N126DL

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 82,952 hrs · 35,112 cycles

EMERGENCY LIGHT INOPERATIVE AT ROW 42 RT SIDE. MAINTENANCE REPLACED THE LIGHTS AND REPAIRED THE WIRING AT SEAT HARNESS CONNECTOR. SYSTEM OPS IS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 80,346 hrs · 34,372 cycles

CABIN EMERGENCY EXIT LIGHTS ARE INOPERATIVE AT LT MID LAVATORY. MAINTENANCE CONNECTED LIGHTS. SYSTEM OPERATION IS NORMAL.

Part: SKIN — WORN (NR 1 NACELLE) · airframe 78,257 hrs · 33,785 cycles

NR 1 PYLON UPPER STRUT SKIN, FWD PANEL, RT & LT SPLICE STRAPS, NAC STA 163.50: REPAIR OF WEAR DAMAGE. ACCOMPLISHED ERA 096790-14, REV A.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 78,240 hrs · 33,780 cycles

RT WING INBD MAIN FLAP L/E OTBD END FAIRING DELAMINATED AS MARKED. FAIRING COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 78,240 hrs · 33,780 cycles

LT WING T/E FLAP, INBD NOSE SKIN AREA FOUND SEVERAL DELAMINATES LT WING - T/E OTBD FLAP INBD NOSE SKIN AREA COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01 REPAIR 1, SRM 51-70-05.

Part: FRAME — CRACKED (BS 859) · airframe 78,240 hrs · 33,780 cycles

BS 859.5 FRAME CRACKED. REPAIR ACCOMPLISHED IAW ER/A 513105-14AD, REV ORIG.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 78,240 hrs · 33,780 cycles

FWD CARGO BAY FLOOR PANEL 121LT BACKSIDE AFT SKIN FOUND BROKEN AND SURFACE SKIN FOUND DEFORMED AT AFT SECTION. FLOOR PANEL FABRICATED IAW ER/A 513125-14, REV.

Part: FAIRING — DELAMINATED (LT WING) · airframe 78,240 hrs · 33,780 cycles

LEFT WING INBD MAIN FLAP L/E OTBD END FAIRING DELAMINATED. LT WING INBD MAIN FLAP L/E OTBD END FAIRING COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05.

Part: FRAME — CRACKED · airframe 78,240 hrs · 33,780 cycles

FRAME CRACKED. REPAIRED IAW ER/A 513104-14AD, REV ORIG.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 78,240 hrs · 33,780 cycles

NR 2 PYLON, LT PANEL NR 447AL SKIN HOLE ELONGATED. NR 2 PYLON LT PANEL 447AL SKIN. REPLACED IAW ER/A 513112-14 REV ORIG SECTION I.

Part: FRAME — CRACKED (BS 859) · airframe 78,240 hrs · 33,780 cycles

BS 859.5, RBL 89 BELOW WL 200 FRAME TRANSITION RADIUS FOUND CRACK ABOUT 0.8" RUNNING UP. REPAIR ACCOMPLISHED IAW ER/A 513105-14AD REV ORIG SECTION I.

Part: SKIN — DAMAGED (NR 1 PYLON) · airframe 78,240 hrs · 33,780 cycles

NR 1 PYLON SKIN PANEL 437AR HAS SEVERAL SCREW HOLES ELONGATED. SKIN REPLACED IAW ER/A 513112-14 REV ORIG SECTION I.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 78,240 hrs · 33,780 cycles

NR 2 PYLON SKIN PANEL 447AR HAS A HOLE ELONGATED. REPLACED SKIN IAW ER/A 513112-14 REV ORIG.

Part: FRAME — CRACKED (BS 883) · airframe 78,240 hrs · 33,780 cycles

BS 883.5, RBL 89 BELOW WL 200 FRAME TRANSITION RADIUS FOUND CRACK ABOUT 0.4" RUNNING UP AS MARKED. REPAIR ACCOMPLISHED ER/A 513104-14AD REV ORIG SECTION

Part: SKIN — BULGED (BS 1219) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

EXTERNAL SKIN AT BS 1219, S38R FOUND BULGED. REPAIRED IAW SRM 51-10-02, 51-40-02.

Part: SKIN — DAMAGED (NR 1 PYLON) · airframe 78,240 hrs · 33,780 cycles

NR 1 PYLON SKIN PANEL 437AL HAS SEVERAL SCREW HOLES ELONGATED. SKIN REPLACED IAW ER/A 513112-14, REV ORIG SECTION I.

Part: FAILSAFE — CRACKED (BS 955) · airframe 78,240 hrs · 33,780 cycles

BS 955 RT BULKHEAK FITTING FAILSAFE STRAP FOUND CRACKED. REPAIRED IAW IAW ER/A 513102-14AD, REV ORIG.

Part: SKIN — DAMAGED (BS 1461-1502) · airframe 78,240 hrs · 33,780 cycles

EXTERNAL SKIN BETWEEN, BS 1461 TO 1502, BETWEEN STR 23-32L DAMAGED. REPAIRED IAW ER/A 513108-14, REV ORIG.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

LT WING INBD MAIN FLAP LOWER SURFACE INBD AFT EDGE PANEL FOUND BULGED. REPAIR ACCOMPLISHED IAW ER/A 513107-14, REV.

Part: STRUCTURE — DAMAGED (BS 654) · airframe 78,240 hrs · 33,780 cycles

FWD CARGO COMPT BS 654+22, RBL 35 ANCHOR NUT HOLE FOUND ELONGATED. MX REPAIRED IAW SRM 53-00-07, REPAIR 4, FIG 201.

Part: FLOORBEAM — DAMAGED (BS 434) · airframe 78,240 hrs · 33,780 cycles

FWD CARGO COMPT BS 434, LBL 20-30, FLOORBEAM ANCHOR NUTS DAMAGED. FLOORBEAM REPAIRED IAW SRM 53-00-07, REPAIR 4.

Part: FLOORBEAM — CORRODED (BS 654) · airframe 78,257 hrs · 33,785 cycles

FWD CARGO BAY BS 654 + 44, LBL 20 -44 FLOORBEAM UPPER & LWR SURFACE FOUND CORROSION. FWD CARGO STA654+44 CARGO FLOORBEAM REPLACED AND INSTALLED IAW SRM 51-10-02, 51-40-02, 51-40-05.

Part: STRUCTURE — DAMAGED (BS 1241) · airframe 78,240 hrs · 33,780 cycles

AFT CARGO BAY BS 1241 RBL 8, ANCHOR NUT HOLE ELONGATED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 4.

Part: STRUCTURE — CORRODED (BS 1197) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

AFT CARGO BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1197+66, S38-39R. MX REPLACED AS SRM 51-10-02, 51-40-05, 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 78,257 hrs · 33,785 cycles

AFT CARGO COMPT, BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1197+22, STR 38-39L. AFT CARGO STA 1197+22 BETWEEN STR 38L TO 39L SHEAR TIE CORROSION AND REMOVED IAW SRM 51-10-02, 51-20-01. BLENDED DEPTH OUT OF LIMITS SHEAR TIE REPLACED AND INSTALLED IAW SRM 51- 10-02, 51-40-05, 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

AFT CARGO BAY BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1197+132, STR 38R - 39R. MX REPLACED SHEAR TIE IAW SRM 51-10-02, 51-40-05, 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

BS 1219, BETWEEN S39L AND S39R SHEAR TIE CORRODED. (CP 53-156-01I) MX REPLACED AND INSTALLED SRM 51-40-02, SHEAR TIE.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 78,240 hrs · 33,780 cycles

FLOORBEAM BS 325, RBL 28 -55, FOUND CORRODED, FLOORBEAM REPAIRED.

Part: SEAT TRACK — CORRODED (BS 346-350) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

BS 346-350 LBL 88, SEAT TRACK FLANGE FOUND CORRODED. MX REPLACED SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.

Part: UNKNOWN — CORRODED (BS 775) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

FWD CARGO BAY BS 775, S35L FOUND CORRODED. MAINTENANCE REPLACED IAW SRM 53-00-03, REPAIR 2, FIG 201.

Part: SUPPORT BEAM — CORRODED (BS 1461-1480) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

CARGO BAY BS 1461-1480 S24-25L FRAME SUPPORT BEAM CORRODED. MX REPLACED AND INSTALLED IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 412-434) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

FWD CARGO BS 412-434, STRINGER 34R, FOUND CORRODED. REPAIRED IAW SRM 53-00-03, REPAIR 2, FIG 201.

Part: STRUCTURE — CORRODED (BS 1439) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

BULK CARGO, BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1439, S37-38R, REPLACED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

AFT CARGO BAY SHEAR TIE FOUND CORRODED AT BS 1395, S36-37R. REPLACED IAW SRM 51-10-02, 51-40-05, 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1417) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

CARGO BAY BELOW FLOOR, SHEAR TIE FOUND CORROSION AT BS 1417, S36-37R. REPLACED SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

AFT CARGO BAY SHEAR TIE FOUND CORROSION AT BS 1395, STR 38-39R. REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1417) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

CARGO BAY BELOW FLOOR, SHEAR TIE FOUND CORROSION AT BS 1417, STR 35-36R. REPLACED SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (BS 1417) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

BULK CARGO, BELOW FLOOR SHEAR TIE FOUND CORROSION AT STA 1417, S37-38R. REPLACED IAW SRM 51-40-05, 51-10-02, 51-40-02.

Part: SHEAR TIE — DAMAGED (BS 1439) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

BULK CARGO BAY BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1439, STR 36R-37R. DAMAGED SHEAR TIE REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (BS 1285) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

AFT CARGO BELOW FLOOR SHEAR TIE FOUND CORROSION AT BS 1285, S39L-39R. REPLACED IAW SRM 51-10-02, 51-40-02.

Part: STRUCTURE — CORRODED (BS 1197) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

AFT CARGO, BELOW FLOOR SHEAR TIE FWD ATT PLATE FOUND CORROSION AT BS 1197+100, S39L-39R. REPLACED IAW SRM 51-10-02, 51-40-02.

Part: STIFFENER — CORRODED (BS 1480) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

BS 1480 LT OTBD CORRODED. FLOOR WEB SUPPORT STIFFENER REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (BS 1462-1480) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

FLOOR PANEL FOUND CORRODED AT BS 1462-1480, LBL 90-96. CRACKED FLOOR PANEL REPLACED IAW SRM 51-10-02 & SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 303) · corrosion level 2 · airframe 78,240 hrs · 33,780 cycles

BS 303, LBL 22-55, FLOORBEAM FOUND CORROSION REPAIRED IAW SRM 53-00-51, REPAIR 4, FIG 201.

Part: ENGINE — COKED (NR 1) · airframe 67,538 hrs · 30,876 cycles

WHILE WORKING MCO ON LT ENGINE OVERHEAT DETECTION SYSTEM LOOP 2 OBSERVED SEVERE COKING ON UPPER ENGINE CASE AND HEAT DAMAGE TO PYLON INSULATION AND ELECTRICAL CONNECTORS AT J BOX. INSULATION AND ELECTRICAL CONNECTORS ON PYLON REPLACED. ENGINE SENT TO SHOP FOR REPAIR / TO BE REINSTALLED ON A/C. SECURED MULTIPLE HYD AND FUEL LINES INTERNAL TO PYLON. REPLACED MAIN FUEL FEED LINE. WILL T/S OVERHEAT DETECTION SYSTEM AND RE-CHECK PYLON FOR LEAKS AFTER ENGINE IS REINSTALLED.

Part: STRUT — UNKNOWN (MLG) · airframe 65,654 hrs · 30,247 cycles

MLG SHOCK STRUT CYLINDER REPAIR IAW ERA 01-471561-14 REV A C/W ERA 01-471561-14.

Part: ATTACH FITTING — CORRODED (NLG) · airframe 63,518 hrs · 29,531 cycles

NLG W/W LT AND RT NLG TRUNNION ATTACH FITTINGS. CORROSION IN FITTING BORES AND TOOLING DAMAGED FASTENER HOLES. OVERSIZED BORES AND INSTALLED NEW ENLARGED BUSHINGS.

Part: ELBOW — CRACKED (NR 1 ENGINE) · airframe 63,475 hrs · 29,510 cycles

L ENG FIRE LP1 STATUS MESSAGE ABOUT 15 MINUTES INTO FLIGHT FOLLOWED BY ILLUMINATION OF L ENGINE FIRE WARNING LIGHTS. ENGINE SHUTDOWN IN ACCORDANCE WITH QRH. NOTE, FIRE SWITCH WAS PULLED, HOWEVER, FIRE BOTTLE WERE NOT DISCHARGED. FOUND NR 1 ENG LT HIGH PRESSURE RECOUP LINE ELBOW CRACKED WITH HOLE IN IT. REMOVED AND REPLACED ELBOW REF IPC 75-23-01-10 ITEM 475. RESET FIRE HANDLE AND GEN FIELD. PERFORMED ENG RUN ON NR 1ENG. GEN CKS NORMAL. FIRE WARNING CHKS NORMAL AND ENG INDICATIONS NORMAL ON NR 1 ENG.

Part: SKIN — DAMAGED (FS 536 S27R) · airframe 63,266 hrs · 29,442 cycles

FOUND SKIN BLENDS AT FS 536 - FS 625, AND S-27R TO S-33R.

Part: SKIN — DAMAGED (FS 522-544) · airframe 63,229 hrs · 29,430 cycles

FOUND FUSELAGE SKIN BLENDS/STA 522-540 AND STR 27R-32R.

Part: SKIN — SCRATCHED (FS 654) · airframe 63,126 hrs · 29,397 cycles

FUSELAGE SKIN FS 654 + 24 TO 654 +37 AT VHF ANTENNA BLENDS.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 61,835 hrs · 28,948 cycles

NOTICED BURNING ODOR DISCOVERED C/B G-26 FLT CONT ELEC 2R POPPED. NO OTHER ABNORMAL INDICATIONS. REPLACED CSEU PER AMM, OPS NML.

Part: FLOOR SUPPORT — WORN (BS 785-977) · airframe 59,777 hrs · 28,259 cycles

FOUND STA 785.9 TO STA 977, RBL 34, FLOORBEAM UPPER CHORD SCREW HOLES WORN BY CLIPNUTS. BLENDED DAMAGE PER SRM 53-00-04, FIG 101. TREATED AND PAINTED. LOCATION AT STA 941 REPAIRED PER SRM 53-50-51, FIG 201, REPAIR 4.

Part: STRINGER — CORRODED (BS 413-434 S35L) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 35L CORRODED BETWEEN STA 412-434. INSTALLED STRINGER SECTION PER SRM 53-00-03, FIG 201, REPAIR NR 2.

Part: STRINGER — CORRODED (BS 434-456 S34L) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 34L CORRODED BETWEEN STA 434-456. INSTALLED STRINGER SPLICE PER SRM 51-40-02, PG 1.

Part: FLOORBEAM — CORRODED (BS 632) · airframe 59,777 hrs · 28,259 cycles

FOUND CORROSION ON FWD CARGO FLOORBEAM UPPER CHORD AT STA 632, LBL 18. REPLACED CHORD SECTION 142T1060-5 PER DWG 143T1209 AND SRM 51-40-02.

Part: SKIN — WORN (BS 1772-1776) · airframe 59,777 hrs · 28,259 cycles

FOUND AFT FUSELAGE, SEC 48, STAINLESS RUBSTRIP WORN THROUGH UNDER HORIZONTAL STAB AT STA 1772-1776, STR 21L. REPAIRED AND INSTALLED SKIN PANEL PER SRM 53-80-01, FIG 201, REPAIR 3.

Part: SILL — CORRODED (R2 DOORWAY) · airframe 59,777 hrs · 28,259 cycles

FOUND R2 DOORWAY LWR SILL, FLOOR SUPPORT TEE (REF P/N 146T0051-26) VERTICAL FLANGE EXFOLIATED BETWEEN MIDDLE AND AFT SECTION. REPLACED FLOOR SUPPORT TEE PER SRM 51-40-02 PG 1.

Part: FRAME — CRACKED (BS 1725) · airframe 59,777 hrs · 28,259 cycles

FOUND SMALL CRACK AFT SIDE OF FRAME AT STA 1725.5 2:00 POSITION. REPAIRED PER SRM 53-80-01 REPAIR 5 FIG 201 DETAIL 3.

Part: FLOORBEAM — CORRODED (BS 698) · airframe 59,777 hrs · 28,259 cycles

FOUND CORROSION ON FWD CARGO FLOORBEAM UPPER SURFACE AT STA 698, LBL 19. REPLACED UPPER CHORD SECTION PER SRM 51-40-02, PG 1.

Part: STRINGER — CORRODED (BS 412-434 S35R) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 35R AT STA 412-434 CORRODED. REPAIRED PER SRM 53-30-03, FIG 201, REPAIR 1.

Part: STRINGER — CORRODED (BS 412-434 S38R) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 38R STA 412-434 CORRODED. REPAIRED PER SRM 53-00-03 FIG 201 REPAIR 2.

Part: STRINGER — CORRODED (BS 412-456 S36R) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 36R STA 412-456 CORRODED. REPAIRED PER SRM 53-30-03 FIGURE 201 REPAIR 1.

Part: STRINGER — CORRODED (BS 434-456 S37L) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 37L STA 434-456 CORRODED. REPAIRED PER SRM 53-30-03 FIG 201 REPAIR 1.

Part: STRINGER — CORRODED (BS 500-522 S38R) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 38R STA 500-522 CORRODED. STRINGER REPAIRED PER SRM 53-00-03 FIG 201, REPAIR 2.

Part: STRINGER — CORRODED (BS 412-434 S37R) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 37R STA 412-434 CORRODED. REPAIRED PER SRM 53-30-03 FIG 201 REPAIR 1.

Part: STRINGER — DEFORMED (BS 434-456 S34R) · airframe 59,777 hrs · 28,259 cycles

FOUND STRINGER 34R DEFORMED AT STA 434-456. REPAIRED PER SRM 53-30-03 FIG 201 REPAIR 1.

Part: FITTING — SCORED (PYLON) · airframe 59,777 hrs · 28,259 cycles

DURING THE ACCOMPLISHMENT OF BOEING S/B 767-54-0081 R1 WHILE IN HMV AT ACTS THE OUTBOARD PYLON SIDE LOAD FITTING BORE WAS WITH DEEP SCORE MARKS AND OVERSIZED TO 2.244" WHICH EXCEEDS S/B CLEANUP LIMITS. THIS IS SUBJECT TO AD 2004-16-12. THE DAMAGE WAS CLEANED UP AND A REPAIR BUSHING WAS INSTALLED. AN AMOC WAS RECIEVED AND DOCUMENTED PER ER/A 459797-14.

Part: STRINGER — CORRODED (BS 412-434 S36L) · airframe 57,194 hrs · 27,254 cycles

FOUND STRINGER 36L CORRODED BETWEEN STA 412-434. INSTALLED STRINGER SPLICE PER SRM 51-40-02 PG 1.

Part: PULLEY — FRACTURED (RT WING SLIDE) · airframe 56,663 hrs · 27,033 cycles

WHILE PERFORMING OPN 7013 RIGHT FWD DOOR OVERWING SLIDE DOOR ACTUATOR CHANGE FOUND THE DOOR CABLE PULLEY BROKEN AND CABLE OFF OF PULLEY IPC REF 25-65-51-01-ITEM 730. REPLACED PULLEY AND REINSTALLED CABLE, C/W OPN 7013 SLIDE DOOR ACTUATOR CHANGE.

Part: ENGINE — MAKING METAL (NR 1) · airframe 53,759 hrs · 25,801 cycles

LT ENGINE OIL FILTER MSG IN FLIGHT RETARDED LT ENGINE TO IDLE WITH MSG STILL THERE SHUTDOWN LT ENG IN FLIGHT. CHECKED SCAVENGE FILTERS AND ALL CHIP DETS FOUND HEAVY FUZZON MASTER CHIP DET LARGE AMOUNT OF SHINY FLAKES ON AFT B-SUMP DET FOUND TWO OR THREE SHINY CHIPS ON FWD B-SUMP DET, ALL OTHER DETECTORS OK. REPLACED NR 1 ENGINE.

Part: ENGINE — MAKING METAL (NR 1) · airframe 53,759 hrs · 25,801 cycles

LEFT ENG OIL FILTER MESSAGE. DID NOT EXT WITH THROTTLE REDUCTION. OIL PRESS AND TEMP NORMAL. PERFORMED ENG SHUTDOWN PER QRH. DIVERTED TO JAX. DEBRIS FOUND ON CHIP DETECTORS. REPLACED ENGINE.

Part: CHARGER — INOPERATIVE (ROW 35) · airframe 53,310 hrs · 25,571 cycles

EMERGENCY LIGHTS INOP ROW 35 AFT BOTH SIDES. REPLACED M9010 BATTERY CHARGER ASSY.

Part: GASKET — FAILED (NR 1 ENGINE) · airframe 50,723 hrs · 24,264 cycles

ON LANDING ROLL TOWER REPORTED SMOKE AND FUEL COMING FROM LT ENG AFTER TOUCHDOWN ALL LEFT ENGINE INDICATION VERY LOW. TURNED FUEL SWITCH OFF. MTC FOUND FUEL LINE FROM PUMP TO MEC GASKET BAD. REPLACED GASKET. RAN ENGINE. CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,286 hrs · 24,035 cycles

ON LAYOVER FOUND LT OVERHEAD EMERGENCY LIGHT OUT. REPLACED BATTERY PACK.

Part: PROJECTOR — FAULTY (CABIN) · airframe 46,588 hrs · 22,200 cycles

AT CRUISE F/A'S NOTICED SMELL IN MID CABIN AREA. TENTATIVE IDENTIFIED AS PROJECTOR 525. ALL PROJECTORS TURNED OFF FOR DURATION OF FLT. PROJECTOR VERIFIED AS HAVING ELECT SMELL. DEACTIVATED PROJECTOR, FWD TO MCO AND PLA-MEL 25-20-02L.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 43,409 hrs · 20,677 cycles

EMERGENCY FLASHLIGHT AT 1L NOT FLASHING. FOUND DURING LAYOVER CHECK. REPLACED SAME.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,107 hrs · 20,533 cycles

CRACKS FOUND IN THE RBL 54.75 OVERWING LONGITUDINAL FLOORBEAM AT FS 788 IN THE UPPER CHORD. THE CHORD WILL BE TRIMMED AND A NEW SECTION SPLICED IN.

Part: RELAY — FAILED (CABIN) · airframe 42,975 hrs · 20,473 cycles

SQUIB TEST N1 RT OVERWING LIGHT WILL NOT TEST. T/S PER FIRM AND M/M REPLACED K 839 AND BATTERY PACK ON RIGHT SIDE OVERWING SLIDE, OPS NORMALLY OK FOR SERVICE PER MM.

Part: SEQUENCE VALVE — MALFUNCTIONED (RT MLG) · airframe 40,161 hrs · 19,120 cycles

RT MAIN GEAR TOOK VERY LONG TO COME DOWN AND LOCK APPROX 5 MIN, IT EVENTUALLY SIGNALED DOWN AND LOCKED LANDING UNEVENTFUL. REPLACED SEQUENCE VALVE AND LUBED GEAR.

Part: LIGHT — MISSING (SEAT 33 & 45)

ON L/O, FOUND SEATS 33AB AND 45AB MISSING EMERGENCY PATH LIGHTING FIXTURES. INSTALLED EMERGENCY PATH LIGHTING FIXTURES AT 33AB AND 45AB.

Part: BATTERY PACK — INOP (CABIN)

EMERGENCY LIGHT INOP. REPLACED BATTERY RACK.

Part: AIR DISTRIBUTION — ODOR (GALLEY)

AT TOP OF DESCENT INTO ATL, WE HAD A REPORT OF ELECTRICAL FUMES AT THE 2R DOOR (NEAR AFT GALLEY). WE PULLED ALL BREAKERS IN GALLEY, SHUTOFF LIGHTS AND CKED AFT RIGHT LAV. WHILE LATE INTO DESCENT, THE SMELL OF ELECT FUMES WAS DISSIPATING. ALL PROCEDURES WERE EXECTUTED IAW THE POM FROM THE C/PIT. TURNED ON ALL POWER TO GALLEY AND LAV INCLUDING LIGHTS, CHECKED ABOVE CEILING AND BELOW FLOOR. NO FUMES PRESENT AND NO PROBLEMS FOUND.

Part: SKIN — GOUGED (BS 1109)

THE FUSELAGE SKIN SUFFERED A DEEP GOUGE AT FS 1109 AND S-19R FROM A DAMAGED SECTION OF ADJACENT FAIRING. THE DAMAGED AREA OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 366133-14, REV A.

Part: LINE — WORN (NR 2 ENGINE)

RIGHT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO SOON AFTER TAKEOFF. COMPLETED POM PROCEDURES AND RETURNED FOR LANDING. PER CREW COMMENT ENGINE HYD PUMP DID NOT RUN DRY. NO PRESSURE LOSS NOTED. ENGINE PUMP SHUT DOWN PRIOR TO PRESSURE LOSS. FOUND NR 2 ENGINE HYD PRESSURE LINE WORN THRU. REPLACED HYD LINE (P/N 291201624). SERVICED RIGHT HYD SYSTEM. ENGINE RUN LEAK CHECK OPN CHECK OK.

Part: SKIN — DENTED (BS 450)

FUSELAGE/SKIN, FS 434-500, STRG 32R-38R, SKIN SPLICE REPAIR. THE FUSELAGE SKIN BETWEEN FS 434 AND 500 AND BETWEEN STRINGERS 32R AND 38R WAS BADLY DENTED OR TORN FROM A GROUND EQUIPMENT IMPACT. THE DAMAGED SECTION OF SKIN WAS TRIMMED AWAY AND A NEW SECTION OF SKIN WAS SPLICED IN PER ER/A 364572-14, REV B.

Part: LIGHT — INOPERATIVE (CABIN)

PIREP - EMERGENCY OVERWING RIGHT EMERGENCY TRACK LIGHTING FLOOR LIGHT DAMAGED. REINSTALLED LIGHT IN FLOOR TRACK.

Part: HYD LINE — LEAKING (CTR HYD SYST)

CTR HYD SYS FAILED WHEN LOWERING MLG. FOUND PRESS LINE FROM ADP TO BULKHEAD LEAKING. REPLACED LINE, SERVICED HYD SYS AND HAD 1.8 GAL REMAINING. LEAK CKD OK.

Part: ENGINE — FAILED (NR 1)

LT ENG FAILED ON T/O WITH LOAD BANG AND SHUT ITSELT DOWN.

Part: WIRE — DAMAGED (CABIN)

EMERGENCY FLOOR TRACK WIRING AT MID GALLEY IS DAMAGED. REPAIRED DAMAGED WIRING.

Part: SKIN — CRACKED (FS 445/490)

THE FUSELAGE SKIN AT FS 445 AND FS 490 BETWEEN STR 33R AND34R ON THE RT SIDE WERE FOUND WITH PREVIOUS DAMAGE. ALSO A CRACK WAS FOUND AT FS 500 STR 38. THE CRACK WAS CUT OUT, REINFORCED AND THE PREVIOUS DAMAGE HAD UPDATED REPAIRS.

Part: TE WEDGE — DELAMINATED (NR 5 LE SLAT)

THE NR 5 LEADING EDGE SLAT ON THE LT WING WAS DELAMINATED ON THE T/E WEDGE. THE DAMAGE IS AT THE AFT, I/B CORNER WITH 3.5 INCH DIA COVERAGE. IN ADDITION, THE NR 5 SLAT WAS FOUND WITH AN UNIDENTIFIED PREVIOUS REPAIR EXTENDING FROM THE I/B EDGE OF THE TRAILING EDGE WEDGE TO THE EDGE OF THE NEW DAMAGE LOCATION. THIS REPAIR WILL BE REMOVED AND INCORPORATED INTO THE CURRENT REPAIR SCHEME PER DL ERA 273469-14 REV A.

Part: SKIN — DELAMINATED (NR 4 LE SLAT)

THE NR 4 LEADING EDGE SLAT WAS FOUND WITH THE UPPER SKIN DELAMINATED AT THE T/E WEDGE. THE DAMAGE IS ON THE LT WING WITH THE LOCATION OF THE DAMAGE 4 INCHES FROM TE, 81 FROM I/B EDGE AND 3 INCHES IN DIA. ACCOMPLISHED REPAIRS PER DL ERA 273469-14 RA.