N590JB

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 70,143 hrs · 25,046 cycles

FLT # 48, TPA-LGA. SMOKE LAV SMOKE ECAM ON TAXI OUT MOC ADVISED RETURN TO GATE.; R/R SDCU IAW AMM 26-17-34, R/R AFT L/H LAV SMOKE DETECTOR IAW AMM 26-17-15. OPS CHK OK AT THIS TIME, NO FAULTS NOTED.

Part: CONTROL UNIT — FAILED (SMOKE DETECTOR) · airframe 70,143 hrs · 25,046 cycles

FLT # 48, TPA-LGA. SMOKE LAV SMOKE ECAM ON TAXI OUT MOC ADVISED RETURN TO GATE.; R/R SDCU IAW AMM 26-17-34, R/R AFT L/H LAV SMOKE DETECTOR IAW AMM 26-17-15. OPS CHK OK AT THIS TIME, NO FAULTS NOTED.

Part: OIL COOLER — LEAKING (APU) · airframe 64,563 hrs · 22,993 cycles

FLT 733, MCO-SJU. DIRTY SOCK ODOR REPORTED BY FA'S FROM ROW 17 AND TOWARDS THE REAR OF THE AIRCRAFT. ODOR SMELLED DURING TAKEOFF AND DESCENT BELOW 10,000'; C/W INFORMATION NOTICE 2017-T015F SECTION C. AIRCRAFT IS OK FOR SERVICE. ECS DECONTAMINATION WAS PERFORMED PER AMM 21-00-00. NO SMELL NOTED AT THIS TIME. DURING INFO NOTICE 2017-T015F OF THE APU, FOUND OIL COOLER LEAKING OIL ( APU SYSTEM ). R & R APU OIL COOLER PER AMM 49-91-44. OPS AND LEAK CHECK GOOD. THIS CLEARS MDDR# 431257. MX4 UPDATED PLACARDS REMOVED.

Part: SLIDE — INADEQUATE (DOOR) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, IMPROPERLY PACKED SLIDE, DOOR 842 (HITS FUSELAGE WHEN OPEN), REF AEM NR 2020/159/1-2020-383866. R & R SLIDE RAFT 842, IAW A320 AMM 25-62-44-400-803-A.

Part: FLOOR SUPPORT — CORRODED (AFT GALLEY) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, REFERENCE AEROMAN NR 2020-383925. CORROSION FLOOR STRUCTURE WEB LOCATED FR 69 TO 70 AND STR 23R AT AFT GALLEY AREA. RESOLVED ON W/O: 1075575 TASKCARD: NR-00031. R & R FLOOR STRUCTURE WEB LOCATED FR 69 TO 70 AND STR 23R AT AFT GALLEY AREA, IAW A320 SRM 51-72-11 AND DRAWING D53470100. CLASSIFIED AS MAJOR.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, EPSU 11WL FAILED OPERATIONS TEST, REF AEM NR 2020-159/1-2020-383782. PERFORMED TSM OF 11WL EPSU 33-51-00-810-801-A STEP 1-3A. PERFORMED OPERATIONS TEST, IAW A320 AMM 33-51-00-710-001-A, TEST IS OK. CLEANED CONNECTOR IAW A320 ESPM 20-55-50.

Part: SEAT TRACK — CORRODED (FRAME 12-24) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK -Y 765 LOCATED BETWEEN FR 12-24 FWD GALLEY AREA. R & R SEAT TRACK -Y 765, REF AEROMAN NR 2020-383969 FOR DETAILS.

Part: SLIDE — INADEQUATE (DOOR) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, IMPROPERLY PACKED SLIDE, DOOR 831 (HITS FUSELAGE WHEN OPEN), REF AEM NR 2020-159/1-2020-383864. R & R SLIDE RAFT 831, IAW A320 AMM 25-62-44-007-A.

Part: SUPPORT — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, REFERENCE AEROMAN NR 2020-383928. CORROSION LOWER SILL LOCATED FR 66 AT LEVEL STRINGER 23RT SIDE OF AFT GALLEY. RESOLVED ON W/O: 1075575 TASKCARD: NR-00032. R & R (PREVIOUSLY REPAIRED) LOWER SILL LOCATED BETWEEN FR 66 TO FR 68 AT LEVEL STRG 23R AFT GALLEY AREA, IAW A320 SRM 51-72-11-911-001 AND DRAWING D53480505, E53474250.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION EXIT DOOR 833 FWD AND AFT INNER FRAME SEGMENTS, REF AEM NR 2020-159/1-2020-383897. ACCOMPLISHED MODIFICATION TO REINFORCE DOOR STRUCTURE, IAW A320 SRM 51-42-11 AND EC A320-52-144.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION EXIT DOOR 843 FWD AND AFT INNER FRAME SEGMENTS, REF AEM NR 2020-159/1-2020-383898. ACCOMPLISHED MODIFICATION TO REINFORCE DOOR STRUCTURE, IAW A320 SRM 51-42-11 AND EC A320-52-144.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION EXIT DOOR 834 FWD AND AFT INNER FRAME SEGMENTS, REF AEM NR 2020-159/1-2020-383899. ACCOMPLISHED MODIFICATION TO REINFORCE DOOR STRUCTURE, IAW A320 SRM 51-42-11 AND EC A320-52-144.

Part: DUMMY RAIL — CORRODED (FWD GALLEY) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CORROSION RAIL DUMMY Y 503.2 LOCATED BETWEEN FR 12-16 FWD GALLEY AREA. R & R RAIL DUMMY Y 503.2, REF AEROMAN NR 2020-384008.

Part: SEAT TRACK — CORRODED (FWD GALLEY) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y1292 LOCATED BETWEEN FR 12-24 FWD GALLEY AREA. R & R SEAT TRACK +Y1292, REF AEROMAN NR 2020-383994.

Part: FLOOR SUPPORT — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y464 FR 64-67 AT AFT GALLEY AREA. RESOLVED ON W/O: 1075575 TASKCARD: NR-00015. R & R FLOOR BEAM -Y464 LOCATED BETWEEN FR 64-67, REF AEROMAN NR 2020-383927 FOR DETAILS.

Part: WEB — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, REFERENCE AEROMAN NR 2020-383921. CORROSION FLOOR STRUCTURE WEB LOCATED FR 69 TO FR 70 AND STR 23L AT AFT GALLEY AREA. RESOLVED ON W/O: 1075575 TASKCARD: NR-00033. R & R FLOOR STRUCTURE WEB LOCATE FR 69 TO FR 70 AND STR 23L AFT GALLEY AREA, IAW A320 SRM 51-72-11 AND DRAWING D53374180.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED BETWEEN FR 12-24. RESOLVED ON W/O: 1075575 TASKCARD: NR-00011. R & R SEAT TRACK +Y765, REF AEROMAN NR 2020-383992.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION EXIT DOOR 844 FWD AND AFT INNER FRAME SEGMENTS, REF AEM NR 2020-159/1-2020-383896. ACCOMPLISHED MODIFICATION TO REINFORCE DOOR STRUCTURE, IAW A320 SRM 51-42-11 AND EC A320-52-144.

Part: FLOOR SUPPORT — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM +Y254 LOCATED FR 12-24 FWD GALLEY AREA. R & R FLOOR BEAM +Y254 LOCATED FR 12 TO FR 24 FWD GALLEY AREA, IAW A320 SRM 51-72-11 AND DRAWING D53112816.

Part: SEAT TRACK — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 64,423 hrs · 22,942 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK -Y1292 LOCATED BETWEEN FWD GALLEY AREA. R & R SEAT TRACK -Y1292 LOCATED BETWEEN FR 12 TO FR 24 FWD GALLEY AREA, IAW A320 SRM 51-72-11 AND DRAWING D53112812.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 64,163 hrs · 22,845 cycles

FLT 92, TPA-BOS. EMERGENCY LIGHTS IN CENTER CABIN INOPERABLE. FOUND EXPOSED AND SHORTED WIRES ON ESPU TO ROW 5 SEAT HARNESS (FIN 7260VC). REPLACED CONNECTOR AND PINS, IAW AMM ESPM 20-48-21. REPLACED ESPU (FIN 11WL), IAW AMM 33-51-38.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 64,163 hrs · 22,845 cycles

FLT 92, TPA-BOS. RT EMERGENCY LIGHT OVERWING INOPERABLE (12WL). REMOVED AND REPLACED EPSU 12WL AND BATTERY PACK, IAW 33-51-38. OPERATIONS CHECK GOOD, NO FURTHER DEFECTS.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 64,163 hrs · 22,845 cycles

FLT 92, TPA-BOS. RT EMERGENCY LIGHT OVERWING INOPERABLE (12WL). REMOVED AND REPLACED EPSU 12WL AND BATTERY PACK, IAW 33-51-38. OPERATIONS CHECK GOOD, NO FURTHER DEFECTS.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 64,161 hrs · 22,844 cycles

FLT 91, BOS-TPA. OVERHEAD EXIT LIGHT INOPERABLE CENTER CABIN AND LEFT SIDE MID CABIN. R & R EMERGENCY LIGHT BATTERY AND PACK. OPERATIONS CHECKS OK, IAW 33-51-00.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 64,161 hrs · 22,844 cycles

FLT 91, BOS-TPA. OVERHEAD EXIT LIGHT INOPERABLE CENTER CABIN AND LEFT SIDE MID CABIN. R & R EMERGENCY LIGHT BATTERY AND PACK. OPERATIONS CHECKS OK, IAW 33-51-00.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 64,047 hrs · 22,801 cycles

FLT 828 MCO-EWR. AFT EXIT LIGHTS INOPERABLE (AFT DOORS AND OVERHEAD). R & R EPSU AND EPSU BATTERY (AFT LEFT), PER AMM 33-51-38. OPS CK GOOD, OK FOR SERVICE.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 64,004 hrs · 22,782 cycles

FLT 6459, MCO-TPA. (REF. PEMCO N/R 2906N156) EMERGENCY LIGHTS ABOVE R2 AND L2 INOP; (PER PEMCO N/R 2906N156) R & R EPSU AND EMERGENCY BATTERY IAW AIRBUS A320 AMM 33-51-400-001-A. OPS TEST GOOD LIGHTS ABOVE R2 AND L2 ARE OPERATING.

Part: LIGHT — FAILED (LT OVERWING) · airframe 63,889 hrs · 22,734 cycles

FLT 560, LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EPSU (11WL) IAW AMM 33-51-38. R & R OVERWING AFT LIGHT ASSY (63WL) IAW AMM 33-51-15. R & R AISLE EXIT SIGN (51WL) IAW AMM 33-51-17. OPS CHECKED OK.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 63,889 hrs · 22,734 cycles

FLT 560, WHILE T/S PROBLEM FOR EPSU FIN 11WL, SWAPPED EPSU ON RT SIDE FIN 12WL OVER TO LEFT SIDE. NO HELP, PLACED 12WL BACK IN NORMAL POSITION ON RT SIDE. NOW PROBLEM ALSO CARRIED OVER TO RT SIDE. 12WL LIGHTS INOPERATIVE. R & R EPSU (FIN 12WL) IAW 33-51-38 AND BATTERY ASSY ALL OPS CHECKED NORMAL.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 63,889 hrs · 22,734 cycles

FLT 560, LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EPSU (11WL) IAW AMM 33-51-38. R & R OVERWING AFT LIGHT ASSY IAW AMM 33-51-15. R & R AISLE EXIT SIGN (51WL) IAW AMM 33-51-17. OPS CHECKED OK.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 63,889 hrs · 22,734 cycles

FLT 560, LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EPSU (11WL) IAW AMM 33-51-38. R & R OVERWING AFT LIGHT ASSY IAW AMM 33-51-15. R & R AISLE EXIT SIGN IAW AMM 33-51-17. OPS CHECKED OK.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 63,889 hrs · 22,734 cycles

FLT 560, WHILE T/S PROBLEM FOR EPSU FIN 11WL, SWAPPED EPSU ON RT SIDE FIN 12WL OVER TO LEFT SIDE. NO HELP, PLACED 12WL BACK IN NORMAL POSITION ON RT SIDE. NOW PROBLEM ALSO CARRIED OVER TO RT SIDE. 12WL LIGHTS INOPERATIVE. R & R EPSU (FIN 12WL) IAW 33-51-38 AND BATTERY ASSY ALL OPS CHECKED NORMAL.

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 63,148 hrs · 22,464 cycles

AFT LH EPSU FAILED DURING A CAPACITY TEST. R & R ESPU IAW AMM 33-51-58. OPS CHECK PASSED. ACFT OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 59,926 hrs · 21,220 cycles

FLT 1136, LGB-SFO. ON-FLIGHT CREW REPORTS EMER LIGHT LENS COVER MISSING AT 13C AISLE; REPLACED MISSING EMERG. LIGHT COVER AS REQUIRED. OPS CKS GOOD.

Part: EPSU — FAILED (CABIN) · airframe 59,292 hrs · 20,963 cycles

FLT 857, HPN-PBI. FOUND LOWER EMERGENCY EXIT WALL LIGHTS AT OVERWING EXITS INOP; FOUND ESPU 12WL TO BE AT FAULT. R&R ESPU ASSY. OPS TEST NORMAL IAW AMM 33-51-38.

Part: FAN — FAILED (E/E BAY) · airframe 58,457 hrs · 20,643 cycles

FT # 1234, SJU-FLL. DURING CRUISE WE RECEIVED A SMOKE LIGHT AND AURAL WARNING ON THE AFT AVIONICS COMPT PANEL; PERFORMED INSP FOR ELEC BURNING SMELL IN CABIN COCKPIT CARGO AND AVIONICS COMPARTMENT FOUND NO DAMAGE OR SIGNS OF FIRE OR SMOKE IAW AMM 24-00-00-810-823-A. PERFORMED INSP OF ELECTRICAL ODORS DUE TO LIVE TV SYS IAW AMM 23-39-00-810-000-A. NO DAMAGE FOUND. FOUND AFT AVIONICS RACK VENT FAN FAILED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,898 hrs · 20,447 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM FROM FR 66 +4 " TO FR 67 + 16" BTW -Y1262 TO -Y1162 AT AFT GALLEY AREA; REPLACED FLOORBEAM FROM FR 66 + 4" TO FR 67 + 16" BETWEEN -Y1292 TO -Y1162 AT AFT GALLEY AREA. REF NR 2018-283244

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,898 hrs · 20,447 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y1162 BETWEEN FR 67 + 16' TO FR 70 AT AFT GALLEY AREA; REPLACED FLOORBEAM -Y1162 BETWEEN FR 67 +16' TO FR 69 AT AFT GALLEY AREA IAW SRM 51-72-11 & DWG D53472089 ISSUE A. REF NR 2018-283242.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,898 hrs · 20,447 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON HOLES SEAT TRACK -Y765 PAX CABIN AFT GALLEY AREA (1EA); REPLACED FLOORBEAM -Y765 BTW FR 64 TO FR 66 + 4" AFT GALLET AREA AS PER SRM 51-72-11 & DWG 53472816 REF NR 2018-283296.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,898 hrs · 20,447 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM FROM FR 66 + 4" TO FR 67 + 16" BTW +Y1292 & +Y1162 AFT GALLEY AREA; REPLACED FLOORBEAM FROM FR 66+ 4" TO FR 67 + 16" BTW +Y1292 TO +Y1162 AFT GALLEY AREA . IAW A320 SRM 51-72-11 AND DWG D53472780 REF NR 2018-283245.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,898 hrs · 20,447 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM +Y1162 BETWEEN FR 67 + 16' TO FR 70 AT AFT GALLEY AREA; REPLACED FLOORBEAM +Y1162 BETWEEN FR 67 + 16" TO FR 70 AT AFT GALLEY AREA PER SRM 51-72-11 & DWG D53472780 REF NR 2018-283243.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,898 hrs · 20,447 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y317.9 BETWEEN FR 65 TO FR 67 AT AFT GALLEY AREA; REPLACED FLOORBEAM -Y317.9 BETWEEN FR 65 TO FR 67 AT AFT GALLEY AREA AS PER SRM 51-72-11 & DWG D53472814 REF NR 2018-283247.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,898 hrs · 20,447 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y 1292 FROM FR 64 TO FR 66 +4" AT AFT GALLEY AREA; REPLACED FLOORBEAM -Y1292 FROM FR 64 TO FR 66 + 4" AT AFT GALLEY AREA AS PER DRW D53472090 & SRM 51-72-11 REF NR 2018-283246.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,785 hrs · 19,998 cycles

EPSU BATTERY 12WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,785 hrs · 19,998 cycles

EPSU 10WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKED NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,785 hrs · 19,998 cycles

EPSU BATTERY 11WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKED GOOD.

Part: LINKAGE — OUT OF ADJUST (R2 DOOR) · airframe 54,334 hrs · 19,082 cycles

R2 DOOR SLIDE ARMED INDICATION GOES OFF AND ARMED WITH HANDLE IN THE ARMED POSITION. ARMING HANDLE DOES NOT FULLY STAY DOWN, BOUNCES UP SLIGHTLY FROM CLOSED (ARMED) POSITION; ADJUSTED RELEASE MECHANISM BOTTOM LINKAGE ON R2 DOOR. OPS CHECKED GOOD. PRESSURIZED ACFT. ALL INDICATIONS NORMAL IAW 52-13-22.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 53,850 hrs · 18,892 cycles

AFT EMERGENCY LIGHT BATTERY (13WL) FAILED THE EMERGENCY LIGHT TEST. R & R AFT BATTERY IAW AMM 33-51-38, BATTERY AND EMERGENCY LIGHT SYSTEM TESTED OK.

Part: ENGINE — FAILED (NR 1) · airframe 52,880 hrs · 18,543 cycles

CAPTAIN REPORTED AN ODOR IN THE COCKPIT AFTER TAKEOFF. THE ODOR DISSIPATED AND THEN REAPPEARED DURING DESCENT. NR 1 ENGINE REMOVED AND REPLACED. OPS CHECK NORMAL IAW 36-10-00.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 48,087 hrs · 16,720 cycles

BOTH FRONT EXIT SIGNS DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED; R & R EPSU FWD OVERHEAD LT SIDE AND BATTERY EMERGENCY UNIT IAW AMM 33-51-38. OPS CK SYS IAW AMM 33-51-00, ALL CHECKS GOOD.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 48,087 hrs · 16,720 cycles

BOTH FRONT EXIT SIGNS DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED; R & R EPSU FWD OVERHEAD LT SIDE AND BATTERY EMERGENCY UNIT IAW AMM 33-51-38. OPS CK SYS IAW AMM 33-51-00. ALL CHECKS GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 47,420 hrs · 16,469 cycles

EMERGENCY EXIT SIGN OVER L1 DOOR WILL NOT ILLUMINATE. R & R EPSU IAW 33-51-18. OPS CHECKED NORMAL.

Part: VALVE — LEAKING (PARKING BRAKE) · airframe 38,987 hrs · 13,502 cycles

CREW DECLARED AN EMERGENCY DUE TO Y HYD RESERVOIR LOW ECAM, Y HYD QTY DECREASED TO 2010 AND ACCUMULATOR PRESSURE BLED TO ZERO. R & R PARKING BREAK VALVE IAW AMM 32-45-14. NO LEAKS NOTED, ALL OPS OK.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 36,656 hrs · 12,707 cycles

FLT 780 MBJ-JFK, ON MAINTENANCE CHECK FOUND EMERGENCY LIGHT BATTERY LOW MESSAGE DURING CIDS TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT PER 33-51-00. OPS CHECK OK.

Part: SENSOR — DIRTY (TEMP SYSTEM) · airframe 36,203 hrs · 12,556 cycles

FLT 796 SXM-BOS, AIRCRAFT DIVERTED TO SJU. CLIMBING THROUGH FL 320 COCKPIT AND CABIN BECAME EXCESSIVELY HOT TEMP EXCEEDING 94 DEG F. DESCENT THROUGH 6000 FEET COCKPIT AND CABIN TEMP STARTED RETURNING TO NORMAL TEMP. PER TSM 21-63-00-810-843-A INSPECTED AND CLEANED COCKPIT & CABIN TEMP SENSOR PERFORMED OPS TEST OF COCKPIT AND CABIN TEMP CTRL PER AMM 21-63-00-05 TEST OK. PERFORMED OPS TEST OF PACK 1 & 2 PER AMM 21-61-00 TEST OK. NO FAULTS PRESENT OR FOUND ON MCDU FOR PREVIOUS FLT. AIRCRAFT OK FOR CONTINUE IN SERVICE AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,803 hrs · 10,663 cycles

FLT 399 LGA-MCO, CREW REPORTED EMERGENCY EXIT LIGHTS OVER L1 AND R1 PASSENGER DOORS INOP. THE TECHNICIAN REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY (41WL) REF AMM 33-51-00. ALL CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,194 hrs · 8,654 cycles

FLT 1757 FLL-SJU A/C DIVERTED TO NASSAU - STRONG BURNING SMELL REPORTED BY MULTIPLE FLT CREW MEMBERS AND FAA JUMPSEATER ROWS 5-13. PERFORMED TSM 24-00-00-810-823. NO EVIDENCE OF ANY SMELL OF ANY KIND IN ENTIRE A/C ESPECIALLY NEAR ROWS 5-13. LIVE TV SYS WAS PREVIOUSLY DEACTIVATED.

Part: PROXIMITY SENSOR — FAILED (CABIN DOOR) · airframe 25,168 hrs · 8,641 cycles

FLT 1432 LGB-SFO RT REAR CABIN DOOR OPEN INDICATION IN FLIGHT. FLIGHT RETURNED TO FIELD (LGB). PER TSM 52-13-00-810-804 REMOVED AND REPLACED PROX SENSOR 17WV2 IAW AMM 52-73-21. ALL INDICATIONS NORMAL WHILE A/C WAS PRESSURIZED TO 2 PSI. A/C OK FOR SERVICE.

Part: POWER CABLE — FAULTY (CABIN) · airframe 13,617 hrs · 4,584 cycles

FLT 728, APPROX 8 AM, BQN TO JFK - ELECTRICAL/SMOKE ODOR AT ROW 24/25. SMELL CEASED WHEN TV'S WERE SHUT OFF. PERFORMED TSM 23-39-00-810-801 PROCEDURE. FOUND VDU CABLE ON SEB AT 23DEF WHICH POWERS THE VDU'S ON ROW 24DEF TO BE AT FAULT. CONNECTOR CONTAINS LIQUID RESIDUE AND REQUIRES MAINTENANCE. REMOVED AND REPLACED VDU CABLE AT 23DEF AND SEB AT 23E AS PRECAUTIONARY MEASURE. PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW 23-39-00 PG 5043-5045. SYSTEM OPS OK IAW 23-39-00.

Part: ACTUATOR — MALFUNCTIONED (AILERONS) · airframe 3,770 hrs · 1,270 cycles

AIRCRAFT EXPERIENCED WING FLUTTER ON CLIMB-OUT PASSING 6000 FT STEADY 250KIAS WHILE TURNING. NO ABNORMAL YAW, NO ABNORMAL INDICATION ON FLIGHT CONTROL ECAM PAGE. NO ABNORMAL INDICATION ON HYD ECAM PAGE. ONSET OF FLUTTER WAS FASTER AT HIGHER SPEED. MAX SPEED WAS 307, MAX ALTITUDE WAS FL 240. FLUTTER IN TURN (ROLL IN / ROLL OUT) CONTINUED THROUGH OUT THE FLIGHT. FLIGHT CREW DECLARED EMERGENCY AND RETURNED TO FIELD. TECHNICIANS DUPLICATED FAULT WITH RT GREEN AILERON SERVO ACTUATOR FLUCTUATING DURING TROUBLESHOOTING PROCEDURE. REMOVED AND REPLACED GREEN SYSTEM RT AILERON SERVO ACTUATOR (FIN 33CE2) IAW AMM 27-14-51. NO LEAKS NOTED, OPERATION TEST NORMAL IAW MM 27-14-00.

Part: ACTUATOR — LEAKING (L2 DOOR) · airframe 3,615 hrs · 1,212 cycles

L2 DOOR ASSIST DAMPER CYLINDER LEAKING. REPLACED L2 DOOR ASSIST ACTUATOR PER AMM 52-13-14-04. NO LEAKS NOTED.