N50051

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY EXIT SIGN AT OVERHEAD RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED EXIT SIGN ASSEMBLY FOR EMERGENCY EXIT SIGN AT OVERHEAD RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 11G INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

MIA- EMERGENCY LIGHT AT SEAT 18G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 18G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT SEAT 15G INOPERATIVE. RESECURED SEAT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LANDING GEAR — UNKNOWN (RIGHT)

JFK - INFLIGHT RIGHT LANDING GEAR WOULD NOT EXTEND. EXTENDED RIGHT LANDING GEAR MANUALLY. LANDED JFK WITHOUT INCIDENT. REPLACED RIGHT HAND MAIN LANDING GEAR DOWN (RETURN) LINE RESTRICTOR. REPLACED RIGHT HAND GEAR SEQUENCE VALVE AND UPLOCK ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (MLG)

INFLIGHT UPON RETRACTION OF GEAR ON TAKEOFF GOT ECAM LANDING GEAR SYSTEM FAULT. EXCESSIVE NOISE, ELECTED TO PUT GEAR DOWN AND GOT THREE GREEN. NO DOOR LIGHTS. ELECTED TO ONCE AGAIN RETRACT GEAR RESULTING IN GEAR UP NO FAULT OR DOOR LIGHTS UNTIL GEAR HANDLE WAS PLACED IN NEUTRAL OR MID POSITION. AT THAT TIME NOISE RETURNED WITH NO AMBER LIGHTS. FOUND LEFT NOSE GEAR DOOR ACTUATOR LOCK TAB BROKEN. THE ACTUATOR ROD END LENGTHENED DUE TO THE SHAFT ROTATION. DOOR WOULD NOT CLOSE PROPERLY. REPLACED LEFT HAND NOSE GEAR DOOR ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (NLG DOOR)

JFK INFLIGHT T1683/27SEPTEMBER, NOSE GEAR UNSAFE LIGHTS ILLUMINATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND NOSE LANDING GEAR UPLOCK ACTUATOR AND DOOR CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BEAM — CRACKED (FUSELAGE)

TUL - FRAME 51 LEFT HAND GANTRY BEAM NUMBER 4 CRACKED AT LOWER OUTBOARD FLANGE AT STATION 3195. CRACK IS 2 INCHES IN LENGTH. REPAIRED PER ESO 30595 DATED 2004 JULY 01 REPAIR NUMBER 40 531500 3505.

Part: CLAMP — LOOSE (EQUIP BAY)

AFTER TAKEOFF SMOKE OR BURNING SMELL IN CABIN DETECTED. CREW DECLARED AN EMERGENCY AND RETURNED TO BOG WITHOUT FURTHER INCIDENT. TIGHTENED SEVERAL PNEUMATIC DUCT CLAMPS. SWAPPED MINIMUM EQUIPMENT BAY DETECTOR WITH ZONE 125 DETECTOR. HISTORY OF HOT FLOORS AND LEAKS AND APU BLEED ON MEL. SYSTEM LEAK AND OPS CHECK NORMAL. (M)

Part: INDICATOR — FAULTY (COCKPIT)

BOS - FLT 989 - EN ROUTE BOS-MIA, LEFT OUTER FUEL QUANTITY STARTED DROPPING AFTER TAKEOFF ON ECAM AND FUEL QUANTITY PANEL. RETURNED BOS AND LANDED WITHOUT INCIDENT. REPLACED FUEL QUANTITY INDICATOR. SUMPED LEFT OUTER FUEL TANK. SUMP OF FUEL QUANTITY BITE SHOWED NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — CONTAMINATED (LT WING)

JFK - FLT 1270 - EN ROUTE SJU-EWR, LEFT ENGINE WAS SHUTDOWN FOR APPROXIMATELY 10 MINUTES DUE TO LEFT WING OUTER TANK INDICATION SHOWING FUEL QUANTITY GOING UP AND DOWN. LANDED JFK WITHOUT INCIDENT. AFTER AIRCRAFT LANDED INSPECTED LEFT WING WITH NO FUEL LEAKS BEING NOTED. CLEARED AND CLEANED COMPENSATOR HARNESS CONNECTOR OF ALL CONTAMINATES AND PERFORMED CAPACITANCE AND RESISTANCE CHECK OF LEFT WING OUTER TANK. ALL CHECKS WITHIN LIMITS. SUMPED LEFT WING OUTER TANK AS REQUIRED. ACCOMPLISHED INSPECTION OF LEFT WING TANKS. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY LIGHT WIRE AT SEAT 30G BROKEN. REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DAMPENER — BROKEN (AUTOPILOT SYS)

MIA - FLT 2139 - EN ROUTE MIA-CCS - UNCOMMANDED RUDDER MOVEMENT DURING CLIMB-OUT. ISOLATING A/P SYSTEM DID NOT HELP. NO AIRFRAME VIBRATION NOTICES. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FLIGHT AUGMENTATION COMPUTERS. DID NOT RESOLVE PROBLEM. REPLACED YAW DAMPER SERVO ACTUATOR AND ACCOMPLISHED YAW DAMPER SERVO ACTUATOR OPERATIONAL CHECK. DID NOT RESOLVE THE PROBLEM. REPLACED YAW DAMPENER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND SPLICE ANGLE CORRODED. REPLACED SPLICE ANGLE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND SPLICE ANGLE CORRODED. REPLACED SPLICE ANGLE. (M)

Part: STRINGER — CORRODED (FUSELAGE)

TUL - FOUND STRINGER CORRODED FS 69-70. REPLACED STRINGER. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON STRINGER SPLICE ANGLE. REPLACED SPLICE ANGLE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND CORROSION OF SPLICE ANGLE. REPLACED SPLICE ANGLE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND CORRODED STRINGER SPLICE ANGLE. REPLACED STRINGER SPLICE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND CORRODED SPLICE ANGLE. REPLACED SPLICE ANGLE. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND CORRODED STRINGER SPLICE ANGLE AT FRAME 65. REPLACED SPLICE ANGLE. (M)

Part: HOSE — LEAKING (MLG)

FLT 1416 - EN ROUTE SJU-JFK, GREEN HYDRAULIC SYSTEM RESERVOIR QUANITITY SLOWLY DECREASED TO ZERO. AIR INTERRUPTED, RETURNED SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT MAIN GEAR LOCK ACTUATOR FLEXIBLE HOSE. SERVICED HYDRAULIC SYSTEM. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT DOOR 3L INOPERATIVE. REPLACED EMERGENCY EXIT SIGN AT DOOR 3L. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STRINGER — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON STRINGER 48L 2 PLACES BETWEEN FRAME 70 AND 71 BELOW THE WASTE WATER TANK JUNCTION BOX. REMOVED AND REPLACED SECTION OF STRINGER 48L PER SRM 51-72-10. (M)

Part: STRINGER — CORRODED (E/E COMPT)

TUL - FOUND CORROSION ON AFT SIDE OF FRAME C-20 ON STRINGER. STRINGER 53L IS CORRODED FROM FRAME 20 FORWARD ABOUT 8 INCHES TO 10 INCHES. REPLACED SECTION OF STRINGER AND SPLICED PER SRM 53-00-00. (M)

Part: ANGLE — CORRODED (CARGO COMPT)

TUL - FOUND CORROSION ON NUT PLATE AT POWER ROLLER TRAY 4TH FROM AFT, RT SIDE, OUTBOARD OF NR 5 TRAY. REMOVED AND REPLACED FLOOR ANGLE PER MM 53-10-15-2. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION IN SEAT TRACK AND NR 10 RIGHT SIDE OF AIRCRAFT. REMOVED AND REPLACED RT SIDE NR 10 SEAT TRACK PER SRM 51-72-10-8. (M)

Part: SUPPORT — CORRODED (CABIN)

TUL - FOUND CORROSION AT LAV TIE DOWN AF TOF FRAME C79 ON FLOOR SUPPORT 59 INCHES LEFT OF AIRCRAFT CENTER LINE. REMOVED DAMAGE TRACK SECTION AND INSTALLED NEW ONE OF SAME P/N USING HI-LOCKS AND PRO PR870 REF A300 SRM 51-72-10. (M)

Part: FITTING — CORRODED (CABIN)

TUL - FOUND AFT LEFT GALLEY ON TRACK B HAS CORROSION AROUND TWO ATTACH FITTING. REMOVED DAMAGED TRACK SECTION AND INSTALLED NEW ONE OF SAME P/N USING HI-LOCKS AND PRO BR870 RAF A300 SRM 51-72-10. (M)

Part: SUPPORT — CORRODED (CARGO COMPT)

TUL - FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 26 BELOW CENTER SCISSOR. REPAIRED PER SRM 53-10-15, BY REPLACING SECTION OF SUPPORT ANGLE. (M)

Part: ANGLE — CRACKED (LT WING)

TUL - FOUND LEFT WING ROOT ANGLE CRACKED. REPLACED LEFT PICK UP ANGLE PER ESO 3095, DATED 10-7-98. (M)

Part: VALVE — DEFECTIVE (NR 1 ENGINE)

SJU - FLT 1915 - DURING CLIMB-OUT, NR 2 PACK FAILED AT 25,000 FEET AND CABIN ALTITUDE CONTINUED TO CLIMB AT 1,000 FEET PER MINUTE. NR 1 PACK FAILED AND BOTH PACKS UNABLE TO BE RESET. OXYGEN MASKS DEPLOYED AT 14,000 CABIN ALTITUDE DURING EMERGENCY DESCENT. AIRCRAFT AIR INTERRUPTED AND RETURNED SJU AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE FAN AIR VALVE AND RESECURED CLAMPS AT RIGHT SIDE OF PACK. ACCOMPLISHED LEAK AND OPERATIONAL CHECKS OF SYSTEM WITH NO FAULTS NOTED. PASSENGER OXYGEN MASKS WERE REPACKED ADN OXYGEN BOTTLES REPLACED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: PACKING — LEAKING (MLG WW)

BOS - FLT 1096 - DURING DESCENT INTO BOS, ECAM MESSAGE HYDRAULIC RESERVOIR GREEN SYSTEM LOW. TURNED OFF GREEN SYSTEM HYDRAULIC PUMPS AND MANUALLY EXTENDED LANDING GEAR. AIRCRAFT LANDED BOS WITHOUT INCIDENT. REPLACED PACKING AT GREEN HYDRAULIC MANIFOLD ELBOW. SERVICED GREEN HYDRAULIC SYSTEM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. RESTORED LANDING GEAR FREEFAL SYSTEM. (M)

Part: STRINGER — CORRODED (FRAME NR 57.2)

TUL - CORROSION ON S56R BETWEEN FRAMES 57.2 AND 57.3. SPLICED NEW SECTION OF STRINGER PER SRM 53-10-4. TST: 25,726:17 HOURS, CYCLES 10,398. (X)

Part: FRAME — CORRODED (FRAME 57.2)

TUL - CORROSION ON AFT SIDE OF FR 57.2 BETWEEN S55L AND S55R. INSTALLED NEW SECTION OF FRAME PER SRM 53-10-3. TST: 25,726.17 HOURS. CYCLES: 10,398. (X)

Part: SEAT TRACK — CORRODED (BS 1976-2135)

TUL - NR 8 SEAT TRACK HAS SEVERAL AREAS OF CORROSION BETWEEN FRAMES 30 TO 33. INSTALLED NEW SEAT TRACK, NR 8, FROM FRAMES 30 TO 33 PER SRM 51-72-10-0. ALODINED, PRIMED AND PAINTED PER SRM 51-21-00-0. TST: 25,729.17 HOURS. CYCLES: 10,398. (X)

Part: SEAT TRACK — CORRODED (FRAMES 26-29)

TUL - SEAT TRACK AND FLOOR BOARD SUPPORT FROM FRAME 26 TO FRAME 29 HAS SEVERAL AREAS OF INTERGRANULAR CORROSION. INSTALLED NEW SEAT TRACK, NR 10, FROM FRAMES 26 TO 30 PER SRM 51-72-10-0. ALODINED, PRIMED AND PAINTED PER SRM 51-21-00-0. TST: 25,726.17 HOURS. CYCLES: 10,398. (X)

Part: ANGLE — CORRODED (CARGO COMPT)

TUL - CORROSION ON ANGLE AT LEFT CENTER ROLLER TRACK, FRAME 58. SPLICED IN NEW SECTION OF FLOOR ANGLE SUPPORT PER SRM 53-10-13. TST: 25,726.17 HOURS. CYCLES: 10,398. (X)

Part: SUPPORT — CORRODED (LAVATORY FLOOR)

TUL - CORROSION ON LAVATORY-V FLOOR SUPPORT BEAM AT FRAME C-73. INSTALLED FLOOR BEAM UNDER LAV-V PER SRM 51-72-10-0. TST: 25,726.17 HOURS. CYCLES: 10,398. (X)

Part: SUPPORT — CORRODED (BS 26-29)

TUL - FLOOR BOARD SUPPORT AT SEAT TRACK NR 9 BETWEEN FRAMES 26-29 HAVE INTERGRANULAR CORROSION. REMOVED DAMAGED SUPPORT, ALODINED, RPIMED AND PAINTED SERVICEABLE REPLACEMENT SUPPORT. INSTALLED WET USING PR-870 PER A-300-600 SRM'S 51-72-10-0 AND 51-21-00. TST: 25,726.17 HOURS. CYCLES: 10,398. (X)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - CORROSION ON SEAT TRACK NR 8 BETWEEN FRAME 26 - FRAME 29, BOTH SIDES OF FLANGE. INSTALLED NEW SEAT TRACK NR 8 BETWEEN FRAME 26 - FRAME 29 PER SRM 51-72-10-0. TST: 25,726. CYCLES: 10,398. (X)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - CORROSION AROUND LAVATORY 'L' MOUNT, OUTBOARD. INSTALLED DOUBLER AFTER CORROSION REMOVAL PER AARD 53-20-00-2. (X)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - CORROSION AROUND LAVATORY L-MOUNT, INBOARD. INSTALLED DOUBLER AFTER CORROSION REMOVAL PER AARD 53-20-00-2. TST: 25,726. CYCLES: 10,398. (X)

Part: FRAME — CRACKED (A/C BAY)

TUL - FRAME 45, LEFT, HAS CRACK BELOW ANGLE FITTING. INSTALLED FRAME DOUBLER REPAIR PER AARD 53-00-00-5, REPAIR 5. TST: 25,726. CYCLES: 10,398. (X)

Part: FRAME — CRACKED (BS 45)

TUL - FRAME 45 HAS CRACK BENEATH ANGLE FITTING. REPAIRED CRACKED AREA PER AARD 53-00-00-5. TST: 25,726. CYCLES: 10,398. (X)

Part: SUPPORT — CORRODED (BS 32)

TUL - CORROSION PITS ON FLOORBOARD SUPPORT, STA 32, TRACK 3. REPAIRED SUPPORT PER ESO BY RESHAPING FLANGE AND REMOVING PITS ESO 30595, 7-7-97. TST: 25,726. CYCLES: 10,398. (X)

Part: FRAME — CRACKED (BS 46)

TUL - FRAME 46 HAS CRACK BENEATH ANGLE FITTING. REPAIRED CRACKED AREA PER AARD 53-00-00-5, REPAIR 5. TST: 25,726 HOURS. CYCLES: 10,398. (X)

Part: FRAME — CRACKED (BS 46)

TUL - FRAME BASE FITTING AT INNER FLANGE CRACKED. INSTALLED DOUBLER PER AARD 53-00-00-5, REPAIR 5. TST: 25,726. CYCLES: 10,398. (X)

Part: LIGHT — DEFECTIVE (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE BETWEEN PAX SEAT ROWS 12B AND 20B INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT LEFT AISLE BETWEEN PAX SEAT ROWS 12B AND 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SUPPORT — CORRODED (LAVATORY FLOOR)

TUL - FLOOR SUPPORT INBOARD OF Y-LAVATORY HAS CORROSION BETWEEN FORWARD AND AFT MOUNTS. REPLACED NEW FLOOR SUPPORT INBOARD OF Y-LAVATORY PER AARD 51-10-00-3 AND SRM 51-72-10-0. TST: 25,726 HOURS. CYCLES: 10,398. (X)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROWS 25AB AND 26AB INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 25AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

JFK - DURING OVERNIGHT CHECK EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 14 AB TO 19AB INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIPS FROM PAX SEAT ROW 14AB TO 19AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT LEFT AISLE BETWEEN L2 AND L3 DOORS INOPERATIVE. RESECURED LOOSE EMERGENCY FLOORLIGHT STRIP CONNECTOR BY L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRIP — DEFECTIVE (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROWS 27AB AND 28AB INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROWS 27AB AND 28AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ELBOW — BROKEN (NR 2 ENGINE)

JFK - FLT 0587 - AFTER TAKEOFF JFK DURING CLIMB-OUT AT FL 270, NR 2 ENGINE ECAM ADVISORY ON ENGINE PAGE FOLLOWED BY FIRE WARNING BOTH LOOPS. RETARDED NR 2 ENGINE TO IDLE AND ENGINE FIRE WARNING WENT OUT. ACCOMPLISHED ABNORMAL PROCEDURE AND AIRCRAFT RETURNED TO JFK LANDING WITHOUT INCIDENT. REPLACED BROKEN HPT ELBOW AT REAR TURBINE CASE FRAME ON NR 2 ENGINE. ACCOMPLISHED LEAK AND GROUND ENGINE RUN CHECK AT HIGH POWER WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)