N546US

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,186 hrs · 27,032 cycles

SHIP 5646 L CTR ENT DOOR CAS AND DOORS OVERHEAD LIGHT CYCLED ON/OFF AFTER LANDING DURING TAXI-IN. CORRECTIVE ACTION: ADJUSTED 2L DOOR WARNING SENSOR PER B757 AMM 52-71. OPS CK NML. (9635361)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,089 hrs · 26,978 cycles

SHIP 5646 ENTRY DOOR LIGHT AFTER PUSHBACK, WENT OFF CAME BACK ON. CORRECTIVE ACTION: ADJUSTED 2L DOOR SENSOR BRACKET IAW B757 AMM 52-71. LIGHT AND EICAS MSG OPERATES NML NOW. (9536686)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,991 hrs · 26,932 cycles

SHIP 5646 LEFT CENTER ENTRY DOOR LIGHT ILLUMINATED AND STAYED ON. CORRECTIVE ACTION: PERFORMED DOOR WARNING SYSTEM OPS CHECKS PER B757 AMM 52-71. OPS CHECKS GOOD. PRESSUREIZED A/C PER B757 AMM. NO FAULTS NOTED. (9536648)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,936 hrs · 26,902 cycles

SHIP 5646 LEFT CENTER ENTRY DOOR MESSAGE FLICKERED ON 3 TIMES AS A/C ROLLED OUT. EXITED RUNWAY AND ONCE MORE APPROACHING THE GATE. CORRECTIVE ACTION: INSPECTED L2 DOOR NO DAMAGE TO PROX SENSORS NOTED. VERIFIED DOOR WARNING SYSTEM OPS CHECKS NORMAL PER B757 AMM 52-71. (9536606)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,967 hrs · 26,410 cycles

SHIP 5646 PILOT AND CO PILOT REPORT DIRTY SOCK SMELL IN FLIGHT AND DECENT. CORRECTIVE ACTION: T/S R/R BOTH REC FILTERS PER B757 AMM 21-25. REMOVED AND REPLACED COWL DOOR OPENING ACT PER B757 AMM 78-31. PEFORMED BORO AND FOUND OIL WETNESS #1 ENGINE, REMOVED AND REPLACED ENGINE. (2803833 AND 2790621)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,948 hrs · 26,400 cycles

SHIP 5646 -ATB- DUE TO WEATHER ENROUTE AND LEFT ENGINE ANTI ICE VALVE DISAGREE. CORRECTIVE ACTION: T/S R/R NBR 1 ENG HIGH STAGE PILOT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,793 hrs · 26,329 cycles

SHIP 5646 - SMKE - WHILE BOARDING AT GATE SMOKE STARTED FILLING UP THE FLIGHT DECK AND CABIN WHILE APU RUNNING. GROUND CREW NOTE APU SMOKING OUT THE EXHAUST. CORRECTIVE ACTION: CONFIRMED APU FAILURE WITH OIL TANK EMPTY AND METAL ON THE CHIP DETECTORS, APU REPLACED. PERFORMED DUCT DECONTAMINATION AND REPLACED RECIRC FILTERS. NO ADDITIONAL SMOKE OR ODORS PRESENT.

Part: SKIN — UNKNOWN (UNKNOWN) · airframe 83,759 hrs · 26,310 cycles

SHIP 5646 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589044-14AD REV C. CORRECTIVE ACTION: REF ERA 589044-14AD. (2757683)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,514 hrs · 26,213 cycles

SHIP 5646 HISTORY BUILDING OF 2L SLIDE LIGHT INOP T /S AND REPAIR. CORRECTIVE ACTION: T/S PER B757 WDM 25-66-11 & FIM 25-66-00-815-802. FAULT INTERMITTENT. R/R BOTH FWD & AFT GIRT BAR PROX. SWITCHES PER B757 AMM 25-66. OPS CK GOOD NUMEROUS TIMES. (2705805)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,472 hrs · 26,188 cycles

SHIP 5646 2L ENTRY DOOR SLIDE LIGHT ILLUMINATED W/ DOOR OPEN & SLIDE UN-ARMED. CORRECTIVE ACTION: CLOSED DOOR AND ARMED SLIDE, DISARMED SLIDE, LIGHT EXTINGUISHED. DOOR SLIDE OK FOR SVC. PER B757 AMM 25-66. (4628450)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,483 hrs · 26,191 cycles

SHIP 5646 ER/A 483952-14 / SECTION V ONE TIME INSPECTION. CORRECTIVE ACTION: REF ERA 483952-14. (2697767)

Part: NONE — NONE · airframe 83,218 hrs · 26,021 cycles

SHIP 5646 2L SLIDE LIGHT STILL ILLUMINATED WHEN DOOR IS DISARMED. CORRECTIVE ACTION: CLOSED DOOR AND CYCLED ARM AND DISARM LEVER. LIGHT WHEN OUT. OPS CHK MNL. CLEANED PROX SW. ALL CKS GOOD. (4158012)

Part: NONE — NONE · airframe 83,205 hrs · 26,011 cycles

SHIP 5646 L CTR ENTRY DOOR EICAS CAUTION AFTER LANDING ON ROLLOUT. CORRECTIVE ACTION: PERFORMED SYSTEM TEST FOR L CENTER PAX DOOR IN REF TO B757 AMM 52-71. PROX SENSOR ON DOOR VERIFIED NEAR TARGET DURING PSEU BITE. DOOR INDICATION ON EICAS VERIFIED NORMAL. (9810696)

Part: NONE — NONE · airframe 83,204 hrs · 26,010 cycles

SHIP 5646 L2 DOOR ARM LIGHT INOP. CORRECTIVE ACTION: L2 (CTR) DOOR ARM LIGHT INDICATION OPS NORMAL. (9810693)

Part: NONE — NONE · airframe 83,205 hrs · 26,011 cycles

SHIP 5646 1R DOOR EXIT PLACARD COVER FELL. CORRECTIVE ACTION: INSTALLED EXIT SIGN COVER. (9810690)

Part: NONE — NONE · airframe 83,205 hrs · 26,011 cycles

SHIP 5646 L2 ENTRY DOOR INDICATION. CORRECTIVE ACTION: L2 ENTRY DOOR INDICATION CHECKS NORMAL. (9810694)

Part: UNKNOWN — UNKNOWN · airframe 83,091 hrs · 25,933 cycles

SHIP 5646 L CTR ENT DOOR ON AFTER LANDING. CORRECTIVE ACTION: UPON ARRIVAL TO A/C NO MESSAGES NOTED. PERFORMED DOOR WARNING SYSTEM TEST PER B757 AMM 52-71. OPS CHK OK. (9810636)

Part: WARNING LIGHT — FALSE ACTIVATION (L2 DOOR SLIDE) · airframe 82,863 hrs · 25,805 cycles

SHIP 5646 L2 DOOR SLIDE LIGHT ILLUMINATED. CORRECTIVE ACTION: DOOR OPN AND INDICATION NORMAL. (9853154)

Part: PROXIMITY SWITCH — OUT OF ADJUST (L2 DOOR) · airframe 82,879 hrs · 25,811 cycles

L2 DOOR SLIDE LIGHT INOPERATIVE. INSPECTED PROXIMITY SWITCHES S10218 AND S10219 IAW AMM 25-66. INSPECTED WIRING. PERFORMED ADJUSTMENT OF PROXIMITY SWITCH IAW AMM 25-66-11-822-011. CHECKED GOOD.

Part: INDICATOR — INOPERATIVE (R1 DOOR SLIDE) · airframe 82,839 hrs · 25,793 cycles

R1 DOOR SLIDE INDICATOR LIGHT INOP OR DAMAGED. R & R THE R1 SLIDE INDICATOR LIGHT IAW AMM 25-60.

Part: NONE — NONE (NONE) · airframe 82,707 hrs · 25,753 cycles

SHIP 5646 COMPLY WITH ERA 604360-14AD REV. ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH ERA 604360-14AD REV. ORIGINAL. (2537526)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,876 hrs · 26,863 cycles

SHIP 5646 REPETITIVE INSPECTIONS AT FRAME 1260. CORRECTIVE ACTION REF ERA 604360-14. (2532837)

Part: NONE — NONE · airframe 82,414 hrs · 25,598 cycles

SHIP 5646 WHILE WORKING WORKCARD 3352-01042-01E, FOUND 1L,2L,4L,1R,2R, AND 4R THE WRONG EXIT ROW IDENTIFIER. CORRECTIVE ACTION: R/R EXIT ROW IDENTIFIERS PER AA WORK CARD. (2464926)

Part: SEAT TRACK — CRACKED (BS 1190) · airframe 82,414 hrs · 25,598 cycles

SHIP 5646 CRACK ON RH OUTBD SEAT TRACK STA. 1190 AT PASSENGER FLOOR STRUCTURE. (IN REFRENCE NRC #00218). CORRECTIVE ACTION: SUMMARY OF NRC 00273. SEAT TRACK STA. 1190 AT PASSENGER FLOOR STRUCTURE WAS REPAIRED PER B757-200 SRM. (2457394)

Part: PRESSURE DECK — CORRODED (BS 1080-1180) · corrosion level 2 · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 SEVERAL SPOTS OF CORROSION (EXFOLIATION ) ALONG UPPER PRESSURE DECK AT LH MLG W/W FROM STA. 1080 TO STA. 1180 BTW BL0 TO LBL 70. CORRECTIVE ACTION: SUMMARY OF NRC 0142 : AREA WAS REPAIRED PER ER/A 602699-14 REV. ORIG. (2456662)

Part: DRAG FITTING — OUT OF TOLERANCE (LT ENGINE) · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 WR. A.A. MEASUREMENTS OUT OF TOLERANCE DIAMETER IN BORE HOLES # 1,3,4, 8 - 18 AT LH ENG DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC00209 BORE HOLES # 1,3,4, 8 - 18 AT LH ENG DRAG FITTING WERE REPAIRED PER ER/A 589044-14AD REV. B ; SECTION VI: PERMANENT REPAIR. (2455140)

Part: PRESSURE DECK — CORRODED (BS 1080-1150) · corrosion level 2 · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 SEVERAL CORROSION SPOTS (EXFOLIATION) ON UPPER PRESSURE DECK AT RH MLG WHEEL WELL, BTW STA 1080 TO 1150 AND BL 0 TO RBL 63. CORRECTIVE ACTION: SUMMARY OF NRC 00119. SEVERAL CORROSION SPOTS (EXFOLIATION) ON UPPER PRESSURE DECK AT RH MLG WHEEL WELL, BTW STA 1080 TO 1150 AND BL 0 TO RBL 63 WAS REPAIRED PER ER/A 602588 -14 REV ORIGINAL SECTION I. (2452461)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 DTE, 602699-14 FUSELAGE / ATTACH FITTINGS / LH LANDING GEAR / PRESSURE DECK ASSY WEB / STA 1080 - 1180, LBL 8.20 - LBL 70 / CORROSION. CORRECTIVE ACTION: REF ERA 602699-14. (2453104)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 DTE, 602588-14 FUSELAGE / MAIN FRAME / RH LANDING GEAR / PRESSURE DECK WEB, STA 1080 TO 1153.78 & BL 0 TO RBL 70 / CORROSION. CORRECTIVE ACTION: REF ERA 602588-14. (2447743)

Part: NONE — NONE · corrosion level 2 · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 CORROSION (EXFOLIATION) ON KEEL BEAM AT RH MLG WHEEL WELL, ADJACENT TO LDG GEAR HYD LINE, STA. 1112 APROX., BL0. CORRECTIVE ACTION: SUMMARY OF NRC 117: AREA WAS REPAIRED PER ER/A 602566-14 PRI REV . 0. (2446342)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

AIRCRAFT 5646, DURING LCK AND QRO, WHILE PERFORMING A BASE ZONAL INSPECTION PER WC 2020-2326, MULTIPLES CRACKS WERE FOUND AFFECTING THE COCKPIT FLOOR WEB, APPROX. BETWEEN STA 278-284 AND RBL 4-13. NO APPLICABLE REPAIR METHOD WAS FOUND WITHIN B757-200 SRM. CORRECTIVE ACTION: ER/A 14-602641 AUTHORIZES TO TRIM OUT THE CRACKED AREA AND THEN, INSTALL A REPAIR FILLER AND A REPAIR DOUBLER. (LP 2442314)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 SUMMARY OF NRC 00184:REPAIR WAS PERFORMED UNDER PRI 589045-14 REV 1 AND ERA 589045-14AD REV B , SECTION VI. CORRECTIVE ACTION: SUMMARY OF NRC 00184:REPAIR WAS PERFORMED UNDER PRI 589045-14 REV 1 AND ERA 589045-14AD REV B , SECTION VI. (2438038)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 CORROSION ON UPPER SKIN WING BTW WS 231.50 AND WS 285.65 AT LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00041. AREA WAS REPAIRED PER PRI 602545-14 REV 0 AND ER/A 602545-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (2430321)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 L CTR ENT DOOR MESSAGE ON TAXI IN. CORRECTIVE ACTION: SENSOR FOR THE LEFT NO. 2 PASSENGER DOOR WAS ADJUSTED AND SYSTEM TEST ON DOOR WARNING SYSTEM WAS PERFORMED PER B757-200 AMM 52-71. (9163604)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 SNUBER COMPENSATOR INDICATOR EXTENSION IS NOT CORRECT AT 4R DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00104: 4R ROTARY SNUBBER WAS REPLACED PER B757- 200 AMM 52-11-10. (2427570)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 CORROSION ON EXTERNAL DOUBLER FASTENERS FROM STA 1525 TO 1535 AND BTW S-1 TO S-2L AT OUTER FUSELAGE. CORRECTIVE ACTION: SUMMARY, OF NRC 00230 CORROSION ON EXTERNAL DOUBLER FASTENERS FROM STA 1525 TO 1535 AND BTW S-1 TO S-2L AT OUTER FUSELAGE. FASTENERS WERE REPLACED PER ER/A 602445-14 REV. ORIGINAL. (2426585)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 FWD AND AFT LEAF SPRING DIT NOT HOLD THE GIRT BAR SLIDER AT4L DOOR. (IN REF. AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00101: DAMAGED 4L DOOR GIRT BAR WAS REPLACED BY SERVICEABLE PER B757-200 AMM 25-66-10 AND LEAF SPRINGS (FWD AND AFT) OPERATE CORRECTLY. (2421934)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 CRACKS ON FLOOR PANEL STA. 278 FROM RBL 6 TO 7 APPROX. AT COCKPIT. CORRECTIVE ACTION: AREA WAS REPAIRED PER ER/A NO.511562-14 REV.ORIGINAL SECTION I PERMANENT REPAIR. (2422550)

Part: SKIN — DAMAGED (LT WING) · airframe 82,411 hrs · 25,597 cycles

SHIP 5646 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589044-14AD REV A. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED PER ER/A 589044-14AD, REV. B. (2367841)

Part: NONE — NONE · airframe 80,420 hrs · 24,994 cycles

SHIP 5646 EXIT LIGHT COVER LOOSE. CORRECTIVE ACTION: SECURED LIGHT COVER AS NEEDED, CHECKS GOOD. (8442938)

Part: NONE — NONE · airframe 80,420 hrs · 24,994 cycles

SHIP 5646 EXIT SIGN 2L FELL OFF INTO DOOR OPENING DURING DOOR CLOSURE. CORRECTIVE ACTION: RESECURED 2L EXIT SIGN ABOVE DOOR PER B757 AMM 33-51, OPS CHECK NORMAL. (8442934)

Part: NONE — NONE · airframe 80,320 hrs · 24,966 cycles

SHIP 5646 AFTER LANDING WE HAD EICAS MSG "L CTR ENTRY DOOR" WITH ALL INDICATION (FA) BEING ARMED. CORRECTIVE ACTION: TROUBLESHOT AND FOUND THE TARGET ON THE DOOR WAS LOOSE. READJUSTMENT OF SENSOR AND TARGET ON THE DOOR PER B757 AMM 52-71-00. OPS CHECK GOOD. (8492674)

Part: NONE — NONE · airframe 80,473 hrs · 25,009 cycles

SHIP 5646 L3 DOOR SLIDE ' COVER' DAMAGE. COSMETIC DAMAGE. CORRECTIVE ACTION: REPAIRED L3 SLIDE PER B757 AMM 25-00-00. (8492670)

Part: NONE — NONE · airframe 79,633 hrs · 24,755 cycles

SHIP 5646 DOOR 1R GUST LOCK INOP. FOUND COLLAR SHEARED. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR 1R LOCK COLLAR (HOLD OPEN) AND CATCH PER B757 AMM 52-11-08. OPS CHECK NORMAL. (8336062)

Part: NONE — NONE · airframe 79,522 hrs · 24,725 cycles

SHIP 5646 EXIT PATH LIGHT LENSES MOUNT TO FWD GALLEY WALL COSMETICALLY DAMAGED. CORRECTIVE ACTION: REPLACED FWD GALLEY EXIT PATH LENS COVERS PER B757 AMM 33-51 OPS CHK GOOD. (2005475)

Part: NONE — NONE · airframe 79,282 hrs · 24,657 cycles

SHIP 5646 ON SVC CHK FOUND MULTIPLE EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R BATTERY PACKS AT LOCATIONS M733 & M736 PER B757 AMM 33-51. OPS NML. (8102298)

Part: NONE — NONE · airframe 79,131 hrs · 24,616 cycles

SHIP 5646 WHILE PERFORMING WORKCARD# 2561-01257-01E THE L4 DOOR GIRT BAR FAILED SPRING CHECK. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 022-0001:2561-01257- 01E/001 00006 REPLACED GIRT BAR PER B757 AMM 25-66. (1961430)

Part: LIGHT — BROKEN (SEAT 33D) · airframe 78,833 hrs · 24,532 cycles

SHIP 5646 33D EMERGENCY LIGHT BROKEN. CORRECTIVE ACTION: C/W TERMINATING ACTION PER ERA 593637-14 REV ORIG. R/R SEAT 33D BUMPER ASSY PER B757 AMM 25-25. (8014830)

Part: COVER — MISSING (R3 DOOR HANDLE) · airframe 78,833 hrs · 24,532 cycles

SHIP 5646 3R DR HANDLE COVER/PLATE MISSING. CORRECTIVE ACTION: INSTALLED COVER PLATE FOR 3R HANDLE. CHECKS GOOD. (7800190)

Part: SKIN — GOUGED (BS 1787 S19-20L) · airframe 78,703 hrs · 24,491 cycles

SHIP 5646 WORKING PRI 593292-14 MTC DISCOVERED A GOUGE IN THE SECTION 48 FUSELAGE SKIN BETWEEN STRINGERS 19L AND 20L AND AFT OF FS 1787. CORRECTIVE ACTION: ALL WORK COMPLETED IAW ERA 593292-14 REV ORIG. (1902684)

Part: SKIN — GOUGED (FUSELAGE) · airframe 78,695 hrs · 24,488 cycles

SHIP 5646 DURING EXT CLEANING EVENT 206 FOUND DENT AND GOUGE AFT LT SIDE JUST BELOW HORIZ STAB. CORRECTIVE ACTION: REMOVED DAMAGE IAW B757-200 SRM. C/W HFEC-NO CRACK. C/W BHEC OF REMOVED FASTENER HOLES - NO CRACKS PER B757 SRM. REPAIR INSTALLED PER ERA 593292-14. (7800157)

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 78,661 hrs · 24,478 cycles

SHIP 5646 ON ARRIVAL FOUND DENT ON LEFT HORIZONTAL APPROX 87.75" FROM INBOARD. CORRECTIVE ACTION: NO DELAM NOTED. TEMP REPAIR ACCOMPLISHED PER ERA 592939-14, REV ORIG. REPLACED PANEL PER B757 AMM 55-15 IAW SEC III PER ERA 592939-14 REV A . (7801678)

Part: COVER — MISSING (L4 DOOR HANDLE) · airframe 78,495 hrs · 24,435 cycles

SHIP 5646 L4 DOOR HANDLE DUST COVER MISSING. CORRECTIVE ACTION: REPLACED MISSING L4 DOOR HANDLE DUST COVER. (7801670)

Part: DOOR — OUT OF ADJUST (LT AFT) · airframe 77,814 hrs · 24,248 cycles

SHIP 5646 WHILE TROUBLESHOOTING R AFT DOOR FOUND LT AFT DOOR OUT OF ADJUSTMENT. REMOVED DOOR LINER. CORRECTIVE ACTION: ADJUSTED UPPER AND LOWER GATES PER B757 AMM 52-11. OP TEST PULL TEST OK. REINSTALLED L4 DOOR LINER REF B757AMM 52-11.

Part: GATE — OUT OF ADJUST (AFT PAX DOOR) · airframe 77,814 hrs · 24,248 cycles

SHIP 5646 R AFT ENTRY DOOR EICAS MESSAGE CAME ON CLIMBOUT. THE LIGHT IS INTERMITTENT. FA STATE HANDLE POPPED UP SLIGHTLY AFTER TAKEOFF BUT SHE IS UNABLE TO PUSH IT DOWN, PRESSURIZATION NORMAL. CORRECTIVE ACTION: FOUND UPPER AND LOWERTHRESHOLD GATES TO BE OUT OF ADJUSTMENT. ADJUSTED UPPER AND LOWER GATES PERB757 AMM 52-11. OM TEST PULL TEST OK. REINSTALLED R4 DOOR LINER REF B757 AMM 52-11.

Part: GIRT BAR — OUT OF ADJUST (R3 DOOR) · airframe 77,807 hrs · 24,246 cycles

SHIP 5646 RT 3 DOOR GIRT BAR NEEDS ADJUSTMENT. CORRECTIVE ACTION: FOUND FWD PAW WILL NOT RE ENGAGE WHEN DISARMED. RE SECURED FWD PAW ALL OPS NML. B757 AMM 25-66. (7326754)

Part: TARGET — OUT OF RIG (RT DOOR) · airframe 77,807 hrs · 24,246 cycles

SHIP 5646 AFTER TXI OUT, R AFT ENTRY DOOR EICAS, ENTRY DOORS LIGHT ON OVR HD PANEL CAME ON AS WELL AS FALSE TAXI OUT PAGE IN ACARS. RETURNED TO GATE. CORRECTIVE ACTION: VERIFIED THAT PROX SENSOR IS GOOD AND FOUND PLUNGER TO TARGET OUT OF RIG ADJUSTED PLUNGER IAW AMM 52-71 B757. OPS CHECK NOW GOOD. (7413070)

Part: DOOR — FOD (RT AFT DOOR) · airframe 77,499 hrs · 24,153 cycles

SHIP 5646 R AFT ENT DOOR MESSAGE INTERMITTENT ON TAXI. CORRECTIVE ACTION: T/S PER B757 WDM 52-71-21. CLEANED AND REMOVED DEBRIS FOUND 4R DOOR. DOOR OPS NORMAL. (7395450)

Part: SEAT TRACK — DAMAGED (ROW 42) · airframe 77,407 hrs · 24,129 cycles

SHIP 5646 SEATS AT ROW 42 ABC HAS DAMAGED SEAT TRACK. CORRECTIVE ACTION: REF ERA 590838-14. REMOVED SEAT TRACK AND REPAIRED SEAT TRACK PER SRM AND INTALLED PER SRM AND ERA 590838-14 REV ORG.

Part: HANDLE — DAMAGED (RT OVERWING DOOR) · airframe 76,724 hrs · 23,927 cycles

FORWARD RIGHT OVER WING EXIT DOOR HANDLE DAMAGED. MAINTENANCE REPLACED DOOR HANDLE. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 76,715 hrs · 23,923 cycles

DURING L CHECK MAINTENANCE FOUND THE LT WING WITH CRACK INDICATION WERE ON HOLES NR 3, 4, 12, 13, 15 & 17. ADDITIONALLY HOLES NR 1, 9, 10 & 16 WERE FOUND WITH CORROSION IN FITTINGS AND SKIN LAYER AT BORE HOLE AND SURFACE. REPAIRED PER ERA 589044-14AD.

Part: SKIN — CRACKED (RT WING) · airframe 76,715 hrs · 23,923 cycles

DURING INSPECTION MAINTNENACE FOUND RT WING CRACK INDICATIONS ON HOLES NR 4, 7, 13, 16 AND 18 AND CORROSION ON HOLE NR 8. CORROSION WAS NOTED AFFECTING UPPER SURFACE AT FITTING HOLE NR 4 AND UPPER SKIN AT HOLES NR 4 AND NR 18. REPAIRED PER ERA 589045-14.

Part: SKIN — CORRODED (LT WING ROOT) · corrosion level 2 · airframe 76,715 hrs · 23,923 cycles

DURING L CHECK MAINTENANCE FOUND LEVEL 2 CORROSION ON LEFT WING UPPER SURFACE AT WING ROOT APPROXIMATELY STRINGER 9. FOUND 2 AREA OF EXFOLIATION. REPAIRED PER ERA 589139-14.

Part: SKIN — NONE · airframe 82,092 hrs · 25,498 cycles

SHIP 5646 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589045-14AD. CORRECTIVE ACTION: REF ERA 589045-14AD. (1696169)

Part: NONE — NONE · airframe 82,411 hrs · 25,597 cycles

AIRCRAFT 5646, DURING LCK AND QRO, WHILE PERFORMING A BASE ZONAL INSPECTION PER WC 2020-2326, MULTIPLES CRACKS WERE FOUND AFFECTING THE COCKPIT FLOOR WEB, APPROX. BETWEEN STA 278-284 AND RBL 4-13. NO APPLICABLE REPAIR METHOD WAS FOUND WITHIN B757-200 SRM. CORRECTIVE ACTION: ER/A 56-589045 AUTHORIZES TO TRIM OUT THE CRACKED AREA AND THEN, INSTALL A REPAIR FILLER AND A REPAIR DOUBLER. (LP 4696177)

Part: SKIN — NONE · airframe 82,092 hrs · 25,498 cycles

SHIP 5646 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589044-14AD. CORRECTIVE ACTION: REF ERA 589044-14AD. (1696546)

Part: SKIN — DAMAGED (BS 822) · airframe 85,959 hrs · 27,414 cycles

SHIP 5646 LIGHTNING STRIKE DAMAGE TO THE 143N3121-4 UPPER SKIN IN THE S-4L LAP AT BS 822. CORRECTIVE ACTION: REF ERA 483952-14. (1670263)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,711 hrs · 23,922 cycles

EXIT SIGNS AT UPPER L4, AFT GALLEY OVERHEAD AND LOWER R4 ARE INOPERATIVE. CORRECTIVE ACTION: MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY P10/F1. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 74,791 hrs · 23,327 cycles

(AIRCRAFT 5646, L/P 6089934) ON SVC CHECK FOUND SEAT 4 AND 5 DC AND 15/16 DEF EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK M732 IAW AMM 3351.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 74,786 hrs · 23,326 cycles

(AIRCRAFT 5646, L/P 6089925) L1 DOOR EMERGENCY LIGHT TEST SWITCH INOP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT TEST SWITCH REF WDM 33-51-12. LIGHTS CHECK GOOD.

Part: QUICK DISCONNECT — DISCONNECTED (CABIN) · airframe 73,273 hrs · 22,944 cycles

SHIP 5646 EMER LIGHTS AT 4C INOP. CORRECTIVE ACTION: FOUND QUICK DISCONNECT WIRE UNDER SEAT 4D DISCONNECTED. RECONNECTED SAME AND LIGHT OPS CHECK GOOD. (5810631)

Part: LIGHT — DAMAGED (CABIN) · airframe 72,809 hrs · 22,821 cycles

SHIP 5646 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:18D / SEAT MOUNTED EMERG LT PUSHED INTO HOUSING. CORRECTIVE ACTION: REINSTALLED EMERGENCY LIGHT, OP'S NORMAL. (1001546)

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 72,415 hrs · 22,725 cycles

SHIP 5646 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:02L. CORRECTIVE ACTION: RE ADJUSTED AND RE INSTALLED EXIT SIGN (2L). (0952171)

Part: HARNESS — TORN (EVAC SLIDE) · airframe 71,099 hrs · 22,379 cycles

R1 SLIDE HARNESS TORN. REMOVED AND REPLACED R1 DOOR SLIDE HARNESS IAW 2040-0057- / 1R.

Part: FRAME — DENTED (FUSELAGE) · airframe 71,099 hrs · 22,379 cycles

AFT CARGO COMPLT FS 1320 FRAME UPPER SURFACE HAS LIGHT CORROSION ABOVE STR 26R. REMOVED CORROSION AND EVALUATED AFT CARGO STA 1320 FRAME UPPER SURFACE STR 26R ORIG .071 LOSS .003 REMAINING .068 AND WITHIN ALLOWABLE LIMITS IAW SRM 53-00-07 UPON EVALUATION FOUND DENT ON FRAME UPPER FLANGE SURFACE AT SAME LOCATION CUT OUT DAMAGED SECTION OF FRAME STA 1320 ABOVE STRINGER 26R AND REPAIRED FRAME IAW SRM 53-00-07 REPAIR 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

(AIRCRAFT 5646, L/P 0764437) CORROSION IN THE MAIN CABIN FLOORBEAM EXISTING UPPER SURFACE BS 365 BETWEEN BL.0 AND RBL. 38. REMOVED PREVIOUS REPAIR FROM MAIN CABIN FLOORBEAM UPPER SURFACE STA 365 BETWEEN BL0 - RBL 38 DUE TO NO ALLOWABLE LIMITS ON PREVIOUS REPAIRS CUT OUT SECTION OF STA 365 FLOORBEAM FROM RBL 38 TO RBL 65 AND INSTALLED NEW REPAIR IAW SRM 53-00-51 REPAIR 10 FROM BL0 TO RBL65.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

CORROSION MAIN CABIN FLOOR STRUCTURE CHANNEL, UPPER SURFACE, BETWEEN BS 330 TO BS 345 RBL 3.5. REMOVED AND INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-40-02 AND DRW 141N5160 REV E.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

(AIRCRAFT 5646, L/P 0760991) CORROSION MAIN CABIN CREASE BEAM ANGLE FROM 1020-1040 LT SIDE. CUT OUT DAMAGED SECTION DIM 29.4 IAW SRM 53-00-13 REP 2, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02 AND 53-00-13 REP 2.

Part: SUPPORT CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

(AIRCRAFT 5646, L/P 0759203) CORROSION IN THE MAIN CABIN FLOOR STRUCTURE SUPPORT CHANNEL, UPPER SURFACE, BETWEEN BS.355.5 TO BS.365.5 LBL.62.0 CP53-221-01I DOT 129-003. FABRICATED SUPPORT CHANNEL FROM 70750 P.O # FC1800007 AND HEAT TREATED TO T6 IAW BDRW 141N5170 REV C AND 4TW0127 WO#11335 FROM HI TECH WELDING. INSTALLED CHANNEL SUPORT IAW B577 SRM 51-40-02.

Part: SKIN — DENTED (BS 617-638) · airframe 71,099 hrs · 22,379 cycles

(AIRCRAFT 5646, L/P 0757501) COMPLY PERMANENT REPAIR ON LH SIDE FUSELAGE SKIN DENTED AT FS 617-638 S-18L TO S-19L. ACCOMPLISHED A FUSELAGE SKIN REPAIR STA 590 TO 661 STR. 14LT TO STR. 19LT IAW DELTA ER/A# 569016-14AD REV. ORIGINAL. THIS REPAIR REQUIRES A DTE ON OR BEFORE 50,000 TOTAL AIRFRAME CYCLES. THIS IS BEING TRACKED ON LOG PAGE #0755803.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

CABIN CREASE BEAM ANGLE STA 440 LBL 50 CORRODED. REMOVED CORROSION FROM CREASE BEAM INNER CHORD/ANGLE STA 440 LBL 50 IAW SRM 51-10-02. PERFORMED UT INSP OF BLENDED AREA PER NDTM PT 4 51-00-10 PROC 1. ORIG MAT .071" MAT REM .052" LOSS .019" FOUND AREA OUT OF LIMITS IAW SRM 53-30-13. REMOVED DAMAGED CREASE BEAM INNER CHORD STA 440 LBL 50. FABRICATED NEW CHORD AND INSTALLED NEW CHORD ALL IAW SRM 51-40-02, AND 53-10-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

CORROSION IN THE MAIN CABIN FLOORBEAM EXISTING REPAIR, UPPER SURFACE, BS 377 BETWEEN LBL 14.5 AND LBL 35.0. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-02. REMOVED PREVIOUS REPAIR PARTS FROM FLOORBEAM, FABRICATED NEW REPAIR PARTS AND INSTALLED NEW REPAIR PARTS IAW SRM 53-00-51 FIG 201 REPAIR 10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

CORROSION IN THE MAIN CABIN FLOORBEAM, UPPER SURFACE, BS 345 RBL 61.5. REMOVED CORROSION AT MAIN CABIN FLOORBEAM UPPER SURFACE IAW SRM 51-10-02. CUT OUT DAMAGED AREA OF FLOORBEAM STA 345 DIM 16.9" AND REPAIRED FLOORBEAM ALL IAW SRM 53-00-51 REPAIR 8 FIG 201.

Part: TEAR STRAP — DEBONDED (FUSELAGE) · airframe 71,099 hrs · 22,379 cycles

POSSIBLE DISBOND NOTED BETWEEN SKIN AND TEARSTRAP STA 800 STR 8L, SKIN THICKNESS -.050". REPAIRED DISBOND ON TEARSTRAP STA 800 STRINGER 8L IAW SRM 53-00-01 REPAIR 12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

MAIN CABIN BETWEEN STA 1660 - 1681 LBL60 APPROX FLOOR SUPPORT CORRODED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT P/N 146N5246-5 IAW SRM 51-40-02 AND DWG 146N524 REV A AND REV D ORIG .071".

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 71,099 hrs · 22,379 cycles

SEAT TRACK FOUND DAMAGED AT STA 630 RT OUTBOARD SEAT TRACK CROWN. CUT OUT DAMAGED SEAT TRACK SECTION STA 590 TO 640 RBL 46. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 3 FIG 201.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 70,706 hrs · 22,270 cycles

ON SERVICE CHECK FOUND OVERHEAD AISLE EMERGENCY LIGHT AT STATION 770 INOP. LAMPED NO HELP REF AMM 33-51. REMOVED AND REPLACED BATTERY CHARGER M732 OPS NORMAL.

Part: LENS — ABNORMAL (CABIN) · airframe 70,604 hrs · 22,245 cycles

FWD GALLEY AFT WALL JUST FWD OF SEATS 1CD FLOOR EMERGENCY LIGHT LENSES MISSING. 1 RED AND 1 WHITE. REPLACED BOTH LIGHT ASSY PER CMM 25-31-88.

Part: GENERATOR — FAILED (LEFT) · airframe 69,470 hrs · 21,948 cycles

LEFT GENERATOR FAILURE WITH ASSOCIATED EICAS AMBER MESSAGE. FOLLOWED QRH PROCEDURES. RESET ONCE, NO LUCK, STARTED APU & CONTINUED ON TO DESTINATION. R & R THE C901 LEFT GEN CIRCUIT BREAKER IAW AMM 24-22. 927856. PERFORMED IDG ADJUSTMENT TEST IAW AMM 24-11-00. PERFORMED MULTIPLE TRANSFER & RECONFIGURATION, NO FAULTS.

Part: ELECTRICAL SYS — POWER LOSS · airframe 69,433 hrs · 21,940 cycles

AIR TURNBACK DUE TO A LOSS OF ALL ELECTRICAL POWER, THE AUTOPILOT DISCONNECTED AND BOTH EICAS SCREENS WERE BLANK, SELECTED EMERGENCY POWER. LEFT GENERATION SYSTEM FAILED WITH NO AUTOMATIC TRANSFER TO RIGHT AND STBY POWER DID NOT COME ON. THE APU WAS STARTED AND NORMAL POWER WAS RESTORED. RAN THE QRH FOR GENERATOR OFF. CREW DECLARED AN EMERGENCY AND LANDED. R & R THE K109 RELAY, C901 LT GEN CIRCUIT BREAKER IAW AMM 24-22. R & R THE LT IDG, GCU, AND BPCU IAW AMM 24-22. OPS CHECKED GOOD.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 68,977 hrs · 21,817 cycles

CREW REPORTED THE R1 DOOR WILL NOT ARM. REPOSITIONED DOOR LANYARD, OPS CHECKED OK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,825 hrs · 21,773 cycles

EMERGENCY LIGHTS AT SEATS 27 - 32 INOPERATIVE. R & R THE BATTERY AND CHARGER IAW AMM 33-51. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,213 hrs · 21,073 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. SECURED EMERGENCY EXIT SIGN. OK FOR SERVICE IAW AMM 33-24.

Part: ATTACH FITTING — BROKEN (EXIT SIGN) · airframe 65,999 hrs · 21,007 cycles

EXIT SIGN DOOR 2. FOUND ATTACH CLIP BROKEN. R & R EXIT SIGN COVER AT 2R.

Part: SKIN — DENTED · airframe 71,099 hrs · 22,379 cycles

(AIRCRAFT 5646, L/P 2870917) WHILE IN C CHECK IN ATL, MTC WAS ASKED TO DISPOSITION A DENT THAT HAD BEEN PREVIOUSLY DISPOSITIONED PER THE SRM AND TRACKED BY LOG PAGE 8841850. UPON FINDING THE DAMAGE, MTC FOUND A SECOND DENT OUTSIDE OF PERMANENT ALLOWABLE LIMITS. THE DENT LOCATIONS AND DIMENSIONS (PRIOR TO REWORK) ARE DESCRIBED IN FIGURE 1 OF THIS ER/A 553167-14. AFTER ACCOMPLISHED DTE (PER LOG PAGE 2787792), THE SKIN DENTS MUST BE INSPECTED AND REPAIRED PER SRM GUIDELINES ACCORDING TO ER/A 553167-14 REV A. ASSOCIATED ER/A CHANGED FROM 00-553167 TO 14-553167 FOR AC 5646 SECTION 3 OF DELTA ER/A# 553167-14 REV. B, REPAIR OF FUSELAGE SKIN STA. 590 TO 661 STR. 14LTTO STR. 19LT ACCOMPLISHED ON LOG PAGE# 0757501. PLEASE CLOSE LOG PAGE# 2870917.

Part: CONTROL UNIT — FAILED · airframe 64,318 hrs · 20,581 cycles

DURING CLIMB OUT, LT & RT UTILITY BUSS OFF CAUTION MESSAGES ON EICAS. NO LUCK RESETTING OR RECYCLING CIRCUIT BREAKERS. RETURNED TO DEPARTURE. PASSENGERS REPORTED A BURNING ODOR IN THE MID CABIN. FOUND BPCU WILL NOT POWER UP AND TO HAVE A FAINT ODOR. R & R THE BPCU, CHECKED OK.

Part: SLIDE — ABNORMAL · airframe 64,247 hrs · 20,563 cycles

DOOR SLIDE WILL NOT FIT INTO BUSTLE. REMOVED AND REPLACED THE SLIDE IAW AMDS CARD.

Part: PLATE — WORN (L1 DOOR) · corrosion level 2 · airframe 71,104 hrs · 22,384 cycles

SHIP 5646 L-1 DOOR LOWER CAM PLATES WORN (REF; N/R 211). CORRECTIVE ACTION: REF ERA 476391 MA, REV B. REMOVED AND REPLACED L-1 DOOR TORQUE TUBE LOWER CAMPLATE IAW ERA 476391-14MA SECTION III PERMANENT (2789854)

Part: PLATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

(AIRCRAFT 5646, L/P 2789996) R-2 DOOR LOWER CAM PLATE HAS CORROSION (FROM NR 219). COMPLIED WITH REMOVAL AND REPLACEMENT OF R-2 DOOR LOWER CAM PLATE, P/N: 140N2634-46, PO 546US-00037 IAW T/C: 5211-6005-2R AND AMM 52-11-09-004-001 AND 52-11-09-404-017.

Part: CAM — WORN (R1 DOOR) · airframe 71,104 hrs · 22,384 cycles

SHIP 5646 R-1 DOOR LOWER CAMS ARE WORN (REF; N/R 217) CORRECTIVE ACTION: REF ERA 476391-14 REV B AND REMOVED AND REPLACED L-1 DOOR TORQUE TUBE LOWER CAMPLATE IAW ERA 476391-14MA SECTION III PERMANENT REPAIR. (2790095)

Part: PLATE — CORRODED (R4 DOOR) · corrosion level 2 · airframe 71,099 hrs · 22,379 cycles

(AIRCRAFT 5646, L/P 2789984) R-4 DOOR LOWER CAM PLATE HAS CORROSION. COMPLIED WITH REMOVAL AND REPLACEMENT OF R-4 DOOR LOWER CAM PLATE IAW TASK CARD 5211-6005-4R AND AMM 52-11-09-004-001 AND 52-11-09-404-017.

Part: SUPPORT BRACKET — CORRODED (BS 1060) · airframe 61,708 hrs · 19,834 cycles

LEFT UPPER FUSELAGE BS 1060, SUPPORT BRACKET FOR FAIRING 195ALIS CORRODED. REMOVED OUT OF LIMITS CLIP INSTALLED NEW CLIP ON LT UPPER FUSELAGE, BS 1060 FOR FAIRING 195AL IAW SRM 51-40-01 & 51-40-02.

Part: HEADSET — FAILED (SEAT 27B) · airframe 60,584 hrs · 19,538 cycles

PAX SEAT 27B WHEN AUDIO HEADPHONES PLUGGED IN, PAX REPORTED HEADSET HEATING UP AND SAW SMOKE. TRIED A BRAND NEW PAIR OF EAR BUDS AND THEY BEGAN TO GET HOT. DEFER TO MEL 23-37-01A. PLACARD INSTALLED. PULLED AND SECURED C/B ON P11 AND P70 IAW MEL, M, PROCEDURES. PLACED "DO NOT USE" PLACARD ON IFE PANEL IAW MEL, M, PROCEDURES. ALL MEL M, PROCEDURES COMPLYED WITH. REVERSED, M, PROCEDURE & PERFORMED T/S. VISUALLY CHECKED WIRING & HARNESS FOR ANY DAMAGE. FURTHER T/S FOUND PCU AT FAULT. REPLACED PCU AT 27B REF AMM 23-34. OPS CHECKED OK. MONITORED FOR 15 MINUTES, NO HEATING NOTED. REMOVED MCO & PLACARD. ACFT OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (NR 6 SLAT) · airframe 58,992 hrs · 19,058 cycles

NR 6 SLAT DAMAGE FOUND ON 2 PLACES. 1.3.5" X 3.5" COLATED 37" FROM OTBD EDGE. 2.3.5" X 5.0" DAMAGE COLATED 58" FROM OTBD EDGE. IN ORDER TO REMOVE NR 6 SLAT. REMOVED 3 UNDER WING PANEL. REPLACED RT INBD L/E SLAT AND INSTALLED 3 UNDER WING PANELS AND OP CKS OK IAW AMM 27-81. LP5576820.

Part: TERMINAL — UNSECURE (EMERGENCY LIGHT) · airframe 58,719 hrs · 18,976 cycles

EMERGENCY LIGHT UNDER OVERHEAD BIN 26DEF INOPERATIVE. SWAPPED LIGHT ASSEMBLIES, CONFIRMED GOOD. TROUBLESHOT IAW WIRING DIAGRAM 33-51-13, AND FOUND NO CONTINUITY GROUND TO D7546. FOUND NUT AT GROUND TERMINAL LOOSE, AND SECURED.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 58,658 hrs · 18,958 cycles

EMERGENCY LIGHT ROW 25 RT UNDER O/H BIN WON'T ILLUMINATE. FOUND WIRE LOOSE AT PLUG CONNECTOR, RECAPPED, RESECURED IAW AMM 20-60.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,078 hrs · 18,782 cycles

AISLE EMERGENCY PACK LIGHT OUT AT 26D O/H BIN. REPLACED BATTERY PACK IAW AMM 33-51. CHECKED GOOD.

Part: DOOR FRAME — DEFORMED (APU BAY) · airframe 57,829 hrs · 18,706 cycles

APU BAY RT ACCESS DOOR FRAME DEFORMED. REPAIRED IAW ERA 529472-14, REV 0.

Part: SKIN — PUNCTURED (BS 1862) · airframe 57,737 hrs · 18,679 cycles

DAMAGE WAS FOUND NEAR BS 1862 S25L. DAMAGE CONSISTED OF A PUNCTURE TO FUSELAGE SKIN. REFERENCE ERA 520161-14, REV B FOR REPAIR.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 56,587 hrs · 18,337 cycles

SEAT 22 ABC EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE BROKEN FROM SPLICE. SPLICED BROKEN WIRE. OPS CHECKED GOOD. NO DEFECTS NOTED, IAW SWPM 20.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,938 hrs · 17,850 cycles

DURING EMERGENCY LIGHT BATTERY PACKS CHECK, CHECK FAILED AT ALL LOCATIONS. CHECKED EMERGENCY BATTERY PACKS AFTER COMPLETELY DISCHARGED AND RECHARGED TWO HOURS, THEN FOUND BATTERY PACK M732 FAILED. REPLACED BATTERY PACK M732 IAW AMM 33-51 AND CHECKED OK.

Part: SKIN — PUNCTURED (BS 1862) · airframe 54,668 hrs · 17,768 cycles

FOUND SKIN PUNCTURED BS 1862 S-25L. DAMAGE OUT OF LIMITS IAW SRM 53-80-01 AND 53-00-01. ACCOMPLISHED ER/A 520161-14 AND NO OTHER DAMAGE FOUND.

Part: ENGINE — LEAKING (OIL SYSTEM) · airframe 54,668 hrs · 17,768 cycles

CREW ACCOMPLISHED AN AIR TURN BACK TO NRT DUE TO SMOKE, HAZE AND ODOR IN CABIN. MAINTENANCE FOUND 2.5 BLEED PORT WET WITH OIL SUSPECT BEARING SEAL LEAKAGE. REPLACED NR 1 ENGINE.

Part: TERMINAL — LOOSE (EMERGENCY LGIHT) · airframe 52,897 hrs · 17,218 cycles

LEFT OVERWING EMERGENCY ESCAPE LIGHT INOPERATIVE. TROUBLESHOT IAW SSM33-51-01/103, FOUND GROUND WIRE TERMINAL LOOSE, SECURED THE TERMINAL STUD NUT, CHECKED & OK FOR SERVICE.

Part: LEAF SPRING — FAILED (GIRT BAR) · airframe 52,329 hrs · 17,034 cycles

R1 DOOR SLIDE GIRT BAR FWD LEAF SPRING FUNCTIONAL CHECK FOUND FAILED IAW WC 2561-01257-01B. SUMMARY: REFER TO WC 2040-0057-1R FOR R1 DOOR SLIDE REMOVAL AND INSTALLATION DETAILS. R1 SLIDE NEW GIRT BAR LEAF SPRING F UNCTIONAL CHECK CARRIED OUT IAW WC 2561-01257-01B AND RESULT FOUND SATISFACTORY. R1 SLIDE GIRT BAR R & R IAW AMM 25-66-10 AND R1 DOOR GIRT BAR MECHANISM ADJUSTED IAW AMM 52-11-25. RII INSPECTION COMPLETED.

Part: BUCKLE — LOOSE (SLIDE) · airframe 52,329 hrs · 17,034 cycles

L1 DOOR SLIDE HARNESS BUCKLE FOUND LOOSE. REFER TO WC 2040-0057-1L FOR L1 DOOR SLIDE REMOVAL AND INSTALLATION DETAILS. L1 DOOR SLIDE HARNESS ASSY R & R IAW AMM 25-66-01. RII INSPECTION COMPLETED.

Part: LEAF SPRING — FAILED (GIRT BAR) · airframe 52,329 hrs · 17,034 cycles

R2 DOOR SLIDE GIRT BAR FWD LEAF SPRING FUNCTIONAL CHECK FOUND FAILED IAW WC 2561-01257-01D. SUMMARY: REFER TO WC 2040-0057-2R FOR R2 DOOR SLIDE REMOVAL AND INSTALLATION DETAILS. R2 SLIDE NEW GIRT BAR LEAF SPRING FUNCTIONAL CHECK CARRIED OUT IAW WC 2561-01257-01D AND RESULT FOUND SATISFACTORY. R2 SLIDE GIRT BAR R & R IAW AMM 25-66-10 AND R2 GIRT BAR MECHANISM ADJUSTED IAW AMM 52-11-25. RII INSPECTION COMPLETED.

Part: ATTACH FITTING — CORRODED (BS 897) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

LOWER FUSELAGE, BS 897, BODY FAIRING ATTACHMENT FRAME AT BL 0, CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-02, MATERIAL REMOVED 0.072 " (L-18" W-1") ORIGINAL MATERIAL THICKNESS MEASURED 0.090" AND FOUND OUT CORROSION STILL EXISTS IAW BSOPM 20-20-02 REV 5. DAMAGED FRAME ATTACHMENT R & R IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 332) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 332, RBL 2-24, FLOORBEAM FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 AND FOUND EXCEED LIMITS IAW SRM 53-00-04, FIG 101. ORIGINAL THK=0.050", L=4", W=2", MATERIALS REMOVED=0.028". FLOORBEAM R & R IAW SRM 51-40-02.

Part: BOX BEAM — CORRODED (BS 345-365) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 345-365, RBL 63 BOX BEAM FOUND CORROSION. SUMMARY: CABIN BS345-365, RBL63 BOX BEAM CORROSION REMOVED IAW SRM 51-10-02 AND FOUND EXCEED LIMITS IAW SRM 53-00-04, FIG 101. ORIGINAL THK=0.050", L=5", W=2", MATERIALS REMOVED==0.020". BOX BEAM SUPPORT R & R IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 365-405) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 365-405, RBL 45 SEAT TRACK FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 AND FOUND EXCEED LIMITS IAW SRM 53-00-52, FIG 101. ORIGINAL THK=0.070", L=2", W=1.5", MATERIALS REMOVED=0.030". SEAT TRACK R & R IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 345, LBL 1 AREA FLOORBEAM FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02, FOUND EXCEED LIMIT IAW SRM 53-00-04, FIG 101. ORIGINAL THK=0.063",L=2", W=1", MATERIALS REMOVED=0.030". FLOORBEAM R & R IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 405) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 405, RBL 24-45, FLOORBEAM FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 AND FOUND EXCEED LIMIT IAW SRM 53-00-04, FIG 101. ORIGINAL THK=0.050", L=3", W=2", MATERIALS REMOVED=0.030". FLOORBEAM SUPPORT R & R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1660-1680) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

CABIN BS1660-1680, LBL 0 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 AND FOUND EXCEEDED LIMITS IAW SRM 53-00-04 FIG 101. ORIGINAL THK=0.050",L=2", W=1", MATERIALS REMOVED=0.035". FLOOR SUPPORT R & R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1675) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 1675, LBL 50 FLOOR SUPPORT FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND FOUND EXCEED LIMITS IAW SRM 53-00-51, FIG 101. ORIGINAL THK=0.071", L=3", W=2", MATERIALS REMOVED=0.060". FLOOR SUPPORT R & R IAW SRM 51-40-02.

Part: DECK PLATE — CORRODED (BS 1680) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 1680, LBL 10 FLOORBEAM ATTACHED DECK PLATE FOUND CORROSION. CORROSION ON DECK PLATE REMOVED IAW SRM 51-10-02 AND FOUND EXCEEDS LIMITS IAW SRM 53-60-51, FIG 201. ORIGINAL THK=0.070", L=2.5", W=1. 75", MATERIALS REMOVED=0.050". REPAIR CARRIED OUT IAW SRM 53-60-51 (REPAIR 2) FIG 201, ALTERNATIVE 2.

Part: FLOOR SUPPORT — CORRODED (BS 1650) · corrosion level 2 · airframe 52,322 hrs · 17,033 cycles

BS 1650 LBL 1 FLOOR SUPPORT FOUND CORROSION. CORROSION FLOOR SUPPORT REMOVED IAW SRM 51-10-02 AND FOUND EXCEEDED LIMITS IAW SRM 53-00-04, FIG 101. ORIGINAL THK=0.050", L=2", W=1", MATERIALS REMOVED=0.030". FLOOR SUPPORT R & R IAW SRM 51-40-02.

Part: SLIDE — NO TEST (RT OVERWING) · airframe 52,322 hrs · 17,033 cycles

RIGHT OVERWING SLIDE FOUND NOT DEPLOY DURING OPS CHECK IAW WC 2565-3003. RT OVERWING SLIDE SYS TROUBLESHOT IAW FIM TASK 25-65-00-815-804 AND SLIDE SYS COMPONENTS LUBRICATED IAW AMM 12-21-25. RT OVERWING SLIDE PNEUMATIC DEPLOYMENT CHECK CARRIED OUT IAW WC 2565-3003 AND AMM 25-65-00 AND RESULT FOUND SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,065 hrs · 16,954 cycles

ON PDC CHECK, FOUND ACFT, THE EMERGENCY LIGHT STILL ON AT L2 DOOR EXTERIOR. TROUBLESHOT AND FOUND POWER SUPPLY INOPERATIVE. REPLACED POWER SUPPLY IAW IAW AMM33-51, THEN FUNCTION CHECKED OK.

Part: WIRE — OPEN (EMERGENCY LIGHT) · airframe 51,478 hrs · 16,763 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 3 9 AND 40. FOUND OPEN WIRE AT UNDER THE SEAT 38. REPAIRED WIRE WITH SPLICE PER SWPM 20-30-12. PERFORMED EMERGENCY LIGHT CHECKED OK PER AMM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,530 hrs · 1,362 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THE EMERGENCY OVERWING EXIT SIGNS AT SEATS 21F & 23A INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. OPERATIONAL CHECK WAS GOOD.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 52,322 hrs · 17,033 cycles

HOLE IN AFT CARGO COMPARTMENT FLOOR INBD OF DOOR. INTERIM REPAIR WAS ACCOMPLISHED IAW DWG 5A53-37933 AND DEFER LOG PAGE TO MON FOR PERMANENT REPAIR IAW SRM 51-70-13, FIG 1 AT NEXT SCHEDULED FLOORBOARD REMOVAL NOT TO EXCEED 4 C-C. R & R THE REPAIRED DOUBLER IAW SRM 51-70-13 CARRIED OUT HFEC INSPECTION IAW NDTM D634N301, REV 100 PART 6 51-00-19 ON TRIMMED OUT AREA AND NO CRACK FOUND. NO FURTHER ACTION REQUIED AND JOB COMPLETED.

Part: SPLICE — DAMAGED (CABIN) · airframe 47,797 hrs · 15,664 cycles

SEATS 21C, 22C, AND 23C EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE APPLIED NEW SPLICE IAW SWPM 23-30-12. OPERATIONS TESTED GOOD.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 45,391 hrs · 15,321 cycles

DURING L-CHECK FOUND NR 2 PYLON STRUT LT SKIN PANEL, CRACKED AT FWD UPPER CORNER INNER AND OUTER SKIN APPROX .5" IN LENGTH. NR 2 PYLON STRUT LT SKIN PANEL REPAIRED IAW EM 5451-01010-02C.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 45,391 hrs · 15,321 cycles

DURING L-CHECK FOUND NR 2 PYLON STRUT RT SKIN PANEL CRACKED FOUND AT FWD UPPER CORNER OUTER SKIN APPROX .3750" IN LENGTH. NR 2 PYLON STRUT RT SKIN PANEL REPAIRED IAW EM 5451-01010-02D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,096 hrs · 15,005 cycles

DURING LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT SEAT 23 ABC INOPERATIVE. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 43,030 hrs · 14,995 cycles

DURING LAYOVER CHECK, MX FOUND EMERGENCY PATH LIGHT AT SEAT 30L INOPERATIVE. MX REPAIRED THE WIRING. OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,914 hrs · 14,978 cycles

FOUND LT ROW SEATS 36-40 EMERGENCY ESCAPE PATH LIGHTING AND AISLE OVERHEAD BIN WOULD NOT ILLUMINATE DURING TEST. REPLACED BATTERY AND POWER SUPPLY IAW AMDS 33-51-07-201-925A-A.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,162 hrs · 14,694 cycles

EMERGENCY FLOOR PROXIMITY LIGHT INOPERATIVE AT ROW 38. REPLACED FLOOR PROXIMITY LIGHT WIRE HARNESS ASSY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,753 hrs · 14,538 cycles

DURING LINE CHECK EMERGENCY LIGHTS BELOW OVERHEAD BIN DOORS 20L BETWEEN 23 AND 24L, AND 25R EXTINGUISHED AFTER 20 SECONDS OF EMERGENCY LIGHT SWITCH ACTIVATION. MAINTENANCE REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING AN OVERNIGHT LINE CHECK THE EMERGENCY LIGHTS AT BOTH SETS OF OVERWING EXITS WERE FOUND TO BE INOPERATIVE. MX FOUND THE ASSOCIATED BATTERY PACKS TO BE DEFECTIVE AND REPLACED THEM. SYS OPS WAS NORMAL AFTER THE BATTERY PACKS WERE REPLACED. (K)

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS)

DURING AN OVERNIGHT LINE CHECK, THE EMERGENCY LIGHTS AT ROWS 30 THROUGH 34 FAILED TO ILLUMINATE. MX FOUND BATTERY PACK M735 TO BE DEFECTIVE AND REPLACED IT. SYS OPS WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED. (K)

Part: SKIN PANEL — CRACKED (RT PYLON) · airframe 33,538 hrs · 13,239 cycles

DURING "M" CHECK FOUND CRACK IN NR 2 PYLON RT SKIN PANEL ASSEMBLY HOLE CUTOUT NEAR NAC STA 132. REPAIRED PER EA 56-194174.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,027 hrs · 11,979 cycles

DURING LINE CHECK, FOUND EMERGENCY PATH LIGHTING ROWS 40 TO 42 AND DOOR 4 RIGHT ESCAPE SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED (M736) BATTERY PACK AND CHECKS NORMAL.

Part: ENGINE — FLAMED OUT (NR 1) · airframe 25,229 hrs · 9,987 cycles

DURING CRUISE FLIGHT, THE NR 1 ENGINE FLAMED OUT. FLIGHT RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL CONTROL, FUEL PUMP, AND EEC. MAINTENANCE ALSO INSPECTED THE EEC ALTERNATOR AND PMA STATOR. NO TROUBLE FOUND.

Part: WHEEL — FAILED (NLG) · airframe 17,669 hrs · 7,123 cycles

DURING TAXI, APPROACHING RUNWAY FOR TAKEOFF, FLIGHT CREW HEARD NOSE GEAR POP. IMMEDIATELY INFORMED BY ANOTHER AIRCRAFT THAT THE TIRE APPEARED TO BE SEPARATING FROM THE WHEEL. MAINTENANCE FOUND THE BEAD FLANGE ON THE WHEEL SEPARATED. REPLACED BOTH NOSE GEAR WHEEL ASSEMBLIES.

Part: POWER SUPPLY — INOP (ROW 16-19)

DURING SCHEDULED MAINTENANCE, THE SEAT MOUNTED EMERGENCY LIGHTS ON ROWS 16-19 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY WITH A SERVICEABLE UNIT. OPERATIONAL TESTS WERE SATISFACTORY.

Part: PUMP — FAILED (RT HYD SYST)

EN ROUTE PHX-DTW, THE RIGHT HYDRAULIC SYSTEM OVERHEATED. THE RIGHT HYDRAULIC PUMP WAS DEACTIVATED. RIGHT SYSTEM PRESSURE WAS NORMAL FOR APPROXIMATELY 15 MINUTES THEN THE RIGHT SYSTEM QUANTITY SLOWLY DECREASED TO ZERO. THE FLIGHT DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP AND ITS ASSOCIATED FILTERS. SYSTEM TESTS WERE SATISFACTORY.