N678DL

Part: INDICATOR — NO DISCREPANCY (R3 DOOR SLIDE) · airframe 92,463 hrs · 42,066 cycles

SHIP 678 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:610. CORRECTIVE ACTION: CYCLED ARM/DISARM 3R DOOR PER B757 AMM 25-66. CYCLED DOOR PER B757 AMM 52-11. OPS NORMAL. (0432331)

Part: LIGHT — MISSING (SEAT ROW 22D) · airframe 92,304 hrs · 41,954 cycles

SHIP 678 WHITE EMERGENCY PATH LIGHT ASSY MISSING AT SEAT ROW 22D. CORRECTIVE ACTION: REPLACED MISSING EMERGENCY PATH LIGHT ASSY AT SEAT 22D REF B757 AMM 33-51. OPS CHECKS GOOD. (5627343)

Part: PROXIMITY SWITCH — INOPERATIVE (R3 DOOR SLIDE) · airframe 91,534 hrs · 41,508 cycles

UPON ARMING DOOR 3R SLIDE ARM LIGHT INOP. CLEANED AND REMOVED DEBRIS FROM PROX SWITCH PERFORMED OPS CHECK OF ENGAGEMENT LIGHT AS PER B 757 AMM 25-66. OPS CHECK OK. LIGHT WORKING NORMAL A/C OK FOR SVC.

Part: ROD — BROKEN (GIRT BAR) · airframe 91,505 hrs · 41,491 cycles

SHIP 678 OOR 2L JAMMED CLOSED. CORRECTIVE ACTION: FOUND FWD CORNER OF GIRT BAR NOT ENGAGING THE ARMING LEVER, RESECURE ARMING LEVER, REMOVED L2 DOOR SLIDE COVER PER B757 AMM 52-12, FOUND L2 DOOR GIRT BAR BEARING SPRING ROD BROKEN. REMOVED PER B757 AMM 52-11. PINNED BOTTLE FOR RII INSPECTION. VERIFIED PIN REMOVAL ON L2 DOOR. ALL RII COMPLIED WITH (777616) REINSTALLED L2 DOOR SLIDE COVER. DOOR OPS NML. ARM AND DISARM PER NML. DOOR OPEN AND CLOSED NML. (5477784)

Part: PROXIMITY SWITCH — FAULTED (L3 DOOR SLIDE) · airframe 91,530 hrs · 41,505 cycles

SHIP 678 3L DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT PROX SWITCH AS PER B 757 AMM 25-66 OPS CHECK OK A/C OK FOR SVC. (5477790)

Part: INDICATOR — INOPERATIVE (L2 DOOR) · airframe 91,492 hrs · 41,481 cycles

SHIP 678 THE 2L ENTRY DOOR KNUCKLE KNOCKER INOP. CORRECTIVE ACTION: FOUND DEBRIS ON TOP OF KNUCKLE KNOCKER CAUSING KNOCKER TO STICK IN RECESSED POSITION. REMOVED DEBRIS. OPS CHECK NORMAL. (5477762)

Part: TARGET — OUT OF ADJUST (L1 DOOR SENSOR) · airframe 91,303 hrs · 41,361 cycles

SHIP 678 ILLUMINATED. BOTH EICAS & OVRHEAD. FLIGHT ATTENDANT REPORTED DOOR APPEARED CLOSED & ARMED NORMALLY. AIRCRAFT SENT ON/IN ACARS AS IF DOOR OPENED. AFTER 33MIN SITTING ON GROUND, THE LIGHT WENT OUT W/NO CREW ACTION TAKEN (1433Z) RE-ILLUMINATED AT 1452Z, APPROX 20MIN LATER. CORRECTIVE ACTION: ADJUSTED L1DOOR TARGET PER B757AMM 52-71-00 INDICATION NORMAL. (5484646)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 91,264 hrs · 41,330 cycles

SHIP 678 CORROSION IN AFT CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME UPPER SURFACE BS.1480 APROX BETWEEN BL.0 AND RBL.7.5. DOT 129-030. CORRECTIVE ACTION: -SUMMARY OF NR-00378- REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ON AFT CARGO COMPARTMENT FLOOR STRUCTURE MAIN FRAME UPPER SURFACE BS.1480 APROX BETWEEN BL.0 AND RBL.7.5 IAW ER/A 614192-14AD REV ORIGINAL. (0128062)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 FUSELAGE / FRAME / STA 1480, BETWEEN BL 0 & RBL 7.5 / CORROSION. CORRECTIVE ACTION: REF ERA 614192-14AD. (0121926)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 WHILE PREFORMING L-2 DOOR TORQUE TUBE OVERHAUL ROTARY SNUBBER FOUND TO BE OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED L-2 DOOR ROTARY SNUBBER ASSY AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW B757 AMM 52-11. (0118611)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 678 (2) INDICATIONS OF DEFECTS NOTED ON R/H FRAME STA 1640 LWR INBD OPEN HOLE. INDICATIONS ARE AT THE 3 AND 9 OCLOCK POSITIONS LOOKING AFT. CORRECTIVE ACTION: SUMMARY OF NR-00527 AND NR-00567- REMOVED DAMAGED FRAME SECTION AT STA 1640RH AND ACCOMPLISHED PERMANENT REPAIR IAW ER/A 613088 -14AD REV ORIG. REFERENCE LOG PAGES 0087928 AND 0087932 FOR FOLLOW ON INSPECTIONS. (0109855)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 2 INDICATIONS NOTED ON FRAME 1681, RIGHT HAND SIDE INBOARD LOWER OPEN HOLE AT 3 AND 9 O'CLOCK POSITION LOOKING FWD (INDICATION GOING INBOARD AND OUTBOARD) SEPERATION OF LAYERS IS REQUIRED TO DETERMINE WHICH LAYER OR LAYERS ARE DEFECTED. CORRECTIVE ACTION: SUMMARY OF NR-00404: REMOVED DAMAGED FRAME SECTION AND ACCOMPLISHED PERMANENT FRAME REPAIR AT RH STA 1681 STR 14R-STR 21R IAW ERA 613080-14AD. (0108384)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 MAIN CABIN SEAT TRACK LOWER SURFACE HAS A CRACK AT RADIUS APROX BS.1322 RBL.45. CORRECTIVE ACTION: SUMMARY OF NR-00354- ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR SEAT TRACK APROX STA 1320-1350 RBL 45 IAW B757-200 SRM 53-00. (0106911)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 MAIN CABIN SEAT TRACK LOWER SURFACE HAS A CRACK AT RADIUS APROX BS.1322 RBL.45. CORRECTIVE ACTION: SUMMARY OF NR-00355- ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR SEAT TRACK APROX STA 1320-1350 LBL 45 IAW B757-200 SRM 53-00. (0106861)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 FUSELAGE / FRAME / LHS BSTA 1681 / WL 208 / S-17L & S-18L / CRACK INDICATION. CORRECTIVE ACTION: SUMMARY OF NR-00403- ACCOMPLISHED FRAME SECTION REPAIR AT STA 1681 LH FROM PRODUCTION SPLICE STR 14L TO STR 25L IAW ER/A 613012-14. (0102403)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 AFT CARGO DOOR APPROX 29 INCHES AFT OF FWD LWR EDGE INTERIOR L-ANGLE AND SUPPORT ANGLE ARE CORRODED. CORRECTIVE ACTION: SUMMARY OF NR-00659- REMOVED CORRODED SUPPORT ANGLE AND ATTACH ANGLE FROM AFT CARGO INTERIOR OF DOOR APROX 29 INCHES AFT OF FWD LWR EDGE AND INSTALLED NEW SUPPORT ANGLE & ATTACH ANGLE IAW B-757-200 SRM 51-40. (0102274)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 FUSELAGE / FRAME / STA 1300 AND S-26R / EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 613245-14. (0096518)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 FUSELAGE / FRAME / STA 1300 AND S-26R / EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 613245-14. (0095090)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 #1 ENGINE INTAKE COWL, COMPOSITE MISSING JUST INBOARD OF THE MOUNTING FLANGE @ THE 9 O CLOCK POSITION. CORRECTIVE ACTION: REF ERA 613806-14. (0089286)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 FUSELAGE / FRAME / STA 1640, S-14R / INNER CHORD / CRACKS. CORRECTIVE ACTION: REF ERA 613088-14. (0087928)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 FUSELAGE / FRAME / LHS BSTA 1681 / WL 208 / S-17L & S-18L / CRACK INDICATION. CORRECTIVE ACTION: REF ERA 613012-14. (0084402)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,264 hrs · 41,330 cycles

SHIP 0678 FUSELAGE / FRAME / RHS BSTA 1681 / WL 208 / S-17R & S-18R / CRACK INDICATION. CORRECTIVE ACTION: REF ERA 613080-14. (0084483)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,130 hrs · 41,233 cycles

SHIP 678 3R DOOR NOT ARMED . CORRECTIVE ACTION: ARMED DOOR. NO ISSUE FOUND. OPS NML. (4508476)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,865 hrs · 41,058 cycles

AIRCRAFT 678, LT WING - #3 FLAP TRACK FWD FUSE PIN AND 2EA BUSHINGS ARE CORRODED. CORRECTIVE ACTION: REPLACED #3 LEFT WING FLAP TRACK FWD FUSE PIN AND BUSHINGS. (LP 2887833)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,865 hrs · 41,058 cycles

AIRCRAFT 678, LH OUTBOARD FLAP, OUTBOARD FLAP TRACK, FORWARD FUSE BOLT HAS CORROSION AND BOTH FORWARD INBOARD AND OUTBOARD BUSHINGS ARE CORRODED AND GOUGED. CORRECTIVE ACTION: REPLACED FORWARD FUSE BOLT AND BUSHINGS PER B757 AMM 27-51-03. (LP 2888019)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,865 hrs · 41,058 cycles

AIRCRAFT 678, R/H INBOARD FLAP, OUTBOARD FLAP TRACK, FORWARD FUSE PIN CHROME SURFACE IS CHIPPED AND OUTBOARD BUSHING EVIDENCE OF CORROSION. CORRECTIVE ACTION: REPLACED FUSE PIN AND BUSHING RIGHT WING INBOARD FLAP OUTBOARD TRACK PER B757 AMM 27-51-03. (LP 2887928)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,840 hrs · 41,044 cycles

SHIP 0678 R3 DOOR ARMING LEVER IS DIFFICULT TO ARM AND IS STICKING. CORRECTIVE ACTION: REMOVED DEBRI FROM R3 DOOR MATING SURFACE CYCLED DOOR & ARMING LEVER MULTIPLE TIMES CHECKS NML AT THIS TIME REF B757 AMM 52-11. (4950976)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,619 hrs · 40,922 cycles

SHIP 678 3R DOOR WILL NOT ARM, CORRECTIVE ACTION: ARMED THE 3R DOOR. NTF - OPS NML. (4723750)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,619 hrs · 40,922 cycles

SHIP 678 3R DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR FITTING CHECKED ARMING FUNCTION PER B757 AMM 52-11 (4723752)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,967 hrs · 40,539 cycles

SHIP 678 DOOR 1R HANDLE COVER MISSING. CORRECTIVE ACTION: REPLACED COVER PER B757 AMM 52-11. CK GOOD. (4096640)

Part: NONE — NONE · airframe 89,885 hrs · 40,499 cycles

SHIP 678 EMERGENCY EXIT SIGN IN AISLE KNOCKED DOWN WHILE DEPLANING. CORRECTIVE ACTION: REFASTENED EXIT SIGN PER B757 25-00. (4096608)

Part: DOOR LATCH — UNSERVICEABLE · airframe 89,502 hrs · 40,246 cycles

SHIP 678 R1 DOOR WILL NOT CLOSE FROM INSIDE. CORRECTIVE ACTION: REMOVED & REPLACED UPPER & LOWER AFT LATCH FITTINGS ON R1 DOOR PER B757 AMM 52-11. ADJUSTED R1 DOOR PER B757 AMM 52-11. OPS CK OK. (8923072)

Part: BOLT — LOOSE (R1 GUIDE ARM) · airframe 89,134 hrs · 40,022 cycles

R1 DOOR DIFFICULT TO CLOSE. FOUND R1 DOOR GUIDE ARM BOLT LOOSE, SECURED SAME PER REF B757AMM 52-11-04, R1 DOOR OPS CK'S GOOD.

Part: GIRT BAR — DIRTY (R2 DOOR) · airframe 89,134 hrs · 40,022 cycles

R2 DOOR EMERGENCY SLIDE LIGHT INOP. CLEANED AND LUBED R-2 DOOR GIRT BAR FITTINGS. OPERATIONAL CHK GOOD REF B757 AMM 52-11-25. INSTALLED PNL AFT OF R2 DOOR REF B757 AMM 25-21.

Part: NONE — NONE · airframe 89,030 hrs · 39,938 cycles

SHIP 678 RIGHT FWD DOOR WOULD NOT CLOSE. CORRECTIVE ACTION: REMOVED DEBRIS DOOR OPERATES NORMALY. (9359522)

Part: NONE — NONE · airframe 89,001 hrs · 39,916 cycles

SHIP 678 PRIOR TO PUSH WHILE ARMING THE DOORS, THE AFT LEFT DOOR ARMED LIGHT DID NOT ILLUMINATE. CORRECTIVE ACTION: RESCURED TRIM ON GRIT BAR AT 3L DOOR. PER B757 AMM 52-00. LIGHT OPS CHECK GOOD. (9359502)

Part: NONE — NONE · airframe 88,496 hrs · 39,508 cycles

AIRCRAFT 0678, 2R DOOR ARMED LIGHT FAILS TO ILLUMINATE UNTIL HANDLE IS VERY FIRMLY PUSHED TO CLOSED. CORRECTIVE ACTION: REMOVED DEBRIS AND LUBED GIRT BAR OPS CHK GOOD. PER B757 AMM 12- 21. (9303522)

Part: GIRT BAR — DIRTY · airframe 88,475 hrs · 39,489 cycles

AIRCRAFT 0678, 3R DOOR SLIDE LIGHT DOESN'T ILLUMINATE. CORRECTIVE ACTION: FOUND DEBRIS IN ARMING MECH (SLIDE-GIRT BAR), REMOVED SAME, 3R DOOR ARMS/DISARMS NML. (8862798)

Part: NONE — NONE · airframe 88,189 hrs · 39,336 cycles

SHIP 678 AT R1 DOOR FOUND UPPER ROLLER AFT FRAME FITTINGAND ROLLER DAMAGED. CORRECTIVE ACTION: INSTALLLED NEW ROLLER & BRACKET (LATCH) FITTING OPS CKS GOOD OK FOR SVC IAW B757 IPC 52-11. (8808154)

Part: FLAP — WARNING MESSAGE · airframe 88,105 hrs · 39,281 cycles

SHIP 0678 - MISC/DE - DUE TO T/E FLAP DISAGREE MESSAGE. CORRECTIVE ACTION: BITE ALL 3 FSEUS. NO FAULTS FOUND. RAN FLAPS THROUGH 2 COMPLETE CYCLES. C/W NO-GO PROCEDURES.

Part: NONE — NONE · airframe 87,979 hrs · 39,213 cycles

SHIP 678 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS: 1L. CORRECTIVE ACTION: R&R CONTROL ROD FOR KNUCKLE KNOCKER AND ADJUSTED PER B757 AMM 52 -11. OPS CHK OK. (2197757)

Part: NONE — NONE · airframe 87,238 hrs · 38,774 cycles

SHIP 678 EXIT TRACK LIGHTING AT ROW 2C BROKEN. CORRECTIVE ACTION: REPLACE EMERGENCY SEAT LIGHT REF B757 AMM 33-51. CHECKS GOOD. (6983092)

Part: NONE — NONE · corrosion level 2 · airframe 87,176 hrs · 38,744 cycles

SHIP 678 A.A.- CORROSION ON: HOLE 1 BTW 4-5 HRS FITTING, HOLE 2 BTW 2-3 HRS & 7-9 HRS SKIN/FITTING, HOLE 4 BTW 2-3 HRS SKIN/FITTING, HOLE 6 BTW 11-12 HRS FITTING, HOLE 7 BTW 1-7 HRS SKIN/FITTING AND HOLE 10 BTW 1-5 HRS SKIN/FITTING AT RH ENG DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00319 HOLES WERE REPAIRED PER ER/A 594709-14AD REV: ORIGINAL; SECTION I: PERMANENT REPAIR AND ETI-57-21-489 REV:19. (2015024)

Part: NONE — NONE · airframe 87,176 hrs · 38,744 cycles

SHIP 678 A.A.- CORROSION ON: HOLE 11 BTW 10-5 HRS SKIN/FITTING, HOLE 12 BTW 7-9 HRS SKIN/FITTING AND HOLE 16 BTW 12-3 HRS FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00320: HOLE 11 BTW 10-5 HRS SKIN/FITTING, HOLE 12 BTW 7-9 HRS SKIN/FITTING AND HOLE 16 BTW 12-3 HRS FITTING WERE REPAIRED PER ER/A 594709-14AD REV.ORIGINAL SECTION I PERMANENT REPAIR AND ETI-57-21-489 REV.19 AND DOCUMENTED UNDER NRC 00319. (2015534)

Part: NONE — NONE · airframe 87,176 hrs · 38,744 cycles

SHIP 678 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 594709-14AD. CORRECTIVE ACTION: REF ERA 594709-14AD. (2014311)

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 87,166 hrs · 38,736 cycles

SHIP 678 AD:A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW: HOLE #2 CORROSION ON SKIN AND FITTING BTW 1 TO 4 AND 8 TO 10 OCLOCK POSITION, HOLE #3 CORROSION ON SKIN AND FITTING BTW 9 TO 5 OCLOCK POSITION, HOLE #4 CORROSION ON SKIN AND FITTING BTW 1 TO 11 OCLOCK POSITION, HOLE #5 CORROSION ON SKIN AND FITTING BTW 6 TO 11 OCLOCK POSITION, HOLE #6 CORROSION ON FITTING BTW 5 TO 6 OCLOCK POSITION, HOLE #7 CORROSION ON SKIN AND FITTING BTW 7 TO 10 O? CLOCK POSITION, HOLE #8 CORROSION ON SKIN AND FITTING BTW 2 TO 5 AND 8 TO 11 OCLOCK POSITION, HOLE #9 CORROSION ON FITTING BTW 4 TO 5 OCLOCK POSITION. HOLE #10 CORROSION ON SKIN AND FITTING BTW 1 TO 2 O?CLOCK POSITION, IN REF. CARD. (1990709)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 WORN ON L/E (BTW MFSTA 300 TO 309) AT RH WING OUTBRD MAIN FLAP. CORRECTIVE ACTION: SUMMARY OF NRC 00325 : L/E (BTW MFSTA 300 TO 309) AT RH WING OUTBRD MAIN FLAP. WAS REPAIRED PER ETI-57-21-504 REV. 5 AND ERA 594582-14 REV ORIG. SECTION I PERMANENT REPAIR. (1981253)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 594672-14. CORRECTIVE ACTION: REF ERA 594672-14. (1981260)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 DENT ON TRAILING EDGE WEDGE, BTW OSS 744 TO 747 AT LH WING SLAT #1. (IN REF. NRC 00287). CORRECTIVE ACTION: SUMMARY OF NRC 00361 : TRAILING EDGE WEDGE, BTW OSS 744 TO 747 AT LH WING SLAT #1 WAS REPAIRED PER B757-200 SRM. (1963587)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 OUT OF LIMITS (NEEDLE ON RED ARC) ESCAPE SLIDE BOTTLE DISCHARGER. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00050: L2 SLIDE DOOR WAS REPLACED BY SERVICEABLE PART PER B757-200 AMM 25-66. (1960661)

Part: NONE — NONE · corrosion level 2 · airframe 87,166 hrs · 38,736 cycles

SHIP 678 CORROSION ON FRAME CLIP ANGLE STA.1700 BTW STGR 29R TO 28R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00346: FRAME CLIP ANGLE STA 1700 BTW STGR 29R TO 28R AT AFT CARGO COMPARTMENT WAS REPLACED PER B 757-200 SRM. (1961710)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 AA.AD.INITIAL INSPECTION: L4 DOOR GIRT BAR LEAF SPRINGS DO NOT GET THE MINIMUM ENGAGEMENT DIMENSION IN REF. AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00020: GIRT BAR LEAF SPRINGS WERE REPLACED PER B757-200 SRM AND GIRT BAR WAS REMOVED/INSTALLED AND ADJUSTED PER B757-200 AMM 25-66 AND AMDS. (1957845)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 FOUND DENT ON AFT CARGO DOOR SKIN AT LOWER FWD CORNER. CORRECTIVE ACTION: SUMMARY OF NRC 00337: DENT ON AFT CARGO DOOR SKIN AT LOWER FWD CORNER WAS REPAIRED PER B 757-200 S.R.M.(1956706)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 FOUND DENT ON AFT CARGO DOOR SKIN AT LOWER FWD CORNER. CORRECTIVE ACTION: SUMMARY OF NRC 00337: DENT ON AFT CARGO DOOR SKIN AT LOWER FWD CORNER WAS REPAIRED PER B 757-200 S.R.M.(1956699)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 LOW PRESSURE ON EMERGENCY RESERVOIR AT R2 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00322: R2 EMERGENCY POWER RESERVOIR WAS REMOVED AND SERVICEABLE EMERGENCY POWER RESERVOIR WAS INSTALLED PER B757-200 AMM 52-11. (1954473)

Part: NONE — NONE · airframe 87,166 hrs · 38,736 cycles

SHIP 678 OUT OF LIMITS COMPENSATOR INDICATOR ON SNUBBER AT L2 DOOR. CORRECTIVE ACTION: SNUBBER WAS REMOVED AND REPLACED PER B757-200 AMM 52-11.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 87,162 hrs · 38,735 cycles

SHIP 678 REPLACE 1EA. EMERGENCY LIGHT BATTERY CHARGER IN AFT GALLEY CEILING RH SIDE. CORRECTIVE ACTION: REMOVED AND REPLACED 1EA. EMERGENCY LIGHT BATTERY CHARGER IN AFT GALLEY CEILING RH SIDE IAW B757 AMM 33-51. (7165484)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,624 hrs · 37,594 cycles

DURING S/C, FOUND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. R/R BOTH LT AND RT AFT CABIN (M736 AND M737) EMERGENCY LIGHT BATTERY PACKS IAW B757 AMM 33-51.

Part: SLIDE — FAILED (L2 DOOR) · airframe 84,109 hrs · 37,363 cycles

2L SLIDE RAFT BUSTLE DEPLOYED UPON DOOR OPENING SLIDE RAFT DID NOT INFLATE. SLIDE DID NOT INFLATE DUE TO FALLING ON JETWAY FLOOR RMVD EMERG. POWER RESERVOIR REF B757 M/M 52-11-30. INST POWER RESERVOIR PER B757 M/M 52-11. SLIDE CHANGE RII C/W ON AMDS. (5675766)

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 87,166 hrs · 38,736 cycles

SHIP 678 FOUND DENT ON AFT CARGO DOOR SKIN AT LOWER FWD CORNER. CORRECTIVE ACTION: SUMMARY: AREA ON AFT CARGO DOOR SKIN AT LOWER FWD CORNER WAS REPAIRED PER B757-200 SRM 52-30-01. (3757282)

Part: SKIN — DAMAGED (BS 690) · airframe 83,115 hrs · 36,879 cycles

SHIP 678 WHILE IN ATL FOR INSPECTIONS FROM ER/A 571907-14MA, MAINTENANCE DISCOVERED AN APPROX. 24" X 24" AREA OF THE CROWN SKIN AT STA 690, BETWEEN S-2L AND S-2R WITH PREVIOUS LOCAL BLENDING AT FASTENER LOCATIONS. CORRECTIVE ACTION: REF ERA 572109-14 REV ORG AND REV B. (0777311)

Part: BATTERY — DISCHARGED (CABIN) · airframe 81,983 hrs · 36,347 cycles

EXIT LIGHTS AT OVER WING EXIT LT SIDE OF A/C WILL NOT EXTINGUISHED. REPLACED EMERG LIGHTS BATTERY AND CHARGER PER AMM 33-51 LIGHTS TEST AND OP OK.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 81,695 hrs · 36,245 cycles

EMERGENCY LIGHTS AT SEATS 43 - 45 ONLY ILLUMINATE FOR LESS A MINUTE. REPLACED THE BATTERY PACK AT POWER SUPPLY M9102 IAW AMM 33-51.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 81,482 hrs · 36,156 cycles

DURING PREFLIGHT, ELECTRICAL SMELL IN COCKPIT STRONG ENOUGH TO SMELL IN THE FORWARD GALLEY. SECURED RIGHT PACK, NO SMOKE EVIDENT, SMELL DISSIPATED WITHIN 5 MINUTES. UTILITY BUSSED L/R TRIPPED. CONFIGURED A/C IN EXACT STATE IT WAS IN WHEN SMELL WAS DISCOVERED. PERFORMED DETAILED INSPECTION OF COCKPIT AND E/E COMPARTMENT, INCLUDING EXTERNAL POWER CONTACTOR AREA, NO DEFECTS NOTED. THIS INCLUDES RECIRC AND EQUIPMENT COOLING FANS. PERFORMED NEXT FLIGHT NO GO ODI STEPS WITH NO DEFECTS NOTED. CHECKS OK PER FIM 21-00-01/301.

Part: GIRT BAR — DIRTY (L2 DOOR) · airframe 81,433 hrs · 36,132 cycles

L2 DOOR SLIDE REMAINED ON AFTER DOOR WAS DISARMED. LIGHT WENT OUT AFTER DOOR ARM WAS CYCLED AND SEVERAL MINUTES WENT BY. REMOVED DEBRIS FROM THE GIRT BAR AND CLEANED THE PROX SENSOR, NO DEFECTS FOUND, ARMED AND DISARMED SEVERAL TIMES, OP CHECKED NORMAL IAW AMM 52-11.

Part: WIRE — DAMAGED (SLIDE LIGHT) · airframe 81,433 hrs · 36,132 cycles

L2 DOOR GIRT BAR SLIDE LIGHT WILL NOT EXTINGUISH WHEN DOOR DISARMED. FOUND THE AFT L2 DOOR PROXIMITY SENSOR 510218 MISSING ONE ENVIRONMENT SPLICE SHEATHING. REMOVED & TERMINATED THE WIRE SPLICE IAW WDM 25-66-11, & SWPM 20. THE L2 SLIDE LIGHT EXTINGUISHED.

Part: SKIN — CRACKED (SLAT COVE) · airframe 81,363 hrs · 36,098 cycles

NR 1 SLAT COVE SKIN IS CRACKED AT INBD SIDE OF INBD SLAT TRACK FITTING. REPAIRED THE SLAT COVE SKIN AT OSS 736.70 IAW ER/A 556511-14, REV, ORIGINAL.

Part: SKIN — DEBONDED (NR 8 SLAT) · airframe 81,363 hrs · 36,098 cycles

RIGHT NR 8 SLAT T/E WEDGE UPPER SURFACE METAL BOND REPAIR 58 INCHES FROM INBD END IS DEBONDED. REPAIRED THE SKIN IAW B757 57-43-02, REPAIR 1, AND SRM 51-70-10, REPAIR 3 & 4.

Part: CONNECTOR — BROKEN (SLIDE BOTTLE) · airframe 81,363 hrs · 36,098 cycles

AFT CARGO FWD BULKHEAD, RT OVERWING INFLATION BOTTLE PRESSURE INDICATOR CONNECTOR BACK SHELL BROKEN. REMOVED AND REPLACED THE CONNECTOR D5542 IAW WDM 25-65-21, AND SWPM 20-61-00. PERFORMED OPS CHECK IAW AMDS 2565-4646, STEP 8.

Part: PIN — LOOSE (SNUBBER) · airframe 81,352 hrs · 36,094 cycles

DURING INSPECTION, L4 DOOR ROTARY SNUBBER, FOUND COMPENSATOR EXTINSION PIN LOOSE IN SNUBBER BODY. REMOVED AND REPLACED THE SNUBBER.

Part: SKIN — DENTED (BS 460) · airframe 81,352 hrs · 36,094 cycles

MULTIPLE DENTS FOUND AT BS 460, BETWEEN STRINGERS 22L - 24L. FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM. REPAIRED THE SKIN IAW ERA 556498-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1640) · airframe 81,352 hrs · 36,094 cycles

BS 1640 FRAME FOWARD BEND RADIUS IS CRACKED APPROXIMATELY .5 INCHES IN LENGH, STRINGER 14L. REPAIRED THE FRAME IAW ERA 556495-14AD, REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (BS 1620-1640) · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN INTERCOSTAL CRACKED AT THE FWD EDGE BETWEEN BS 1640 - 1620, STRINGER 12L. FABRICATED A NEW INTERCOSTAL IAW DWG REV C.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 81,352 hrs · 36,094 cycles

LEADING EDGE COMPOSITE GOUGED, APPROXIMATELY 60 INCHES LONG, ON THE LT INBD MAIN FLAP. REPAIRED IAW ER/A 482402-14MA.

Part: SHEAR TIE — CORRODED (BS 1520) · corrosion level 2 · airframe 81,352 hrs · 36,094 cycles

BULK CARGO BAY, CORROSION FOUND ON THE UPPER SURFACE OF SHEAR TIE, BS 1520, BETWEEN STRINGERS 28L AND 29L. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED A REPAIR IAW SRM.

Part: WEDGE — DEBONDED (NR 8 SLAT) · airframe 81,352 hrs · 36,094 cycles

RIGHT NR 8 SLAT T/E WEDGE UPPER SURFACE METAL BOND REPAIR 31 INCHES FROM INBD END IS DEBONDED. REMOVED A 2 INCH DIA CORE AND ACCOMPLISHED PERMANENT REPAIR BONDED DOUBLER 5 INCHES IN DIAMETER AND CORE PLUG IAW SRM 57-43-02, REPAIR 1, AND SRM 51-70-10 REPAIR 3 AND 4.

Part: WEDGE — DEBONDED (RT NR 8 SLAT) · airframe 81,352 hrs · 36,094 cycles

RIGHT NR 8 SLAT T/E WEDGE UPPER SURFACE METAL BOND REPAIR 58 INCHES FROM INBD END IS DEBONDED. REMOVED A 2INCH DIAMETER CORE AND ACCOMPLISHED PERMANENT REPAIR BONDED DOUBLER 5 INCH DIA AND CORE PLUG IAW 57-43-02, REPAIR 1, AND SRM 51-70-10, REPAIR 3, & 4.

Part: SEAT TRACK — DAMAGED (BS 365-440) · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN SEAT TRACK FLAGES BETWEEN BS 365 - 440, RBL 24 HAS ELONGATED HOLES. REMOVED AND REPLACED THE SEAT TRACK IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 333-345) · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN BS 333 - 345, LBL 58 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED, FABRICATED AND INSTALL A REPAIR IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1667-1672) · corrosion level 2 · airframe 81,352 hrs · 36,094 cycles

CORROSION ON TOP AT BS 1667 - 1672 INCLUDING NUTPLATES AND LOWER SURFACE ON LBL 54 FLOOR SUPPORT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 365-377) · corrosion level 2 · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN, FLOOR SUPPORT BETWEEN BS 365 - 377, LBL 58 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141N5170, REV C.

Part: FLOOR SUPPORT — CRACKED (BS 345-365) · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN, FLOOR SUPPORT BETWEEN BS 345 - 365, RBL 24 CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141N5160, REV E.

Part: FLOOR SUPPORT — CORRODED (BS 345-365) · corrosion level 2 · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN BS 345 - 365, LBL 58 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM AND DWG.

Part: SEAT TRACK — DAMAGED (BS 365-440) · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN, BETWEEN BS 365 - 440, RBL 44, THE SEAT TRACK FLANGES HAD ELONGATED HOLES. FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 345-365) · airframe 81,352 hrs · 36,094 cycles

MAIN CABIN, FLOOR SUPPORT BETWEEN BS 345 - 365, RBL 44 CRACKED. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM.

Part: SEAL — LOOSE (R1 DOOR) · airframe 80,927 hrs · 35,937 cycles

R1 DOOR WILL NOT ARM. FOUND MUD FLAP SEAL LOOSE AT CORNER AND CAUGHT IN GIRT BAR FITTING. SECURED THE SEAL.

Part: ADC — MALFUNCTIONED (RIGHT) · airframe 80,123 hrs · 35,669 cycles

DURING CLIMB OUT, ALTITUDE DISAGREE EICAS MESSAGE AT FL 280, CAPTAIN`S ALTIMETER 28,000 FT, STANBY ALTIMETER 27, 920 FT, AND FIRST OFFICER`S ALTIMETER 27, 680 FT. CTR NR 1 AUTOPILOT, ATC SHOWED FL 280 EXACTLY. TROUBLESHOT IAW FIM. REPLACED THE RT ADC. OPS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 78,240 hrs · 34,996 cycles

EMERGENCY LIGHT INOP AT 39D. WIRE BROKEN UNDER SEAT. REPAIRED BROKEN WIRE REF SWPM CH 20. OP'S CK NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,632 hrs · 34,659 cycles

CORROSION WAS FOUND AT THE AFT LAVATORY SERVICE PANEL AT APPROXIMATELY STA 1681, S-26R TO S-29R. CORROSION WAS FOUND ON THE SKIN COMMON TO THE AREA UNDERNEATH THE LAVATORY SERVICE PAN ON THE FORWARD EDGE OF THE CUTOUT. REFERENCE ERA 552662-14 REV B FOR REPAIR.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 77,632 hrs · 34,659 cycles

ON WALK AROUND FOUND CORROSION ON LEADING EDGE OF AFT LAV SERVICE PAN WITH FASTENERS PULLING THRU. COMPLETED REPAIR PER ERA 552662-14 REV B AND LOG 2773654.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 77,601 hrs · 34,632 cycles

EMER LIGHTS INOP AT ROWS 1 C/D AND 19 DEF. RESEATED CONNECTOR AT LAMINATOR SEATS 1 CD AND 19DEF. LIGHTS CK OK REF AMM 33-50.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 76,850 hrs · 34,209 cycles

EMERGENCY EXIT COVER DIFFUSER LENS MISSING. REINSTALLED EMERGENCY EXIT COVER IAW AMM. (2611239)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 75,581 hrs · 33,732 cycles

EMERGENCY EXIT SEAT LIGHT ROW 5 RT INOPERATIVE. WIRE ON BACK SIDE OF LIGHT SOCKET HANGING LOOSE. REPLACED LIGHT AND HARNESS, EMERGENCY LIGHT AT 5CD, OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 74,912 hrs · 33,469 cycles

EMERGENCY LIGHT ON SEAT 38 EFG INOPERATIVE. FOUND BROKEN WIRE ON SEAT DISCONNECT. REPAIRED WIRE IAW SWPM 20-10-13. LIGHT TESTS GOOD IAW AMM 33-51-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 72,237 hrs · 32,300 cycles

SEAT 40C EMERGENCY LIGHT INOPERATIVE. FOUND A DAMAGED WIRE AT UNDER SEAT HARNESS CONNECTOR. REPAIRED IAW SWPM 20-30-12. OPS CHECKED OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 72,201 hrs · 32,282 cycles

SEAT 4C, 4D EMERGENCY LIGHT WIRE BROKEN. REPLACED EMERGENCY LIGHT SEAT HARNESS, OPS NORMAL IAW AMM 33-50.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 69,987 hrs · 31,304 cycles

ROW 1R 2R EMERGENCY LIGHTS INOPERATIVE. TERMINATED WIRES AT CONNECTORS. OPS CHECKED GOOD.

Part: SKIN — GOUGED (BS 1660-1668) · airframe 69,842 hrs · 31,247 cycles

FUSELAGE SKIN, BS 1660-1668, S1- 2L GOUGED.

Part: SKIN — DAMAGED (BS 1323) · airframe 69,851 hrs · 31,250 cycles

FUSELAGE SKIN BS 1323, S4R, LAP SPLICE HAS A LIGHTNING STRIKE.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 69,522 hrs · 31,116 cycles

RT CREASE BEAM, BS 1020-1040 FOUND CORRODED. REPAIRED IAW ERA 524030-14.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 68,580 hrs · 30,725 cycles

EMERGENCY LIGHTS INOPERATIVE FROM 37D AFT. FOUND FUSE BLOWN AT POWER SUPPLY M9002. REPLACED FUSE.

Part: LIGHT — INOPERATIVE (SEAT 34 FED) · airframe 67,153 hrs · 30,178 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 34 FED. R & R EMERGENCY LIGHT ASSY OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,078 hrs · 30,146 cycles

DOOR 2R EXTERIOR EMERGENCY LIGHT OUT. REPLACED POWER SUPPLY ASSY IAW AMM 33-51-07.

Part: SKIN — GOUGED (BS1660-68 S1L-2L) · airframe 63,683 hrs · 28,681 cycles

UPON REMOVING DORSAL FIN ANGLE FOUND DEEP GOUGE IN THE SKIN. REPAIRED PER ERA 501934-14 REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON FUSELAGE SKIN SEAM AT STA 1335, STR 4R. REPAIRED PER ERA 499403-14 REV ORIG.

Part: FITTING — CRACKED (NLG WW) · airframe 63,683 hrs · 28,681 cycles

NOSE LANDING GEAR OVER CENTER LINK SUPPORT FITTING CRACKED. REPLACED IAW ERA 499399-14 REV ORIGINAL.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

RIGHT AFT OF KEEL BEAM STRUCTURE ATTACHED ANGLE CRACKED BS 1180. REMOVED AND REPLACED RT AFT KEEL BEAM ATTACH ANGLE IAW BAC DWG 149N7528 AND B757 SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

LEFT AFT OF KEEL BEAM STRUCTURE ATTACHED ANGLE CRACKED BS 1180. REMOVED AND REPLACED LEFT AFT KEEL BEAM ATTACHED ANGLE IAW BAC DWG 149N7238 REV AA AND B757 SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON SKIN SEAM AT STA 1264 STR 4R. REPAIRED IAW ERA 499400-14 REV ORIGINAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

DURING INSTALLATION OF AN INTERCOSTAL AT STA 1545 BETWEEN STR 26L AND STR 27L A DENT WAS FOUND ON THE SKIN. REPAIRED IAW ERA 499412-14 REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON FUSELAGE SKIN SEAM AT STA 1297 STR 4R. REPAIRED IAW ERA 499402-14 REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON UPPER FUSELAGE SKIN STA 885 AND STR 3R. REPAIRED IAW B757 SRM 51-40-02 FIG 5 AND 53-00-01 FIG 201.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

AFT PIT STRINGER CORRODED AT STA 1464 STR 28R. REPLACED SECTION IAW B757 SRM 53-00-03.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON EXTERNAL FUSELAGE SKIN AT STA 940- STA 960 AT STR 3R. REPAIRED IAW ERA 499405-14 REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON UPPER FUSELAGE SKIN STA 393 STR 8R. REPAIRED IAW ERA 499407-14 REV ORIGINAL.

Part: TRANS PANEL — CORRODED (CARGO BAY) · airframe 63,683 hrs · 28,681 cycles

AFT BAG PIT RT TRANSITION PANEL CORRODED STA 1380-1440- PANEL CHORD CORRODED. REPLACED TRANSITION PANEL AND INBOARD CHORD- LOCATED AND DRILLED TRANSITION PANEL AND INBOARD CHORD IAW B757 SRM 51-40-05.

Part: FRAME — CORRODED (BS 1480 S25-27L) · airframe 63,683 hrs · 28,681 cycles

BULK CARGO COMPARTMENT FRAME CORRODED BS 1480, STR 25-27L. REPAIRED FRAME IAW SRM 53-00-07 FIG 201.

Part: FRAME — DENTED (BS 1520 S25-27L) · airframe 63,683 hrs · 28,681 cycles

CARGO FRAME DENTED BS 1520 STR 25 - 27L. REPAIRED IAW SRM 53-00-07 FIG 201 DETAIL 3.

Part: FRAME — BENT (BS 620 S26-27L) · airframe 63,683 hrs · 28,681 cycles

FORWARD CARGO BAY FRAME BENT BS 620 STR 26L-27L. REPAIRED IAW SRM 53-00-07 FIG 201.

Part: FRAME — DENTED (BS 1560 S26L) · airframe 63,683 hrs · 28,681 cycles

CARGO BAY FRAME DENTED BS 1560 STR 26L. FRAME REPAIRED IAW SRM 53-00-07 FIG 201.

Part: FRAME — DENTED (BS 1580 S25-26R) · airframe 63,683 hrs · 28,681 cycles

CARGO BAY FRAME DENTED FS 1580 STR 25 - 26R. REPAIRED IAW SRM 53-00-07 FIG 201.

Part: FRAME — DENTED (BS 1500 S23-24L) · airframe 63,683 hrs · 28,681 cycles

CARGO BAY FRAME DENTED BS 1500, STR 23-24L. REPAIRED IAW SRM 53-00-07 FIG 201 DETAIL 3.

Part: SKIN — DAMAGED (BS 393 S8R) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON UPPER FUSELAGE SKIN BS 393 8R. REPAIRED IAW ERA 499407-14.

Part: FRAME — DENTED (BS 1520) · airframe 63,683 hrs · 28,681 cycles

BULK CARGO FRAME DENTED BS 1520 STR 25L-STR 27L. REPAIRED IAW B757 SRM 53-00-07.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 63,683 hrs · 28,681 cycles

NR 1 PYLON DIAGONAL BRACE WING SIDE I/B BUSHING MIGRATED. REMOVED AND INSTALLED NEW 2 EA BUSHINGS IAW BAC DWG 112N2011 REV B AND ERA 499397-14AD REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON SKIN SEAM AT STA 1335 STR 4R- REPAIR REF 53-00-01. THIS IS A DISCOVERY- FINAL REPAIR TO BE DETERMINED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON SKIN SEAM AT STA 1297 STR 4R REPAIR REFERENCE 53-00-01. THIS IS A DISCOVERY- FINAL REPAIR TO BE DETERMINED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON SKIN SEAM AT STA 1264 STR 4R REF SRM 53-00-01 FOR REPAIR. THIS IS A DISCOVERY- FINAL REPAIR TO BE DETERMINED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON EXTERNAL FUSELAGE SKIN AT STA 947 AND STR 3R DISCOVERY- REPAIR TO BE DETERMINED REF: SRM 53-00-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

STATIC DISCHARGE ON EXTERNAL SKIN AT STA 1025 BETWEEN STR 3R AND 4R DISCOVERY- FINAL REPAIR TO BE DETERMINED REF: SRM 53-00-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

WEB CRACKED AT AFT RADIUS LOCATED STA 660-680 STR 12L FWD OF L-2 DOOR. REPLACED IAW BAC 143N8334 AND SRM 51-10-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

WEB CRACKED AT AFT RADIUS LOCATED 660-680 STR 11R FWD OF R-2 DOOR. REPLACED IAW BAC 143N8334 AND SRM 51-10-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

WEB CRACKED AT AFT RADIUS LOCATED STA 660-680 STR 11L FWD OF L-2 DOOR. REPLACED IAW BAC 143N8334 AND SRM 51-10-02.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,683 hrs · 28,681 cycles

WEB CRACKED AT AFT RADIUS LOCATED 660-680 STR 12R FWD OF R-2 DOOR. REPLACED IAW BAC 143N8334 AND SRM 51-10-02.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 63,595 hrs · 28,635 cycles

LINE MAINTENANCE FOUND 1L DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY, OPERATION NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 61,272 hrs · 27,716 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE FIRST CLASS EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 58,229 hrs · 26,363 cycles

FIRST CLASS SEAT-MOUNTED EMERGENCY LIGHTS AND MID CABIN DOOR EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED M9101 POWER SUPPLY AND DEFERRED DAMAGED WIRE AT SEAT 3CD IAW MEL 33-51-03. MCO MX REPAIRED BROKEN WIRE BENEATH SEAT AND REPLACED M9101 POWER SUPPLY.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 58,187 hrs · 26,345 cycles

FUSELAGE FS 1410 KEEL CHORD CORROSION. REPAIRED IAW ERA 482205-14.

Part: SKIN SPLICE — CORRODED (FUSELAGE) · airframe 58,181 hrs · 26,341 cycles

CORROSION FOUND AT SKIN SPLICE AT STA 1401 FROM STR 27 LEFT TO 27 RIGHT. REPAIRED PER ERA.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 57,894 hrs · 26,184 cycles

EMERGENCY LIGHT AT ROW 6C INOP. REPAIRED WIRES AND REPLACED LIGHT ASSY AT 6C, CKS GOOD.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 48,873 hrs · 21,923 cycles

FUSELAGE SKIN SKY RADIO ANTENNA. REPAIRED IAW ERA 453879-14.

Part: SKIN — DENTED (BS 570-605 S-27L) · airframe 44,917 hrs · 20,480 cycles

THE FUSELAGE SKIN WAS STRUCK BY GSE AND SUFFERED DENTS AND GOUGES BETWEEN STR 27L AND 27R AT BS 570 - 605. THE DAMAGED SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED PER ER/A 452483-14.

Part: WINDOW — BROKEN (CABIN) · airframe 37,252 hrs · 17,732 cycles

A/C ARRIVED WITH P/R WINDOW AT 45A CRACKED. ON INSPECTION FOUND UPPER HALF OF OUTER PANE MISSING,AND SEVERAL SMALLER PIECES HELD IN THE SEAL. REPLACED WINDOW.

Part: ODOR — DETECTED (A/C DUCTING) · airframe 35,501 hrs · 16,977 cycles

ODOR IN COCKPIT COMING FROM OVERHEAD AIR CONDITIONING DUCT. FOUND TO BE RIGHT RECIRCULATION FAN THE CAUSE. DEACTIVATED FAN AND FWD TO MCO/PLAC PER MEL 21-25-01A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,545 hrs · 16,513 cycles

SEVERAL AFT EMERG LIGHTS INOP IN AFT CABIN. REPLACED MODULE 737 BATTERY PACK. CKS OK.

Part: BATTERY — SHORTED (E/E BAY) · airframe 33,338 hrs · 15,924 cycles

FLT CREW REPORTED VISIBLE SMOKE IN AFT GALLEY WHILE AT GATE PRIOR TO BOARDING. CONTRACT MTC FOUND APU BATTERY SHORTED AND THE SOURCE OF SMELL/SMOKE. REPLACE THE APU BATTERY. THE BATTERY CHARGER AND THE K117 START CONTACTOR.

Part: ENGINE — FAILED (NR 2 ENGINE) · airframe 29,582 hrs · 14,152 cycles

AT CRUISE FLT LVL 390 NUMBER 2 ENGINE COMPRESSOR STALLED AND SHUT DOWN. REPLACED NUMBER 2 ENGINE.

Part: FAN — OVERHEATED (CABIN) · airframe 29,239 hrs · 14,009 cycles

ELECTRICAL SMELL IN COCKPIT. MTC ISOLATED PACKS AND FANS AND DETERMINED RT RECIRC FAN TO BE THE SOURCE OF ODOR. PULLED AND COLLARD C/BS FOR RT RECIRC FAN AT P37 PNL-CBS J5 AND D7. FWD MCO AND PLAC PER MEL 21-25-01A. RT RECIRC FAN SELECTED OFF.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,092 hrs · 13,937 cycles

FIRST CLASS ESCAPE PATH LIGHTING INOP. REPLACED THE POWER SUPPLY AND BATTERY PACK. CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,469 hrs · 13,662 cycles

FOUND DURING LAYOVER CHK ON 11/03/00, EMERGENCY PATH LIGHTS IN FIRST CLASS ROWS 1 THROUGH 6 SIDE SEATS INOP. REPLACED E-PATH BATTERY PACK SLED-POWER SUPPLY PER MM. OPS CHECK NORMAL.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 27,587 hrs · 13,245 cycles

DURING LEFT ENG START GROUND CREW REPORTED ENGINE FIRE. ABORTED ENG START AND RETURNED TO GATE. F/F ON START 1.4. REPLACED LEFT EEC PER FIM, RAN ENG CHECKS OK.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 27,390 hrs · 13,152 cycles

THE FUSELAGE SKIN WAS FOUND WRINKLED BETWEEN FS 395 AND FS 418 JUST ABOVE STRINGER 20R. THE SKIN WAS CUT OUT IN THE AREA TO REMOVE THE WRINKLES AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. INSTALLED PER ER/A 363903-14, REV C.

Part: POWER SUPPLY — INOP (SEAT 3C)

ON CABIN MAINTENANCE VISIT 2525, FOUND FIRST CLASS SEAT EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY AND BATTERY PACK. ALSO, REPAIRED SEAT LIGHT AT 3C.

Part: SEQUENCE VALVE — FAILED (RT MLG DOOR)

GEAR DOORS LIGHT REMAINED ON DURING GEAR EXTENSION. GEAR DOOR FOUND DOWN UPON ARRIVAL AT GATE, WITH DOOR LIGHT ON IN COCKPIT. DUE TO HISTORY, REPLACED RT MLG DOOR AND OPERATED GEAR SEQUENCE VALVE.

Part: SEQUENCE VALVE — FAILED (RT MLG DOOR)

EICAS MSG GEAR DOORS OPEN LIGHT. DOORS LIGHT STAYED ON. RT MAIN GEAR DOOR OPEN AFTER BLOCK IN. REPEAT W/U. REPLD DOOR DOWNLOCK SEQUENCING VALVE AND DOOR DOWN LOCK MODULE. OPN SYS NO LEAKS AND DOOR OPN NRML.