N713TW

Part: D-RING — DAMAGED (ZONE 800) · airframe 94,531 hrs · 24,626 cycles

R1 LOCATION D-RING DAMAGE/MISSING. FOUND D RING BEHIND R1 DOOR BUSTLE. REATTACHED D RING REF B757 AMM 25-66. (8413413)

Part: DOOR FRAME — FOD (ZONE 800) · airframe 94,353 hrs · 24,582 cycles

AT APPROX 16,000 - 17,000 FEET, L AFT ENT DOOR CAUTION MSG ILLUMINATED ON EICAS. CABIN PRESS NORMAL. OBSERVED EXCESS DEBRIS BUILD-UP ON L AFT ENTRY DOOR, CLEANED AS REQUIRED. REFERENCED QRH FOR CONFIG DEVIATIONS, NO DISCREPANCIES NOTED. (7692940)

Part: LIGHT — FAILED (ZONE 200) · airframe 94,306 hrs · 24,573 cycles

ENROUTE FA'S NOTIFIED OF BURNING SMELL NEAR DOOR 2L. INDENTIFIED FUME COMING FROM CEILING NEAR LIGHTS. NO SMOKE. INSTRUCTED FAS TO TURN OFF CABIN LIGHTS SMELL DISAPIATED. QRH 8.4 COMPLIED WITH. PERFORMED OPS TEST OF CEILING LTS, FOUND BURNING SMELL FROM OVERHEAD BINS LIGHT STRIP ROWS 21/22 ABC. R/R LIGHT STRIP M91035 , CHKS GOOD IAW B757 AMM 33-21. OK FOR SVC. REF LOG 1347261 FOR NO GO ODI LOG COMPLETION. (7692924)

Part: GIRT BAR — FOD (ZONE 800) · airframe 93,660 hrs · 24,426 cycles

L4 ENTRY DOOR WOULD NOT TOTALLY ARM NOR DISARM. FOUND DEBRIS UNDER GIR BAR AT AFT SIDE OF DOOR 4L. CLEARED ANDCYCLED IAW B757 AMM 52-11. OPS CHECK OK. (7640992)

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 92,959 hrs · 24,265 cycles

L4 PAX DOOR SLIDE WON'T DISARM. REPLACED AFT RADIUS ROD PER AMM 52-11. ADJUSTED GIRT BAR MECHANISM PER B757 AMM 52-11. C/W RII OF ROD INSTALL REF AMM 52-11.

Part: STRUCTURE — DAMAGED (ZONE 500) · airframe 92,538 hrs · 24,140 cycles

SHIP 6809 ACCOMPLISH SECTION VI: TIME-LIMITED REPAIR (FLAME SPRAY) WITHIN 24 MONTHS (730 DAYS) AFTER ACCOMPLISHMENT OF SECTION V PER ER/A 532885-14 REV D (LH WING / FUEL TANK AUX STRUCTURE / WS 285.65 TO WS 313.5 / DRY BAY BARRIER PANEL / CRACKED). CORRECTIVE ACTION: REF ERA 532885-14 REV D. (1030751)

Part: BARRIER — DAMAGED (ZONE 100) · airframe 92,538 hrs · 24,140 cycles

SHIP 6809 WHILE PERFORMING REPETTIVE INSPECTION PER SECTION2 OF ERA 532885 -14 REV C REF LOG PG 1919279 FOUND ERRORS IN PAPERWORK THAT L/H DRY BAY BARRIER PNL 532HZ WAS NOT ACCOMPLISHED. CORRECTIVE ACTION: ACCOMPLISHED SECTION 5 TIME LIMITED REPAIR PER ERA 532885-14 REV D ALSO REF LOG PG 2961772 AND LOG PG 1030751. (1032137)

Part: DOOR — MALFUNCTIONED (ZONE 700) · airframe 92,097 hrs · 24,023 cycles

SHIP 6809 ON FINAL APP GEAR DOORS CAUTION. RAN QRH AND CONTINUED WITH LANDING. RAMP CREW SAID RIGHT MAIN GEAR DOOR WAS SLIGHTLY OPEN. CORRECTIVE ACTION: MLG DOORS 5 TIMES IAW B757 AMM 32-12. DOORS OPENED AND CLOSED NORMALLY. BITE CHECKED THE PSEU IAW B757 FIM 32-09 WITH NO FAULTS NOTED. A/C OK FOR SERVICE. (7223925)

Part: MECHANISM — OUT OF ADJUST (ZONE 800) · airframe 91,915 hrs · 23,955 cycles

SHIP 6809 MCD L2 WILL NOT CLOSE CORRECTLY. CORRECTIVE ACTION: READJUSTED 2L PASSENGER DOOR KNUCLE BUSTER MACHANISM PER B757 AMM 25-11. OPS TEST OK. (6912420)

Part: LANYARD — UNSECURE (ZONE 800) · airframe 91,476 hrs · 23,812 cycles

SHIP 6809 4R DOOR SLIDE LANDYARD HANGING. CORRECTIVE ACTION: SECURED 4R LANYARD, A/C OK FOR SVC PER B757 AMM 52-11. (7259322)

Part: SKIN — DAMAGED (ZONE 500) · airframe 91,476 hrs · 23,812 cycles

SHIP 6809 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 616812-14AD REV A. CORRECTIVE ACTION: REF ERA 616812-14AD. (0803679)

Part: DOOR — UNKNOWN (L2) · airframe 89,878 hrs · 23,368 cycles

SHIP 6809 2 L DOOR WOULD NOT ARM. CORRECTIVE ACTION: CYCLED DOOR LATCH OPS NML IAW B757 AMM52-26. (6204896)

Part: GIRT BAR — LACK OF LUBE (R1 DOOR AREA) · airframe 89,878 hrs · 23,368 cycles

SHIP 6809 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: T/S PER B757 AMM 52-71. INSPECTED ,CLEANED AND LUBED 1R DOOR GIRT BAR. OPS CHK NRML (0473712)

Part: DOOR — NONE (L2) · airframe 89,847 hrs · 23,361 cycles

SHIP 6809 2L ENTRY DOOR WON'T ARM. CORRECTIVE ACTION: INSPECTED & ARMED / DISARMED 2L DOOR MULTIPLE TIMES , N.T.F. (6204884)

Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 89,847 hrs · 23,361 cycles

SHIP 6809 2L DOOR STILL WILL NOT ARM. CORRECTIVE ACTION: READJUSTED DOOR BUSTLE AND STRAP REF B757 AMM 52-11. OPS CHECK NORMAL. (6204864)

Part: GIRT BAR — FOD (ZONE 200) · airframe 89,847 hrs · 23,361 cycles

SHIP 6809 2L DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS NEAR GIRT BAR MECHANISM FOR 2L DOOR. DOOR OPS CHECK NORMAL REF B757 AMM 52-10. (6204862)

Part: DOOR FRAME — FOD (L2 DOOR) · airframe 89,820 hrs · 23,353 cycles

SHIP 6809 LEFT DOOR 2 WONT'CLOSE AND ARM NORMAL. CORRECTIVE ACTION: CLEANED DEBRIS ADJUSTED SLIDE COVER OP CHECK NORMAL. (6204854)

Part: GIRT BAR — FOD (L2 DOOR) · airframe 89,739 hrs · 23,337 cycles

SHIP 6809 UNABLE TO ARM L2 DOOR. CORRECTIVE ACTION: CLEARED DEBRIS ON GRIT BAR DOOR ARMS NORMALLY AND DISARMS NORMALLY REF B757 AMM 52-11. (6204812)

Part: GIRT BAR — FOD (L2 DOOR) · airframe 89,728 hrs · 23,335 cycles

SHIP 6809 FA'S UNABLE TO ARM L2 DOOR. CORRECTIVE ACTION: REMOVED DEBRI FROM GIRT BAR- OPS CHK NML. (6204810)

Part: DOOR — NONE (L2) · airframe 89,597 hrs · 23,309 cycles

SHIP 6809 2L DOOR WOULD NOT ARM. CORRECTIVE ACTION: CYCLED 2L DOOR, ARMS OK. (5610684)

Part: INDICATOR — MALFUNCTIONED (R1 DOOR SLIDE) · airframe 89,499 hrs · 23,283 cycles

R1 DOOR SLIDE LIGHT WENT OUT DURING CRUISE WITH DOOR ARMED. UNABLE TO DUPLICATE SLIDE LIGHT OPERATES NORMAL.

Part: LATCH — FOD (R1 GIRT BAR) · airframe 89,478 hrs · 23,279 cycles

R1 DOOR SLIDE INDICATOR DOES NOT ILLUMINATE WITH SLIDE LEVER IN ARM POSITION. REMOVED DEBRIS FROM GIRT BAR LATCH OPS CK'D LATCH MECHANISM OK IAW B757 AMM 52-12. (5610640)

Part: DOOR — FOD (R1 DOOR) · airframe 89,462 hrs · 23,275 cycles

SHIP 6809 AT PUSHBACK DOOR 1 R ARMING LEVER WILL NOT ARM VERY HARD TO MOVE. CORRECTIVE ACTION: CLEANED DEBRIS PER B757 AMM 52-11 OP CHECK NORMAL. (5610634)

Part: GIRT BAR — FOD (R1 DOOR) · airframe 89,462 hrs · 23,275 cycles

SHIP 6809 AT PUSHBACK DOOR 1R ARMING LEVER WOULD NOT MOVE TO THE ARM POSITION. CORRECTIVE ACTION: FOUND AND CLEARED DEBRI FROM GIRT BAR TRACK OPS CHECK NORMAL PER B757 AMM 25-66. (5610630)

Part: INDICATOR — INOPERATIVE (R3 DOOR SLIDE) · airframe 89,365 hrs · 23,251 cycles

SHIP 6809 3R ESCAPE SLIDE KNUCKLE KNOCKER WILL NOT EXTEND WHEN DOOR IS ARMED. CORRECTIVE ACTION: OPERATED 3R DOOR SLIDE ARMING LEVER MULTIPLE TIMES. COULD NOT DUPLICATE FAULT. OPS CHK GOOD. (0387119)

Part: GIRT BAR — LACK OF LUBE (NOT REPORTED) · airframe 89,362 hrs · 23,250 cycles

SHIP 6809 LIGHT DIDNT TURN ON UNTIL TRYING MULTIPLE TIME OF ARMING. CORRECTIVE ACTION: LUBE & CLEAN GIRT BAR, CHKS OK. (0384926)

Part: INDICATOR — UNKNOWN (DOOR) · airframe 89,362 hrs · 23,250 cycles

SHIP 6809 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:608. CORRECTIVE ACTION: 4R KNUCKLE KNOCKER CHK OK.

Part: BULB — FAULTED (SLIDE INDICATOR) · airframe 89,246 hrs · 23,226 cycles

AIRCRAFT 6809, ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S/ ARMED DOOR INDICATOR LIGHT AT 1R NOT LIGHTING UP. CORRECTIVE ACTION: RELAMPED ESCAPE SLIDE INDICATOR LAMP PER B757AMM 33-20. OPS CHK GOOD. (LP 0369675)

Part: DOOR — UNKNOWN (L2) · airframe 89,185 hrs · 23,214 cycles

SHIP 6809 DOOR 2L WILL NOT ARM. CORRECTIVE ACTION: CYCLED 2L DOOR. OPS CHK NML. (5330018)

Part: LAMP — INOPERATIVE (R1 SLIDE LIGHT) · airframe 89,095 hrs · 23,195 cycles

SHIP 6809 1R SLIDE ARM LIGHT NOT ILLUMINATING. CORRECTIVE ACTION: RELAMPED, PERFORMED ADJUSTMENT PER B757 FIM 25-66-00-815-802 AND AMM 25-66 . TARGETS OKAY SIDE LIGHT ILLUMINATION OPS CHK GOOD. (4376181)

Part: DOOR — FOD (L4) · airframe 89,062 hrs · 23,189 cycles

SHIP 6809 4L DOOR WILL NOT FULLY ARM. CORRECTIVE ACTION: REMOVED DEBRIS. OPS NML PER B757 AMM 52-11. (4376164)

Part: COVER — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 89,029 hrs · 23,182 cycles

SHIP 6809 2L DOOR WOULD NOT ARM ON DEPARTURE. CORRECTIVE ACTION: FOUND SLIDE COVER NEED TO BE ADJUSTED, ARM DOOR FEW TIMESE OK FOR SVC IAW B757 AMM 52-11. (4376160)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 88,968 hrs · 23,168 cycles

SHIP 6809 3 EMERGENCY LIGHTS IN AFT CABIN INOP. CENTER AISLE OVERHEAD, L3 SIDE EXIT, R3 EXIT SIGN. CORRECTIVE ACTION: FOUND BATTERY PACK OVERHEAD AT 3L BAD.EQUIPMENT M735. REMOVED AND REPLACED EMERGENCY BATTERY PER B757 AMM 33-51. OPS CHECKED GOOD. (4376113)

Part: HANDLE — STUCK (L1 DOOR) · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 STUCK 1L DOOR SLIDE ARM HANDLE. CORRECTIVE ACTION: GIRT BAR MECHANISM ADJUSTMENT HAS BEEN ACCOMPLISHED THE SYSTEM IS OK B757-200 AMM 52-11-25. (5593088)

Part: SKIN — CORRODED (BS 680-760 S3L&R) · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON SEVERAL POINTS BTW STA 680 TO STA 760 AND BTW S-3R TO S-3L ALSO DETERIORATION OF PROTECTIVE TREATMENT ON EXTERNAL DOUBLER. CORRECTIVE ACTION: SUMMARY OF NRC 00526: GO GO KU EXTERNAL DOUBLER WAS REPAIRED PER ER/A 617006-14 REV. ORIGINAL SECTION I. PERMANENT REPAIR.

Part: SKIN — DAMAGED (LT WING) · airframe 88,964 hrs · 23,166 cycles

AIRCRAFT 6809, LOOSE FASTENERS NBR 13 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT LH WING UPPER SKIN DRAG FITTING. (IN REF AMDS 5720-01100-02A STEP 13). CORRECTIVE ACTION: LH WING UPPER SKIN DRAG FITTING HOLE #13 WAS REPAIRED PER ER/A 616812-14AD REV. ORIG SECTION I: REPAIR INSTRUCTIONS IN REF NRC 00435. (LP 0313950)

Part: SKIN — DAMAGED (LT WING) · airframe 88,964 hrs · 23,166 cycles

AIRCRAFT 6809, LOOSE FASTENER NBR 3 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT LH WING UPPER SKIN DRAG FITTING. (IN REF AMDS 5720-01100-02A STEP 12). CORRECTIVE ACTION: LH WING UPPER SKIN DRAG FITTING HOLE #3 WAS REPAIRED PER ER/A 616812-14AD REV. ORIG SECTION I: REPAIR INSTRUCTIONS IN REF NRC 00398 PER ER/A 616812-14. (LP0313953)

Part: SKIN — CRACKED (BS 1220 S4L) · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 ERA 472891-14AD, FUSELAGE / SKIN / STA 1220, STR 4L / SKIN REPAIR / INSPECTION. CORRECTIVE ACTION: REF ERA 472891-14AD. (0313439)

Part: DRAG FITTING — DAMAGED · airframe 88,964 hrs · 23,166 cycles

AIRCRAFT 6809, DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON SKIN BTW 1 TO 2 O CLOCK POSITION, HOLE #2 CORROSION ON SKIN AND FITTING BTW 9 TO 6 O CLOCK POSITION, HOLE #4 CORROSION ON SKIN AND FITTING IN THE HOLE (ALL), HOLE #5 CORROSION ON SKIN AND FITTING BTW 9 TO 11 O CLOCK POSITION, HOLE #7 CORROSION ON SKIN AND FITTING IN THE HOLE (ALL), HOLE #8 CORROSION ON SKIN AND FITTING BTW 8 TO 2 O CLOCK POSITION, HOLE #9 CORROSION ON SKIN AND FITTING BTW 2 TO 4 O CLOCK POSITION AND HOLE #10 GOUGE ON FITTING BTW 2 TO 8 O CLOCK POSITION IN REF. CARD 5720-011-00-04A JOB 131-0001. STEP 14. C. CORRECTIVE ACTION: LH ENG DRAG FTG CLAMP-UP & DIAG BRACE HOLE #1, HOLE #7, HOLE #8 AND HOLE #10 WERE REPAIRED PER CARD 5720-011-00-04A AND HOLE #2, HOLE #4, HOLE #5 AND HOLE #9 WERE REPAIRED PER PRI 616812-14 REV 5 AND ER/A 616812-14 AD REV. ORIG SECTION I: REPAIR INSTRUCTIONS. (LP 0313508)

Part: DRAG FITTING — DAMAGED (LT WING) · airframe 88,964 hrs · 23,166 cycles

AIRCRAFT 6809, DURING H CHECK MAINTENANCE VISIT AT MX (QRO), WHILE ACCOMPLISHING INSPECTIONS ON THE LH WING, FORWARD DRAG FITTINGS PER EM 5720-01100-04A & EM 5720-01100-05A DAMAGE INDICATION WAS FOUND ON WING SKIN AND FITTING LAYER ON HOLES #2-#5, #7-#9, #12, #18, AT FITTING LAYER ON HOLE #10 & #11 AND AT WING SKIN ON HOLE #1. AFTER THE 1ST OVZ DAMAGE REMAINS ON HOLES #2-#5, #9, #13 & #14. CORRECTIVE ACTION: CAREFULLY REAM DISCREPANT HOLE(S) CONCENTRICALLY THROUGH THE STACK UP TO 2ND OVERSIZE (0.5932-0.5942-INCH DIAMETER). INSPECT THE HOLE LOCATION USING HFEC OPEN HOLE INSPECTION TECHNIQUES PER 757 NDTM, PART 6, 51-00-16, USING AN 0.020 INCH NOTCH SENSITIVITY. FABRICATE SOLID SHIMS, AND INSTALL REPAIR PARTS PER ER/A 616812-14AD. (LP 0313695)

Part: SKIN — DAMAGED (LT WING) · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 DTE, ERA 616812-14, LHS UPPER SKIN &FITTING AT FWD DRAG FITTINGS HOLES CORROSION. CORRECTIVE ACTION: REF ERA 616812-14AD.

Part: SKIN — CORRODED (BS 960-1000) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

AIRCRAFT 6809, DURING H CHECK MAINTENANCE, HE WING CENTER BOX SKINS P/N 111N3101 & P/N 111N3102-4 AT STA 960 & STA 1000 AND BETWEEN RBL 59.00 & RBL 64.00 WERE FOUND CORRODED. THE MRT IS OUT OF AP57.2-0602 SRM 57-10-01 ADL DUE TO MORE THAN 0.028 INCHES OF MATERIAL WAS REMOVED. CORRECTIVE ACTION: 2 ENSURE THE CORROSION HAS BEEN BLENDED SMOOTHLY. PERFORM A DETAILED VISUAL INSPECTION PER B757-200 SRM 51-10-08 TO ENSURE THAT NO ADDITIONAL DAMAGE EXISTS ON BLENDED AREAS AND SURROUNDINGS. 4 PERFORM AN HFEC INSPECTION PER B757 NDT MANUAL PART 6, 51-00-01 OF THE BLENDED AREA TO ENSURE THAT NO CRACK EXISTS. TRIM OUT THE UPPER SKIN AS REQUIRED TO REMOVE THE DAMAGE AS SHOWN IN FIGURE 5, ENSURING TO REMOVE ALL BLENDED UPPER SKIN AREAS. FABRICATE SKIN, INTERNAL FILLERS, NAD INTERNAL DOUBLERS AND TRIPLERS AND FABRICATE EXTERNAL DOUBLER AND TRIPLER AND INSTALL PER ER/A 617062-14. (LP 0312142)

Part: FRAME — CRACKED (BS 1640 S14L) · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 FUSELAGE / FRAME / LHS BS 1640 / S-14L / UPPER I/B & O/B HOLES / CRACK DTE ERA 616689-14. REF ERA 616689-14AD. (0310451)

Part: TEE ANGLE — CORRODED (BS 1240 R/LBL10) · corrosion level 2 · airframe 89,451 hrs · 23,272 cycles

SHIP 6809 CORROSION ON FWD SETTLEMENT AREA OF ACCESS PANEL197NL. CORRECTIVE ACTION: SUMMARY OF NRC 00596: FUSELAGE FAIRING STRUCTURE CHORD TEE AT STA 1240 BTW RBL 10 TO LBL 10 WAS REPAIRED PER ER/A 616892-14 REV ORIGINAL SECTION I: PERMANENT REPAIR (0302949)

Part: PLATE — CORRODED (BS 1410-1530) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON LH SIDE PLATE SECTION STA Y= 1410-1530 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00197: CORROSION ON LH SIDE PLATE SECTION STA Y=1410-1530 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT (C2) WAS REMOVED PER B757-200 SRM. MEASUREMENT THICKNESS WAS ACCOMPLISHED ON LH SIDE PLATE SECTION STA 1466-1504 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT (C2). AREA IS WITHIN LIMITS PER B757-200 SRM-53-00-53-1A-1. MEASUREMENT THICKNESS WAS ACCOMPLISHED ON LH SIDE PLATE SECTION STA Y=1410-1466 AND STA 1504-1529 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT AND WAS FOUND OUT OF LIMITS PER B757-200 SRM-53-00-53-1A-1. AREAS OUT LIMITS WERE REPAIRED PER B757-200 SRM. (0300851)

Part: FLOOR SUPPORT — CORRODED (BS 1470-1510) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 EXFOLATION CORROSION ON FLOOR STRINGER SUPPORTS STA 1470 RBL=16, STA 1510 LBL=7, AND RBL=7 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00621: FLOOR STRINGER SUPPORTS STA 1495 TO 1548 LBL=7, AND RBL=7 AT AFT CARGO COMPARTMENT WERE REPAIRED PER B757-200 SRM 53-00-53-2R REPAIR 1 AND FLOOR STRINGER SUPPORTS STA 1445 TO 1505 RBL=16, WAS FABRICATED PER DWG 146N5447 REV C AND INSTALLED PER B757-200 SRM. (0299508)

Part: FLOORBEAM — CORRODED (BS 1440) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 SECONDARY NRC IN REF TO NRC 209: AFTER REMOVAL CORROSION ON FLOOR SUPPORT LBL=2, LBL=15 RBL=3, RBL=8 STA 1469, LBL=7 STA 1640, WERE FOUND OUT LIMITS AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00683: FLOOR SUPPORT LBL=2, LBL=15 RBL=3, RBL=8 STA 1469, LBL=7 STA 1640 WERE REPAIRED PER B757-200 SRM. (0299261)

Part: SEAT TRACK — CORRODED (BS 690) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON OUTB RH SEAT TRACK FLOOR SEATLEMENT REA BTW STA 690. CORRECTIVE ACTION: SUMMARY OF NRC 00551. AREA WAS REPAIRED PER ER/A 617088-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (0297295)

Part: PLATE — CORRODED (S 1530-1640) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON LH SIDE PLATE SECTION STA Y= 1530-1640 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY OF NRC 00198. LH SIDE PLATE SECTION STA Y=1530-1640 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (0295124)

Part: SPLICE — CORRODED (BS 1442) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 SECONDARY NRC IN REF NRC 00199: HIDDEN CORROSION ON SPLICE OF SIDE PLATE STA. 1442 AND RBL 18 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00618: SPLICE OF SIDE PLATE STA . 1442 AND RBL 18 AT AFT CARGO COMPARTMENT WAS FABRICATED PER DWG 146N5391 REV. U.AND INSTALLED PER B757-200 SRM. (0287855)

Part: SKIN — CRACKED (R2 DOOR) · airframe 88,964 hrs · 23,166 cycles

CRACK SKIN ON UPPER HINGE CUT OUT AREA AT 2R PASSENGER DOOR. SKIN ON UPPER HINGE CUT OUT AREA AT 2R PASSENGER DOOR. WAS REPAIRED PER B757-200 SRM 52-10-02-2R PROCEDURE 1, REPAIR 1.

Part: PLATE — CORRODED (BS 1440-1530) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON RH SIDE PLATE SECTION STA Y= 1440-1530 UPPER/LOWER SURFACE AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00199 SIDE PLATE ON SECTION STA Y=1440-1530 RH SIDE AT AFT CARGO COMPARMENT.WAS REPLACED PER B757-200 SRM 51-40-02. (0287461)

Part: PLATE — CORRODED (BS 1310-1380) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON RH SIDE PLATE FROM STA 1310- 1380 (UP/LWR SURFACE) AT AFT CARGO COMPARMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00131: SIDE PLATE FROM STA 1310 -1380 RH SIDE AT AFT CARGO COMPARMENT WAS REPLACED PER B757-200 SRM. (0285962)

Part: SNUBBER — OUT OF TOLERANCE (R4 DOOR) · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 IN REF. TASK 5211-3001-4R STEP 3: R4 ROTARY SNUBBER PIN EXTENSION WAS FOUND OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00627: R4 ROTARY SNUBBER WAS REMOVED AND REPLACED BY A NEW ROTARY SNUBBER PER B757-200 AMM 52-11-10 AND ADJUST AT THE SAME DOOR R4 PERFORM ON AMDS. (0287340)

Part: PANEL — CORRODED (BS 1380-1440) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON LOWER SEAL PANEL AREA (UPPER AND LOWER SURFACE) BTW STA 1380 TO STA 1440 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00275. LOWER SEAL PANEL WAS REPLACED PER DWG 146N5391-92 REV. F AND B757-200 SRM. (0287036)

Part: FLOOR SUPPORT — CORRODED (BS 324-331 RBL45) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON INTERCOSTAL BETWEEN STA 324/ STA 331 AND RBL 45 AT FLOOR STRUCTURE OF CABIN PAX. CORRECTIVE ACTION: SUMMARY OF NRC 00537: INTERCOSTAL WAS REPLACED PER B757-200 SRM. (0285386)

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 IN REFERENCE TO NRC 00470: AFTER CORROSION REMOVAL, FLOOR BEAM STA 1640 BTW LBL 37 TO RBL 26 WAS FOUND OUT OF LIMITS AT FLOOR STRUCTURE OF CABIN PAX W4. CORRECTIVE ACTION: SUMMARY OF NRC 00584: FLOOR BEAM STA 1640 BTW LBL 37 TO RBL 26 WAS REPAIRED PER B757-200 SRM 53-00-51-2R. (0279311)

Part: FLOORBEAM — CORRODED (BS 324 RBL 45-67) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 5809 CORROSION ON FLOOR BEAM BETWEEN STA 324 AND RBL 45/ RBL 67 TO FLOOR STRUCTURE OF CABIN PAX (W1). CORRECTIVE ACTION: SUMMARY OF NRC 00536: FLOOR BEAM BETWEEN STA 324 AND RBL 45/ RBL 67 WAS REPAIRED PER B757-200 SRM 53-10-08-2R PROCEDURE 1 REPAIR 1. (0275831)

Part: STRAP — CORRODED (BS 775-800 RBL25) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON STABILIZER TRAP ON FWD CARGO COMPARTMENT CEILING STRUCTURE BTW STA 775 AND 800 ON RBL 25. CORRECTIVE ACTION: SUMMARY OF NRC 00245: STABILIZER STRAP ON FWD CARGO COMPARTMENT CEILING STRUCTURE BTW STA 775 AND 800 ON RBL 25 WAS REPAIRED PER B757-200 SRM 53-00-51-2R PROCEDURE 13. (0275196)

Part: INTERCOSTAL — CORRODED (BS 1660-1681 BL0) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON INTERCOSTAL BETWEEN STA 1681.8/ STA 1660 AND BL 0 AT FLOOR STRUCTURE OF CABIN PAX W4. INTERCOSTAL BETWEEN STA 1681.8/ STA 1660 AND BL 0 AT FLOOR STRUCTURE OF CABIN PAX W4 WAS REPLACED PER B757-200 SRM. (0273349)

Part: SEAT TRACK — CORRODED (BS 1620-1640) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 SECONDARY NRC IN REF. NRC 00177: CORROSION OUT OF LIMITS ON LH INBOARD SEAT TRACK STA 1620-1640 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00572: SEAT TRACK LH INBOARD STA 1640 TO 1540 WAS REPLACED PER B757-200 SRM. (0268777)

Part: SEAT TRACK — CORRODED (BS 1640) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 IN REF. NRC 173: CORROSION OUT OF LIMITS ON RH SEAT TRACK OUTBOARD SEAT TRACK STA 1640. CORRECTIVE ACTION: SUMMARY OF NRC 00602. SEAT TRACK RH OUTBOARD BTW STA Y= 1540 TO STA Y= 1640 WAS REPLACED PER B757-200 SRM. (0268829)

Part: FLOORBEAM — CORRODED (BS 378 LBL 63) · corrosion level 2 · airframe 88,964 hrs · 23,166 cycles

SHIP 6809 CORROSION ON FLOOR BEAM STA Y=377.7 LBL=63 AT PAX. CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00054 , FLOOR BEAM STA Y= 377.7 LBL=63 AT PAX. CABIN WAS REPAIRED PER B757-200 SRM 53-00- 51-2R PROCEDURE 8 REPAIR 8. (0267203)

Part: STRUCTURE — UNSECURE (SLIDING WINDOW) · airframe 87,582 hrs · 22,863 cycles

DURING INSPECTION FOUND R3 WINDOW WILL NOT OPEN FULLY BLOCKING EGRESS. CORRECTIVE ACTION: RE-SECURED TRIM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,967 hrs · 22,733 cycles

EMERGENCY LIGHT BATTERY PACK FOR M735 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,967 hrs · 22,733 cycles

EMERGENCY LIGHT BATTERY PACK FOR M736 INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY PACK. SYSTEM OPERAITON IS NORMAL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,967 hrs · 22,733 cycles

EMERGENCY BATTERY PACK M10919 INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 86,892 hrs · 22,718 cycles

FOUND R2 DOOR SLIDE GAUGE IND AT RED. R/R R2 DOOR SLIDE PER WORK CARD 2566-9001-2R. ALL STEPS COMPLIED WITH.

Part: LANYARD — UNSECURE (L4 DOOR) · airframe 86,268 hrs · 22,589 cycles

L4 DOOR HAS GREEN LANYARD EXPOSED. RESTOWED MOORING LANYARD.

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 85,635 hrs · 22,458 cycles

L HYD QTY EICAS MESSAGE WITH L RSVR LIGHT ILLUMINATED. HYD Q READS .47 AT THAT POINT. 0.39 AFTER 5-10 MINTUTES. SHUT OFF L ENG HYD PUMP PER MCC. DECREASED TO .30. SHUT OFF L ELEC HYD PUMP PER MCC AS WELL. DECREASING STOPPED AT .30. CORRECTIVE ACTION: INSPECTED FOUND NBR 5 SPOILER PCA LEAKING. REMOVED NBR 5 SPOILER PCA REF B757 AMM 27-61. INSTALLED NBR 5 SPOILER REF B757 AMM 2761. OPS CK AND LEAK CK GOOD. ALL RII STEPS C/W

Part: INTERROGATOR — FAILED (DME) · airframe 84,513 hrs · 22,249 cycles

LEFT DME CIRCUIT BREAKER POPPED. FOLLOWED BY ACRID SMELL IN COCKPIT. REMOVED AND REPLACED DME INTERROGATOR PER B757 AMM 34-55.

Part: LANYARD — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 84,285 hrs · 22,206 cycles

NOT ABLE TO ARM R1 DOOR PRIOR TO PUSHBACK. ADJUSTED 1R DOOR LANYARD. REVIEWED, MEETS MCC RAM LEVEL 1 CRITERIA.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 84,360 hrs · 22,219 cycles

R1 DOOR DIFFICULT TO ARM. REMOVED R1 DOOR BUSTLE. RE-STOWED SLIDE PACK LANYARD. OPERATED DOOR SEVERAL TIMES OPS CKED OK. (1210909)

Part: GIRT BAR — FOD (R1 DOOR SLIDE) · airframe 84,285 hrs · 22,206 cycles

R1 DOOR WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR. OPS CHECK NORMAL. OK FOR SVC.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 84,237 hrs · 22,197 cycles

DOOR 1R WILL NOT ARM. REMOVED OBSTRUCTION FROM GIRT BAR ENGAGEMENT AREA + SECURED LANYARD. DOOR OPS CHK IAW B757 AMM 25-66. OPS CHK OK AC.

Part: ATTACH FITTING — FOD (R1 GIRT BAR) · airframe 83,489 hrs · 22,062 cycles

R1 DOOR HANDLE WONT FULLY ARM. REMOVED DEBRI FROM GIRT BAR ATTACHED FITTING-ARMED DOOR. CHECKS OK.

Part: D-RING — OUT OF POSITION (R1 DOOR) · airframe 83,282 hrs · 22,026 cycles

(AIRCRAFT 6809, L/P 5560284) PRIOR TO PUSHBACK, FA'S REPORT UNABLE TO ARM THE 1R DOOR. REPOSITIONED AND RESECURED THE D-RING SURVIVAL KIT ATTACHMENT STRAP PER AMM 25-66. 1R DOOR ARMS AND DISARMS NORMALLY.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 83,000 hrs · 21,974 cycles

SHIP 6809 R FWD ENT DOOR WON'T ARM. CORRECTIVE ACTION: REMOVED DEBRIS OF R1 DOOR GIRT BAR OPS CHK NML. (5534174)

Part: STRAP — UNSECURE (R1 DOOR) · airframe 82,571 hrs · 21,896 cycles

FA UNABLE TO ARM 1R DOOR. RESTOWED GREEN STRAP. DOOR ARMS NORMAL AMM 52-11.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 82,511 hrs · 21,885 cycles

F/A UNABLE TO ARM 1R DOOR. REMOVED DEBRIS FROM 1R GIRT BAR. 1R SLIDE ARM ALL OPS CHECK GOOD PER B757 AMM 52-11.

Part: STRAP — EXPOSED (R1 DOOR SLIDE) · airframe 82,480 hrs · 21,879 cycles

DOOR 1R WILL NOT ARM SLIDE STRAPS EXPOSED. CORRECTIVE ACTION: RE-STOWED GREEN ROPE AND RING AT BOTTOM OF SLIDE. NOW LISE ARS NML. (5557724)

Part: LINE — UNSECURE (L1 DOOR) · airframe 82,418 hrs · 21,866 cycles

SHIP 6809 L-1 DOOR HAS GREEN CORD PULLED OUT OF DOOR SLIDE. CORRECTIVE ACTION: RESURED MOORING LINE REF AMM 25-66 AND W/C. (5525278)

Part: ROPE — OUT OF ADJUST (R2 DOOR) · airframe 81,649 hrs · 21,712 cycles

SHIP 6809 2R DOOR WILL NOT ARM. CORRECTIVE ACTION: RE-STORED ROPE AND RING UNDER SLIDE. OPS NML. (3741658)

Part: O-RING — LEAKING (SPOILER SYS) · airframe 81,462 hrs · 21,676 cycles

SHIP 6809 - ALT GEAR EXT - DECLARED AN EMERGENCY INTO JFK DUE TO LT HYD SYS QUANTITY DECREASING. CORRECTIVE ACTION: #5 SPOILER O-RING VALVE CAP LEAKING. REPLACED O-RING, AND PTU AS PRECAUTIONARY.

Part: INDICATOR — INOPERATIVE (DOOR ARMED) · airframe 81,050 hrs · 21,599 cycles

(AIRCRAFT 6809, L/P 0825928) DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:607 / DISARMED PLACARD LOOSE. / INTERIOR. R/R DISARMED PLACARD ASSY. OPS CHECK NORMAL PER B757 AMM 52-11.

Part: HANDLE — OUT OF POSITION (ENTRY DOOR) · airframe 80,793 hrs · 21,550 cycles

DURING CLIMB THOUGH FL 220, L AFT DOOR HANDLE MOVED OUT OF SECURE POSITION WITH ASSOCIATED L AFT ENTRY DOOR EICAS MESSAGE. LT AFT DOOR OPENED AND CLOSED SEVERAL TIMES NO PROBLEMS FOUND. AFT LT DOOR LOCKED AND ARMED AND DISARMED WITHOUT REMARKS. OK AT THIS TRANSIT REF AMM 52-12-00.

Part: SWITCH — INOPERATIVE (LAVATORY) · airframe 80,212 hrs · 21,443 cycles

FWD LAV OCCUPIED LIGHT SHORTED AND BURNED OUT MCC/0630Z. VERIFIED LIGHT BURNED OUT. NO SIGNS OF SHORTING OR ARCING IN LIGHT SOCKET OR BEHIND PANEL. TRIED RELAMP NO HELP. REMOVED AND REPLACED FWD LAV LOCK SWITCH PER WDM 33-26-21. OCCUPIED LIGHT CHKS GOOD.

Part: LIGHT — SPARKS (LAVATORY) · airframe 80,121 hrs · 21,426 cycles

(AIRCRAFT 6809, L/P 4832874) FWD LAV OCCUPIED LT EMITS SPARKS WHEN ITS TURNED TO DIM. OPERATED DOOR MULTIPLE TIMES. NO FAULTS FOUND. UNABLE TO DUPLICATE FAULT. NO SPARKS SEEN AT LAV OCCUPIED LIGHT. OK FOR SVC.

Part: HANDLE — UNSECURE (L4 DOOR) · airframe 79,807 hrs · 21,369 cycles

APPROXIMATELY 3 HOURS INTO THE FLT, AN EICAS CAUTION LIGHT AFT ENT DOOR ILLUM. QRH FOLLOWED, ASKED F/A TO CHECK THE DOOR SECURITY. THE HANDLE WAS UP 2 OR 3 INCHES ON THE AFT ENTRY DOOR HANDLE, PUSHED BACK DOWN AND EICAS MESSAGE ELIMINATED. PRESSURIZATION NORMAL THROUGHOUT. COMPLIED WITH DOOR INSPECTION IAW AMM 52-11-00-206-021, OPS CHECKED AND INDICATION NORMAL.

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 78,234 hrs · 21,078 cycles

ATB DUE TO LOSS OF RT GENERATOR. APU WAS ON MEL. CREW FOLLOWED QRH PROCEDURES, NO EMERGENCY WAS NOT DECLARED. CONTACTED DISPATCH AND MC AND INITIATED ATB. BPCU FAULT IDG LOW OIL PRES/IDG HIGH RISE TEMP. REPLACED RIGHT IDG PER AMM. OPS CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: GIRT BAR — DISLODGED (L1 DOOR) · airframe 76,922 hrs · 20,810 cycles

AT PUSHBACK, WHEN THE L1 DOOR WAS CLOSED. THE GIRT BAR FELL IN TRACK AT BASE OF DOORS AND JAMMED. DISLODGE THE GIRT BAR.

Part: BRACKET — BROKEN (E/E BAY) · airframe 75,199 hrs · 20,476 cycles

FIRST OFFICER`S SIDE BRACKET BROKEN. REMOVED DAMAGED BRACKET. FABRICATED A NEW BRACKET IAW DRAWING 284N1029, AND INSTALLED.

Part: HANDLE — OBSTRUCTED (L1 DOOR) · airframe 75,022 hrs · 20,442 cycles

PRIOR TO DEPARTURE L1 DOOR KNUCKLE KNOCKER WAS DEPRESSED AFTER DOOR WAS ARMED. ALL OTHER INDICATIONS WERE NORMAL. CLEANED AND LUBED GIRT BARS. REMOVED OBSTRUCTION FROM KNOCKER. OPS NORMAL. OK FOR SERVICE.

Part: BOLT — UNSECURE (R2 DOOR) · airframe 74,740 hrs · 20,393 cycles

R2 DOOR KNUCKLE KNOCKER DOES NOT EXTEND WHEN DOOR ARMED. ALL OTHER ARMING INDICATIONS NORMAL. FOUND LOOSE SHOULDER BOLT ON MECHANISM THAT OPENS & CLOSES KNUCKLE KNOCKER. SECURED THE BOLT. OPS CHECKED NORMAL.

Part: HINGE — DAMAGED (R4 DOOR) · airframe 74,235 hrs · 20,304 cycles

R4 DOOR DAMAGED UPPER HINGE. REMOVED R4 PASSENGER DOOR, REINSTALLED NEW R4 PASSENGER DOOR. OPS CHECK NORMAL. PRESSURIZED A/C TO 4 PSI NO LEAKS NOTED. DOOR OPS NORMAL DURING PRESSURIZING REF AMM 52-11-00-825-001.

Part: GUARD — OUT OF POSITION (LIGHT SWITCH) · airframe 73,979 hrs · 20,246 cycles

EMERGENCY LIGHTS DO NOT COME ON WHEN SELECTING ON. POSITIONED EMERGENCY LIGHT SWITCH GUARD. PERFORMED OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51. OPS TESTED GOOD. ACFT OK FOR SERVICE.

Part: GIRT BAR — DAMAGED (R1 DOOR) · airframe 73,709 hrs · 20,176 cycles

R1 DOOR GIRT BAR FWD SLIDER FAILED DURING TEST. INSTALLED A NEW GIRT BAR.

Part: SKIN — DENTED (BS 620) · airframe 73,709 hrs · 20,176 cycles

DENT ON FUSELAGE SKIN AT BS 620, BETWEEN STRINGERS 16 & 17L. ACCOMPLISHED A PERMANENT REPAIR IAW ER/A 555993-14, REV ORIG.

Part: SHEAR TIE — DENTED (BS 620) · airframe 73,707 hrs · 20,175 cycles

FOUND SHEAR TIE DENTED AT BS 620 BETWEEN STRINGERS 16 - 17L. FABRICATED A NEW SHEAR TIE IAW DWG. REMOVED AND REPLACED THE SHEAR TIE IAW SRM.

Part: GIRT BAR — NO TEST (R4 DOOR) · airframe 73,707 hrs · 20,175 cycles

R4 DOOR GIRT BAR, AFT SLIDER FAILED DURING TEST. REPLACED THE R4 DOOR GIRT BAR.

Part: BRACKET — CRACKED (R2 DOOR SLIDE) · airframe 73,707 hrs · 20,175 cycles

DISCOVERED AFT END OF THE R1 DOOR SLIDE, UPPER HANGER BRACKET CRACKED. REPLACED THE R1 DOOR SLIDE.

Part: SKIN — CRACKED (LT WING) · airframe 73,707 hrs · 20,175 cycles

LT WING FIXED LE UPPER SURFACE HAS CRACKED AT WS 459350. ON LT WING FIXED LE UPPER SURFACE REPAIRED CRACKED AREA AT WS 459.50 IAW ER/A 401605-14MA REV L AND SRM.

Part: SKIN — CRACKED (LT WING) · airframe 73,707 hrs · 20,175 cycles

LT WING FIXED LE UPPER SURFACE HAS CRACKED AT WS 397.50. ON LT WING FIXED LE UPPER SURFACE REPAIRED CRACKED AREA AT WS 397.5 IAW ER/A 401605-14MA REV L AND SRM.

Part: HANDLE — OUT OF POSITION (L4 DOOR) · airframe 71,883 hrs · 19,796 cycles

L4 DOOR WOULD NOT CLOSE AND ARM. DOOR WAS OPENED AND CLOSED BY FLIGHT ATTENDANT. STILL INDICATES IT WAS NOT ARMED. (NO LIGHT) ARMED THE HANDLE AND NOT IN CORRECT POSITION. PILOT CAME BACK AND VERIFIED INDICATIONS. CAPTAIN OPENED DOOR AND SLIDE BLEW. ARMED AND CYCLED L4 DOOR SEVERAL TIMES. FOUND DOOR INTERIOR PANEL LOOSE CAUSING HANDLE TO STICK. SECURED THE PANEL. HANDLE NOW HAS CLEARANCE FROM LOWER DOOR LINEING, OPS GOOD NOW. R & R THE L4 DOOR SLIDE IAW AMDS WORK CARD 2566-9001-4L. R & R THE L4 DOOR EMERGENCY POWER RESERVOIR IAW AMM 52-11-30. REPLACED THE LAMP IN THE SLIDE LIGHT.

Part: SEAL — DIRTY (R4 DOOR) · airframe 69,319 hrs · 19,309 cycles

TOP OF 4R DOOR FROZEN WITH ICE INTERIOR. PERFORMED INSPECTION OF 4R DOOR. CLEARED DEBRIS FROM SEAL AREA. CHECKED OPERATION OF 4R IAW AMM 52-11.

Part: PANEL — CRACKED (LT WING) · airframe 73,751 hrs · 20,186 cycles

INSPECTION REPORTED A CRACK BETWEEN WSTA 285 AND WSTA 313 ON LT WING FUEL TANK AUXILIARY STRUCTURE DRY BAY BARRIER PANEL. REF ERA 532885-14 REV A. REF LOG PAGES 1919279 AND 2961772.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 64,961 hrs · 18,487 cycles

C-1 DOOR AFT EDGE BEAM IS GOUGED AND DENTED BETWEEN DOOR STOPS, 2ND & 3RD FROM THE BOTTOM. CUT OUT DAMAGED AREA AT C-1 DOOR AFT EDGE BEAM BETWEEN STOPS 2 AND 3 IAW SRM 52-30-02 AND 51-70-11 FIG 1, FAB ANGLE REPAIR FILLER AND INSTALLED IAW SRM 51-70-11, FIG 1 AND 51-40-02. LP 1915459.

Part: SKIN — DAMAGED (NR 5 SLAT) · airframe 64,961 hrs · 18,487 cycles

NR 5 SLAT HAS A SHARP CREASE ON UPPER T/E WEDGE APPROXIMATELY 1.5 LONG. EVALUATED DAMAGE AND FOUND IT TO BE OUT OF LIMITS ON 5 SLAT T/E WEDGE IAW SRM 57-43-02, FIG 101 AND BONDED PERMANENT REPAIR 4.5"DIA IAW SRM 51-70-10, REPAIR 2, ID TAGGED REPAIR IAW DPS 900-5-1, NR 04. LP1916961.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

AFT CARGO COMPT LOWER SILL DOOR THRESHOLD FWD. FITTING HAS CORROSION ON FWD SIDE. R & R FITTING PN 69-4557807, PO 713TA-00257 IAW DWG 69-45578, REV D. INSTALLED FITTING IAW SRM 51-40-02 AND DWG 69-45578, REV D. LP1906543.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

AFT CARGO COMPT. CARGO DOOR LOWER SILL THRESHOLD SECOND FROM AFT. FITTING HAS CORROSION, AND CORRODED NUTPLATES. R & R FITTING, PN 69-4557807, PO 713TA00257 IAW SRM 51-40-02 & DWG 69-45528, REV D. INSTALLED FITTING IAW DWG 69-45578, REV D. LP1906550.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

FOUND CORROSION ON FLOORBEAM AT FS 365 BETWEEN RBL 11 TO RBL 17 PASSENGER CABIN. REMOVED CORROSION AT FLOORBEAM FS 365, RB 11 TO RBL 17 IAW SRM 51-20-01. ORIGINAL MATERIAL 125 REMAINING MAT. 098 MAT LOSS .027. AREA FOUND TO BE OUT LIMIT IAW SRM 53-00-51 FIG 101. CUT OUT DAMAGE SECTION AT FS 365, LBL 9.10 TO RBL 65 IAW SRM 53-00-51. FABRICATED REPAIR PARTS IAW SRM 53-00-51, FIG 201. INSTALLED REPAIR PARTS IAW SRM 53-00-51, FIG 201. ID TAGGED REPAIR IAW PS 900-5-1, NR 04. LP 1899180.

Part: FLOOR SUPPORT — CRACKED (BS 1420-1440) · airframe 64,961 hrs · 18,487 cycles

AFT CARGO CEILING FS 1420-1440 FLOOR SUPPORT STIFFNER CRACKED. BL 0. REMOVED AFT CARGO CEILING STA 1420-1440 FLOOR SUPPORT UPPER ANGLE. INSTALLED ANGLE IAW SRM 53-60-5 & DWG 146N5180, REV A. LP1898213.

Part: LIFE RAFT — MISINSTALLED (PAX CABIN) · airframe 64,961 hrs · 18,487 cycles

MAINTENANCE FOUND THE MAIN PASSEMGER CABIN LIFE RAFT INCORRECTLY PACKED. WHILE REMOVING IT IAW AMDS JOB CARD 2500-4612. THE CABIN SLIDE RAFT WAS REMOVED AND THE INSTALLATION WILL BE ACCOMPLISHED ON AMDS JOB CARD 2500-4208. LP1897753.

Part: FLOOR SUPPORT — CRACKED (BS 1520-1540) · airframe 64,961 hrs · 18,487 cycles

AFT CARGO CEILING FS 1520-1540 CRACKED FLOOR SUPPORT STIFFNER BL 0. R & R AFT CARGO CEILING FS 1520-1540 FLOOR SUPPORT UPPER ANGLE. INSTALLED ANGLE IAW SRM 53-60-05 AND DWG 146N5180, REV A. LP1898222.

Part: STRAP — CRACKED (BS 377) · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN UNDER FLOOR BS 377, LBL 45 STABILIZER STRAP BELOW FRAME IS CRACKED. INSTALLED REPAIRS PARTS IAW SRM 53-00-51, REPAIR 12.

Part: FLOOR SUPPORT — CORRODED (BS 345-365) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN FLOOR SUPPORT BETWEEN FS 345 TO 365, RBL 54 CORRODED. R & R FLOOR SUPPORT PN 141N-5160U78, PO 713TA-00203. INSTALLED FLOOR SUPPORT IAW DWG 141N5160, REV B. LP1895325.

Part: FLOOR SUPPORT — CORRODED (BS 1650) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

AFT MAIN CABIN FLOOR HAS SURFACE CORROSION, STA 1650, RBL 58, JUST INBD OF R-4 DOOR SILL 5" X 2". R & R FLOOR SUPPORT USING PN 146N5246U8, PO 713TA-00238 IAW DWG 146N5246, REV A INSTALLED FLOOR SUPPORT IAW DWG 146N5246, REV A. LP1894362.

Part: FRAME — GOUGED (BS 1280) · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN FRAME AT BS 1280 BETWEEN STR 10 LT TO 13 LT GOUGE ON 2 EA AREAS. BLENDED OUT AREAS AT BS 1280 BETWEEN STRINGER 10LT TO 13LT IAW SRM 51-10-02. COMPLIED FS 1280, LT FRAME REPAIR IAW ERA 532822-14AD, REV 1.

Part: FRAME — GOUGED (BS 1280) · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN FRAME AT BS 1280 BETWEEN STRINGER 10 RT TO 13 RT 2 EA DEEP GOUGES. CREATED FOR REPAIR ID WORK IN PROCESS. LP1891955

Part: FLOORBEAM — CRACKED (BS 1640) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

CABIN FLOOR STRUCTURE STA 1640, RT SIDE OF ACFT JUST FWD OF R4 DOOR HAS CORROSION, UPPER SURFACE, FLOORBEAM UPPER CAP. CUT OUT DAMAGE AREA DIM 31", FABRICATED "T" CHORT USING BAC 1505-100880 PO 707TW-00185, DIM 36", 2 EA SPLICES FROM 7075 "O" .071, PO ST00003441, DIM 7.3750" X 3 AND 7075 "O" .063 PO ST00003441, DIM 9.5" X 3" 2 EA STRAP USING 7075T6.071 PO ST00004231 DIM 7.5" X .8750" AND 7075T6.063, PO ST00004012, DIM 9.2500" X .8750" IAW SRM 53-00-51, REPAIR 8. INSTALLED REPAIR PARTS IAW SRM 53-00-81, REPAIR 8., LP1893544

Part: SKIN — CRACKED (LT WING) · airframe 64,961 hrs · 18,487 cycles

LEFT WING FIXED 4E GAP COVER NOSE SKIN IS CRACKED. C/W LT WING FIXED L/E GAP COVER NOSE SKIN REPAIR IAW ERA 529550-14MA. LP1891143

Part: FLOORBEAM — CORRODED (BS 1660) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN FLOOR STRUCTURE HAS CORROSION JUST INBD OF L-4 DOOR SILL, STA 1660 BEAM. FOUND CORROSION AT MAIN CABIN FLOORBEAM, BS 1660 WITH MATERIAL LOSS .022. OUT OF LIMITS IAW SRM 53-00-51, FIG 101. CUT OUT DAMAGE AREA DIM 26". FABRICATED "T" CHORD USING BAC1505-100880, PO 707TW-00185, DIM 30", 2 EA SPLICES FROM 7075 "O " .071 PO ST00003441, DIM 9.5" X 2.5" & 7075 "O" .063 P.O ST00003441 DIM 11.5" X 2.5", 2 EA STRAPS FROM 7070T6.071 PO ST00003441 DIM 9.5" X 1" AND 7075T6.063, PO ST00003441 DIM 11.5" X 1". HEAT TREATED PARTS FROM "O" CONDITION TO T6 IAW FORM FAS 0115, REV .012. REPAIRS PARTS MADE IAW SRM 53-00-51, REPAIR 8, FIG 201. INSTALLED REPAIR PARTS IAW SRM 53-00-51, REPAIR 8, FIG 201 INSTALLED ID TAG IAW PS 900-5-1, NR 04. LP1891073

Part: PANEL — CRACKED (LT WING) · airframe 64,961 hrs · 18,487 cycles

LT WING DRY BAY PANEL 52 HZ, INSIDE OF FUEL PANEL 541CB, ANTI-CHAFE STRIP IS CRACKED. LOG PAGE CREATED FOR REPAIR ID, WORK IN PROGRESS ASSOCIATED ER/A 14-532885 ADDED FOR AC 6809, LP1908678.

Part: SEAT TRACK — CORRODED (BS 1210) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN SEAT TRACK RBL 24, BS 1210 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 700-780) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN SEAT TRACK LT OTBD, BS 700-780 IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM. R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1240) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN SEAT TRACK, RBL 45 AT BS 1240 WITH A DEEP SPOT OF CORROSION. FOUND OUT OF LIMITS R & R SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1638) · corrosion level 2 · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN SEAT TRACK, LBL 45 AT BS 1638, CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM.

Part: STRINGER — DENTED (BS 520) · airframe 64,961 hrs · 18,487 cycles

MAIN CABIN STR 16L IS DAMAGED FROM EXISTING DENT ON EXTERNAL SKIN, STA 520. FABRICATED NEW STR SECTION DIM: 13" AND 2 EA SPLICES DIM: 9.3750, AND 4 EA SHIM DIM: 9.3750, AND INSTALLED REPAIR PARTS IAW SRM 53-00-03, FIG 201, REP 1.

Part: SKIN — DENTED · airframe 64,479 hrs · 18,370 cycles

DENT ON LT SIDE OF FUESLAGE ABOUT 15FT FWD OF L2 DOOR. REPAIRED IAW ERA 532692-14.

Part: LIGHT — DAMAGED (CABIN) · airframe 64,256 hrs · 18,316 cycles

EMERGENCY LIGHT AT 2R GALLEY DAMAGED. REPLACED LIGHT ASSY IAW AMM 33-52. OPS NORMAL.

Part: UNKNOWN — SMOKE (CABIN) · airframe 64,256 hrs · 18,316 cycles

WHILE ENROUTE AT CRUISE, THE DOOR 2L LAV SMOKE DETECTOR ACTIVATED AND A THIN LAYER OF SMOKE DEVELOPED IN THE CABIN. SMOKE LATER DISSIPATED. CREW COMPLETED THE QRH FOR SMOKE, FIRE OR FUMES. CREW ELECTED TO DIVERT. EMERGENCY DECLARED AND DISPATCH AND MC WERE NOTIFIED. OXYGEN MASKS WERE NOT REQUIRED, NO SMOKE OF FUMES EVIDENT IN COCKPIT. MAINTENANCE PERFORMED A HIGH POWER ENGINE RUN AND DETERMINED THE NR 1 ENGINE TO BE SOURCE OF THE SMOKE. ENGINE WAS REPLACED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,008 hrs · 16,882 cycles

EXTERIOR EMERGENCY LIGHTS DO NOT OPERATE. REPLACED LAMPS. OPS CHECKED GOOD. IAW AMM 33-50.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 55,482 hrs · 16,580 cycles

EMERGENCY TEST FOUND L1 DOOR AND G1 EXIT SIGNS ALSO FOUND RED PATH LIGHTS FOR R1 AND G2 INOPERATIVE. T/S IAW WDM 33-51-12 FOUND BATTERY PACK M731 TO BE THE COMMON LINK BETWEEN THOSE LIGHTS. R & R BATTERY AND CHARGER. M731 IAW AMM 33-51. NO HELP FOUND NR 2 FUSE CONNECTED TO PINS 11-12. OPEN REPLACED FUSE, MPN 251005L IT BLEW AFTER 3 SECS. FOUND MID GALLEY AFT SIDE RED EPATH LIGHT WIRES CHAFING REPLACED SAME LIGHT ASSY, OPS NOW NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,985 hrs · 16,483 cycles

THE EMERGENCY EXIT SIGN ABOVE L1 DOOR INOPERATIVE. R & R F2 FUSE AT POWER SUPPLY M731. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,589 hrs · 16,403 cycles

EMERGENCY EXIT SIGN ABOVE L1 DOOR INOPERATIVE. FOUND BATTERY PACK M731 FAULTY. REPLACED BATTERY PACK IAW AMM 33-51 CHECKED GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,300 hrs · 16,348 cycles

DURING EMERGENCY LIGHTS TEST, FOUND LT DOOR EXIT OVERHEAD SIGN OUT AND GALLEY 1A EMERGENCY EXIT LIGHT OUT. FOUND EMERGENCY LIGHT POWER SUPPLY M0731 BAD. R & R POWER SUPPLY M0731 IAW AMM 33-5. CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,120 hrs · 16,313 cycles

DURING MAINTENANCE CHECK, FOUND L1 OVERHEAD EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND CHARGER M731 PER IAW 33-51. OPERATION OF LIGHT NOW CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 52,222 hrs · 15,961 cycles

LINE MAINTENANCE FOUND EMERGENCY EXIT SIGN INOPERATIVE AT DOOR 1L. REPLACED POWER SUPPLY, OPERATION NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,516 hrs · 15,256 cycles

DURING A LIGHTING TEST, MAINTENANCE FOUND THE DOOR 1L EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. OPERATIONAL CHECK WAS GOOD.

Part: OIL SYSTEM — LOW (IDG) · airframe 43,526 hrs · 14,301 cycles

RT GEN DRIVE MSG ILLUMINATED IN EICAS/ R DRIVE OVER HEAD. DISCONNECTED RT GEN NOTE RT IDG OIL LEVEL MSG. SERVICED IDG NR 2 ENG IAW MM CHECKED IDG FILTER . FILTER CLEAN. RAN NR 2 ENG AND CHECKED FOR LEAKS IAW MM NO LEAKS NOTED. VOLTS AND FREQ GOOD, ACFT OK FOR SERVICE ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: SLIDE — UNWANTED DEPLOY (CABIN) · airframe 41,999 hrs · 13,990 cycles

R1 DOOR SLIDE INADVERTLY BLOWN BY CABIN SERVICE. DETACHED SLIDE FROM 1R DOOR. DEFLATED SLIDE AND LOADED IN FWD CARGO BIN. VERIFIED PROPER OPEN CLOSE OPERATION OF 1R DOOR. C/W OPN 7893-OPN 9998 OPN 7809. DOOR SLIDE RPLCMNT. RPLD EMERGENCY POWER RESEVOIR IAW TASK 52-11-30-404-013. C/W R11 INSPECTION IAW TOPP 40-30-05. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: DOUBLER — CORRODED (BS 1510 LBL 10) · airframe 39,019 hrs · 13,455 cycles

AFT CARGO FS 1510 LBL 10 AIR PHONE ANTENNA INNER DOUBLER AND NUT PLATE ASSY CORRODED. REMOVED CORROSION AND FABRICATED NEW DOUBLER AT SAA/SAT DURING HMV VISIT ON NR 129454 JOB NUMBER 82598520001.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN FLOORBEAM STA 1640 BL0 TO RBL 59 CORROSION UPPER AND LOWER SURFACES. REPAIRED WITH SPLICE AT SAA/SAT DURING HMV VISIT ON NR 126386 JOB NUMBER 82598850001.

Part: STRUCTURE — CORRODED (BS 365-377) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN LT INNER CUSP CHORD CORRODED ON BOTH LEGS STA 365+3-377+8. REMOVED AND REPLACED CHORD IAW DRW 148N8322 ON NR58710 JOB NUMBER 82599770001.

Part: STRUCTURE — CORRODED (BS 324-377) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN FLOOR RT CUSP INNER CHORD CORRODED ON BOTH LEGS STA 324-377 RBL 64. REPLACED CHORD AT SAA/SAT DURING HMV VISIT ON NR 126393 JOB NUMBER 82599190001.

Part: CUSP WEB — CORRODED (BS 1340) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN FLOOR INNER CUSP CORD HAS NUMEROUS AREAS OF CORROSION AND SCRIBE LINE IN RADIUS STATION 1340-1380 LT LBL - 58 REMOVE AND REPLACED CHORD IAW BAC DRW 146N83601 ON NR 58510 AT SAT/SAA DURING HMV VISIT JOB NUMBER 8260132001.

Part: SEAT TRACK — CORRODED (BS 1540-1640) · airframe 39,019 hrs · 13,455 cycles

CABIN SEAT TRACK GOUGED SEVERAL AREAS STA 1540-1640 RBL 45. REMOVED AND REPLACED SECTION OF SEAT TRACK AT SAA/SAT DURING HMV VISIT ON NR 58510 JOB NUMBER 82602210001.

Part: SEAT TRACK — CORRODED (BS 640-700) · airframe 39,019 hrs · 13,455 cycles

MAIN SEAT TRACK CORRODED STA 640-700 RBL45. REMOVED AND REPLACED SEAT TRACK SECTION AT SAA/SAT DURING HMV VISIT ON NR 126441 JOB NUMBER 82600230001.

Part: CUSP WEB — CORRODED (BS 686-740) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN FLOOR CUSP INNER CHORD CORRODED STA 686-740 RT RBL 56. REMOVED AND REPLACED CUSP CHORD IAW BAC DRW143N8328 AT SAA/SAT DURING HMV VISIT ON NR 58710 JOB NUMBER 82600250001.

Part: SEAT TRACK — WORN (BS 440-640) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN SEAT TRACK STA 440-640 WORN AND HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52 DURING HMV AT SAA IN SAT ON NR 127597.

Part: CUSP WEB — CORRODED (BS 1380) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN CUSP WEB STA 1380-1400 CORRODED. REMOVED AND REPLACED WEB AND ANGLE PER SRM 51-40-02 DURING HMV AT SAA IN SAT NR 134497

Part: STRUCTURE — CORRODED (BS 720) · airframe 39,019 hrs · 13,455 cycles

CORROSION ON CHORD STA 720 LBL62. REMOVED AND REPLACED CHORD PER SRM 51-40-02 ON NR 127685 DURING HMV AT SAA IN SAT.

Part: STRUCTURE — CORRODED (STA 720-740) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN INNER CUSP CHORD STA 720-740 RT CORRODED. REMOVED AND REPLACED CHORD PER SRM 51-40-05, 51-40-02 ON NR 127704 DURING HMV AT SAA IN SAT.

Part: FLOOR SUPPORT — CORRODED (BS 297-378) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN FLOOR CUSP CHORD CORRODED STA 297-378 RT. REMOVED AND REPLACED CHORD IAW SRM 51-40-02. DURING HMV AT SAA IN SAT NR 134493.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN FLOORBEAM STA 1640 BL0 LBL 59 HAS MULTIPLE AREAS OF CORROSION. REPAIRED PER ERA474162-14 REV ORIG DURING HMV IN SAT ON NRC 134488.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 39,019 hrs · 13,455 cycles

FLOORBEAM STA 324 RBL47 HAS CORROSION. REPAIR C/W ON NR 127584 IAW SRM 53-10-08 FIG 202 AT SAA IN SAA DURING HMV.

Part: FRAME — DENTED (BS 1480) · airframe 39,019 hrs · 13,455 cycles

AFT CARGO FRAME STA 1480 S26-27L FLANGE DENTED. REPAIRED PER SRM 53-00-07, 51-40-02 CAT B REPAIR NR 5 REINSPECT EVERY 12,000 CYCLES.

Part: FRAME — DENTED (BS 520) · airframe 39,019 hrs · 13,455 cycles

FRAME DENTED IN FWD CARGO STA 520 BETWEEN STR 25 AND 24L. REPAIRED PER ERA474163-14 REV ORIG DURING HMV AT SAT ON NRC133877.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 39,019 hrs · 13,455 cycles

MAIN CABIN FLOORBEAM STA 1660 LBL57 CORRODED. REPAIRED PER ERA 4741455-14 REV O DURING HMV IN SAA AT SAT ON NR 134572.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 39,019 hrs · 13,455 cycles

RT WING OTBD FORE FLAP AT WS 652.50 LOWER OTBD CORNER HAS CHAFE WEAR AT LEADING EDGE. REPAIRED PER SRM 57-53-01 FIG 201. REPAIR 3 DURING HMV CHECK AT SAA ON NRC 134488.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 39,019 hrs · 13,455 cycles

LEFT INBD FLAP LWR SURFACE T/E HAS DENT AT STA 224. REPAIRED DURING HMV AT SAA IN SAT ON NR 134448 IN CONJUNCTION WITH JIC OPN 1000 CARD NR 82667990001.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 39,019 hrs · 13,455 cycles

UPPER SURFACE RT ELEVATOR HAS DAMAGE APPROX 2 INCHES THROUGH COMPOSITE MATERIAL. REPAIR C/W ON NR 114471 AT SAA IN SAT IN CONJUNCTION WITH JIC OPN 1000 CARD NO 82667810001.

Part: TRANSPONDER — INOPERATIVE (NR 1) · airframe 38,605 hrs · 13,381 cycles

ON DEPARTURE FROM JFK GOT ATC, FAULT LIGHT WITH TRANSPONDER NR 1 FAIL LIGHT. SWITCHED TO NR 2 TRANSPONDER. ATC INFORMED US THAT THAT THEY HAD NO SQUAWK ON US ENTIRE FLIGHT. BOTH TRANSPONDERS INOP. FWD TO MCO/PLAC PER MEL 34-53-01B.

Part: ENGINE — UNKNOWN (NR 2) · airframe 34,443 hrs · 12,623 cycles

IN CRUISE GOT RT ENG PRI CONT AND A RT ENG SEC CONT MESSAGE. THE EPCS MESSAGES WERE: P SVA OR FCU/EEC AND S SVA OR FCU/EEC. DUE TO HISTORY AND UNABLE LOCATE DEFINITIVE PROBLEM. REPLACING NR 2 ENGINE.

Part: SKIN — GOUGED (BS 665 S19R) · airframe 34,102 hrs · 12,564 cycles

DURING THE WINGLET MOD AT SAA, A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT STA 665, BETWEEN S-19R AND S-20R. THE DAMAGE WAS REPAIRED PER BOEING INSTRUCTIONS.

Part: LONGERON — CUT (BS 730-740 L21R) · airframe 34,102 hrs · 12,564 cycles

LONGERON R21 BETWEEN STATIONS 730 AND 740 WAS CUT. REPAIRED IN ACCORDANCE WITH SRM 51-40-02.

Part: LIGHT — LOOSE (CABIN)

DFW - EMERGENCY LIGHT STRIP IN FIRST CLASS LOOSE. SECURED EMERGENCY LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHAFT — SHEARED (ENGINE OIL PUMP)

DFW INFLIGHT T663/20OCT - AT 2000 FEET ON TAKE OFF, LEFT ENGINE OIL PRESSURE WENT TO ZERO AND RED LIGHT ANNUNCIATED AROUND LEFT OIL PRESSURE WITH ASSOCIATED EICAS MESSAGE. SHUT DOWN ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AFTER LANDING OIL QUANTITY WAS 18. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. FOUND OIL PUMP SHAFT SHEARED. FLIGHT DATA RECORDER SHOWED EXCESSIVE RUN TIME WITH NO OIL PRESSURE. CHANGED NR 1 ENGINE ON 22 OCTOBER AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — BROKEN (GIRT BAR) · airframe 20,998 hrs · 7,170 cycles

DURING CHECK-C THE EVACUATION SLIDE GIRT BAR LEAF RETENTION SPRING WAS FOUND BROKEN AND REPLACED AT THE L1 AND R1 CABIN DOORS. THE SPRINGS WERE FOUND DEFORMED AND REPLACED AT THE L2, R2, L4 AND R4 CABIN DOORS.

Part: MONITOR · airframe 19,482 hrs · 6,586 cycles

THE PASSENGER ENTERTAINMENT MONITOR AT CABIN ROW 27, LEFT SIDE, OVERHEATED AND CAUSED AN ELECTRICAL ODOR. FLIGHT MADE AN UNSCHEDULED LANDING AT JAX. THE ELECTRICAL CONNECTOR WAS REMOVED FROM THE MONITOR AND THE AIRCRAFT OPERATED MINIMUM EQUIPMENT. THE MONITOR WAS LATER REPLACED. CHECK-C 12-20-01 MCI. ---CLOSED--

Part: CONNECTOR — DETACHED · airframe 16,993 hrs · 5,643 cycles

DURING LAYOVER SERVICE, THE EGRESS LIGHTING STRIP FOUND INOP AT -D- LAVATORY DOOR. REPAIRED ELECTRICAL CONNECTION TO MAIN POWER SUPPLY FOR -D- LAV DOOR AND OPS CHECK NORMAL. CHECK-C 12/12/01. ---CLOSED---

Part: LAMP — MISSING · airframe 16,993 hrs · 5,643 cycles

DURING LAYOVER SERVICING, EGRESS LAMP MISSING AT FIRST CLASS SEAT - ROW 2L. INSTALLED MISSING LAMP, OPS CHECK NORMAL. CHECK-C 12/12/01. ---CLOSED---

Part: SKIN — CORRODED (FUSELAGE) · airframe 16,541 hrs · 5,479 cycles

DURING CHECK-C MAINT FOUND TWO STATIC BURN PITS WITH 3 INCH CIRCLE OF LIGHT CORROSION. AREA HAD BEEN GROUND APPROX 0.025 DEEP, LOCATED CENTER OF LAP SEAM, STRINGER 4L AND STA 1223. REPAIRED PER ARA 17864.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,496 hrs · 5,461 cycles

THE EMERGENCY LIGHT AT SEAT ROW 2D, AND THE EGRESS LIGHTS ROW 14 TO 18, WERE INOPERATIVE. REPLACED THE LAMP, PN 8074-1, AT ROW 2D, AND REPLACED SPLICE, PN 65801-003, AT ROW 14 FOR THE EGRESS LIGHTS AT ROW 14 TO 18.

Part: POWER SUPPLY (WDM M-734) · airframe 16,029 hrs · 5,307 cycles

WHEN ELECTRICAL POWER WAS LOST THE FLOOR AND CEILING EMERGENCY LIGHTS IN THE MID AND AFT CABIN STAYED ON AND WOULD NOT RESET. REPLACED THE POWER SUPPLY. CHECK-C 7-22-00 LAX. --CLOSED--

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 14,897 hrs · 4,991 cycles

WITH POWER REMOVED FROM THE AIRCRAFT THE EMERGENCY EXIT LIGHTS AT ROWS 24 AND 26 ILLUMINATED. FOUND LOOSE ELECTRICAL CONNECTOR AT M10919 AND SECURED SAME. CHECK-C 7-22-00 LAX.

Part: SKIN — DENTED (TE FLAP) · airframe 11,411 hrs · 3,920 cycles

DURING CHECK-C MAINT, THE LT WING I/B TRAILING EDGE FLAP, ON THE BOTTOM TOWARDS THE TRAILING EDGE, A DENT AND SCRATCH WAS FOUND APPROX 1 IN BY 1 IN BY .0625 IN DEEP. EDDY CURRENT FOUND A .75 INCH CRACK. INSTALLED A 4 INCH DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10.

Part: LIGHT — INOP (LAVATORY)

THE CABIN EGRESS LIGHTS WERE INOPERATIVE AT THE RT AFT LAVATORY. CLEANED THE EGRESS STRIP. CHECK-C 1-20-99 LAX.

Part: BEARING — FAILED (LT NLG)

DURING TAKEOFF FROM STL, THE LEFT NOSE WHEEL ASSEMBLY SEPARATED FROM THE AIRCRAFT. FLIGHT OPERATED AND LANDED AT MCO WITHOUT INCIDENT. CHECK-C 1-20-99 LAX. INVESTIGATION FOUND THE OUTER BEARING OF THE LEFT NOSE GEAR WHEEL FAILED. THIS COMPROMISED THE RETENTION OF THE WHEEL AND THE WHEEL DEPARTED FROM THE AIRCRAFT. IN ADDITION TO THE WHEEL ASSEMBLY, THE NOSE GEAR PISTON/AXLE ASSEMBLY HAD TO BE REPLACED DUE TO DAMAGE.

Part: OVEN — FAILED (NR 3)

STL - FLT 2 - AFT GALLEY NR 3 OVEN HAD ELECTRICAL SMELL WHEN POWER APPLIED. PULLED CB AND DID NOT USE OVEN. REPLACED THE OVEN. (M)

Part: OVEN — OVERHEATED (GALLEY)

JFK - FLT 901 - DURING CRUISE, THE B-6 OVEN OVERHEATED EMITTING SMOKE INTO THE CABIN AND SOUNDED THE ALARM. REMOVED AND REPLACED OVEN, MFG PN 8201-11-0000, MANUFACTURED BY BUDERUS SELL CORPORATION. OPERATIONAL CHECK NORMAL. OP16-7/16/97. (X)