hrs · 13,967 cycles

WHILE PERFORMING BOROSCOPE INSPECTION OF THE SECOND STAGE NR 1 ENG HPT BLADES, FOUND LEADING EDGE DENTED IN AREA B WITH AXIAL CRACK APPROX .223 INCH IN LENGTH ON CONCAVE SIDE & INTERSECTING RADIAL CRACKS ON CONVEX SIDE .564 INCH. REPLACED THE NUMBER 1 ENGINE

Part: SEAT TRACK — BROKEN (BS 1372) · airframe 94,944 hrs · 13,751 cycles

LEFT INBD SEAT TRACK LUG BROKEN AT BS 1372, REMOVED THE DAMAGED SECTION OF THE SEAT TRACK AND FABRICATED A REPAIR IAW SRM 53-00-52.

Part: SOCKET — LOOSE (CABIN) · airframe 93,224 hrs · 13,483 cycles

EMERGENCY ESCAPE PATH MARKER AT SEAT 37HJ IS INOPERATIVE. MAINTENANCE FOUND A SOCKET LOOSE AND LAMPS AND LENS MISSING AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,318 hrs · 13,180 cycles

EXIT SIGNS ARE INOPERATIVE. REPLACED THE LAMPS. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 90,962 hrs · 13,124 cycles

EMERGENCY PATH LIGHTS AT SEAT 1A ARE INOPERATIVE. MAINTENANCE FOUND LIGHT CONNECTOR DISCONNECTED AND RECONNECTED. SYSTEM OPERATION IS NORMAL.

Part: STRINGER — CRACKED (RT WING) · airframe 87,841 hrs · 12,664 cycles

RIGHT WING STR 6.5 CRACK INDICATION IN HOLES 1 AND 2. REPAIRED IAW ERA 542739-14.

Part: SKIN — CRACKED (LT WING) · airframe 87,841 hrs · 12,664 cycles

LT WING, FASTENER HOLE CRACK AT HOLE NR 1 IN GROUP A, AA5724-01010-03B WING SKIN REWORK. C/W REPAIR.

Part: SKIN — CRACKED (RT WING) · airframe 87,841 hrs · 12,664 cycles

RT WING, FASTENER HOLE CRACK AT HOLE 1 AND 2 IN GROUP A, AA5724-01010-04B WING SKIN REWORK. C/W REPAIR.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,066 hrs · 12,541 cycles

ROWS 16 AND 18 EMERGENCY CEILING LIGHTS ARE INOPERATIVE. MAINTENACE FOUND NO DC VOLTAGE AT PANEL PLUGS AND REPLACED CHARGER. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 85,333 hrs · 12,273 cycles

FOUND SEAT 36F EMERGENCY LIGHT NOT ILLUMINATED. RESEATED EMERGENCY LIGHT CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 83,525 hrs · 12,015 cycles

DURING SERVICE CHECK FOUND MULTIPLE AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND PULLED WIRES FROM CONNECTOR. REPAIRED, SYS OPS NORMAL.

Part: PANEL — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 92,997 hrs · 13,443 cycles

CORROSION LVL 2, NR 2 PYLON AFT STRUT FAIRING I/B AFT PANEL CORRODED AND REPLACED PER ERA 521585-14.

Part: PANEL — DAMAGED (NR 2 NACELLE) · airframe 79,350 hrs · 11,422 cycles

NR 2 PYLON PANEL 447AR SCREW HOLE FOUND ELONGATE REPLACED IAW ERA 521576-14.

Part: SKIN — DAMAGED (BS 900) · airframe 79,291 hrs · 11,410 cycles

BS 900, LBL40 CENTER WING LOWER SKIN LOWER SURFACE FOUND CHAFING REWORKED IAW ERA 521572-14.

Part: PANEL — DAMAGED (NR 2 NACELLE) · airframe 79,350 hrs · 11,422 cycles

NR 2 PYLON PANEL 447AL SCREW HOLE FOUND ELONGATED. REPLACED IAW ERA 521576-14.

Part: FRAME — CRACKED (BS 883) · airframe 79,343 hrs · 11,420 cycles

RIGHT BS 883.5, RBL 89, BELOW WL 200, FRAME FOUND CRACKED APPROX .1875" IN LENGTH. REPAIRED IAW ERA 521583-14AD.

Part: SKIN PANEL — CORRODED (NR 2 PYLON) · airframe 93,129 hrs · 13,469 cycles

NR 2 PYLON, AFT STRUT FAIRING I/B S/W PANEL EXTERNAL SURFACE FOUND CORRODED AND REPLACED.

Part: WEB — CORRODED (NR 2 PYLON) · airframe 92,997 hrs · 13,443 cycles

NR 2 PYLON, AFT STRUT FAIRING SHIELD PAN UPPER WEB LWR SIDE PITTING. REPAIRED PER ERA 521573-14.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 79,291 hrs · 11,410 cycles

NR 2 PYLON INBD SIDE INNER SKIN AND DOUBLER CUTOUT BETWEEN NAC STA 180, ACCESS PANEL 442AL. REPAIRED IAW ER/A 521579-14, REV.

Part: ACCESS PANEL — CRACKED (NR 2 NACELLE) · airframe 79,291 hrs · 11,410 cycles

NR 2 PYLON ACCESS DOOR 426BR CUTOUT FOUND CRACK AND REPAIRED IAW SRM 54-53-01.

Part: STRINGER CLIP — CORRODED (BS 478) · airframe 79,291 hrs · 11,410 cycles

BS 478, STRINGER CLIP 17R FOUND CORRODED. REPLACED IAW SRM 51-10-02 & SRM 51-40-02.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 79,291 hrs · 11,410 cycles

NR 2 PYLON INBD SIDE STRUT SKIN, AFT TRAPEZOIDAL ACCESS DOOR CUTOUT CRACKED. COMPLIED WITH ERA 090076-14.

Part: WEDGE — DEFORMED (NR 4 SLAT) · airframe 79,291 hrs · 11,410 cycles

NR 4 SLAT WEDGE AREA UPPER SURFACE OTBD EDGE DEFORMED. REPAIRED IAW SRM 57-43-02.

Part: ATTACH ANGLE — CORRODED (NR 2 PYLON) · airframe 92,997 hrs · 13,443 cycles

NR 2 PYLON AFT STRUT FAIRING SHIELD PAN O/B ATT ANGLE CORRODED. REPLACED.

Part: WEB — CORRODED (BS 1043-1048) · corrosion level 2 · airframe 79,350 hrs · 11,422 cycles

BS 1043-1048, STRINGER 18L SUPPORT WEB FOUND CORRODED. REPLACED & INSTALLED IAW SRM 51-10-02 & SRM 51-40-02.

Part: FRAME — CRACKED (BS 883) · airframe 79,350 hrs · 11,422 cycles

LT BS 883.5, LBL 89, BELOW WL 200, FRAME TRANSITION RADIUS FOUND CRACKED APPROX .1895 IN LENGTH. REPAIRED.

Part: SHEAR TIE — CORRODED (BS 1502) · airframe 79,291 hrs · 11,410 cycles

BULK CARGO SHEAR TIE BS 1502, S38-39L FOUND CORRODED. REPLACED SHEAR TIE IAW ERA 521584-14.

Part: SHEAR TIE — CORRODED (BS 1502) · airframe 79,291 hrs · 11,410 cycles

BULK CARGO BS 1502, S38-39L SHEAR TIE FOUND CORRODED. REPLACED IAW ERA 521584-14.

Part: FRAME — CRACKED (BS 883) · airframe 79,350 hrs · 11,422 cycles

LEFT BS 883.5, LBL 89, BELOW WL 200, FRAME TRANSITION RADIUS FOUND CRACKED, APPROXIMATELY .1875" IN LENGTH. REPAIRED.

Part: STRINGER CLIP — CORRODED (BS 1131) · corrosion level 2 · airframe 79,350 hrs · 11,422 cycles

BS 1131, STRINGER CLIP 16L FRAME FOUND CORRODED. REPLACED IAW SRM 51-10-02 AND 51-40-02.

Part: WEB — CORRODED (BS 1043-1048) · corrosion level 2 · airframe 79,291 hrs · 11,410 cycles

BS 1043 - 1048, S18L FRAME TO FRAME SUPPORT WEB FOUND CORRODED. REPLACED IAW SRM 51-10-02 AND 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 79,291 hrs · 11,410 cycles

BULK CARGO SHEAR TIE BS 1540, S37-38L FOUND CORRODED. REPLACED IAW SRM 51-10-02.

Part: STRINGER CLIP — CORRODED (BS 1131) · corrosion level 2 · airframe 79,291 hrs · 11,410 cycles

BS 1131, STRINGER CLIP AT 16L FRAME CORRODED AND REPLACED.

Part: FITTING — DAMAGED (NACELLE) · airframe 79,291 hrs · 11,410 cycles

AFT PITCH LOAD BACKUP FITTING DAMAGED. REPAIRED IAW ER/A 521570-14AD.

Part: FITTING — CRACKED (NR 2 NACELLE) · airframe 79,291 hrs · 11,410 cycles

NR 2 PYLON FWD UPPER SPAR FITTING ATTACH BUSHING EDGE SEALANT FOUND CRACKED. FABRICATED AND INSTALLED IAW SRM 54-53-90.

Part: BUSHING — CRACKED (NR 1 NACELLE) · airframe 79,291 hrs · 11,410 cycles

NR 1 PYLON FWD UPPER SPAR FITTING ATTACH BUSHINGS EDGE SEALANT FOUND CRACKED. REPLACED BUSHING AND WASHERS IAW SRM 54-53-90.

Part: COMPUTER — FAILED (CENTER) · airframe 79,027 hrs · 11,370 cycles

AFTER APPROXIMATELY 4 HRS OF FLIGHT, WITH ACFT LEVEL AT 370, SMELLED ELECTRICAL ODOR. SHORTLY AFTER, NOTED NO LAND 3 ON AUTO LAND STATUS, ODOR DECREASED CONTINUOSLY TO ZERO BY END OF FLIGHT. PERFORMED TROUBLESHOOTING IAW FIM 22-02, FAULT TREE 808 , PERFORMED TEST OF FCC L-C-R CENTER FCC FAILED, UPON REMOVAL OF FCC. CENTER FOUND, ELECTRICAL ODOR DETECTED, ALL PINS CHECK OK, NO DAMAGE REPLACED CENTER FCC IAW AMM. PERFORMED FCC TEST 1 AND A/C LAND TEST 40 , ALL TEST COMPLETE AND OK . SYSTEM CHECKS NORMAL.

Part: FLOORBEAM — CRACKED (BS 1439) · airframe 75,361 hrs · 10,818 cycles

BS 1439, LBL 24-27 FLOORBEAM LOWER CHORD CRACKED. REPAIRED IAW ERA 509192-14 REV ORG.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 75,361 hrs · 10,818 cycles

RT WING INBD MAIN FLAP OTBD L/E FAIRING FOUND DELAMINATED PERFORMED COMPOSITE. PREPREG HOT BOND REPAIR IAW SRM 57-53-01 REPAIR 1 AND B767 51-70-05 PARA 5A, FIG 5.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 75,361 hrs · 10,818 cycles

LT WING INBD MAIN FLAP OTBD L/E FAIRING FOUND DELAMINATED. PERFORMED PREPREG HOT BOND REPAIR IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05 PAR 5A, FIG 5.

Part: SKIN — DELAMINATED (LT NR 5 SLAT) · airframe 75,361 hrs · 10,818 cycles

LT NR 5 SLAT INBD UPPER CORNER DELAMINATED. PERFORMED METAL HOT BOND REPAIR IAW SRM 57-43-02, REPAIR 1, FIG 201 AND SRM 51-70-10 REPAIR NR 4, FIG 202

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 75,361 hrs · 10,818 cycles

RIGHT WING INBD AFT FLAP DENTED WITH AN AREA 1.0X1.25", DEPTH .2187" LOCATED AT LWR SURFACE APPROX 84" FROM INBD EDGE AND 3" FROM AFT FLAP LE. HOT BOND REPAIR PERFORMED IAW SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 201.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,842 hrs · 10,595 cycles

EMERGENCY PATH LIGHTS ARE INOPERATIVE FROM ROW 6F-20F. MX REPLACED THE FUSE IN POWER SUPPLY M9011. SYSTEM OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,223 hrs · 10,386 cycles

DURING DAILY CHECK, FOUND EMERGENCY LIGHTS RIGHT SIDE ROW 6 THROUGH 20 INOPERATIVE. REPLACED POWER SUPPLY PER AMM 33-51. OPERATES NORMAL.

Part: FUSE — OPEN (EMERGENCY LIGHT) · airframe 71,003 hrs · 10,213 cycles

EMERGENCY LIGHTS ON SEATS 17AB TO 20 AB DO NOT ILLUMINATE. REPLACED FUSE IN POWER SUPPLY M9011 PER AMM33-51.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 70,823 hrs · 10,193 cycles

STA 955 FAIL SAFE STRAP REPAIR C/W ON ERA 499813-14AD (ERA 499813-14AD).

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 69,423 hrs · 10,006 cycles

UPON ARRIVAL AT AMS FOUND SCRATCH AT FUSELAGE AT LOWER AFT POS OF FWD CARGO DOOR OPENING BETW STA 618 & 632. 2.5 BY 0.25 INCH. INSPECTED AND REPAIRED BY SHEET METAL WORKER PER SRM 767-300 53-00-15. OK FOR SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 68,884 hrs · 9,938 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 17AB ARE INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AND REPAIRED IT. SYSTEM OPERATION IS NOW NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,380 hrs · 9,872 cycles

MAINTENANCE FOUND THE L1 AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN MODULE M736. EMERGENCY EXIT LIGHTS NOW TEST GOOD.

Part: SKIN — DENTED (BS 654) · airframe 66,124 hrs · 9,587 cycles

FUS DENT AT STA 654+44 STRINGER 34R AND 35R. DENT WAS REPAIRED IAW ERA 488689-14 REV A. THERE WAS NO NEGATIVE, OPS AFFECT AS A RESULT OF THIS DAMAGE. REPAIR IS PERMANENT IN NATURE.

Part: SKIN — DENTED (BS 1373 S28-29R) · airframe 66,124 hrs · 9,587 cycles

FUSELAGE SKIN INTERCOSTAL, FS 1373 S28R TO S 29R DENT PERMENANT REPAIR TO SKIN.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,492 hrs · 9,113 cycles

EMERGENCY LIGHTS INOP AT ROWS 14-20 LEFT. REPLACED BATTERY MFG P/N AD-2013-1A AND BATTERY CHARGER MFG P/N 2012-1, EMERGENCY LIGHTS OPS CHECK GOOD AT ROWS 14-20 LEFT.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 62,451 hrs · 9,107 cycles

ON TAKEOFF CAPT AIRSPEED INDICATOR INOP. ABORTED TAKEOFF AT 75 KNTS INDICATED ON F/O AIRSPEED INDICATOR. REPLACED INDICATOR, CHECKS OK

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,435 hrs · 9,103 cycles

EMERGENCY SEAT LIGHTS INOPERATIVE FROM 6FG TO 20 FG, MX REPLACED BATTERY CHARGER PACK. OPS CHECKS GOOD.

Part: FUSE — FAILED (EMERGENC LIGHT) · airframe 62,026 hrs · 9,054 cycles

EMERGENCY LIGHTS INOP ON SEAT ROWS 7-19 ON RT SIDE. FOUND BAD FUSE ON POWER SUPPLY M9011 REPLACED SAME. EMERGENCY LIGHTS CK GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 62,026 hrs · 9,054 cycles

EMERGENCY LIGHTS INOP ON SEAT ROWS 7-19 ON RT SIDE. FOUND BAD FUSE ON POWER SUPPLY M9011 REPLACED SAME, EMERGENCY LIGHTS CK GOOD. ETOPS CATEGORY 'E', PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 61,257 hrs · 8,946 cycles

NR 1 ENGINE WILL NOT START. FOUND BAD STARTER. REMOVED AND REPLACED STARTER ON NR 1 ENG PER AMM. FLIGHT CREW RAN ENG NR 1, ALL CHECKS GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: CHILLER — FAILED (GALLEY) · airframe 60,571 hrs · 8,858 cycles

STRONG BURNING ODOR FROM REAR GALLEY, FROM CHILLER AND CART VENTS. INSPECTED AFT GALLEY CHILLERS FOUND RT CHILLER INOP WITH STRONG BURNING ODOR. REPLACED AFT RT CHILLER PER MM. OPS CHECK OK. NO ODOR PRESENT. ALSO INSPECTED AFT EQUIPMENT AREAS NO BURNING SMELL NOTED. CHECKED LAVS AND GALLEY CEILINGS, NO TROUBLE FOUND. DURING INSPECTION FOUND AFT EXH FAN 1 INOP. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: ADC — FAILED (E&E BAY) · airframe 60,447 hrs · 8,841 cycles

DIVERSION - LT ADC FAILED IN FLT. IAS AND ALT FLAG IN VIEW/C REPLACED LT ADC. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: CIRCUIT CARD — FAILED (ENGINE SPEED) · airframe 59,435 hrs · 8,719 cycles

L ENG SPEED CARD STATUAS MESSAGE. R & R LT ENG SPEED CARD PER AMM. PERFORMED SPEED CARD TESTS.ALL CHECKS NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: RELAY — INOPERATIVE (SERVICE BUSS) · airframe 58,872 hrs · 8,651 cycles

DURING TAXI LT FWD BOOST PUMP EICAS MESSAGE AND LOW PRESS LIGHT. REMOVED AND REPLACED LT FWD BOOST PUMP PER AMM. NO HELP. FOUND NO VOLTAGE ON PH A OR B OF 115VAC GROUND SERVICE BUSS. CYCLED CB C316 GROUND SERVICE BUSS AND POWER RETURNED TO BOOST PUMP CB C372. SUSPECT K102 STUCK. BOOST PUMP NOW OPERATING NORMAL. MCO/PLACARD REMOVED. ACFT OK FOR SVC.

Part: CONNECTOR — CONTAMINATED · airframe 57,344 hrs · 8,463 cycles

JUST CLEARING MAIN AIRSPACE GOT LEFT FUEL SYSTEM PRESS MSG DIV TO JFK FOR REPAIRS. FOUND PUMP OPERATING NORMAL. FOUND C/P PINS GREEN AND SWITCH PINS CONTAMINATED AT LOW PRESS SWITCH S71. REPINNED CONNECT AND REPLACED LOW PRESSURE SWITCH S71. WITH SWITCH OUT AND P ON FOUND NO FLOW FROM LOW PRESS LINE-AFTER SEVERAL MINUTES BLOCKAGE CLEARED-PURGED LINE FOR SEVERAL MORE MINUTES UNTIL ALL FLOW CLEAR. REINSTALLED SWITCH ALL OPS NORMAL. NO FURTHER CONTAMINATION FOUND IN TANK.

Part: PUMP — FAILED (FUEL BOOST) · airframe 57,344 hrs · 8,463 cycles

RTB - TAXI OUT LT FWD FUEL BOOST PUMP FAILED. FOUND PUMP OPERATING NORMAL. FOUND C/P PINS GREEN AND SWITCH PINS CONTAMINATED AT LOW PRESS SWITCH S71. REPINNED CONNECT AND REPLACED LOW PRESSURE SWITCH S71. WITH SWITCH OUT AND P ON FOUND NO FLOW FROM LOW PRESS LINE-AFTER SEVERAL MINUTES BLOCKAGE CLEARED-PURGED LINE FOR SEVERAL MORE MINUTES UNTIL ALL FLOW CLEAR. REINSTALLED SWITCH ALL, OPS NORMAL NO FURTHER CONTAMINATION FOUND IN TANK.

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 57,241 hrs · 8,451 cycles

ON ENGINE START LT GEN DROPPED OFF LINE, GEN OFF LIGHT AND FIELD LIGHT AT AFT PNL CAME ON. RESET FIELD BIT BPCU FOUND UNDER FREQ TRIP. CLEARED MESSAGE, RAN ENG CHECKS, OK NO HISTORY. FAULTS DID NOT REOCCUR.

Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 56,189 hrs · 8,327 cycles

EMERGENCY ESCAPE SLIDE RT AND LEFT SPOILER FAIL SQUIB TEST. REPLACED BOTH BATTERY AND BATTERY CHARGERS FOR ESCAPE SLIDE AND SPOILER SQUIBS.

Part: CLUTCH — DAMAGED (APU STARTER) · airframe 55,780 hrs · 8,278 cycles

APU WILL NOT START. REMOVED APU STARTER AND FOUND CLUTCH DAMAGED. REMOVED APU. STARTED INSTALLING NEW APU. INSTALLED NEW APU PER AMM. RAN APU CHECKS GOOD. MCO AND PLACARD REMOVED.

Part: ISOLATION VALVE — INOPERATIVE (CUSTOMER AIR) · airframe 53,075 hrs · 7,953 cycles

L ISOL VALVE EICAS MSG, SWAPPING WITH CTR LEFT ISOLATION VLV. REPLACED AND CHECKED OK. PN 2780539-103.

Part: BRAKE ASSY — DAMAGED (LT MLG) · airframe 48,932 hrs · 7,433 cycles

ON LANDING NOTICED HIGH BRAKE TEMP ON LT MLG FIM PROCEDURE 32-46-00/104 FIG 103 AND FIM PROCEDURE 32-46-00/105 FIG 104 C/OUT. NO FAULTS FOUND ON BRAKES TEMPERATURE INDICATION SYSTEM AND NO ANTISKID OR AUTOBRAKE FAILURE FOUND. NO FAILURE FOUND ON WHEEL 4 AND INDICATION NORMAL. AT A/C ARRIVAL FOUND WHEEL 6 WITH TEMP INDICATION A UNIT. HIGH ENERGY STOP INSPECTION PERFORMED 05-51-14. NO FUSE MELTED. FOUND BRAKE 6 DAMAGED. BRAKE 6 DO NOT TURN FREE. BRAKE 6 REMOVED AND REPLACED IAW AMM 32-41-08 CHECKED FOR LEAKAGE NIL FOUND. A/C RTS ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: PROBE — MALFUNCTIONED (NR 1 ENGINE) · airframe 47,321 hrs · 7,227 cycles

L ENG EEC MODE EICAS WITH ALT LIGHT IN EEC CONTROL PANEL AFTER START L ENG EEC INLET PT2/TT2 PROBE REPLACED.

Part: COMPUTER — MALFUNCTIONED (LT ADC) · airframe 46,880 hrs · 7,171 cycles

CAPTAINS ALTIMETER INOP. REMOVED AND REPLACED L ADC AND CAPT ALTIMETER PERFORMED TEST CHKS OK.

Part: PROCESSOR — UNSERVICEABLE (TCAS) · airframe 46,054 hrs · 7,072 cycles

PRIOR TO TAKEOFF WHEN TCAS SELECTED TCAS INOP ON VSI AND NO TCAS ON RADAR SCREEN. REPLACED TCAS PROCESSOR. TEST OK.

Part: SMOKE — DETECTED (E/E BAY) · airframe 45,857 hrs · 7,049 cycles

F/A ADVISED CREW OF ACRID ODOR COMING FROM ENTERTAINMENT CENTER UPON CLOSER INSP F/A NOTICED THIN WHISP OF SMOKE FROM BOTTOM OF EQUIPMENT STACK AND REMOVED POWER FROM SYSTEM. DETECTED SOURCE OF SMOKE COMING FROM VMOD AS SOON IFE PWR IS TURNED ON FWD TO MCO PER MEL 25-20-01MM PROCEDURE C/W PLACARD INSTALLED. REACT IFE AND REPLACED VMOD PER MM. IFE CHECKS GOOD. MCO/PLAC REMOVED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,990 hrs · 6,947 cycles

FOUND SEAT 41FG EMERGENCY ESCAPE PATH LIGHT ASSY INOP.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 43,952 hrs · 6,814 cycles

RIGHT GENERATOR DRIVE LIGHT ILLUMINATED DISCONNECTED IDG IN FLT. REPLACED IDG.

Part: CONNECTOR — LOOSE (EMERGENCY LGHT) · airframe 42,013 hrs · 6,565 cycles

SEAT 38B EMERGENCY SEAT LIGHT INOP. RESEATED CONNECTOR AT SIDEWALL, OPS CHECK OK.

Part: BLEED VALVE — MALFUNCTIONED (RT ENGINE) · airframe 41,522 hrs · 6,497 cycles

RIGHT ENG BLEED VALVE WILL NOT OPEN. HPSOV DEACT IN CLOSED POSITION. REACTIVATED VALVE BACK TO NORMAL. ENG GRD RUN OK. A/C OK FOR SERVICE.

Part: PANEL — MISSING (LT WING) · airframe 40,631 hrs · 6,382 cycles

LEFT WING PANEL (NR 521EB) COMPLETELY MISSING FROM WING WHEN AIRCRAFT ARRIVED IN LGW. REPLACED SAME.

Part: ACM — FAILED (LEFT) · airframe 40,581 hrs · 6,373 cycles

STRONG FUMES IN CABIN AND COCKPIT ON TAKEOFF. REPLACED LEFT ACM.

Part: COMPRESSOR — MALFUNCTIONED (WATER PRESSURE) · airframe 38,892 hrs · 6,147 cycles

SMELL OF SMOKE ELEC FROM AROUND ROW 38. REPLACED WATER COMPRESSOR.

Part: ENGINE — MAKING METAL (NR 2) · airframe 38,536 hrs · 6,097 cycles

ENGINE SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE. FOUND METAL ON CHIP DETECTORS. REPLACED ENGINE.

Part: WIRE — CHAFED (ENTERTAIN SYS) · airframe 38,290 hrs · 6,061 cycles

F/A REPORT SEAT 1A ENTERTAINMENT CONTROL WIRE SHORTED OUT. SHOWS SIGNS OF BURNS ON ELECTRICAL CHORD. REPLACED SAME.

Part: INDICATOR — UNSERVICEABLE (ALTIMETER) · airframe 38,243 hrs · 6,055 cycles

F/O ALTIMETER INOP AFTER T/O. RESET C/B, NO HELP. REPLACED F/O`S ALTIMETER PER A/C MM 34-13-01-404. ALT CHECKS OK.

Part: ENGINE — FAILED (NR 2) · airframe 38,111 hrs · 6,038 cycles

DUE NR 1 OP 50103 7TH STG HPC BLADES INSPECTION. REPLACED ENGINE.

Part: SHUTOFF VALVE — FAILED (TE FLAPS) · airframe 36,879 hrs · 5,856 cycles

FLAPS FAILED TO RETRACT PAST 5 AFTER T/O. ALSO RECEIVED A TRAILING EDGE DISAGREE LIGHT. REPLACED RELAY K351 AND SHUTOFF VALVE SOLENOID V1.

Part: LIGHT — MALFUNCTIONED (AFT GALLEY) · airframe 34,325 hrs · 5,496 cycles

ELECTRICAL ODOR COMING FROM RT SIDE AFT GALLEY (DUTYFREE CART AREA). REPLACED WORK LIGHT.

Part: BRAKE — LOOSE (MLG) · airframe 34,274 hrs · 5,483 cycles

FOUND NR 5 BRAKE ROTOR/STATORS LOOSE. REPLACED NR 5 BRAKE ASSY PER M/M.

Part: WEDGE — DELAMINATED (T/E FLAP) · airframe 27,702 hrs · 4,402 cycles

DELAMINATION TO INBOARD AFT FLAP T/E WEDGE. REPAIR AUTHORIZED PER ER/A 417896-14.

Part: WIRE HARNESS — FAILED (CABIN) · airframe 27,062 hrs · 4,300 cycles

FOUND EMERGENCY LIGHTS AT SEAT 6FG INOP. FOUND HARNESS BAD AND REPLACED SAME. OPS CHECKS OK.

Part: FAN — FAILED (E/E BAY) · airframe 21,153 hrs · 3,323 cycles

FWD EQPT EXHAUST FAN STATUS MESSAGE ILLUMINATED. FWD EXH EQUIP COOL FAN C/B POPPED. CAPT REPORTED SMOKE IN COCKPIT. REPLACED LING ON LAND LINE. REPLACED FWD EQUIPMENT COOLING FAN.

Part: BATTERY — FAILED (FUSELAGE) · airframe 19,892 hrs · 3,099 cycles

MAIN BATTERY CHARGER MESSAGE APPEARED ON EICAS. A/C RETURNED TO JFK. REPLACED MAIN BATTERY AND CHARGER. ETOPS CATEGORY ''B'': DIVERSION OR TURNBACK

Part: FUSE — FAILED (CABIN) · airframe 17,023 hrs · 2,618 cycles

DURING PDC FOUND E-PATH LIGHTS INOP SEATS SECTION THREE LEFT AND RIGHT AISLES. REPLACED FUSE IN M9009 AND REPAIRED WIRING AT SEAT 24AB. E-PATH LIGHTS NOW OPS OK.

Part: SLIDE — DEPLOYED (R1 DOOR)

TWENTY MIN AFTER REACHING TOP OF CLIMB FL310, LOUD NOISE HEARD IN R-1 DOOR AREA. AIR LEAK HEARD ON FWD EDGE OF R-1 DOOR. NO PROBLEM WITH PRESSURIZATION OR CABIN ALTITUDE. AFTER LANDING JFK DURING TAXI R-1 DOOR OPENED AND SLIDE DEPLOYED ON TAXI-WAY. REPLACED SLIDE, DOOR OPERATION OK.

Part: SKIN — PUNCTURED (BS 654)

THE FUSELAGE SKIN, UNDERLYING STRINGER AND UNDERLYING FRAME CHORD WERE PUNCTURED AND DAMAGED BY GROUND SUPPORT EQUIPMENT. A NEW SECTION OF STRINGER WAS SPLICED, THE FRAME CHORD REPAIRED, AND A SKIN DOUBLER INSTALLED PER THE B767 SRM AND DOCUMENTED PER ER/A 367542-14.

Part: COFFEEMAKER — DIRTY (FWD GALLEY)

FAS NOTICED ELECTRICAL SMELL ASSOCIATED W/ FWD GALLEY C/MS. SMELL DISSIPATED WHEN THE C/MS WERE SHUT OFF. REMOVED BOTH COFFEEMAKERS AND INSPECTED WIRING. WIRING OK. OPERATED BOTH C/MS, CKD OK. REMOVED REMNANTS OF PLASTIC ON C/M 1 HOT PLATE, OPS OK.

Part: SKIN — DENTED (BS 401)

THE FUSELAGE SKIN AND UNDERLYING STRINGER WERE DENTED AND SCRATCHED BY GROUND EQUIPMENT AT FS 401, STRINGER 33R. THE DAMAGED AREA SKIN WAS CUTOUT 16 X 3.5 AREA AND THE DAMAGED SECTION OF STRINGER WAS CUTOUT. THE STRINGER WAS REPAIRED PER THE B767 SRM AND THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 366402-14, REV A.

Part: AIR DIST — ODOR (MID GALLEY)

HEAVY HOT DUCT ELECTRICAL SMELL AFT OF MID GALLEY. PULLED AFT EQ EXHAUST FAN NR 1, NO HELP. INSPECTED ENTIRE AREA AFT OF MID GALLEY INCLUDING GALLEY OVENS AND COFFEEMAKERS. RAN BOTH PACKS AND ENTERTAINMENT SYSTEM, NO FAULTS FOUND, A/C DISPATCHED. AS A PRECAUTION, CLEANED GALLEY VENT FAN SCREEN, REPLACED S75 THERMAL SWITCH AND V13 CARGO HEAT VALVE PER MSU SET UP. RAN ALL GALLEY AND CABIN SYSTEMS, NO PROBLEM NOTED.

Part: SAM MODULE — FAILED (E/E COMPT)

EICAS/OVERHEAD RUDDER RATIO AND AILERON LOCK-OUT MESSAGE CAME ON AFTER LEVEL OFF AND A/P DISCONNECT. TRIED RESET, NO HELP. A/C SUSTAINED LIGHTNING STRIKE AFTER TAKEOFF. REPLACED LEFT AND RIGHT SAM MODULES PER MM. MCDP TEST NUMBER 40 ALL OK. PERFORMED LIGHTNING STRIKE INSPECTION PER 05-51-19-2, ALL OK.