N813DE

Part: AILERON — PUNCTURED (LH WING) · airframe 29,786 hrs · 4,656 cycles

WING / LH / INBD AILERON / INBD TRAILING EDGE : GROUND DAMAGE REPAIR THE UPPER SKIN, TRAILING EDGE WEDGE, AND INBD CLOSEOUT RIB OF THE LH WING INBD AILERON WERE DAMAGED WHEN THE AIRCRAFT STRUCK A MTC. WORK STAND. THE DAMAGED SECTION OF UPPER SKIN WAS CUT AND REMOVED AND A NEW SECTION SPLICED IN WITH AN ALUMINUM DOUBLER. NEW SECTIONS OF RIB CAP WERE SPLICED IN WITH ALUMINUM ANGLES, AND THE WEDGE SECTION REPLACED. THE REPAIR WAS ACCOMPLISHED PER ER/A 418035-14, REV A.

Part: SKIN — PUNCTURED (FS 2000, L-46L) · airframe 29,786 hrs · 4,656 cycles

FUSELAGE / SKIN / FS 1997-2015 / L-45L-47L : GROUND EQUIPMENT PUNCTURE REPAIR THE FUSELAGE SKIN WAS PUNCTURED BY A WORK STAND BETWEEN FS 1997 & 2015 AND BETWEEN LONGERON 45L & 47L. THE DAMAGE WAS REMOVED WITH A 19" X 6" CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM DOUBLERS PER ER/A 384125-14, REV A.

Part: SKIN — PUNCTURED (FS 2140, L-36R) · airframe 29,786 hrs · 4,656 cycles

FUSELAGE / SKIN / FS 2122-2145 / LONG. 36R-37R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 2122 & 2145 AND BETWEEN LONGERONS 36R & 37R WHEN THE AIRCRAFT STRUCK A MTC. WORK STAND. THE DAMAGE WAS REMOVED WITH A 24" X 6" CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384123-14, REV A.

Part: SPAR CAP — CRACKED (XE 50) · airframe 29,786 hrs · 4,656 cycles

HORIZ STABILIZER / RH / REAR SPAR / LOWER CAP : GROUND DAMAGE REPAIR THE RH HORIZONTAL STABILIZER REAR SPAR LOWER CAP STRUCK A WORK PLATFORM DURING A TOWING OPERATION. THE AFT FLANGE OF THE LOWER CAP WAS CRACKED BETWEEN XE 49 & 61. THE CRACK WAS REMOVED BY TRIMMING OFF THE AFT FLANGE OVER A 12" LENGTH. THE TRIMMED ARE WAS REPAIRED WITH AN ALUMINUM REPAIR ANGLE AND REPAIR STRAP PER ER/A 384119-14, REV A.

Part: SOCKET — SHORTED (SEAT 34H) · airframe 28,060 hrs · 4,339 cycles

2030 5/16/02 DURING PREFLIGHT INSPECTION EMERGENCY LIGHT TEST FAILED WITH A EMERGENCY LIGHT BATTERY LOW MESSAGE REPLACED BATTERY 4 AND CHARGER NO HELP FOUND IN SEAT LIGHT SOCKET AT 34H SHORTED. RPLD SAME.

Part: WIRE — DISCONNECTED (CABIN) · airframe 24,558 hrs · 3,738 cycles

ON L/O FOUND EMERGENCY LIGHTS AT SEAT 32Â¥ 33Â¥ 34, 35 INOP. RECONNECTED WIRE SPLICE AT SEAT 32Â¥, ALL SEAT LIGHTS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,502 hrs · 3,231 cycles

EMERGENCY LIGHT AFT OF 2R DOOR INOP. RELAMPED.

Part: TRANSFORMER — FAILED (AC ELECTRICAL) · airframe 19,640 hrs · 2,970 cycles

AUTOSLAT FAIL NR 3 OIL PRESS INVALID AND NR 3 HYD QTY INVALID ANNUNCIATED. FOUND TRANSFORMER T1-33 FAILED. SWAPPED WITH AFT CARGO LOADNG TRANSFORMER T1-187, NBR 3 28VAC BUS OPS NORMAL. NOTE: C/B WAS POPPED NR 3 XFER BUS.

Part: TRANSFORMER — FAILED (AC ELECTRICAL) · airframe 19,640 hrs · 2,970 cycles

EN ROUTE ATL-LGW, HAD AUTOSLAT FAIL, NR 3 OIL PRESS INVALID AND NR 3 HYD QUANTITY INVALID ANNUNCIATED. DIVERTED TO JFK. SWAPPED TRANSFORMER WITH UNIT INSTALLED IN LOCATION T1-187 AFT CARGO LOADING SYSTEM. NR 3 28VAC BUS, OPS NOW NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

JUMPSEAT 4R EMERGENCY FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED JUMPSEAT 4R EMERGENCY FLASHLIGHT BATTERY AND CHARGING CHECKS OK. STRAP INSTALLED.

Part: ENGINE — UNRESPONSIVE (NR 3)

NR 3 ENGINE APPEARED TO FLAME-OUT DURING DESCENT. DID NOT RESPOND WHEN PWR INCREASE. CREW SHUTDOWN ENG. REPLACED EEC.

Part: WIRE — SHORTED (ROW 11C)

WHEN OPERATING B/C SEAT 11C SPARKS AND SMOKE CAME FROM UNDER SEAT. FOUND HARNESS SHORTED TO FOOT REST ACTUATOR. REPAIRED SAME.

Part: SKIN — GOUGED (BS 990)

THE C1 DOOR FUSELAGE SURROUND SKIN WAS DAMAGED NEAR THE LOWER AFT CORNER OF THE DOOR CUTOUT. THE DAMAGE WAS TO THE OUTER SKIN ONLY. THE SKIN WAS CUT AWAY WITH A 3 X 4 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 368029-14.

Part: OXY GENERATOR — ACTIVATED (SEAT 2A & 2B)

MASK AT SEATS 2A AND 2B CAME DOWN ON LANDING GENERATORS ACTIVATED COULD SMELL IT. REPLACED GENERATOR AND REPACKED MASKS.

Part: STRUCTURE — TAIL STRIKE (BS 1862-2047)

UPON LANDING IN CAMBRIDGE, ENGLAND THE AC EXPERIENCED A TAIL STRIKE. DAMAGE EXTENDS FROM FS 1865 TO FS 2039 AND IS BETWEEN APPROX L49R AND JUST O/B OF L50L. BESIDES THE FUSELAGE SKIN ASSEMBLY DAMAGES, THE AFT PRESSURE BLKHD WAS DAMAGED. REPAIRED PER ERA 367462-14.

Part: STRUCTURE — DAMAGED (TAIL)

TAIL STRIKE ON LANDING CBG. FUSELAGE/PRESSURE BULKHEAD DAMAGE. SKIN AND STRUCTURAL DAMAGE TO BE REPAIRED PER ERAS AND SRM AS APPLICABLE.

Part: SMOKE DETECTOR — MALFUNCTIONED (NR 2)

NUMBER 2 SMOKE DETECTOR C/B PULLED DUE TO ERRONEOUS LAV SMOKE INDICATIONS. ERRONEOUS LAV SMOKE INDICATIONS DID NOT REOCCUR. C/B NOT RESET, NO FURTHER DIAGNOSIS ATTEMPTED BY FLIGHT CREW. INSPECTED SMOKE DETECTOR AND FOUND NO DEFECTS. REPLACED NR 2 LAV SMOKE DETECTOR CAPTS SIDE F/C AS PRECAUTIONARY, PERFORMED SATISFACTORY OPERATIONAL TEST ALL OK.

Part: COMPRESSOR — DAMAGED (NR 3 ENGINE)

AT APPROX 95 KTS ON TAKEOFF, COMPRESSOR STALL ON RT ENGINE. REPLACED ENGINE.

Part: PINS — PULLED (L 2 DOORSLIDE)

FOUND L2 DOOR SLIDE PINS PULLED OUT OF SLIDE PACK. REPLACED PACK.

Part: FIRE BOTTLE — LOW CHARGE (4L DOOR)

HALON FIRE BOTTLE AT 4L IS LOW.