N6704Z

Part: LIGHT — NO TEST (ZONE 200) · airframe 80,616 hrs · 31,414 cycles

DURING CHECK 55 EMERGENCY LIGHTS CHECK, FOUND 4L & 4R EXTERIOR DOOR LIGHTS INOP. T/S PER B757 FIM33-51-00-815-803. PERFORMED WIRE CHECKS AT L56, HAS 6VDC & .4 OHM GROUND REF B757 WDM 33-51-15. REMOVED AND REPLACED 4L (L56) LIGHT FERRULE ASSY REF CMM 33-51-42. OPS CHECK OF 4L & 4R GROUND/SLIDE ILLUMINATION LIGHTS GOOD REF B757 AMM 33-51. (7787819)

Part: HANDLE — BROKEN (ZONE 800) · airframe 80,360 hrs · 31,305 cycles

WHILE OPENING L1 DOOR, HANDLE BROKE OFF. R & R L1 DOOR HANDLE IAW AMM 52-11. (8219403)

Part: PUSHROD — CORRODED (ZONE 800) · airframe 80,239 hrs · 31,256 cycles

WHILE PERFORMING W/C 5210-01065-03-4R, 4R PAX DOOR NEEDS ADJUSTMENT. DURING INSPECT OF EMERGENCY MECHANISM OF R4 DOOR, FOUND PUSHROD A WITH CORROSION. REMOVED PUSHROD IAW CMM 52-11-25. REMOVED CORROSION. INSTALLED PUSHROD IAW CMM 52-11-25. (7534662)

Part: SLIDE — NO TEST (ZONE 800) · airframe 79,558 hrs · 30,931 cycles

SHIP 6704 LEFT OVERWING ESCAPE SLIDE FAILED TO DEPLOY PER AMDS 2566-2003- LT. REMOVED UNPRESSURIZED BOTTLE PER AMDS WORK CARD 2565-4646-LH. REMOVED OFF WING ESCAPE ACTUATOR AND INSTALLED OFF -WING ESCAPE SYSTEM ACTUATOR PER AMM 25-65-05. SLIDE REPLACED ON WC 2560-9901-LT. BOTTLE REPLACED ON WC 2565-4646-LH.

Part: COVER — LOOSE (ZONE 200) · airframe 79,277 hrs · 30,813 cycles

SHIP 6704 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603 / MYCABIN TEXT: FRC335101603 EMERGENCY EXIT SIGN COVER FELL OFF DURING TAKEOFF. CORRECTIVE ACTION: SECURED SIGN OK FOR SERVICE. (1035217)

Part: GIRT BAR — FOD (ZONE 800) · airframe 79,250 hrs · 30,802 cycles

SHIP 6704 R1 DOOR ARM LIGHT DOES NOT ILLUMINATE WITH DOOR ARMED. CORRECTIVE ACTION: FOUND DEBRIS @ R1 GIRT BAR DOOR SNSR CLEANED SNSR OPS CHK NML IAW B757 AMM 25-66. (1028210)

Part: COVER — DETACHED (ZONE 200) · airframe 79,222 hrs · 30,794 cycles

SHIP 6704 EXIT SIGN COVER CAME OFF AT L2 DOOR. CORRECTIVE ACTION: RESECURED COVER REF B757 AMM 33-51. (7498600)

Part: LIGHT — DAMAGED (ZONE 200) · airframe 78,574 hrs · 30,452 cycles

SHIP 6704 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:16D EMERGENCY LIGHT BOX KEEPS FALLING OFF SEAT FRAME. CORRECTIVE ACTION: REPLACED HOUSING ON EMERGENCY LIGHT BOX AT 16D PER B757 CMM 25- 22-58. (0868386)

Part: LANYARD — UNSECURE (ZONE 800) · airframe 78,392 hrs · 30,365 cycles

SHIP 6704 AT DEPARTURE CREW REPORTS L2 DOOR SLIDE MOORING LINE HANGING OUT. CORRECTIVE ACTION: REINSTALLED MORRING LINE REF B757 AMM 25-66. (6882908)

Part: GIRT BAR — STUCK (ZONE 800) · airframe 78,259 hrs · 30,309 cycles

SHIP 6704 R1 SVC DOOR GIRT BAR STUCK. CORRECTIVE ACTION: PINNED SLIDE TO REPOSITION GIRT SLIDE PER B757 AMM 25-66. ALL CHKS GOOD. RMVD PIN. (6410140)

Part: LANYARD — UNSECURE (ZONE 800) · airframe 78,259 hrs · 30,309 cycles

SHIP 6704 A STRING WAS HANGING OUT OF THE L2 DOOR UPON ARRIVAL. CORRECTIVE ACTION: RESECURED L2 ESCAPE SLIDE LANYARD, OK FOR SVC. (6410128)

Part: GIRT BAR — LACK OF LUBE (ZONE 800) · airframe 78,016 hrs · 30,169 cycles

SHIP 6704 DOOR 1R "SLIDE" WILL NOT EXTINGUISH EVEN WHEN DOOR IS DIS-ARMED. CORRECTIVE ACTION: FOUND ARMNG/DISARMING DIFFICULT. LUBED GIRT BAR FITTINGS PER B757 AMM 52-11. (6501806)

Part: PROXIMITY SENSOR — DIRTY (ZONE 800) · airframe 78,016 hrs · 30,169 cycles

SHIP 6704 SLIDE LIGHT AT 1R DOOR WILL NOT EXTINGUISH. CHECK HISTORY. CORRECTIVE ACTION: INSTALLED NEW SLIDE ARMED LIGHT LED CAP- PUT ORINIGAL BACK IN. FOUND DEBRIS ON AFT GIRT BAR PROX SENSOR- CLEANED OFF. OPS CHECKS GOOD. REF B757 AMM 25-66. (6501810)

Part: GIRT BAR — FOD (ZONE 800) · airframe 77,931 hrs · 30,131 cycles

SHIP 6704 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S/ R2 ARM LIGHT INOP. CORRECTIVE ACTION: CLEANED DEBRIS AND BUILD UP FROM GIRT BAR R1 TRACK AND PROX SWITCHES. IAW B757 AMM 25-66. LUBRICATED COMPONENTS. OPS CHK NML. (0723987)

Part: LEVER — OUT OF ADJUST (ZONE 800) · airframe 77,904 hrs · 30,120 cycles

SHIP 6704 L-1 DOOR SLIDE ARMING LEVER OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED GIRT BAR MECHANISM AT L1 DOOR IAW B757 AMM 52-11-25. (0715078)

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 77,898 hrs · 30,115 cycles

SHIP 6704 **AD RELATED** L4 DOOR "SLIDE" LIGHT FAILED TO ILLUMINATE. CORRECTIVE ACTION: LOCATED AND RE-CONNECTED L4 DOOR "SLIDE" LIGHT IAW B757 AMM 25- 21-06. PERFORMED SATISFACTORY GIRT BAR ENGAGEMENT LIGHT OPERATIONAL CHECK IAW B757 AMM 25-66-11. (0713214)

Part: ACTUATOR — FAILED (SLIDE DOOR) · airframe 77,893 hrs · 30,111 cycles

SHIP 6704 UPON OPS CHECK OF OVERWING SLIDE PNEUMATIC DEPLOYMENT, R/H ACTUATOR FAILS TO OPEN SLIDE COMPARTMENT DOOR AND DEPLOY SLIDE CARRIER. FOLLOWED FRMFIM 25-65-00-815-804, STILL FAILS FUNCTIONAL CHECK. CORRECTIVE ACTION: REMOVED, REPLACED AND PERFORMED SATISFACTORY OPS CHECK OF OFF-WING ESCAPE SYSTEM ACTUATOR IAW B757 AMM 25-65-05. (0712111)

Part: ELEC CONNECTOR — MISSING (ZONE 200) · airframe 77,893 hrs · 30,111 cycles

SHIP 6704 EEPL CABLES MISSING CONNECTOR AT FOLLOWING LOCATIONS: BS 560, 780, 820, 880, 940, 1040, 1440, 1560, 1580. CORRETIVE ACTION: REPLACED EEPLS CONNECTORS AT BS 560, 780, 820, 880, 940, 1040, 1440, 1560, 1580. IAW B757 SWPM 20-42-01. PERFORMED A SATISFACTORY OPS CHECK OF EEPLS LIGHTS AT BS 560, 780, 820, 880, 940, 1040, 1440, 1560, 1580 IAW B757 AMM 33-51-04. (0711738)

Part: NONE — NONE (NONE) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 AD RELATED: CONTACT LIAISON ENGINEERING, ADDITIONAL ENGINEERING DOCUMENTATION, APPROVAL AS AN AMOC TO AD 2019-07-04, MAY BE REQUIRED BEFORE FURTHER FLIGHT. LAP SPLICE AT S-14 FOUND EXISTING REPAIR AT STA 570. REPAIR DOT # 510972-14. CORRECTIVE ACTION: REF ERA 510972-14. (0709890)

Part: SKIN — NOT REPORTED (ZONE 100) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 REPAIR TO FUSELAGE SKIN AT STA 600-650, S-14L-19L REQUIRES MODIFICATION PER SECTION II OF ERA 510972-14AD REV A. CORRECTIVE ACTION: REF ERA 510572-14AD. (0708742)

Part: GATE — CORRODED (ZONE 800) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 #4 LEFT PASSENGER DOOR LOWER GATE HAS PITTING CORROSION, LOWER EXTERNAL SURFACE ALONG THE EDGE. DOT 129-065. CORRECTIVE ACTION: REMOVED AND REPLACED L4 LOWER GATE IAW B757 AMM 52-11-38. (0703051)

Part: TRANSITION PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 AFT CARGO COMP. LH TRANSITION PANEL STA 1410 TO STA 1530 HAS CORROSION ON SEVERAL AREAS. CORRECTIVE ACTION: SUMMARY OF NR-00609- REMOVED CORROSION AND EVALUATED LH TRANSITION PANEL FROM STA 1410 TO 1500 IAW B757 SRM 51-10-02 AND ERA 491157-14 MA REV A, FOUND WITHIN LIMITS, TRANSITION PANEL FROM STA 1500 TO STA 1530 FOUND OUT OF LIMITS WITH 100% MAT LOSS, REMOVED, FABRICATED REPAIR AND INSTALLED LH TRANSITION PANEL STA 1500 TO STA 1530 IAW B757 SRM. (0703073)

Part: STOP FITTING — WORN (ZONE 200) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 R1 AFT DOOR FRAME DOOR STOP THRID STOP DOWN FROM TOP PAD IS WORN . DOT 45. I-13. CORRECTIVE ACTION: REMOVED AND REPLACED R1 DOOR STOP PAD AFT THIRD PAD DOWN IAW DELTA PS 900-11-3 NO. 03. (0701218)

Part: STOP FITTING — WORN (ZONE 200) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 R1 AFT DOOR FRAME DOOR STOP PAD FIFTH ONE DOWN IS WORN. DOT 45. I-13. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR STOP PAD ON R1 DOOR AFT FRAME 5TH ONE DOWN IAW DELTA P.S. 900-11-3 #03. (0701238)

Part: STOP FITTING — WORN (ZONE 200) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 R1 AFT DOOR FRAME DOOR STOP PAD FOURTH ONE DOWN FROM TOP IS WORN . DOT 44. I-13. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR STOP ON R1 DOOR AFT FRAME 4TH ONE DOWN IAW DELTA P.S. 900-11-3 #03. (0701232)

Part: STOP FITTING — WORN (ZONE 200) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 R1 DOOR FRAME UPPER AFT DOOR STOP PAD IS WORN. DOT 44. I-13. CORRECTIVE ACTION: REMOVED AND REPLACED R1 DOOR FRAME UPPER AFT DOOR STOP PAD IAW DELTA PS 900-11-3 NO. 03. (0700053)

Part: STOP FITTING — MISINSTALLED (ZONE 800) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 #1 LT PASSENGER DOOR AFT FRAME DOOR-MOUNTED STOP FITTINGS #2 AND #3 FROM BOTTOM TO TOP HAVE LOCK SPRINGS NOT PROPERLY INSTALLED. DOT 129-068. CORRECTIVE ACTION: REPOSITIONED AND PROPERLY INSTALLED LOCK SPRINGS ON #1 LT PASSENGER DOOR AFT FRAME DOOR-MOUNTED STOP FITTINGS #2 AND #3 IAW B757 AMM 20-10-23. (0700031)

Part: GUIDE FITTING — WORN (ZONE 800) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 L1 DOOR FRAME AFT DOOR GUIDE FITTING IS WORN. DOT 43. I-13. CORRECTIVE ACTION: REMOVED AND REPLACED TRACK AT L-1 CUT DOOR AFT FRAME IAW B 757 AMM 52-11-37-094-32 AND AMM 52-11-37-404-038. (0700046)

Part: STOP FITTING — MISINSTALLED (ZONE 200) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 #4 LEFT PASSENGER DOOR FWD FRAME DOOR-MOUNTED STOP FITTING #3 FROM TOP TO BOTTOM HAS THE LOCK SPRING NOT PROPERLY INSTALLED. DOT 129-067. CORRECTIVE ACTION: REPOSITIONED AND PROPERLY INSTALLED LOCK SPRING ON #4 LEFT PASSENGER DOOR FWD FRAME DOOR-MOUNTED STOP FITTING #3 IAW B757 AMM 20-10-23. (0700035)

Part: SKIN — CRACKED (ZONE 500) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 INDICATION OF CRACK NOTED ENG DRAG FTG CLAMP UP HOLE # 13 IN THE TOP SKIN AT APPROX. 3 O'CLOCK POSITION FACING AFT. CORRECTIVE ACTION: -SUMMARY OF NR-00252- ACCOMPLISHED REPAIR ON HOLE #13 ON LH OUTER WING UPPER SKIN AT DRAG FITTINGS IAW ER/A 622147-14AD REV ORIG SECTION I. (0698105)

Part: SKIN — DAMAGED (ZONE 500) · airframe 77,892 hrs · 30,109 cycles

REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 622147-14AD. CORRECTIVE ACTION: REF ERA 622147-14AD. (0696718)

Part: PRESSURE PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION IN AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE, BS.1680 RBL.12.5. DOT 129-046. CORRECTIVE ACTION: COMPLIED WITH ER/A 622427-14 REV ORIGINAL AT AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE, BS.1680 RBL.12.5. (0694590)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,445 hrs · 30,389 cycles

SHIP 6704 MAIN CABIN, Z FLOOR SUPPORT HAS CORROSION AT STA 330 TO STA 365 RBL59. CORRECTIVE ACTION: COMPLIED WITH ER/A 622556-14 REV ORIGINAL MAIN CABIN, Z FLOOR SUPPORT AT STA 330 TO STA 365 RBL59. (0695014)

Part: PRESSURE PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION AROUND FASTENER HOLES IN AFT CABIN FLOOR STRUCTURE PRESSURE PLATE BS.1680 BETWEEN LBL.3 AND LBL .53.5. DOT 129-0554. CORRECTIVE ACTION: COMPLIED WITH ER/A 622427-14 REV ORIGINAL AT AFT CABIN FLOOR STRUCTURE PRESSURE PLATE BS.1680 BETWEEN LBL.3 AND LBL.53.5. (0694563)

Part: FRAME — DENTED (STA 1520 STR 26-) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 AFT CARGO FRAME AT STA 1520 STR 26-27 LEFT DENT FOUND UNDER UPPER FLANGE. CORRECTIVE ACTION: TRIM OUT DENTED AREA ON FRAME STA 1520 BETWEEN S26L TO S25L IAW 757 SRM 53-00-07-2R, VERIFIED MATERIAL TO FABRICATE U CHANNEL, HEAT TREATED, FABRICATED LOCATED, DRILLED, TRIMMED APPLIED SURFACE FINISH AND INSTALLED REPAIR PARTS, IAW B 757 SRM 53-00-07-2R-5. (0691606)

Part: BEAM — CORRODED (STA 365 RBL46 TO) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 MAIN CABIN, FLOOR BEAM HAS CORROSION AT STA 365 RBL46 TO RBL59. CORRECTIVE ACTION: SUMMARY OF- EVALUATED BLENDED AREA WITH AT MAIN CABIN COMPARTMENT FLOOR BEAM STA 365.25 BWTN RBL. FOUND TO BE OUT LIMITS IAW B757 SRM 53-00-51. REPAIRED MAIN CABIN FLOOR BEAM AT STA 365 RBL46 TO RBL59 IAW DELTA ERA 481634-14MA REV. B

Part: FRAME — DENTED (STA 1500 STR 26-) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 AFT CARGO FRAME AT STA 1500 STR 26-27 LEFT HAND SIDE DENT FOUND UNDER UPPER FLANGE. CORRECTIVE ACTION: SUMMARY OF- TRIM OUT DENTED AREA ON FRAME 1500 BETWEEN SRT 26L TO STR 25L, VERIFIED MATERIAL ID 7075-O .071" PO # FS71436 TO FABRICATE U CHANNEL REPAIR, FABRICATED, HEAT TREATED LOCATED, DRILLED, TRIMMED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B 757 SRM 53-00-07-2R-5. (0691566)

Part: FRAME — DENTED (STA 1440 STR 26-) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 AFT CARGO LEFT HAND FRAME AT STA 1440 STR 26-27 DENTS FOUND UNDER UPPER FLANGE. CORRECTIVE ACTION: SUMMARY OF- TRIM OUT DENTED AREA ON FRAME 1440 BETWEEN STR 25LTO STR 26L, VERIFIED MATERIAL TO FABRICATE U CHANNEL REPAIR, FABRICATED, HEAT TREATED, LOCATED DRILLED, APPLIED SURFACE FINISH AND INSTALLED REPAIR PARTS IAW B 757 SRM 53-00-07-2R-5 REPAIR 5. (0691326)

Part: ANGLE — CORRODED (L-2 DOOR) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 MAIN CABIN, L-2 DOOR, STA 720 TO STA 720, FLOOR SUPPORT ANGLE HAS CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SUPPORT AND ANGLE AT MAIN CABIN, L-2 DOOR, STA 720 TO STA 720, IAW B757-200 SRM 51-40-02, SRM. (0691636)

Part: PLATE — CORRODED (AFT CABIN FLOOR) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION IN AFT CABIN FLOOR STRUCTURE PRESSURE PLATE EXISTING REPAIR, APROX' BS.1716 LBL.41. DOT 129-056. CORRECTIVE ACTION: REMOVED IN AFT CABIN FLOOR STRUCTURE PRESSURE PLATE EXISTING REPAIR, APROX' BS.1716 LBL.41 IAW B757 SRM 51-40-02, FABRICATED NEW DOUBLER AND FILLER REPAIR. IAW B757 SRM 53-60-51-2R PROCEDURE 2, FIG 201, TABLE II , IAW B757 SRM 51-40-05 AND IAW B757 SRM 51-40-08 INSTALLED NEW DOUBLER REPAIR AND FILLER IN AFT CABIN FLOOR STRUCTURE PRESSURE AT APROX' BS.1716 BTW LBL 15 LBL TO LBL.41, IAW B757 SRM 51-40- 02 AND IAW B757 SRM 53-60-51-2R PROCEDURE 2.

Part: PRESSURE PLATE — CORRODED (BS.1716 RBL.23) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION AROUND DRAIN HOLE AT EXISTING REPAIR AFT CABIN FLOOR STRUCTURE PRESSURE PLATE APROX' BS.1716 RBL.23. DOT 129-057. CORRECTIVE ACTION: REMOVED EXISTING REPAIR LOCATED AT DECK PLATE BSTA.1716 RBL.23. IAW. B757 SRM .51-40-02-0G, INSTALLATION OF REPAIR PARTS, DOUBLER AND FILLER ACCOMPLIHED IAW B 757 SRM 53-60-51-2R ON N/R 00390. (0681429)

Part: PLATE — CORRODED (AFT MAIN CBN FLO) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION IN AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE, APROX' BS.1714 RBL.48. DOT 129-060. CORRECTIVE ACTION: REMOVED CORROSION AT AFT MAIN CABIN FLOOR SRUCTURE PRESSURE PLATE BS 1714 RBL 48 IAW B 757 SRM 51-10-02 EVALUATED AREA, FOUND AREA TO BE OUT OF LIMITS IAW B 757 SRM 53-00-51, FABRICATED FILLER REPAIR, FABRICATED DOUBLER AS REQ IAW B 757 SRM 53-60-51-2R, INSTALLED REPAIR PARTS AT BS 1714 AT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE IAW B757 SRM. (0681306)

Part: PRESSURE PLATE — CORRODED (AFT MAIN CABIN F) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION IN AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE APROX' BS.1716 RBL.9.5. DOT 129-059. CORRECTIVE ACTION: REMOVED CORROSION FROM AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE APROX' BS.1716 RBL.9.5 IAW B757-200-SRM-51-10-02, EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51 AD1, REPAIR OF AREA DEEMED OUT OF LIMITS AT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE APROX' BS.1716 RBL.9.5 WAS ACCOMPLISHED ON N/R'S 00390 AND 00392. (0681331)

Part: PLATE — CORRODED (AFT CABIN FLOOR) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION ON TOP OF AFT CABIN FLOOR STRUCTURE ATTACH PLATE, BS.1681 BL.0. DOT 129-049. CORRECTIVE ACTION: SUMMARY OF-REMOVED ATTACH PLATE FROM TOP OF AFT CABIN FLOOR STRUCTURE BS.1681 BL.0. IAW B757-200-SRM-51-40-02, FABRICATED, LOCATED AND DRILLED NEW STRUCTURE ATTACH PLATE IAW DWG ID: 0011 REV: -, INSTALLED NEW ATTACH PLATE FROM TOP OF AFT CABIN FLOOR STRUCTURE BS.1681 BL.0. IAW B757-200-SRM. (0679408)

Part: WIRE HARNESS — DAMAGED (ZONE 200) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 RH EEPLS EWIS HARNESS PROTECTIVE SLEEVING DAMAGED MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED RH EEPLS HARNESS PROTECTIVE SLEEVING AT MULTIPLE LOCATIONS IAW B757 SWPM 20-10-11. (0675931)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION ON TOP OF MAIN CABIN FLOOR BEAM BS.1640 LBL.40. DOT 129-048. CORRECTIVE ACTION: ACCOMPLISHED FLOOR BEAM CAP BLEND REPAIR AT TOP OF MAIN CABIN FLOOR BEAM BS.1640 LBL.40 IAW ER/A 481634-14MA REV B. (0674307)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 CORROSION ON TOP OF MAIN CABIN FLOOR BEAM EXISTING REPAIR BS.1640 BETWEEN BL.0 AND LBL.5. CORRECTIVE ACTION: REMOVED EXISTING REPAIR AT MAIN CABIN FLOOR BEAM STA 1640 BL 0 IAW B 757 SRM 51-40-02, FABRICATED, LOCATED, DRILLED, TRIMMED APPLIED FINISH TO NEW REPAIR PART BAC 1505-100617. 7075T6 AND INSTALLED IAW B 757 SRM 53-00-51-2R, B 757 SRM 51-20-01, B 757 SRM 51-40-02. (0674326)

Part: LINE — DISCONNECTED (L2 DOOR) · airframe 77,892 hrs · 30,109 cycles

SHIP 6704 DURING OPEN UP, FOUND L2 PNEUMATIC ACTUATOR LINE DISCONNECTED. CORRECTIVE ACTION: CONNECTED L2 PNEUMATIC ACTUATOR PRESSURE LINE IAW B757 AMM 52-11-34 (0671255)

Part: TAILPIPE — FIRE (LT ENGINE) · airframe 77,726 hrs · 30,012 cycles

SHIP 6704 -FIRE/DE- DURING LEFT ENGINE START, LEFT ENGINE EXPERIENCED A TAIL PIPE FIRE. FLIGHT RETURNED TO THE GATE AND FIRE EXTINGUISHED ON ITS OWN ON SHUTDOWN. ARFF RESPONDED BUT NO ACTION WAS TAKEN. AIRCRAFT WAS CLEARED TO BE TOWED BACK TO THE GATE. CORRECTIVE ACTION: REPLACED LEFT ENGINE EEC AND ENGINE BORO. REPLACED #5 SPOILER AND CANOE FAIRING, SUBSEQUENTLY CHANGED LEFT ENGINE.

Part: GIRT BAR — DETACHED (ZONE 800) · airframe 77,623 hrs · 29,940 cycles

SHIP 6704 AFT LEFT DOOR GIRT BAR FELL OUT OF DOOR. CORRECTIVE ACTION: REINSTALLED GIRT BAR PER B757 AMM 25-66-10. GIRT BAR ENGAGES/ DISENGAGES NORMALLY. (5532896)

Part: TIRE — FAILED (NR 3) · airframe 77,136 hrs · 29,688 cycles

SHIP 6704 -TIRE- NUMBER 3 TIRE FOUND BLOWN AFTER LANDING. CORRECTIVE ACTION: PERFORMED BURST TIRE INSPECTION AND REPLACED NUMBER 3 MAIN TIRE/WHEEL ASSY.

Part: NUT — MISSING (L4 GIRT BAR) · airframe 76,888 hrs · 29,571 cycles

AIRCRAFT 6704, DUE TO REPORTS OF THE 4L DIFICAULT TO ARM. CORRECTIVE ACTION: INSTALLED SLIDE PIN ON 4L DOOR FOR MTC. INSPECTED AND PERFORM TEST OF GIRT BAR MECHANISM REF B757 AMM 52-11-25, FOUND GIRT BAR AFT SECURE CAM MISSING NUT AND NOT SECURED REF B757 IPC 52-11-20-34 ITEM 516, RESECURED CAM, OPS CHECKS GOOD. (LP 0371664)

Part: GIRT BAR — DETACHED (L3 DOOR) · airframe 76,888 hrs · 29,571 cycles

AIRCRAFT 6704, 3L GIRT BAR LOCK ASSY FELL OFF 3L GIRT BAR. CORRECTIVE ACTION: FOUND GIRT BAR END RE-ATTACHED GIRT BAR END WITH ORIG HARDWARE. OPERATED DOOR ENGAGMENT HANDLE OPERATES NORMAL. (LP 4832077)

Part: GIRT BAR — LOOSE (L3 DOOR) · airframe 76,888 hrs · 29,571 cycles

AIRCRAFT 6704, 3L ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOP. CORRECTIVE ACTION: FOUND GIRT BAR CAM LOOSE, RESECURED. GIRT BAR OPS GOOD REF B757 AMM 52-11. GIRT BAR ARM LIGHT OPS GOOD. (LP 0371257)

Part: INDICATOR — MALFUNCTIONED (R1 DOOR) · airframe 76,849 hrs · 29,556 cycles

SHIP 6704 R1 DOOR SLIDE LIGHT NOT ILLUMINATED AT DEPT. CORRECTIVE ACTION: CYCLED R1 DOOR ARMING LEVER - NOW CKS OK PER 757 AMM 2560. (4832048)

Part: LOCK — MISSING (L4 GIRT BAR) · airframe 76,664 hrs · 29,466 cycles

SHIP 6704 4L AFT LEFT DOOR WAS MAKING UNUSUAL SOUNDS ON THE CLIMBOUT. FA SAIT WAS LOUDER THAN USUAL. CORRECTIVE ACTION: INSPECTED DOOR FOUND FWD GIRT BAR LOCK ASSY WAS MISSING, INSTALLED REPLACEMENT ASSY PER B757 AMM 25-66-10 OPS CK GOOD. (5674576)

Part: NONE — NONE (NONE) · airframe 76,415 hrs · 29,334 cycles

SHIP 6704 MAN CUTS HIS LEG ON SEAT 40C ON A PIECE OF METAL. BLOOD ON IT. CLEANERS ON TOP OF IT. CORRECTIVE ACTION: INSP. SEAT AREA AT SEAT 40C, COULD NOT FIND SHAP OBJECT OR EDGES ON SEAT. PASSENGER DOESN'T KNOW WHERE HE RECIEVED CUT. OK FOR SVC. PER B757 AMM 25-21. (5830448)

Part: GIRT BAR — FOD (L3 DOOR AREA) · airframe 76,219 hrs · 29,226 cycles

SHIP 6704 3L SLIDE LIGHT EXTINGUISHED WHILE DOOR WAS ARMED. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR MECHANISM. OPS CK GOOD. (5774330)

Part: LANYARD — UNSECURE (L4 DOOR SLIDE) · airframe 76,128 hrs · 29,180 cycles

SHIP 6704 4L SLIDE LANYARD IS HANGING DOWN. CORRECTIVE ACTION: SECURED 4L SLIDE LANYARD.OK FOR SERVICE.SLIDE ARMS FINE. (5043086)

Part: ROPE — OUT OF POSITION (R1 DOOR SLIDE) · airframe 76,115 hrs · 29,171 cycles

SHIP 6704 MOORING ROPE HANGING FROM R1 DOOR SLIDE PACK. CORRECTIVE ACTION: RE-INST ROPE IN R1 SLIDE PACK- CKS GOOD. B757 AMM 2566. (5043083)

Part: COMPUTER — INOPERATIVE (TCAS) · airframe 76,090 hrs · 29,156 cycles

SHIP 6704 -ATB- DUE TO TCAS INOP. UNABLE TO CONTINUE DUE TO THEATER RESTRICTIONS. CORRECTIVE ACTION: REPLACED TCAS COMPUTER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,519 hrs · 28,889 cycles

SHIP 6704 2L DOOR WONT CLOSE. CORRECTIVE ACTION: REMOVED DEBRIS. OPS CHECKS GOOD PER B757 AMM 52-11 DOOR OPENS AND CLOSES WITHOUT ANY PROBLEMS. (4268306)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,500 hrs · 28,876 cycles

SHIP 6704 POST FLIGHT FOUND COVER FOR OVERWING EXIT SIGN (FWD COVER) DETACHED. CORRECTIVE ACTION: REATTACHED FWD COVER. (4362976)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,407 hrs · 28,823 cycles

SHIP 6704 COULD NOT ARM THE AFT LEFT DOOR. CORRECTIVE ACTION: CYCLED ARM/ DISARM LEVER IAW B757 AMM 25-66. SLIDE LIGHT NOW OPERATES NORMALLY. OK FOR SERVICE. (4362954)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,137 hrs · 28,684 cycles

SHIP 6704 DOOR 3L REPORTED TO BE DIFFICULT TO ARM. CORRECTIVE ACTION INSTALLED SLIDE PIN FOUND GIRT BAR LOCK R/H MISSING. INSTALLED NEW GIRT BAR LOCK OPS CK GOOD REF B757 AMM 25-66 REMOVED AND STOWED SLIDE PIN. (4475730)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,960 hrs · 28,582 cycles

SHIP 6704 THE 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: RESECURED SLIDE GIRT BAR FOLDED PACK MATERIAL INTO PROPER POSITION ARMS NORMAL. (998143)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,920 hrs · 28,554 cycles

SHIP 6704 SLIDE ARMING LATCH ON DOOR 1R IS DIFFICULT TO OPERATE. CORRECTIVE ACTION: T/S PER B757 FIM 52-11-00-815-813. REMOVED DEBRIS. OPS CHECK GOOD. (9981416)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,917 hrs · 28,552 cycles

SHIP 6704 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED FOD FROM GIRT BAR ATTACHMENT. CHECK OK PER B757 AMM 52- 11. DOOR ARMS/DISARMS NORMALLY. (9981412)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,868 hrs · 28,537 cycles

SHIP 6704 R-1 DOOR WONT ARM. CORRECTIVE ACTION: REMOVED DEBRIS AT R1 DOOR. (4874896)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,629 hrs · 28,435 cycles

SHIP 6704 3 LEFT DOOR ARMING LEVER IS NOT GOING INTO THE DISARM POSITION. CORRECTIVE ACTION: REMOVED DEBRIS; DOOR OPS CKS NML REF B757 AMM 52-11. (4916564)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,210 hrs · 28,236 cycles

SHIP 6704 1R DOOR DIFFICULT TO ARM AND SLIDE LIGHT WILLL NOT ILLUMINATE. CORRECTIVE ACTION: PERFORMED R1 DOOR ADJUST & CHECK. CLEARED BLOCKING DEBRIS IAW B757 AMM 52-11. OPS CHK NML. (9725778)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,210 hrs · 28,236 cycles

SHIP 6704 R1 DOOR SLIDE LIGHT NOT ILLUMINATING. ARMING HANDLE SEEMS TO BE IN A BIND. CORRECTIVE ACTION: SLIDE ARM LIGHT OPS NML REF B757 25-66. (9725760)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,997 hrs · 28,113 cycles

SHIP 6704 R1 DOOR WILL NOT ARM. CORRECTIVE ACTION: RESET DOOR AT 1R, CLEARED OBSTRUCTION DOOR NOW WILL ARM & DISARM PER B757 AMM 52-11. OPS CHECKS GOOD. (9970036)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,902 hrs · 28,049 cycles

SHIP 6704 EMERGENCY EXIT SIGN FELL OFF DURING FLIGHT. CORRECTIVE ACTION: RESECURED EMER EXIT SIGN AS REQUIRED REF B757 AMM 33-50. CHECKS GOOD. (2742119)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,749 hrs · 27,960 cycles

SHIP 6704 R4 DOOR INDICATION INOP WITH R4 DOOR OPEN. CORRECTIVE ACTION: REMOVED AND REPLACED R4 DOOR WARNING SENSOR PER B-757 A.M.M. 52- 71-00 AND SWPM CH.20 OP'S CHECK GOOD. (9640063)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,531 hrs · 27,835 cycles

DURING CRV FOUND R2 DOOR SEAT ROW 18 EXIT LIGHT DIFFUSER LENS MISSING. CORRECTIVE ACTION: INSTALLED NEW DIFFUSER LENS AT R2 DOOR PER CMM 33-51-31.

Part: ARMING LEVER — BINDING · airframe 73,218 hrs · 27,659 cycles

SHIP 6704 1L DOOR SLIDE ARMING LEVER BINDING. CORRECTIVE ACTION: REMOVED L1 DOOR ESCAPE SLIDE PER B757 AMM 25-66. ARMING LEVER NO LONGER BINDING, PERFORMED GRIT BAR MECHANISM SYSTEM TEST AS PER B757 52-11 & GRIT BAR AND FLOOR FITTING INSPECTION/CHECK AS PER B757 AMM 25-66, VERIFIED ADJUSTMENTS & MECHANISM ARE GOOD. INSTALLED L1 DOOR SLIDE AS PER AMDS WORKCARD. REPLACED GIRT BAR LOCKS AS PER B757 AMM 25-66. (9810154)

Part: LEVER — UNKNOWN (L1 DOOR) · airframe 73,206 hrs · 27,652 cycles

SHIP 6704 ARMING LEVER AT DOOR L1 WILL NOT MOVE TO THE FULL DISARMED POSITION. CORRECTIVE ACTION: PERFORMED SYSTEM CK FOR L1 DOOR IAW B757 AMM 52-11. CK NORMAL. (9810142)

Part: NONE — NONE (NONE) · airframe 73,186 hrs · 27,646 cycles

ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS FOR L1 DOOR SLIDE ENGAGE LIGHT INOPERATIVE. REINSTALLED GIRT BAR IAW AMM 52-11. . PERFORMED GIRT BAR SYS TEST IAW AMM 52-11. TEST PASSED.

Part: MECHANISM — OUT OF ADJUST (CONTROL HANDLE) · airframe 73,148 hrs · 27,628 cycles

WHILE PERFORMING AMDS 2040-0191-4L STEP 17, THE MODE SELECTOR LEVER DOES NOT RETURN COMPLETELY TO THE DISARMED POSITION AFTER OPENING THE DOOR WITH THE EXTERIOR HANDLE. MODE SELECTOR LOCKOUT MECHANISM WAS ADJUSTED IAW AMM 52-11. ARM / DISARM OPERATION CHECK WAS PERFORMED PER AMDS AND THE MODE SELECTOR LEVER RETURNS COMPLETELY TO THE DISARMED POSITION AFTER OPENING THE DOOR WITH THE EXTERIOR HANDLE.

Part: SNUBBER — OUT OF LIMITS (L4 DOOR) · airframe 73,148 hrs · 27,628 cycles

ROTARY SNUBBER FLUID LEVEL OUT LIMIT AT L4 DOOR. L4 DOOR ROTARY SNUBBER WAS REPLACED IAW AMM 52-11-10.

Part: DRAG FITTING — DAMAGED (RT NACELLE) · airframe 73,148 hrs · 27,628 cycles

DAMAGE FOUND ON OPEN HOLES AT RT ENG DRAG FITTING CLAMP-UP & DIAG BRACE, HOLE 4 CRACK ON SKIN BTW 8 O CLOCK POSITION AND HOLE 8 CORROSION ON SKIN BTW 7 TO 8 O CLOCK POSITION IAW CARD. OPEN HOLES AT RT ENGINE DRAG FITTING HOLE 4, HOLE 5 AND HOLE 8 WERE REPAIRED IAW ER/A 604438-14AD, REV ORIGINAL, SECTION I

Part: NONE — NONE (NONE) · airframe 73,148 hrs · 27,628 cycles

REPAIR TO RT WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS IAW ERA 604438-14AD.

Part: BOTTLE — MALFUNCTIONED (EMERG POWER) · airframe 73,148 hrs · 27,628 cycles

PRESSURE OUT OF LIMITS OF EMERGENCY POWER RESERVOIR IN REF AMDS. EMERGENCY POWER RESERVOIR AT DOOR 4L WAS REMOVED PER AMDS: 2040-0191-4L STEP 4. AND NEW EMERGENCY POWER RESERVOIR INSTALLED PER AMDS.

Part: SNUBBER — OUT OF ADJUST · airframe 73,148 hrs · 27,628 cycles

SHIP 6704 ROTARY SNUBER LEVEL OUT LIMIT AT 1R DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00066: 1R DOOR ROTARY SNUBBER WAS REPLACED BY SERVICEABLE ROTARY SNUBBER PER B757-200 AMM 52-11-10. (2545673)

Part: LEAF SPRING — BROKEN (GIRT BAR) · airframe 73,148 hrs · 27,628 cycles

BROKEN GIRT BAR LEAF SPRING AT R1 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00018: GIRT BAR AT 1R DOOR ESCAPE SLIDE WAS REPLACED PER B757-200 AMM 25-66-10. (2545701)

Part: SNUBBER — OUT OF LIMITS (R2 DOOR) · airframe 73,148 hrs · 27,628 cycles

ROTARY SNNUBER FLUID LEVEL OUT LIMIT AT 2R DOOR. ROTARY SNUBBER ON PASSENGER DOOR 2R WAS REPLACED BY SERVICEABLE ROTARY SNUBBER IAW AMM 52-11-10.

Part: DRAG FITTING — DAMAGED (LT ENGINE) · airframe 73,148 hrs · 27,628 cycles

A.A. / AD (VT) (GVI) WAS PERFORMED AND DAMAGE WAS FOUND ON OPEN HOLES AT THE LT ENG DRAG FTG CLAMP-UP, SECTION 04, HOLE #1 CORROSION ON FITTING, BTW 6 AND 5 O CLOCK POSITION, HOLE #3 CORROSION ON FITTING AT 9 O CLOCK POSITION, HOLE #4 CORROSION ON FITTING AT 9 O CLOCK POSITION, HOLE #7 CORROSION ON SKIN AT 10 O CLOCK POSITION, HOLE #8 CORROSION ON SKIN BTW 11 AND 12 O CLOCK POSITION. OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP WERE REAMED TO FIRST OVERSIZE (0.5778") PER AMDS.

Part: FITTING — CORRODED (GIRT BAR) · airframe 73,148 hrs · 27,628 cycles

CORROSION ON FITTINGS OF SLIDE GIRT BAR, L1, L2 AND R4 DOOR SLIDES. FITTINGS WERE REPLACED IAW SRM.

Part: DRAG FITTING — DAMAGED (LT ENGINE) · airframe 73,148 hrs · 27,628 cycles

A.A. / AD (VT) (GVI) WAS PERFORMED AND DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP, SECTION 05, HOLE #13 CORROSION ON FITTING AT 9 O CLOCK POSITION AND HOLE #17 CORROSION ON FITTING BTW 8 AND 9 O CLOCK POSITION. OPEN HOLES AT LT ENG DRAG FTG CLAMP-UP HOLES #13 AND #17 WERE REAMED TO FIRST OVERSIZE (0.5778") PER AMDS.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 72,985 hrs · 27,533 cycles

SHIP 6704 2R DOOR "EXIT" PLASTIC COVER POPPED OFF. REINSTALLED 2R DOOR "EXIT" PLASTIC COVER SIGN AS REQUIRE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 72,985 hrs · 27,533 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. SECURED EMERGENCY EXIT COVER IN PLACE.

Part: POWER SUPPLY — INOPERATIVE · airframe 72,973 hrs · 27,523 cycles

SHIP 6704 ON SVC CHECK FOUND EEPLS ON ROWS 18 - 22 INOP. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY OVER L2 DOOR PER B757 AMM 33-51. CHECKS GOOD. (9380572)

Part: NONE — NONE · airframe 72,536 hrs · 27,271 cycles

SHIP 6704 ELECTRIC BURNING ODOR AROUND SEAT 18E. CORRECTIVE ACTION: REMOVED AND REPLACED OUTLET 18E REF IPC 23-82-04 OUTLET CKS GOOD CMM 25-21. (9030930)

Part: NONE — NONE · airframe 72,493 hrs · 27,245 cycles

SHIP 6704 -ATB- DUE TO DUAL VHF FAILURE. CORRECTIVE ACTION: REPLACED OBS HAND MIC AND F/O'S FREQ SELECT PANEL DUE TO STUCK MIC AND TRANSFER SWITCH INOP. OPS CHECK SUCCESSFUL.

Part: INDICATOR — OUT OF ADJUST · airframe 71,972 hrs · 26,959 cycles

SHIP 6704 DOOR 2R KNUCKLE GUARD NOT EXTENEDED WHEN DOOR ARMED. CORRECTIVE ACTION; ADJUSTED 2R KNUCKLE GUARD AS PER B757 AMM 52-11. OPS NML. EXTENDS FULLY. (8473698)

Part: LIGHT — INOPERATIVE · airframe 71,624 hrs · 26,825 cycles

SHIP 6704 SEAT MOUNTED EMERGENCY LIGHT OUT AT SEAT 21D. CORRECTIVE ACTION: REMOVED AND REPLACED LIGHT ASSY AT SEAT 21D IN REF TO B757-AMM- 33-51. NOW CKS GOOD. (8826257)

Part: NONE — NONE · airframe 71,282 hrs · 26,675 cycles

SHIP 6704 R4 DOOR GIRT BAR FALLING OFF. CORRECTIVE ACTION: RMVD SLIDE BUSTLE AND INSTALLED SAFETY PIN IN SLIDE BOTTLE. INSPECTED R4 DOOR GIRT BAR PER B757 AMM 25-66, NO DEFECTS NOTED. SLIDE ARMS AND DISARMS AS NORMAL. ADJUSTED GIRT BAR MECHANISM PER B757 AMM 52-11. OPS CHECK GOOD. REMOVED R4 DOOR SLIDE FOR MTC PER WORK CARD. INSTALLED R4 SLIDE AND BUSTLE PER WORK CARD. SLIDE PIN REMOVED PER WORK CARD. (8561498)

Part: NONE — NONE · airframe 71,250 hrs · 26,662 cycles

SHIP 6704 FOUND 1R PAX DOOR "SLIDE LIGHT" ONE BULB BURNT ABOVE DOOR. CORRECTIVE ACTION: R/R R1 DOOR ESCAPE SLIDE ARMED LIGHT, LIGHT WORKING NORMAL PER B757 AMM 25-66. (8561486)

Part: NONE — NONE · airframe 71,151 hrs · 26,622 cycles

SHIP 6704 FOUND R4 DOOR ESCAPE SLIDE BULGING. CORRECTIVE ACTION: REPL R4 DOOR SLIDE IAW W/C. (8561460)

Part: NONE — NONE · airframe 70,807 hrs · 26,439 cycles

SHIP 6704 GIRT BAR DISLODGED ON 4R DOOR. CORRECTIVE ACTION: INSTALLED SLIDE SAFETY PIN TO FOM. SECURED GIRT BAR AND REMOVED SAFETY PIN. VERIFIED PIN REMOVAL RII COMPLETED. (8396102)

Part: NONE — NONE · airframe 70,710 hrs · 26,394 cycles

SHIP 6704 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS DOOR 3L INOP. CORRECTIVE ACTION: FOUND DEBRIS BLOCKING GIRT BAR ON 4L DOOR. REMOVED DEBRIS CHECKS GOOD PER B757 AMM 52-11. (2043917)

Part: NONE — NONE · airframe 70,626 hrs · 26,350 cycles

SHIP 6704 3L DOOR SLIDE ARMED LIGHT INOP. DOOR OPERATING ARMING HANDLE BINDING. CORRECTIVE ACTION: OPS TESTED DOOR SLIDE ARM LIGHT. CHK OK PER B757-20 AMM 33-51. (7979422)

Part: INDICATOR — FAULTED (TE FLAPS) · airframe 70,421 hrs · 26,230 cycles

SHIP 6704 -MISC/DE- FLIGHT PERFORMED GO AROUND DUE TO FLAP INDICATION SPLIT AND NOT AT 20 ON FINAL. FLAPS DID REACH 20 AND FLIGHT LANDED SAFELY. FLIGHT OPS DECISION FOR DECLARED EMERGENCY. CORRECTIVE ACTION: T/S FLAP INDICATOR REPLACED, FWD TO MEL 27-08-02. (11/01 ATL) R/R FSEU-2 PER B757 AMM 27-51. NO BINDING OR FAULTS

Part: UNKNOWN — UNKNOWN · airframe 70,329 hrs · 26,183 cycles

'SUPPLEMENTAL INFORMATION' SHIP 6704 EXIT SIGN OVER 2L DOOR HAS FALLEN OFF. CORRECTIVE ACTION: REINSTALLED SAME. REMOVED AND REPLACED EXIT LIGHT COVER, LIGHT OPS CK NML B757 CMM 33-51. (1986693)

Part: UNKNOWN — UNKNOWN · airframe 70,329 hrs · 26,183 cycles

SHIP 6704 L1 DOOR GIRT BAR FOUND DETACHED AT DEPARTURE. CORRECTIVE ACTION: REINSTALLED L1 GIRT BAR PER AMDS TASK CARD 2566-9001-1L. OP CHECKED GOOD. VERIFIED INSTALLATION AND OPERATION OF L1 GIRT BAR. (7308578)

Part: GIRT BAR — UNSECURE (R3 DOOR) · airframe 70,174 hrs · 26,100 cycles

SHIP 6704 3R ENTRY DOOR WILL NOT CLOSE AND ARM PROPERLY. CORRECTIVE ACTION: RESECURED GIRT BAR PER B757 25-66 OPS NORMAL. (7365280)

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 69,840 hrs · 25,955 cycles

SHIP 6704 1L ENTRY DOOR SLIDE GIRT BAR COULD NOT ENGAGE/DISENGAGE. CORRECTIVE ACTION: AT GIRT BAR OUT OF POSITION. ADJUSTED GIRT BAR LATCHES PER B757 AMM 52-11. OPS NML. (7785652)

Part: GIRT BAR — FAILED (L1 DOOR) · airframe 69,727 hrs · 25,905 cycles

SHIP 6704 GIRT BAR ASSY LATCH SEPARATE ON LOWER FWD OF 1L DOOR. CORRECTIVE ACTION: FOUND GIRT BAR MOUNTING BRACKET LOOSE ON FWD SIDE OF L1 DOOR. SECURED SAME. (7424688)

Part: SLIDE — DETACHED (R4 DOOR) · airframe 69,526 hrs · 25,813 cycles

SHIP 6704 R4 DOOR SLIDE FELL ON GALLEY FLOOR. CORRECTIVE ACTION: PINNED R4 DOOR SLIDE. INSTALLED DOOR ESCAPE SLIDE PER JIC AND PIN REMOVED AND STOWED. (7424612)

Part: GIRT BAR — FAULTED (L1 DOOR SLIDE) · airframe 69,434 hrs · 25,778 cycles

SHIP 6704 AT DEPARTURE - L1 DOOR SLIDE WOULD NOT ENGAGE. CORRECTIVE ACTION: PINNED BOTTTLE AND SLIDE PER B757 AMM 25-66. FOUND GIRT INTERFERRING WITH SLIDE ENGAGEMENT. REMOVED AND REINSTALLED GIRT BAR ASSY PER 757 AMM 25-66. RII ACCOMPLISHED FOR SLIDE & DOOR BOTTLE PINS REMOVAL. DOOR AND SLIDE ARMING CHECKS GOOD. (7558560)

Part: GIRT BAR — PARTIAL DEPLOY (L1 DOOR) · airframe 69,424 hrs · 25,774 cycles

SHIP 6704 PARTIAL DEPLOYMENT OF GIRTBAR AT DOOR L1. CORRECTIVE ACTION: INSPECTED GIRT BAR PER 757AMM 25-66-10 UNHOOKED GIRTBAR FROM SLIDER AND REATTACHED DOOR OPERATES AND ARMS NORMAL. (7558554)

Part: GIRT BAR — MALFUNCTIONED (R3 DOOR) · airframe 69,397 hrs · 25,759 cycles

SHIP 6704 SLIDE LIGHT AT 3R DOOR WILL NOT ILLUMINATE WHEN DOOR IS ARMED. CORRECTIVE ACTION: RE-INSTALLED GIRT BAR SLIDE ARMS NML (7558544)

Part: LENS — UNSECURE (EMERGENCY SIGN) · airframe 69,193 hrs · 25,689 cycles

SHIP 6704 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:606. CORRECTIVE ACTION: SECURED LOOSE COVER. (1755197)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,882 hrs · 25,592 cycles

SHIP 6704 EMERGENCY SEAT LIGHTS AT ROW 18 ARE INOPERATIVE. CORRECTIVE ACTION: MAINTENANCE REPLACED MOUNTED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL (LP 7505036)

Part: SKIN — DENTED (BS 640-680) · airframe 76,344 hrs · 29,285 cycles

SHIP 6704 REF ERA 589617-14 FUSELAGE / SKIN / BS 640-680 / BETWEEN STRINGERS 21R-23R / DENTS. CORRECTIVE ACTION: REF ERA 589617-14. (1717885)

Part: PANEL — CRACKED (NR 7 SLAT TRACK) · airframe 68,862 hrs · 25,586 cycles

DURING INSPECTION MAINTENANCE FOUND RIGHT WING FIXED LEADING EDGE PANEL CRACKED BEHIND NR 7 SLAT INBOARD TRACK. REPAIRED PER SRM 51-70-08.

Part: SKIN — DENTED (FUSELAGE) · airframe 68,862 hrs · 25,586 cycles

DURING HEAVY MAINTENANCE CHECK MAINTENANCE FOUND 2 EACH DENTS AT FUSELAGE SKIN BETWEEN STA 640-680 BETWEEN STR 21R-23R. REPAIRED PER ERA 589617-14.

Part: PANEL — CRACKED (RT WING LE) · airframe 68,862 hrs · 25,586 cycles

DURING INSPECTION MAINTENANCE FOUND RT WING FIXED LEADING EDGE PANEL CRACKED BEHIND NR 7 SLAT OUTBOARD SLAT TRACK. REPLACED PER SRM 51-70-08.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,779 hrs · 25,561 cycles

DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY EXIT LIGHTS AT ROWS 1, 2, 3, L1, R1 AND OVERHEAD AT ENTRANCE TO FLIGHT DECK INOPERATIVE. THE M730 AND M731 BATTERY PACK WERE REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,866 hrs · 25,213 cycles

DURING INSPECTION, FOUND FWD EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,770 hrs · 25,158 cycles

EMERGENCY OVERHEAD LIGHTS AT 40 ABC, 45 FED ARE INOPERATIVE. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL. ORIGINAL WRITE UP ON LP 7144326 WAS MCO/PLAC FOR 40C AND 45D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,692 hrs · 25,134 cycles

EMERGENCY CEILING LIGHTS ABOVE 40C AND 45D ARE INOPERATIVE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,770 hrs · 25,158 cycles

EMERGENCY CEILING LIGHTS ABOVE 40C AND 45D ARE INOPERATIVE. REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: CONTACT — DIRTY (EXTERIOR LIGHT) · airframe 67,512 hrs · 25,045 cycles

(AIRCRAFT 6704, L/P 6963600) 4R EXTERIOR EMERGENCY LIGHT INOP. CORRECTIVE ACTION: CLEANED LIGHT ASSY CONTACTS. R4 EXTERIOR EMG LIGHT.

Part: LATCH — OUT OF ADJUST (L1 DOOR) · airframe 67,135 hrs · 24,935 cycles

SHIP 6704 L-1 DOOR HARD TO CLOSE. CORRECTIVE ACTION: ADJUSTED LWR LATCH CAM IAW B757 AMM 52-11. LUBRICATED PER B757 52-11. OPS CHECK GOOD. (6528562)

Part: FITTING — OUT OF ADJUST (R4 GIRT BAR) · airframe 67,098 hrs · 24,916 cycles

(AIRCRAFT 6704, L/P 1468165) 4R DOOR ARM/DISARM ISSUES. CORRECTIVE ACTION: FOUND GIRT BAR FLOOR FITTINGS OUT OF ADJ - ADJ SAME IAW B757 AMM 52-11.

Part: SLIDER — OUT OF POSITION (R4 DOOR) · airframe 67,098 hrs · 24,916 cycles

SHIP 6704 PRIOR TO DEPT 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND SLIDER OUT OF PLACE. CORRECTIVE ACTION: FOUND SLIDER REF. B757 AMM 25-66. DOOR SLIDE ARMS OK. (6528536)

Part: GIRT BAR — MALFUNCTIONED (R4 DOOR) · airframe 67,098 hrs · 24,916 cycles

(AIRCRAFT 6704, L/P 6528531) DOOR 4R GIRT BAR. CORRECTIVE ACTION: REMOVED 4R DOOR ESCAPE SLIDE AS PER B757 W/C 2566-9001-4R. INSP GIRT PUSH RODS AND ROLLER CAM. FOUND BELL CRANK ASSY BEND/DAMAGED. REMOVED BELL CRANK ASSY. REMOVED LOWER LINING DOOR 4R PER B757 AMM 52-11. RE-INSTALLED NEW BELLCRANK ASSY, ADJUSTED DOOR MECHANISM AND DOOR GIRT BAR MECHANISM REF B-757 AMM 52-11-25 AND 52-11-20. RE-INSTALLED ORIGINAL DOOR 4 RIGHT SLIDE REF JOB CARD 2566-9001-4R. OPERATED DOOR THROUGH FULL TRAVEL NO PROBLEMS NOTED. SLIDE ARMED AND DISARMED NORMAL.

Part: GIRT BAR — DISENGAGED (R3 DOOR SLIDE) · airframe 67,068 hrs · 24,903 cycles

ON ARRIVAL THE R3 DOOR SLIDE ASSEMBLY BECAME DISENGAGED FROM THE DOOR. SECURED GIRT BAR FOR 3R DOOR.

Part: SLIDER — MISSING (GIRT BAR) · airframe 67,051 hrs · 24,899 cycles

SHIP 6704 AFT RIGHT SERVICE DOOR FWD GIRTBAR SLIDER MISSING. DISARM AFT RIGHT SLIDE PER B757 25-66-10 . INSTALLED AFT RIGHT GIRT BAR SLIDER B757 25-66-10.REARMED RIGHT DOOR SLIDER PER AMM B757 25-66-10. A/C OK FOR SERVICE.

Part: SENSOR — INOPERATIVE (R4 GIRT BAR) · airframe 67,040 hrs · 24,896 cycles

AFT RIGHT SERVICE DOOR INOP WITH DOOR ARMED. CORRECTIVE ACTION: R/R 4R DOOR FWD GIRT BAR SENSOR PER AMM 25-66. DUE TO HISTORY R/R 4R DOOR GIRT BAR PER AMM 25-66. REMOVED AND STOWED SLIDE SAFETY PIN. RII C/W OF REMOVAL AND STOWING OF SLIDE SAFETY PIN.

Part: GIRT BAR — UNSECURE (R3 DOOR) · airframe 67,040 hrs · 24,896 cycles

FOUND GIRT BAR LOOSE AT THE R3 DOOR. SECURED THE GIRT BAR.

Part: SCREW — LOOSE (GIRT BAR FITTING) · airframe 67,040 hrs · 24,896 cycles

DUE TO HISTORY OF THE R4 DOOR GIRT BAR LOCK COMING OFF. REMOVED BUSSLE AND PINNED SLIDE. PERFORMED INSPECTION ON GIRT BAR, LEAF SPRINGS, AND GIRT BAR SLIDERS. CHECKED GOOD. FOUND SLIDERS CATCHING ON FLOOR FITTINGS. FLOOR FITTINGS SCREWS LOOSE. TIGHTENED IAW AMM 25-66. REMOVED AND STOWED SLIDE SAFETY PIN.

Part: FITTING — SEPARATED (GIRT BAR) · airframe 67,013 hrs · 24,889 cycles

4R GIRT BAR FOOT ON GROUND. CORRECTIVE ACTION: REINSTALLED FOOT.

Part: LANYARD — UNSECURE (R4 DOOR) · airframe 67,013 hrs · 24,889 cycles

UNABLE TO DISARM 4R DOOR. CORRECTIVE ACTION: FOUND LANDYARD FOR RAFT NEAR GIRT BAR RESECURED LANDYARD AND INSPECTED DOOR SLIDE PER B757 AMM 52-11.

Part: GIRT BAR — DAMAGED (R4 DOOR) · airframe 67,003 hrs · 24,887 cycles

ON WALKAROUND FOUND DOOR 4R GIRT BAR FOOT ON GROUND. CORRECTIVE ACTION: REINSTALLED FOOT. ARM/DISARM OPERATES NORMALLY.

Part: SLIDE — DETACHED (R4 DOOR) · airframe 66,978 hrs · 24,882 cycles

R4 DOOR SLIDE CAME OFF WHEN CATERING OPENED DOOR. REPLACED THE R4 DOOR SLIDE IAW JOB CARD 2566-9001-4R.

Part: DOOR — MALFUNCTIONED (R4) · airframe 66,833 hrs · 24,848 cycles

(AIRCRAFT 6704, L/P 6627260) R4 DOOR WILL NOT CLOSE. CORRECTIVE ACTION: CORRECTED PER AMDS WC 5211-9001-4R.

Part: DOOR — OUT OF ADJUST (L2) · airframe 66,668 hrs · 24,799 cycles

(AIRCRAFT 6704, L/P 6627213) L2 DOOR WON'T LATCH CLOSED. CORRECTIVE ACTION: REMOVED 2L SLIDE PACK, ADJUSTED 2L DOOR PER AMM 757- 52-11. INSTALLED 2L SLIDE PER AMDS 2566-9001-2L.

Part: HINGE — LOOSE (PAX DOOR) · airframe 67,098 hrs · 24,916 cycles

SHIP 6704 AFT LEFT ENTRY DOOR WOULD NOT OPEN. CORRECTIVE ACTION: FOUND LOWER HINGE HAD A POPPED RIVET, REMOVED COVER. REMOVED DAMAGED LOWER LUG. INSTALLED NEW 4L LOWER HINGE COVER ASSY PER B757 AMM 52-11 - ALL CKS GOOD. (6031729)

Part: PROXIMITY SENSOR — MALFUNCTIONED (PAX DOOR) · airframe 66,009 hrs · 24,510 cycles

ENTRY DOORS ADVISORY LIGHT & L AFT ENT DOOR ADVISORY MESSAGE DISPLAYED ON EICAS WITH LEFT AFT ENTRY DOOR CLOSED, LATCHED, AND ARMED FOR DEPARTURE. REPLACED THE L4 DOOR WARNING PROXIMITY SENSOR IAW AMM 52-71. TESTED GOOD.

Part: SENSOR — OUT OF ADJUST (ENTRY DOOR) · airframe 65,838 hrs · 24,444 cycles

(AIRCRAFT 6704, L/P 6137006) L AFT ENT DOOR EICAS ON GROUND. ADJUSTED AND CLEANED SENSOR PER AMM 52-71. CYCLED DOOR SEVERAL TIMES NO FAULTS. NO HISTORY.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 64,818 hrs · 24,064 cycles

SHIP 6704 -ATB- RETURNED TO ATL DUE TO LOSS OF THE NR 1 AND NR 2 AUTO PRESSURE CONTROLLERS. CORRECTIVE ACTION: BOTH CONTROLLERS FAULT AC MOTOR REPLACED OUTFLOW VLV. MTC FOUND UPPER PRESSURE RELIEF VLV TRIPPED, REPLACED SAME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,765 hrs · 24,041 cycles

SHIP 6704 ROW 33 SEAT EMER LIGHT INOP. CORRECTIVE ACTION: FOUND SEAT LIGHT ASSY OPEN. REMOVED/REPLACED LIGHT ASSY. (5442672)

Part: GUARD — DAMAGED (LIGHT SWITCH) · airframe 64,707 hrs · 24,010 cycles

(AIRCRAFT 6704, L/P 5442654) EMERGENCY LIGHT SWITCH GUARD ON OVERHEAD DAMAGED. REPLACED SWITCH GUARD. CHECKS GOOD. OK FOR SVC.

Part: WIRE — SHORTED (CABIN) · airframe 64,682 hrs · 24,000 cycles

(AIRCRAFT 6704, L/P 5442640) EMERGENCY LIGHTS ROW 33-37 INOP. FOUND EMERGENCY LIGHT WIRES SHORTED UNDER ROW 36 DEF. REPAIRED WIRING PER SWPM CH 20. REPLACED FUSES IN POWER SUPPLY M11648 PER AMM 33-51. ALL EMERGENCY LIGHTS. OP CK NML NOW.

Part: HANDLE — OUT OF SEQUENCE (R4 DOOR) · airframe 64,653 hrs · 23,987 cycles

(AIRCRAFT 6704, L/P 5442620) R4 DOOR WILL NOT CLOSE. FOUND OUTSIDE HANDLE OUT OF SEQUENCE. RESET DOOR OPENED AND CLOSED SEVERAL TIMES CKS GOOD INDICATION NORMAL.

Part: LANYARD — TANGLED (R3 GIRT BAR) · airframe 64,285 hrs · 23,834 cycles

3R DOOR SLIDE GIRT BAR TANGLED WITH ROPE DOOR WONT CLOSE. R/R 3R DOOR BUSTLE COVER AND PIN BOTTLE. REMOVED DEBRIS AND INSTALLED BUSTLE PER WORK CARD. (5020780)

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 63,914 hrs · 23,677 cycles

SHIP 6704 AFT LT DOOR LOWER EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REPAIRED WIRE FROM POWER SUPPLY TO LIGHT ASSY IAW B757 AWM 33-51 TEST OK. (5307730)

Part: SKIN — CRACKED (L4 DOOR) · airframe 63,635 hrs · 23,569 cycles

(AIRCRAFT 6704, L/P 0905560) DAMAGE T: DURING INSTALLATION OF L4 DOOR, CRACK ON INNER SKIN WAS FOUND (IN REF. CARD 5211-9001). (PTAS). SUMMARY OF NRC 00586: L4 DOOR INNER SKIN WAS REPAIRED PER ETI-57-19-006 REV: ORIGINAL AND ER/A: 574633-14 REV: ORIGINAL.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 63,632 hrs · 23,568 cycles

SHIP 6704 NDT FOUND DISBOND BETWEEN SKIN AND THE BEAR STRAP ON FWD/UPPER CORNER OF THE EDGE OF THE CUTOUT AT L1 DOOR. CORRECTIVE ACTION: NRC 00570-DISBONDED AREA BETWEEN SKIN AND THE BEAR STRAP ON FWD/UPPER CORNER OF THE EDGE OF THE CUTOUT AT L1 DOOR WAS REPAIRED PER SRM, ER/A 574459-14AD REV. ORIG SECTION I AND CARD

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 63,632 hrs · 23,568 cycles

SHIP 6704 CRACK ON FWD UPPER CORNER OF BEAR STRAP AT L1 DOOR (FUS). CORRECTIVE ACTION: NRC 00558 CRACK ON FWD UPPER CORNER OF BEAR STRAP AT L1 WAS REPAIRED PER ETI AND ER/A 574459-14AD REV. ORIG. (0902705)

Part: NUT — CORRODED (TE FLAP) · airframe 63,631 hrs · 23,567 cycles

SHIP 6704 INITIAL INSPECTION. CORROSION IN OUTBD BALLSCREW NUT OF INBD FLAP AT LT WING. CORRECTIVE ACTION: REF NRC 00446, OUTBOARD BALL SCREW OF INBD FLAP LT WING WAS REPLACED. (0893121)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,631 hrs · 23,567 cycles

SHIP 6704 CORROSION ON FITTING STA 1400 IN AFT CARGO DOOR CUT OUT LWR EDGE AT AFT CARGO COMP. CORRECTIVE ACTION: SUMMARY ON NRC 00280 CORROSION LEVEL 2: FITTING STA 1400 IN AFT CARGO DOOR CUT OUT LWR EDGE AT AFT CARGO COMP WAS REPLACED PER DWG. (0888508)

Part: DOOR TRACK — CONTAMINATED (R4 DOOR) · airframe 62,255 hrs · 23,023 cycles

CATERING DOOR R(4) DOOR HANDLE NO ROTATING, NOT ARMING. CLEARED DOOR TRACK, DOOR OPS CKS NML.

Part: LIGHT — MISSING (L1 DOOR SLIDE) · airframe 61,997 hrs · 22,945 cycles

L1 DOOR SLIDE INDICATOR LIGHT DAMAGED. LIGHT FELL OFF IN FLIGHT AND MISSING. INSTALLED THE LED LIGHT ASSY 2677-001.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,966 hrs · 22,934 cycles

1 SEAT MOUNTED EMER LIGHT INOP AT ROW 18D. REMOVED & REPLACED SEAT MOUNTED ASSY.

Part: FITTING — DETACHED (GIRT BAR) · airframe 61,445 hrs · 22,744 cycles

R3 DOOR SLIDE INDICATOR LIGHT INOPERATIVE OR DAMAGED. FOUND THE R3 FWD GIRT BAR SHOE DETACHED FROM THE BAR. PINNED SLIDE & DOOR ASSIST & REINSTALLED THE SHOE IAW MM 25-66.

Part: PLATE — MISSING (DOOR FRAME) · airframe 61,416 hrs · 22,732 cycles

L2 DOOR CUTOUT BEARING PLATE MISSING FROM FWD SIDE, THIRD FROM THE BOTTOM. INSTALLED THE BEARING PLATE IAW AMM 52-11.

Part: UNKNOWN — ODOR (CABIN) · airframe 61,389 hrs · 22,720 cycles

DIVERTED DUE TO BURNING PLASTIC ODOR IN THE CABIN WHICH DID NOT DISSIPATE. INSPECTED CEILING AND SIDEWALL LIGHTS, DROPPED PSI PANELS IN ODOR AREA. INSPECTED INSIDE OF PSU PANELS FOR DAMAGED WIRING OR DAMAGED PCB. RAN PED POWER ON EXTERNAL POWER AND ENGINES, RAN BOTH PACKS WITH APU AND ENGINES. INSPECTED LEFT AND RIGHT RECIRCULATION FANS. DROPPED CEILING PANELS AT ROW 19-21.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 60,173 hrs · 22,286 cycles

(AIRCRAFT 6704, L/P 0320392) SEAT ROW 43 R/H EMERGENCY LITES INOP. INSPECTED, RESECURED LOOSE CONNECTOR AT SEAT ROW 43 R/H EMERGENCY LITES. EMERGENCY LITES OP CHK NORMAL.

Part: NONE — NONE (MODIFICATION) · airframe 63,476 hrs · 23,496 cycles

SHIP 6704 WHILE IN FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING REV. C AT FS 620 BETWEEN STR 2R AND 3R, MTC FOUND SIX (6) EXISTING HOLES IN THE LOCATION WHERE THE TEE CLIP IS TO BE MOUNTED TO THE FRAME. ER/A 563725 AUTHORIZES MTC TO PLUG TWO (2) HOLES IN FS 620 AND TO UTILIZE THE EXTENDED BASE T-CLIP ON FS 620 TO PICK UP FOUR (4) EXISTING FASTENER HOLES AND CONTINUE THE RADOME INSTALLATION PER GOGO DRAWING REV. C. CORRECTIVE ACTION: REF ERA 563725-14AD REV A

Part: GIRT BAR — DETACHED (R3 DOOR) · airframe 58,608 hrs · 21,807 cycles

THE R3 DOOR WILL NOT ARM. FOUND THE GIRTBAR DETACHED ON ONE SIDE. ATTACHED AND OP CHECKED OK IAW AMM 52-11.

Part: GIRT BAR — DETACHED (R3 DOOR SLIDE) · airframe 58,103 hrs · 21,645 cycles

R3 DOOR DOES NOT ARM AND SLIDE LIGHT ISN'T ILLUMINATING. RT SIDE GIRT BAR APPEARS DISPLACED. REINSTALLED GIRT BAR IAW MM 52-11. SLIDE LIGHT OPERATES NORMAL.

Part: BRAKE ASSY — LEAKING (RT MLG) · airframe 58,062 hrs · 21,633 cycles

RT BRAKE IS SMOKING AFTER LANDING AND RT BRAKE READS NR 2234. FIRE DEPARTMENT REPORTED 300 F DEG AFTER BLOCK IN. FIRE DEPT REPORT HYD LEAK IN VICINITY OF BRAKE. FOUND NR 07 BRAKE LEAKING HYD FLUID. REPLACED BRAKE ASSY PER AMM 32-41- 10. OK FOR SERVICE.

Part: BUSTLE — UNSECURE (ZONE 800) · airframe 57,800 hrs · 21,548 cycles

RIGHT AFT DOOR WILL NOT ARM WHEN CLOSED. FOUND BUSTLE NOT SECURE ON AFT RT DOOR RESECURED BUSTLE A/C OK FOR SVC.

Part: FUSE — BLOWN (CABIN) · airframe 57,425 hrs · 21,422 cycles

EMERGENCY LIGHTS AT SEAT ROWS 33-37 INOP. REPLACED FUSES AT BP M11648 PER AMM 33-51. CKS OK.

Part: COVER — DETACHED (CABIN) · airframe 57,202 hrs · 21,347 cycles

DOOR 2R EMER EXIT LIGHT CAME OFF. REINSTALLED EXIT LIGHT COVER OK FOR SVC.

Part: SKIN — DENTED (L1 DOOR) · airframe 57,117 hrs · 21,323 cycles

L1 CABIN DOOR LOWER SKIN HAS PROTRUDING DENTS FROM INSIDE LOWER TORQUE TUBE BAY. FOUND OUT OF LIMITS IAW SRM 52-10-01. REMOVED DAMAGE AND FABRICATED A DOUBLER AND INSTALLED IAW PRI 553847-14 REV ORIGINAL.

Part: SKIN — DELAMINATED (LT WING LE) · airframe 57,098 hrs · 21,316 cycles

LEFT WING LEADING EDGE DELAMINATED APPROXIMATELY LWS 369 UPPER SURFACE. ACCOMPLISHED A COMPOSITE REPAIR IAW SRM.

Part: SKIN — CRACKED (LT WING LE) · airframe 57,098 hrs · 21,316 cycles

MULTIPLE CRACKS AT LEFT WING LEADING EDGE UPPER COMPOSITE SURFACE, BETWEEN LWS 397 AND 425. ACCOMPLISHED A COMPOSITE REPAIR IAW SRM.

Part: GIRT BAR — LOOSE (R3 DOOR) · airframe 56,353 hrs · 21,066 cycles

R3 DOOR WILL NOT ARM WITH SLIDE LIGHT ILLUMINATED. FOUND FWD GIRT BAR FOOT WAS LOOSE. SECURED GIRT BAR FOOT. DOOR CLOSES & ARM NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 52,673 hrs · 19,631 cycles

EMERGENCY EXIT LIGHT ABOVE R2 DOOR INOPERATIVE. TROUBLESHOT AND FOUND GROUND WIRE FOR THE R2 DOOR EMERGENCY EXIT LIGHT BROKEN. SPLICED WIRE W3632-0151-20, REF BSWPM 20-10-13 AND WDM 33-51-13, CRIMPER 13-1635, DUE 21APR16. OP/C CHECKS GOOD REF AMM 33-51-01-402-003.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,673 hrs · 19,631 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 38-42. TROUBLESHOT EMERGENCY LIGHTS AT SEAT ROWS 38-42 FOUND POWER SUPPLY M735 TO BE INOPERATIVE IN REF TO DWG 27751EM028 SH 5.04. R & R POWER SUPPLY AND BATTERY PACK M735 IN REF TO AMM 33-51-07-23, AMM 33-51-07-862 AND AMM 33-51-07-502. PERFORMED OPS TEST OF POWER SUPPLY AND BATTERY PACK IN REF TO 33-51-07. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 52,673 hrs · 19,631 cycles

L4 AND R4 DOOR EMERGENCY SLIDE LIGHTS ARE INOPERATIVE WHEN USING EMERGENCY LIGHT TEST SWITCH ON P62. PERFORMED TROUBLESHOOTING FOUND BROKEN WIRE W3054-004 AT PIN D ON CONNECTOR D40488 IN REF TO WDM 33-51-11, PG 3. REPINNED WIRE W3054-004 AT PIN D ON CONNECTOR D40488 IN REF TO WDM 33-51-11, PG 3 AND SWPM 20-61-19. PERFORMED OPS TEST OF EXTERIOR EMERGENCY LIGHTS USING P62 TEST SWITCH IN REF TO AMM 33-51-00-715-003, TEST CHECKED GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 52,609 hrs · 19,608 cycles

SEAT 23 D, E, F EMERGENCY LIGHT INOPERATIVE. R & R LIGHT PIGTAIL ASSY. OPS CHECKED GOOD.

Part: LOCK — MISSING (GIRT BAR) · airframe 52,539 hrs · 19,577 cycles

DOOR 4R GIRT BAR FELL OUT. FOUND FWD POSITION GIRT BAR LOCK MISSING AT 4R DOOR. INSPECTED SLIDE PACK AND GIRT BAR ASSY NO DAMAGE NOTED. INSTALLED SERVICEABLE GIRT BAR LOCK AT FWD POSITION. 4R DOOR SLIDE ARMING AND DISARMING OK IAW AMM 25-66-07.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 52,067 hrs · 19,410 cycles

MAINTENANCE FOUND SEAT 38 DEF, EMERGENCY ISLE LIGHT INOPERATIVE. TWO WIRES WERE SPLICED AT SEAT 38 DEF, OPS CHECKED GOOD.

Part: WINDOW — FAILED (COCKPIT) · airframe 51,680 hrs · 19,281 cycles

F/O WINDSHIELD SHATTERED WITH RT FWD WINDOW EICAS MESSAGE. R & R R1 WINDOW IAW AMM 56-11. ALSO CHANGED WINDOW HEAT CONTROL UNIT IAW AMM 30-41. ALL CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: SKIN — DENTED · airframe 50,723 hrs · 18,936 cycles

2 EACH DENTS WERE FOUND ON THE FUSELAGE SKIN LOWER FWD OF E/E DOOR ADJACENT TO AN EXISTING REPAIR DOUBLER AT STA 216, BETWEEN, LBL 0, LBL 14.10. FOUND TO BE OUT OF LIMITS IAW SRM. REF ERA 380375-14, REV C AND ERA 510981-14, REV ORIG.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 50,467 hrs · 18,846 cycles

RUST EMINATING FROM INBD FLAP INBD TORQUE TUBE AT CARRIAGE ATTACHMENT. CLEANED AREA AND CHECKED FOR CORROSION REF SRM. INSTALLED FLAP TRACK REF AMM 27-51, REF NR 62.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,476 hrs · 18,848 cycles

LBL 53.5 - 58.5 FLOOR PANEL DAMAGED. REPAIRED IAW ER/A 511568-14AD, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,847 hrs · 18,614 cycles

SKIN DENTED LT SIDE OF FUSELAGE, THREE INCHES FWD OF L2 DOOR. CUTOUT DAMAGE AREA, INSPECTED. FABRICATED REPAIR AND INSTALLED IAW SRM AND ER/A 527553-14, REV B.

Part: SKIN — DENTED (BS 600) · airframe 57,346 hrs · 21,395 cycles

FUSELAGE SKIN DENTED AT BS 600 AND STRINGER 16L REPAIRED IAW ER/A 527553-14 REV B.

Part: SKIN — DENTED (BS 600) · airframe 49,847 hrs · 18,614 cycles

FOUND A DENT AT BS 600, STR 16L FUSELAGE SKIN. REPAIRED IAW ERA 527553-14, REV B.

Part: SKIN — GOUGED (BS 620) · airframe 48,719 hrs · 18,219 cycles

SKIN GOUGED AT BS 620 BETWEEN S16-17L. REPAIRED IAW ERA516600-14, REV ORIG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,493 hrs · 17,753 cycles

EMERGENCY LIGHT BATTERY PACK M11648 FAILED TEST. REPLACED BATTERY PACK AND TESTED IAW CARD 3351-7004.

Part: SKIN — DAMAGED (LT WING) · airframe 45,481 hrs · 17,048 cycles

FUSELAGE DAMAGE TWO FT FWD OF LT WING LIGHT. CLEANED UP DAMAGE IAW SRM 53-00-01 CHART AREA B. REPAIR C/W ON N/R 001 AND ERA 55-516600-1.

Part: LATCH — OUT OF ADJUST (LIFE RAFT) · airframe 44,282 hrs · 16,590 cycles

UNABLE TO OPEN LIFT RAFT COMPARTMENT. ADJUSTED DOOR LATCH IAW AMM 25-22-03-424.

Part: STRINGER — CRACKED (BS 610 S16L) · airframe 44,282 hrs · 16,590 cycles

STRINGER CRACKED BS 610 S16L. ACCOMPLISHED REPAIR IAW SRM 53-00-03, FIG 201, REPAIR 1.

Part: DOOR — CHAFED (FWD CARGO) · airframe 44,281 hrs · 16,589 cycles

FWD CARGO DOOR UPPER AFT CORNER IS CHAFED ON INNER SURFACE. REPLACED CORNER IAW SRM 51-40-02, PG 31 AND 2.

Part: FLOORBEAM — CORRODED (BS 1660 LBL 50) · airframe 44,281 hrs · 16,589 cycles

AFT PAX CABIN FLOORBEAM HAS CORROSION STA 1660, LBL 50 NEAR FASTENER HOLE. REPAIRED IAW ERA 481634-14MA, REV A.

Part: GATE — CORRODED (R4 DOOR LOWER) · airframe 44,281 hrs · 16,589 cycles

R4 DOOR LOWER GATE BOTTOM EDGE HAS PITTING. REPLACED GATE IAW MM 52-11-02-404-004.

Part: GATE — CORRODED (L4 DOOR LOWER) · airframe 44,281 hrs · 16,589 cycles

L4 DOOR LOWER GATE BOTTOM EDGE HAS PITTING. REPLACED GATE IAW AMM 52-11-38-404-009.

Part: DECK PLATE — CORRODED (BS 1640-1700) · airframe 44,281 hrs · 16,589 cycles

AFT PAX CABIN DECK PLATE HAS CORROSION BS 1640-1700, RBL 7, RBL 12. R & R REPAIR IAW SRM 53-60-51, FIG 201.

Part: DECK PLATE — CORRODED (BS 1700 LBL 50) · airframe 44,281 hrs · 16,589 cycles

AFT PAX CABIN DECK PLATE HAS CORROSION STA 1700, LBL 50. REPAIRED IAW SRM 53-60-51, FIG 201.

Part: DECK PLATE — CORRODED (BS 1710 RBL 56) · airframe 44,281 hrs · 16,589 cycles

AFT PAX CABIN DECK PLATE HAS CORROSION STA 1710 RBL 56. FOUND WITHIN LIMITS IAW SRM 53-60-51.

Part: STRAP — CORRODED (BS 1680-1684) · airframe 44,281 hrs · 16,589 cycles

AFT PAX CABIN DECK PLATE STRAP CORRODED BS 1680-1684 LBL3 RBL 3. REMOVED CORROSION AND REPLACED AFT PAX CABIN DOOR PLATE STRAP IAW SRM 51-40-02.

Part: GATE — CORRODED (R1 DOOR LOWER) · airframe 44,281 hrs · 16,589 cycles

R-1 DOOR LOWER GATE 2 BOTTOM EDGES HAVE PITTING THROUGHOUT, REPLACED GATE IAW SRM 51-40-02, PG 21, FIG 4.

Part: GATE — CORRODED (L1 DOOR LOWER) · airframe 44,281 hrs · 16,589 cycles

L-1 DOOR LOWER GATE BOTTOM EDGE HAS PITTING AND INSIDE POCKET FOUND CORRODED. REPLACED GATE IAW AMM 52-11-38-404-009.

Part: DECK PLATE — CORRODED (BS 1710-1718) · airframe 44,281 hrs · 16,589 cycles

AFT PASSENGER CABIN DECK PLATE HAS CORROSION STAT 1710-1718 RBL 56- LBL 58.27 REPAIRED AREA IAW SRM 53-60-51, FIG 201, REPAIR 2.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 44,281 hrs · 16,589 cycles

AFT CARGO DOOR EXTERIOR SKIN DENTED AT FWD LOWER CORNER. ACCOMPLISHED REPAIR IAW REPAIR 4 FIG 201.

Part: FITTING — CORRODED (BS 321 RBL 3) · airframe 44,281 hrs · 16,589 cycles

MAIN CABIN FLOOR STRUCTURE MOUNT FITTING HAS CORROSION AT BS 321, RBL 3. REPLACED FITTING IAW SRM 51-40-02.

Part: GATE — CORRODED (R2 DOOR) · airframe 44,281 hrs · 16,589 cycles

R2 LOWER DOOR DATE BOTTOM EDGE HAS PITTING CORROSION. PART REPLACED IAW 52-11-38004-001.

Part: FRAME — DENTED (BS 600 S24-25L) · airframe 44,281 hrs · 16,589 cycles

FRAME DENTED AT BS 600. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5 TO 108/100.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 37,055 hrs · 13,897 cycles

ON 11/09/10 DURING A LIGHTNING STRIKE INSPECTION, A FASTENER HOLE WAS MISDRILLED AT BS 778, STR 16L. REMOVED DAMAGE AND INSTALLED A PERMANENT REPAIR PER ER/A 487276-14. (DL757103074)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 35,668 hrs · 13,445 cycles

DURING LAYOVER CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHT AT ROW 5C INOPERATIVE. MAINTENANCE REPAIRED THE CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: ENTERTAIN SYS — ODOR (CABIN) · airframe 35,239 hrs · 13,315 cycles

DURING FLIGHT, F/A DISCOVERED A BURNING ODOR AROUND ROW 32. IFE SYS WAS TURNED OFF. ODOR THEN DISSIPATED. MX CHECKED AND OPERATED ENTIRE IFE SYS AND ALL WAS NORMAL.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 13,316 hrs · 6,010 cycles

ON LAYOVER FOUND EMERENGCY EXIT LIGHTS AT FWD RT OVERWING EXIT, OVERHEAD LIGHT AT 20DEF-26ABC-33ABC INOPERATIVE. FOUND BULB SHORTED AT 20DEF AND REPLACED FUSE IN AFT GALLEY BATTERY PACK

Part: SKIN — DENTED (FUSELAGE) · airframe 12,191 hrs · 5,577 cycles

THE FUSELAGE SKIN WAS FOUND WITH 2 DENTS. ONE DENT WAS LOCATED JUST ABOVE THE S-17L CREASE AT STRINGER 16L & FS 600. THE OTHER DENT WAS BELOW THE S-17L CREASE AT FS 620. THE DENTS WERE REMOVED WITH 4 INCH CUTOUTS AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS. THE REPAIRS WERE ACCOMPLISHED PER ER/A 088228-14, REV B AND ER/A 088229-14, REV B.

Part: WEDGE — DENTED (NR 2 SLAT) · airframe 12,191 hrs · 5,577 cycles

FOUND ON PSV - 3 DENT ON NUMBER 2 SLAT WEDGE 48 INCHES FROM INBOARD EDGE. REPAIRED PER SRM 57-43-02D AND OPERATION 1000.

Part: PIN — BROKEN (POWER SUPPLY) · airframe 11,926 hrs · 5,479 cycles

ON L/O, FOUND EMERGENCY EXIT LIGHT ABOVE EMERGENCY EXIT DOOR AT 16A INOP. FOUND PIN BROKEN ON POWER SUPPLY. REMOVED AND REPLACED SAME, OPS OK.

Part: ODOR — DETECTED (CABIN) · airframe 7,224 hrs · 3,399 cycles

F/A, PASS, AND F/O OBSERVED ODOR OF BURNT POPCORN ON RT SIDE OF AIRCRAFT BETWEEN ROWS 31 AND 34. ODOR BEGAN AT 35,000FT AND RETURNED 2 TIMES DURING FLIGHT. ODOR DISSIPATED AFTER 10 MINUTES. NO ABNORMALITIES W/PES OR PACKS. DURING T/S ALL LAV HOT WATER HEATERS TURNED OFF. TURNED ON LAV WTR HTRS. INSPT ROW 31-34 DEF PSUS. CHECKS OK. REMOVED CEILING PANELS OVER 31-34 DEF NO PROBLEMS NOTED. CHECKED SEAT HARNESS AND SEBS CHECKED ALL READING AND ATTENDANT LIGHTS IN AREA. NO SMELL OR DEFECTS NOTED.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 6,921 hrs · 3,240 cycles

PILOT REPORT - L HYD QTY MSG ILLUMINATED. REPLACED DAMAGED O-RING ON S27 PRESS SW LT PYLON LEAK CK OK. SERVICED HYD FLUID TO FULL.

Part: O-RING — CUT (NR 1 ENGINE) · airframe 6,354 hrs · 2,942 cycles

LEFT ENGINE LOW PRESS LIGHT ILLUM, LT ENG OIL QTY AT ZERO, PRESS STARTED TO DECREASE AND ENG SHUTDOWN ONCE OIL PRESS IN THE RED. MTC IN PROGRESS, NO DETAILS AS YET AS TO SOURCE OF OIL LOSS. MTC FOUND O-RING CUT ON MAIN OIL FILTER HOUSING. REPLACED SAME. ALSO OIL LINE WAS LEAKING AT FUEL/OIL HEAT EXCHANGER. TIGHTENED LINE.

Part: SKIN — DENTED (FUSELAGE) · airframe 3,311 hrs · 1,527 cycles

THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED IN SEVERAL AREAS BETWEEN FS 200 & 231 AND BETWEEN STRINGER 26R AND BL0.THE DAMAGE WAS REMOVED WITH AN 8.5 INCHES X 8.5 INCHES CUTOUT AND A 10.5 INCHES X 13.75 INCHES CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 380375 -14, REV A.

Part: INVERTER — ODOR (CABIN) · airframe 3,258 hrs · 1,501 cycles

ON INITIAL DESCENT STBY INVERTER STATUS MESSAGE APPEARED FOLLOWED BY FAINT ODOR THROUGHOUT CABIN. C/A REPLACED STATIC INVERTER

Part: SOCKET — FAILED (INDICATOR LIGHT) · airframe 2,253 hrs · 1,048 cycles

NOSE GEAR INDICATION DID NOT SHOW DOWN AND LOCKED ON GEAR EXTENSION. JACKING ACFT TO SWING GEAR. C/W NOSE GEAR RETRACTION AND EXTENTION, ADJ AND TEST PER M/M AND RAN BITE ON PSEU BOX. NO TROUBLE FOUND. NOSE GEAR GREEN LIGHT SOCKET FOUND NOT TO BE FULLY SEATED. RESEATED LIGHT SOCKET, OPS CHECKED OK.

Part: B-NUT — LOOSE (RT WHEEL WELL) · airframe 117 hrs · 53 cycles

AFTER T/O CABIN AND FLIGHT CREW SMELLED BURNING ELECTRIC ACRID ODOR. PAX COMPLAINED OF BURNING EYES. RETURNED TO CVG. FOUND HYD LEAK IN RIGHT W/W. TIGHTEN B- NUT ON LINE FROM HYD FILTER RETURN LINE.