N616DL

Part: BUSHING — MIGRATED (AFT PYLON) · airframe 89,780 hrs · 43,373 cycles

AFT PYLON MOUNT BUSHING MIGRATING. CLEANED HOLE REPAIRED IAW SRM 54-51-02. INSTALLED BUSHING IAW SRM.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT) · airframe 88,354 hrs · 42,759 cycles

EMERGENCY PATH LIGHT INOP AT 38F. REPLACED LIGHT MODULE AND CLEANED CONNECTOR.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 88,275 hrs · 42,726 cycles

DURING EMERGENCY LIGHT CHECK, FOUND BROKEN WIRE UNDER SEAT 6C. REPAIRED BROKEN WIRE. OPS CHECK NORMAL.

Part: SKIN — DELAMINATED (RT WING) · airframe 88,113 hrs · 42,661 cycles

WING PANEL INSPECTION, FOUND RT PANEL HAS ELEVEN FASTENERS PULLING THROUGH AND APPROXIMATELY 16 INCHES OF DELAMINATION LOCATED ON FWD EDGE 8TH FASTENER FROM INBD EDGE. REMOVED RT WING PANEL FOR REPAIR OF DELAMINATION. DRILLED UP NEW PANEL. COMPLETED NEW PANEL INSTALLATION IAW BAC DWG 113N1610.

Part: SKIN — CORRODED (BS 1710-1720) · airframe 88,108 hrs · 42,658 cycles

FUSELAGE SKIN BS 1710-1720, S28L - 28R CORRODED. REPAIRED IAW ER/A 512965-14AD.

Part: NONE — NONE (NONE) · airframe 91,046 hrs · 43,906 cycles

THIS LOG REPLACES 1345288, WHICH WAS TERMINATED IN ERROR. ER/A 523919-14AD, REV A / THIS LP IS TERMINATED, NEW STAGE III, DTA RESTRICTION IS TRACKING ON LP 1839036. ASSOCIATED ER/A 00-523919 ADDED FOR AC 0616. CLOSED LOG AND REMOVED MONITOR. INSPECTION IAW ALERT 05 MAR 15 AND LOG COMMENT.

Part: SKIN — DAMAGED (BS 445) · airframe 91,046 hrs · 43,906 cycles

ER/A 523919-14AD FOR LIGHTNING STRIKE AT FS 445 AND S-14L. ADDITIONAL FOLLOW-ON ACTIONS REQUIRED. ER/A REQUIRES ADDITIONAL AMOC APPROVAL PRIOR TO 1500 CYCLES FROM 42624 TOTAL CYCLES. NO MAINTENANCE WORK REQUIRED. REF A 523919-14AD FOR ADDITIONAL INFORMATION. ASSOCIATED ER/A 00-523919, ADDED FOR AC 0616. ER/A 523919-14AD, REV A, THIS LP IS TERMINATED, AMOC APPROVAL RECEIVED AND INCORPORATED INTO ER/A, NO FURTHER AMOC APPROVAL TRACKING IS REQUIRED. CLOSED LOG AND REMOVED MONITOR INSPECTION IAW ALERT 05 MAR 15 AND LOG COMMENT.

Part: SKIN — CRACKED (BS 445) · airframe 88,030 hrs · 42,627 cycles

FOUND A CRACK INDICATION UNDERNEATH THE LAP JOINT AT STRINGER 14L AND BS 445. STRIPPED PAINT AND REMOVED DAMAGE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 87,989 hrs · 42,611 cycles

FLOOR EMERGENCY LIGHT AT 29-37 AND 45 INOPERATIVE. REPLACED LIGHT ASSY AT 29 AND 45. REPAIRED BROKEN WIRE AT SEAT ASSY 37 IAW AMM 33-51 AND SWPM 20.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 86,668 hrs · 42,053 cycles

EMERGENCY LIGHTS AT 38DEF AND 19DEF AFT INOPERATIVE, FOUND BROKEN WIRES. TERMINATED WIRES IAW AMM 20, CHECKED NORMAL.

Part: SKIN — CORRODED (BS 1720 S28L-R) · airframe 85,051 hrs · 41,441 cycles

CORROSION ON FUSELAGE SKIN AFT LAV PANEL-CORROSION BS 1710-1720 S-28R-L DAMAGED. INSTALLED SKIN DOUBLER IAW ERA 512965-14, REV ORG 03/26/2013.

Part: STRUCTURE — CORRODED (BS 1720) · airframe 85,051 hrs · 41,441 cycles

BS 1720 BREAKING FWD CHORD BL-0 BETWEEN STR. 25L AND 25R. CORROSION DAMAGE. REPAIR IAW ERA 512791-14 REV ORIG.

Part: SKIN — CORRODED (BS 1720) · airframe 91,111 hrs · 43,931 cycles

FUSELAGE SKIN AFT OF BS 1720, S29R- S29L, CORRODED. REPAIRED IAW PRI 513046, REV 0-3. FINAL ERA 513046-14, REV B MATCHES PRI 513046-14, REV 0-3.

Part: SKIN — CORRODED (BS 1720) · airframe 85,051 hrs · 41,441 cycles

CORROSION ON FUSELAGE SKIN BS 1720, STR 29L-R. REPAIRED IAW ERA 513046-14, REV 0.

Part: MOUNT — CORRODED (ANTENNA) · airframe 93,501 hrs · 44,954 cycles

NAVIGATION-RADIO ALTIMETER LEFT, FWD ANTENNA MOUNT CORROSION. REMOVED AND REPLACED IAW ERA 511063-14 REV ORIG SECTION II.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,847 hrs · 40,959 cycles

MX DISCOVERED CABIN SEAT EMERGENCY LIGHTS INOPERATIVE ON SEATS 3C, 5C, 24D, 25D AND 27D. LAMPED EMERGENCY LIGHTS AS REQUIRED.

Part: ENTERTAIN SYS — MALFUNCTIONED (CABIN) · airframe 79,786 hrs · 39,302 cycles

ENTERTAINMENT SYSTEM STARTED TO SMOKE DURING FLIGHT. ELECTRICAL FUMES DISSIPATED WHEN SYSTEM SHUT DOWN. FLIGHT CONTINUED TO ATL AND LANDED WITHOUT INCIDENT. REPLACED VIDEO CONTROL UNIT AND THE OPERATIONAL CHECK WAS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,668 hrs · 38,831 cycles

AIRCRAFT STRUCK BY GROUND EQPT AT FS 1590 STRINGER 20L. REPAIRED PER ERA 490209-14 REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 77,718 hrs · 38,352 cycles

REPORT OF PERMANENT REPAIR OF AC 616 FUSELAGE SKIN STA 755 S-14L DENT REPAIR PER ERA 485637-14 REV B (DL757102923)

Part: STRINGER — DAMAGED (BS 637 S15L) · airframe 75,584 hrs · 37,325 cycles

UPON REMOVAL OF SKIN SECTION WHILE WORKING N/R 144372 FOUND 1 EA. EXISTING HOLE WITH A PLUG BESIDE IT ON LT STRINGER 15 AT STA 637. REPAIRED AT SAA SAT ON N/R CARD 143096.

Part: STRINGER — CRACKED (BS 651 S6L) · airframe 75,584 hrs · 37,325 cycles

MAIN CABIN FUSELAGE STR 6L IS CRACKED AT STA 651/REPAIRED AT SAA SAT DURING HMV ON N/R CARD 140418.

Part: STRINGER — CRACKED (BS 624 S16L) · airframe 75,584 hrs · 37,325 cycles

MAIN CABIN FUSELAGE STRINGER 16L IS CRACKED AT STA 624/ REPAIRED IAW SRM 53-00-03 AT SAA SAT ON N/R CARD 140419.

Part: FLOOR PANEL — CORRODED (BS 1716) · airframe 75,584 hrs · 37,325 cycles

MAIN CABIN FLOOR AFT DECK PLATE UPPER SURFACE REPAIR DOUBLER HAS CORROSION AT STA 1716 LBL 12 TO 26 AT 3 PLACES / FABRICATED AND INSTALLED NEW DOUBLER AT SAA SAT ON N/R CARD 140043.

Part: SKIN — CORRODED (BS 1500 S28L) · airframe 75,584 hrs · 37,325 cycles

SURFACE CORROSION ON LWR FUSELAGE SKIN AT LT AIRFONE ANTENNA MOUNT SURFACE/REPAIRED AT SAA SAT ON N/R CARD 136524.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 75,584 hrs · 37,325 cycles

LT WING NR 5 SLAT T/E UPPER SKIN SURFACE HAS MULTIPLE DENTS, HAIL DAMAGE, LOWER SURFACE HAS 1 EA DENT/REPAIRED AT SAA SAT ON N/R CARD 140591.

Part: SHEAR TIE — CORRODED (BS 1420 RBL 20) · airframe 75,584 hrs · 37,325 cycles

AFT CARGO COMPARTMENT BILGE FRAME ANGLE LOWER FLANGE HAS CORROSION AT STA 1420 RBL 20 / REPAIRED DURING HMV AT SAA SAT ON N/R CARD 140008.

Part: SKIN — WORN (NR 8 SLAT) · airframe 75,584 hrs · 37,325 cycles

NR 8 SLAT T/E WEDGE LOWER SURFACE HAS WEAR MARKS. REPAIRED AT SAA SAT ON N/R CARD 140657.

Part: INTERCOSTAL — CORRODED (BS 1600) · airframe 75,584 hrs · 37,325 cycles

AFT CARGO LWR BILGE TO FLOOR SUPPORT ANGLE INTERCOASTAL WEB HAS CORROSION STA 1600 TO 1620 RBL2 /REPAIRED AT SAA SAT ON N/R CARD 124336.

Part: INTERCOSTAL — CORRODED (BS 1600-1620) · airframe 75,584 hrs · 37,325 cycles

AFT CARGO LOWER BILGE TO FLOOR SUPPORT ANGLE INTERCOASTAL WEB HAS CORROSION STA 1600 TO 1620 LBL2 / REPAIRED AT SAA SAT ON N/R CARD 124338.

Part: INTERCOSTAL — CORRODED (BS 1300-1320) · airframe 75,584 hrs · 37,325 cycles

AFT GARGO INTERCOASTAL VERTICAL WEB HAS CORROSION BETWEEN STA 1300 AND 1320 STR 27R / REPAIRED AT SAA SAT ON N/R CARD 136036.

Part: SKIN — DENTED (BS 1415 S28-29R) · airframe 75,584 hrs · 37,325 cycles

FUSELAGE LWR EXTERNAL SKIN HAS A DENT AT STA 1415.5 BETWEEN S28R AND S29R/ ACCOMPLISHED ER/A 478372-14 ORIG AT SAA SAT ON N/R CARD 145013.

Part: SKIN — DENTED (BS 1425 S27R-28L) · airframe 75,584 hrs · 37,325 cycles

FUSELAGE LOWER EXTERNAL SKIN HAS A DENT AT STA 1425 BETWEEN S27R AND S28L. ACCOMPLISHED ER/A 478372-14 ORIG AT SAA SAT ON N/R CARD 145014.

Part: SKIN — DENTED (BS 1429 S29-30L) · airframe 75,584 hrs · 37,325 cycles

FUSELAGE LWR EXTERNAL SKIN HAS DENT AT STA 1429 BETWEEN S29L AND S30L/ ACCOMPLISHED ER/A 478372-14 ORIG AT SAA SAT ON N/R CARD 145017.

Part: SKIN — DENTED (BS 1428 S28-30R) · airframe 75,584 hrs · 37,325 cycles

FUSELAGE LWR EXTERNAL SKIN HAS A DENT AT STA 1428 BETWEEN S28R AND S30R/ ACCOMPLISHED ER/A 478372-14 ORIG AT SAA SAT ON N/R CARD 145016.

Part: SKIN — GOUGED (BS 1685 S19-20L) · airframe 75,584 hrs · 37,325 cycles

FUSELAGE LWR EXTERNAL SKIN HAS A GOUGE AT STA 1685 BETWEEN S19L AND S20L / ACCOMPLISHED ER/A 478209-14 ORIG AT SAA SAT ON N/R CARD 124302.

Part: SKIN — GOUGED (BS 1687 S19-18L) · airframe 75,584 hrs · 37,325 cycles

FUSELAGE LOWER EXTERNAL SKIN HAS A GOUGE AT STA 1687.5 BETWEEN S19L AND S18L. ACCOMPLISHED ER/A 478209-14 ORIG AT SAA SAT ON N/R CARD 124303.

Part: SKIN — DENTED (BS 1676 S19L) · airframe 75,584 hrs · 37,325 cycles

DENT IN LT FUSELAGE STA 1676.5 BETWEEN S19L AND S20L TAGGED BUT LESS THAN 3 INCHES FROM NEAREST FASTENER IN LAP SPLICE/ACCOMPLISHED ER/A 478209-14 ORIG AT SAA SAT ON N/R CARD144379.

Part: SKIN — DAMAGED (BS 740 S20-21R) · airframe 75,584 hrs · 37,325 cycles

RT LWR FUSELAGE EXTERNAL SKIN HAS A LIGHTNING STRIKE AT STA 740.6 BETWEEN S20R AND S21R/ ACCOMPLISHED ER/A 478204-14 AT SAA SAT ON N/R CARD 144548.

Part: SKIN — DENTED (BS 450 S16L) · airframe 75,584 hrs · 37,325 cycles

LT FUSELAGE STA 450 AND 454 ABOVE AND BELOW S16L 2 EA DENTS, AFT DENT HAS A GOUGE/ REPAIRED AT SAA SAT ON N/R CARD 144489

Part: SKIN — DENTED (BS 579-581 S17L) · airframe 75,584 hrs · 37,325 cycles

LT FUSELAGE STA 579 AND 581 BETWEEN S17L AND S18L HAS 2 EA DENTS/ ACCOMPLISHED ER/A 477161-14 AD REV B AT SAA SAT ON N/R CARD 144372.

Part: FRAME — CORRODED (FS 1540) · airframe 73,753 hrs · 36,449 cycles

DURING AGING AIRCRAFT INSPECTIONS ON THE SUBJECT AIRCRAFT, VISUAL INSPECTIONS NOTED CORROSION ON THE FORWARD SIDE OF THE 1540 BOTTOM FRAME BETWEEN S-29L AND S-30L. THE CORROSION WAS UNDER THE ATTACHING SHEAR TIE. SUBJECT CORROSION WAS REMOVED PER SRM GUIDELINES, WITH THE EXCEPTION OF THE PROXIMITY TO NEAREST FASTENER. AS A RESULT, BOEING WAS CONTACTED FOR APPROVAL TO LEAVE THE BLEND AS IS NEAR THE SUBECT FASTENERS. BOEING APPROVED AND INFO IS DOCUMENTED IN ER/A 471250-14.

Part: FRAME — CORRODED (BS 1540 LBL5) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY FRAME CORRODED AT STA 1540 LBL 5. REPAIRED PER ERA 471250-14REV ORG ON NRC 00043.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 73,753 hrs · 36,449 cycles

DURING AGING AIRCRAFT INSPECTION, FOUR AREAS OF TOOLING DAMAGE WERE FOUND ON THE VERTICAL STABILIZER CHORD. BOEING WAS CONTACTED FOR APPROVAL TO LEAVE THE BLENDED MARKS AS IS. THE REPAIR IS DOCUMENTED IN ER/A 471254-14.

Part: FLOORBEAM — CORRODED (BS 1516 RBL 12) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY FLOORBEAM 1516 AT RBL 12 CORRODED. REPAIRED PER 51-40-02 ON NR 00044.

Part: FLOOR PANEL — CORRODED (BS 1470-1510) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY FIXED FLOOR PANEL CORRODED AT STATION 1470 TO 1510 RBL 17. REPAIRED PER 51-40-02 ON NR 00086.

Part: THRESHOLD — CORRODED (CARGO BAY) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY THRESHOLD CORRODED ON UPPER SURFACE. REPAIRED ON NR 00059 PER ERA 471251-14 REV ORG.

Part: WEB — CORRODED (BS 1533) · airframe 73,753 hrs · 36,449 cycles

CRACK ON FLOOR SUPPORT WEB AT STATON 1533 LBL 33 AFT CARGO COMPARTMENT. REPAIRED ON NR 00100 PER 53-20-04.

Part: FLOOR PANEL — CORRODED (BS 1510-1538) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY AT STATION 1510 - 1538 LBL 17 FIXED FLOOR PANEL CORRRDED. REPAIRED ON NR 00033 PER 53-20-02.

Part: FLOOR PANEL — CORRODED (BS 1510-1540) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO FIXED FLOOR PANEL CORRODED AT 1510 TO 1540 RBL 17. REPAIRED PER ERA 47249-14 REV ORIGINAL ON NR 00033.

Part: SHEAR TIE — CORRODED (BS 1701 S29R) · airframe 73,753 hrs · 36,449 cycles

CORROSION AT SHEAR TIE STATION 1701 STRINGER 29R. REPAIRED BY REPLACEMENT PER 51-40-02 ON NR 00112.

Part: CARGO TRACK — CORRODED (BS 1460) · airframe 73,753 hrs · 36,449 cycles

AFT TIE DOWN FITTING CORRODED AT STATION 1460 RBL 14. REPAIRED PER 51-40-02 ON NR 00049.

Part: STIFFENER — DENTED (BS 333) · airframe 73,753 hrs · 36,449 cycles

TOOLING MARKS ON STIFFENER AT STATION 333 RBL 5. REPLACED STIFFENER ON NR 00073 PER 51-40-02

Part: INTERCOSTAL — CORRODED (BS 1520) · airframe 73,753 hrs · 36,449 cycles

INTERCOSTAL AT STATION 1520 LBL 11 CORRODED. REPAIRED PER 53-00-04 ON ATS NR 00101

Part: PANEL — CORRODED (BS 1470) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY STATION 1470 PANEL SPLICE HAD SURFACE CORROSION. REPAIRED ON NR 00051 PER 53-00-53.

Part: SUPPORT — CORRODED (BS 620) · airframe 73,753 hrs · 36,449 cycles

CORROSION AT FLOOR TO SIDE WALL SUPPORT BS 620 AT RBL 23. REPIARED ON NR 00061 PER 51-40-02.

Part: SPLICE — CORRODED (BS 1510) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY STATION 1510 PANEL SPLICE CORRODED. REPAIRED ON NR CARD 00037 PER 53-00-53.

Part: WEB — CORRODED (BS 1520-1540) · airframe 73,753 hrs · 36,449 cycles

WEB AT STATION 1520 -1540 RBL 12 CORRODED. REPAIRED ON NR 00040 PER 51-30-01 STEP 8 AND 51-40-02 FIG 1.

Part: WEB — CORRODED (BS 1500-1520) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY WEB AT STATION 1500- 1520 RBL 3 CORRODED. REPAIRED ON NR 00039 PER 51-20-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO BAY STATION 1510 LBL 7 FLOORBEAM CORRODED. REPAIRED PER 53-60-53D ON NR 00035.

Part: MOUNT — CORRODED (G1 GALLEY) · airframe 73,753 hrs · 36,449 cycles

G1 GALLEY LEFT GALLEY MOUNT PAD CORRODED. REPAIRED PER 51-40-02 BY REPLACEMENT ON NR 00079.

Part: MOUNT — CORRODED (G1 GALLEY) · airframe 73,753 hrs · 36,449 cycles

G1 GALLEY MOUNT LEFT FORWARD CORRODED. REPIARED BY REPLACEMENT PER 51-40-02 ON NR 00078.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 73,753 hrs · 36,449 cycles

AFT CARGO STATION 1439 AT STRINGER 30 TO 29 RIGHT SHEAR TIE DEFORMED BY TOOLING DAMAGE. REPAIRED BY REPLACEMENT ON NR 00053.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,753 hrs · 36,449 cycles

WEB AT STATION 1500-1520 AT LBL 3 CORRODED. REPAIRED PER 51-40-01 BY REPLACEMENT ON NR 00039.

Part: STRUCTURE — UNKNOWN (NR 7 SLAT) · airframe 72,629 hrs · 35,941 cycles

SUPPLEMENTAL SDR RT WING NR 7 SLAT TRAILING EDGE WEDGE REPAIR IAW ERA 468804-14, C/W ERA 468804-14.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 70,505 hrs · 34,977 cycles

ON FINAL APPROACH AFTER SELECTING LANDING FLAPS LEFT HYD QTY STATUS MSG AND QTY LEVEL ZERO. FOUND OUTBOARD NOSE STEERING FLEX HYD LINE LEAKING IN AFT RT SIDE OF NOSE WHEEL WELL. INSTALLED TEMP HYD LINE TO FOM. REMOVED TEMP HYD LINE AND INSTALLED NEW FLEX HYD L PER AMM. LEAK CK OK.

Part: DUCT — BLOWN (RT A/C PACK) · airframe 70,119 hrs · 34,826 cycles

LEFT DUCT LEAK THEN RIGHT DUCT LEAK, LOST REMAINING RT PACK AUTO PRESS 1 AND 2 FAIL MSGS. LOST CABIN PRESS, EMERGENCY DESCENT TO 10,000 FT. FOUND DUCT IN RT SIDE BLOWN BLOWING HOT AIR INTO THE RT AND LT A/C BAYS GIVING DUCT LEAK MSGS. DUCT BLOWN WAS THE REHEATER DUCT FOR THE RT PACK. REPLACED SAME. LEFT PACK WAS ALREADY ON MCO.

Part: ENGINE — MAKING METAL (NR 2) · airframe 63,499 hrs · 32,277 cycles

FL380 LEVEL FLT .79 MACH RT ENGINE CHUGGED AND RT OIL TEMP ROSE TO 166 THROTTLED BACK OIL TEMP RECOVERED EICAS MSG RT OIL FILTER APPROX 5 MINUTES LATER ENGINE CONTINUALLY CHUGGED SHUT IT DOWN. NO METAL FOUND IN TAILPIPE. ALL CHIP DETECTORS HAVE METAL STATUS MSG R ENGINE SEC SEL AND RT OIL FILTER. EPCS MSG DIS/EEC AND OIL P YELLOW. ENGINE EXCD NONE OIL QTY 20. ENGINE CHANGE IN PROGRESS.

Part: ACTUATOR — FAILED (NR 1 ENG BLEED) · airframe 59,069 hrs · 30,551 cycles

FLAMEOUT DURING LANDING ROLLOUT. REPLACED 2.5 BLEED ACTUATOR.

Part: WINDSHIELD — FAILED (R-1) · airframe 57,401 hrs · 29,896 cycles

R1 WINDOW SHATTERED IN FLIGHT. REPLACED SAME.

Part: BULKHEAD — DAMAGED (NACELLE) · airframe 57,394 hrs · 29,893 cycles

OVERSIZE HOLE REPAIR WHILE ACCOMPLISHING THE PYLON MODIFICATION REQUIRED BY AD 2000-20-09, SEVERAL HOLES IN THE NAC STA 203 BULKHEAD COMMON TO THE MIDSPAR ATTACH FITTING WERE DAMAGED. THE HOLES WERE OVERSIZED, HFEC INSPECTED, AND LARGER DIAMETER FASTENERS INSTALLED IAW ER/A 385451-14AD.

Part: FITTING — GOUGED (RT WING) · airframe 57,394 hrs · 29,893 cycles

GOUGE REPAIR THE INBD SURFACE OF THE INBD SIDE LOAD FITTING ON THE RT WING NACELLE ATTACH STRUCTURE WAS GOUGED DURING ACCOMPLISHMENT OF THE STRUT INPROVEMENT MODIFICATION IAW AD 2000-20-09. THE GOUGE WAS BLENDED SMOOTH AND ROTO PEENED AND THE ADJACENT FASTENER HOLE SPOTFACED TO REMOVE THE DAMAGE. THE REPAIR WAS ACCOMPLISHED IAW ER/A 385419-14AD.

Part: BRACKET — OUT OF POSITION (GIRT BAR) · airframe 55,750 hrs · 29,170 cycles

1R SLIDE INDICATOR LIGHT INOPERATIVE. FOUND 1R DOOR FORWARD GIRT BAR VISUAL INDICATOR ARMING BRACKET CAME OFF. REINSTALLED FWD VISUAL INDICATOR ARMING BRACKET AND REATTACHED BUSTLE. DOOR NOW ARMS NORMALLY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,143 hrs · 28,391 cycles

ON LAYOVER FOUND EXTERIOR EMERGENCY LIGHT ABOVE LEFT WING AFT OF EXIT HATCH INOP. RELAMPED EMERGENCY LIGHT.

Part: MONITOR — FAILED (CABIN) · airframe 53,944 hrs · 28,289 cycles

FAINT SMELL OF BURNT/ELECTRICAL ON FINAL AND ON TAXI IN. FOUND FIRST CLASS VIDEO MONITOR FAILED. MONITOR SMELLED AND SHOWED EVIDENCE OF ELECTRICAL DISTRESS. REPLACED MONITOR.

Part: HOSE — CRACKED (OXYGEN BOTTLE) · airframe 48,883 hrs · 25,932 cycles

DOOR 3L PORTABLE OXYGEN BOTTLE MASK HOSE CRACKED. REPLACED MASK AND HOSE ASSY.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 48,220 hrs · 25,626 cycles

NR 2 ENG LOSS OF THRUST INTO ATL. NR 2 GEN DROPPED OFF LINE, LOW OIL PRESS INDICATED WINDMILLING N1 AND N2 PARAMETERS. ELECTED TO SHUT DOWN NR 2 ENG AS PER CK LIST. REPLACED NR 2 EEC.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,331 hrs · 25,207 cycles

STRONG FUMES OF UNKNOWN ORIGIN IN AFT GALLEY. FIRST NOTED WHEN OVENS POWERED IN FLIGHT. DID NOT DISSIPATE WITH GALLEY POWER OFF. NOTED AT FL 350. DIVERTED TO KDFW. FUMES GOT STRONGER ON DESCENT THROUGH 10,000 FT. SEVERAL PASSENGERS REPORTED NAUSEA AND HEADACHE. RAN ENGINES TO TAKEOFF POWER. UNABLE TO DUPLICATE. SUSPECT AFT GALLEY OVEN FOOD DEBRI. ALSO, DFW AIRPORT DPS SUSPECT POSSIBLE PEPPER SPRAY LEAKAGE FROM PASSENGER LUGGAGE. RAN BOTH PACKS AND PERFORMED CABIN INSPECTION, NO DISCREPANCIES NOTED. OK FOR SERVICE.

Part: DUCT — CRACKED (RT AIR COND BAY)

AIRPLANE WOULD NOT PRESSURIZE ON RIGHT PACK. DIVERTED TO LAX. FOUND RT PACK DISTRIBUTION DUCT LEAKING. REPLACED DUCT, LEAK CHECK OK REF IPC 36-1101-07ITEM 165.

Part: SKIN — DAMAGED (NR 2 LE SLAT)

DURING REPLACEMENT OF THE TE WEDGE PER E.O. 6-71653-3AD, SEVERAL WEDGE-TO-UPPER SKIN ATTACH FASTENERS WERE INSTALLED WITH TENSION HEAD FLUSH FASTENERS, RESULTING IN OVERSIZED COUNTERSINKS. AUTHORIZED INSTALLATION OF TENSION HEAD HI-LOKS IN DISCREPANT LOCATIONS.

Part: WINDSHIELD — FAILED (RIGHT COCKPIT)

AT FL350 CREW REPORTED LOUD BANG AND NOTICED F/O WINDSCREEN HAD SHATTERED. CREW ALSO REPORTED SUBSEQUENT ARCING IN LOWER CORNER OF WINDOW. WINDOW HEAT FOR THAT WINDOW WAS TURNED OFF. DISPATCH ELECTED TO DIVERT INTO ORD DUE TO ICING CONDITIONS AT OTHER ALTERNATE AIRPORTS. MTC IN ORD IS REPLACING WINDOW.

Part: ENGINE — DAMAGED (NR 2)

RT ENGINE OIL PRESS WARNING LIGHT AND EICAS MSG AT APPROX 0000Z IN LEVEL CRUISE FLIGHT 31,000 MSL. OIL QTY WAS APPROACHING ZERO. ACCOMPLISHED INFLIGHT SHUTDOWN AS PER POM. FOUND DAMAGE TO TOWER SHAFT AND HOUSING. ENGINE CHANGE IN PROGRESS.

Part: WIRE — BROKEN (CABIN)

INTERIOR EMERGENCY TRACK LIGHTING ON FLOOR NEXT TO FIRST CLASS CLOSET INOP. FOUND BROKEN WIRE. SPLICED SAME, OPS CKS GOOD.

Part: SKIN — CRACKED (RT PYLON)

DURING HMV, FOUND NR 2 PYLON SKIN CRACKED ON OUTBD SIDE, JUST AFT OF NAC STA 107.70. REPAIRED PER SRM 54-51-01 PG 206 TO 210.

Part: CORNER — DAMAGED (BAGG DOOR)

AFT REAR BAG BIN DOOR, FWD BOTTOM CORNER DAMAGED. REPAIRED PER SRM 52-30-01. FOUND AT LTR CHECK.

Part: RADOME — DAMAGED (NOSE)

RADOME HAD A BIRD STRIKE ON CENTER OF NOSE. AFTER INSPECTION RADOME DELAMINATION AND MOISTURE ABOVE LIMITS. REBUILD RADOME COMPLETE PER SRM 53-10-72. CUT RADOME OFF ABOVE BASE RING AND REBUILD IN 757 MOLD SYSTEM. PAINT PER SP 900-9-1-11, NR 05, TRANSMISSIVITY TESTED. RETURN TO STOCK SERVICABLE.