N25071

Part: SERVO VALVE — INOPERATIVE (BREAKS)

JFK INFLIGHT T1892/28DEC - DURING LANDING, BRAKES THREE AND SEVEN REACHED BRAKE TEMPERATURE OF 370 DEGREES. AIRCRAFT TAXIED TO GATE. REPLACED BRAKE SYSTEM CONTROL UNIT AND SERVO VALVE 75GC. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (HYD SYSTEM)

MIA INLFIGHT T902/04NOV - CREW REPORTED YELLOW HYDRAULIC SYSTEM OVERHEAT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE DRIVEN PUMP YELLOW SYSTEM, NUMBER TWO ENGINE CASE DRAIN FILTER AND RESERVOIR FILTER FOR YELLOW HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPUTER — FAULTED (PITCH FEEL)

MIA INFLIGHT T2110/29AUG - AFTER TAKEOFF LOST SECOND PITCH FEEL SYSTEM. FIRST SYSTEM WAS ALREADY ON PLACARD. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED SLAT FLAP CONTROL COMPUTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 11C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 11C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 34C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 34C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — DAMAGED (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 13C DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 13C. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL BOX — INOPERATIVE (ANTI-SKID SYS)

JFK - INFLIGHT FERRY FLIGHT TUL JFK. MESSAGE ON ECAM ANTI-SKID WITH BRAKES NUMBER 5 AND 8 RELEASE INDICATIONS INTERMITTENT DISPLAYED WITH GEAR HANDLE IN NEUTRAL AND BRAKE RELEASE INDICATIONS ON 1 THROUGH 7 BRAKES. WITH GEAR HANDLE DOWN DID NOT HAVE BRAKE RELEASE INDICATIONS ON BRAKES 5 AND 8. FLT DECLARED AN EMERGENCY INTO JFK. LANDED WITHOUT INCIDENT AFT JFK. AIRCRAFT INSPECTED AND TAXIED TO THE HANGAR. REPLACED ANTI SKID CONTROL BOX. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

JFK - RIGHT MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR RIGHT HAND MID CABIN EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (ROW 29)

MIA - EMERGENCY LIGHTS AT ROW 29 AND AFT INOPERATIVE. REPAIRED EMERGENCY LIGHTS AT ROWS 29 AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPUTER — INOPERATIVE (FLT CONTROL)

EN ROUTE MIA-MEX, AFTER TAKEOFF RECEIVED AN ECAM CAUTION WITH A PITCH FEEL FAULT. PITCH FEEL WAS NOTICEABLE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 FCC, DIODE 156VD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

BOS - LEFT HAND MID CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN WIRES AT FORWARD FLOOD LIGHT AT L3 DOOR. REPAIRED WIRE PER MM CHAPTER 20 FOR LEFT HAND MID CABIN EMERGENCY LIGHTS AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ROLLER TRAY — CORRODED (CARGO BAY)

TUL - FOUND CORROSION ON SIX INCH BY FIVE INCH SECTION OF UNDERSIDE OF ROLLER TRAY NUMBER 6 BETWEEN FRAME 57.3 AND 58 AT STATION NUMBER 3885. CORROSION HAD A DEPTH OF 0.100 INCH. REMOVED CORRODED SECTION OF NUMBER 6 ROLLER TRAY AND SPLICED IN NEW SECTION PER SRM 53-10-15-2.

Part: ROLLER TRAY — CORRODED (CARGO BAY)

TUL - CORROSION ON LEFT FLOORBOARD FLANGE OF NUMBER 4 ROLLER TRAY BETWEEN FRAME 60 AND 61. AREA OF CORROSION IS 1 INCH BY 2 INCHES WITH A DEPTH OF .050. BLENDED OUT CORROSION PER SRM 51-74-0 AND INSTALLED REPAIR STRAP PER 53-30-00-1.

Part: BALLAST — OVERHEATED (CABIN LIGHTS)

INFLIGHT T882/5 FLIGHT ATTENDANT REPORTED SMOKE AND ELECTRICAL ODOR NEAR SEAT 15G. SHUT OFF OVERHEAD LIGHT SYSTEM AND SMOKE AND ELECTRICAL ODOR WENT AWAY. FOUND BALLAST AT 15 CENTER HOT AND SIGNS OF OVERHEAT. REPLACED BALLAST AND INSPECTED ALL BALLAST LIGHT ASSEMBLIES FROM ROW 10 THROUGH 20. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT L2 DOOR INOPERATIVE. REPLACED FLIGHT ATTENDANTS EMERGENCY EXIT FLASHLIGHT AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

JFK - FOUND 2R DOOR OVERHEAD EXIT SIGN AND OVERHEAD CEILING EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY FOR 2R DOOR EXIT SIGNS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ADC — FAILED (COCKPIT)

ATC 2 FAULTED CONTINUED AURAL WARNING UNTIL DESCENT. ACCOMPLISHED ATC BITE CHECK. ALL CHECKS NORMAL. ADC FAULT NR 1 SWITCHED TO 2. REPLACED NR 1 AIR DATA COMPUTER ACCOMPLISHED ADC BITE AND AFS TEST. ALL TEST PASSED. (M)

Part: LIGHT — BROKEN (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 7D BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PROXIMITY SWITCH — MALFUNCTIONED (RT MLG)

JFK - FLT 92 - RIGHT MLG INDICATED RED/UNLOCKED, FOLLOWING TAKEOFF IN BOTH CENTER INSTRUMENT PANEL AND OVERHEAD GEAR POSITION INDICATORS WITH GEAR HANDLE UP. REMOVED AND REPLACED PROX DETECTION UNIT. PERFORMED BITE CHECK. OPS OK. NEEDS GEAR SWING. ACCOMPLISHED LANDING GEAR RETRACTION AND EXTENSION AS PER MM ON GROUND. ALL INDICATIONS WERE NORMAL DURING SEVERAL RETRACTIONS AND EXTENSIONS OF LANDING GEAR. (M)

Part: LIGHT — LOOSE (CABIN)

EGLL - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT OVER 4L DOOR FLICKERS ON AND OFF. RESEATED 4L LAMP. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 32,500 hrs · 10,677 cycles

TUL - CORROSION ON FLOOR SUPPORT IN LINE WITH SEAT TRACK RIGHT BETWEEN C71 AND C72. REPLACED FLOOR SUPPORT FROM FRAMES 71.5 TO 73.5. REF: A300 SRM 51-72-10 AND 51-21-00. (X)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - CORROSION ON FLOOR SUPPORT BEAM BETWEEN SEAT TRACKS D AND E AND FRA C71 AND C73. INSTALLED NEW LAVATORY SUPPORT BEAM PER SRM 51-72-10. (X)

Part: SIGN — MALFUNCTIONED (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, LHR PREVIOUSLY REPORTED INTERMITTENT EMERGENCY EXIT LIGHT OPERATION AFFECTED BY MOVEMENT OF R3 OVERHEAD EXIT SIGN. INSPECTED AND CLEANED. NO FAULT FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

LHR - FLT 0155 - DURING FLIGHT WITH EMERGENCY EXIT LIGHT SIWTCH IN ARM POSITION, EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATE INTERMITTENTLY. RE-SEATED R3 EMERGENCY EXIT LIGHT PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: DISPLAY — FAILED (CABIN)

LHR - FLT 0108 - EN ROUTE BOS/LHR, MASTER DISPLAY UNIT AND AIRSHOW PORTION SMELLED OF SMOKE AND THEN WENT BLANK. REPLACED CMT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — SHORTED (PA SYSTEM)

BOS - FLT 121 - EN ROUTE LGW-BOS - DURING CRUISE, THE TRANSFORMER AT SEAT 29G SHORTED OUT CAUSING SPARKS AND SMOKE. ALL VIDEOS IN ZONE WERE BLANK. SECURED SYSTEM. LANDED BOS WITHOUT INCIDENT. REPLACED WIRING HARNESS AT SEAT 29G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — FAILED (PAX DOOR)

JFK - DURING OVERNIGHT MAINTENANCE, CHECK OF L3 DOOR SLIDE DEPLOYMENT WAS UNSUCCESSFUL. REPLACED L3 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DIRTY (GALLEY)

LHR - FLT 0106 - DURING CRUISE, NR 1 FIRST CLASS OVEN WAS EMITTING SMOKE WHILE HEATING FOOD. REMOVED BURNED FOOD AND THOROUGHLY CLEANED ENTIRE INTERIOR OF NR 1 FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STRUT — DEFECTIVE (NLG)

JFK - FLT 107 - DURING APPROACH, THE NOSE LANDING GEAR RED UNLOCK LIGHT ILLUMINATED ON GEAR EXTENSION. CREW MISSED THE APPROACH, GEAR WAS CYCLED WITH THREE GREEN GEAR SAFE LIGHT ILLUMINATED. AIRCRAFT LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED NOSE GEAR TELESCOPING DRAG STRUT. ACCOMPLISHED NOSE LANDING GEAR RETRACTION AND ALTERNATE EXTEND CHECKS WITH NORMAL INDICATION. SYSTEM LEAKED AND GROUND CHECKED NORMAL OPERATION. (M)

Part: SILL — CORRODED (BS 1711-1722)

TUL - CORROSION AROUND SEVERAL ROLLER TRAY ATTACH HOLES IN SILL BEAM AT FORWARD CARGO DOOR. REMOVED CORROSION, TREATED, PRIMED, AND PAINTED AREA THEN INSTALLED 2 EACH STRAPS AT FR 25 AND FR 25A PER ESO 30595 DATED 2-11-98. TST: 265,415.42 HOURS. CYCLES: 9,488. (X)

Part: STRUCTURE — CORRODED (LE FLAP)

TUL - CORROSION INSIDE MAIN SECTION OF KRUEGER FLAP. REPLACED MAIN KRUEGER FLAP WITH NEW SERVICEABLE FLAP. TST: 25,415.42 HOURS. CYCLES: 9,488. (X)

Part: FRAME — CORRODED (CARGO COMPT)

TUL - FRAME 58 CORRODED AT LONGERON 55R TO 55L. INSTALLED DOUBLER PER SRM 53-10-13. TST: 25,415.42 HOURS. CYCLES: 9,488. (X)

Part: STRUT — ICED UP (NLG DRAG STRUT)

ORY - FLT 0146 - DURING APPROACH ORY, LANDING GEAR HANDLE SELECTED DOWN, NOSE LANDING GEAR FAILED TO INDICATE SAFE. CREW CYCLED GEAR AND THE UNSAFE MESSAGE EXTINGUISHED. AIRCRAFT LANDED ORY WITHOUT INCIDENT. INSPECTION FOUND DRAG STRUT COVERED IN ICE. STRUT WAS CLEANED AND LUBRICATED, SENSORS WERE CHECKED AND OPERATED NORMALLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: IDG — FAILED (NR 1 ENGINE)

JFK - 104 -ABOUT 30 MINUTES AFTER T/O, IDG NR 1 OIL OUTLET TEMP WENT TO 196 DEGREES CELCIUS WITH ASSOCIATED ECAM WARNING. FOLLOWED ECAM ACTIONS, DISCONNECTED NR 1 IDG AND COMPLIED WITH OPS MANUAL PROCEDURE. REPLACED IDG AS PER MM 24-11-11-4. REPLACED OIL COOLER FLEX LINE AND PRESS RELIEF VALVE. RAN ENGINE. IDG OPS AND LEAKS CKS NORMAL. AFTER APU WAS STARTED AND APU GEN CAME ON LINE. APU VOLTAGE SHOWED AMBER MESSAGE ON ECAM AND OVERHEAD PNL SHOWED APU VOLTAGE FLUCTUATING BETWEEN 119 AND 123 VOLTS. APU GEN DID CARRY BUS 1 OK. HOWEVER, IN FLT TO COMPLY WITH IDG NR 1 LOSS PROCEDURE. REPLACED APU GEN CONTROL UNIT. OPS CHECK OK. (M)

Part: OVEN — DIRTY (CABIN)

LHR - FLT 106 - EN ROUTE JFK/LHR DURING CRUISE, NR 2 OVEN IN FIRST CLASS CABIN SMOKED EXCESSIVELY, NR 2 OVEN WAS TURNED OFF. AIRCRAFT PROCEEDED TO LHR AND LANDED WITHOUT INCIDENT. NR 2 OVEN CLEANED BY CABIN SERVICES. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE NOTED. (M)

Part: ANGLE — CORRODED (CABIN)

TUL - FOUND CORROSION ON TOP FLANGE OF FLOOR SUPPORT T-ANGLE. REMOVED AND REPLACED DAMAGED SECTION OF T-ANGLE AND INSTALLED A .050 THICK 301 .5 H DOUBLER OVER TOP FLANGE OF T-ANGLE AND OVER FLOORBEAM PER ESO 30595 DATED 4/9/96. (M)

Part: SKIN — CORRODED (RT TE FLAP)

TUL - FOUND R/W OUTBOARD FLAP OUTBOARD END CORROSION UNDER STATIC WICK BASE. CUT OUT CORRODED AREA AND REPAIRED SKIN PER SRM 57-50-00 FIG 205. (M)

Part: LONGERON — CORRODED (BS 4468)

TUL - FOUND LONGERON HAS CORROSION DAMAGE UNDER INTERCOSTAL , BELOW SIDE WALL SUPPORT STRUCTURE. REMOVED AND REPLACED STRINGER, PER SRM 33-10-14, PG 201. (M)

Part: FITTING — CORRODED (BS 1711)

TUL - FOUND LOWER AFT CORNER FITTING ON FORWARD CARGO DOOR CORRODED. REMOVED AND REPLACED PART. (M)

Part: FITTING — CORRODED (BS 1450)

TUL - LOWER FORWARD CORNER FITTING ON FORWARD CARGO DOOR IS CORRODED. REMOVED AND REPLACED PART. (M)

Part: ROLLER TRAY — CORRODED (BS 2559)

TUL - FOUND CORROSION UNDER AFT EDGE OF ROLLER TRAY NR 6. REPAIRED NR 6 ROLLER TRAY IAW SRM 53-10-15. (M)

Part: SUPPORT — CORRODED (BS 2559)

TUL - FOUND CORROSION ON TOP FLANGE OF FLOOR SUPPORT 'T' WHERE NR 6 ROLLER TRAY IS SUPPORTED BY 'T'. REPAIRED FLOOR SUPPORT 'T' WHERE NR 6 ROLLER TRAY IS SUPPORTED PER SRM 51-71-50. (M)

Part: ANGLE — CORRODED (BS 4740-4801)

TUL - FOUND CORROSION ON THIRD TO RIGHT OF CENTER FLOOR SUPPORT BETWEEN FRAME 74 AND 75, FIVE PLACES AT FASTENERS HOLES. REPAIRED PER AARD 53-20-00-2. (M)

Part: ANGLE — CORRODED (FRAME 74-75)

TUL - FOUND 3 AREAS OF CORROSION AROUND CLIP NUT HOLES FOR FLOORBOARDS, ONE AREA BLENDED BEYOND LIMITS. REMOVED AND REPLACED WITH A NEW SECTION OF 'L' ANGLE PER SRM 51-72-10 PAGE 1 AND PAGE 2. (M)

Part: RETAINER — CORRODED (FRAME 74-75)

TUL - FOUND CORROSION ON TOP SIDE OF R4 DOOR LOWER RETAINER 3 PLACES ABOUT 4 INCHES APART BLENDED BEYOND LIMITS (AREA UNDERNEATH TOP LIP OF SCUFF PLATE). REMOVED AND REPLACED RETAINER PER SRM 51-72-10 PAGE 1 AND PAGE 2. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION IN 2 PLACES ON TOP FLANGE OF SEAT TRACK BLENDED BEYOND LIMITS. REMOVED AND REPLACED WITH A NEW SECTION OF SEAT TRACK. (M)

Part: SUPPORT — CORRODED (BS 4574-4627)

TUL - FOUND FLOOR SUPPORT BEAM BETWEEN FRAME 71-72, 3RD FRAME FROM CENTER ON LEFT SIDE HAS CORROSION ON TOP SIDE. INSTALLED REPAIR ESO 30595. (M)

Part: PLATE — CORRODED (BS 4680)

TUL - FOUND PLATE FORWARD OF L-4 DOOR HAS CORROSION JUST OUTBOARD OF FLOORBOARD 251PG AND FORWARD OF FRAME 73. INSTALLED DOUBLER PER SRM 53-10-12. (M)

Part: ANGLE — CORRODED (FR 72-73)

TUL - FOUND SMALL AREA OF CORROSION ON TOP FLANGE OF TEE ANGLE USED PRIMARILY FOR FLOORBOARD SUPPORT. INSTALLED A STRAP .050 THICK 301 CRES .5 HARD OVER TOP FLANGE OF TEE ANGLE WITH 5 (HL 329-5 HI-LOCKS) PAST LAST DAMAGE PER AARD A-300 ESO 30595 DATED 10/10/95. (M)

Part: SUPPORT — CORRODED (FR 72-73)

TUL - FOUND SMALL AREA OF CORROSION ON TOP FLANGE OF TEE ANGLE USED PRIMARILY FOR FLOORBOARD SUPPORT. INSTALLED A STRAP .050 THICK 301 CRES .5 HARD OVER TOP FLANGE OF TEE ANGLE WITH 5 (ML 329-5 HI-LOCKS) PAST LAST DAMAGE PER AARD A-300 ESO 30595, DATED 10/10/95. (M)

Part: COALESCER — DIRTY (ACM BAY)

JFK - FLT 1445 - AFTER TAKEOFF DURING CLIMB-OUT, ODOR/FUMES NOTED IN COCKPIT. AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN OUT PROCEDURE AND REPLACED ALL COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED APU WITH NO DEFECTS OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CABLES — CHAFED (NR 1 ENGINE)

TUL - GROUND CABLE AND C-PHASE CABLE OF NR 1 IDG, CHAFING AT HYDRUALIC MODULE LINE, LEFT SIDE OF ENGINE. REPAIRED GROUND AND C-PHASE CABLES AND REPOSITIONED FOR CLEARANCE. TST, 19,154.41 HOURS. CYCLES, 7,633. (X)

Part: WIRE — DAMAGED (CABIN)

JFK - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTING IN CROSS AISLE BETWEEN DOORS 3L AND 3R INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE BETWEEN SEATS 24C AND 27C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)