N503JB

Part: SLIDE — NO TEST (RT OVERWING) · airframe 80,645 hrs · 30,199 cycles

FLT 2080, FLL-DCA. EPSU R/H OVERWING LOCATION 12WL FOUND EXTERIOR RED LIGHT FAULT ON TEST; R & R R/H OVERWING SLIDE PER AMM 25-62-42, OPS CHECK GOOD (EMER LTS). OK FOR SVC.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 79,765 hrs · 29,880 cycles

FLT 6435, VQQ - MCO. EMERGENCY, BAT AT 12 WL FAILED BAT CAP TEST. R & R EMERGENCY BAT AT 12WL, IAW AMM 33-51-38-400.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 79,765 hrs · 29,880 cycles

FLT 6435, VQQ - MCO. EMERGENCY BAT AT 11WL FAILED BAT CAP TEST. R & R EMERGENCY BAT AT 11WL, IAW AMM 33-51-38-400.

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 79,764 hrs · 29,879 cycles

DURING HEAVY MAINTENANCE, ROW 11 RT ESCAPE LIGHT INOPERABLE, REF FLIGHTSTAR WO N503JB-01-01 N/R 00026. R & R ROW 11 RT ESCAPE SLIDE PATH LIGHT ASSEMBLY, IAW A320 AMM 33-51-19-000-003-A. EMERGENCY LIGHT OPERATIONS CHECK CARRIED OUT, IAW A320 AMM 33-51-00-710-001. OPERATIONS CHECK GOOD.

Part: FASTENER — SHEARED (FRAME 36) · airframe 79,764 hrs · 29,879 cycles

DURING HEAVY MAINTENANCE, ACCOMPLISH REPAIR OF SHEARED FASTENERS AND CRACKS FOUND AT CENTER FUSELAGE AT FR 36 LT & RT PRESSURE PANEL AFFECTING LT & RT FITTING CONNECTION. REPAIRED IAW FLIGHTSTAR EA 20046& RDAS 80854592/003/2020 ISSUE A. REFER TO JETBLUE EC A20-838-01. CLASSIFIED AS MAJOR.

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 79,764 hrs · 29,879 cycles

DURING HEAVY MAINTENANCE, CRACKS FOUND DURING INSPECTION SB A320-53-1254. REPAIRED PER SB A320-53-1263 & FLIGHTSTAR EA 20046 & RDAS 80854592/003/2020.

Part: CROSSBEAM — CRACKED (FRAME 16) · airframe 79,764 hrs · 29,879 cycles

DURING HEAVY MAINTENANCE, FR 16 RT AND CROSSBEAM HOLE 2 CRACKED. REPAIRED FR 16RT AND CROSSBEAM HOLE 2, IAW JETBLUE EC 2018-14-09-FAA-01 & REPAIR DRAWING R531-12926 D RDAS 80857172/003/2020.

Part: CIDS — NO TEST (L2 DOOR SLIDE) · airframe 79,764 hrs · 29,879 cycles

DURING HEAVY MAINTENANCE, CIDS TEST FAIL ESPU EXT LOAD AFT LT MESSAGE. R & R L-2 DOOR SLIDE, IAW A320AMM 25-62-44-000-012-A AND 25-62-44-400-007-A. PERFORMED SATISFACTORY OPERATIONS CHECK ON L-2 DOOR SLIDE, IAW A320 AMM 33-51-00-710-001-A REF FLIGHTSTAR NR 00157. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,764 hrs · 29,879 cycles

DURING HEAVY MAINTENANCE, OVERHEAD EMEGENCY EXIT SIGN CENTER AISLE AT ROW 18 INOPERABLE, REF FLIGHTSTAR WO N503JB-01-01 N/R 00027. R & R LIGHT BULBS ON OVERHEAD EMERGENCY EXIT SIGN CENTER AISLE ROW 18 WITH SATISFACTORY OPERATIONS CHECK, IAW A320 AMM 33-51-11.

Part: CYLINDER — LOW PRESSURE (L1 DOOR ASSIST)

L1 DOOR EMERGENCY CYL/ ACCUMULATOR BELOW LIMITS; SEVICED L1 DOOR AS PER AMM 52-10-00OK FOR SERVICE + REPLACED DIAPHRAM SEAL DISK IAW AMM 52-11-14. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 77,418 hrs · 28,995 cycles

FT # 225, FWD LEFT AND AFT LEFT EMERG LIGHT BATTERIES FAILED TEST; REMOVED AND REPLACED EMERG LIGHT BATTERIES FWD LEFT 10WL AND AFT LEFT 13WL IAW AMM 33-51-38

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 77,418 hrs · 28,995 cycles

FT # 225, FWD LEFT AND AFT LEFT EMERG LIGHT BATTERIES FAILED TEST; REMOVED AND REPLACED EMERG LIGHT BATTERIES FWD LEFT 10WL AND AFT LEFT 13WL IAW AMM 33-51-38

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16. FLOORBEAM Y765 CORRODED REF NR 40126. REMOVED AND REPLACED FLOORBEAM Y765 IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL FR61 +9 REF NR 40198. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER IAW SRM REF 53-41-48-300-063 FIG 001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16, DUMMY FLOORBEAM Y 254. REMOVED AND REPLACED FLOORBEAM Y254 IAW SRM 51-72-11 STEP C & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16 DUMMY FLOORBEAM Y503.2. REMOVED AND REPLACED FLOORBEAM 503.2 IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16 Y1292. REMOVED AND REPLACED FLOORBEAM Y1292 AT FR 16 IAW SRM 51-42-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL AT FR 61 +1 REF NR 40196. REMOVED CORROSION AND INSTALLED DOUBLER AS PER SRM REF 53-41-49-300-03 FIG 1 SHEET 001 A.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL FR60+11 REF NR 40195. CORROSION REMOVED AND INSTALLED REPAIR AS PER SRM REF 53-41-40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,670 hrs · 27,564 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN AT FR 16 DUMMY FLOORBEAM Y 940. REMOVED AND REPLACED DUMMY FLOORBEAM Y940 IAW SRM 51-42-11 PAR F.

Part: OIL SYSTEM — LEAKING (APU) · airframe 72,919 hrs · 27,274 cycles

FLT 950, GND-JFK. DIRTY SOCK SMELL FROM PACK NOTICE IN DECENT SEE CABIN ODOR REPORT. (APU BLEED AIR SUPPLY SYSTEM) TROUBLESHOT PER INFO NOTICE 2017-T015C SECTION "B". FOUND OIL ON THE MATTING SURFACE OF APU INTAKE WHERE INTAKE DUCT SEATS. ENG RUN & CHK PERFORMED TO ISOLATE ENG. NO DEFECTS FOUND ON ENG. CONCLUDED APU TO BE THE CAUSE OF SMELL. APU BLEED AIR SUPPLY PUT ON MEL 36-12-01 CATEGORY "C". REQUIRES FURTHER TROUBLESHOOTING OF APU, FOR LEAKS. REQUIRED MORE GROUND TIME. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: EPSU — FAILED (EMERGENCY LIGHT) · airframe 71,344 hrs · 26,663 cycles

EMERGENCY LIGHT FAILED TO TEST. R & R THE EPSU 13WL. OPS CHECKED GOOD IAW AMM 33-51-38.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 71,277 hrs · 26,639 cycles

FWD EPSU 10WL BATTERY FAILED AN EMERGENCY LIGHTS SYS TEST. REPLACED THE EPSU BATTERY IAW AMM 33-51-38, OPS CHECKED GOOD.

Part: SLIDE — NO TEST (RT) · airframe 71,277 hrs · 26,639 cycles

FWD RT EMERGENCY SLIDE RAFT FAILED AN EMERGENCY LIGHT TEST. REPLACED THE SLIDE RAFT IAW AMM 25-62-44. FUNCTIONAL CHECKED GOOD, EMERGENCY LIGHTS TEST GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 71,277 hrs · 26,639 cycles

EMERGENCY LIGHT EPSU 11WL BATTERY FAILED AN EMERGENCY LIGHTS SYS TEST. REPLACED THE BATTERY IAW AMM 33-51-38, OPS CHECKED GOOD.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 62,498 hrs · 23,347 cycles

ACFT DIVERTED. ODOR IN AFT GALLEY. PULLED CIRCUIT BREAKERS TO COFFEEMAKERS WITH NO EFFECT. NOTED ODOR AT AFT GALLEY CIRCUIT BREAKER PANEL SO SECURED GALLEY/CABIN POWER FROM FLIGHT DECK. ODOR DISSIPATED. ELECTRICAL ODOR INSPECTION PERFORMED. DURING COFFEEMAKER TEST, FOUND MACHINE WITH SN 243161411, WARMER PLATE WIRING AREA WITH STRONG BURNING ODOR. REPLACED BOTH AFT COFFEEMAKERS. NO ODOR WITH NEW MACHINES.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 62,362 hrs · 23,301 cycles

AFT WET AREA FLOORBEAM 765 FRAME 64-FRAME 66 HAS CORROSION ON UPPER SURFACE. REF NON-ROUTINE 440271-22354. R & R FLOORBEAM IAW SRM 51-72-11, 51-44-11.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,312 hrs · 23,287 cycles

NUMEROUS EMERGENCY LIGHTS OUT THROUGHOUT ACFT. FOUND EMERGENCY LIGHT POWER SUPPLY 11WL FAILED. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-38 AND BATTERY PACK IAW AMM 33-51-38. OPS CHECKS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 62,089 hrs · 23,196 cycles

DURING MAINTENANCE, MULTIPLE SEAT EMERGENCY LIGHTS FOUND INOPERATIVE. R & R EPSU AT POSITION 11WL IAW AMM 33-51-38-400-001-A. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 61,166 hrs · 22,846 cycles

EMERGENCY LIGHT SYS TEST FAILED, FWD EXT LOAD FAULT. FOUND R-1 DOOR CONNECTOR ON FRONT OF SLIDE PACK PARTIALLY DISCONNECTED. CONNECTED, EMERGENCY SYS LIGHT TEST OK. REF AMM 33-51-00.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 60,356 hrs · 1,589 cycles

DURING MAINTENANCE CABIN EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 3, 5, 7, 9, 15, 23, 25C. APPLIED TSM 33-57-00-810-801A, FOUND PSU (11WL) UNIT FAULT. R & R EMERGENCY PSU (11WL) OPS CKD OK IAW 33-57-38. CABIN EMER. LIGHTS OPS CKD NORMAL IAW 33-57-00.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 22,407 hrs · 59,851 cycles

ON MAINTENANCE CHECK FOUND EPSU 11WL UNIT FAULTED. EMERGENCY PATH LOW LEVEL LIGHTS INOPERATIVE EVERY OTHER SEAT. R & R EPSU 11 WL IAW AMM 33-51-38. OPS CHECK GOOD.

Part: EPSU — NO TEST (EMERGENCY LIGHT) · airframe 59,769 hrs · 22,382 cycles

DURING MAINTENANCE, THE RED OVERWING EMERGENCY EXIT LIGHT IS NOT WORKING. R & R ESPU & BATTERY PACK IAW AMM 33-51-38. ALL EMERGENCY LIGHTS NOW CHECK OK. ADDITIONAL PART REPLACED, DIEHL, PN 3214-31, SN 767628, TAT 2218, TAC 816, TIME SINCE 2218.

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 59,664 hrs · 22,342 cycles

DURING WEEKLY CHECK EMERGENCY LIGHT SYS TEST FAILED AND SOME CABIN RT EMERGENCY LIGHT FOUND INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY AT 12WL IAW AMM 33-51-38. EMERGENCY LIGHT CHECKED OK. IN ADDITION EMERGENCY LIGHT SYSTEM TEST FAILED AND SOME AT THE FORWARD CABIN LT SIDE, 11WL, FOUND INOPERATIVE. PERFORMED T/S IAW TSM 33-51-00-810-801-A. R & R POWER SUPPLY, SN 2879 AT POSITION 11WL WITH TOTAL HOURS 53957, TOTAL CYCLES 20076, TIME SINCE 67. OPS CHECK OK.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 59,627 hrs · 22,328 cycles

DURING HEAVY MAINTENANCE CHECK, EMERGENCY EXIT LIGHTS ON SEATS 15 AND 19 DID NOT ILLUMINATE. R & R EPSU AT 11WL IAW AMM 33-51-38-000-001 AND AMM 33-51-38-400-001-A. OPS CHECK GOOD.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 59,384 hrs · 22,229 cycles

DURING THE WEEKLY CHECK, EMERGENCY LIGHT TEST FAILED ON LT EPSU AT FIN 11WL. R & R EMERGENCY LIGHT EPSU AT FIN 11WL IAW AMM 33-51-38. LIGHT CHECKED OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 58,554 hrs · 21,932 cycles

ON MAINTENANCE CHECK, THE EMERGENCY LIGHT TEST HAD AFT LT EXTERNAL LOAD FAULT MESSAGE. FOUND L-2 DOOR SLIDE CONNECTOR ON SLIDE PACK NOT FULLY CONNECTED. CLEANED PLUG AND RE-CONNECTED. EMERGENCY LIGHT TEST OK. NO FAULTS REF. AMM 33-51-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,550 hrs · 21,566 cycles

DURING MAINTENANCE CHECK, FOUND RT EMERGENCY POWER SUPPLY UNIT FAILED THE EMERGENCY LIGHT TEST. R & R RT EPSU AND BATTERY IAW AMM 33-51-38, OPS CHECKED OK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHT) · airframe 57,550 hrs · 21,566 cycles

DURING MAINTENANCE CHECK, FOUND RT EMERGENCY POWER SUPPLY UNIT FAILED EMERGENCY LIGHT TEST. R & R RT EPSU AND BATTERY IAW AMM 33-51-38, OPS CHK OK.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 54,226 hrs · 20,404 cycles

CREW DECLARED AN EMERGENCY AND ACFT DIVERTED DUE TO FCTL FLAPS LOCKED. ALIGNMENT FAULT ECAM ON LANDING. INSPECTED INTEGRITY OF LT FLAP MECHANISM IAW TSM 27-51-00. NO FAULTS NOTED. RESET SYS, ACCOMPLISHED TEST OF FLAPS IAW AMM 27-54-00. NO FAULTS NOTED. OK FOR CONTINUED SERVICE.

Part: BOTTLE — EMPTY (L1 DOOR ASSIST) · airframe 54,222 hrs · 20,401 cycles

DURING MAINTENANCE CHECK, FOUND L1 DOOR ASSIST BOTTLE AT 0 PSI. R & R L1 DOOR ASSIST BOTTLE DIAPHRAGM AND SERVICED BOTTLE. NO LEAKS NOTED REF 52-11-14. ACFT RESTORED TO NORMAL CONFIGURATION.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 53,328 hrs · 20,100 cycles

AIR RETURN TO DEPARTURE DUE TO VENT SKIN VALVE ECAM FAULT AND ACFT COULD NOT PRESSURIZE. IAW TSM 21-26-00-810-804A, R & R SKIN AIR OUTLET VALVE IAW AMM 21-26-53. CHECKED NORMAL.

Part: TACHOMETER — SHEARED (NR 2) · airframe 46,553 hrs · 17,702 cycles

FLT 824 SDQ-JFK, CREW DECLARED EMERGENCY DUE TO ECAM MESSAGE "BRAKES" AUTO BRK FAULT "BRAKES RELEASED". THE TECHNICIAN FOUND NR 2 TACHOMETER DRIVE SHAFT SHEARED. REMOVED AND REPLACED TACH AND DRIVE SHAFT IAW AMM 32-42-57-04. OPS CHECK GOOD.

Part: FUEL — CONTAMINATED (WING TANK) · airframe 45,703 hrs · 17,425 cycles

FLT 318 OAK-IAD, CREW EXECUTED AN EMERGENCY LANDING DUE TO FUEL LOSS OF 1000 LBS UNACCOUNTED FOR ON LEFT SIDE OF AIRCRAFT. COULD NOT ISOLATE LEAK BUT IT STOPPED AFTER CENTER TANK CLOSED. COULD BE APU OR CENTER TANKS. TECHNICIAN SUMPED L&R WING TANKS PER AMM 12-11-28. FOUND 1+ QTS WATER IN EACH WING TANK (INNER). CTR TANKS NORMAL. NO FUEL LEAKS NOTED AT THIS TIME. INTERROGATION OF CFDS (FQIC) NORMAL. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 45,235 hrs · 17,265 cycles

FLT 415 BOS-SAN, HAD AN AIR RETURN TO BOSTON DUE TO CENTER TANK PUMP 1 FAILED AFTER SLAT RETRACTED. PERFORMED OPS CHECK OF NR 1 CENTER TANK PUMP PER AMM 28-21-51. OPS CHECK NORMAL. SUSPECT IMPROPER CONFIGURATION OF AIRCRAFT DUE TO MEL 28-21-02 CONDITION 1 BEING APPLIED TO THE NR 2 CENTER TANK PUMP.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,055 hrs · 14,634 cycles

FLT 708, SJU-JFK, FLT CREW REPORTED SMELL COMING FROM ROW 9 AREA AND DISSIPATED WHEN LTV SYS WAS TURNED OFF. COMPLIED WITH TSM TASK 24-00-00-81-823. NO DEFECTS NOTED. INSPECTED SEAT TO SEAT CABLE AND DPCU CABLE 7-9 ABCDEF, UNABLE TO IDENTIFY ANY DAMAGE, TSM TASK 23-39-00-810-801 ACCOMPLISHED. ALL SYS OPS NORMAL.

Part: ENTERTAIN SYS — ODOR · airframe 38,055 hrs · 14,634 cycles

LIVE TV SYSTEM ALL, FLT CREW REPORTED ODOR COMING FROM ROW 9 AREA AND DISSAPATED WHEN LIVE TV SYSTEM WAS TURNED OFF. COMPLIED WITH TSM TASK 24-00-00-810-823. NO DEFECT NOTED. TSM TASK 23-39-00-810-801 NEEDS TO BE ACCOMPLISHED ON LIVE TV SYSTEM. LIVE TV SYSTEM DEACTIVATED AND PLACED ON MEL 25-22-03 COND 1 CAT D PER MCC. LIVE TV C/B B8 OF 2000V4 PULLED AND COLLAED MCC NOTIFIED MX-4 UPDATED PLACARD INSTALLED. INSPECTED SEAT TO SEAT CABLE, VDU CABLE, AND DPCU CABLE ROW 7-9 ABCDEF UNABLE TO IDENTIFY ANY DAMAGE OR ABNORMAL. ALL LIVE TV SYSTEM OPS NORMAL REACTIVATE SYS PER TSM 23-39-00-810-801 MDDR 62587, CLEARED MX-4 UPDATED PLACARD REMOVED MCC NOTIFIED.

Part: COMPUTER — FAULTY (NR 1) · airframe 37,248 hrs · 14,335 cycles

FLT 1756 - SJU-FLL - WHEN SELECTING FLAPS 2 RECEIVED F/CTL FAULT ECAM. FLAPS WERE STUCK AT 0. COMPLETED ECAM AND QRH AND LANDED PER QRH/DISPATCH/MTC IN THAT CONFIGURATION. PERFORMED TROUBLESHOOTING AS PER TSM 27-51-00. DURING TROUBLESHOOTING FOUND THAT ALL FAULTS AND FAILURES FOLLOWED SFCC ORIGINALLY INSTALLED IN POSITION NR 1 AS IT WAS SWAPPED MULTIPLE TIMES TO POS 2 AND BACK. REMOVED & REPLACED SFCC NR 1 IAW AMM 27-51-34. OPS CHECKS GOOD. NO FAULTS NOTED.

Part: THERMOSTAT — FAILED (BLEED AIR SYS) · airframe 37,078 hrs · 14,271 cycles

FLT 180, PHX-JFK, CRUISING AT 37,000, BLEED 2 THEN BLEED 1 FAULTED (BLEED AIR SUPPLY SYSTEMS). REMOVED AND REPLACED NR 1 ENG BLEED AIR SUPPLY SYS THERMOSTAT IAW 36-11-43-04, LEAK CHECK & OPS CHECKS OK.

Part: MONITOR — FAILED (CABIN) · airframe 35,966 hrs · 13,849 cycles

FLT 204, LGB-JFK, SEAT 16A TV INOP, BURNING SMELL PRIOR TO FAILURE. SEAT BOX WAS WARM TO TOUCH. ACCOMPLISHED INSPECTION PER 24-00-00-810-823. NO DEFECTS NOTED.

Part: ACTUATOR — CONTAMINATED (T/E FLAP) · airframe 31,290 hrs · 12,151 cycles

FLT 352, BUR-JFK. DURING CONFIGURATION FROM FLAPS 1 TO 2 F/CTL FLAPS LOCKED ECAM. WING TIP BRAKE ON. REMOVED AND REPLACED NR 1 & 2 RT WING FLAP ACTUATORS, RIG/ADJUST OF RT FLAP OPERATIONAL TEST GOOD IAW 27-54-49 AND 27-54-00-05.

Part: ACTUATOR — CONTAMINATED (T/E FLAP) · airframe 31,290 hrs · 12,151 cycles

FLT 352, BUR-JFK. DURING CONFIGURATION FROM FLAPS 1 TO 2 F/CTL FLAPS LOCKED ECAM. WING TIP BRAKE ON. REMOVED AND REPLACED NR 1 & 2 RT WING FLAP ACTUATORS. RIG/ADJUST FLAP OPERATIONAL TEST GOOD IAW 27-54-49 AND 27-54-00-05.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 29,342 hrs · 11,502 cycles

UPON TEST L1 & R1 EMERGENCY LIGHTS DID NOT WORK. REPLACED POWER SUPPLY IAW AMM 33-51-38-04. OPS CHECK NORMAL UPON TEST.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 29,342 hrs · 11,502 cycles

UPON TEST ROW 10 ABC EMERGENCY LIGHTS DID NOT WORK. REMOVED AND REPLACED POWER SUPPLY (12WL) PER AMM 33-51-38-04. OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 22,746 hrs · 9,193 cycles

DURING EMERGENCY LIGHT SYSTEM TEST. EPSU EMER. L DISPLAYED. REMOVED AND REPLACED EPSU (11WL) BATTERY PACK IAW AMM 33-51-38. SYSTEM OPS CHECK GOOD.

Part: ENTERTAIN SYS — MALFUNCTIONED (CABIN) · airframe 19,961 hrs · 8,215 cycles

FAINT BURNING SMELL FOR SHORT DURATION SMELLED ON FRONT GALLEY. COMPLIED WITH INFO NOTICE 2004-T023TR. ALSO COMPLIED WITH TSM TASK 24-00-00-801-832. LTV FOUND TO BE INOP ALL CHANNELS, MEL'D LTV SYS (REF L/P 88796 ITEM 1). NO OTHER SMELLS OR SMOKE NOTED DURING TEST. UPON ARRIVAL AT JFK ACCOMPLISHED INFO NOTICE 2004-T023 TR, FOUND TVS WORKING SATISFACTORY AND AT THIS TIME NO BURNING SMELL NOTICED. MEL CLEARED. NO COMPONENTS CHANGED.

Part: ELECTRICAL BOX — MALFUNCTIONED (ENTERTAIN SYS) · airframe 17,254 hrs · 7,260 cycles

3O MINS INTO FLIGHT FA NR 1 REPORTED AN ODOR EMITTING FROM ROW 1-4, TURNED LIVE TV MASTER SWITCH TO OFF, SMELL WAS GONE AFTER 3 MIN. TV'S WERE WORKING PRIOR TO TURNING THE MASTER SWITCH OFF. COMPLIED WITH INFO NOTICE 2003-T050TR A. NO ABNORMALITIES WERE FOUND. REMOVED AND REPLACED SEB'S AT 2B & 2E FOR PRECAUTIONARY MEASURE IAW CMM 23-39-00. SYSTEM OPERATION SATISFACTORY. SEB S/N 5460 & 2017.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 14,310 hrs · 6,220 cycles

LANDING GEAR MALFUNCTIONED ON FIRST ATTEMPT. SECOND ATTEMPT LANDING GEAR FUNCTIONED PROPERLY. UPON LANDING ECAM L/G SYS DISAREE. CHECKED LGCIU 1 AND 2 FOR LAST LEG HISTORY. FOUND RT DOOR PROX FAULT ON LGCIU NR 2. CHECKED SENSOR 34GA REF TSM TASK 32-31-00-810-816 STEP 3. FAULT NOT CONFIRMED. BITE CHECKED LGCIU 1AND 2 OPERATES NORMALLY. OK FOR FURTHER SERVICE.

Part: WIRE HARNESS — NICKED (EMERGENCY LIGHT) · airframe 13,760 hrs · 6,172 cycles

EMMERGENCY LIGHT HARNESS AT LT ROW LOCATION 3, 6, 8, 10, 12, 14, 18, 22 AND 26 HAS NICKS AND POSSIBLE DAMAGE. REPAIRED HEAT SRINK TUBING IAW ESPM 20-53-29 AT 6 LOCATIONS AND REPLACED HARNESS AT ROW 14, 22, 26.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,243 hrs · 5,855 cycles

DURING WEEKLY CHECK FOUND AFT EPSU BATTERY FAILING TEST. REPLACED LEFT AFT BATTERY PER AMM; TEST OK.

Part: TUBE — LEAKING (HYD SYSTEM) · airframe 11,287 hrs · 5,143 cycles

APPROX 1 HOUR AFTER DEPARTURE FROM JFK, FLT. 91, CREW REPORTED GREEN HYD SYSTEM QTY LOW. APPROX 1 HOUR LATER CREW REPORTED ECAM GRN RES LOW QTY. CREW C/W ECAM ACTION, DISCUSSED OAK ARRIVAL ACTION. GRAVITY GEAR EXTENSION, ALT BRAKES AVAILABLE AND HAVING A/C MAINT MEET AIRCRAFT AT END OF RUNWAY WITH TUG AND TOWBAR. CREW AS PRECAUTIONARY DECLARED EMERGENCY. FOUND EDP CASE DRAIN LINE LEAKING IN PYLON. REPLACEMENT LINE NOT AVAILABLE LOCALLY. PERMASWAGE OR RYNGLOC PERMANENT REPAIR NOT AN OPTION DUE TO SPACE CONSTRAINTS. C/W TEMP FLEX LINE REPAIR IAW AMM 20-23-11-300-004. PERMANENT REPAIR DUE AT NEXT -A- CHECK AND DAILY REINSPECT REQUIRED.

Part: SHOCK ABSORBER — MISALIGNED (NOSE GEAR) · airframe 10,723 hrs · 4,892 cycles

FLT #3, BUF to JFK, Landing gear shock absorber fault Wheel Nose wheel Steer fault ECAM after take off. Gear would not go up. Nose gear 90 degree on landing with failure.Inspected nose gear, Removed and replaced shockstrut assy per AMM 32-21-13-401 and AMM 32-21-13-000-001, Ops and leak check ok, performed normal and alt gear operation, all normal and OK for service as per ref AMM 32-21-16-000-002. Note: Crew reported that after take off from BUF gear would not retract. research of PFR data showed L/G shock absorber fault with associated NLG prox sensor faults identified by both LGCIU 1 and 2. Also a NW Steering fault was identified by BSCU 1 and 2.Aircraft landed at JFK iaw FCOM procedures 3.02.32 P1. N

Part: POWER SUPPLY — FAILED (CABIN) · airframe 9,028 hrs · 4,226 cycles

AT JFK, ON WEEKLY EMERGENCY LIGHT SYSTEM TEST HAD EPSU LEFT FAILURE. REMOVED AND REPLACED LEFT EPSU AND GROUND OPS CHECKED OK PER MM 33-51-00.

Part: TACHOMETER — DAMAGED (NR 1 BRAKE) · airframe 10,534 hrs · 4,212 cycles

AT JFK FLT 77, EXPERIENCED BRAKE ECAM ON T/O ROLL AT LOW SPEED. ABORTED T/O AND RETURNED TO GATE. T/S FOUND NR 1 TACH SPLINE DAMAGED & HUB CAP, ALSO NR 3 HUB CAP SPLINE FAN TACH. REMOVED AND REPLACED NR 1 TACH, NR 1 HUB CAP AND NR 3 HUB CAP PER AMM 32-42-68, 32-38-51, PERFORMED OPS CHECK PER AMM 32-42-00, SYSTEM OPS CHECK GOOD.

Part: SKIN — PUNCTURED (FUSELAGE)

AT JFK ON WALK AROUND INSPECTION, FOUND PUNCTURE ON FORWARD LEFT FUSELAGE BELOW CAPTAINS FIXED WINDOW. REMOVED EXISTING FASTENERS, MANUFACTURED REPAIR DOUBLER AND PICKED UP NEW FASTENERS IN REPAIR PER SRM 53-00-11. INSTALLED DOUBLER AS PER SRM 53-00-11. (M)