N707TW

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 104,137 hrs · 27,269 cycles

ON SVC CHK FOUND L3 DOOR SIDEWALL EXIT EMERGENCY LIGHT INOP. R & R L3 SIDEWALL EXIT LIGHT ASSY REF AMM 33-51. OPS CHK GOOD. (7689624)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 103,578 hrs · 27,136 cycles

SEAT ROW 26 DEF UNDER BIN EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY M10699 IAW AMM 33-51. EMERGENCY LIGHTS OPS NORMAL. (7956820)

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 103,488 hrs · 27,118 cycles

SHIP 6805 WHITE EMERGENCY LIGHTS IN SEATS 1-4 INOP. CORRECTIVE ACTION: T/S PER B757 WDM 33-52-12. FOUND P2 CONNECTOR UNDER ROW 2 DISCONNECTED. SWAPPED PICO FUSE (F1) ON BATTERY CHARGER ASSY. M731. OPS CHK OK. (7956812)

Part: SKIN — CORRODED (ZONE 200) · airframe 101,321 hrs · 26,582 cycles

FOUND BULGE ON SKIN AT STA 420 13L TO 14L. CORRECTIVE ACTION:THE EVALUATION OF BULGE AT ST 420 STR 13L TO 14L FOUD IT TO BE OUT OF LIMITS IAW B757-200 SRM 53-00-01 DETAIL III. DAMAGE WAS REMOVED AND REPAIRED IAW ER/A 625043-14.

Part: SKIN — CHAFED (ZONE 200) · airframe 101,321 hrs · 26,582 cycles

SHIP 6805 DTE, ERA 625043-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE SKIN AT STA 420-440 & S-14/15L. CORRECTIVE ACTION: REF ERA 625043-14. (0873043)

Part: SNUBBER — OUT OF TOLERANCE (ZONE 800) · airframe 101,321 hrs · 26,582 cycles

SHIP 6805 R1 DOOR ROTARY SNUBBER COMPENSATOR INDICATOR PIN IS BELOW MINIMUM EXTENSION FOR AMBIENT TEMPERATURE. (BELOW FLUSH). CORRECTIVE ACTION: REMOVED AND REPLACED R1 BOAR TORQUE TUBE ROTARY SNUBBER IAW B757 AMM 52-11. (0862842)

Part: TRIGGER — OUT OF ADJUST (ZONE 800) · airframe 101,321 hrs · 26,582 cycles

AIRCRAFT 6805, AFTER CABLE OPS CHECK ON DOOR 4L, EMERGENCY SYSTEM ON UPPER HINGE ASSEMBLY DOES NOT DISENGAGE/DISARM. CORRECTIVE ACTION: ADJUSTED L-4 DOES EMERGENCY POWER TRIGGER IAW B757 AMM 52-11-32. OPS CHECK GOOD. (LP 0855878)

Part: STOP FITTING — CRACKED (ZONE 900) · corrosion level 2 · airframe 101,321 hrs · 26,582 cycles

AIRCRAFT 6805, UPPER CABIN BETWEEN STA-1680 TO 1710, RBL 24.75, GALLEY G4 PARTITION STOP FITTING IS CRACKED/CORRODE. CORRECTIVE ACTION: REPLACED GALLEY G4 PARTITION STOP FITTING AT STA 1680-1710 RBL 24.75 IAW B757-200 SRM 51-40-02. (LP 0856394)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 100,846 hrs · 26,406 cycles

SHIP 6805 18DE EMER EXIT LIGHT BATTERY PACK INOP. CORRECTIVE ACTION: R/R ROW 18 EMR EXIT BATTERY PACK PER B757 AMM 33-55. (6361085)

Part: ARMING LEVER — LOOSE (R1 DOOR) · airframe 100,679 hrs · 26,362 cycles

SHIP 6805 R-1 ENTRY DOOR GREEN ARMED LEVER LOOSE. CORRECTIVE ACTION: R/R DOOR ARM IND. SPRING REF B757 IPC 25-11-02-05 CKS GOOD. (6361033)

Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 100,679 hrs · 26,362 cycles

SHIP 6805 L-2 ENTRY DOOR KNUCKLE KNOCKER WILL NOT EXTEND. CORRECTIVE ACTION: FOUND CONDITION INDICATOR PLACARD INTERFERING WITH INDICATOR MOVEMENT. R/R INDICATOR PLACARD, CKS GOOD REF B757 AMM 52-11. (6361032)

Part: TRANSMITTER — FAULTED (RT WING TE FLAP) · airframe 98,763 hrs · 25,888 cycles

SHIP 6805 -DE/FCNT- DUE TO TRAILING EDGE FLAP ASYMMETRY. CORRECTIVE ACTION: REPLACED RIGHT FLAP POSITION TRANSMITTER. (5763374)

Part: D-RING — OUT OF POSITION (SURVIVAL PACK) · airframe 98,241 hrs · 25,776 cycles

SHIP 6805 SURVIVAL PACK D RING CONNECTION NOT IN PROPER PLACE IS LAYING ON THE FLOOR. CORRECTIVE ACTION: RESECURED SURVIVAL PACK D RING PER B757 AMM 25-66. (0295368)

Part: SENSOR — DIRTY (L2 DOOR) · airframe 98,022 hrs · 25,724 cycles

SHIP 6805 DOOR 2L INITIALLY SHOWED AS ARMED DURING TAXI SLIDE LIGHT WENT OUT AND KNUCKLE KNOCKER NOT EXTENDED. CORRECTIVE ACTION: CLEARED DEBRIS FROM SENSOR. PER B757 M/M 52-71 OPS CHK NML. ALL INDICATIONS PRESENT. (5777612)

Part: DOOR — FOD (L1) · airframe 97,803 hrs · 25,671 cycles

SHIP 6805 1L DOOR JAMMED ON ARRIVAL, COULD NOT MOVE LEVER TO OPEN. CORRECTIVE ACTION: REMOVED DEBRIS FROM 1L DOOR. NO FURTHER ISSUES NOTED A/C OK FOR SERVICE. (5291322)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 97,706 hrs · 25,651 cycles

SHIP 6805 DURING GOGO DEMOD FORWARD CROWN AREA FOUND ERA STICKER # 590389- 14 HOLE SIZE .305 . CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 005-0001:2330-01322- 21D/001 00004 ACCOMPLISHED ER/A 590389-14 REV B. (0216355)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,855 hrs · 25,450 cycles

SHIP 6805 LEFT DOOR ESCAPE SLIDE INOP. CORRECTIVE ACTION: DEPLOYED SLIDE PER CARD AND LIGHTS DID NOT COME ON. BATTERY IS GOOD, DID NOT DETACH TO OPERATE LIGHTS CORRECTLY. (5510338)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,003 hrs · 25,251 cycles

SHIP 6805 AFT LEFT DOOR WONT ARM. CORRECTIVE ACTION: FOUND DEBRIS IN GRIT BAR TRACK REMOVED DEBRIS, ARMED DOOR. ALL OPS NML PER B757 AMM 52-11. (4625066)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,905 hrs · 25,231 cycles

SHIP 6805 1 RIGHT BOARDING DOOR WON'T ARM PROPERLY AND ARMED LIGHT WON'T ILLUMINATE. CORRECTIVE ACTION: CYCLED R1 DOOR SLIDE ARMING LEVER SEVERAL TIMES. OPS CK NORMAL. OK FOR SVC. (4625040)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,825 hrs · 25,214 cycles

SHIP 6805 -DIV/DE- DIVERTED TO IAD DUE TO LEFT ENGINE SURGE. ENGINE AT IDLE ON LANDING. METAL FOUND IN TAIL PIPE. CORRECTIVE ACTION: R/R NUMBER 1 ENGINE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,814 hrs · 25,211 cycles

SHIP 6805 AFT RIGHT CABIN SEAT EMERG LIGHTS WEAK. CORRECTIVE ACTION: REPLACED M734 BP PER B757AMM 33-51. OP CHECK GOOD. (4625010)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,704 hrs · 25,188 cycles

SHIP 6805 HISTORY FOR R1 DOOR HARD TO, OR WILL NOT ARM. CORRECTIVE ACTION: REMOVED AND REPLACED BOTH BAR LOCKS AT 1R DOOR. OPS CHK NML. LUBED 1R DOOR GIRT BAR PER B757 AMM 52-10. (2920149)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,704 hrs · 25,188 cycles

SHIP 6805 SHIP DOOR 1R WOULD NOT ARM. CORRECTIVE ACTION: REMOVED DEBRI FROM GIRT BAR AREA. CYCLED DOOR. OPS NML PER B757 AMM 52-11. (4634780)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,704 hrs · 25,188 cycles

SHIP 6805 DOOR 1R HARD TO ARM. CORRECTIVE ACTION: REMOVED FOD FROM DOOR GIRT BAR. ALL OPS NRML. A/C OK FOR SVC AND SECURED DOOR COVER LANYARD. ALL OPS NRML PER B757-200 AMM 52-12. (4634782)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,679 hrs · 25,182 cycles

SHIP 6805 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: STOWED LANYARD AND CLEANED DEBRIS. 1R DOOR ARMS PER B757 AMM 25- 61. (4634776)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,679 hrs · 25,182 cycles

SHIP 6805 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR PER B757 AMM 52-11. 1R DOOR ARMS NORMALLY. (4634774)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,475 hrs · 25,139 cycles

AIRCRAFT 6805, PAX AT 1D REPORTED SEEING SPARK. CORRECTIVE ACTION: FOUND HARNESS FSW5308-145 UNDER SEAT 1D DAMAGED AND 3 WIRES CUT AND BURNED. REPAIRED WIRE HARNESS PER SWPM 20-10-13. ALL SEATS OPS CHECK NML. (LP 4829882)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,274 hrs · 25,098 cycles

SHIP 6805 DURING PERFORMANCE OF WORK CARD 3351-7001 FOUND ALL EXTERIOR LIGHTS WOULD NOT TURN ON AT THE NOSE GEAR P62 TEST SWITCH. CORRECTIVE ACTION: REMOVED AND REPLACED SWITCH S10035 ON THE P62 PANEL PER B757 WDM 33-51 & B757 AIPC 33-51. REPLACED TERMINAL FOR GROUND WIRE AT G29-DC PER B757 WDM 33-51. OPS CHECK GOOD. (4829834)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,146 hrs · 25,064 cycles

SHIP 6805 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND GRID BAR LINER LOOSE. REPACKED OPS CK NML PER B757 AMM 52 -12. (4837594)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,146 hrs · 25,064 cycles

SHIP 6805 DIRTY SOCK FUME SMELL PASSING THRU 2K IN THE FLIGHT DECK. CORRECTIVE ACTION: PERFROMED GVI OF ENGINE IAW B757 FIM 21-00 TASK 301. FOUND EVIDENCE LEAKAGE AROUND 10 HEAT EXCHANGER. CLEANED OIL. R/R RECIRC FILTERS PER AMM 21-58. PERFORMED NBR 2 ENG WATER WAS PER AMDS JOB CARD. (4837584)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,072 hrs · 25,045 cycles

SHIP 6805 1R DOOR WILL NOT ARM. ARMING LVR IS JAMMED. CORRECTIVE ACTION: FOUND MANUAL RELEASE STRAP STUCK BETWEEN GIRT BAR AND FRAME. STRAP RELEASED AND STOWED TO CORRECT POSITION. (4837558)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,059 hrs · 25,042 cycles

SHIP 6805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 1R. CORRECTIVE ACTION: REMOVED DEBRIS AT 1R. OPS NML. (2824904)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,957 hrs · 25,018 cycles

SHIP 6805 1R DOOR GIRT BAR ENGAGEMENT LIGHT ISSUES. CORRECTIVE ACTION: PERFORMED AMM TASK 25-66-11-201-822. CHECKED GOOD. R+R LED CAP ASSY PER B757 AMM 33-51. CHECKS GOOD. (2803612)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,878 hrs · 25,001 cycles

SHIP 6805 FLT CREW REPORTS 1R DOOR ARMED LIGHT INOP. CORRECTIVE ACTION: REMOVED DEBRIS AND RELUBED GIRT BAR PER JIC 5211-2301. OPERATIONAL CHECK NORMAL. (4837516)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,819 hrs · 24,990 cycles

SHIP 6805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:01R. CORRECTIVE ACTION: CLEAR DEBRIS ON 1R DOOR, SLIDE LIGHT INDICATOR OPS NORMAL. (2790350)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,663 hrs · 24,952 cycles

SHIP 6805 EXIT LIGHT COVER ON 2R EXIT DOOR FELL OFF AND COULDNT BE RE-ATTACHED. CORRECTIVE ACTION: REATTACHED EXIT LIGHT COVER @ 2R EXIT DOOR. (4802832)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,223 hrs · 24,854 cycles

SHIP 6805 AWR IN REF TO ER/A 600262-14 REV. ORIGINAL, SECTION.III: PERMANENT REPAIR, STEP 1: SUNKED FASTENERS (10EAS) AND CORROSION ON FASTENER (1EA) WERE FOUND ON SURROUNDING STRUCTURE AT AFT STRUT FAIRING RH. CORRECTIVE ACTION: SUMMARY OF NRC 00179 FASTENERS ON SURROUND STRUCTURE AT AFT STRUT FAIRING RH WERE REPLACED PER PRI NO.607761-14, REV.0. AND ER/A NO.607761-14, REVISION ORIGINAL, SECTION I TEMPORARY REPAIR. (2709444)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,411 hrs · 24,896 cycles

SHIP 6805 ER/A 607761-14; PYLON #2 / AFT STRUT FAIRING / SKIN, INBD & OUTBD SIDE / NAC STA. 274 TO 279 / FASTENER CORROSION. CORRECTIVE ACTION: REF ERA 607761-14. (2708770)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,221 hrs · 24,853 cycles

SHIP 6805 AD - AA DAMAGES WERE FOUND ON HOLES AT RH ENG DRAG FTG CLAMP-UP AS FOLLOW: HOLE #12 CORROSION ON SKIN BETWEEN 9 TO 4 CLOCK POSITION, SCRATCHES ON SKIN AND FITTING ALL AROUND, HOLE #14 CORROSION ON SKIN BETWEEN 12 TO 4 CLOCK POSITION, SCRATCHES ON SKIN AND FITTING ALL AROUND, HOLE #15 SCRATCHES ON SKIN AND FITTING ALL AROUND, HOLE #16 CORROSION ON FITTING AT 5 CLOCK POSITION, SCRATCHES ON SKIN AND FITTING ALL AROUND, HOLE #17 SCRATCHES ON SKIN AND FITTING AT 12 AND 6 CLOCK POSITIONS IN REFERENCE TO JOB 022-0001 / CARD 5720-01100-05B. CORRECTIVE ACTION: SUMMARY OF NRC 00157: HOLES #12, 14, 15, 16 & 17 WERE REPAIRED PER CARD 5720-01100-05B, PRI 590487-14 REV. 1 AND ER/A 590487- 14AD REV A SECTION VI PERMANEN REPAIR. (2707416)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,221 hrs · 24,853 cycles

SHIP 6805 AD - AA DAMAGES WERE FOUND ON HOLES AT RH ENG DRAG FTG CLAMP-UP AS FOLLOW: HOLE #6 CORROSION ON FITTING AT 6 CLOCK POSITION, SCRATCHES ON SKIN BETWEEN 6 TO 8 CLOCK POSITION, HOLE #8 SCRATCHES ON SKIN AND FITTING BETWEEN 5 TO 9 AND AT 9 CLOCK POITIONS, HOLE #10 SCRATCHES ON SKIN AND FITTING BETWEEN 1 TO 6 CLOCK POSITION IN REFERENCE TO JOB 156-0001 / CARD 5720-01100. CORRECTIVE ACTION: SUMMARY OF NRC 00155: HOLES #6, #8 AND #10 WERE REPAIRED PER PRI 590487-14 REV. 1 AND ER/A 590487-14AD REV A SECTION VI PERMANENT REPAIR. (2707433)

Part: UNKNOWN — UNKNOWN · airframe 93,924 hrs · 24,780 cycles

SHIP 6805 EMERGENCY LIGHTS INOP ON SEAT ROWS 2,3,4. CORRECTIVE ACTION: INSPECTED AND FOUND LOOSE CONNECTOR @ 2C RECONNECTED EMERGENCY LIGHTS WORK. (9901369)

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 93,806 hrs · 24,750 cycles

SHIP 6805 EXIT SIGNS AT 1L AND 3R HAVE AN ARROW. CORRECTIVE ACTION: REPLACED LIGHTS WITH PROPER LIGHT LENS WITH NO ARROW PER B757 IPC 33-50-02-33. REPLACED PER B757 AMM 33-51. (9901321)

Part: LIGHT — NOT SEATED (L2 DOOR SLIDE) · airframe 93,799 hrs · 24,748 cycles

SHIP 6805 DOOR 2L SLIDE LIGHT ARMED DOES NOT ILLUMINATE. CORRECTIVE ACTION: FOUND 2L DOOR SLIDE ARMED LIGHT ASSEMBLY NOT LOCKED INTO RECEPITCLE. RESEATED LIGHT ASSEMBLY REF B757 WDM 25-66-11. (9901300)

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 93,442 hrs · 24,665 cycles

R1 DOOR ARM LIGHT DID NOT EXTINGUISH WHEN DISARMED. CLEANED & OPERATED GIRT BAR MECHANISM IAW AMM 52-11. OPS CHECKED NORMAL.

Part: NONE — NONE · airframe 92,730 hrs · 24,506 cycles

SHIP 6805 SLIDE LIGHT AT DOOR 1R WHEN DISARMED. CORRECTIVE ACTION: PERFORMED CHECK OF 1R DOOR GIRT DOOR ENGAGEMENT/DISENGAGEMENT REF B757 AMM 25-66. 1R SLIDE LIGHT OPS NORMAL. (8582798)

Part: NONE — NONE · airframe 92,025 hrs · 24,342 cycles

SHIP 6805 UNABLE TO ARM 1R DOOR. CORRECTIVE ACTION: SECURED SAFETY LANYARD CKS OK. (9249794)

Part: NONE — NONE · airframe 90,269 hrs · 23,922 cycles

SHIP 6805 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:604. CORRECTIVE ACTION: RESECURED LENS COVER AT R2 DOOR. (2061173)

Part: DUCT — DISCONNECTED (MAIN SUPPLY) · airframe 90,233 hrs · 23,915 cycles

SHIP 6805 CREW REPORTS: APPROX 4 HOURS AFTER T/O, FLT ATTS NOTICED (AND PAX TOO) INVISIBLE FUMES THAT BOTHERED THE SENSES OF EYES AND SMELL. CAPTAIN INVESTIGATED AND FOUND AREA NEAR ROW 25 +- 3 ROWS AND FELT WARM. SHUT DOWN IFE GALLEY POWER AND LIGHTS. CAPT CONFIRMED THIS ALLEVIATED PROBLEMS. GALLEY POWER RESTORED. CORRECTIVE ACTION: NO GO ODI CHECKLIST COMPLETE. FOUND TWO RISER DUCTS DISCONNECTED FROM MAIN SUPPLY AT ROW 25. REPAIRED PER AMM 21-23. NO MORE FUMES PRESENT. (8305422)

Part: NONE — NONE · airframe 90,187 hrs · 23,903 cycles

SHIP 6805 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 2L. CORRECTIVE ACTION: SECURED SIGN HARDWARE AND SIGN. (2052939)

Part: NONE — NONE · airframe 89,329 hrs · 23,719 cycles

SHIP 6805 -IFSD- RT OIL FILTER EICAS MSG, QRH PROCEDURES FOLLOWED AND ENGINE SHUTDOWN. CORRECTIVE ACTION: FOUND MAIN OIL FILTER CONTAMINATED WITH METAL. METAL SAMPLES COLLECTED FOR ANALYSIS. REMOVED AND REPLACED ENGINE.

Part: PROXIMITY SWITCH — DIRTY (R1 DOOR) · airframe 89,182 hrs · 23,689 cycles

SHIP 6805 R1 DOOR SLIDE ARMED LIGHT ON ALL THE TIME. CORRECTIVE ACTION: INSPECTED BOTH PROX SWITCHES 1 AND 3 AND FOUND NO DAMAGE TO VISIBLE PORTION OF WIRES AND HARDWARE. REMOVED AND CLEAN DEBRIS FROM PROX SWITCHES 1 AND 2 THEN PERFORMED OPS CHECKS PER B757 AMM 25-66 GOOD. (7634773)

Part: SLIDE — OUT OF ADJUST (L4 DOOR) · airframe 89,156 hrs · 23,684 cycles

SHIP 6805 L4 DOOR SLIDE W/N ARM. CORRECTIVE ACTION: ALIGNED PACKBOARD PER B757 AMM 52-02 DOOR + SLIDE NML. (7634744)

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 89,069 hrs · 23,667 cycles

SHIP 6805 AFTER BLOCK-IN WHEN THE 1R DOOR WAS DIS-ARMED, THE SLIDE LIGHT REMAINED ILLUMINATED. CORRECTIVE ACTION: REMOVED DEBRIS FROM 1R DOOR GIRT BAR SWITCH S10217. SLIDE LIGHT OPS CHECK NORMAL PER B757-200ER AMM 52-71. (7634708)

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 88,865 hrs · 23,624 cycles

SHIP 6805 2L EXIT SIGN TORN OFF. CORRECTIVE ACTION: REINSTALLED SIGN. NO DAMAGE NOTED. (7909925)

Part: ROLLER — DAMAGED (L2 DOOR) · airframe 88,372 hrs · 23,512 cycles

SHIP 6805 FOUND 2L DOOR UPPER FWD CAM ROLLER DAMAGED. CORRECTIVE ACTION: REMOVED & REPLACED #2L DOOR UPPER FWD CAM ROLLER AS REQUIRED. REF B757 AMM 52-11. ALL OPS NORMAL. (7838312)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 88,221 hrs · 23,480 cycles

SHIP 6805 LOWER RT SIDE EMERGENCY EXIT LTS FOR SEATS 2-4 INOP. CORRECTIVE ACTION: TS AND FOUND LOOSE CONNECTOR UNDER SEAT 2C. RECONNECTED OPS CHECK GOOD. B757 WDM 33-51. (7436873)

Part: GIRT BAR — UNSECURE (L1 DOOR SLIDE) · airframe 87,773 hrs · 23,386 cycles

SHIP 6805 L-1 DOOR GIRT BAR WILL NOT PROPERLY ENGAGE. OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 021-0001:2560-01492-AND ADJUST PER B757 AMM 52-11. (1792524)

Part: GIRT BAR — FAILED (R1 DOOR) · airframe 87,773 hrs · 23,386 cycles

SHIP 6805 R-1 DOOR GIRT BAR WILL NOT PROPERLY ENGAGE. OUT OF LIMITS. CORRECTIVE ACITON: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 021-0001:2560-01492-0101/002 00011 REPLACED GIRT BAR. REF B757 25-66. (1792388)

Part: LIGHT — UNKNOWN (R1 DOOR) · airframe 87,583 hrs · 23,333 cycles

SHIP 6805 SLIDE LIGHT ABOVE 1R DOOR IS ON EVEN WITH THE DOOR DISARMED. CORRECTIVE ACTION: CREW REPORTS LIGHT OPS NML. OPS CK PER B757 AMM 25-66. OPS CK GOOD. (7416446)

Part: SUPPORT — CORRODED (BS 900) · airframe 87,462 hrs · 23,302 cycles

SHIP 6805 FRETTING CORROSION ON ACCESS PANEL SUPPORT STA 900 BTW LBL 20 TO RBL 45 BODY FAIRING AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00448: OUTBOARD CHORD STA 900 BTW LBL 20 TO RBL 45 BODY FAIRING AREA (FUS) WAS REPAIRED PER ETI-57-21-118 REV. 2 AND ER/A 590549-14 REV. ORIGINAL SECTION I PERMANENT REPAIR. (1754427)

Part: DRAG FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON OPEN HOLES AT LH ENG DRAG FITTING CLAMP UP DIAGONAL BRACE AND REPAIRED PER ERA 590489 14. (LP 1754486)

Part: STRINGER SPLICE — CRACKED (RT WING) · airframe 87,462 hrs · 23,302 cycles

SHIP 6805 OF 1.300" APROX. ON LOWER STRINGER-8 SPLICE ANGLE AT WS:709. RIGHT WING. CORRECTIVE ACTION: SUMMARY OF NRC 00578: STRINGER-8 SPLICE ANGLE AT WS: 709. RIGHT WING WAS REPAIRED PER ETI-57-21-109 REV. ORIGINAL AND ER/A 590251-14 SECTION I: PERMANENT REPAIR REV. ORIGINAL. (1754379)

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,458 hrs · 23,300 cycles

DURING HCK MAINTENANCE FOUND A CRACK LOCATED AT FRAME WEB IN INBD UPPER FASTENER HOLE AT 4'O CLOCK POS IWTH LENGTH = 0.024" APROX AND TWO CRACKS LOCATED AT FRAME & OUTER CHORD IN LOWER OUTBD FASTENER HOLE AT 2'CLOCK POSTION WITH LENGTH = 0.040" APROX AND 8'CLOCK POSITION WITH LENGTH 0.048" APROX, AT BS 1640 FUSELAGE FRAME COMMON TO THE INTERCOSTAL TEE CLIP LH SIDE. CW ERA 59055514. (LP 1754942)

Part: FRAME — DENTED (ZONE 100) · airframe 87,458 hrs · 23,300 cycles

DURING HCK MAINTENANCE FOUND DENT ON FUSELAGE FRAME STATION 540 BETWEEN STRINGERS 24L AND 25L IN FORWARD CARGO. REPAIRED PER ER/A 590433-14. (LP 1753627)

Part: FRAME — UNKNOWN (ERA 590555-14AD) · airframe 99,511 hrs · 26,054 cycles

SHIP 6805 ERA 590555-14AD SECTION I ISSUED FOR REPAIR TO LH STA 1640 FRAME . DTE DTA IS REQUIRED. CORRECTIVE ACTION: REF ERA 590555-14AD. (1754299)

Part: BRACKET — LOOSE (BS 740-760 S1-2L) · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND LOOSE BRACKET SUPPORT ON EXTERNAL DOUBLER OF AEROSTAT RADOME BTW STA 740 TO 760 AND S-1 AND S-2L ONE ELONGATED HOLE WAS FOUND AFFECTIING OEM SKIN/STC DOUBLER. C/W ERA 590389-14 (LP 1753443)

Part: FRAME — CRACKED (BS 640 S8-9R) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACK ON FRAME STA 640RH BTW S-8R AND S-9R AT PASSENGER CABIN. CRACKED REPAIRED PER ERA 590399-14.

Part: DRAG FITTING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOWS; HOLE #1 SCRATCHES ON FITTING BTW 9 TO 3 CLOCK POS, CORROSION ON SKIN AND FITTING BTW 3 TO 5 CLOCK POS; HOLE #2 SCRATCHES ON FITTING BTW 12 TO 2 CLOCK POS, CORROSION ON SKIN AND FITTING BTW 3 TO 4 AND 9 TO 10 CLOCK POS, CORROSION ON SKIN BTW 5 TO 7 POS ; HOLE #3 SCRATCHES ON FITTING BTW 5 TO 7 AND 12 TO 1 CLOCK POS, CORROSION ON SKIN AT 11 CLOCK POS ; HOLE #4 SCRATCHES ON SKIN AND FITTING BTW 8 TO 12 CLOCK POS, CORROSION ON SKIN AND FITTING BTW 7 TO 9 CLOCK POS ; HOLE #5 SCRATCHES ON SKIN BTW 6 TO 1 CLOCK POS; HOLE #6 SCRATCH ON FITTING BTW 2 TO 4 CLOCK POS, SCRATCH ON SKIN BTW 6 TO 12 CLOCK POS ; HOLE #7 SCRATCH ON FITTING BTW 12 TO 4 CLOCK POS, SCRATCHES ON SKIN BTW 4 TO 7 CLOCK POS ; HOLE #8 SCRATCH ON FITTING BTW 3 TO 7 CLOCK POS, CORROSION ON SKIN AND FITTING BTW 3 TO 5 AND 8 TO 10 CLOCK POS, SCRATCHES ON SKIN BTW 7 TO 1 CLOCK POS : HOLE #9 CORROSION ON SKIN/FITTING BTW 4 TO 12 CLOCK POS; HOLE #10 SCRATCHES ON SKIN BTW 7 TO 1 CLOCK POS AND CORROSION ON SKIN/FITTING BTW 11 TO 12 CLOCK POS. C/W ERA 590487-14. (LP 1752686)

Part: NONE — NONE · airframe 90,892 hrs · 24,060 cycles

SHIP 6805 ERA 590389-14 ISSUED FOR REWORK TO FUSELAGE SKIN AT KU GROUNDING STRAP, INSTALLED PER STC ST03330CH. CORRECTIVE ACTION: REF ERA 590389-14 REV A. (1752459)

Part: NONE — NONE · airframe 90,915 hrs · 24,065 cycles

SHIP 6805 ERA 590399-14 ISSUED FOR REPAIR TO FUSELAGE FRAME AT STA 640, BE TWEEN STRINGERS 8R AND 9R. AMOC TO 2020-01-18 IS REQD. CORRECTIVE ACTION: REF ERA 590399-14AD REV A. (1752472)

Part: NONE — NONE · airframe 90,144 hrs · 23,894 cycles

SHIP 6805 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 590487-14AD. CORRECTIVE ACTION: REF ERA 590487-14AD. (1752220)

Part: DRAG FITTING — DAMAGED · airframe 91,190 hrs · 24,128 cycles

SHIP 6805 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 590489-14AD. CORRECTIVE ACTION: REF ERA 590489-14AD. (1752045)

Part: STRUCTURE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 SEVERAL NUTS ON STA 1330 LBL 10.45 AT AFT CARGO COMPARTMENT. REPAIRED PER SRM. (LP 1751176)

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON STRINGERS LBL 0, LBL 7.55, RBL 16.10, LBL 2.90, RBL 7.55, BTW STA 1440 TO 1480 AT AFT CARGO COMPARTMENT. STRINGERS REPAIRED PER SRM. (LP 1750362)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR SUPPORT BTW STA 700 TO 720 RBL 64. FLOOR SUPPORT WAS REPLACED. (LP 1748578)

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECITON MAINTENANCE FOUND CORROSION LEVEL 2 ON FWD LAVATORY SERVICE PANEL INNER SIDE BTW FS400 TO FS420 AND STGR 26L TO 29L AT FWD FUSELAGE. REPLACED SERVICE PANEL. (LP 1748114)

Part: PLATE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LH SIDE PLATE BTW TA 1310 TO 1400 AT AFT CARGO COMPARTMENT. SIDE PLATE WAS REPLACED. (LP 1747216)

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON STRINGERS RBL 7.55, BTW STA 1320 TO 1340 AT AFT CARGO COMPARTMENT. STRINGERS REPAIRED PER SRM. (LP 1748025)

Part: PANEL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECITON MAINTENANCE FOUND CORROSION LEVEL 2 ON SIDE PANEL UP/LOWER FACE, RH SIDE BTW STA 560 TO 646 AT FWD CARGO COMPARTMENT. SIDE PANEL REPLACED. (LP 1746925)

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING MAINTENANCE FOUND LEVEL 2 CORROSION ON SEAT TRACK SETTLEMENT AREA BTW 698 TO STA 720 RBL 24.75 AT PASSENGER CABIN. SEAT TRACK REPLACED. (LP 1746748)

Part: PANEL — DAMAGED (LT WING LE) · airframe 87,462 hrs · 23,302 cycles

SHIP 6805 INSPECTION OF THE LH AND RH WING LEADING EDGE PANELS TO VERIFY AD COMPLIANCE REQUIRED PER ER/A 590367-14AD. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR PER ER/A 590367-14AD REV. ORIGINAL SECTION I AND II. (1743351)

Part: FRAME — CRACKED (ZONE 200) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACK ON FRAME STA 800RH BTW S-8R AND S-9R AT PASSENGER CABIN. REPAIRED PER ERA 590292-14 (LP 1743226)

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SUPPORT ANGLE BTW STA 1675 TO 1681 LBL 52 APPROX. ANGLE WAS REPLACED. (LP 1740295)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND SEVERAL POINTS OF CORROSION LEVEL 2 ON BEAM STA 1640 BTW LBL 55 TO RBL55 AND REPAIRED PER SRM 53-00-51. (LP 1742132)

Part: NUT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 SEVERAL NUTS ON STA 1330 LBL 2.90 AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 53-00-53. (LP 1741080)

Part: DOOR SILL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LOWER DOOR SILL BTW STA 1380 TO 1440 AT AFT CARGO COMPARTMENT AND REPLACED. (LP 1740557)

Part: PLATE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SIDE PLATES LH FROM STA 1530 TO STA 1640 AT AFT CARGO COMPARTMENT. SIDE PLACED WS REPLACED. (LP 1739894)

Part: FLOOR SUPPORT — CRACKED (CABIN) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SUPPORT ANGEL BTW STA 1675 TO 1681 RBL 52. SUPPORT ANGLE WAS REPLACED. (LP 1739892)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACK ON INTERCOSTAL OF FLOOR STRUCTURE BTW STA. 1320 TO 1340 AN LBL 45.5. INTERCOTAL WAS REPLACED PER SRM. (LP 1739889)

Part: RESERVOIR — ACTIVATED (L2 DOOR SLIDE) · airframe 87,458 hrs · 23,300 cycles

DURING REMOTION OF L2 DOOR ESCAPE SLIDE WITH LEVER ON DISARM POSITION AND SAFETY PINS INSTALLED, EMERGENCY POWER RESERVOIR WAS FOUND ACTIVATED. EMERGENCY POWER RESERVOIR WAS REPLACED. (LP 1738652)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR SUPPORT BTW STA 1640 TO 1681 RBL 52 APPROX. FLOOR SUPPORT REPLACED. (LP 1739309)

Part: FLOOR SUPPORT — CRACKED · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACK BELOW OF FLOOR STRUCTURE BWT STA 1320 AND RBL 45.5. REPLACED FLOOR STRUCTURE. (LP 1739314)

Part: STRAP — CRACKED (CARGO BAY) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACKED STRAP (CEILING AREA OF CARGO) STA 1640 LBL 45 (W4). STRAP REPAIRED PER SRM. (LP 1736546)

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON STRINGERS RBL 10.45, RBL 16.10 BTW STA 1320 TO 1340 AT AFT CARGO COMPARTMENT. STRINGERS REPLACED PER SRM. (LP 1735401)

Part: GIRT BAR — OUT OF TOLERANCE · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND GIRT BAR SLIDERS WERE MEASURED BTW FLOOR FITTING AND NOT MEET THE MINIMUM ENGAGEMENT AT L1 FWD SLIDER. L2 FWD/AFT SLIDER AND R1 FWD/AFT SLIDER. GIRT BAR SLIDERS L1 FWD, L2 FWD/AFT AND R1 FWD WERE REPLACED. (LP 1734028)

Part: ANGLE — CRACKED (WNG-BDY FAIRIING) · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CRACK ON ANGLES STA 1180 AT LBL=12 AND RBL=12 AT WING TO BODY FAIRING STRUCTURE. WING TO BODY FAIRING STRUCTURE WAS REPLACED PER SRM. (LP 1733980)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR SUPPORT BTW STA 1640 TO 1681 LBL 52 APPROX AND REPLACED. (LP 1734524)

Part: PLATE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON RT SIDE PLATE BTW STA 1380 TO 1200 AT AFT CARGO COMPARTMENT. SIDE PLATE REPLACED. (LP 1733890)

Part: FRAME — CRACKED (CABIN) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACK ON FRAME STA 760RT BTW S-8R AND S-9R AT PASSENGER COMPARTMENT. REPAIRED PER SRM 53-00-07.

Part: FRAME — CRACKED (CABIN) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACK ON FRAME STA 760RH BTW S-8R AND S-9R AT PASSENGER CABIN. CRACK REPAIRED PER SRM 53-00-07. (LP 1729415)

Part: FRAME — CRACKED (CABIN) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND CRACK ON FRAME STA 840RH BTW S-8R AND S-9R AT PASSENGER CABIN AND REPAIRED PER SRM 53-0-07. (LP 1729791)

Part: FRAME — CRACKED (CABIN) · airframe 87,458 hrs · 23,300 cycles

DURING INSPECTION MAINTENACE FOUND CRACK ON FRAME STA 760 BTW S-8L AND S-9L WAS REPAIRED SRM 53-00-07. (LP 1729865)

Part: FORK — WORN (L4 DOOR) · airframe 87,458 hrs · 23,300 cycles

DURING INITIAL INSPECTION MAINTENANCE FOUND WEAR IN TRIGGER FORK IN PASSENGER L4 DOOR. TRIGGER FORK REPLACED. (LP 1726774)

Part: ACM — SEIZED (LEFT) · airframe 81,373 hrs · 22,085 cycles

ON CLIMB OUT, DUE TO HAZY SMOKE IN THE COCKPIT, CREW DONNED OXYGEN MASKS AND RAN SMOKE AND FUMES CHECKLIST. FOUND LT ACM SEIZED RENDERING LT PACK INOPERATIVE. REPLACED THE LT ACM, RE-HEATER & LOW LIMIT VALVE. PERFORMED DUCT BURNOUT AND LEAK CHECKS. OK FOR SERVICE.

Part: PANEL — MISSING (LT WING TE FLAP) · airframe 80,730 hrs · 21,958 cycles

SHIP 6805 A/C ARRIVED + FOUND ON O/B L/H FLAP A FIXED PANEL IS MISSING. CORRECTIVE ACTION: INSPECTED A/C THERE WAS NO DAMAGE TO THE L/H SIDE OF THE FUSELAGE OR TAIL REF L/P 5741509 + 5741510 FOR FINDING + REMOVED AND REPLACED O/B LH FLAP IAW PER B757 AMM 27-51. INSTALLED CARRIAGE TO GIMBAL ON LEFT OUTBD T/G FLAP AND RIGGED PER AMM 27-51. R/R LEFT T/E FLAP OUTBD XMTR PER B757 AMM 27-58 ALL MD NML. PERFORMED OUTBOARD FLAP ADJUSTMENT PER JIC. ALL ADJUSTMENTS CKS GOOD. PERFOMED FLAP TEST PER JIC NO FAULTS PRESENT. (5741508)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 80,465 hrs · 21,903 cycles

SHIP 6805 O2 MASKS AT 22 CDE DROPPED DOWN. CORRECTIVE ACTION: REPACKED O2 MASK AT LOC 22CDE IAW AMM 35-21. (5572707)

Part: OXYGEN MASK — UNSECURE (CABIN) · airframe 80,484 hrs · 21,908 cycles

O2 MASKS AT 36ABC DROPPED DOWN. REPACKED O2 MASK AT LOC 36ABC IAW AMM 35-21.

Part: SKIN — CRACKED (RT WING) · airframe 80,418 hrs · 21,891 cycles

SHIP 6805 RIGHT WING UPPER SURFACE HAS CRACKED PAINT AT TWO FASTENER LOCATIONS WITH ASSOCIATED FUEL LEAK. FASTENERS LOCATED WS 425.50 (APPROX.), STR U11.5. -MARKED- REF. A.A. TASK CARD. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 066-0002:5732-01014-01B/001 00264 REPAIRED PER ERA 574573-14 REV ORG. (0910663)

Part: SKIN — BULGED (FUSELAGE) · airframe 80,418 hrs · 21,891 cycles

SHIP 6805 FUSELAGE EXTERIOR SKIN IS BULGED WITH STRESSED RIVET IN AREA. FS 445 AT STRINGER 23L. CORRECTIVE ACTION: REF: WO, N/R 044 AND N/R 156. C/W ERA 574429-14 REV ORG FOR SKIN REPAIR AND STRINGER SPLICE AT STA: 445, STR: 23L. (0903467)

Part: LEAF SPRING — DEFECTIVE (GIRT BAR) · airframe 80,418 hrs · 21,891 cycles

SHIP 6805 GIRT BAR AFT LEAF SPRING LOST TENSION, SLIDER WONT REMAIN ON GIRT BAR WITH VERY LITTLE PRESSURE APPLIED. R1 DOOR. CORRECTIVE ACITON: REPLACED/INSTALLED R1 DOOR GIRT BAR REF AMM 25-66. (0899401)

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 79,748 hrs · 21,753 cycles

(AIRCRAFT 6805, L/P 0815205) EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:604 / 2L EMERGENCY / EXIT LIGHT FELL OFF / INTERIOR. EXIT SIGN REINSTALLED.

Part: LIGHT — DAMAGED (EXTERIOR) · airframe 79,748 hrs · 21,753 cycles

(AIRCRAFT 6805, L/P 5138636) EXIT EMERGENCY LIGHTS 2R DOOR INOP. FOUND EXIT INDICATOR LIGHT L860 DAMAGED. REPLACED LIGHT ASSY PER B757 AMM 33-51-10. REPLACED FUSE AT POWER SUPPLY M733 PER B757 AMM 33-51-07, NOW OPS OK.

Part: LINKAGE — BROKEN (L4 DOOR) · airframe 79,528 hrs · 21,710 cycles

4L DOOR HARD TO CLOSE FOUND BROKEN LINKAGE AT LOWER FLAP MECHANISM. REPLACED AFT LWR LATCH TORQUE TUBE RADIUS ROD, ROD END IAW AMM 52-11. ADJUSTED GIRT BAR ALL OPS CHECK NML AT THIS TIME.

Part: INDICATION SYS — MALFUNCTIONED (R1 DOOR) · airframe 77,285 hrs · 21,302 cycles

UNABLE TO DISARM 1R DOOR SLIDE ARM LIGHT WOULD NOT GO OUT. CYCLED DISARM HANDLE, DOOR DISARMED, NO DEFECTS NOTED. LIGHT EXTINGUISHED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,868 hrs · 21,209 cycles

EMERGENCY LIGHT DAMAGED OR INOPERATIVE. SECURED THE EMERGENCY LIGHT.

Part: GIRT BAR — FROZEN (L2 DOOR) · airframe 72,999 hrs · 20,444 cycles

L2 DOOR WILL NOT DISARM. FOUND THE GIRT BAR AND RECEPTACLE FITTINGS FULL OF WATER, BAR POSSIBLY FROZEN DUE TO RAIN. DOOR DISARMED AFTER 10 MINUTES. CLEANED FITTINGS-CLOSED AND ARMED SEVERAL TIMES.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 72,271 hrs · 20,281 cycles

RIGHT WING INBD, FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED IAW SRM 51-70-07.

Part: ACCESS PANEL — DAMAGED (RT AILERON) · airframe 72,271 hrs · 20,281 cycles

RIGHT AILERON INBD UPPER ACCESS PANEL HAS ONE FASTNER PULLED THROUGH. REPAIRED IAW ERA 554315-14.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,247 hrs · 20,276 cycles

LOWER EXTERIOR FUSELAGE HAS DENT AT APPROX STA 590 JUST BELOW FWD CARGO DOOR AT STRINGER 26R. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN LWR EXT AT STA 590 BELOW FWD CARGO DOOR IAW ER/A 554312-14 REV ORIG. SEE NRC 100-68 REF LOGPAGE 2890215 FOR DECAL MONITOR INSPECTION EVERY L-CHECK PER TOPP 30-10-70 PAGE 14.

Part: STRAP — CRACKED (FUSELAGE) · airframe 72,247 hrs · 20,276 cycles

AFT CARGO RT STA 1640 STRINGER 17R UNDER MAIN DECK FLOOR HAS A CRACKED STABILIZATION STRAP. CUT OUT DAMAGE AT AFT CARGO RT STA 1640 STRINGER 17R UNDER MAIN DECK FLOOR, STABILIZATION STRAP IAW SRM 53-00-51 FIG 201, REPAIR 13 REQUEST NDT NO CRACK. FABRICATED REPAIR DOUBLER AND FILLER, TREATED & PRIMED AND INSTALLED IAW SRM 53-00-51 FIG 201, REPAIR 13. THIS IS A CATEGORY "A" PERMANENT MAJOR REPAIR.

Part: RESERVOIR — DISCHARGED (L4 DOOR) · airframe 71,498 hrs · 20,129 cycles

4L DOOR EMERG POWER RSVR EMPTY. FOUND ON SVC CK. REPLACED SAME IAW AMM 52-11.

Part: HEADSET — SHORTED · airframe 70,679 hrs · 19,970 cycles

PAX REPORTED ELECTRICAL SHOCK FROM HEADSET JACK, SEAT 3B. OPS CHECK NORMAL ON GROUND. TRIED MULTIPLE HEADSET WHILE PLAYING MOVIES AND AUDIO, OPS OK.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 70,471 hrs · 19,932 cycles

EMERGENY LIGHTING NOT OPERATING IN COMMANDED POSITION. FOUND EMERGENCY LIGHT SWITCH AT P62 NLG PANEL INTERMIT. R & R S10035 SWITCH IAW SWPM 20 SHOOK WIRES DOWN NO FAULTS NOTED. R & R EMERGENCY LIGHT BATTERY M732, M731, M10919. IAW AMM 33-51-07. OPS OK.

Part: PLACARD — BINDING (R2 DOOR) · airframe 68,971 hrs · 19,655 cycles

2R DOOR ARM, DISARM PLACARD DOES NOT PREVENT DOOR FROM ARMING. FREED ARM, DISARM PLACARD. OK FOR SERVICE.

Part: BOTTLE — EMPTY (R1 DOOR ASSIST) · airframe 64,695 hrs · 18,815 cycles

DOOR ASSIST BOTTLE AT DOOR R1 WAS FOUND DEPRESSURIZED. JFK MAINTENANCE R & R ASSIST BOTTLE AT DOOR R1. LP7013389.

Part: SERVICE DOOR — DENTED (PNEUMATIC SYS) · airframe 72,364 hrs · 20,302 cycles

LT GROUND PNEUMATIC SVC DOOR HAS 1" X 1" DENT IN THE CUTOUT OB EDGE. ACCOMPLISHED PERMANENT REPAIR ON LT GROUND PNEUMATIC SVC DOOR AT O/B CUTOUT EDGE IAW SRM.

Part: FILTER — LEAKING (ENGINE FUEL) · airframe 64,542 hrs · 18,785 cycles

CREW REPORTED A FUEL DISAGREE-PROG 2 MESSAGE AFTER 4 HRS OF FLIGHT WITH A 3500LB DIFFERENCE BETWEEN TOTALIZER AND CALCULATED. THE CHECKLIST WAS USED TO VERIFY THAT THERE WAS NOT A FUEL LEAK. TOTALIZER WAS 3500 LB LESS THAN CALCULATED. MAINTENANCE TROUBLESHOT AND FOUND FUEL LEAKING FROM THE NR 1 ENGINE FUEL FILTER. THE FUEL FILTER WAS REPLACED, LEAKED CHECKED AND THAT ACFT WAS RETURNED TO SERVICE. LP7013316.

Part: LINER — OUT OF ADJUST (R1 DOOR) · airframe 64,021 hrs · 18,672 cycles

R1 DOOR WILL NOT DISARM SLIDE HANDLE ENOUGH TO INSERT SAFETY LATCH. ADJUSTED DOOR LINER IAW AMM 52-11.

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN SEAT TRACK FROM BS 1540-1640 LBL 45.5 IS CORRODED. FOUND TO BE OUT OF LIMITS. R & R THE SEAT TRACK IAW SRM.

Part: DUCT — TORN (NR 4 SLAT) · airframe 64,018 hrs · 18,670 cycles

LEFT WING NR 4 SLAT I/B OF ANTI /ICE DUCT SLAT TORN. REMOVED NR 4 SLAT, FABRICATED REPAIR AND INSTALLED IAW AMM AND SRM.

Part: INTERCOSTAL — CRACKED (BS 1320-1340) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN INTERCOSTAL, BS 1320-1340, RBL 24. IS CRACKED. REMOVED INTERCOASTAL AND FABRICATED NEW AND INSTALLED IAW SRM. 1854154.

Part: INTERCOSTAL — CRACKED (BS 1320) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN FLOOR INTERCOASTAL ATTACH BRACKET CRACKED AND MISSING FASTENERS. APPROXIMATELY, STA 1320, LBL 45 MARKED. REMOVED CRACKED BRACKET AND FABRICATED AND INSTALLED NEW IAW SRM. 1854134.

Part: INTERCOSTAL — CRACKED (BS 1320) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN INTERCOASTAL, BS 1320-, LBL 45 IS CRACKED. REMOVED INTERCOASTAL, FABRICATED AND INSTALLED NEW INTERCOASTAL IAW SRM. 1854150.

Part: FLOOR SUPPORT — CORRODED (BS 1515) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

AFT CARGO COMPT, FS 1515; CORROSION AT STA 26R, RBL 19 UNDERNEATH NUT PLATE. C/W REPAIR AT AFT CARGO COMPARTMENT FS 1515, STR 25L, RBL 19, FLOOR SUPPORT IAW ERA 332525-14MA, REV D.

Part: FLOOR SUPPORT — CORRODED (BS 1515) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

AFT CARGO COMPT; FS 1515 CORROSION AT STR 29L, LBL7. UNDERNEATH NUT PLATE. C/W REPAIR AT AFT CARGO COMPT FS 1515, FLOOR SUPPORT STR 29L AT LBL 7 IAW ERA 332525-14MA, REV D.

Part: FLOOR SUPPORT — CORRODED (BS 1515) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

AFT CARGO COMPARTMENT, FS 1515, CORROSION AT S-27R, RBL 16, UNDERNEATH AT NUT PLATE. C/W REPAIR AT AFT CARGO COMPARTMENT FS 1515, S-27R, RBL 16 IAW ERA 332525-14 MA.

Part: NONE — NONE (NONE) · airframe 64,021 hrs · 18,672 cycles

ATG ANTENNA DOUBLER WILL BE 6" FROM EXISTING REPAIR. C/W STA 1340 TO 1360, STR 29L TO 30 R FABRICATION AND INSTALLATION OF ATG ANTENNA DELETION DOUBLER REPAIR IAW ERA 527407-14, REV "O".

Part: SUPPORT — CORRODED (BS 340-348) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, R1 THRESHOLD SUPPORTS, 2 EA, STA 340-348 CORROSION UNDER NUT PLATES. REMOVED THRESHOLD SUPPORTS AND FOUND OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM. 1850209.

Part: CUSP WEB — CORRODED (BS 1190) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN CUSP WEB CORRODED AT APPROXIMATELY FS 1190, RBL 61, NEAR S-17R. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED NEW REPAIR AND INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 440-640) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN SEAT TRACK RBL 24, BS 440 TO 640 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

BS 345, FLOORBEAM PREVIOUS REPAIR CORRODED AT LBL 12. FOUND CORROSION TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 345-418) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, CORROSION ON TOP OF FLOOR STRUCTURE BL-0 STA 345-STA 418. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED AND INSTALLED FLOOR SUPPORT IAW SRM.

Part: ATTACH BRACKET — CRACKED (BS 1320) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN FLOORBEAM INTERCOSTAL ATTACH BRACKET APPEARS TO BE CRACKED AND MISSING FASTENERS. APPROXIMATELY STA 1320, LBL 25. REMOVED, FABRICATED AND INSTALLED NEW BRACKET IAW SRM. 1850321.

Part: INTERCOSTAL — CRACKED (BS 1320-1340) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN INTERCOSTAL BS 1320-BS1340, RBL 45 IS CRACKED. REMOVED INTERCOSTAL AND FABRICATED REPAIR. HEATED AND INSTALLED IAW SRM. 1850339.

Part: ATTACH ANGLE — CRACKED (BS 1320) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN FLOORBEAM INTERCOSTAL ATTACH ANGLE BRACKET CRACKED. APPROXIMATELY STA 1320, RBL 25. REMOVED CRACKED BRACKET AND FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED IAW SRM. 1850258.

Part: FRAME — DENTED (BS 1420) · airframe 64,018 hrs · 18,670 cycles

AFT CARGO COMPARTMENT BS 1420, FRAME IS DENTED BETWEEN STRINGER 26-27 LT. CUT OUT DAMAGE AND INSPECTED-NO CRACKS NOTED. REPAIRED FRAME DAMAGE AT BS 1420 BETWEEN STRINGERS 26L & 27L IAW SRM.

Part: SEAT TRACK — GOUGED (BS 780-879) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN SEAT TRACK FROM BS 780- 879, LBL 45 IS GOUGED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN FLOOR SUPPORT HAS SEVERAL AREA'S OF CORROSION FROM BS 324-345, RBL 2. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: ATTACH BRACKET — CRACKED (BS 1320) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN FLOORBEAM INTERCOSTAL ATTACH BRACKET CRACKED, APPROXIMATELY STA 1320, RBL 45. REMOVED BRACKET, FABRICATED, AND INSTALLED IAW SRM. 1850330.

Part: FRAME — DENTED (BS 1420) · airframe 64,018 hrs · 18,670 cycles

AFT CARGO COMPARTMENT BS 1420, FRAME IS DENTED BETWEEN STR 26-27LT. REPAIRED FRAME DAMAGE AT BS 1420 BETWEEN STR 26L AND 27L IAW SRM.

Part: FRAME — DENTED (BS 1400) · airframe 64,018 hrs · 18,670 cycles

AFT CARGO COMPARTMENT, BS 1400, FRAME IS DENTED BETWEEN STR 26-27 LT. REPAIRED FRAME DAMAGE AS BS 1400 BETWEEN STR 26L AND 27L IAW SRM.

Part: FRAME — DENTED (BS 1400) · airframe 64,018 hrs · 18,670 cycles

AFT CARGO COMPT, BS 1400, FRAME IS DENTED BETWEEN STRINGER 26-27 LT. CUT OUT DAMAGE AND INSPECTED. REPAIRED FRAME DAMAGE AS BS 1400 BETWEEN STRINGERS 26L & 27L IAW SRM.

Part: SEAT TRACK — CORRODED (BS 642) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN SEAT TRACK, RBL 48, STA 642 WITH AREA CORRODED. FOUND CORROSION OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 345-365) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, R-1 FLOOR SUPPORT CORRODED FROM STA 345-365. REMOVED CORROSION AND FOUND OUT OF LIMITS. R & R FLOOR SUPPORT IAW DWG 141N5160, REV B.

Part: FRAME — GOUGED (BS 1280) · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN FRAME AT BS 1280 BETWEEN STR 13-11 RT HAS MULTIPLE GOUGES. BLENDED OUT AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN FLOORBEAM NUT PLATE CORRODED STA 1680, RBL 25. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED.

Part: FLOORBEAM — CORRODED (BS 405) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, CORROSION ON FLOOR SUPPORT BS 405, BETWEEN RBL 24 & 45. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. DRILLED AND DEBURRED NEW FLOOR SUPPORT IAW SRM AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,154 hrs · 20,060 cycles

MAIN CABIN, CORROSION ON FLOORBEAM STA 324 RBL 61. REMOVED REPAIR, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 338-370) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, CORROSION ON FLOOR SUPPORT IN FRONT OF R1 DOORWAY STA 338 TO 370. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED.

Part: DECK PLATE — CORRODED (BS 1715) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN AFT DECK PLATE CORRODED STA 1715, LBL 13. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 1380-1400) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, RT CUSP WEB CORRODED, STA 1380-1400. REMOVED CUSP WEB AND BRACKET SUPPORT, REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: SNUBBER — LEAKING (R2 DOOR) · airframe 64,018 hrs · 18,670 cycles

R2 DOOR TORQUE TUBE SNUBBER IS LEAKING. R & R R2 DOOR TORQUE TUBE SNUBBER ASSY REF AMM 52-11.

Part: DECK PLATE — CORRODED (BS 1715) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN AFT DECK PLATE CORRODED, STA 1715, LBL 23. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED.

Part: PANEL — BROKEN · airframe 64,018 hrs · 18,670 cycles

RT WING NR 10 SPOILER PANEL BROKEN ON INBD T/E. NR 10 SPOILER REPAIRED AND INSTALLED IAW AMM 27-61-01 IAW SRM.

Part: DECK PLATE — CORRODED · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN AFT DECK PLATE IS CORRODED AT BS 1681-8 BETWEEN LBL 30-50. REMOVED CORROSION, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN SEAT TRACK BS 1540-1640, RBL 45 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: MOUNT — CORRODED (BS 330) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, CORROSION ON GALLEY MOUNT RBL 42, BS 330. FOUND CORROSION OUT OF LIMITS. R & R GALLEY MOUNT FITTING IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 365-377) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN, CORROSION TOP & BOTTOM SIDE OF FLOOR SUPPORT, LBL 63, BS 365 -377. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN SEAT TRACK FROM BS 1540-1640, RBL 24 IS CORRODED. FOUND CORROSION OUT OF LIMITS, R & R THE SEAT TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

BS 365 FLOORBEAM PREVIOUS REPAIR CORRODED FROM LBL 10 TO RBL 60. CORRECTIVE ACTION: REMOVED PREVIOUS REPAIR, INSPECTED, NO CRACKS NOTED. FABRICATED REPAIR AND INSTLLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 418) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

CORROSION FOUND ON THE SEAT TRACK BS 418, RBL 24. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: DECK PLATE — CORRODED · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN AFT DECK PLATE PREVIOUS REPAIR DOUBLER CORRODED STA 1715, RBL 23. REMOVED REPAIR DOUBLE FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1540-1640) · corrosion level 2 · airframe 64,018 hrs · 18,670 cycles

MAIN CABIN SEAT TRACK FROM BS 1540- 1640, LBL 24.5 IS CORRODED. R & R THE SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 58,445 hrs · 17,497 cycles

AFT CARGO, LOWER FLOOR SUPPORT CORRODED, FOUND FIXED FLOOR PANEL CORRODED OUT OF LIMITS OF SRM 53-00-53, REMOVED FIXED FLOOR PANEL AND FOUND CORROSION ON CHORD. REMOVED NUT PLATES REMOVED CORROSION, MEASURED AND FOUND TO BE WITHIN LIMITS OF SRM 53-60-15. 177747, 881955 OK TO TREAT AND PAINT 881955. TREATED AND PAINTED REF SRM 53-00-53 177747. REPLACED NUT PLATES. BEGAN INSTALLATION IAW ERA 373211-14MA, REV G/ DWG 146N5391-92 455329. INSTALLED IAW ERA 373211-14MA AND BAC DWG 146N5391-92 437335. FLOOR PANEL INSTALLED ON N/R 65.

Part: SKIN — DAMAGED (SLAT) · airframe 55,349 hrs · 16,939 cycles

WING SLAT T/E WEDGE PANELS DAMAGED. REPAIRED IAW AA 5742-01022.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 51,390 hrs · 16,176 cycles

SPARKS AND SMOKE REPORTED COMING FROM SEAT 1A/1B. MAINTENANCE FOUND SEAT WIRING HARNESS ROUTED INCORRECTLY AND PINCHED IN SEAT TRACK. REPAIRED WIRING HARNESS PER AMM CHAPTER 20, OPERATION NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 50,885 hrs · 16,074 cycles

DURING LINE CHECK, MX FOUND MID GALLEY FORWARD EMERGENCY LIGHT INOPERATIVE. MX REPAIRED LOOSE WIRE AND REPLAMPED LIGHT. LIGHT OPERATES NORMAL.

Part: TEE FITTING — DAMAGED (PAX DOOR) · airframe 44,087 hrs · 14,761 cycles

DOOR INTERCOSTAL TEE FITTING DAMAGED. REPLACED IAW AA 5310-01371.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 40,497 hrs · 14,108 cycles

CABIN ALT INOP EICAS MESSAGE SYSTEM 1 AND SYSTEM 2. REPLACED NR 1 AND NR 2 AUTO PRESS CONTROLLERS, CHECKS GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 39,680 hrs · 13,962 cycles

ON TAXI OUT, CABIN PRESSURE AUTO INOP ILLUMINATED BOTH AUTO 1 AND AUTO 2. T/S PER SSM 21-30-00. SUSPECT K207 RELAY ON ENG START. REMOVED AND REPLACED SAME PER MM. REMOVED AND REPLACED CABIN PRESS OVHD PANEL PER AMM DUE TO BOTH AUTO MSGS. DUE TO PREVIOUS HIST OF AUTO 2 CNTLR CHANGED AND ON BITE FND CONTROLLER FAULT AND MOTOR FAULT ON 2ND ATTEMPT NO FAULT. REMOVED AND REPLACED AUTO 2 CONTROLLER PER AMM. NOW NO MSGS. A/C OK FOR SERVICE.

Part: FITTING — GOUGED (LT WING TE FLAP) · airframe 39,134 hrs · 13,867 cycles

LEFT WING INBD AFT FLAP INBD PROGRAMMER FITTING IS GOUGED. C/W AT SAA - SAT ON N/R 118711 SAA JOB 82298770001.

Part: SKIN — GOUGED (BS 1808) · airframe 39,134 hrs · 13,867 cycles

RT FUSE SKIN APPROX STA 1808 HAS A GOUGE JUST BELOW FAIRING FOR HORIZ STAB. C/W AT SAA - SAT ON N/R 115955 JOB 82297790001.

Part: STRUCTURE — CRACKED (LT WING BARRIER) · airframe 39,134 hrs · 13,867 cycles

LT DRY BAY HAS 1 INCH CRACK AT TOP CORNER OF BARRIER AND WS 285.65 RIN INBD OF INNER DOOR 532HZ, FOUND DURING DRY BAY LEAK CHECK. C/W AT SAA - SAT ON N/R 119332 JOB 82305140001.

Part: SEAT TRACK — CORRODED (BS 695-780) · airframe 39,134 hrs · 13,867 cycles

MAIN CABIN SEAT TRACK STA 695 TO 780 RBL 24-25 HAS CORROSION ON MULTIPLE AREAS BOTTOM SURFACE AND CROWN. C/W AR SAA - SAT ON N/R 119046 SAA JOB 82301770001.

Part: PLATE — CORRODED (BS 1720) · airframe 39,134 hrs · 13,867 cycles

MAIN CABIN AFT DECK PLATE STA 1720 BL0 - RBL 52N HAS CORROSION ON UPPER SURFACE. C/W AT SAA - SAT ON N/R 108688 SAA JOB 82299900001.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 39,134 hrs · 13,867 cycles

CORROSION ON MAIN DECK FLOORBEAM UPPER CHORD TOP SURFACE AT STA 324 RBL 42 CP53-222-01-02-05I. C/W AT SAA - SAT ON N/E 104189 SAA JOB 82302100001.

Part: PAN — CORRODED (BS 710) · airframe 39,134 hrs · 13,867 cycles

CORROSION ON LAV S SERVICE PAN AROUND DUMP CHUTE IN FWD CARGO COMPARTMENT LT SIDE STA 710. C/W AT SAA - SAT ON N/R 119516 SAA JOB 82302250001.

Part: SKATE ANGLE — CORRODED (L-2 DOOR) · airframe 39,134 hrs · 13,867 cycles

L-2 DOOR LOWER SILL SKATE ANGLE UPPER SURFACE STA 665-755 HAS CORROSION ON NUMBER OF AREAS CP53-232-01 01 05I. C/W AT SAA - SAT ON N/R 119041. SAA JOB 82301810001.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 39,134 hrs · 13,867 cycles

MAIN CABIN FLOORBEAM STA 345 HAS CORROSION AROUND FASTENER HOLES LBL 10 - LBL 20. COMPLIED WITH AT SAA - SAT ON N/R 108681 SAA JOB 82299830001.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 39,134 hrs · 13,867 cycles

CORROSION ON FLOORBEAM AT FASTENER HOLES STA 1660 AND LBL 9 TO LBL 16 UPPER SURFACE OF BEAM CP53-251-01-02-051/COMPLIED WITH AT SAA, SAT ON N/R 119120 SAA JOB 82302660001.

Part: SKIN — DENTED (BS 281) · airframe 39,134 hrs · 13,867 cycles

DENT ON FUSE SKIN AT STA 281 AND BETWEEN S 17R AND S 18R WITH A 10 INCH CREASE ENDING AT APPROX SRA 271. COMPLIED WITH AT SAA - SAT ON N/R 122231 SAA JOB 82298230001.

Part: STRAP — CORRODED (BS 1510) · airframe 39,134 hrs · 13,867 cycles

NUT PLATE STRAP CORRODED IN BILGE AREA AT STA 1510 BETWEEN S- 28R AND S-29R AND CP53-156-01I, COMPLIED WITH AT SAA - SAT ON N/R 103990 SAA JOB 82301370001.

Part: HEATER — SPARKS (COCKPIT) · airframe 38,988 hrs · 13,837 cycles

MOMENTARY SPARKS EMITTED FROM F/O FOOT HEATER SWITCH INFLIGHT WHEN SWITCHING FROM OFF TO HIGH. ITEM PLACED ON MEL 21-45-01B CBS COLLARED. REMOVED AND REPLACED SWITCH. CHECKS NORMAL. MCO AND PLACARD REMOVED.

Part: CONTROL UNIT — MALFUNCTIONED (HYD PUMP) · airframe 38,797 hrs · 13,800 cycles

RIGHT ELECTRIC HYD PUMP. CIRCUIT BREAKER POPPED. CLEANED AND RESEATED CONNECTOR RAN ELEC HYD PUMPS. ACTUATED ALL CONTROL SURFACES AND DROPPED FLAPS ALSO DEPLOYED SPEEDBRAKES L-ALL AT THE SAME TIME. C/B DID NOT POP- PUMP IND ALL NORMAL. REMOVED AND REPLACED M10005 ELEC HYD PUMP RIGHT ELCU ACTUATED ALL CONTROL SURFACES. C/B DID NOT POP RAN RIGHT PUMP 15 MIN ALL IND NORMAL.

Part: CONTROLLER — INOPERATIVE (LT A/C PACK) · airframe 38,218 hrs · 13,681 cycles

LT PACK TEMP CONTROL INOP. RE- RACKED LT PACK TEMP CONTROL PER BITE. NO FAULTS. LT PACK OPS NML.

Part: OVEN — SMOKE (GALLEY) · airframe 34,308 hrs · 12,635 cycles

FWD GALLEY NR 1 OVEN REPORTED SMOKE AFTER OVEN FOOD SPILL. CLEANED OVEN THEN CYCLED OVEN FOR 2 HRS OK FOR SVC MCO/PL RMVD.

Part: CAP — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY FLOOR LIGHT IN FIRST CLASS MISSING BOTH END CAPS. REPLACED BOTH END CAPS FOR EMERGENCY FLOOR LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY FLOOR LIGHT IN FIRST CLASS HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY FLOOR LIGHT IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT)

DFW - FLOOR MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16 INOPERATIVE. REPLACED HARNESS AT SEAT ROW 13 FOR INOPERATIVE FLOOR MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - FORWARD ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS FOR FORWARD ESCAPE PATH EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW FLOOR EMERGENCY ESCAPE PATH LIGHTING SEGMENT AT SEAT 1AB INOPERATIVE. REPLACED FLOOR EMERGENCY ESCAPE PATH LIGHTING SEGMENT ASSEMBLY AT SEAT 1AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: SPRING — DEFORMED (GIRT BAR) · airframe 22,260 hrs · 7,631 cycles

THE EVACUATION SLIDE GIRT BAR LEAF RETENTION SPRING AT THE R1, L2, AND R4 DOOR WERE DEFORMED AND ADJUSTED. THE RETENTION SPRING AT THE L4 DOOR WAS REPLACED ACCOUNT DEFORMED.

Part: INDICATOR · airframe 19,589 hrs · 6,614 cycles

LT MLG POSITION INDICATOR LOOSE IN SOCKET AND WILL NOT STAY LATCHED IN. R & R LT MLG POS IND 26-1424. OPS CK POS IND OK. LAST CHECK C PERFORMED LAX 8/3/01. --CLOSED--

Part: SKIN — DENTED (FUSELAGE) · airframe 16,671 hrs · 5,573 cycles

DURING MAINTENANCE SMALL DENTS WERE DISCOVERED AT FLIGHT STATION 640 AND WL 200. REMOVED OLD EXTERNAL DOUBLER ALSO REMOVED DOUBLER FROM NEW DAMAGED AREA AND INSTALLED NEW EXTERNAL DOUBLER PER SRM BETWEEN STN. 640 TO 196 AND BETWEEN STN. 196 AND 216.