N607DL

Part: ENGINE — LEAKING (NR 1) · airframe 63,615 hrs · 33,460 cycles

ON T/O OUT OF ATL, F/C ALARM WENT OFF WITH BURNING ODOR OF RUBBER OR PLASTIC. REPLACED NR 1 ENGINE FOR INTERNAL OIL LEAK.

Part: CHIP DETECTOR — CRACKED (NR 1 IDG) · airframe 63,408 hrs · 33,381 cycles

EICAS MSG LEFT GENERATOR DRIVE DISPLAYED. SERVICED OIL. REPLACED CRACKED CHIP DETECTOR.

Part: ODOR — DETECTED (AFT CABIN) · airframe 62,572 hrs · 33,050 cycles

ON TAXI OUT UNIDENTIFIED ODOR POSSIBLY ELECTRICAL NOTED IN AFT PART OF A/C NEAR AFT F/A. UNABLE TO CONFIRM, IDENTIFY, OR LOCATE SOURCE. CHECKED FOR ODOR IN AFT CABIN AREA, NONE FOUND. CHECKED AFT CARGO COMPT AND AFT E/E RACK, NO ODOR DETECTED.

Part: SILL — CORRODED (FUSELAGE) · airframe 56,410 hrs · 30,366 cycles

THE OUTER CHORD OF THE C1 DOOR LOWER SILL WAS FOUND CORRODED. TO REPLACE THE CHORD, THE FS 620 FRAME OUTER CHORD AND WEB WERE CUT AND LOWER ENDS REMOVED. A NEW SILL CHORD WAS INSTALLED AND LOWER FRAME SECTION REINSTALLED WITH REPAIR ANGLE SPLICES. THE WORK WAS ACCOMPLISHED PER ER/A 383339-14, REV A.

Part: SKIN — DENTED (FS 598, S-14L) · airframe 56,410 hrs · 30,366 cycles

FUSELAGE / SKIN / FS 598 / STRG. 14L-15L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS 598 BELOW THE STRINGER 14L SKIN LAP JOINT. THE DENT WAS REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 383418-14, REV A.

Part: SKIN — DENTED (FS 1617, S-17R) · airframe 56,410 hrs · 30,366 cycles

FUSELAGE / SKIN / FS 1617 / STRG. 17R : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED AT FS 1617 JUST BELOW STRINGER 17R. THE DENT WAS REMOVED WITH A CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 383406-14, REV A.

Part: SKIN — DENTED (FS 1670, S-18R) · airframe 56,410 hrs · 30,366 cycles

FUSELAGE / SKIN / FS 1661-1680 / STRG. 18R-19R : DENT REPAIR THE FUSELAGE SKIN BETWEEN FS 1661 & 1680 AND BETWEEN STRINGERS 18R & 19R WAS FOUND DENTED. THE DENT WAS REMOVED WITH A CUTOUT AND REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383296-14, REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,410 hrs · 30,366 cycles

THE FUSELAGE SKIN WAS FOUND WITH 2 TIME-LIMITED SKIN REPAIRS FWD AND AFT OF THE FS 1720 BULKHEAD AND BETWEEN STRINGERS 29L & 29R. THE PREVIOUS REPAIR AREAS WERE CUTOUT TO COMPLETELY REMOVE ALL EXISTING FASTENER HOLES. THE CUTOUTS WERE REPAIRED WITH 2 EXTERNAL DOUBLERS EACH PER ER/A 383392-14, REV A.

Part: SKIN — DENTED (FS 280, WL 205) · airframe 56,410 hrs · 30,366 cycles

FUSELAGE / SKIN / FS 278-288 / WL 200-208 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 278 & 288 AND BETWEEN WL 200 & 208. THE DENT WAS REMOVED WITH A 5" X 5.2" CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383331-14, REV A.

Part: SKIN — GOUGED (FUSELAGE) · airframe 56,410 hrs · 30,366 cycles

THE FUSELAGE SKIN WAS FOUND WITH A DENT AND GOUGE AT THE STRINGER 14L LAP JOINT AT FS 1691. THE DAMAGE WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383291-14, REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,410 hrs · 30,366 cycles

THE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE UPPER CAP FLANGE WAS TRIMMED OFF ALONG THE ENTIRE LENGTH OF THE BEAM TO REMOVE ALL OF THE CORROSION. A NEW ALUMINUM EXTRUSION CAP WAS FABRICATED AND INSTALLED PER ER/A 383326-14, REV A.

Part: SKIN — WORN (CARGO DOOR) · airframe 56,410 hrs · 30,366 cycles

THE NR 2 CARGO DOOR OUTER SKIN WAS FOUND WORN BEYOND SRM LIMITS. REPAIR PER ER/A 417449-14.

Part: CLAMP — FAILED (HYD SYSTEM) · airframe 56,086 hrs · 30,207 cycles

FUEL SUPPLY LINE CHAFED THROUGH IN LEFT ENG STRUT. CHAFING CAUSED BY FAILED HYD TUBE CLAMP/BRACKET ABOVE FUEL LINE. REPLACED FUEL LINE AND LEAK CHECKED. REPAIRED CLAMP PER ER/A 382986-14.

Part: OUTFLOW VALVE — INOP (CABIN)

CABIN ALTITUDE AUTO INOP ON T/O. REPLACED OUTFLOW VALVE.

Part: LATCH ROLLER — OUT OF ADJUST (PAX DOOR)

LT AFT ENTRY DOOR EICAS LIGHT INFLIGHT WITH AN ENTRY DOOR LIGHT ON FINAL APPROACH THE DOOR OPENED. 37,000 FT WHEN LIGHT CAME ON. CREW MADE EMERG DESCENT. ADJUSTED LATCH ROLLER OVER CTR PER MM AND ADJUST ESCAPE SLIDE HEIGHT. CHECKS GOOD.

Part: POWER SUPPLY — SHORTED (CABIN)

FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM FLOOR WIRING EXPOSED, SOME LIGHTS INOP. REPAIRED FLOOR PROX EMERG ESCAPE PATH TRACK WIRING AND REPLACED F/C POWER SUPPLY MODULE, ALL OPN NOW NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

F/A FOUND 2R ATTENDANT FWD FLASHLIGHT BATTERY DEAD.REPLACED BATTERY AND BULB. OLD BULB OPS GOOD.

Part: TE WEDGE — DELAMINATED (WING)

TRAILING EDGE WEDGE UPPER AND LOWER SKIN DELAMINATED AT INBOARD END. REPLACED TRAILING EDGE WEDGE. REF SRM 57-43-02.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, FOUND AFT 3 LT AISLE EMERGENCY LIGHT INOP. REPLACED M737 BATTERY PACK EMERGENCY LIGHTS AND CK NORMAL.

Part: LENSE — CRACKED (CABIN)

EMERGENCY LIGHT/EXIT SIGN AT R-1 DOOR FOUND WITH CRACKED LENS. REPLACED EXIT SIGN LIGHT ASSEMBLY AND LENS, OPERATION NORMAL.

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

T/E WEDGE WAS FOUND TO BE DELAMINATED DURING SHOP INSPECTION FOR NR 5 L/E SLAT. THE NOTED T/E WEDGE WAS REPLACED PER SRM 57-43-02.

Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)

DURING INSPECTION, FOUND FWD CABIN EMERGENCY TRACK LIGHT INOP. REPLACED F/C EMERGENCY LIGHT POWER PACK. FOUND BROKEN GROUND STUD IN OVERHEAD INSTALLATION. REPLACED GROUND STUD, OPS NORMAL.

Part: HARNESS — BURNED (FS 700)

WHILE TROUBLESHOOTING PROBLEM FOR RT AFT MAIN FUEL BOOST PUMP, A BURNING ODOR WAS REPORTED IN THE AFT CABIN. AIRCRAFT POWER WAS REMOVED AND ODOR INVESTIGATED. FOUND WIRE BUNDLE W4216 AND W4106 SHORTED AND BURNED, WITH 60 WIRED IN BUNDLE W4216 COMPLETELY BURNED THROUGH. DAMAGE WAS LOCATED IN FWD FUSELAGE FS 700, APPARENT CAUSE WAS WIRE CHAFING ON CLAMP. ALL WIRES WERE REPAIRED AND AFFECTED SYSTEMS TESTED NORMAL.