N80057

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR LENS INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHT AT AFT CABIN RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT CABIN RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SERVO VALVE — INOPERATIVE (SPOILER)

MIA INFLIGHT T1075/24AUG MCO - SJU EXPERIENCED VIBRATIONS AND FOUND THE NUMBER FIVE SPOILER WAS FLOATING. TURNED OFF YELLOW SERVO CONTROLLER AND VIBRATIONS STOPPED BUT NUMBER THREE SPOILLER POPPED. DECLARED AN EMERGENCY AND DIVERTED IN MIA. LANDED WITHOUT INCIDENT. REPLACED LEFT NUMBER FIVE SPOILER SERVO VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — MISSING (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 3G MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 7G INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 7G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 14C INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 14C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ELBOW — LEAKING (HHYDRAULIC SYS)

JFK - INFLIGHT AFTER TWO HOURS GREEN HYDRAULIC QUANTITY WENT TO ZERO. MANUALLY LOWERED LANDING GEAR. AFTER GEAR EXTENSION GREEN HYDRAULIC QUANTITY WENT UP BUT STILL BELOW MINIMUM. HYDRAULIC PRESSURE NORMAL. LANDED JFK WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. FOUND GREEN HYDRAULIC SYSTEM LOWER ELBOW LEAKING. ACCOMPLISHED REPAIRS TO GREEN HYDRAULIC SYSTEM E58D3 9333546 9333547 9331858 9331857. REPLENISHED GREEN SYSTEM HYDRAULIC FLUID AND RESET MANUAL GEAR EXTENSION SYSTEM TO NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (ZONE 100)

YELLOW HYDRAULIC SYSTEM RESEVOIR OVERHEAD ILLUMINATED FOLLOWED BY ECAM INDICATION. OVERHEAT WENT OUT TEN MINUTES AFTER PUMP WAS TURNED OFF. LANDED MIA WITHOUT INCIDENT. REPLACED PUMP AND FILTER ELEMENTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT DID NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PACK FOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (LT WING)

TUL LEFT HAND UPPER WING SKIN PANEL NUMBER 2 HAS A CRACK FROM FASTNER AT RIB 4, INBOARD FASTNER THIRD ROW AFT OF JOINT. CRACK LENGTH IS 0.821 AND 0.255 AT A DEPTH OF 0.167. INSTALLED DOUBLER PER AIR BUS DRAWING R57340132. CRACK REPAIRED PER ESO 30595 DATED 04/27/2004. (CLOSED)

Part: BATTERY BOX — CORRODED (FUSELAGE)

TUL CORROSION FOUND ON FORWARD SIDE OF AIRCRAFT EXTERNAL POWER BOX CENTERLINE BETWEEN FRAME 18 AND FRAME 19 AT STATION 1340. REPAIRED POWER BOX PER ESO 30595 DATED 4/26/04. (CLOSED)

Part: SHEAR TIE — CORRODED (FUSELAGE)

TUL - SHEAR TIE ON FRAME 18 AT STATION 1340 HAS 2 INCH BY 2 INCH SECTION OF CORROSION. REPAIRED FRAME 18 AT SECTION 1340 PER SRM 53-10-13.

Part: FRAME — CORRODED (FUSELAGE)

TUL - SHEAR TIE ON FRAME 18 AT STATION 1340 HAS A 2 INCH BY 2 INCH SECTION OF CORROSION. REPAIRED FRAME 18 AT STATION 1340 PER SRM 53-10-13.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY LIGHTS AT DOOR 2R AND RIGHT FIRST CLASS SEAT LIGHTS INOPERATIVE. REPLACED DOOR 2R AND RIGHT FIRST CLASS SEAT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COMPUTER — FAILED (FUEL QTY)

EN ROUTE ALL FUEL QUANTITY INDICATIONS FAILED. AIRCRAFT DIVERTED MIA AND LANDED WITHOUT INCIDENT. REPLACED FUEL QTY PROCESSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — INTERMITTENT (CABIN)

MIA - TOILET EMERGENCY LIGHT CIRCUIT BREAKER POPPED. TROUBLESHOT FAULT TO AN EMERGENCY LIGHT SWITCH INTERMITTENT FAULT. REPLACED SWITCH ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: BALLAST — DEFECTIVE (CABIN)

MIA - FLT 915 - EN ROUTE MIA-BOG - DETECTED SMOKE IN CABIN. RETURNED MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACED BALLAST NR 5, 6, AND 7. PERFORMED INSPECTION OF AFT GALLEY OVERHEAD PANEL. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ROLLER TRAY — CORRODED (BS 58-63)

TUL - FOUND CORROSION ON BOTTOM OF NR 3 ROLLER TRAY AT FRAME 58. REMOVED AND REPLACED NR 3 ROLLER TRAY FROM FRAME 58 TO FRAME 63 IAW SRM 51-72-10. (M)

Part: STIFFENER — CRACKED (BS 13-14)

TUL - VERTICAL STIFFENERS IS CRACKED ON RIGHT CONNECTING FITTING IN NLG BAY BET FRAME 13A AND FRAME 14. BLENDED CRACK WITHIN MAX BLEND DEPTH OF .314, RESULTANT BLEND IS ACCEPTALE FOR AN ADDITIONAL 3.300 FC BEFORE PERMANENT REPAIRS ARE REQ IAW S/B 53-6102 AND ESO 30595 DATED 11/29/99. (M)

Part: ROLLER TRAY — CORRODED (BS 58-63)

TUL - FOUND CORROSION ON BOTTOM OF NR 1 ROLLER TRAY AT FRAME 58 IN AFT CARGO COMPARTMENT. REMOVED CORRODED ROLLER TRAY AND INSTALLED NEW ROLLER TRAY FROM FRAME 58 TO FRAME 63 IAW SRM 51-72-10. (M)

Part: ROLLER TRAY — CORRODED (B 56-58)

TUL - CORROSION ON BOTTOM NR 5 ROLLER TRAY FRAMES 56 AND 58. REMOVED AND REPLACED NR 5 ROLLER TRAY FROM FRAME 56 TO FRAME 63 IAW SRM 57-72-10. (M)

Part: ROLLER TRAY — CORRODED (BS 58)

TUL - FOUND CORROSION ON BOTTOM AND TOP OUTBOARD AFT CORNER OF NR 5 ROLLER TRAY AT FRAME 58. REMOVED CORROSION AND SPLICED IN NEW SECTION OF ROLLER TRAY IAW 51-74-01 AND 53-10-15-2 BOTH OF THE SRM. (M)

Part: SILL — CORRODED (BS 59-63)

TUL - FOUND CORROSION ON AFT CX DOOR JAMB LOWER SILL BEAM FROM FRAME 59 TO FRAME 63. REMOVED CORROSION INSTALLED SILL BEAM REPAIR AT FRAME 60 IAW SRM 53-17-18 AND ESO 30595 DATED 11-17-99 AND DATED 11-22-99, OTHER BLENDOUTS THAT WERE OUT OF LIMITS PER SRM ARE OK PER ESO 30595 DATED 11-22-99 AFTER TREATING, PRIMING, PAINTING, AND APPLY A CORR PRSV COMPOUND. (M)

Part: STRINGER — CORRODED (BS 60-62)

TUL - STRINGER 50R IS CORRODED FROM FRAME 60 TO FRAME 62. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER SRM 53-10-14 AND ESO30595 DATED 11-22-99. (M)

Part: FLOORBEAM — CORRODED (BS 38.2)

TUL - FOUND CORROSION ON AFT SIDE OF FLOORBEAM AT FRAME 38.2 BETWEEN NR 4 AND NR 5 ROLLER TRAYS. REMOVED AND REPLACED FLOORBEAM AT FRAME 38.2 PER SRM 51-72-10. (M)

Part: STRINGER — CORRODED (BS 62)

TUL - FOUND CORROSION ON STRINGER 52L AT FRAME 62. INSTALLED NEW REPAIR STRINGER ON 52L AT FRAME 62 PER ESO 30595, DATED 11-19-99. (M)

Part: STRINGER — CORRODED (BS 64)

TUL - FOUND STRINGER 52L IS CORRODED BELOW FRAME 64. REMOVED CORROSION AND INSTALLED REPAIR SPLICE IAW SRM 53-10-14. (M)

Part: SPLICE — CORRODED (BS 72)

TUL - FOUND CORROSION ON STRINGER SPLICES AT STRINGER 45L, 46L, AND 47L IN AREA OF FRAME 72. REMOVED AND REPLACED STRINGER SPLICES AT STRINGER 45L, 46L, AND 47L AT FRAME 72. (M)

Part: STRINGER — CORRODED (BS 54.1-54.3)

TUL - LEVEL 2 CORROSION BEYOND LIMITS. REMOVED AND REPLACED STRINGER SECTION FROM STATION 54.1 TO 54.3 AS PER SRM 53-10-14. (M)

Part: FRAME — CORRODED (BS 58)

TUL - LEVEL 2 CORROSION BEYOND LIMITS. COMPLETED A STRINGER SPLICE IAW SRM 53-10-14-2. (M)

Part: FRAME — CORRODED (BS 58)

TUL - LEVEL 2 WIDESPREAD CORROSION ON FITTING AND FRAME. REMOVED AND REPLACED FITTING PER 51-72-10. (M)

Part: FITTING — CORRODED (BS 58)

TUL - LEVEL 2 WIDESPREAD CORROSION ON FITTING AND FRAME. REMOVED AND REPLACED FITTING PER 51-72-10. (M)

Part: CONNECTOR — LOOSE (L2 DOOR)

SJU - EMERGENCY EXIT SIGN AT 2L DOOR INOPERATIVE. MAINTENANCE FOUND CANNON PLUG LOOSE AT BATTERY PACK. RESEAT CANNON PLUG AT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DEFECTIVE (ROW 14-25)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 14 THROUGHT 25 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT FLAP JUMPER WIRE AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — FAILED (CABIN)

SJU - FLT 574 - AFTER TAKEOFF SJU EN ROUTE TO MIA, THE NR 1 ENGINE EXPERIENCED A FIRE. CREW DECLARED AN EMERGENCY AND SHUT ENGINE DOWN. AIRCRAFT AIR INTERRUPTED BACK TO SJU AND LANDED WITHOUT FURTHER INCIDENT. AFTER AIRCRAFT CAME TO A STOP AN EMERGENCY EGRESS WAS EXECUTED. THE 3R DOOR SLIDE FAILED TO FUNCTION NORMALLY AND DID NOT SUCCESSFULLY DEPLOY. ALL PASSENGERS AND CREW MEMBERS SUCCESSFULLY USED ALTERNATE AREAS TO EXIT THE AIRCRAFT. AFTER NTSB INVESTIGATION THE 3R DOOR SLIDE WAS REPLACED. DOOR AND SLIDE WAS CHECKED FOR NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ADAPTER — FAILED (NR 1 ENGINE)

SJU - FLT 574 - DURING CRUISE NR 1 ENGINE WAS SHUT DOWN BY CREW DUE TO ENGINE FIRE. RETURNED AND LANDED SJU. REPLACED NR 1 ENGINE. SHOP FOUND THE AGB IDLER ADAPTER THREADED INSERTS WERE PULLED OUT CAUSING FUEL TO LEAK, FIRE AND ENGINE SHUTDOWN. GENERAL ELECTRIC ISSUED SB 73-A283 REV2 TO CORRECT SITUATION. (M)

Part: CONNECTOR — LOOSE (R3 DOOR)

JFK - DURING OVERNIGHT MAINTENANCE, R3 DOOR OVERHEAD AND CEILING EMERGENCY LIGHTS WERE INOPERATIVE. RESEATED CONNECTOR AT R3 EMERGENCY EXIT DOOR LIGHT PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: BEAM — CORRODED (CARGO DOOR)

TUL - FOUND CORROSION ON LOWR DOOR BEAM FROM FRAME 2070 25A. CORROSION REMOVED AND DOUBLERS INSTALLED PER ESO 30595 DATED 11-19-97. (M)

Part: FITTING — CORRODED (CABIN)

TUL - CORROSION ON CORNER FITTING FORWARD SIDE OF FRAME 20 UNDER ROLLER TRAY NR 1. REMOVED AND REPLACED FITTING PER SRM 51-72-10-0. (M)

Part: SUPPORT — CORRODED (CABIN)

TUL - FOUND CORROSION ALONG TOP OF FLOORBOARD SUPPORT AT FRAME 15B IN LINE WITH SEAT TRACK NR 9. REMOVED AND REPLACED FLOOR UPPORT PER SRM 51-7210-0 FRAME 17-13. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ALONG TO OF SEAT TRACK NR 8 FROM FRAME 30-33. REMOVED AND REPLACED SEAT TRACK FROM FRAME 30-33 PER SRM 51-72-10. (M)

Part: SUPPORT — CORRODED (GALLEY)

TUL - CORROSION ALONG TRACK SUPPORT BEYOND LIMITS. REMOVED AND REPLACED TRACK SUPPORT FOR GALLEY PER SRM 51-72-10-0. (M)

Part: SUPPORT — CORRODED (CABIN)

TUL - FOUND CORROSION BEYOND LIMITS LAVATORY A AREA. REMOVED AND REPLACED TRACK PER SRM 51-72-10-0. (M)

Part: SUPPORT — CORRODED (CARGO COMPT)

TUL - FORWARD CORROSION UNDER ROLLER TRAY RN 1 AT FRAME 56. SPLICED IN A SECTION OF FLOORBEAM PER SRM 53-10-15. (M)

Part: SUPPORT — CORRODED (CABIN)

TUL - CORROSION TOP SURFACE OF SUPPORT BEYOND LIMITS AT 29 RBL AT APPROX FRAME 15B. REMOVED AND REPLACED SECTION PER SRM 72-10-0. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

TUL - BALL MAT FORWARD SUPPORT C-CHANNEL IS CORRODED AT FRAME NR 20. INSTALLED EXTRUDED SECTION REPAIR TO FRAME 20 C-CHANNEL STRINGER 44L TO 45L AS PER A-300 SRM 51-71-50-2. REPAIR SECTION CPN 4054049. (M)

Part: ANGLE — CORRODED (COCKPIT)

TUL - FOUND CORROSION ALONG 'Z' ANGLE AT COCKPIT ENTRY FOR ABOUT 2 FT LEFT AND RT. REPLACED 'Z' ANGLE FROM BEAM NR 1 TO BEAM NR 5 WITH SPLICE PER SRM 51-71-40-2. ALODINED, PRIMED AND PAINTED PER SRM 51-21-00. (M)

Part: CONNECTOR — BROKEN (CABIN)

JFK - DURINV OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT 3L/3R CROSS AISLE AND AT LEFT AISLE BETWEEN PAX SEAT ROWS 12 AND 16 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT 3L/3R CROSS AISLE AND REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT LEFT AISLE BY PAX SEAT ROW 12. SYSTEM GROUND CHECKED NROMAL OPERATION. (M)

Part: ENG MOUNT — CORRODED (LT ENGINE)

TUL - FORWARD PYLON TRUSS ENGINE MOUNT, RT AFT HOLE HAS PITTING ON INNER WALL. HOLE REAMED BUSHING AND REPAIRED WASHER. INSTALLED PER ESO 30595, DATED 1-23-96. TST, 20,955 HOURS. CYCLES, 8,316. (X)

Part: FLOOR SUPPORT — CORRODED (FS 3619)

TUL - CORROSION ON T-ANGLE SUPPORT FOR FLOOR/CARGO ROLLER TRACK/TRAY AT FRAME NR 56 AT NR 6 TRAY. INSTALLED NEW T-ANGLE, AND SPLICE SUPPORT DOUBLER PER SRM 53-10-15 AND SRM 51-71-50. TST, 20,955.4 HOURS. CYCLES, 8,316. (X)

Part: SUPPORT — CORRODED (CABIN)

TUL - CORROSION ON FLOOR SUPPORT 'A', RT SIDE AT R-4 DOOR FROM FRAME 73A TO FRAME 75A. INSTALLED FABRICATED PART PER AARD 51-10-00-3. ALODINED, PRIMED, AND PAINTED. TST, 20,955 HOURS. CYCLES, 8,316. (X)

Part: FLOOR BEAM — CORRODED (BS 63)

TUL - CORROSION BEAM LT SIDE OUTBOARD END AT THE ROLLER TRAY, FRAME STA 63. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-15 AT FRAME 63 AND TREATED, PRIMED, AND PAINTED PER SRM 51-74-10. TST, 20,955 HOURS. CYCLES, 8,316. (X)

Part: SKIN — DENTED (FS 432-446)

TUL - DENT IN FUSELAGE SKIN AT FORWARD LOWER CORNER OF FORWARD CARGO CUT-OUT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-12. TST, 20,955 HOURS. CYCLES, 8,316. (X)

Part: CONNECTOR — BROKEN (CABIN)

MAI - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS INOPERATIVE BETWEEN PAX SEAT ROWS 23 AND 27. REPLACED BROKEN EMERENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TRANSMITTER — DEFECTIVE (GREEN HYD SYST)

MIA - FLT 0095 - DURING DESCENT INTO MIA, GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL INDICATION AND RESERVOIR GAUGE DROPPED TO RED DOT. ACCOMPLISHED ALTERNATE LANDING GEAR EXTENSION AND AIRCRAFT LANDED MIA WITHOUT INCIDENT. GAUGE READING RETURNED TO NORMAL AFTER LANDING. REPLACED GREEN HYDRAULIC SYSTEM QUANTITY TRANSMITTER. ACCOMPLISHED LEAK AND SYSTEM GROUND CHECKS WITH NO DEFECTS FOUND. RETURNED LANDING GEAR SYSTEM TO NORMAL CONFIGURATION. (X)