N627DL

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 92,786 hrs · 43,642 cycles

EMERGENCY EXIT LIGHT OUT AT SEAT 3C. FOUND WIRE BROKEN UNDER SEAT, REPAIRED IAW SWPM 20-30-12. REPLACED POWER SUPPLY FUSE. OPS CHECK GOOD, OK FOR SERVICE.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,051 hrs · 43,391 cycles

DURING S/C FOUND LUMINATOR AT SEAT 4C INOPERATIVE. R & R HARNESS AS REQUIRED. OPS CHECK NORMAL IAW AMM 33-52.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 91,696 hrs · 43,236 cycles

ON SC FOUND EMERGENCY LIGHT SEAT HARNESS WIRE DAMAGED AT ROW 21 RT. REPAIRED HARNESS IAW SWPM 20-30-12, OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 89,516 hrs · 42,303 cycles

EMERGENCY AISLE SEAT MOUNTED LIGHT INOPERATIVE. REPLACED FEMALE CONTACTS AND NEW CONNECTORS IAW WDM 33-51. OPS CHECKED GOOD. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 89,103 hrs · 42,112 cycles

EMERGENCY AISLE LIGHTING AT ROWS 32 DEF AND 43 DEF INOPERATIVE. PINNED THE CONNECTORS IAW SWPM.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 88,440 hrs · 41,810 cycles

FOUND TWO EMERGENCY LIGHTS INOPERATIVE AT SEATS 33D AND 25D. SECURED THE LOOSE CONNECTORS AT SEATS 33D AND 25D.

Part: SKIN — DENTED (BS 1340-1360) · airframe 88,114 hrs · 41,671 cycles

SKIN BS 1340-1360 STRINGERS 29 - 30L IS DENTED. REPAIRED IAW ERA 518439-14, REV. A.

Part: SKIN — DENTED (BS 1340-1360) · airframe 91,536 hrs · 43,155 cycles

FUSELAGE SKIN, BS 1340-1360 AND S29 - 30L AT G4 ANTENNA INSTALLATION DENTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 87,065 hrs · 41,265 cycles

EMERGENCY LIGHT AT ROW 6CD INOPERATIVE. REPAIRED BROKEN WIRE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,754 hrs · 41,133 cycles

EXIT SIGN OVER L1 DOOR WILL NOT TEST. REPLACED POWER SUPPLY & BATTERY PACK IAW AMM 33-51.

Part: BATTERY PACK — UNSECURE (EMERGENCY LIGHTS) · airframe 85,886 hrs · 40,753 cycles

EMERGENCY LIGHTS OUT AT DOOR 1L AND LT SIDE FIRST CLASS OVERHEAD BINS. FOUND BATTERY PACK NOT SECURE. SECURED BATTERY, OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (BS 500) · airframe 89,454 hrs · 42,274 cycles

THIS LOG OPENED FOR ACTL 2101 FOR ERA479431-14, REV C, FUSELAGE SKIN FS 500, S9L LIGHTNING DAMAGE. AT OR PRIOR TO 42000 TOTAL ACFT FLIGHT CYCLES AND REPETITIVELY EVERY 2200 FLIGHT CYCLES THEREAFTER, ACCOMPLISH INTERNAL HFEC INSP OF THE FUSELAGE SKIN AT THE PERIPHERAL FASTNER ROW HOLES EXCEPT WHERE COVERED BY INTERNAL TEAR STRAP OR STRINGER ASSOCIATED ER/A 00-479431, ADDED FOR AC 0627.

Part: SKIN — DAMAGED (BS 717 S24R) · airframe 83,392 hrs · 39,729 cycles

INSPECT LIGHTNING STRIKE DAMAGE ON SKIN BS 717 STR 24R. REPAIRED IAW SRM 53-00-01, REPAIR 3

Part: SKIN — DAMAGED (BS 682 S24R) · airframe 83,392 hrs · 39,729 cycles

LIGHTNING STRIKE SKIN DAMAGE BS 682 STR 24R. REPAIRED IAW SRM 53-00-01, REPAIR 2

Part: SKIN — DAMAGED (FUSELAGE) · airframe 83,282 hrs · 39,688 cycles

LIGHTNING STRIKE ON APPROACH. APPARENT RT SIDE NOSE. FWD RT DOOR COMPOSITE DAMAGE. INSTALLED PERMANENT REPAIR TO RT FWD NLG DOOR. OUTER SKIN IAW SRM 52-80-02 AND IAW SRM 51-70-05.

Part: SKIN — DAMAGED (BS 439 S21-22L) · airframe 83,278 hrs · 39,686 cycles

LIGHTNING STRIKE ON FUSELAGE BS 439 AT BUTT SPLICE BETWEEN STRINGER 21L AND 22L. REPAIRED IAW ERA 511512-14.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 82,896 hrs · 39,535 cycles

FOUND FIRST CLASS SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND WIRE SHORTED AT SEAT ROW 3CD. REPAIRED WIRING, FOUND POWER SUPPLY M731 NOT POWERING L1 EXIT SIGN. REPLACED M731 IAW AMM 33-51. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 5CD) · airframe 81,876 hrs · 39,130 cycles

SHIP 627, MAINTENANCE DISCOVERED SEAT 5CD ESCAPE PATH LIGHT INOPERATIVE. REPLACED SEAT 5CD ESCAPE PATH LIGHT ASSY PER AMM 33-51. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 500) · airframe 89,454 hrs · 42,274 cycles

ERA479427-14AD, REV C, FUSELAGE SKIN/S-4L LAP JOINT/FS 500, FS 620-640/LIGHTNING DAMAGE AD 2006-11-11 TIME-LIMITED. ERA REP CYC ACTL/2100 CONVERTED TO SCEPTRE ON 03OCT13 03:12 UTCAD NR FROM ACTL 2006-11-11, ENG, ACTL AD NR DOES NOT HAVE ASSOCIATED ACTL EA NR (ENG) AD TO AA CONVERSION NOT COMPLETED ASSOCIATED ER/A 00-479427 ADDED FOR AC 0627.

Part: DOUBLER — MISSING (LE SLAT) · airframe 80,193 hrs · 38,422 cycles

RT SIDE 10 SLAT HAS PREVIOUS REPAIR DOUBLER MISSING. INSTALLED PERMANENT REPAIR DOUBLER PER B757-200 SRM 57-43-02 REPAIR 1 FIG 201 SEALED AND RE-APPLIED FINISH JPER B757-200 AMM 51-21-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

DENT IN FUSELAGE SKIN STA 1846 STR 27R. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 195187 W/O 87873840001. AS PER ER/A 492128-14 REV ORIGINAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

DENT ON FUSELAGE SKIN GOING ACROSS STRINGER BETWEEN STA 1320-1340 AND BETWEEN STR 29L TO 27R (ADF ENTRY 004). COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 194994 W/O 87873110001. AS PER ER/A 492121-14 REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

REPAIR DOUBLE ON FUSELAGE SKIN HAS IMPACT DAMAGE SKIN AROUND DOUBLER BULGING OUTWARD STA 610 TO STA 630 BETWEEN STR 15L AND 18L. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 181076 W/O 87872980001. AS PER ER/A 492129-14AD REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN INTERCOSTAL FWD OF R2 DOOR CRACKED IN 2 PLACES STA 680-683 IN LINE WITH STR 12R. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 187353 W/O 87881490001.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN INTERCOSTAL FWD OF L2 DOOR CRACKED IN RADIUS STA 681 IN LINE WITH STR 12L. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 187352 W/O 87881480001.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

2 EA DENTS ON FUSELAGE SKIN STA 1393 AND 1396 ABOVE STR28R. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 194991 W/O 87872870001. AS PER ER/A 493029-14 REV ORIGINAL.

Part: SKIN — GOUGED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

GOUGE ON EXTERNAL SIDE OF FUSELAGE SKIN AT STA 500 3 INCHES ABOVE STR 28L. COMPILED WITH AT SAA/SAT ON NON ROUTINE NR 181089 W/O 87873070001. AS PER ER/A 492122-14 REV ORIGINAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FLOORBEAM CORRODED STA 377.7 LBL 24 TO RBL 24 TO RBL 24 WITH A GOUGE FROM A CHERRY MAX STEM AT LBL 32. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187276 W/O 87881700001. PER ER/A 493049-14 REV ORIGINAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

DENT ON FUSELAGE SKIN AT STA 1569 ABOVE STR 20R. C/W AT SAA/SAT ON NON ROUTINE 181074 W/O 87872730001. COMPLIED WITH ER/A 403021-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FLOORBEAM CORRODED STA 1640 BL 0 TO RBL 23. C/W AT SAA/SAT AS PER ER/A 493040-14 REV, ORIGINAL. ON NONROUTINE 194594 W/O 87878960001.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

DENT ON FUSELAGE SKIN STA1630 ABOVE STR 18L. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 194995 W/O 87872740001. AS PER ER/A 493036-14 REV ORIGINAL.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

AFT CARGO STR 29R KEEL BEAM O/B FLANGE CORRODED STA 1390-1415. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 187541 W/O 87878520001. AS PER ER/A 492124-14 REV ORIGINAL.

Part: PUSHROD — CORRODED (L4 DOOR) · airframe 78,279 hrs · 37,642 cycles

L4 DOOR LOWER GATE AFT PUSH ROD CORRODED. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 194534 W/O 87877900001. AS PER CMM 52-11-25

Part: RIB — CORRODED (CARGO DOOR) · airframe 78,279 hrs · 37,642 cycles

UPON REMOVAL OF LEVELING COMPOUND IN LOWER AREA OF AFT CARGO DOOR ON N/R 187989 SAA JOB 87883410001, FOUND CORROSION ON ALL LOWER FLANGES OF RIBS. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187321 W/O 87884220001.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 78,279 hrs · 37,642 cycles

RUST ON LEFT WING I/B MAIN FAIL SAFE STRAP TORQUE TUBE INNER SURFACE. REFERENCE ER/A 6-097981-14 FOR REPAIR PROCEDURES. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 182569 W/O 87874120001.

Part: FRAME — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

AFT CARGO FRAME DENTED ON UPPER FLANGE STR N25&26 REPAIR ANGLE HAS INCORRECT NUMBER OF FASTENERS ON LOWER FLANGE. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187563 W/O 87878730001.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

AFT CARGO FRAME CORRODED ON FWD SIDE ABOVE SHEAR TIES AND AFT SIDE UNDER FAIL SAFE STRAP CHORD STA 1420 STR 29L TO DOOR FRAME 27R. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187544 W/O 87878550001.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

UPON REMOVAL OF AFT CARGO ENTRY SILL CHORD FOUND CORRODED INTERCOSTAL AT FUSELAGE STA,1360 1380 RBL16. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187988 W/O 87883440001.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN INTERCOSTAL FWD OF L2 CRACKED IN RADIUS STA 681 IN LINE WITH STR 12L. COMPILED WITH AT SAA/SAT ON NON-ROUTINE 187352 W/O 87881480001.

Part: FRAME — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

AFT CARGO FRAME DENTED ON UPPER FLANGE STA 1400 BETWEEN STR 25 AND 26L REPAIR ANGLE DOES NOT HAVE THE CORRECT NUMBER OF FASTENERS PAST CUTOUT ON LOWER O/B FLANGE. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187460 W/O NR 87878500001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FLOORBEAM CORRODED STA 740 RBL 11-22. COMPLIED WITH AT SAA/SAT4 ON NON ROUTINE 187264 W/O NR 8788187001. FABRICATED REPAIR ANGLES PER ER/A 481634-14MA STEP 4.

Part: FRAME — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

AFT CARGO FRAME DENTED ON UPPER FLANGE STA 1460 ABOVE STR 29L. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187562 W/O NR 87878720001. FABRICATED REPAIR J SECTION PER SRM 53-00-07 FIG 201.

Part: FRAME — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FRAME DENTED ON LIP STA 940 AT STR 5R. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187359 W/O 87881570001.

Part: SPAR — DAMAGED (LT WING) · airframe 78,279 hrs · 37,642 cycles

WHILE PERFORMING WINGLET MOD FOUND 2 EA HOLES AT WSTA 810 WITH INCOMING TOOLING MARKS LT WINGLET FWD SPAR WEB. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 195146.W/O 87883240001. AS PER ER/A 493028-14,

Part: STRINGER — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

UPON REMOVAL OF FUSELAGE SKIN BETWEEN STA 590-633 BETWEEN STR14L-19L FOUND STRINGER 16L DENTED AND CRACKED AT STA 610. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 181642 W/O NR 87883560001. FABRICATED STRINGER SEGMENT PER DRAWING NR 143N3110-REV AK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FLOORBEAM UPPER AND LOWER SURFACE AND ADJACENT. REPAIR ANGLE ALSO CORRODED STA 720 RBL 33. COMPLIED WITH AT SAA/SATON NON ROUTINE 187256 W/O NR 8788180001.

Part: NONE — NONE (NONE) · airframe 89,454 hrs · 42,274 cycles

SRM D/R 53-00-03, FIG 201, REP 3 DAMAGE AT FS 610, STR 16L. THE REF SRM 53-00-03, FIG 201, REPAIR 3 DOES NOT EXIST WITHIN THE SRM. THE DAMAGE REF AT FS 610 AT STR 16L DEFINED IN THIS MONITOR HAS ALSO BEEN DEFINED IN ERA 492129-14AD, REV ORIGINAL AND COVERS FS600 THRU 640, STR 15L TO 19L. ERA 492129-14AD IS CURRENTLY UNDER DTA ANALYSIS. NEED TO KNOW THE INSPECTION REQ REP INTERVAL AND CORRECT REF. UPDATE RECORD 350719. INSPECTED FUSELAGE SKIN FS 600 THROUGH 640 STR 15L TO 19L. ONE BAY ABOVE AND BELOW THE REPAIR AREA, NO DISCREPANCIES NOTED.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

AFT CARGO STR 29R REPAIR SPLICE ANGLES CORRODED ON SURFACE AND IN BETWEEN THE TWO ANGLES STA 1420 - 1440. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 187548.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

ACCOMPLISH REPAIR PER SRM 53-00-01 FIG 101, NOTE 1 ATCL3251/3107 SKIN DENTED FS 600 BETWEEN STR 28L AND 28R (BL-0) (REF,OMI LOG W/CN: U01200083). COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 162196 W/O NR 87870590001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FLOORBEAM CORRODED STA 345 BL 0 LBL 24. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187255 W/O NR 87881790001.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN SEAT TRACK GOUGED AND CORRODED INSIDE STA 760-880 - RBL 24. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 188032 W/O NR 87882750001.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN SEAT TRACK GOUGED AND CORRODED ON CROWN STA 760-880 RBL 45. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 188033 W/O NR 87882770001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN SEAT TRACK CORRODED INSIDE AND GOUGED ON CROWN STA 760-880 LBL 45. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 188029 W/O NR 87882690001.

Part: STRAP — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

AFT CARGO STRAP INSIDE STR 29L CORRODED STA1440-1445. COMPLIED WITH AT SAA/SAT ON NON ROUTINE NR 187550 W/O NR 87878610001.

Part: ROD END — CORRODED (EVAC SLIDE) · airframe 78,279 hrs · 37,642 cycles

LT OVERWING SLIDE CARRIER SNUBBER RODEND CORRODED. REPLACED ROD END AT SAA ON N/R CARD 188054.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FLOORBEAM UPPER SURFACE CORRODED STA 680 LBL 24 RBL 24. REPAIRED DURING HMV AT SAA ON N/R CARD 187261.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

MAIN CABIN FLOORBEAM CORRODED STA 760 LBL 3 TO LBL 22. REPAIRED DURING HMV AT SAA ON N/R CARD 187266.

Part: GATE — CORRODED (R4 DOOR) · airframe 78,279 hrs · 37,642 cycles

R4 DOOR LOWER GATE HAS CORROSION THRU-OUT. REPLACED GATE AT SAA ON N/R CARD 194538.

Part: LIFTER — DAMAGED (GIRT BAR) · airframe 78,279 hrs · 37,642 cycles

L4 DOOR FWD AND AFT GIRT BAR LIFTER GOUGED AND CORRODED. REPLACED LIFTERS AT SAA ON N/R CARD 194541.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

1 EA DENT ON FUSELAGE SKIN STA 633 BELOW STR 17L NO ID TAG. ACCOMPLISHED ERA 492129-14 AD AT SAA ON N/R CARD 181076.

Part: SKIN — DENTED (FUSELAGE) · airframe 78,279 hrs · 37,642 cycles

1 EA DENT 3 INCHES LONG ON FUSELAGE SKIN STA 612 BELOW STR 17L. ACCOMPLISHED ERA 492129-14 AD AT SAA ON N/R CARDS 181078.

Part: SKIN — DAMAGED (FS 500 S9L) · airframe 77,441 hrs · 37,275 cycles

FUSLELAGE SKIN, FS 500, S-9L, LIGHTNING STRIKE DAMAGE REPAIRED IAW ERA 479431-14.

Part: LAP JOINT — DAMAGED (FS 500-640 S4L) · airframe 77,423 hrs · 37,266 cycles

FUSELAGE SKIN, S-4L LAP JOINT, FS 500, FS 620-640 LIGHTNING STRIKE DAMAGE REPAIRED IAW ERA 479427-14AD.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 75,924 hrs · 36,586 cycles

DURING LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT HARNESS. OPERATIONAL CHECK WAS GOOD (2010-D0863)(DL757101934).

Part: ACTUATOR — NO TEST (OUTFLOW VALVE) · airframe 72,068 hrs · 34,603 cycles

IRR AT FL 350 CABIN ALT WARNING FOLLOWED BY CABIN ALT AUTO 1 INOP. CABIN ALT REACHED APPROX 12.5-13.0. REPLACED NR 1 CABIN PRESS CONTROLLER. REPLACED OUTFLOW VALVE ACTUATOR PER MM OPN CKS GOOD BITE ON AUTO 1 AND AUTO 2 VERIFY NO FAULTS MANUAL, OPS NORMAL.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 67,001 hrs · 32,216 cycles

DURING ACCOMPLISHMENT OF EA 06-070332-03AD, SIP MOD, HOLE NR 51 AS IDENTIFIED IN THE EA REQUIRED OVERSIZING BEYOND THE EA MAX. THE EA ALLOWS OVERSIZING TO 1ST OVER, AND THE HOLE REQUIRED OVERSIZING TO 2ND OVER. BOEING PROVIDED AMOC 8100 APPROVAL OF THE OVERSIZE HOLE CONDITION AS DETAILED IN 461451-14AD

Part: FAN — OVERHEATED (CABIN) · airframe 56,171 hrs · 28,184 cycles

FLIGHT ATTENDANT CALLED FLT DECK WITH REPORT OF SMOKE COMING OUT OF THE FLOOR VENT FWD. NOTED THE RIGHT RECIR FAN ICAS MSG WAS ILLUMINATED. TURNED L AND R RECIR FANS OFF. TURNED L AND R UTILITY SWITCH OFF AND SMOKE DISSIPATED. PROBLEM OCCURRED ON 12/09/03, RIGHT RECIR FAN OVERHEATED. REPLACED RT RECIRC FAN.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,377 hrs · 27,459 cycles

FUSELAGE SKIN WAS FOUND DENTED AT FS 1695 ABOVE THE STRINGER 26R SKIN LAP JOINT. THE DAMAGED AREA OF SKIN WAS REMOVED WITH A 3 X 9 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 385021-14,REV B.

Part: SKIN — GOUGED (FUSELAGE) · airframe 51,493 hrs · 26,114 cycles

FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT 2 LOCATIONSBETWEEN FS 605 & 625 AT STRINGER 16L AND JUST BELOW STRINGER17L. THE DAMAGE WAS REMOVED WITH 2 CUTOUTS. THE CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER AND TRIPLER REPAIR PER ER/A 385022-14, REV A.

Part: SIGN — DAMAGED (R1 DOOR) · airframe 49,533 hrs · 25,200 cycles

R1 DOOR EMERGENCY LIGHTING EXIT SIGN IS DAMAGED. REPLACED LIGHT ASSY, CHECKS OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 46,433 hrs · 23,728 cycles

ATB, ON T/O NOTICED A STRONG ODOR IN COCKPIT, FWD AND AFT F/A REPORTED ODOR SIMILAR TO MELTING/HOT ELECTRICAL INSULATION. CHECKED FWD/MAIN EE, FWD AFT CARGO BINS, A/C BAY, APU FOR SIGNS OF ARCING/BURNING, NONE FOUND. RAN ENGINES TO TAKEOFF WITH BOTH PACKS. NO SMELL OR SMOKE PRESENT ON VERIFICATION. ALL NORMAL. OK FOR SERVICE.

Part: SENSOR — INOPERATIVE (BLEED AIR TEMP) · airframe 45,997 hrs · 23,506 cycles

ON T/O, RT ENG BLEED INTERMITTENT DURING CLIMB AND FOR TEN MINUTES OF CRUISE. AT CRUISE MSG RE-APPEARED, THEN LT ENG BLEED ILLUMINATED WITH ASSOCIATED PACK TRIPS. REPLACED RT HIGH STAGE PILOT.

Part: SENSOR — OUT OF ADJ (RIGHT AFT) · airframe 45,625 hrs · 23,324 cycles

RT AFT ENTRY DOOR LIGHT CAME ON AT 100 KIAS ON T/O ROLL. ABORTED T/O AT 110 KIAS. - ADJUSTED PROX SENSOR 10093

Part: WEDGE — DAMAGED (NR 10 LE SLAT)

AD 90-23-06: NR 10 LE SLAT TE WEDGE REPLACEMENT, FASTENER SUBSTITUTION. DURING REPLACEMENT OF THE TE WEDGE PER EO 6-71653-3AD AND SRM 57-43-02, FIGURE 202 (REF SB 757-57A0038). SEVERAL EXISTING COVE SKIN-TO-WEDGE ATTACH FASTENERS WERE CSK FOR TENSION HEAD HI-LOCKS. REQUIRED FASTENERS ARE SHEAR HEAD FLUSH FASTENERS. AUTHORIZED USE OF TENSION HEAD HI-LOCKS IN EXISTING OVER-CSK HOLES.

Part: GUIDE — WORN (2L DOOR)

DOOR 2L UNABLE TO USE FROM OUTSIDE IN BHM. LINKAGE DAMAGED, REPLACED GUIDE.

Part: OVEN — DIRTY (NR 2 GALLEY)

FLIGHT ATTENDANT REPORTED SMELL OF SMOKE TAXIING OUT SLC. RETURNED TO GATE. CHECKED OVENS AND COFFEEMAKERS IN QUESTION, FOUND BURNED TAPE IN NR 2 OVEN CENTER GALLEY FOOD CARRIER. ALSO, CHECKED FWD BAG BIN, NO ODORS NOTED.

Part: SKIN — PEELING (RT WING)

SKIN COMING OFF AIRCRAFT UNDERSIDE OF RT WING 6 INCHES INBOARD OF WING TIP. INSTALLED TIME LIMITED REPAIR PER 757 SRM 57-41-01-1 FIG 101 TO L/E SLAT UNDERWING PNL AT OSS 761. SEALED WITH SPEED TAPE.

Part: CUB STRAP — CORRODED (RT EMER EXIT)

FOUND CORROSION ON THE FWD SIDE OF THE RT OVERWING EXIT DOOR INNER SIDE, CUB STRAP. REPAIRED PER BACO TWX DAL-ATL-96-1144RR, DATED 7/29/96.

Part: PANEL — DELAMINATION (WS 313.5 LE)

RT WING FIXED L/E AT WS 313.5 HAS DAMAGE AND FIXED L/E PANEL RT WING WS 459.5 HAS DAMAGE. REPAIRED AS PER ERA 302136-14 PER PERMANENT INSTRUCTIONS AND PER SRM 57-70-07. REPAIRS ACCOMPLISHED AT SPECIAL MTC VISIT.

Part: TE WEDGE — DELAMINATED (NR 7 LE SLAT)

DURING HMV NR 7 SLAT T/E WEDGE WAS FOUND TO HAVE DELAMINATION ON THE T/E WEDGE 33 FROM THE I/B END.

Part: HARNESS — CHAFED (FLIGHT DECK)

DURING CRUISE HAD 4 FLIGHT DECK PANEL LIGHTING CIRCUIT BREAKERS POP. REMOVED CAPTAINS P1-3 INSTRUMENT PANEL, FOUND W-1 WIRE BUNDLE WITH BURNED WIRES. THE CAUSE WAS FROM THE WIRE BUNDLE CHAFING ON THE CAPTAINS WINDOW DEFROSTER AIR HOSE. A TOTAL OF 17 WIRES WERE REPAIRED AND WIRE BUNDLE WAS PROTECTED WITH ANTI-CHAF MATERIAL. A FLEET INSPECTION WAS INITIATED ONE ADDITIONAL AIRCRAFT WAS FOUND WITH CHAFED WIRES.