N625DL

Part: SKIN — DENTED (BS 1650 S20R) · airframe 72,977 hrs · 35,316 cycles

FOUND DENT AT OVERLAPPING SKIN BELOW AND FWD OF R4 DOOR, APPROX STA 1650 STR 20R. REPAIR IAW ERA 474887-14.

Part: SKIN — DENTED (BS 360 S17L) · airframe 72,977 hrs · 35,316 cycles

FUSELAGE DENTED AT STA 620 BELOW STR 17L REPAIRED IAW ERA 474836-14.

Part: SLIDE — UNWANTED DEPLOY (4L DOOR) · airframe 72,455 hrs · 35,093 cycles

WHILE T/S 4L DOOR ARMING LEVER BEING HARD TO OPERATE 4L DOOR SLIDE DEPLOYED. REPLACED DOOR SLIDE AND EMERGENCY DOOR RESERVOIR PER M/M. CLEANED AND LUBED MECHANISMS. OK FOR SERVICE.

Part: GIRT BAR — JAMMED (L2 DOOR) · airframe 59,705 hrs · 29,818 cycles

A/C WOULD NOT PRESSURIZE AFTER T/O. OUTFLOW VALVE FULLY CLOSED, FOUND L2 DOOR GIRT BAR JAMMED IN FWD END OF DOOR. REPLACED BAR AND FITTINGS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,125 hrs · 29,155 cycles

ON LAYOVER, FOUND TRACK LIGHTS INOP AT 3D AND 12D. RELAMPED, OPN OK.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 55,698 hrs · 28,198 cycles

IR/ IVSI C/B POPPED OUT, ACCOMPANYING BURNING ODOR FROM IVSI. FOUND IVSI IND C/B POPPED F/O`S SIDE. INSTALLED NEW IVSI IND. OPS OK. F/O`S IND CAUSE OF BURNING ODOR .

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 55,402 hrs · 28,071 cycles

LIGHTING STRIKE REPAIR LIGHTING STRIKE DAMAGE WAS FOUND ON THE UPPER SKIN AT THE STRINGER 4R SKIN LAP JOINT AT FS 1242. THE DAMAGE WAS REMOVED WITH A CUTOUT TO THE UPPER SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED IAW ER/A 087125-14, REV A.

Part: FAN — SEIZED (E/E BAY) · airframe 52,925 hrs · 26,939 cycles

AFTER TWO HOURS OF FLIGHT, STRONG ELECTRICAL/SULPHUR SMELL NOTED IN CABIN AND COCKPIT. ALSO GOT EQUIP OVERHEAT EICAS AND LIGHT. LIGHT WENT OUT AFTER SELECTING OVERRIDE. FOUND FWD EQUIPMENT SUPPLY FAN NR 1 SEIZED. REPLACED FAN AND SYSTEM NOW OPERATES NORMALLY.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 51,958 hrs · 26,433 cycles

AT 10,000 FEET RT ENG SURGED, EGT WENT TO 678, A/C PITCHED LEFT. C/W ENG SURGE CK LIST, PER F/A SPARKS STILL COMING FROM RT ENG. C/W RT ENG SHUTDOWN. REPLACED NR 2 ENGINE.

Part: LIGHT — DAMAGED (CABIN) · airframe 49,447 hrs · 25,234 cycles

PASSENGER SEAT 26D EMERGENCY LIGHT DAMAGED, INSTALLED NEW SEAT MOUNTED LIGHT.

Part: ACM — INOP (LEFT)

PILOT REPORTED SMOKE IN COCKPIT, AFTER T/R DEPLOYMENT ON TOUCHDOWN. LT PACK TRIPPED SHORTLY THEREAFTER. REPLACED LT ACM, OPERATIONAL CHECK NORMAL.

Part: SKIN — DAMAGED (NR 5 LE SLAT)

NR 5 LE SLAT / TE WEDGE REPLACEMENT - FASTENER SUB. DURING ACCOMPLISHMENT OF TE WEDGE REPLACEMENT PER B757 SRM 57-54-02, FIGURE 202, TWO HOLES COMMON TO THE WEDGE AND THE UPPER SKIN WERE ELONGATED. AUTHORIZED USE OF OVERSIZED FASTENERS.

Part: STRAP — CORRODED (BS 1440)

CORROSION WAS FOUND IN THE LWR AFT CORNER OF THE INNER STRAP FOR THE C2 DOOR. REPAIRED PER ERA 333195-14, REV A.

Part: SKIN — CRACKED (NR 2 NACELLE)

THE NR 2 ENG NACELLE STRUT SKIN WAS FOUND WITH MULTIPLE CRACKS IN THE RT SIDE SKIN PANEL. REPAIRED PER ERA 333163-14, REV A.

Part: SKIN — DENTED (BS 970)

DAMAGE FOUND IN THE FUSELAGE SKIN AT BS 970, S3R. DAMAGE CUTOUT MEASURES APPROX 4 BY 4. REPAIRED PER ERA 333189-14.

Part: SKIN — DENTED (BS 920)

DAMAGE FOUND TO FUSELAGE SKIN AT BS 920, S3R. DAMAGE CUTOUT WAS APPROX 4 BY 4. REPAIRED PER ERA 333190-14.

Part: SKIN — CRACKED (NR 1 NACELLE)

THE NR 1 ENG NACELLE STRUT SKIN WAS PREVIOUSLY FOUND CRACKED AND REPAIRED. ADDITIONAL CRACKING WAS FOUND DURING THE CURRENT VISIT. THE NEW CRACK WAS APPROX 1 INCH IN LENGTH. REPAIRED PER ERA 333162-14, REV A.

Part: BATTERY — DISCHARGED (CABIN)

F/C EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY PACK.

Part: WEDGE — DENTED (NR 6 LE SLAT)

THE NR 6 L/E SLAT WAS PUNCTURED ON ITS UPPER SURFACE, 16 OB FROM THE IB EDGE, AND 3 FWD OF THE TE. THE TE WEDGE IS MF FROM ALUMINUM HONEYCOMB WITH ALUMINUM FACESHEETS. THE TE WEDGE IS THE SUBJECT OF TWO AD'S, THEREFORE THIS ER/A WILL AUTHORIZE REPAIR.

Part: FSEU COMPUTER — FAILED (TE FLAPS)

ON FINAL APPROACH, FLAPS LOCKED OUT AT 1 UNIT WITH A TE ASYM EICAS MSG AND TE FLAP LT. CREW COMPLIED WITH POM TROUBLESHOT SYSTEM PER FIM 27-51-00. REPLACED NR 1 FSEU, FLAP OPN NML.

Part: FIRE CARD — MALFUNCTIONED (CARGO COMPT)

UPON TAKEOFF ROLL, CARGO FIRE EICAS MSG PLUS WARNING ILLUM. ABORTED TAKEOFF AT 25 KIAS. BRAKES NOT USED. REPLACED CARGO FIRE DETECT CARD (M10427). ALL OPN CKS NORMAL. DETECTORS ALSO CHECK GOOD.

Part: FUEL LINE — CRACKED (NR 1 PYLON)

ON PREFLIGHT, FOUND FUEL LEAK IN PYLON AREA OF NR 1 ENGINE. FOUND FUEL FEED LINE LEAKING DUE TO CRACK AT FLANGE, FWD END OF LINE. REPLACED FUEL FEED LINE.

Part: LIGHT — MISSING (CABIN)

DURING INSPECTION, FOUND THREE EMERGENCY TRACK LIGHTS MISSING. REPLACED LIGHT ASSEMBLIES AND OPERATION NORMAL.

Part: CONTROL PANEL — FAILED (FLT DECK)

ON TAKOFF ROLL HAD SMELL OF ELECTRICAL BURNING. FOUND LEFT RUNWAY TURNOFF LIGHT SWITCH BAD. REPLACED CONTROL PNL FOR TAXI/RUNWAY TURNOFF AND FLOODLIGHTS, OPERATION NORMAL.

Part: COFFEE MAKER — SMOKING (FWD GALLEY)

DURING CRUISE, F/A REPORTED SMOKE COMING OUT OF FORWARD GALLEY COFFEE MAKER. POWER WAS REMOVED AND AS PRECAUTION PORTABLE FIRE EXTINGUISHER WAS USED. COFFEE MAKER WAS REPLACED, OPERATION NORMAL.

Part: EEC — FAILED (NR 2 ENGINE)

ON DESCENT INTO MSP, NR 2 ENGINE FLAMED-OUT, HAD SUCCESSFULL RESTART, LANDED MSP. PER FIM REPLACED EEC, ALT AND RT PDIU PER M/M. RUN UP OK PER M/M.