N718TW

Part: SKIN — DENTED (ZONE 200) · airframe 90,488 hrs · 23,331 cycles

ON ARRIVAL, RAMP REPORTED DENT 32.5 INCHES AFT OF L2 DOOR. DAMAGE EVALUATED & MEASUREMENTS SENT TO ENGINEERING. SIDEWALL PANELS 19A & 20A REMOVED FOR EXCESS 785626. REINSTALLED SIDEWALL PNLS 19A & 20A 715532. C/W SECTIOIN 1 FERRY FLT PREP PER ER/A 630409-14 REV A 785626. REPAIRED DENT PER ER/A 630449-14 REV ORIGIINAL ON N/R LOG 1299616. (7676587)

Part: SKIN — DENTED (ZONE 200) · airframe 90,488 hrs · 23,331 cycles

ER/A 630449-14 REV ORIGINAL: FUSELAGE SKIN, BS 760, S14L - S15L, DENTED AND GOUGED. REPAIRED IAW ERA 630449-14. (1298266)

Part: HINGE — DAMAGED (ZONE 800) · airframe 89,822 hrs · 23,181 cycles

L4 DOOR WILL NOT OPEN. FOUND LOWER HINGE SERRATED PLATE SEPERATED FROM A/C. REMOVED SLIDE PER W/C 2566-9001-4L TO GAIN ACCESS. REPLACED LOWER GUIDE ARM BOLTS AND RIGGED DOOR PER B757 AMM 52-11. SLIDE REMOVED REINSTALLED ON LOG 7774081. DOOR OPS NRML PER B757 AMM 52-11. (7774079)

Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 89,623 hrs · 23,135 cycles

L1 DOOR. KNUCKLE KNOCKER NOT FULLY IN ARMED POSITION WHEN DOOR CLOSED. ADJUSTED DOOR KNUCKLE KNOCKER AT 1L. 1L DOOR OPS NORMAL PER B757 -200ER AMM 52-11. (7774015)

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 89,472 hrs · 23,097 cycles

DURING SVC CHECK, FOUND EMERGENCY LIGHT BETWEEN ROW 2735 INOP. REMOVED AND REPLACED BATTERY CHARGER AT ROW 35, ALL WORK PER B757 AMM 2433. FOUND BROKEN WIRE AT CONNECTOR D9353, REPAIRED SAME PER SWPM 20 IAW B757 WDM 33-51-14 EMER LTS OPS NORMAL.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 87,680 hrs · 22,560 cycles

SHIP 6815 DOOR 2L WILL NOT OPEN FOR DEPLANING. CORRECTIVE ACTION: FOUND SLIDE ASSY HARNESS HAD LOOSENED & SLIDE BUSTLE DROPPED DOWN IMPEADING DOOR OPERATION. SECURED SLIDE BUSTLE PER B757 AMM 25-66. DOOR OPERATES NORMAL. (6942150)

Part: SKIN — NOT REPORTED · airframe 87,641 hrs · 22,545 cycles

SHIP 6815 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 623325-14AD. CORRECTIVE ACTION: REF ERA 623325-14AD. (0756584)

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 87,641 hrs · 22,545 cycles

SHIP 6815 LONGITUDINAL FLOOR BEAM ANGLE AT STA 1640, WL 208, BL 0 WITH CRACK ON PREVIOUS REPAIR. CORRECTIVE ACTION: REMOVED AND REPLACED LONGITUDINAL FLOOR BEAM CLIPS AT STA 1640, WL 208 BL0 IAW B737 SRM 51-40-02-0G AND BOEING DWG 146N5180 REV C. (0753638)

Part: SKIN — DENTED (ZONE 800) · airframe 87,641 hrs · 22,545 cycles

SHIP 6815 DENT ON AFT CARGO DOOR SKIN, 14 INCHES FROM FWD EDGE, 7 INCHES FROM BOTTOM EDGE. CORRECTIVE ACTION: FOUND TO BE OUT OF LIMITS DUE TO GOUGE IN DENT IAW B757 SRM 52-30-01-1A-1 DETAIL G. REMOVED DENT AND REPAIRED IAW B757 SRM 52-30-01-2R-4. REPAIR IS CAT B. (0753592)

Part: SKIN — DENTED (ZONE 800) · airframe 87,641 hrs · 22,545 cycles

SHIP 6815 DENT ON AFT CARGO DOOR SKIN, 14 INCHES FROM FWD EDGE, 7 INCHES FROM BOTTOM EDGE. CORRECTIVE ACTION: FOUND TO BE OUT OF LIMITS DUE TO GOUGE IN DENT IAW B757 SRM 52-30-01-1A-1 DETAIL G. REMOVED DENT AND REPAIRED IAW B757 SRM 52-30-01-2R-4. REPAIR IS CAT B. (0753589)

Part: SKIN — CRACKED (ZONE 500) · airframe 87,641 hrs · 22,545 cycles

SHIP 6815 WORKING AMDS 5720-01100-05A, LH WING STEP,14 HOLE 13 HAS CRACK INDICATION RADIATING FROM THE 7 O'CLOCK FROM FWD. INDICATION REMAINS AFTER 1ST OVERSIZE CUT TO 0.577. CORRECTIVE ACTION: ENSURED SUSCEPTIBLE AREAS ARE PROTECTED PER AMM 20-60. COMPLETED TABLE 1 AND 2 COLUMNS A AND B PER ATS PER 24-03215 REV P1. INSPECTED HOLE 13 PER PER 24 -03125 REV P1 AND 757 NTM PART 6 51-00-16. CRACK INDICATION AT 7 O'CLOCK. PROVIDED RESULTS WC 5720-01100-2A AND 3A TO ATS ENGINEERING. REAMED HOLE#13 INSPECTED HOLE 13 PER 757 NTM PART 6, 51-00-16. HFEC SHOWS CRACK INDICATION REMAINS AT 7 O'CLOCK IN TOP SHEET HALFWAY TO THE SHIM LAYER. REAMED HOLE 13 TO .6089. PERFORMED INSPECTION OF HOLE 13 PER 757 NTM PART 6 51-00-016. NO CRACK INDICATION FOUND. COMPLIED WITH ATS PER 24-03215 REV P2 PART 2 BLOCK 1. COMPLIED WITH PART 2 BLOCK 2. COMPLIED WITH PART 2 BLOCK 3.COMPLIED WITH PART 2 BLOCKS 4, 5 AND 6. COMPLIED WITH ATS PER 24-03215 REVS P1 AND P2.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 87,635 hrs · 22,543 cycles

SHIP 6815 CABIN BULLNOSE EMERGENCY LIGHT INOP AT 4AB. CORRECTIVE ACTION: REPLACED M733 EMERGENCY LIGHTS POWER SUPPLY ABOVE L2 DOOR PER B757 AMM 33-51 - EMERGENCY LIGHTS NOW TEST NORMAL. (6942107)

Part: TRANSMITTER — FALSE INDICATION (SLAT SYSTEM) · airframe 85,763 hrs · 22,046 cycles

SHIP 6815 -ATB/FCNT/DE- DUE TO L/E SLAT ASYMMETRY MESSAGE. CORRECTIVE ACTION: REPLACED RIGHT LEADING EDGE SLAT POSITION TRANSMITTER.

Part: SKIN — DAMAGED (UNKNOWN) · airframe 85,250 hrs · 21,922 cycles

SHIP 6815 DURING BHEC INSPECTION FASTENER HOLES PER STEP 12 OF WORKCARD, FOUND 1 EA. FASTENER HOLE UNINSPECTABLE DUE TO PLUG AND TOOLING DAMAGE ADJACENT TO FASTENER HOLE. CORRECTIVE ACTION: REF ERA 616745-14. (0260182)

Part: SKIN — NOT REPORTED (BS 1400 S2R) · airframe 85,250 hrs · 21,922 cycles

SHIP 6815 DTE, ER/A 616745-14 - SECTION I REPAIR / FUSELAGE / CROWN SKIN / STA 1400 / STR S-2R / TEAR STRAP PLUG. CORRECTIVE ACTION: REF ERA 616745-14. (0258849)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,243 hrs · 21,677 cycles

SHIP 6815 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. FELL OFF DURING TAKEOFF / INTERIOR. CORRECTIVE ACTION: SECURED LENS OF EXIT SIGN. (0085945)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,207 hrs · 21,668 cycles

SHIP 6815 AT DEPARTURE L4 DOOR WOULD NOT ARM. CORRECTIVE ACTION: ADJUSTED CHORD. DOOR ARMING CKS OK PER B757 AMM 25-66. (4360110)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,101 hrs · 21,637 cycles

SHIP 6815 4R DOOR WON'T ARM AT DEPARTURE. CORRECTIVE ACTION: AFTER DEBRIS REMOVAL, OPS CK NML. (4306786)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,101 hrs · 21,637 cycles

SHIP 6815 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. CORRECTIVE ACTION: RESECURED COVER. (0066381)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,995 hrs · 21,608 cycles

SHIP 6815 2L DOOR FAILS TO TRACK PROPERLY DURING CLOSING PREVENTING THE ARM SLIDE LEVER TO MOVE ALL THE WAY TO THE ARM POSITION. CORRECTIVE ACTION: 2L DOOR SLIDE ARM LEVER OPERATES NORMALLY. SLIDE GIRT BAR ENGAGEMENT LIGHT. (4306746)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,995 hrs · 21,608 cycles

SHIP 6815 2L ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR AREA AND LUBE PER B757- AMM 52-11. OPS CHECK NORMAL. DOOR ARMED AND DISARMED OK. (4306749)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,833 hrs · 21,573 cycles

SHIP 6815 1R DOOR ARMED LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED 1R DOOR ARMED LIGHT REF B757 AMM 33-21 OPS CHK NORMAL. OK FOR SERVICE. (5155786)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,767 hrs · 21,559 cycles

SHIP 6815 CREW REPORTS L 1 DOOR KNUCKLE KNOCKER INOPERATIVE. CORRECTIVE ACTION: OPS CHK L1 DOOR REF B757 AMM 52-11, OPS CHK NML, KNUCKLE KNOCKER WORKING AS INTENDED. (5155762)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,684 hrs · 21,542 cycles

SHIP 6815 4L DOOR COULD NOT ARM AT DEPT. CORRECTIVE ACTION: CLEANED DEBRIS ON 4L DOOR ARMED DOOR IAW B757 AMM 52-11. (5155730)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,584 hrs · 21,520 cycles

SHIP 6815 DOOR 4L WONT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR AREA. RESET DOOR. PERFORMED 4L DOOR ARM PROCEDURE. OPS CK OK PER B757 AMM 52-11. (5365098)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,756 hrs · 21,322 cycles

SHIP 6815 36D EMERGENCY LIGHT FELL OFF (DAMAGED). CORRECTIVE ACTION: RESECURED LIGHT ASSY TO SEAT TRIM. LIGHT CHKS OKAY. (4837792)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,356 hrs · 21,236 cycles

SHIP 6815 4L DOOR DID NOT ARM ON DEPARTURE. CORRECTIVE ACTION: INSPECTED GRIT BAR AND REMOVED FOD PER B757 AMM 25-66. DOOR ARMS GOOD. (4797356)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,064 hrs · 21,169 cycles

SHIP 6815 4L DOOR WOULD NOT ARM. CORRECTIVE ACTION: SECURED ROPE AND OPS NML PER B757 AMM 52-11. (4644356)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,974 hrs · 21,144 cycles

SHIP 5815 L2 DOOR WILL NOT CLOSE WITH PROPER EQUIPAGE INSTALLED. CORRECTIVE ACTION: SECURED DOOR L2 SLIDE COVER PER B757 AMM 52-11. CHKD OK. (4644312)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 DURING LIGHTNING STRIKE INSP FOUND DMG AFTER BLEND OUT LWR FUSELAGE 1.25 DIAMETER & 0.030 DIMETER AT FUSELAGE STA 535 & STRINGER L-28. CORRECTIVE ACTION: FOR 3 REMOVED RIVITS REQUIRE BHEC INSP AT STA 540 ST 28-L PER SRM REPAIR 53-00-01-2R-28. PREFORMED BHEC INSP PER B757-200 NDT PART 6 51-00-16 NO CRACKS INDICATION FOUND. PREFORMED STEPS 3,4,5 OF R.I 606946-14 NO FINDING NOTED SENT INFO TO ENGINEERING. CUTOUT COMPLETE AND ALL PICKUP HOLES ON DAMAGE STA 520 TO STA 540 STR 27-L TO BUTTLINE REG HFEC PER B757 SRM 53-00-01-2R-28 STEP 2E. PREFORMED HFEC ON STA 520 TO 540 STR CUTOUT PER 51-00-19 NO DAMAGE FOUND. FABRICATION DOUBLER AND FILLER AS LER R.I 606946-14. INSTALL SRM REPAIR 28 PER B757-200 SRM 53-00-01 REPAIR 28 REF RI 606946-14. (4785536)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,566 hrs · 21,051 cycles

SHIP 6815 2 LIGHTING STRIKES LOCATION AT FUSELAGE STA 418 STR L-28. CORRECTIVE ACTION: BLENDED AND REPAIRED AREA PER B757 SRM 53-00-01. (2673075)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,566 hrs · 21,051 cycles

SHIP 6815 DUE TO LIGHTEN STRIKE INSP FOUND DAMAGE AFTER BLENDING AT STA 535 AND STL 28-L. CORRECTIVE ACTION: C/W UT THINKNESS INSP PER B757-200 NDT PART 4 51-00-10. WORKING R.I 606946-14 FOUND 2 SMALL RIVITS IN BLEND C/W STEPS 3,4,5 ON RI INFO SENT TO ENGINEERING NO CRACK INMOTION POST NEW BLEND REF TO LOG 4785536 (QC2000) SEE LOG 4785536 FOR CORRECTIVE ACTION. (2673096)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 1 LIGHTNING STRIKE LOCATED @ FUSELAGE STA 600 STRINGER L27. CORRECTIVE ACTION: BLENDED AND REMOVED AREA AS PER B757 SRM 53-00-01. (2672134)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,566 hrs · 21,051 cycles

SHIP 6815 1 LIGHTNING STRIKE LOCATED AT FUSELAGE SKIN BETWEEN STA 620 AND STA 640 SAND STR L27. CORRECTIVE ACTION: BLENDED AND REMOVED AREA AS PER B757 SRM 53-00-01. (2672164)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 2 LIGHTNING STRIKES LOCATED AT STA 395 AND STR L28. CORRECTIVE ACTION: BLENDEE AND REPAIRED AREA AS PER B757 SRM 53-00-01. (2672130)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 1 LIGHTNING STRIKE LOCATED FUSELAGE SKIN STA 215 AND STR L-28. CORRECTIVE ACTION: BLENDED AND REPAIRED AREA PER B757 SRM 53-00-01. (2672110)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 3 LIGHTNING STRIKES LOCATED AT FUSELAGE STA 490 STRINGER L28. CORRECTIVE ACTION: BLENDED AND REMOVED AREA AS PER B757 SRM 53-00-01. (2672166)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 2 LIGHTNING STRIKES LOCATED @ FUSELAGE STA 660 STRINGER L27. CORRECTIVE ACTION: BLENDED AND REMOVED AREA AS PER B757 SRM 53-00-01. (2672155)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 2 LIGHTNING STRIKES LOCATED AT FUSELAGE STA 450 AND STR L28. CORRECTIVE ACTION: BLENDED AND REMOVED AREA AS PER B757 SRM 53-00-01. (2672171)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 1 LIGHTNING STRIKE LOCATED AT FUSELAGE STA 580 AND STR L27. CORRECTIVE ACTION: BLENDED AND REMOVED AREA AS PER B757 SRM 53-00-01. (2672138)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 2 LIGHTNING STRIKES LOCATED @ FUSELAGE STA 620 STRINGER L27. CORRECTIVE ACTION: BLENDED AND REMOVED AREA AS PER B757 SRM 53-00-01. (2672146)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,542 hrs · 21,045 cycles

SHIP 6815 LIGHTNING STRIKE DAMAGE AT STA ~530, OVER S-28L. CORRECTIVE ACTION: REF ER/A 606946-14. (2671438)

Part: NONE — NONE · airframe 81,517 hrs · 21,038 cycles

SHIP 6815 AFT RT DOOR SLIDE LIGHT STAYS ILLUMINATED WITH DOOR UNARMED. CORRECTIVE ACTION: CYCLED DOOR ARMING LEVER SEVERAL TIMES AND CKD GIRT BAR SLIDERS AND PROX SWITCHES PER B757 M/M 52-11. OPS CK NML. (4785524)

Part: NONE — NONE · airframe 81,517 hrs · 21,038 cycles

SHIP 6815 AFT RIGHT DOOR 4R SLIDE LIGHT STAYS ILLUMINATED. DESPITE DOOR BEING DISARMED. CORRECTIVE ACTION: CYCLED DR4R. NOTED SLIDE EXTINGUISHED. (4785522)

Part: NONE — NONE · airframe 81,386 hrs · 21,011 cycles

SHIP 6815 -DIV- TO LAX DUE TO LEFT THRUST REVERSER CONTROL MESSAGE. CORRECTIVE ACTION: COMPLETED TROUBLE SHOOTING PER THE FIM. FOUND LEFT LVDT OUT OF ADJUSTMENT. ADJUSTED SAME AND OPS CHECKS GOOD.

Part: NONE — NONE · airframe 81,386 hrs · 21,011 cycles

SHIP 6815 DOOR MOUNTED BUSTLE DELETHALIZATION PAD (ONLY EFFECTIVE FOR 6819 -6823 3R DOOR) / LOCATIONS: 2L. CORRECTIVE ACTION: T/S 2L SLIDE PACK, FOUND PACK NOT UP ALL THE WAY IN HOUSING, ALSO FOUND BOTTOM STRAP OF SLIDE PACK NOT THROUGH THE BUSTLE. RE-ADJUSTED SLIDE PACK AND CORRECTLY INSTALLED BOTTOM STRAP. (2636244)

Part: NONE — NONE · airframe 81,338 hrs · 21,000 cycles

RIGHT DOOR IS DISARMED BUT SLIDE LIGHT REMAINS ILLUMINATED. CORRECTIVE ACTION: SLIDE LIGHT WORKS NML AT THIS TIME. REMOVED AND REPLACED 1R DOOR FWD PROX SWITCH IAW B757 AMM 25-66. OPS CHECK GOOD.

Part: NONE — NONE · airframe 81,321 hrs · 20,997 cycles

SHIP 6815 DOOR 1R SLIDE LIGHT IS ILLUMINATED WHEN DOOR HANDLE IS DISARMED. CORRECTIVE ACTION: INSPECTED DOOR GIRT BARDS NO TROUBLE FOUND CYCLED SEVERAL TIMES FOR PROPER OPERATIONS, ALL INDICATION NORMAL. ARM/DISARM OPS CHKD GOOD. (8267013)

Part: NONE — NONE · airframe 81,321 hrs · 20,997 cycles

SHIP 6815 1 RIGHT DOOR IS DISARMED BUT SLIDE LIGHT REMAINS ILLUMINATED. CORRECTIVE ACTION: NO PROBLEM FOUND. CREW CYCLED HANDLE - ARM LIGHT WENT AWAY. INSPECTED FOR DEBRIES ON TRACK AND OPS CHK NML PER B757 AMM 52- 11. (8267018)

Part: NONE — NONE · airframe 81,321 hrs · 20,997 cycles

SHIP 6815 4R DOOR DISARMED BUT SLIDE LIGHT IS STIL ILLUMINATED. CORRECTIVE ACTION: CYCLED 4R DOOR SEVERAL TIMES. ARMED & DISARMED. ALL INDICATION NML. NO FAULTS. OBSERVED VERIFIED FIRT BAR DISENGAGED. NTF. (8267006)

Part: NONE — NONE · airframe 81,261 hrs · 20,984 cycles

SHIP 6815 1R DOOR DISARMED BUT SLIDE LIGHT IS STILL ILLUMINATED. CORRECTIVE ACTION: CYCLED 1R DOOR SEVERAL TIMES, ARMED AND DISARMED. ALL INDICATIONS NML, NO FAULTS OBSERVED. VERIFIED GIRT BAR ENGAGED/ DISENGAGED. NTF. REF. B757 AMM 52-11. (8267004)

Part: NONE — NONE · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 DTE, ERA 605096-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE LH FRAME AT STA 1280 & S-11/12. CORRECTIVE ACTION: REF ERA 605096-14. (2608686)

Part: NONE — NONE · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 GOUGE ON FRAME BTW STA 1280 AND STR 11 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00330: FRAME STA 1280 WAS REPAIRED PER ER/A N 605096-14 REV ORIGINAL SECTION I: PERMANET REPAIR. (2608930)

Part: NONE — NONE · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 SECONDARY NRC, IN REF NRC: 00233: CORROSION ON LH SIDE PANEL (UPPER AND LOWER SIDES) BTW STA 1310-1410 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00580: (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED, AREA BTW STA 1310 / STA 1410 IT IS OUT OF LIMITS PER B757-200 SRM. THEREFORE, SIDE PLATE STA 1310 TO STA 1410 WAS REPLACED PER B-757-200 SRM. (2605627)

Part: FLOOR SUPPORT — CORRODED (BS 1498-1540) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 CORROSION ON FLOOR STRINGERS RBL 11.4, RBL 7.55 AND RBL 2.90 FROM STA 1498 TO STA 1540 11.4 AT AFT CARGO CMPT FLOOR SUPPORT STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00298: FLOOR STRINGERS ON RBL 11.4, RBL 7.55 AND RBL 2.90 FROM STA 1498 TO STA 1540 WERE REPLACED PER B757-200 SRM. (2600448)

Part: FLOOR SUPPORT — CORRODED (BS 1498-1540) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 CORROSION ON FLOOR STRINGERS LBL 11.4, LBL 7.55 AND LBL 2.90 FROM STA 1498 TO STA 1540 AT AFT CARGO CMPT FLOOR SUPPORT STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00300: FLOOR STRINGERS LBL 11.4, LBL 7.55 AND LBL 2.90 FROM STA 1498 TO STA 1540 AT AFT CARGO WERE REPAIRED PER B757-200 53-00-53-2R PROCEDURE 1 REPAIR 1 AND DWG 146N5444 REV C. (2599314)

Part: SKIN — DENTED (BS 470-480) · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 DENT ON SKIN OF FUSELAGE BTW STA 470&480 AND BTW S22&23 RH. DENT ON FUSELAGE SKIN BTW STA 470-480, LONG 22-23 RH WAS REPAIRED PER ER/A 604885-14 REV.ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 CORROSION ON FLOOR STRINGER PREVIOUS DOUBLER REPAIR (6E/A) BTW STA 1460 AND STA 1480 ON LBL 2.9,LBL 7.55, RBL 2.9, RBL 7.55, RBL 10.45 AND RBL 16.1 AT AFT CARGO CMPT FLOOR SUPPORT STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 307: FLOOR STRINGER PREVIOUS DOUBLER REPAIR (4E/A) BTW STA 1460 AND STA 1480 ON LBL 7.55, RBL 7.55, RBL 10.45 AND RBL 16.1 AT AFT CARGO CMPT FLOOR SUPPORT STRUCTURE WERE REPLACED PER B-757-200 SRM AND FLOOR STRINGER PREVIOUS DOUBLER REPAIR (2E/A) BTW STA 1460 AND STA 1480 ON LBL 2.9 RBL 2.9, AT AFT CARGO CMPT FLOOR SUPPORT STRUCTURE WERE ATTENDED WITH NRC 00571 AND 00572. (2599828)

Part: STRINGER — CORRODED (BS 1445-1498) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 SECONDARY NRC: IN REFERENCE TO NRC 307 AFTER REMOVED REPAIR DOUBLER CORROSION WAS FOUND ON RBL 2.9 BTW STA 1460 AND 1480 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00571: SECTION OF STRINGER ON RBL 2.9 BTW STA 1445 TO 1498 IN AFT CARGO COMPARTMENT. WAS REPLACED PER B757 200 SRM. (2599354)

Part: PANEL — CORRODED (BS 1200-1440) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

CORROSION ON RH SIDE PANELS (UPPER AND LOWER SIDES) BTW STA 1200 / STA 1310, BTW STA 1310 /STA 1380 AND BTW STA 1380 / STA 1440 IN AFT CARGO COMPARTMENT. SIDE PANELS BTW STA 1200 / STA 1310, BTW STA 1310 /STA 1380 AND BTW STA 1380 / STA 1440 IN AFT CARGO COMPARTMENT WERE REPLACED PER B-757-200 SRM. (2598104)

Part: STRINGER — CRACKED (BS 1844-1862) · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 CRACK ON STRINGER 23L BTW STA 1844 AND STA 1862 AT AFTER ACCESORY COMPARTMENT INTERNAL STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00358: STRINGER 23L BTW STA 1844 AND STA 1862 AT AFTER ACCESORY COMPARTMENT INTERNAL STRUCTURE WAS REPAIRED PER ER/A N 605129-14 REV.ORIGINAL. (2598088)

Part: SKIN — CORRODED (LAV SER DOOR) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 CORROSION ON INNER SKIN AT FWD LAV SERVICE ACCESS DOOR 119AL (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00032: LAVATORY SERVICE ACCESS DOOR WAS REPLACED PER B-757-200 SRM. (2597720)

Part: SKIN — DENTED (BS 660 S17L) · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 DENT ON EXTERNAL FUSELAGE SKIN STA 660 AND STG 17 LH SIDE. REPAIR WAS PERFOMED PER ER/A 604879-14 REV.ORIGINAL. AND PER ER/A 604879-14 PRI REV.1.

Part: FLOOR SUPPORT — CORRODED (BS 1450-1500) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

CORROSION ON FLOOR SUPPORT BS 1460 LBL 16.1 IN THE AFT CARGO. THE FLOOR SUPPORT BS 1450 - 1500, LBL 16.1 WAS REPLACED IAW SRM.

Part: WEB — CORRODED · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 CORROSION ON WEB FROM STA 740 TO STA 780 BETWEEN S-27L AND S-26L.FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00244: WEB FROM STA 740 TO STA 780 BETWEEN S-27L AND S-26L.FWD CARGO COMPARTMENT WAS REPAIRED SRM. (2590680)

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 CORROSION ON INTERCOSTAL BETWEEN STA 1300/ STA1320 AND STGR LBL 29/30 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00294: INTERCOSTAL WAS FABRICATED PER DWG 146N3299 AND REPLACED PER B-757-200 SRM. (2590136)

Part: SEAT TRACK — DAMAGED (BS 760-780 RBL25) · airframe 81,164 hrs · 20,962 cycles

SEAT TRACK BETWEEN BS 760 AND 780, AT RBL 24.75 IN PASSENGER CABIN DAMAGED. THE SEAT TRACK SECTION BTW STA 760 AND 780, AT RBL 24.75 WAS REPAIRED PER SRM.

Part: WEDGE — DEBONDED (RT NR 7 SLAT) · airframe 81,164 hrs · 20,962 cycles

DISBOND OF 1.500IN LENGTH X 1.200IN WIDTH ON OSS410 UPPER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE, RT WING. DISBOND ON OSS410 UPPER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE, RH WING WAS REPAIRED IAW SRM.

Part: WEDGE — DEBONDED (LT NR 5 SLAT) · airframe 81,164 hrs · 20,962 cycles

DISBOND OF 1.500IN LENGTH X 1.000IN WIDTH ON ISS109 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. DISBOND ON ISS109 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING WAS REPAIRED PER B757-200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 710-720 RBL56) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 710 & 720, RBL 56. THE FLOOR SUPPORT WAS REPLACED IAW SRM.

Part: FRAME — CRACKED (RT NACELLE) · airframe 81,164 hrs · 20,962 cycles

CRACK ON FRAME NAC STA 200 ON INBOARD CORE COWL OF RH ENGINE. CORRECTIVE ACTION: SUMMARY OF NRC 00450: FRAME NAC STA 200 ON INBOARD CORE COWL OF RH ENGINE WAS REPAIRED PER DELTA CMM 71-11-73 PAGE D601 IN REFERENCE TO EA 06-476772-14 REV. B. (2581590)

Part: STRAP — CRACKED (BS 580) · airframe 81,164 hrs · 20,962 cycles

CRACK ON LT STABILIZATION STRAP BS 580 CEILING AREA C1. THE LT STABILIZATION STRAP WAS REPAIRED IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 720-740) · corrosion level 2 · airframe 81,164 hrs · 20,962 cycles

CORROSION ON INTERCOSTAL 2 EAS BSTA 720/740 AT S-28R AND S-28L. INTERCOSTAL BTW STA 720 TO STA 740 AT S-28R WAS REPLACED AND INTERCOSTAL BTW STA 720 TO STA 740 AT S-28L WAS REPAIRED PER SRM (ET) (HFEC) WAS ACCOMPLISHED ON INTERCOSTAL BTW STA 720 TO STA 740 AT S-28L, NO CRACKS WERE FOUND ON EDGE OF TRIMMED AREA PER & NDT MANUAL.

Part: DRAG FITTING — CORRODED (LT ENGINE) · airframe 81,164 hrs · 20,962 cycles

SHIP 6815 A.A. AD. LH ENG DRAG FTG CLAMP-UP HOLE # 3 AND HOLE # 8 CORROSION WERE FOUND AS FOLLOW: HOLE # 3 CORROSION ON SKIN AT 12 O'CLOCK POSITION AND HOLE # 8 CORROSION ON SKIN AT 12 O'CLOCK POSITION (REF. CARD 5720-01100-04A. JOB # 076-0001. STEP 14.). CORRECTIVE ACTION: SUMMARY OF NRC 00235: [A.A. AD] LH ENG DRAG FTG CLAMP-UP HOLES #3 AND #8 WERE REAMED PER CARD 5720-01100-04A PAR 14 (C) AND B757-200 SRM. (2577928)

Part: STRAP — CRACKED (BS 365-377) · airframe 81,164 hrs · 20,962 cycles

CRACKED STABILIZER STRAP (PREVIOS REPAIR) BTW STA 365.25 TO STA 377.7 AND LBL 25 AT ABOVE NLG W/W. STABILIZER STRAP WAS REPLACED IAW REPAIR PER SRM.

Part: LIGHT — BROKEN (SEAT 36D) · airframe 81,160 hrs · 20,961 cycles

EMERGENCY LIGHT AT 36D BROKEN. SECURED EMERGENCY LIGHT AT 36D.

Part: NONE — NONE · airframe 80,721 hrs · 20,861 cycles

SHIP 6815 EMERGENCY PATHWAY LIGHT @ SEAT 2C INOP. CORRECTIVE ACTION: REMOVED AND REPLACED LIGHT OPS CK GOOD. (9681613)

Part: NONE — NONE · airframe 80,171 hrs · 20,734 cycles

SHIP 6815 - TIRE - DUE TO #2 MLG TIRE BLOWN ON LANDING. CORRECTIVE ACTION: REPLACED #1 AND #2 TIRE ASSEMBLIES. PERFORMED ANTISKID OPS CHECK.

Part: NONE — NONE · airframe 80,028 hrs · 20,702 cycles

SHIP 6815 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 2L / ACARS TEXT: FRC3351012L EXIT SIGN FELL OFF WHEN DOOR WAS CLOSED. CORRECTIVE ACTION: SECURED EXIT SIGN AT 2L. (2374022)

Part: NONE — NONE · airframe 80,028 hrs · 20,702 cycles

SHIP 6815 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:02L. CORRECTIVE ACTION: REPLACED MISSING EXIT SIGN DIFFUSER AT 2L PER B757 AMM 33-51. (2372906)

Part: NONE — NONE · airframe 79,967 hrs · 20,688 cycles

SHIP 6815 EXIT SIGN AT 2L FELL OFF. CORRECTIVE ACTION: REATTACHED EMERGENCY SIGN AS NEEDED. (9028720)

Part: NONE — NONE · airframe 80,018 hrs · 20,700 cycles

SHIP 6815 ON WALK AROUND FOUND SEVERAL SMALL DENTS NEAR E&E EXHAUST. CORRECTIVE ACTION: REF ERA 600543-14 REV ORG.

Part: NONE — NONE · airframe 79,523 hrs · 20,585 cycles

SHIP 6815 4R DOOR SLIDE LIGHT REMAINS IN DISARMED POSITION. CORRECTIVE ACTION: CYCLED GIRT BAR ARMING LEVER, CKS GOOD. (8685134)

Part: NOT REPORTED — NOT REPORTED · airframe 78,659 hrs · 20,393 cycles

SHIP 6815 4L DOOR SLIDE DIFFICULT TO ARM. CORRECTIVE ACTION: REPOSITIONED "D" RING STRAP. SLIDE ARM AND DISARM NORMAL PER B757 AMM 52-11. (8804322)

Part: NONE — NONE · airframe 77,424 hrs · 20,117 cycles

SHIP 6815 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:653. CORRECTIVE ACTION: RESECURED EMERGENCY EXIT SIGN COVER. (1969946)

Part: NONE — NONE · airframe 77,347 hrs · 20,101 cycles

SHIP 6815 DENTS ON VERT SKIN FSS 245. CORRECTIVE ACTION: C/W ERA 594134-14 REV O SECTION I TIME LIMITED REPAIR. VERTICAL SKIN PANEL REPAIRED REF SRM 55-30-01 AND ERA 594250-14 REV O. ERA 594134-14 REV O SECTION II PERMANENT REPAIR COMPLIED WITH. (6821238)

Part: NONE — NONE · airframe 77,342 hrs · 20,097 cycles

SHIP 6815 INITIAL INSPECTION: DENTS (2E/A) ON VERTICAL STABILIZER EXTERNAL SKIN (LH SIDE) FSS 250 AND 20" INCHES AFT AUXILIARY SPAR. CORRECTIVE ACTION: SUMMARY OF NRC 00081: VERTICAL STABILIZER EXTERNAL SKIN (LH SIDE) FSS 250 AND 20" INCHES AFT AUXILIARY SPAR WAS REPAIRED PER ER/A 594134-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. (1948823)

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 77,339 hrs · 20,096 cycles

SHIP 6815 DENT ON LH HOR. STAB. SKIN (LWR SIDE) AT STAB STA. 170 AND 4" FWD FROM FRONT SPAR. CORRECTIVE ACTION: SUMMARY OF NRC 00115: LH HOR.STAB. SKIN (LWR SIDE) AT STAB. STA. 170 AND 4" FWD FROM FRONT SPAR WAS REPAIRED PER ETI-57-21-477 REV.1 AND ER/A NO.593961-14, REV. ORIGINAL SECTION I: PERMANENT REPAIR. (1942738)

Part: ACOUSTIC PANEL — DENTED (NR 2 NACELLE) · airframe 77,339 hrs · 20,096 cycles

SHIP 6815 SEVERAL DENTS ON ACUSTIC PANEL AT ENGINE #2 BTW 7 AND 10 HOURS POSITION. CORRECTIVE ACTION: SUMMARY OF NRC 00227: DENTS ON ACOUSTIC PANEL AT ENGINE #2 BTW 7 AND 10 HOURS POSITION WERE EVALUATED AND WERE FOUND WITHIN LIMITS PER ER/A NO. 593873-14 REV. ORIGINAL, SECTION I: PERMANENT REPAIR AND ETI-57-21-457 REV. 7. (1942117)

Part: WEDGE — DAMAGED (NR 4 SLAT) · airframe 81,164 hrs · 20,962 cycles

ERA 593987-14 ISSUED FOR REPAIR TO SLAT #4 TE WEDGE. SLAT NBR 4 WAS REPLACED FOR SERVICEABLE SLAT PER AMM 27-81-02. AND ER/A 593987-14 REV.ORIGINAL.

Part: DUCT — DENTED (THRUST REVERSER) · airframe 77,339 hrs · 20,096 cycles

SHIP 6815 DENTS (3 E/A) ON INBOARD THRUST REVERSE FAN DUCT COWL FROM STA NAC 126 TO STA NAC 128 AT ENGINE #1. CORRECTIVE ACTION:SUMMARY OF NRC 00251: DENTS WERE EVALUATED AND WERE FOUND WITHIN OF LIMITS PER ER/A NO. 593875-14 REV. ORIGINAL, SECTION I: PERMANENT REPAIR AND ETI-57-21-466 REV. 3. (1939764)

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 77,339 hrs · 20,096 cycles

SHIP 6815 CRACKS ON OUTER SKIN OF FWD LOWER CORNER ON AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00029-OUTER SKIN OF FWD LOWER CORNER ON AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ETI-57-21-463 REV. ORIGINAL AND ER/A 593923-14 REV.ORIGINAL.(1940299)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 77,033 hrs · 20,035 cycles

SHIP 6815 L2 EMERGENCY LT LENS MISSING. CORRECTIVE ACTION: INSTALLED L2 EMERGENCY LT LENS. (6225660)

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 77,025 hrs · 20,033 cycles

(AIRCRAFT 6815, L/P 1484411) EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:653. CORRECTIVE ACTION: SECURED EXIT SIGN LOC 653.

Part: LIGHT — DAMAGED (SEAT 39D) · airframe 76,907 hrs · 20,004 cycles

SHIP 6815 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:39D. CORRECTIVE ACTION: RESECURED LIGHT ASSY. OPS NML. (1467451)

Part: PROXIMITY SWITCH — MALFUNCTIONED (L2 SLIDE LIGHT) · airframe 76,490 hrs · 19,919 cycles

L2 DOOR SLIDE LIGHT CAME BACK ON AFTER DOOR OPENED. SLIDE BASIE COULD BE LOOSE. R & R ARM LIGHT ASSY, NO HELP. T/S AND FOUND FWD PROX SW DAMAGED. R & R FWD PROXIMITY SWITCH IAW AMM 25-66. OPS CHECKED GOOD.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 72,992 hrs · 19,271 cycles

SHIP 6815 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:654. CORRECTIVE ACTION: REPOSITION EMERGENCY LIGHT SIGN TO ORIGINAL POSITION. (0985071)

Part: SLIDE — UNSERVICEABLE (L3 DOOR) · airframe 72,918 hrs · 19,256 cycles

SHIP 6815 L-3 DOOR SLIDE BOTTLE PIN DOES NOT ALIGN WITH COVER. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0299:2020-2368-3L/ 001 00162 REMOVED AND REPLACED SLIDE REF CARD. (0974907)

Part: SLIDER — OBSTRUCTED (R1 GIRT BAR) · airframe 69,576 hrs · 18,613 cycles

FA REPORT, THE R1 DOOR NOT ARMING. REMOVED OBSTRUCTION FROM FWD GIRT BAR SLIDER. ABLE TO ARM/DISARM DOOR.

Part: SEAL — OUT OF POSITION (R1 DOOR) · airframe 69,515 hrs · 18,601 cycles

R1 DOOR WOULD NOT ARM. FOUND INNER DOOR SEAL PARTIALLY OUT OF TRACK. REINSTALLED. DOOR NOW ARMS NORMAL.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 68,504 hrs · 18,399 cycles

R1 DOOR WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR.

Part: STRAP — TWISTED (R1 DOOR SLIDE) · airframe 68,564 hrs · 18,412 cycles

R1 DOOR WOULD NOT ARM. FOUND SLIDE PACK STRAP BINDING AND TWISTED. REPAIRED THE STRAP.

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 68,186 hrs · 18,333 cycles

EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT IAW FIM 33-51-00-815-802. R & R THE EMERGENCY LIGHTS ALTERNATE TRANSFER RELAY K10570 IAW WDM 33-51-11. OPS CHECKED GOOD.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR SLIDE) · airframe 68,047 hrs · 18,305 cycles

L2 DOOR STATUS UNKNOWN. TRIED TO UNLOCK BUT CANNOT CONFIRM DISARMED. REMOVED BUSTLE AND FOUND SLIDE RIGGING JAMMED BENEATH GIRT BAR. REMOVED AND RESTOWED RIGGING FROM BENEATH GIRT BAR AND REINSTALLED BUSTLE.

Part: TIRE — FAILED (MLG) · airframe 67,730 hrs · 18,243 cycles

AIRCRAFT 6815 - TIRE - ON TAXI IN #2 MAIN TIRE BLEW AND IS FLAT SPOTTED. CORRECTIVE ACTION: REPLACED #1 AND #2 MLG TIRE ASSEMBLIES. PERFORMED ANTISKID BITE TEST PER AMM 32-42. NO FAULTS FOUND.

Part: RING — OUT OF POSITION (DOOR RAFT) · airframe 67,383 hrs · 18,175 cycles

L2 DOOR WOULD NOT DISARM OR ARM. LEVER BINDING IN INTERMEDIATE POSITION. INSPECTED THE DOOR AND FOUND THE RAFT ATTACH RING OUT OF PLACE. SECURED & OPS CHECKED THE SLIDE ARM SYSTEM IAW AMM 25-66. ALL OK.

Part: CONNECTOR — CORRODED (WATER HEATER) · airframe 66,789 hrs · 18,053 cycles

WATER HEATER CONNECTOR PLUG CORRODED IN THE L2 LAVATORY. REMOVED AND REPLACED THE WATER HEATER IAW AMM 38-13.

Part: SENSOR — DIRTY (GIRT BAR) · airframe 65,590 hrs · 17,832 cycles

ON PUSH BACK, THE R2 DOOR WILL NOT ARM. TROUBLESHOT IAW AMM 52-09, CLEANED THE GIRT BAR SENSORS, CYCLED ARM HANDLE, OK FOR SERVICE.

Part: PANEL — DENTED (THRUST REVERSER) · airframe 64,302 hrs · 17,564 cycles

LEFT ENGINE OTBD THRUST REVERSER UPPER BIFURCATION PANEL HAS A DENT ON SURFACE. NAC STA 110. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 54-31-01, FIG 101. REPAIRED THE AREA IAW ERA 555231-14, REV O.

Part: STRUCTURE — CORRODED (LAVATORY) · airframe 64,302 hrs · 17,564 cycles

LAVATORY D, AFT WALL LOWER INBOARD CORNER HAS CORROSION. FABRICATED A NEW FITTING IAW ERA 554512-14MA, REV .

Part: SKIN — DAMAGED (LT WING LE) · airframe 64,302 hrs · 17,564 cycles

LEFT WING UPPER FIXED L/E COMPOSITE MATERIAL CRACKED. REPAIRED IAW ER/A 401605-14MA REP. OPTION III AND SRM.

Part: FRAME — GOUGED (BS 1280) · airframe 64,302 hrs · 17,564 cycles

GOUGE AT RIGHT FRAME BS 1280 BETWEEN STRINGERS 12 AND 13R. REMOVED DAMAGE AND EVALUATED THE FRAME, FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED THE FRAME IAW PRRI 555226-14 REVO AND ERA 555226-14AD, REV O.

Part: SKIN — DAMAGED (RT WING TE) · airframe 64,302 hrs · 17,564 cycles

RIGHT WING FIXED T/E, HAD COMPOSITE DAMAGE AT WS 425. REPAIRED IAW ER/A 401605-14MA REP. OPTION III AND IAW SRM.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 64,302 hrs · 17,564 cycles

FLOORBEAM CORRODED AT BS 324 BETWEEN RBL 41 & 58. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM. CUT OUT DAMAGED SECTION AND REPAIRED THE FLOORBEAM IAW SRM.

Part: COUNTER — CORRODED (GALLEY) · airframe 64,302 hrs · 17,564 cycles

GALLEY 4 FILLER AT THE COUNTER TOP WAS FOUND SEVERELY CORRODED. MANUFACTURED NEW FILLER FROM DRAWING 257013 REV C SHEETS 1 AND 9 IAW ENGINEERING REPAIR AUTHORIZATION N: 06-494005-14MA REV B.

Part: SKIN — CRACKED (APU DOOR) · airframe 64,302 hrs · 17,564 cycles

RIGHTT APU BAY ACCESS DOOR AFT LOWER CORNER SKIN CRACKED. REPAIRED AREA IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 64,302 hrs · 17,564 cycles

MAIN CABIN L4 DOOR UPPER AFT SILL SUPPORT HAS CORROSION STA 1680 LBL60. REMOVE AND REPLACED MAIN CABIN L-4 DOOR UPPER AFT SILL SUPPORT STA 1680 LBL 60 PN 146N8016U1 IAW SRM 51-40-02 AND DRW 146N8722 REV B AD BK.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,302 hrs · 17,564 cycles

ON WALK AROUND FOUND DENT 24IN FWD OF L2 DOOR THRESHOLD. CUT OUT DAMAGED SECTION AND REPAIRED FUSELAGE SKIN STA 620 S-16L IAW PRI 553859-14 REV 0, REV 1 & ERA 549536-14 REV C.

Part: RELAY — CORRODED (WATER HEATER) · corrosion level 2 · airframe 61,092 hrs · 16,947 cycles

HOT AND COLD RELAY FOR WATER HEATER CORRODED AT MID LT LAV. CORRECTED LOOSE B-NUT ON RELAY AND REPLACED HOT/COLD SOLENOID CONTROL VALVE REF CMM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,040 hrs · 16,933 cycles

DURING WALKAROUND, FOUND DAMAGE 30 INCHES AFT OF L4 DOOR. REPAIRED DAMAGE IAW EA 543779-14, SECTION 3, REV B AND SRM 53-00-01. REPAIR 3, PAGE 207.

Part: WEDGE — DELAMINATED (NR 7 SLAT) · airframe 55,077 hrs · 15,734 cycles

NR 7 SLAT WEDGE INNER SIDE DELAMINATED AT INBD SIDE. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: CONNECTOR — DAMAGED (CONTROL PANEL) · airframe 53,930 hrs · 15,508 cycles

FWD F/A PANEL EMERGENCY LIGHT BUTTON WILL NOT ILLUMINATE EMERGENCY LIGHTS. TROUBLESHOT IAW AA 3320-00157. SWAPPED AFT & FWD CONTROL PANELS. PROBLEM STILL EXISTS AT FWD ACP. SUSPECT WIRING FAULT AT SP9145. RETURNED CONTROL PANELS TO THEIR ORIGINAL LOCATIONS AND REINSTALLED IAW AMM 33-22. REPAIRED CONNECTOR. OPS CHECKED OK AT FWD F/A PANEL.

Part: SKIN — DAMAGED (BS 272) · airframe 52,814 hrs · 15,297 cycles

LOWER FUSELAGE SKIN AT BS 272, TWO INCHES ABOVE STRINGER 19R HAS LIGHTNING STRIKE DAMAGE. DRILLED OUT DAMAGE IAW SRM 53-00-01, FIG 201 AND APPLIED ALODINED IAW SRM 51-20-01, HFEC INSPECTED IAW NDTM PART 6, 51-00-16, NO CRACKS NOTED. APPLIED PRIMED AREA IAW SRM 51-20-01, INSTALLED FASTENER IAW SRM 51-40-02 AND AMM 51-21-00.

Part: SKIN — DAMAGED (BS 535) · airframe 52,814 hrs · 15,297 cycles

FWD FUSELAGE AT BS 535 ABOVE S25L HAS ONE LIGHTNING STRIKE EXIT. DRILLED OUT DAMAGE IAW SRM 53-00-01. COMPLIED WITH HFEC INSPECTION IAW HDTM P 6, 51-00-16, NO CRACKS NOTED A 15270, APPLIED PRIMED IAW SRM 51-20-01, INSTALLED FASTENERS IAW SRM 51-40-02 AND 53-00-01, APPLIED TOP COAT AREA IAW AMM 51-21-00.

Part: ANGLE — MISALIGNED (BS 395) · airframe 52,814 hrs · 15,297 cycles

PULLEY BRACKET FASTENER CANNOT BE PICKED UP BY INTERCOASTAL ANGLE REQ BY DWG, BS 395 RBL 8.93. TRIMMED ANGLE IAW DWG B223206-107 REV A.

Part: ATTACH ANGLE — INTERFERENCE (BS 660) · airframe 52,814 hrs · 15,297 cycles

STOWAGE ATTACH ANGLE AT BS 660 S5R HAS INTERFERANCE WITH GROUND STUDS. FABRICATED NEW ANGLE FOR STOWAGE BIN INTERCOSTAL IAW DWG B223240-001 REV J.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,320 hrs · 17,360 cycles

MAIN CABIN AT STA 345 BETWEEN LBL 64 - RBL 64 HAS LIGHT CORROSION FLOORBEAM. CUT OUT DAMAGE AREA, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: CUSP WEB — CORRODED (BS 980-1000) · corrosion level 2 · airframe 52,814 hrs · 15,297 cycles

MAIN CABIN RT CUSP WEB BETWEEN BS 980-1000 CORRODED. REPAIRED IAW ER/A 524968-14 .

Part: SEAT TRACK — CORRODED (BS 1640) · airframe 52,814 hrs · 15,297 cycles

MAIN CABIN SEAT TRACKS CORRODED AT BS 1640, RBL 24.75 & 45.5. REMOVED DAMAGED SEAT TRACK BS 1540-1640, FABRICATED NEW SEAT TRACK AND INSTALLED SEAT TRACK IAW SRM 53-60-52, ID 1, FIG 1 51-40-05 & 51-40-02.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 52,814 hrs · 15,297 cycles

MAIN CABIN BS 365.25 BETWEEN LBL 64-RBL 64 CORRODED FLOORBEAM. CUTOUT DAMAGED AREA OF FLOORBEAM UPPER TEE, FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-51.

Part: SKIN — DAMAGED (BS 675) · airframe 52,814 hrs · 15,297 cycles

FWD FUSELAGE AT BS 675, S28R HAS ONE LIGHTING STRIKE. CUTOUT DAMAGED AREA , FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-30-01, IDI, FIG 1 AND 53-00-01, REP 3, FIG 201.

Part: SKIN — DAMAGED (BS 225) · airframe 52,814 hrs · 15,297 cycles

LOWER FUSELAGE AT BS 225, ABOVE S28R HAS ONE LIGHTNING STRIKE. CUTOUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-10-01, IDI, FIG 1 AND 53-00-01, REP 3, FIG 201.

Part: SEAT TRACK — DAMAGED (BS 865) · airframe 52,814 hrs · 15,297 cycles

MAIN CABIN SEAT TRACK DAMAGED AT RBL 24.75, BS 865. REMOVED DAMAGED SEAT TRACK BS 780-880, FABRICATED NEW SEAT TRACK, AND INSTALLED IAW SRM 53-30-52, 51-40-02 & 51-40-05.

Part: SEAT TRACK — CORRODED (BS 865) · airframe 52,814 hrs · 15,297 cycles

MAIN CABIN SEAT TRACK DAMAGED AT RBL 24.75, BS 865. REMOVED DAMAGED SEAT TRACK BETWEEN BS 780-880. FABRICATED NEW AND INSTALLED IAW SRM 53-30-52, ID 1, FIG 1, 51-40-05 & 51-40-02.

Part: SEAT TRACK — CORRODED (BS 730-740) · corrosion level 2 · airframe 52,814 hrs · 15,297 cycles

MAIN CABIN SEAT TRACK AT RBL 45.5, BS 730-740 CORRODED. REMOVED DAMAGED SEAT TRACK BETWEEN BS 700-780, FABRICATED NEW AND INSTALLED IAW SRM 53-30-52, ID 1, FIG 1, 51-40-05 & 51-40-02.

Part: SEAT TRACK — CORRODED (BS 730-740) · corrosion level 2 · airframe 52,814 hrs · 15,297 cycles

MAIN CABIN SEAT TRACK AT RBL 24.75, BS 730-740 CORRODED. REMOVED DAMAGED SEAT TRACK BETWEEN BS 700-780. FABRICATED NEW AND INSTALLED IAW SRM 53-30-52 ID 1, FIG 1, 51-40-09 & 51-40-02.

Part: SKIN — DAMAGED (BS 530) · airframe 51,147 hrs · 14,942 cycles

LIGHTNING STRIKE STR 29 - 30R AT BS 530. DRILLED OUT DAMAGE IAW SRM 53-00-01. INSTALLED FASTENER AND RESTORED FINISH IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 263) · airframe 51,081 hrs · 14,928 cycles

LIGHTNING STRIKE AT FS 263, LBL 10. REMOVED DAMAGED FASTENERS IAW SRM 53-00-01. COMPLIES WITH HFEC INSPECTION AND INSTALLED FASTENERS AND RESTORED FINISH IAW SRM 53-00-01.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 50,269 hrs · 14,765 cycles

SEAT 28 DEF FLOOR EMEREGENCY LIGHT INOPERATIVE. FOUND MATE-N-LOK CONNECTOR BROKEN AT SEAT 28D DISCONNECT. REPLACED IAW BSWPM 20-42-01. OPS CHECKED GOOD.

Part: SWITCH — MALFUNCTIONED (CABIN) · airframe 38,673 hrs · 12,509 cycles

DURING FLIGHT, CREW REPORTED EMERGENCY LIGHTING CYCLING ON AND OFF IN VARIOUS LOCATIONS. MX REPLACED THE EMERGENCY LIGHT TEST SWITCH. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,664 hrs · 12,508 cycles

PILOT REPORTS THE EMERGENCY PATH LIGHTS AT 19DEF THROUGH 26DEF WILL NOT SHUT OFF. MAINTENANCE REPLACED THE BATTERY PACK AT DOOR 2R. OPERATIONAL CHECK WAS GOOD. (2011-D0143)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,654 hrs · 12,504 cycles

MAIN DECK FLOORBEAM STA 377.7 HAS LIGHT CORROSION AROUND FASTENERS HOLES BETWEEN BL0-LBL 16. REPAIRED DURING HMV AT SAA ON NRC 176096.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,654 hrs · 12,504 cycles

MAIN DECK FLOORBEAM STA 365 HAS UPPER FLANGE CORRODED BETWEEN BL0 AND RBL 48. REPAIRED DURING HMV AT SAA ON NRC 176080.

Part: GIRT BAR — CORRODED (L4 DOOR SLIDE) · airframe 38,654 hrs · 12,504 cycles

L4 DOOR GIRT BAR RESTRAINT IS CORRODED. REPLACED GIRT BAR RESTRAINT AT SAA. DURING HMV, ON NR CARD 171239.

Part: GIRT BAR — CORRODED (R1 DOOR SLIDE) · airframe 38,654 hrs · 12,504 cycles

R1 DOOR GIRT BAR RESTRAINT HAS CORROSION. REPLACED GIRT BAR RESTRAINT AT SAA. DURING HMV, ON N/R CARD 181916.

Part: CHECK VALVE — CRACKED (LT PACK) · airframe 35,385 hrs · 11,864 cycles

AFTER T/O BOTH AUTO PRESS CONTROLLERS FAILED. PILOTS COULD NOT CONTROL CABIN PRESS ELECTED TO DESCEND AND DIVERT. CONTRACT MX FOUND A SEAL OUT OF PLACE ON EMERGENCY EXIT DOOR REINSTALLED SAME AND PRESSURIZED ACFT WITH CREW ALL NORMAL. AFTER LEAVING AIRPORT, PASSING THROUGH 10K FT BOTH PRESS CONTROLLERS FAILED. CREW UNABLE TO CONTROL CABIN PRESS DIVERT. MX FOUND VALVE ASSY BLOWN OUT, REPLACING SAME.

Part: CHECK VALVE — RUPTURED (LEFT PACK) · airframe 35,385 hrs · 11,864 cycles

REPEAT WRITE-UP. SEE ITEM 004 THIS LOGSHEET. CABIN PRESS UNCONTROLLABLE IN AUTO 1/ AUTO 2 AND MANUAL. OUTFLOW MANUALLY CLOSED. DUCT PRESS 40 PSI BUT CABIN WILL NOT HOLD PRESSURIZATION. FOUND LT PACK DUCT SUPPLY CHECK VALVE WITH 4 INCH SQ SECTION BLOWN. BLOWN SECTION IS FWD OF CHECK VALVE FLAPPER, THIS CAUSING RT PACK TO ALSO BLOW ITS PRESS TO THE OUTSIDE. REMOVED LT PACK CHECK VALVE DUCT ASSY. INSTALLED LT PACK CHEK VALVE DUCT ASSY. LEAK CHECK OK. PRESSURE A/C. CHECKS OK. REF ITEM 11 OF THIS LOGSHEET. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: ENGINE — MAKING METAL (NR 2) · airframe 30,236 hrs · 10,831 cycles

DURING A CK INSP OF NR 2 ENG OIL FILTER FOUND FULL OF METAL PARTICLES MAGNETIC AND NON-MAGNETIC. FURTHER INSP OF CHIP DET FOUND METAL ON MASTER, ANGLE GEARBOX, AND NR 4 BEARING DET. A CK WAS BEING PERFORMED JFK ON 12/12/08. CHANGED NR 2 ENGINE.

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 30,095 hrs · 10,803 cycles

L ENG SEC CONT STATUS MESSAGE DISPLAYED, UNABLE TO CLEAR OUT RAN NR 1 ENG SEVERAL TIMES AND SELECT EEC TO ALTN POSITION NO MSG ARE NOTED. PERFORMED VISUAL INSPECTION ALL WIRING CHECK OK FOUND LOOSE CONNECTOR AT TCA AND J1 CONNECTOR ON EEC, AS PRECAUTION AND DUE TO HISTORY. REMOVED AND REPLACED EEC PER MM. RAN ENG FOR ABOUT 15 MIN. NO MSG ARE NOTED. CHECK OK.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 29,756 hrs · 10,713 cycles

REJECTED TAKEOFF RWY 13R KJFK FOR LOSS OFF EPR INDICATION LEFT ENG ALL OTHER INDICATIONS NORMAL. RTO INITIATED 50 KTS GS, LOW SPEED REJECT. CONSULTED W/JFK MTC DISPATCH. RESTARTED ENG ALL INDICATIONS NORMAL. EPCS MSGS NR 1 ENG P2 RESET ALSO S DCI DC2 EPR IND FWD TO MCO PER MEL 77-11-01. PLACARD INSTALLED.

Part: FCU — MALFUNCTIONED (NR 1 ENGINE) · airframe 28,095 hrs · 10,377 cycles

MAINTENANCE ATTEMPTING TO REPOSITION A/C STARTED NR 1 ENG AND TRIED TO ADVANCE THE THROTTLES WHEN THE ENGINE ROLLED BACK AND THEY HAD A TAIL PIPE FIRE WHICH THEY BLEW OUT. PERFORMED BORO, NO DAMAGE FOUND. REPLACED FCU AS PRECAUTIONARY. NO EPCS MESSAGES WERE FOUND. FOUND IGVS OUT OF RIG, ADJUSTED IGV'S AND VSV'S. DUE TO HISTORY MAINTENANCE FERRIED TO ATL FOR ENGINE REPLACEMENT.

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE) · airframe 28,067 hrs · 10,372 cycles

AFTER LEFT ENGINE START THROTTLES ADV BUT ENGINE UNRESPONSIVE. LEFT ENG BLEED VALVE WOULD NOT OPEN. FIRE REPORTED TO BE FROM LEFT ENG TO ABOVE WING AND ENG SMOKING. FUEL CONTROL SW TO OFF AND NR 1 ENGINE FIRE BOTTLE DISCHARGED. NO ENG EXCEEDANCES ON MTC PAGE. EPCS MSG P AOX ON FCU/EEC. REPLACED FCU PER AMM. INSPECTED PYLON AND AFT OF ENG WING AREA FOR POSSIBLE DAMAGE. NO TROUBLE FOUND. PERFORMED FUEL CONTROL REPLACEMENT TEST PER 71-00-00-735-328-P00. ENGINE CKS NORMAL. ETOPS CATEGORY 'D': INABILITY TO CTRL ENG OR GET DESIRED PWR.

Part: LIGHT — LOOSE (CABIN)

LAS - EMERGENCY LIGHT EXIT STRIP AT SEAT 13D LOOSE. SECURED EMERGENCY LIGHT EXIT STRIP AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGNECY LIGHT)

DFW - EMERGENCY EXIT LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY FLOOR LIGHTING IN FIRST CLASS SEAT ROWS 1 AND 2 ARE INOPERATIVE. REPLACED LIGHTING RIBBON AT SEAT ROWS 1 AND 2 AND REPLACED COVER FOR SEAT 1G FOR EMERGENCY FLOOR LIGHTING IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — UNKNOWN (RIGHT)

SEA - RIGHT HAND COMPRESSOR STALL DURING INITIAL CLIMB. POSSIBLY DUE WAKE TURBULENCE. ENGINE INDICATION FLUX 2 TO 3 SECONDS THEN STABLE. RETURNED TO SEA AND LANDED WITHOUT INCIDENT. DOWNLOADED FLIGHT DATA RECORDER. NO NEGATIVE REPORT. REPLACED BOROSCOPE PLUGS 6 TO 10, ENGINE CRANKING PLUG AND MAIN OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — DEFORMED (GIRT BAR) · airframe 14,113 hrs · 4,828 cycles

THE EVACUATION SLIDE GIRT BAR LEAF RETENSION SPRINGS WERE ADJUSTED ACCOUNT DEFORMED AT THE L1, R1, L2, R2, L4, AND R4 CABIN DOORS.

Part: BOTTLE — DISCHARGED (DOOR ASSIST) · airframe 6,328 hrs · 2,142 cycles

THE LEFT SIDE FWD CABIN DOOR ASSIST BOTTLE PRESSURE WAS ZERO. REPLACED THE ASSIST BOTTLE. CHECK-C 11-1-00 LAX.

Part: COMPRESSOR — FAILED (LT ENGINE) · airframe 6,297 hrs · 2,133 cycles

ON TAKEOFF THE LEFT ENGINE SURGED AND CREW SECURED THE ENGINE. FLIGHT RETURNED TO STL. SUSPECT FAILURE WAS IN 10TH STAGE OF COMPRESSOR. REPLACED THE ENGINE. CHECK-C 11-1-00 LAX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,252 hrs · 1,159 cycles

THE OUTSIDE EMERGENCY EVACUATION LIGHT WAS INOPERATIVE AT THE NUMBER 1 CABIN DOOR, RT SIDE OF THE AIRCRAFT. REPLACED THE LAMP. CHECK-C 5-26-99 LAX.

Part: WINDOW — WORN (LT COCKPIT)

DURING CRUISE THE R2 WINDOW HEAT TERMINAL SHORTED OUT MELTING THE INSULATION. PLACARD WINDOW HEAT INOPERATIVE PER MEL. *S/D* FOUND THE POWER TERMINAL SHORTED OUT AT THE WINDOW. REPLACED THE WINDOW AND SHORTED TERMINAL.