N727TW

Part: PROXIMITY SWITCH — FAULTED (ZONE 800) · airframe 88,989 hrs · 21,853 cycles

SLIDE LIGHT INOP LOC 607. DOES NOT ILLUMINATE WHEN DOOR IS ARMED. REMOVED AND REPLACED FWD PROX SWITCH PER B757 AMM 25-66. OPS CHECK GOOD. (1372737)

Part: FRAME — BENT (ZONE 100) · airframe 88,886 hrs · 21,824 cycles

THE UPPER CHORD OF THE FRAME IS BENT & DAMAGED AT STA.1480 , S26 - 27L. REPAIRED BS 1480 FRAME BETWEEN S26-27L PER ERA 630812-14AD. (1352785)

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

LOWER SILL, LOWER CHORD CORRODED IN MULTIPLE AREAS. AFT OF CARGO DOOR CUTOUT. BLENDED AREAS MINIMUM REMAINING THICKNESS 0.153 AND IS OUT OF LIMITS IAW SRM 53-60-15, REPAIRED DAMAGE PER ERA 630682-14. (1352869)

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE UPPER CHORD OF FRAME AT BS 1380, BETWEEN S28 - 27R. REPAIRED THE FRAME IAW ERA 631033-14. (1352802)

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

DTA MONITOR INSPECTION LOG REF ERA 630682-14, FUSELAGE, NR 2 CARGO DOOR, LOWER MAIN SILL, BS 1400-1420 CORRODED. REPAIRED IAW ERA 630682-14. (1351401)

Part: FRAME — CORRODED (ZONE 200) · airframe 88,886 hrs · 21,824 cycles

DTA MONITOR INSPECTION LOG REF ERA 631033-14 FUSELAGE, BS 1380 FRAME, INNER CHORD RBL 23 CORRODED. REF ERA 631033-14. (1350256)

Part: TEE ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON WING TO BODY FAIRING TEE ANGLE AT BS 900, LBL 10. FWD OF PANEL 193HL. (REF. PREVIOUS REPAIR LOG PG 1416404 & ERA 583732-14) REMOVED DAMAGE ON WING TO BODY TEE ANGLE AT BS 900, LBL 10 FWD OF PNL 193HL ADDED REPAIR CHORD AND SPLICE IAW DELTA ERA #630813-14 REV: OR FILE CODE: 0053-52. (1349126)

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE LOWER SURFACE OF STR.11L, AT BS 450, LOCATED JUST ABOVE THE CABIN WINDOW. REPAIRED AREA OF CORROSION ON LOWER SURFACE OF STRINGER 11L BS 450 IAW DELTA ER/A 630629-14 TAG REMOVED. JOB COMPLETE. (1349130)

Part: FRAME — DENTED (ZONE 100) · airframe 88,886 hrs · 21,824 cycles

DTA MONITOR INSPECTION LOG REF ERA 630812-14 FUSELAGE FRAME BS 1480, S26L - 27L DENTED. IAW ERA 630812-14. (1350212)

Part: STRINGER — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

DTA MONITOR INSPECTION LOG REF ERA 630629-14 FUSELAGE3, STRINGER 11L & BS 447 CORRODED. REF ERA 630629-14. (1348428)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

FLOOR SUPPORT AT STA 1510 RBL 7 IS CORRODED. BLENDED ALC FLOOR SUPPORT AT STA 1510 RBL 7 FOUND TO BE OUT OF LIMITS AT 1090 IAW B757 SRM 53-00-53-1A-1 DETAIL V. REPAIRED IAW B757 SRM 53-00-53-2R PROCEDURE 1. (1340150)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CABIN SEAT TRACK & FITTING IS RUSTY / CORRODED AT FS 1640 RIGHT HAND, OUT BOARD TRACK. CORRECTIVE ACTION: REPAIRED SEAT TRACK @ FS 1640 OB TRACK IAW B757-200 SRM 53-00-52 FIGURE 201 DETAIL I. (1340168)

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

ALC R/H LOWER Z-TRANSITION ANGLE AND LOWER SPLICE CORRODED AT STA 1440 TO 1510 RBL 22. REMOVED & REPLACED TRANSITION PANEL AT STA 1440 - 1510 RBL 22 IAW B757 SRM 51-40-02 SECTION 7. STREAMER REMOVED. (1340155)

Part: DOOR SILL — CORRODED (ZONE 100) · airframe 88,886 hrs · 21,824 cycles

AFT CARGO LOWER SILL CHORD WEB IS CORRODED AT B STA 1440, BETWEEN S-27R AND S-28R. AFT LWR CORNER OF DOOR CUT OUT. REMOVED & REPLACED WEB AT STA 1440 BETWEEN STR 27R & 28R IAW B757 SRM 51-40-02 SECTION 7. (1335167)

Part: NUT PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE NUTPLATES AND THE INTERCOSTAL PANAL, FOR THE FLOOR SUPPORT FOR THE ALC FLOOR, AT BS 1330, RBL11. TREATED AND PRIMED REWORK AREA IAW AMM 51-21-04 AND 51-21- 14 AND REINSTALLED AND REMOVED NP'S IAW SRM 51-40-02 PARA 4. (1330742)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE LOWER SURFACE OF THE ALC FLOOR SUPPORT AT BS 1330, LBL 8. REPAIRED FLOOR SUPPORT AT BS 1330 LBL8 IAW SRM 53-00-53-212 REPAIR 1 FIG 201. JOB COMPLETE. SEE PW FOR ALL WORK COMPLETED. (1330756)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE ALC FLOOR SUPPORT AT BS 1470, RBL8. BLENDED AND CHECKED LIMITS ON ALC FLOOR SUPPORT AT BS 1470 RBL 8 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 DETAIL V. REPAIRED IAW SRM 53-00-53-2R PROCEDURE 1. (1330748)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE LOWER SURFACE OF THE ALC FLOOR SUPPORT AT BS 1330, LBL11. REPAIRED FLOOR SUPPORT AT BS 1330, LBL 11 IAW SRM 53-00-53-2R REPAIR 1 FIG 201. SEE PW FOR ALL WORK COMPLETED. (1330754)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE ALC FLOOR SUPPORT AT BS 1470, LBL11. REPAIRED CORROSION ON ALC FLOOR SUPPORT AT BS 1470 LBL 11 IAW SRM 53-00-53-2R PROCEDURE 1. (1330771)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 88,886 hrs · 21,824 cycles

CORROSION ON THE LOWER SURFACE OF THE ALC FLOOR SUPPORT AT BS 1330, RBL15. REPAIRED FLOOR SUPPORT AT BS 1330, RBL 15 IAW SRM 53-00-53-WR REPAIR 1 FIG 201. JOB C/W REMOVED STREAMERS. SEE PW FOR ALL WORK COMPLETE. (1330758)

Part: SNUBBER — LEAKING (ZONE 800) · airframe 88,886 hrs · 21,824 cycles

NUMBER 2L DOOR SNUBBER LEAKING. REPLACED L2 DOOR SNUBBER IAW AMM 52-11-10 SNUBBER WILL BE INSTALLED ON JOB CARD 5211-6005-2L JOB COMPLETE. (1321772)

Part: SNUBBER — LEAKING (ZONE 800) · airframe 88,886 hrs · 21,824 cycles

SHIP 6813 NUMBER 4R DOOR SNUBBER LEAKING. CORRECTIVE ACTION: REPLACED R4 DOOR SNUBBER IAW B757 AMM 52-11-10 TO BE INSTALLED ON JC 186950-0800-0066 STEP 6. JOB COMPLETE. (1321145)

Part: SNUBBER — LEAKING (ZONE 800) · airframe 88,886 hrs · 21,824 cycles

NUMBER 4L DOOR SNUBBER LEAKING. REPLACED L4 DOOR SNUBBER IAW B757 AMM 52-11-00. WILL BE INSTALLED ON JC 186950-0800-0054 STEP 6. JOB COMPLETE. (1320168)

Part: SNUBBER — LEAKING (ZONE 800) · airframe 88,886 hrs · 21,824 cycles

SHIP 6813 NUMBER 4L DOOR SNUBBER LEAKING. CORRECTIVE ACTION: REPLACED L4 DOOR SNUBBER IAW B757 AMM 52-11-00. WILL BE INSTALLED ON JC 186950-0800-0054 STEP 6. JOB COMPLETE. (1321113)

Part: SKIN — DELAMINATED (ZONE 500 SLAT) · airframe 88,886 hrs · 21,824 cycles

SHIP 6813 BOTTOM OF LEFT WING LEADING EDGE JUST BEHIND SLAT DELAMINATED/ MISSING COMPOSITE. CORRECTIVE ACTION: C/W ER/A 630248-14 REV. -ORG- SEC 1 TIME LIMITED REPAIR. CLEAN, REMOVED DAMAGE AREA AND REPARE DAMAGE AREA, USING MATERIAL ID BMX8-79-3-120 PREP ROC. BMS 5-101-11-10 ADHESIVE, 6061-T6-040. IAW B757-200 SRM 51-70-05 PARA 5G. LAYUP CURE 250 DEGREES UNDER VACUUM IAW B757-200 SRM 51-70-05 PARA 5G. RESTORED FINISH IAW B757-200 AMM 51-21-10-377-003. (7941804)

Part: PROCESSOR — FAULTED (FUEL QTY) · airframe 88,871 hrs · 21,819 cycles

DIV- TO DTW DUE TO RIGHT FUEL QUANTITY INOP WITH LEFT FUEL QUANTITY ON MEL. R & R LT & RT WING FUEL PROBES 12 EACH SIDE. R & R LT & RT MAIN FUEL TANK HARNESS'S, R & R FQIS PROCESSOR.

Part: PROXIMITY SENSOR — FAULTED (ZONE 800) · airframe 88,494 hrs · 21,742 cycles

L2 DOOR SLIDE LIGHT INOP. REMOVED AND REPLACED L2 DOOR GIRT BAR PROXIMITY SENSOR IAW AMM 25-66-11. OPS CHECKED NORMAL. (1205119)

Part: GIRT BAR — FOD (ZONE 800) · airframe 85,771 hrs · 20,985 cycles

SHIP 6813 1L DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS. ALL OPS SATIS PER B757 AMM 52- 11. (6940200)

Part: CONTACT — DIRTY (SLIDE LIGHT) · airframe 85,588 hrs · 20,925 cycles

SHIP 6813 AFTER DISARMING SLIDE DOOR 1R SLIDE LIGHT REMAINED LIT. CORRECTIVE ACTION: CLEANED DEBRI FROM CONTACTS. VISUALLY VERIFIED GIRT BAR ENGAGEMENT & DISENGAGEMENT. ALL OPS NML

Part: SWITCH — NO DISCREPANCY (ZONE 200) · airframe 85,550 hrs · 20,911 cycles

SHIP 6813 ON CABIN WALKTHROUGH FOUND ROWS 18-26 DEF AISLE ILLUMINATION EMERGENCY LIGHTS ON AND WOULD NOT EXTINGUISH. CORRECTIVE ACTION: T/S PER B757 WDM 33-51-13. R/R RELAY K10570 AND BATTERY PACK/ POWER SUPPLY. FOUND AFT F/A PANEL TEST SWITCH ON, TURNED OFF, EMERGENCY LIGHTS TEST OK REF B757 AMM 33-51. (6638697)

Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 84,597 hrs · 20,659 cycles

SHIP 6813 IR DOOR SLIDE LIGHT ON WITH SLIDE NOT ARMED. CORRECTIVE ACTION: CYCLED A/C POWER, 1R DOOR SLIDE ILLUMINATES WHEN DOOR IS ARMED. (6064014)

Part: DOOR — FOD (L4) · airframe 84,583 hrs · 20,656 cycles

SHIP 6813 4L DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS, OPENED AND CLOSED DOOR SEVERAL TIMES. OPS CHK NML. (6064006)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 84,283 hrs · 20,589 cycles

SHIP 6813 ROW 33 & 35 AILSE EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: FOUND LOOSE ELECTRICAL CONNECTION ON ROW 32. DISCONNECTED & RECONNECTED ELECTRICAL CONNECTOR. EMERGENCY EVAC LIGHTS OPS CHECKED GOOD. (6053911)

Part: D-RING — UNSECURE (DOOR SLIDE) · airframe 84,158 hrs · 20,559 cycles

SHIP 6813 L2 CABIN DOOR SLIDE "D" RING NO VISIBLE. CORRECTIVE ACTION: RESECURED L2 ENTRY DOOR SLIDE SURVIVAL KIT "D" RING PER B757 AMM 25-66-01. CKS GOOD. (5605452)

Part: INDICATOR — INOPERATIVE (R4 DOOR) · airframe 84,061 hrs · 20,535 cycles

SHIP 6813 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:608. CORRECTIVE ACTION: R/R NO 04 RH PASS DOOR PROX SENSORS A/B S10224/S10225 (REF B757 WDM 25-66-11) TO RESTORE INOP SLIDE INDICATOR LIGHT FUNCTION. (0382001)

Part: SIGN — LOOSE (CABIN) · airframe 83,684 hrs · 20,458 cycles

SHIP 6813 CEILING EXIT SIGN OVERHEAD 2L DOOR IS LOOSE. CORRECTIVE ACTION: SECURED CEILING EXIT LIGHT AS PER B757 AMM 33-51. (5317584)

Part: AXLE — BROKEN (NLG) · airframe 83,192 hrs · 20,346 cycles

SHIP 6813 AFTER SETTING THE PARKING BRAKE AT THE GATE, RAMP AGENT INFORMED US LEFT NOSE WHEEL HAS SEPERATED FROM AXLE. UPON INSPECTION, AGREE/NOTICE THE SEPERATION AND ASSOCIATED SHEERED METAL/DAMAGE. SMOOTH LANDING AND AIRCRAFT HANDLED/TAXIED NORMALLY. CORRECTIVE ACTION: R/R NLG AXLE PER B757 CMM 32-21-49 REV 80 07/15/2022. REMOVED AND REPLACED LT & RT NOSE WHEEL/TIRE ASSY REF B757 AMM 32-45.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,603 hrs · 20,199 cycles

SHIP 6813 DOOR 1R SLIDE LIGHT REMAINED ON AFTER BEING DISARMED. CORRECTIVE ACTION: DEBRIS BY PROX SWITCH. CLEANED DEBRIS, ALL INDICATIONS NORMAL. CYCLED DOOR MULTIPLE TIMES. ALL OPS NORMAL. (5514950)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,525 hrs · 20,181 cycles

SHIP 6813 GATE CALL FOR METAL ROD FOUND AT DOOR 1L DOOR SILL. CORRECTIVE ACTION: INSPECTED GVT OF DOOR 1L SLIDE/GIRT BAR. OPERATIONAL CHECK OF ARMING DOOR 1L OK. REF B757 AMM 52-11. (5514934)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,362 hrs · 20,145 cycles

SHIP 6813 R1 SLIDE LIGHT ILLUMINATED WHEN DOOR IS DISARMED. CORRECTIVE ACTION: CYCLED ARM LEVER. SLIDE LIGHT WORKS NORMAL. (5061992)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,309 hrs · 20,132 cycles

SHIP 6813 FUSELAGE / AFT CARGO FRAME / AT STA 1460 / S-25L & S-27L / EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 613990-14.(0098187)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,309 hrs · 20,132 cycles

SHIP 6813A.A EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA STA 1460 BTW S-25L TO S-27L. CONTACT LIAISON ENGINEERING FOR REQUIRED ACTIONS FOR THE REPAIRED AREA PRIOR TO FURTHER FLIGHT IN REF. TO AMDS 5311-01227-01A STEP 2. CORRECTIVE ACTION: SUMMARY OF NRC 00170: PERMANENT REPAIR WAS PERFORMED ON FRAME SECTION ON STA 1460 BTW S-24L TO S-24L. PER ER/A 613990-14AD REV ORG. SECTION I AND PRI 613990-14 AD REV 1. (0098330)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,309 hrs · 20,132 cycles

SHIP 6813 DENTS #11 0.762", Y=0.011", A/Y=69.509, #12 A= 0.935", Y=0.016", A/Y=57.147, #13 A=1.171", Y=0.019", A/Y=61.721, #45 A=1.055", Y=0.017", A/Y=60.622 AND #46 A=0.995", Y=0.010", A/Y= 99.991 OUT LIMITS DUE TO DISTANCE TO SPLICE FASTENER. CORRECTIVE ACTION: REF ERA 614095-14. (0096766)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,309 hrs · 20,132 cycles

SHIP 6813 AD - DAMAGES WERE FOUND IN RH ENG DRAG FTG CLAMP-UP HOLES AS FOLLOW: HOLE #11 CORROSION ON FITTING ALL AROUND, HOLE #12 CORROSION ON FITTING AT 11 CLOK POSITION AND SCRACTCHES ON SKIN AND FITTING BETWEEN 6 TO 9 CLOCK POSITION, HOLE #14 CORROSION ON SKIN AT 6 CLOCK POSITION, HOLE #16 CORROSION ON SKIN AT 10 CLOCK POSITION AND ON FITTING BETWEEN 2 TO 6 CLOCK POSITION, HOLE #18 SCRATCHES ON SKIN AND FITTING ALL AROUND, IN REFERENCE TO JOB 114-0001 CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00229: [AD] RH ENG DRAG FTG CLAMP-UP HOLES 12 AND 18 WERE CLEANED PER DELTA PS 900-1-2-1 NO. 01, HOLES 11 AND 14 WERE REPAIRED PER AMDS 5720-01100-05B AND HOLE 16 WAS REPAIRED PER PRI 584089-14 REV. 1 AND ER/A 584089-14AD REV. C SECTION VI

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,309 hrs · 20,132 cycles

SHIP 6813 DENTS #10, #12 AND #14 THEY ARE OUT LIMITS DUE TO DISTANCE TO SPLICE FASTENER ON UPPER SKIN FROM BSTA 740 TO BSTA 879 BTW S-4RH TO S- 10RH AT FUSELAGE. CORRECTIVE ACTION: REF ERA 614023-14. (0096908)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,309 hrs · 20,132 cycles

SHIP 6813 DAMAGES WERE FOUND IN RH ENG DRAG FTG CLAMP-UP HOLES AS FOLLOW: HOLE #1 CORROSION ON FITTING AT 12 CLOCK POSITION, HOLE #2 CORROSION ON FITTING BETWEEN 12 TO 5 CLOCK POSITION, HOLE #7 SCRATCHES ON FITTING BETWEEN 4 TO 6 CLOCK POSITION, HOLE #8 CORROSION ON SKIN BETWEEN 4 TO 5 CLOCK POSITION, HOLE #9 SCRATCHES ON SKIN ALL AROUND, HOLE #10 SCRATCHES ON SKIN ALL AROUND. CORRECTIVE ACTION: SUMMARY OF NRC 00228: AD RH ENG DRAG FTG CLAMP-UP HOLES 1,2,7,8,9 AND 10 WERE REPAIRED PER DELTA PS 900-1-2-1 NO. 01 AND CARD 5720-01100-04B. (0081562)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,461 hrs · 19,281 cycles

FOUND EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD.

Part: SPOILER — FAILED · airframe 76,858 hrs · 18,907 cycles

SHIP 6813 - FCNT - DUE TO RIGHT OUTBOARD SPOILER CAUSING SIGNIFICANT ROLL TO THE RIGHT WHEN AIRBORNE. CORRECTIVE ACTION: REPLACED #12 SPOILER.

Part: LANYARD — BINDING · airframe 76,771 hrs · 18,884 cycles

SHIP 6813 #4 L DOOR ARM INDICATOR DOES NOT INDICATE FULLY DISARMED. CORRECTIVE ACTION: REMOVED SLIDE COVER AND FOUND SLIDE WOULD NOT DISARM DUE TO LANYARD BINDING IN ARMING MECHANISM. FREED ARMING MECHANISM AND CYCLED ARM/DISARM OPS CHECK NML PER B757 AMM 52-11. (8676482)

Part: LIGHT — BROKEN · airframe 76,713 hrs · 18,872 cycles

SHIP 6813 SEAT 4C AFT AISLE EMERGENCY LIGHT ASSY BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT 4C AFT AISLE EMERGENCY LIGHT ASSY PER B757 AMM 33-51. OPS NML. (8676473)

Part: NONE — NONE · airframe 75,548 hrs · 18,603 cycles

SHIP 6813 PERMANENT REPAIR ON LH WING DRY BAY PANEL. CORRECTIVE ACTION: SUMMARY OF NRC 00072 : LH WING DRY BAY PANEL BTW WSTA 285-313 WAS REPAIRED PER ERA 583546-14 REV A SECTION II. (2078476)

Part: NONE — NONE · airframe 75,548 hrs · 18,603 cycles

SHIP 6813 OUT OF LIMITS COMPENSATOR INDICATOR ON SNUBBER AT 4R PASSENGER DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00077: R4 PASSENGER DOOR WAS REMOVED AND SAME R4 PASSENGER DOOR WAS INSTALLED PER B 757-200 AMM 52-11 AND ROTARY SNUBBER WAS REMOVED AND SERVICEABLE SNUBBER WAS INSTALLED PER B757-200 AMM 52-11. (2077700)

Part: NONE — NONE · airframe 75,548 hrs · 18,603 cycles

SHIP 6813 A.A. DISBOND OF 1.200 IN X 1.000 IN AT UPPER SKIN OSS 600 LE SLAT 9 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF NRC 00032:DURING REPAIR PROCEDURE ON UPPER SKIN OSS 600 LE SLAT 9 TRAILING EDGE WEDGE PER B757-200 S.R.M. (2075374)

Part: NONE — NONE · corrosion level 2 · airframe 75,548 hrs · 18,603 cycles

SHIP 6813 CORROSION ON UPPER CUTOUT BTW STA 1640 AND 1680 AT 4RH PASSENGER DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00030. AREA WAS REPAIRED PER ETI-57-21-620 REV 1 AND ER/A 596413-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (2075288)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 74,226 hrs · 18,320 cycles

SHIP 6813 OXYGEN PANEL MASK DEPLOYED / LOCATIONS: 43. CORRECTIVE ACTION: INSPECTED MASKS PER B757 AMM 35-21. ALL GOOD. CLOSED AND SECURED PSU. (1895298)

Part: WARNING LIGHT — FALSE ACTIVATION (GIRT BAR) · airframe 73,315 hrs · 18,121 cycles

SHIP 6813 AFT RIGHT ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT. CORRECTIVE ACTION: INSPECTED GIRT BAR FOR DEBRIS, NO DEBRIS NOTED. ARMED AND DISARMED DOOR SEVERAL TIMES OPS CHECK NORMAL LIGHT ILLUMINATED EVERY TIME. NO DEFECTS NOTED. (1793397)

Part: HARNESS — DAMAGED (L1 DOOR SLIDE) · airframe 73,206 hrs · 18,094 cycles

SHIP 6813 DOOR IL SLIDE DROPPED DOWN ON TAKEOFF. CORRECTIVE ACTION: REMOVED 1L DR SLIDE PER WORKCARD & PERF INSPECTION OF HINGES & SLIDE. FOUND 1L DR SLIDE HARNESS DAMAGED & BLOCK ASSEMBLY. REINSTALLED 1L DOOR SLIDE PER AMDS W/C NBR. (7426204)

Part: NONE — NONE · airframe 75,548 hrs · 18,603 cycles

SHIP 6813 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 584089-14 REV A. CORRECTIVE ACTION: REF ERA 584089-14AD REVISED TO REV B. (1771281)

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,349 hrs · 17,463 cycles

SHIP 6813 EMERGENCY LIGHTS INOP IN FWD LT GALLEY AND FIRST CLASS SEATS. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY IN FIRST CLASS IAW B757 AMM 33-51. OPS NML. (7123483)

Part: BULKHEAD — CORRODED (BS 900) · airframe 69,889 hrs · 17,367 cycles

(AIRCRAFT 6813, L/P 1504625) CORROSION ON BULKHEAD STA: 900 BTW PROJECTION 28L TO 28R LOWER ARAE AT FWD CARGO COMPARTMENT, TASK: 5330-125-01L. CORRECTIVE ACTION: REPAIRED PER ER/A 585456-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-57-20-036 REV 7 AND REPAIR APPROVAL IS LIMITED TO 50,000 TOTAL FLIGHT CYCLES.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 69,717 hrs · 17,335 cycles

(AIRCRAFT 6813, L/P 6993107) DURING SVC FOUND E-PATH LIGHTS ROW 28-35 INOP. CORRECTIVE ACTION: T/S FOUND PUSHED BACK PIN AT SEAT 27. RESEATED PIN REF SPWM CHAP 20.

Part: LIGHT — UNKNOWN (R2 DOOR) · airframe 69,600 hrs · 17,313 cycles

SHIP 6813 R2 DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: RESECURED 2R SLIDE LT. NO TROUBLE NOTED. OPS CHK NML. VERIFIED GIRT BAR/SLIDE LT OPERATION NORMAL FOR ARM/DISARM. REF B757200ER AMM 52-11. (7208264)

Part: SENSOR — FALSE INDICATION (L2 GIRT BAR) · airframe 69,600 hrs · 17,313 cycles

(AIRCRAFT 6812, L/P 7208258) L2 DOOR SLIDE LIGHT REMAINS ILLUMINATED. CORRECTIVE ACTION: R/R'D GIRT SENSOR S10218 PER WDM 25-66-11.

Part: HEATER — FOULED (L4 DOOR) · airframe 69,351 hrs · 17,265 cycles

(AIRCRAFT 6813, L/P 6343754) F/A REPORTED INTERMITTENT "PLASTICKY" SMELL AT 4L DOOR DURING FLIGHT. BECAME VERY STRONG TAXIING INTO GATE, REPORTED FEELING LIGHT HEADED FROM SMELL. CORRECTIVE ACTION: PUT AIR/GND RELAY SYS. 2 IN AIR MODE. PLASTICKY SMELL PRESENT. FOUND 4L DOOR HEATER FOULED AND DIRTY. R/R 4L DOOR HEATER AS PER AMM 21-45.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,312 hrs · 17,257 cycles

(AIRCRAFT 6813, L/P 1428386) CORROSION ON UPPER/LWR SKIN AT RH SIDE PANEL FROM STA 1530 TO 1640 AT AFT CARGO. CORRECTIVE ACTION: CORROSION LEVEL 2, REPLACED PER B757-200 SRM 51-40-02 PAR 4 AND 7.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 69,271 hrs · 17,250 cycles

(AIRCRAFT 6813, L/P 1426411) CORROSION WAS FOUND IN ALL OPEN HOLES FROM 1 TO 10 AND ADDITIONALLY CRACKS WERE FOUND IN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE. WC 5720-01100-0101B STEP 26. CORRECTIVE ACTION: CORROSION: LEVEL 2 PERMANENT REPAIR WAS PERFORMED ON RH OUTER WING / UPPER SURFACE /SKIN COMMON TO DRAG FITTING PER ER/A 584089-14AD REV. ORG.SECTION I AND ETI-57-19-181 REV. 13.

Part: SKIN — CRACKED (RT WING) · airframe 73,055 hrs · 18,061 cycles

SHIP 6813 WHEN PERFORMING THE INSPECTIONS REQUESTED PER WC 5720-01100-0101B, CRACKS WERE FOUND ON THE BOREHOLES OF THE RHS WING UPPER SKIN HOLES #2, 4, 5, 12, 13, 16, 17 & 18, COMMON TO THE PYLON SUPPORT DRAG FITTINGS. SUBSEQUENTLY, CRACKS WERE REMOVED BY CONCENTRICALLY REAMING HOLES #12, 16 & 18, AND INSTALLING OVERSIZE FASTENERS ON THOSE LOCATIONS. CORRECTIVE ACTION: REF ERA 584089-14 REV A. (1425497)

Part: STRUCTURE — SCRATCHED (LT WING) · airframe 69,271 hrs · 17,250 cycles

(AIRCRAFT 6813, L/P 1425720) SCRATCH ON DRY BAY (INNER FACE OF SETTLEMENT AREA) IN LH MAIN FUEL TANK (GET ACCESS THRU 541CB PANEL). CORRECTIVE ACTION: REPAIRED PER ER/A 583546-14 REV. ORIGINAL SECTION I TIME-LIMITED REPAIR AND ETI-57-19-194.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

CORROSION WAS FOUND ON FLOOR SUPPORT BTW BS 1500 TO 1520 RBL 10.45. REPAIRED IAW SRM 53-00-53 REP 1 FIG 201.

Part: LEAF SPRING — DAMAGED (GIRT BAR) · airframe 69,270 hrs · 17,249 cycles

R4 DOOR LEAF SPRING WON'T HOLD THE GIRT BAR SLIDER AND SLIDER RIDES OVER THE SPRING. GIRT BAR OF R4 DOOR WAS REMOVED AND INSTALLED IAW AMM 25-66-10. SPRINGS OF GIRT BAR WERE REPLACED IAW SRM 51-40-02, PAR 4, AND GIRT BAR WAS ADJUSTED IAW AMM 52-11-25.

Part: PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

CORROSION ON LH SIDE PANEL FROM BS 1310 TO 1410 AT AFT CARGO COMPARTMENT. REPLACED WITH NEW SIDE PANEL. IAW SRM, 51-40-02 PAR. 4 AND 7.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 69,270 hrs · 17,249 cycles

CRACK ON UPPER SKIN AT RH OUTBD MAIN FLAP STA WS=509 APROX AT RT WING. CRACK ON UPPER SKIN AT RH OUTBD MAIN FLAP STA WS=509 APROX AT RH WING WAS REPAIRED PER B-757 S.R.M. (1415444)

Part: SKIN — DEBONDED (NR 9 SLAT TE) · airframe 69,270 hrs · 17,249 cycles

DEBONDED AREA WAS FOUND ON REPAIR DOUBLER AT FSS 619 AT SLAT 9 TRAILING EDGE WEDGE LOWER SKIN. THE NR 9 SLAT TRAILING EDGE WEDGE LOWER SKIN WAS REPLACED IAW SRM.

Part: SKIN — DENTED (BS 600-640) · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1408932) TWO DENTS ON FUSELAGE SKIN, NEAREST TO TWO EXISTING MON DENTS, FROM STA 600 TO 640 BTW ST15 L -ST18 L. FUS. CORRECTIVE ACTION: DENTS ON FUSELAGE SKIN WERE REPAIRED PER. ETI-57-19-187 REV. 2 AND E/RA 584001-14AD REV. ORIG.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 69,351 hrs · 17,265 cycles

(AIRCRAFT 6813, L/P 1409921) DISBONDED AREAS WERE FOUND ON SLAT 2 TRAILING EDGE WEDGE AT FSS 704 LWR SKIN, UPPER SKIN AND FSS 599 UPPER SKIN (REF. CARD 5740-04445-05B). CORRECTIVE ACTION: REPAIRED PER B-757-200-S.R.M. 57-43-02-2R-1 AND PER B-757-200 S.R.M. 51-70-10-2R-4.

Part: FITTING — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1405744) CORROSION OUT OF LIMITS ON FITTINGS (2 EA) AT STA 567 AND 607. CORRECTIVE ACTION: CORROSION LEVEL 2. REPLACED PER B757-200 SRM 51-20-01, 51-40-05.

Part: NONE — NONE · airframe 75,548 hrs · 18,603 cycles

SHIP 6813 LH WING DRY BAY PANEL WSTA 285-313 FOUND WITH CRACK. TEMP REPAIR PER ER/A 583546-14. CORRECTIVE ACTION: REF ERA 583546-14. (1405391)

Part: SKIN — CORRODED (BS 1530-1640) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1401535) CORROSION ON UPPER/LWR SKIN ON LH SIDE PANEL FROM STA 1530 TO 1640 AT AFT CARGO. CORRECTIVE ACTION: REPLACED PER. B757-200 SRM. 51-40-02 PAR. 4 AND 7.

Part: SKIN — CORRODED (BS 1440-1530) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1401792) CORROSION ON UPPER/LWR SKIN AT RH SIDE PANEL FROM STA 1440 TO 1530 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED PER B757-200 SRM. 51-40-02 PAR. 4 AND 7.

Part: DECK PLATE — CORRODED (BS 1716) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1400419) CORROSION OUT OF LIMITS WERE FOUND ON DECK PLATE AT STA 1716, LBL 26. CORRECTIVE ACTION: CORROSION LEVEL 2 PERMANENT REPAIR WAS PERFORMED ON ABOVE AREA OUT OF LIMITS PER B757-200 SRM 53-60-51-2R PROCEDURE 7.

Part: SUPPORT FITTING — CORRODED (GALLEY) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

SHIP 6813 CORROSION ON GALLEY FITTING SUPPORTS (2 EA) AT PASSENGER CABIN (CPAX) GALLEY 4B. CORRECTIVE ACTION: SUMMARY OF NRC.00413 CORROSION ON GALLEY FITTING SUPPORTS ( 2 EA ) INSPECTION WAS PERFORMED AND NO MORE CORROSION WAS FOUND PER B757-200 SRM, MEASUREMENT THICKNESS WAS ACCOMPLISHED PER B757-200 NDT MANUAL, ORIGINAL THICKNESS ON GALLEY FITTING SUPPORTS ( 2 EA ) ARE OUT OF LIMITS PER D.W.G. NEW FITTING MUST BE INSTALLED ON CARD. (1399369)

Part: PANEL — CORRODED (BS 654) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1398610) CORROSION WAS FOUND OUT OF LIMITS AT LH SIDE PANEL AT STA 654. CORRECTIVE ACTION: REPAIRED PER. B757-200 SRM. 53-00-53 REP 2.

Part: PANEL — CORRODED (BS 1380-1440) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1397281) CORROSION ON RH SIDE PANEL FROM 1380 TO 1440 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL 2. SIDE PANEL WAS REPLACED PER B757-200 SRM. 51-40-02 PAR. 4 AND 7.

Part: DECK PLATE — CORRODED (BS 1681) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1389941) CORROSION OUT OF LIMITS WAS FOUND ON DECK PLATE AT STA 1681.8, LBL 25. CORRECTIVE ACTION: REPAIRED PER B757-200 SRM 53-60-51 REPAIR 2 FIGURE 201 ALTERNATIVE I.

Part: SUPPORT — CORRODED (BS 1640-1660) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1390357) CORROSION ON GUTTER SUPPORT BTW STA Y=1640 / 1660 BTW RBL=55 AT PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PER. B757-200 SRM. 51-40-02 PAR.4 AND 7.

Part: SUPPORT — CORRODED (BS 1660-1680) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1390218) CORROSION ON GUTTER SUPPORT BTW STA Y=1660 / 1680 BTW LBL=55 AT PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PER.B757-200 SRM. 51-40-02 PAR. 4 AND 7.

Part: SUPPORT — CORRODED (BS 1640-1660) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1390246) CORROSION ON GUTTER SUPPORT BTW STA Y=1640 / 1660 BTW LBL=55 AT PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PER B757-200 SRM. 51-40-02 PAR. 4 AND 7.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 69,270 hrs · 17,249 cycles

(AIRCRAFT 6813, L/P 1384123) CORROSION ON FLOOR BEAM PREVIOUSLY REPAIRED (UPPER SURFACE) AT PASSENGER CABIN STA. 365, BTW RBL 27 AND RBL 31. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 53-00-51 REP 8.

Part: LIGHT — NOT REPORTED (R1 DOOR SLIDE) · airframe 69,264 hrs · 17,248 cycles

(AIRCRAFT 6813, L/P 1353213) ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - 1R SLIDE LIGHT. CORRECTIVE ACTION: R/R 1R SLIDEARM LIGHT PER B757 AMM 33-51.

Part: PROXIMITY SENSOR — INOPERATIVE (R2 DOOR SLIDE) · airframe 68,768 hrs · 17,152 cycles

SLIDE INDICATOR LIGHT INOPERATIVE. TROUBLESHOT IAW SSM 25-66-01. R & R THE R2 DOOR AFT PROX SENSOR IAW AMM. OPS CHECKED NORMAL.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 67,618 hrs · 16,935 cycles

SHIP 6813 1R ENTRY DOOR ARMED LIGHT INOP. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR. DOOR ARMS/DISARMS NORMALLY. (4742178)

Part: WARNING SYSTEM — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 67,602 hrs · 16,932 cycles

SHIP 6813 EICAS CAUTION MSG IN FLIGHT " R EMER DOOR" COMPLIED WITH QRH OCCURRED AT FL 320 IN LIGHT TURB. CORRECTIVE ACTION: CLEANED DOOR AREA PER FIM. NO CAUTION PRESENT. (4742155)

Part: DOOR — FOD (R4 DOOR) · airframe 67,143 hrs · 16,848 cycles

4R DOOR SLIDE LIGHT NOT ILLUMINATING. CORRECTIVE ACTION: CLEANED DEBRIS. (5916190)

Part: NOT REPORTED — MALFUNCTIONED (R4 DOOR) · airframe 67,177 hrs · 16,854 cycles

AT DEPARTURE 4R DOOR INDICATION MSG ON UPPER EICAS. REMOVED AND REPLACED S10225 PER B757 WDM 25-66. OPS CK NORMAL.

Part: PROXIMITY SENSOR — DIRTY (R4 DOOR) · airframe 66,926 hrs · 16,807 cycles

(AIRCRAFT 6813, L/P 1076601) THE 4R DOOR SLIDE ENGAGEMENT LIGHT WILL NOT ILLUMINATE. CLEANED GIRT BAR MECHANISM AND PROX SENSOR AND OP CK NML PER AMM 52-11 OK FOR SVC.

Part: TIRE — FAILED (NR 7 MLG) · airframe 66,570 hrs · 16,740 cycles

A/C THAT DEPARTED LIS AFTER US REPORTED TIRE DEBRIS ON THE RUNWAY. FOUND #7 TIRE BLOWEN AND DAMAGED TO AFT T/E FLAP. PERFORMED INSPECTION FOR FURTHER DAMAGE PER B757 AMM 05-51. NO OTHER DAMAGE FOUND PERFORMED TEMP REPAIR PER B757 SRM 57-53-01. PAGE 105 PAR. D. A/C OK FOR SVC. (LP# 5646338)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 66,326 hrs · 16,692 cycles

SHIP 6813 GOT R EMERG DOOR EICAS DURING MOD TURB QRH COMPLIED WITH EICAS MSG WENT AWAY PASSING 15000 FEET. CORRECTIVE ACTION: PERFORMED INSPECTION OF 3R EMERG DOOR PER AMM 52-21 NO ABNORMAL INDICATIONS. (5652548)

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 65,758 hrs · 16,578 cycles

1L ENTRY DOOR WILL NOT ARM. FOUND DEBRIS ATTACHED TO GIRT BAR. REMOVED DEBRIS. ARM AND DISARMED 1L DOOR. OPS CK NML.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,518 hrs · 16,160 cycles

DURING A SERVICE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE FROM ROWS 36 - 44. TROUBLESHOT TO A BROKEN WIRE. FOUND MISSING LIGHT ASSY AT ROW 37D AND SHORTED WIRES. R & R LIGHT ASSY AND R & R FUSE IAW SWPM 20 OPS CHECKED NORMAL.

Part: DOOR — OUT OF SEQUENCE (L2) · airframe 62,356 hrs · 15,950 cycles

L2 DOOR WILL NOT FULLY CLOSE AND ARM. LEVER ONLY GOES PARTLY CLOSED AND CANNOT ARM. DOOR OUT OF SEQUENCE. OK FOR SERVICE.

Part: COVER — UNSECURE (GIRT BAR) · airframe 62,036 hrs · 15,880 cycles

L2 DOOR ARMING LEVER WILL NOT ARM OR DISARM. REPAIRED THE GIRT BAR PROXIMITY SWITCH COVER IAW ERA 560980-14 SECTION V. COVER IS SECURE.

Part: DOOR — FOD (R4) · airframe 61,171 hrs · 15,712 cycles

R4 DOOR WOULD NOT ARM DURING PUSHBACK. REMOVED FOD FROM THE DOOR. OPS NORMAL, DOOR ARMS NORMAL.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 60,794 hrs · 15,636 cycles

(AIRCRAFT 6813, L/P 3974057) DOOR 2 LEFT EMERGENCY EXIT MARKING LIGHT HAS 2 BURNED OUT BULBS. BULB REPLACED FROM SHIPS SPARES AMM REF 33-40-00.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 60,587 hrs · 15,587 cycles

VERT STAB / RT FWD TORQUE BOX LOWER PANEL. REPAIR OF OUTER SKIN DAMAGE.

Part: SNUBBER — NO TEST · airframe 60,587 hrs · 15,587 cycles

L2 DOOR SNUBBER FAILED PROTRUSION INSPECTION. REPLACED THE DOOR SNUBBER IAW AMM 52-11-10.

Part: LEVER — LACK OF LUBE (PAX DOOR) · airframe 60,575 hrs · 15,584 cycles

L4 DOOR ARMING LEVER NOT FULLY INTO POSITION. CLEANED DEBRIS FROM THE ARMING LEVER AND LUBRICATED. OPS CHECKED NORMAL IAW AMM 52-12.

Part: GUARD — DETACHED (GIRT BAR) · airframe 60,039 hrs · 15,464 cycles

L2 DOOR GIRT BAR GUARD CAME OFF. REPLACED THE GIRT BAR GUARD AND OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: GUARD — DETACHED (GIRT BAR) · airframe 60,039 hrs · 15,464 cycles

GIRT BAR GUARD AT THE R1 DOOR FELL OFF. PUT GIRT BAR GUARD BACK IN PLACE, OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: DOOR — DIRTY (L4) · airframe 60,033 hrs · 15,463 cycles

UNABLE TO ARM THE L4 DOOR. REMOVED DEBRIS. DOOR OPS CHECKED OKAY. DOOR ARMS AND DISARMS IAW AMM 52-14.

Part: DOOR — MALFUNCTIONED (L3) · airframe 59,940 hrs · 15,446 cycles

L3 DOOR WILL NOT ARM FOR DEPARTURE. DOOR HARD TO ARM. CYCLED DOOR. OPERATED IAW AMM 25-66. VERIFIED GIRT BAR MECHANISM. FULLY ARMS AND DISARMS. CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: DOOR — DAMAGED (R1) · airframe 59,088 hrs · 15,292 cycles

DAMAGED R1 DOOR BUTTERFLY STICKING OUT. REPLACED R1 DOOR IAW AMM 52-11.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 58,757 hrs · 15,234 cycles

DAMAGE OBSERVED AFT CARGO DOOR LOWER FORWARD EDGE AT LIP OF OUTER SKIN. 2 DENTS NOTED AT LOWER FORWARD CORNER. FOUND CRACK APPROX 1/4 INCH LONG. REMOVED CRACK PER SRM 52-30-01. PERMANENT REPAIR PER ERA 559211-14 C/W.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,993 hrs · 14,873 cycles

SEAT ROWS 24 AND 25 EMERGENCY LIGHTS WILL NOT ILLUMINATE DURING TEST. REPLACED THE BATTERY PACK AND POWER SUPPLY IAW AMM 33-51.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 55,776 hrs · 14,639 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT IAW WDM 33-51-12, FOUND CONNECTOR D9352J NOT GETTING POWER. FOUND POOR CONNECTION AT D9352J, REPAIRED IAW SWPM 20-61, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,867 hrs · 14,285 cycles

RED EMERGENCY AISLE LIGHT INOPERATIVE. R & R EMERGGENCY ESCAPE LIGHT IAW AMM 25-61. REPLACED M10919 POWER SUPPLY IAW AMM 33-51, OPS CK GOOD.

Part: GIRT BAR — MALFUNCTIONED (L4 DOOR) · airframe 53,560 hrs · 14,207 cycles

WHEN DOING A REPETITIVE CHECK FOR THE L-4 DOOR. THE GIRT BAR WOULD NOT ENGAGE OR MOVE AT ALL. PINNED L4 SLIDE. R & R L-4 SLIDE GIRT BAR BELL CRANK ASSY. PERFORMED GIRT BAR MECHANISM SYS TEST IAW AMM 52-11, CHECKS OK. REMOVED SLIDE PIN AND INSTALLED BUSTLE. ALL RII COMPLIED WITH.

Part: GUIDE VANE — CORRODED (RT ENGINE) · airframe 52,781 hrs · 14,020 cycles

RT ENGINE EXHAUST GUIDE VANES APPEAR BADLY CORRODED, RUSTY. PERFORMED GVI OF RT ENGINE EXHAUST EXIT GUIDE VANES. NO TROUBLE FOUND AND NO DAMAGE NOTED ON GUIDE VANES. REF AMM 78-11 & 72-33.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 52,624 hrs · 13,977 cycles

RED EMERGENCY LIGHT AND WHITE EMERGENCY LIGHTS INOPERATIVE AT ROW 36. FOUND PUSHED PINS ON EMERGENCY LIGHT CONNECTOR FOR LIGHT AT ROW 36 D, E, F. RESEATED PINS IAW SWPM 20-10. ALL EMERGENCY LIGHTS OPERATE NORMAL. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (BS 760-800) · airframe 52,357 hrs · 13,909 cycles

UPPER FUSELAGE SKIN HAS DENT AT BS 760- 800, S8R TO S9R. INSPECTED AND MEASURED DENT ON EXTERIOR FUSELAGE BS 760 TO 800, STR 8R-9R A/Y=100, FOUND WITH IN LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III.

Part: FLOOR SUPPORT — DAMAGED (E/E BAY) · airframe 51,745 hrs · 13,779 cycles

SUPPORT BRACKET BELOW FLOOR PANEL IN E/E ADJACENT TO P37 PANEL DAMAGED. REPLACED FLOOR SUPPORT IN E/E PN 284N 1035-256, REF DWG 2841392, FLOOR PANELS AND COVERS INSTALLED.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 51,266 hrs · 13,699 cycles

A ONE INCH HOLE IN THE AFT CARGO FLOOR FIVE FEET FWD OF OF DOOR. INSTALLED TEMP REPAIR IAW ERA 489384-14MA.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,813 hrs · 13,437 cycles

MULTIPLE DENTS ON FUSELAGE SKIN IN AREA OF WIFI DOUBLER. FABRICATED & INSTALLED DOUBLERS.

Part: LIFE RAFT — MISINSTALLED · airframe 49,790 hrs · 13,431 cycles

MAINTENANCE FOUND THAT LIFE RAFT COMPARTMENT DOOR IS NOT CLOSING WHEN RAFT IS INSTALLED BETWEEN LAV C AND D DUE TO POSSIBLY BEING PACKED INCORRECTLY. LIFE RAFT ASSY WAS R & R. L

Part: STRAP — DAMAGED (BS 1520) · airframe 49,790 hrs · 13,431 cycles

FLOORBEAM STABILIZATION STRAP AT FS 1520, RBL 45.5 DAMAGED. REMOVED DAMAGED AREA OF FLOORBEAM RBL 45.5 STABILIZER STRAP FS 1520. INSTALLED REPAIR IAW SRM 53-00-51, REP 12, FIG 201. LP1898989.

Part: FRAME — GOUGED (BS 1280) · airframe 49,790 hrs · 13,431 cycles

PREVIOUS REPAIR SPLICE AT STA 1280, FRAME STR 10L IS GOUGED. REMOVED DAMAGE ANGLE, FABRICATED NEW ANGLE FROM 70750 .071 PO ST-00003940. HEAT TREATED TO 7075T6 IAW FAS FORM, FAS 0155, REV 12, DIM 13".500 X 4".250, AND INSTALLED NEW ANGLE IAW SRM 53-00-07. REPAIR 1, FIG 202, INSTALLED REPAIR ID IAW PS 900-5-1. LP1894803.

Part: FRAME — DAMAGED (BS 1280) · airframe 49,790 hrs · 13,431 cycles

PREVIOUS REPAIR AT FS 1280, FRAME STR 10R IS GOUGED. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE FROM 7050, .071 PO ST-00003940. HEAT TREATED PART TO 7075T6 FOR FAS FORM, FAS 0115, REV 012, DIM 13".500 X 4".250 AND INSTALLED NEW ANGLE IAW SRM 53-00-07, REPAIR 1, FIG 202. LP1894796.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 49,788 hrs · 13,430 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. SECURED LOOSE LENS AT 19D.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 49,788 hrs · 13,430 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. SECURED LOOSE LENS AT 19D.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,656 hrs · 13,399 cycles

LIGHT BOX AT 32DEF DAMAGED. EMERGECNY PATH LIGHTING, INSTALLED LIGHT BOX ASSY ON SEAT 32 DEF.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,480 hrs · 13,357 cycles

EMERGENCY LIGHT DAMAGED. REPAIRED. EMERGENCY LIGHT OPS CHECKED NORMAL.

Part: LIGHT — DETACHED (SEAT 19D) · airframe 45,698 hrs · 12,591 cycles

EMERGENCY LIGHT BROKEN OFF SEAT 19D. SECURED LIGHT AT 19D. CHECKS OK.

Part: LIGHT — INOPERATIVE (SEAT 19DEF) · airframe 45,305 hrs · 12,505 cycles

EMERGENCY LIGHT ON SEAT 19 FED INOPERATIVE. INSTALLED NEW ATTACHMENT HARDWARE, EMERGERNCY LIGHT, OPS CHECKED GOOD, OK FOR SERVICE.

Part: GROUND STUD — LOOSE (EMERGENCY LIGHTS) · airframe 44,848 hrs · 12,415 cycles

EMERGENCY LIGHT AT 19-20 DEF OVERHEAD, INOPERATIVE. FOUND GROUND TERMINAL LOOSE IN CEILING AREA ABOVE LIGHT ASSY. SECURED AND OPS CHECKED OK.

Part: SKIN — DENTED (BS 310-440) · airframe 44,032 hrs · 12,251 cycles

FUSELAGE SKIN BS 310-440 S4L - 4R DENTED. ALL DENTS ACCEPTABLE, EXCEPT TWO WHICH WERE REPAIRED PER ER/A 56-520592-14AD.

Part: SKIN — DENTED (BS 440-900) · airframe 44,031 hrs · 12,250 cycles

FUSELAGE SKIN BS 440-900 S4L-4R DENTED. DENTS TRIMMED OUT AND REPAIRED WITH DOUBLERS IAW ER/A 56-520596-14.

Part: SKIN — DENTED (BS 1661-1681) · airframe 44,031 hrs · 12,250 cycles

FUSELAGE SKIN BS 1661 - 1681, S2-4R DENTED. REPAIRED IAW ER/A 519298-14.

Part: FRAME — DENTED (BS 520) · airframe 44,031 hrs · 12,250 cycles

FUSELAGE FRAME BS 520, S24-25L DENTED. DENT TRIMMED OUT AND REPAIRED PER ER/A 519300-14.

Part: SKIN — DENTED (BS 1384-1460) · airframe 44,031 hrs · 12,250 cycles

UPPR FUSELAGE SKIN HAS MULTIPLE DENTS BS 1384-1460 STRINGERS 8-13R. REPAIRED IAW ER/A 519301-14

Part: SKIN — DENTED (BS 620-640) · airframe 44,031 hrs · 12,250 cycles

FUSELAGE SKIN BS 620 - 640 S15-18L, DENTED. DENTS REMOVED AND REPAIR IAW ERA 519282-14.

Part: SKIN — DENTED (BS 605) · airframe 44,031 hrs · 12,250 cycles

FUSELAGE SKIN BS 605 S27-28R DENTED AND CREASED. DAMAGE WAS REMOVED AND REPAIRED IAW ER/A 519285-14.

Part: SKIN — DENTED (BS 574) · airframe 44,031 hrs · 12,250 cycles

FUSELAGE SKIN BS 574, S27-28R, DENTED & CREASED. DAMAGE REMOVED AND REPAIRED IAW ER/A 519284-14.

Part: SKIN — DENTED (BS 1480-1500) · airframe 44,031 hrs · 12,250 cycles

UPPER FUSELAGE SKIN HAS MULTIPLE DENTS IN CROWN AREA BS 1480-1500 S4L-6L. DENTS 2,3 & 4 FOUND TO BE WITHIN LIMITS, DENT FOUR FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REPAIRED IAW ERA 519296-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 44,031 hrs · 12,250 cycles

FLOORBEAM HAS CORROSION AROUND AND IN FASTENER HOLES BS 1640 LBL 10-RBL10. REMOVED CORROSION, FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-51, 51-40-02 AND 51-20-01.

Part: SEAT TRACK — CORRODED (BS 1638) · corrosion level 2 · airframe 44,031 hrs · 12,250 cycles

SEAT TRACK RBL 24 CORRODED AT BS 1638. FOUND OUT OF LIMITS IAW SRM 51-40-02. REMOVED AND REPLACED SEAT TRACK BETWEEN BS 1540 - 1640 IAW SRM 51-40-02 PG 7 & DWG 146N5120-4015.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 44,031 hrs · 12,250 cycles

AFT CARGO, FLOOR SUPPORT CORRODED BS 1500-1520. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53 AND ACCOMPLISHED REPAIR IAW ERA 332525-14MA REV D.

Part: FRAME — GOUGED (BS 1280) · airframe 44,031 hrs · 12,250 cycles

MAIN CABIN FRAME HAS TWO DEEP GOUGES AT BS 1280 BETWEEN S10-11R. REMOVED DAMAGE SECTION, REPLACED & INSTALLED NEW SECTION. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 44,031 hrs · 12,250 cycles

AFT CARGO, FLOOR SUPPORT CORRODED ON LWR SURFACE AROUND NUTPLATE HOLE BS 1535 LBL 2. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53. ACCOMPLISHED REPAIR IAW ERA 332525.

Part: FRAME — GOUGED (BS 1280) · airframe 44,031 hrs · 12,250 cycles

MAIN CABIN FRAME HAS TWO DEEP GOUGES AT BS 1280 BETWEEN S10-11R. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07.

Part: SKIN — DENTED (BS 643) · airframe 44,031 hrs · 12,250 cycles

DENT ON FUSELAGE SKIN AT BS 643, BELOW S26L. REPAIRED IAW ER/A 519289-14 REV ORIG.

Part: BLOWER — INOPERATIVE (SMOKE DETECTION) · airframe 44,031 hrs · 12,250 cycles

AFT CARGO SMOKE DETECTION SYS NR 3 AND 4 BLOWERS ARE INOPERATIVE. R & R NR 3 AFT CARGO SMOKE DETECTOR BLOWER IAW AMM'S 26-16-02-024-001 AND 26-16-02-424-011. R & R NR 4 AFT CARGO SMOKE DETECTOR BLOWER, IAW AMM'S 26-16-02-024-001 AND 26-16-02-424-011.

Part: PUSH-PULL ROD — CORRODED (L4 DOOR) · airframe 44,031 hrs · 12,250 cycles

L4 DOOR FWD AND AFT PUSH/PULL RODS CORRODED. R & R FWD AND AFT PUSH/PULL RODS IAW CMM 52-11-25.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 44,031 hrs · 12,250 cycles

AFT CARGO, FLOOR SUPPORT CORRODED BS 1500-1520, RBL 7. REMOVED CORROSION IAW SRM 53-00-53 ALLOWABLE DAMAGED NOTE C, DETAIL V, FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT IAW ERA 332525-14MA STEP 1, NDT INSPECTION, NO FURTHER DAMAGE NOTED. FABRICATED REPAIR ANGLE ,TREATED AND PRIMED IAW ERA 332525-14MA, STEPS 4 AND 5. INSTALLED REPAIR ANGLE IAW ERA 332525-14MA, STEP 6.

Part: TRANSITION PANEL — CORRODED (FWD CARGO) · airframe 44,031 hrs · 12,250 cycles

FWD CARGO, RT TRANSITION PANEL HAS CORROSION ON UPPER SURFACE BS 765-845. REMOVED CORROSION AND FOUND BLENDED AREA TO BE WITHIN LIMITS IAW SRM 53-00-53.

Part: SEAT TRACK — CORRODED (BS 377) · corrosion level 2 · airframe 44,031 hrs · 12,250 cycles

CORROSION BS 377, LBL 45 SEAT TRACK, UPPER SURFACE. REMOVED & REPLACED SEAT TRACK BETWEEN BS 377 - 440, LBL 45 IAW SRM 51-40-02. REPLACED SEAT TRACK IAW DWG 141N5130-67 & SRM 51-40-02.

Part: TRANSITION PANEL — CORRODED (FWD CARGO) · airframe 44,031 hrs · 12,250 cycles

FWD CARGO, LEFT TRANSITION PANEL CORRODED ON UPPER SURFACE MULTIPLE AREAS, BS 508-645. BLENDED CORROSION IAW SRM 53-00-53, DETAIL V. FOUND TO BE WITHIN LIMITS IAW ERA NR 491157-14MA. TREATED AND PRIMED IAW SRM 51-20-01, PG 3-7 AND 27 AND PROCESS STANDARD NR 5.

Part: SEAT TRACK — CORRODED (BS 365) · airframe 44,031 hrs · 12,250 cycles

SEAT TRACK CORRODED AT BS 365, RBL 45. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-40-02 & DWG 654N0243.

Part: FRAME — DENTED (BS 580) · airframe 44,031 hrs · 12,250 cycles

FWD CARGO, FRAME DENTED BS 580 S24L. TRIMMED OUT DENTED AREA AND ACCOMPLISHED A PERMENANT REPAIR IAW SRM 53-00-07.

Part: FRAME — DENTED (BS 600) · airframe 44,031 hrs · 12,250 cycles

FWD CARGO, FRAME DENTED BS 600 S24L. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-07.

Part: FLOOR SUPPORT — CORRODED (BS 1460-1480) · airframe 44,031 hrs · 12,250 cycles

AFT CARGO, FLOOR SUPPORT HAS CORROSION ON UPPER & LOWER SURFACES, BS 1460-1480, LBL 16. BLENDED CORROSION IAW SRM 53-00-53, FIG 101 DETAIL V.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 44,031 hrs · 12,250 cycles

AFT CARGO, FLOOR SUPPORT HAS CORROSION ON LOWER SURFACE BS 1530, LBL 11. REMOVED CORROSION IAW SRM 53-00-53, ALLOWABLE DAMAGE 1, FIG 101. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE 1, FIG 105, NOTE "C" DETAIL V AND ERA NR 491157-14MA.

Part: RIB — DENTED (LT WING) · airframe 44,031 hrs · 12,250 cycles

LEFT WING LOWER SURFACE RIB DENTED WS 481-50. REPAIRED LT WING RIB IAW ERA 519299-14

Part: SKIN — DENTED (BS 1384) · airframe 44,031 hrs · 12,250 cycles

DENT ON EXTERNAL FUSELAGE SKIN AT BS 1384 BETWEEN S24-25L. FOUND TO BE OUT OF LIMITS IAW SRM-53-00-01, DETAIL III, FIG 101, ALLOWABLE DAMAGE 1, REPAIRED IAW SRM-53-00-01, REPAIR-7, DETAIL I.

Part: FLOORBEAM — DAMAGED (BS 365) · corrosion level 2 · airframe 44,031 hrs · 12,250 cycles

GOUGE DAMAGE TO UPPER SURFACE OF TEE AT BS 365 BL 0 - RBL 64, AND CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, ALLOWABLE DAMAGE 1 PAGE 104, FIG 101. CUT, REMOVED, AND REPLACED IAW SRM 53-00-51 REPAIR 8, PAGE 201-212.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · corrosion level 2 · airframe 44,031 hrs · 12,250 cycles

AFT CARGO FLOOR SUPPORT CORRODED BS 1500-1520 LBL 2. FOUND OUT OF LIMITS IAW SRM 53-00-53. REPAIRED FLOOR SUPPORT IAW ERA 332525-14MA REV D.

Part: SKIN — DENTED (BS 1600-1620) · airframe 44,071 hrs · 12,260 cycles

UPPER FUSELAGE SKIN HAS MULTIPLE DENTS IN CROWN AREA, BS 1600-1620, S1-4R. INSPECTED AND MEASURED DENTS. ALL DENTS FOUND WITHIN LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. I. REPAIRED IAW ER/A 520591-14, REV A.

Part: SKIN — DENTED (BS 1661-1681) · airframe 44,031 hrs · 12,250 cycles

FUSELAGE SKIN DENTED IN CROWN AREA BS 1681-1661 S2-S4R REPAIRED IAW ERA 519298-14.

Part: SKIN — DENTED (BS 1384) · airframe 44,031 hrs · 12,250 cycles

UPPER FUSELAGE SKIN DENTED BS 1384 JUST ABOVE S14R. REPAIRED IAW ERA 519295-14 REV ORIGINAL.

Part: SKIN — DENTED (BS 1160) · airframe 44,031 hrs · 12,250 cycles

UPPER FUSELAGE SKIN HAS PROTRUDING DENTS IN CROWN BS 1160 S4R. REPAIRED IAW ERA 519287-14 REV ORIG.

Part: SKIN — DENTED (BS 401) · airframe 44,031 hrs · 12,250 cycles

LEFT EXTERIOR SKIN DENTED AT BS 401 STRINGER 16L, -DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. TRIMMED OUT DAMAGE AND INSTALLED A PERMENANT REPAIR IAW SRM 53-00-01, REPAIR 3. MAJOR REPAIR

Part: SKIN — DENTED (BS 575) · airframe 44,031 hrs · 12,250 cycles

SKIN DENTED AT BS 575 S28-29R BELOW FWD CARGO CUTOUT. REPAIRED IAW ERA 519284-14 REV ORIGINAL.

Part: SKIN — PUNCTURED (BS 1580 S20L) · airframe 39,329 hrs · 11,331 cycles

DAMAGE ON FUSELAGE SKIN. THE PUNCTURE IS LOCATED BELOW THE S20L LAP JOINT AT APPROX BS 1581, 37 INCHES FWD OF SKIN PANEL EDGE AND 26 INCHES BELOW WL-0. REPAIR IAW ERA 496950-14.

Part: STRUCTURE — DAMAGED (TE F;A[) · airframe 51,270 hrs · 6,487 cycles

T/E FLAP INTER STRUCTURE DAMAGED PER ER/A 491616-14 REV ORIG. REPAIR THE DAMAGE, PER NR-57-011, HT-AC-013 MADE AND HEAT TREATMENT THE REPAIR PART. PER NR-57-017 CHECK THE FITTING. THE REPAIR IS "B" TYP REPAIR. PER ER/A 491616 -14 ACCOMP SECT III DVI INSPECTION NO LATER THAN 24 MONTHS AFTER COMPLETION OF THE SECT II REPAIR AND REPEATING AT INTERVALS NOT EXCEED 24 MONTHS.

Part: MECHANISM — LACK OF LUBE (NLG STEERING) · airframe 26,154 hrs · 8,787 cycles

AFTER DEPARTING GATE A/C UNABLE TO TURN RIGHT, ALL HYD IND NORMAL, A/C CAN TURN LEFT. INSPECTED STEERING CABLES AND PULLEY, FOUND ALL NORMAL. REMOVED STEERING ACTUATOR COVER AND LUBRICATED ACTUATOR COMMAND MECHANISM. OPS CHECK GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: MONITOR — FAULTY (VIBRATION SYS) · airframe 25,673 hrs · 8,706 cycles

A/C RETURNED TO BLOCK FOR EQUIPMENT COOLING FAN 1 MSG. NO ETOPS OPERATION ALLOWED UNDER MEL 21-58-03A. SECOND WRITE UP FOR THIS. EA 06-475397-03 WAS ACCOMPLISHED IN SLC ON 8/8 TO INSTALL VIBE MONITOR ON FAN. FAN FAILED ON FIRST FLT FROM SLC FLT 2039/09. ATL REPLACED THE FAN. JFK MTC THEN REPLACED MONITOR AND FAN AFTER RTB. A/C THEN DEPARTED ON FLT 206 JFK-ZRH. TWO HOURS INTO FLT CREW ADVISED DISPATCH THAT EQUIP OVERHEAT LIGHT ILLUMINATED AND ALTN EQUIP COOLING SELECTED AND OVERHEAT LIGHT EXTINGUISHED. COMPLIED WITH EAV TO REMOVE FAN VIB MONITOR VA78743.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,310 hrs · 8,452 cycles

AFTER TAKEOFF AN ODOR OF BURNING RUBBER WAS APPARENT IN AFT CABIN. THIS ODOR WAS SLOW IN DISSIPATING. ELECTED TO PULL MID GALLEY CB AND MID GALLEY COFFEEMAKER CBS. ALSO, TURNED OFF R RECIRC FAN. THIS SEEMED TO DISSIPATE ODOR. INSPECTED WHEEL WELLS APU AREA AND ALL GALLEY OVENS AND COFFEEMAKERS. RESET C/BS. NO FINDINGS OR ODORS NOTICED. MALF-1T0 POS-CN CTL-627994001, SKILL-02 .

Part: PRESSURE SWITCH — INOPERATIVE (HYD PUMP) · airframe 24,160 hrs · 8,415 cycles

BOTH CTR HYD PRESSURE IND LIGHTS IN OVHD PANEL ILLUMINATED WITH PRESSURE APPLIED. CTR HYD PRESS READING ON EICAS NORMAL. WHEN CREW TOOK THE ACTIVE RUNWAY FOR T/O CTR PRESSURE WENT TO ZERO. REPLACED CENTER HYD PUMP C-1 PRESSURE SWITCH S10003 PER M/M. OPS CHK GOOD

Part: UNKNOWN — ODOR (COCKPIT/CABIN)

AN ACRID ODOR IN THE COCKPIT AND FORWARD CABIN.

Part: BULB — LOOSE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT RIGHT AFT DOOR INOPERATIVE. SECURED LIGHT BULB FOR EMERGENCY LIGHT AT RIGHT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: EEC — INOPERATIVE (ZONE 100)

DEN INFLIGHT T1454/08DEC SEA TO STL - RIGHT ENGINE PRIMARY AND SECONDARY ENGINE CONTROL ILLUMINATED DURING FLIGHT. LANDED DEN WITHOUT INCIDENT. REPLACED RIGHT ENGINE ELECTRONIC ENGINE CONTROL AND PERMANENT MAGNET ALTERNATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: TAPE — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHT SECTION IN FRONT OF THE LAVATORY INOPERATIVE. FOUND BREAK IN THE POWER FEEDER CABLE TAPE JUST FORWARD OF THE LAVATORY. REPLACED FEED CABLE AT ROW 15 TO LAVATORY FOR EMERGENCY ESCAPE PATH LIGHT SECTION IN FRONT OF THE LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

DFW - EMERGENCY ESCAPE PATH LIGHT AT FLOOR AT ROWS 12 TO 13 INOPERATIVE. PLUGGED THE EMERGENCY ESCAPE PATH LIGHT SEGMENT BACK INTO POWER FEEDER CABLE AT ROWS 12 TO 13. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY ESCAPE PATH LIGHT SEGMENTS AT ROWS 1 AND 18 INOPERATIVE. REPLACED THE EMERGENCY ESCAPE PATH LIGHT SEGMENT AT ROWS 1 AND 18. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

DFW FLOOR LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED FEEDER WIRE AND LENSE SYSTEM FOR FLOOR LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OP.

Part: SPRING — DEFORMED (GIRT BAR) · airframe 11,014 hrs · 3,816 cycles

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

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 10,152 hrs · 3,488 cycles

THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 18 LT AND 23 RT SIDE, AND THE EGRESS LIGHTS WERE INOPERATIVE AT ROW 18 AND THE REAR LAV. REPLACED LAMPS P/N 8074-1 FOR THE OVERHEAD LIGHTS, AND REPLACED THE BATTERY PACK P/N 2013-1A FOR THE EGRESS LIGHTS. CHECK-C 1-7-03 MCI.

Part: PANEL — DENTED (VERTICAL STAB) · airframe 5,279 hrs · 1,717 cycles

ON THE RT SIDE OF THE VERTICAL STABILIZER, THE FWD ALUMINUM HONEYCOMB PANEL AT STA 92.250 HAD 24 GROUPS OF DENTS TOO CLOSE TOGETHER AND OUT OF LIMITS PER SRM 55-30-01. ALL DENTS DEPTH WITHIN LIMITS. APPROX 125 DENTS TOTAL. REPAIRED PER ARA 17707. NO CHECK-C.

Part: LIGHT — INOPERATIVE (CABIN)

THE EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE ON THE RT SIDE OF THE CABIN, DOORS 2, 3, AND 4. REPLACED THE LAMP AT EACH OF THE LOCATIONS.