N632JB

Part: UNKNOWN — ODOR (CABIN) · airframe 71,486 hrs · 25,563 cycles

FLT#1015, EWR-PUJ. 'THE INFLIGHT CREW NOTICED A "DIRTY SOCK" SMELL AT TOP OF DESCENT. THEY CALLED ON THE GROUND TO TELL US IT GOT VERY STRONG. APU WAS NOT RUNNING. ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — ODOR (CABIN) · airframe 71,495 hrs · 25,565 cycles

FLT#2319, EWR-AUA. 'LEVEL 1 ODOR EVENT IN DESCENT. OIL SMELL STARTED AT 10,000 AND DISSIPATED AT 3,000. FLT CREW AND FWD FA SMELLED ODOR, AFT FA SMELLED NOTHING. COMPLETED ODOR RECOGNITION GUIDANCE CHECKLIST AND ODOR REPORTING FORM. APU OFF ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: WIRE — DAMAGED (ZONE 200) · airframe 71,372 hrs · 25,512 cycles

FLT#1745, JFK-PSE. 'L-1 INOP SEAT EXIT LT + COVER INOP ( EXIT MARKING SIGNS (WITHOUT PASSENGERS) ); REPLACED EMERGENCY EXIT SIGN ASSEMBLY AT DOOR L1 AND REPAIRED DAMAGED WIRES TO ASSEMBLY PER ESPM 20-43-11-01. TEST OK MCC HANY NOTIFIED.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,377 hrs · 23,931 cycles

FLT#803, JFK-SJU. 'STRONG FUMES ODOR ON DESCENT- THRUST AT IDLE PACKS ON APU OFF IN FLIGHT DECK AND CABIN BELOW 10,800 FEET; PERFORMED LEVEL B DECONTAMINATION AS PER TSM 05-50-00-810-085-B AND INFO NOTICE 2017-T015J STEP B2, COMPLIED WITH GROUND UNIT . R/R RECIRC FILTERS AND OZONE FILTERS PER AMM 21-21-41 AND 21-51-41, PERFORMED IDLE RUN ON LEFT AND RIGHT ENG WITH PACKS RUNNING. AIR QUALITY GOOD. APU FOUND TO BE THE SOURCE OF THE ODOR EVENT. TO BE PLACED ON MEL.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,272 hrs · 23,889 cycles

FLT#182, BNA-FLL. ' DURING DESCENT APPROACHING 10,000 DETECTED A STRONG DIRTY SOCK SMELL TOXIC FUMES ODOR WAS PRESENT UNTIL LANDING AND PERSISTENT. ODOR WAS VERY STRONG IN COCKPIT AND CABIN SOURCE OF ODOR IS VENTILATION SYSTEM; COMPLIED WITH INFONOTICE 2017-T015J IDENTIFIED SOURCE OF ODOR TO BE APU OIL LEAK. PERFORMED ECS DECON WITH GROUND UNIT. REMOVED AND REPLACED LH/RH RECIRC FILTERS. AIR QUALITY CHECK GOOD. APU TO BE PLACED ON MEL . PER AMM 21-52-00.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,053 hrs · 23,793 cycles

FLT#1015, EWR-PUJ. 'DIRTY SOCKS SMELL ON FINAL APP; PERFORMED DECONTAMINATION OF PACK 1 AND 2 IAW AMM 21-00-00-615-803-A. REF ITEM I LG 3634450 (PER INFO NOTICE 2017-T015J ACCOMPLISHED LEVEL B DECONTAMINATION OF ECS IAW AMM 21-00-00615-803-A. AN ODOR PRESENT WITH ENG 1 AND ENG 2 ON IDLE. ) PACK 1 AND 2 OK MDDR CLEAR. MX-4 UPDATED.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,034 hrs · 23,786 cycles

FLT#894, EWR-STI. ' FA'S REPORTED STRONG DIRTY SOCK SMELL ON FINAL STATED REALLY STRONG IN THE AFT C THEN FWD CABIN; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B1. ODOR ISOLATED TO THE APU, APU PLACED ON MEL SEE ITEM 2.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,409 hrs · 23,167 cycles

FLT#765, JFK-GCM. 'STRONG DIRTY SOCK SMELL PASSING 8,000FT, 250KTS POWER IDLE, APU NOT ON SMELL REMAINED. AFTER LANDING AND PARKING APU ON AND APU BLEED ON ( APU SYSTEM ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,412 hrs · 23,168 cycles

FLT#766, GCM-JFK. ' STRONG ODER DURING DESCENT VERY SIMILAR TO PREVIOUS FLT APU WAS MEL'D OUT OF SERVICE, PASSING 8000FT 220 KTS IDLE LASTED UNTIL LANDING THEN SLOWLY WENT AWAY; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2 DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 21-00-00-615-803A AIRCRAFT IS OK FOR SERVICE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H2 AT DOOR STOP FITTING 7, CRACK DIRECTION IS 6 O'CLOCK, AT FWD GALLEY AREA (1 EA ); REF AEROMAN NR 2023-193644 WO 2023 90/1 REMOVED AND REPLACED INTERCOSTAL FITTING #7 AND FASTENER LOC BETWEEN FR15 AND FR16 RH SIDE AT LEVEL DOOR STOP #7 IAW A320 SRM-51-42-11; A320 SRM-51-72-11; DWG D53135400; DWG R53113118 TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N:220272512, DUE DATE:17-DEC-2023; SMALL GAUGES P/N:154-901, S/N: AE-412975, DUE DATE: SEP-05-2023; CALIPER P/N:500-752-20, S/N: B16101293, DUE DATE: OCT-08-2023; ET EQUIPMENT P/N: NORTEC 600D S/N:220272712, DUE DATE: DEC-17-2023; SMALL GAUGES P/N:154-901, S/N: AE-403298, DUE DATE: SEP-08-2023; MICROMETER P/N:293-344-30, S/N:71690646, DUE DATE: NOV-29-2023; TORQUE P/N: QD1200, S/N:0318902711, DUE DATE:OCT-25-2023 DONE BY S. MURCIA 8672520.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: REF A320-52-1145-01-JB. CRACK INDICATIONS WERE FOUND ON THE INSIDE OF THE INNER EMERGENCY EXIT HATCH FRAME SEGMENT )1) AT EMERGENCY EXIT DOOR 833; REF AEROMAN NR 2023-193805 WO 2023 90/1 ACCOMPLISHED EC A320-52-1144, TASK CARD A320-52-1144-01 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH FRAME / REINFORCE DOOR STRUCTURE MODIFICATION. ON EMERGENCY EXIT DOOR 833 FOR REPLACEMENT OF FRAME SEGMENT (1)- TO COLLECT SDR NUMBER FOR TRACKING PURPOSES DONE BY M. MARMOL 8613913.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: REF A320-52-1145-02-JB. CRACK INDICATIONS WERE FOUND ON THE INSIDE OF THE INNER EMERGENCY EXIT HATCH FRAME SEGMENT )1) AT EMERGENCY EXIT DOOR 843; REF AEROMAN NR 2023-193807 WO 2023 90/1 ACCOMPLISHED EC A320-52-1144, TASK CARD A320-52-1144-02 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH FRAME / REINFORCE DOOR STRUCTURE MODIFICATION. ON EMERGENCY EXIT DOOR 843 FOR REPLACEMENT OF FRAME SEGMENT (1)- TO COLLECT SDR NUMBER FOR TRACKING PURPOSES DONE BY M. MARMOL 8613913.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE OF BOTTOM SKIN PANEL NO3 BTW GEAR RIB 5 AND RIB 5A ON LH WING (CPCP RELATED MPD TASK 575167-01); PERFORMED REPAIR ON UPPER SURFACE OF BOTTOM SKIN PANEL NO 3 BTW GEAR RIB 5 AND RIB 5A ON LH WING TOOL USED DIGITAL CALIPER P/N 500-752-20 S/N B16101265 DUE DATE NOV-15-2023. ULTRASONIC THICKNESS GUAGE P/N 45MG /N 130061901 CAL DATE APR 082023 EDDY CURRENT EQUIPMENT P/N NORTEC 500D S/N N500X12101V022233 CAL DATE AUG-30-2023 ALL WORK ACCOMPLISHED ON AEROMAN WO 2023-90/1 NR 2023-193678. (CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: REF A320-52-1145-03-JB. CRACK INDICATIONS WERE FOUND ON THE INSIDE OF THE INNER EMERGENCY EXIT HATCH FRAME SEGMENT )1) AT EMERGENCY EXIT DOOR 834; REF AEROMAN NR 2023-193806 WO 2023 90/1 ACCOMPLISHED EC A320-52-1144, TASK CARD A320-52-1144-03 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH FRAME / REINFORCE DOOR STRUCTURE MODIFICATION. ON EMERGENCY EXIT DOOR 834 FOR REPLACEMENT OF FRAME SEGMENT (1)- TO COLLECT SDR NUMBER FOR TRACKING PURPOSES DONE BY M. MARMOL 8613913.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: ACCOMPLISH DOOR/EMERGENCY EXIT/OVERWING EMERGENCY EXIT HATCH (AFT RH EEH) FRAME/REINFORCE DOOR STRUCTURE MODIFICATION FOR TRACKING PURPOSES; REF AEROMAN NR 2023-193899 WO 2023 90/1 ACCOMPLISHED EC A320-52-1144 TASK CARD A320-52-1144-04 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION TO COLLECT SDR NUMBER FOR TRACKING PURPOSES.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H2 AT DOOR STOP FITTING 7, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA (1 EA ); REF AEROMN NR 2023-193647 WO 2023 90/1 PERFORMED PERMANENT REPAIR LOCATED ON FRAME 16 LH SIDE AT LEVEL DOOR STOP FITTING 7 FWD GALLEY AREA IAW REPAIR INSTRUCTION R5311311. TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D, SN: 220272512, DUE DATE: 17 DEC 23. TOOL USED SMALL HOLE GAUGES P/N: 154-901 S/N: SE-412975. DUE DATE: SEP-05-2023 AND CALIPER P/N: 500-752-20 S/N: B16101293 DUE DATE: OCT-08-2023. MICROMETER P/N: 293-344-30, S/N: 72747780, DUE DATE: NOV-23-2023. ET TOOL USED: PN: MIZ-21C, SN: 769680, DUE DATE: 07-JUL-23. TOOL USED ULTRASONIC THICKNESS GAGE PN 45MG SN 130066401 DUE DATE SEP-21-2023. TORQUE P/N: QD1200; S/N: 0318902711; DUE DATE: OCT-25-2023 DONE BY R. BRITO 8603909.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: REF JB 534195-01-2-A. CRACK FLOOR STRUCTURE SECTION CONNECTION FR 66 AT LEVEL Y1292 IN PASSENGER CABIN; REF AEROMAN WO 2023-90/1, NR 2023-193817. REMOVED AND REPLACED FLOOR STRUCTURE SECTION CONNECTION LOC FR66 AT LEVEL Y1292 IN PASSENGER CABIN ON FWD GALLEY AREA IAW A320-SRM51-72-11 AND DWG E53474250 AND SRM 51-11-12 FIG 020. (SHEET 1).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7, CRACK DIRECTIONS ARE 12, 2, AND 3 CLOCK, AT FWD GALLEY AREA (3 EA); REF AEROMAN NR 2023-193648 WO 2023 90/1 PERFORMED PERMANENT REPAIR LOCATED ON FRAME 16 LH SIDE AT DOOR STOP FITTING 7, AT FWD GALLEY AREA IAW REPAIR INSTRUCTION R5311311. TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D, SN: 220272512, DUE DATE: 17 DEC 23. TOOL USED SMALL HOLE GAUGES P/N: 154-901 S/N: SE-412975. DUE DATE: SEP-05-2023 AND CALIPER P/N: 500-752-20 S/N: B16101293 DUE DATE: OCT-08-2023. MICROMETER P/N: 293-344-30, S/N: 72747780, DUE DATE: NOV-23-2023. ET TOOL USED: PN: MIZ-21C, SN: 769680, DUE DATE: 07-JUL-23. TOOL USED ULTRASONIC THICKNESS GAGE PN 45MG SN 130066401 DUE DATE SEP-21-2023. TORQUE P/N: QD1200; S/N: 0318902711; DUE DATE: OCT-25-2023 DONE BY R. BRITO 8603909.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,340 hrs · 23,140 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FR16 RH OPEN FASTENER HOLE H3 DOOR STOP FITTING 7 CRACJ DIRECTION IS 6 & 9 OCLOCK; REMOVED AND REPLACED INTERCOSTAL FITTING # 7 BETWEEN FR15-FR16 RH SIDE DOOR STOP 7 IAW A320 SRM 51-42-11 & A320 SRM 51-72-11 REF AEROMAN WE 2023-193645 WO 2023 90/1.

Part: NONE — NONE · airframe 64,129 hrs · 22,695 cycles

FLT#841, JFK-SAV. 'DIRTY SOCK SMELL PLUS FUME/ ODOR ON DEPARTURE OUT OF JFK AND VERY STRONG AT 1500 FEET COMING INTO SAV. EXPERIENCED THRU OUT THE CABIN INFLIGHT AND CUSTOMERS SAID VERY NOTICEABLE, ( BLEED AIR SUPPLY SYSTEMS ); PERFORMED TSM 05-50-00-810-831A ISOLATED ODOR TO APU BLEED. PERFORMED LEVEL B ECS DECONTAMINATION ON PACKS 1 AND 2 AND CABIN FILTER CHANGED REF AMM 21-21-41 AND 21-00-00-615-803A. ENG #1 BLEED GOOD. MDDR CLEARED. MX-4 UPDATED.'

Part: NONE — FAILED (12HL) · airframe 63,297 hrs · 22,369 cycles

FLT#1463, LAX-CUN. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO LAX) 'DURING CLIMB THROUGH 15000 FEET NOTICEABLE CABIN PRESSURE FLUCTUATION OCCURRED WITH SIMULTANEOUS ECAM " CAB PRESS SYS 1 FAULT" CAB PRESS V/S FLUCTUATIONS CONTINUED VARYING BETWEEN -1900 TO + 1000. AIR RETURN TO LAX; REF L/P 3358463-1(REMOVED AND REPLACED CABIN PRESSURE CONTROLLER 1 PER AMM 21-31-34 BITE TEST PASSED. OPS CHECK GOOD) FOR CORRECTIVE ACTION. PERFORMED PRESSURIZATION TEST PER AMM 05-53-00-780-003-A01. PRESSURIZED TO 6.0 PSI OBSERVED NO FLUCTUATIONS IN CAB PRESS V/S. ALL INDICATIONS ARE NORMAL. NO DEFECTS NOTED AT THIS TIME.'

Part: NONE — FAILED (10HL) · airframe 63,296 hrs · 22,368 cycles

FLT#1463, LAX-SJD. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO LAX) 'DURING CLIMB CABIN PR SYS 1 FAULT LEVELED AT 21000 DUETO STRONG PRESSURE FLUCTUATIONS. THE CABIN OUTFLOW VALVE OPENED AND CLOSED RAPIDLY. 2800-3100 CABIN ALT. VS CLMB AND 1000 / -1000 10 MIN AFTER SYS 1 FAULT ECAM SYS 1 AND 2 FAULT CABIN PRESSURE USED MANUL BACKUP FOR REMAINDER OF FLIGHT BACK TO LAX; REF LAST LEG REPORT FAULT CODE (81) PER TSM 21-31-00-810-828A. NO ICE OR WATER WAS FOUND. REMOVED AND REPLACED 19HL OUTFLOW VALVE PER AMM 21-31-51. PERFORMED CPC #1 & #2 BITE TEST, PASS. MANUAL MODE CHECK NORMAL.

Part: HYDRAULIC LINE — LEAKING · airframe 62,027 hrs · 21,894 cycles

FLT#54, PBI-JFK. (AIRCRAFT DECLARED EMERGENCY). ' LOST "PARTIAL" GREEN HYDRAULIC FLUID WITH ASSOCIATED LO PRESSURE ECAM GEAR EXTENDED NORMALLY; REF LOG PAGE 3238437 ITEM #2 FOUND GREEN HYD LINE UPPER L/H LANDING GEAR LEAKING.PERMASEWDGE REPAIR WAS ACCOMPLISHED.PERFORMED OPS CHK OF GREEN HYD SYS VIA # 1 EDP & ELECTRICALLY/ PTU OPS CHK O.K.NO LEAKS NOTED.AIRCRAFT O.K FOR SERVICE. 3238437 ITEM #2 PERFORMED PERMASEWDGE REPAIR TO GREEN HYD LINE UPPER LH LANDING GEAR IAW AMM 20-23-11.LEAK CHECK DUE SEE DEFECT 3238435-2.'

Part: WINDOW — DIRTY (24F) · airframe 61,004 hrs · 21,257 cycles

FLT 924, STI-BOS (DIVERTED TO FLL). POSSIBLY WINDOW 24F CRACKED; INSPECTED WINDOW AND FOUND THIN GREASE STREAK ON EXTERNAL CABIN WINDOW AT 24F. CLEANED GREASE FROM WINDOW PER AMM 56-21-13-100-002A. NO FURTHER DEFECTS NOTED. AIRCRAFT OK TO CONTINUE.

Part: A/C PACK — CONTAMINATED (NR 1) · airframe 60,376 hrs · 21,299 cycles

FLT# 1944, PBI-EWR. DIRTY SOCK ODOR AT FL360 IN HIGH ALTITUDE PRECIP - PRIMARILY IN COCKPIT - ODOR REPORT FILLED OUT ; PERFORMED PACK 1 ECS DECONTAMINATION IAW AMM 21-00-00. ODOR HAS DISSIPATED. A/C OK FOR SVC.

Part: UNKNOWN — ODOR (CABIN) · airframe 60,351 hrs · 21,290 cycles

FLT 2028, MCO-EWR. INFLIGHT DURING DESCENT SMELLED TRANSIET ODOR SMELL (DIRTY SOCKS) AND ALSO INFLIGHT CREW REPORTED SAME ODOR IN ROW 7 & 8 AREA AFTER LANDING WHEN ON APU; FOLLOWED REF INFO NOTICE 2017-TO15G LEVEL A, FOLLOWED TSM 05-50-00-810-831A. SUSPECT OVER SVC OF OIL AND FOUND RESIDUE IN THE INTAKE TO THE PLENUM.

Part: BATTERY — FAULTED (EMERGENC LIGHTS) · airframe 60,321 hrs · 21,280 cycles

FLT 1134, SJU-MCO. FWD EMERGENCY LT BATTERY FAULTING. R & R THE FWD EMERGENCY LT BATTERY PER AMM 33-51-38, OPS CHK GOOD.

Part: COMPUTER — FAILED (NR 1 ELAC) · airframe 58,422 hrs · 20,580 cycles

FLT 799, FLL-HAV. RETURNED TO FIELD. F/CTL AIL SERVO FAULT. L AIL BLUE SYSTEM BOXED AMBER ON F/CTL PAGE, REF TSM 27-93-34. R & R NR 1 ELAC, IAW AMM 27-93-34. OPERATIONS CHECKS OK.

Part: UNKNOWN — ODOR (CABIN)

I (F4) WAS PERFORMING MY SAFETY DEMO, WHEN I WAS DEMONSTRATING THE OXYGEN MASK I NOTICED A STRONG MUSTY, DIRTY SOCK LIKE SMELL AND STARTED TO FEEL SLIGHTLY DISORIENTED AND DIZZY AFTER COMPLETING THE SAFETY DEMO THE F3 TOLD ME I HAD MY HANDS UP WITH THE OXYGEN MASK AND WASN’T ALIGNED TO WHAT WAS BEING SAID IN THE SAFETY DEMO PA. I TOLD HER I WASN'T FEELING WELL AND EXPLAINED SOME OF THE SYMPTOMS I WAS HAVING. I CONTINUED FEELING DISORIENTED, DIZZY AND STARTED TO FEEL SLIGHTLY NAUSEOUS. I WAS HAVING TROUBLE UNDERSTANDING MY F3 AND GIVING HER DELAYED RESPONSES. DURING THE CLIMB IS WHEN ALL MY SYMPTOMS INTENSIFIED (DISORIENTED, DIZZY, NAUSEA) AND I ALSO BEGIN TO FEEL IRRITATION AND A BURNING SENSATION IN MY EYES, NOSE AND THROAT. I ALSO FELT VERY LIGHT AND MY ENTIRE BODY WAS TINGLY. PILOTS WERE NOTIFIED OF MY SYMPTOMS AND WE RETURNED TO THE GATE, PARAMEDICS ARRIVED. AFTER EVALUATION FROM PARAMEDICS I WAS TOLD I NEEDED TO BE TAKEN TO THE HOSPITAL. BEFORE LEAVING THE AIRCRAFT CA ASKED ME MORE DETAILS ABOUT MY SYMPTOMS AND ALSO TOLD ME THAT BOTH HIM AND THE FO SMELLED THE ODOR AND EXPERIENCED SIMILAR SYMPTOMS DURING THE DESCENT BACK TO SJU. I WAS PLACED IN AN AMBULANCE AND TAKEN TO HOSPITAL. CA, FO, F2, F3 EXPERIENCED SIMILAR SYMPTOMS AND WERE HOSPITALIZED AS WELL. WE WERE ALL TOLD BY THE DOCTOR THAT WE HAD EXPERIENCED AEROTIXITY DUE TO INHALING TOXIC FUMES FROM THE AIRCRAFT.

Part: UNKNOWN — ODOR · airframe 53,411 hrs · 18,734 cycles

FLT 2824, MEX-MCO. ON DESCENT AT APPROX 6000 TO SURFACE AT IDLE PWR. STRONG "DIRTY SOCK" SMELL OBSERVED. THROAT AND LUNG IRRITATION NOTED; COMPLIED WITH INFORMATION NOTICE 2017-T015D SECTION A. AIRCRAFT IS OK FOR SERVICE. DETERMINED TO BE LEVEL 1 CONDITION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,211 hrs · 18,317 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 FRAME 69-70 STR 23R; REMOVED AND REPLACED FLOORBEAM -Y1292 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 20209.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,211 hrs · 18,317 cycles

DURING HEAVY MAINTENANCE, 15C- EMERGENCY LIGHT ON ISLE INOP; RELAMPED EMERGENCY LIGHT AT 15C IAW AMM CH. 33-51-16. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,211 hrs · 18,317 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292 FRAME 69-70 STR LT; REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 20230.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 52,211 hrs · 18,317 cycles

DURING HEAVY MAINTENANCE, FWD CABIN FLOORBEAM Y254 FRAME 21-22 STR 23L HAD A CRACK (REF N/R 440541-20262); REF N/R 440541-20262 - REMOVED AND REPLACED FWD CABIN FLOORBEAM Y254 FRAME 21-22 STR 23L IAW SRM 51-42-11.

Part: FAN — FAILED · airframe 48,288 hrs · 16,836 cycles

FLT 182, BNA-FLL. METALLIC ODOR IN CABIN & FLIGHT DECK. NOTICED 1ST FROM PAX IN ROW 8. 1 FA USED O2 AND WAS DIZZY FROM THE EVENT DURING DESCENT; ODOR PRESENT DURING DESCENT. COMPLIED WITH INFO NOTICE 2017-T015B SECTION A. AIRCRAFT OK FOR SERVICE. DURING INSP FOUND RIGHT RECIRC FAN C/B POPPED. PLACED FAN ON MEL. SUSPECT BAD RECIRC FAN THE CAUSE OF THE ODOR EVENT. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: SLIDE — FAILED (PAX DOOR) · airframe 45,716 hrs · 15,864 cycles

RIGHT AFT DOOR SHOWS DISARMED ABOVE 8000 FT. LEVER ALSO WORKS OUT OF FLUSH DETENT. R & R THE R2 DOOR SLIDE IAW AMM 25-62-44. OPS CHECKED OKAY. OPS CHECKED THE DOOR LEVER IN ARMED AND DISARMED POSITION, FOUND GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,696 hrs · 15,858 cycles

DURING A HEAVY CHECK, LOW CAPACITY BATTERY EPSU 10WL, 11WL, 12WL, 13WL WERE DISCOVERED IN PASSENGER CABIN. R & R THE BATTERY EPSU 10WL, 11WL, 12WL, 13WL IAW AMM 33-51-38-400-001-A. TESTED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,696 hrs · 15,858 cycles

DURING A HEAVY CHECK, LOW CAPACITY BATTERY EPSU 10WL, 11WL, 12WL, 13WL WERE DISCOVERED IN PASSENGER CABIN. R & R THE BATTERY EPSU 10WL, 11WL, 12WL, 13WL IAW AMM 33-51-38-400-001-A. TESTED OK.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 45,696 hrs · 15,858 cycles

DURING HEAVY CHECK, THERE WAS A CRACK INDICATION ON THE BOX BEAM FLANGE LOCATED 1.5 INCHES FWD FROM FRAME 43. PERFORMED A REPAIR IAW EC 53-1251, EA 53-0126-17 A, AND EC A17-259-01.

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 45,696 hrs · 15,858 cycles

DURING HEAVY CHECK, THERE WAS A CRACK INDICATION FOUND IN PRESSURE PANEL ATTACHMENT HOLE ON FRAME 36 LOCATED 1.5 INCH INBD FROM BS 1292 AT 12 O`CLOCK. PERFORMED A REPAIR IAW EC 53-1263.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 45,696 hrs · 15,858 cycles

DURING HEAVY CHECK, THERE WAS A CRACK INDICATION IN THE BOX BEAM FLANGE LOCATED 1.5 INCHES FWD FROM FRAME 43. PERFORMED A REPAIR IAW EC 53-1251 AND EA 53-0126-17.

Part: COVER — CORRODED (FRAMES 52A-56) · corrosion level 2 · airframe 45,696 hrs · 15,858 cycles

DURING A HEAVY CHECK, CORROSION WAS DISCOVERED ON COVER SHEET FRAMES 52A - 56 IN AFT CARGO BAY. REWORKED & EVALUATED COVER SHEET IAW EA 53-0164-17, & EC A17-253-01. MAJOR REPAIR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,696 hrs · 15,858 cycles

DURING A HEAVY CHECK, LOW CAPACITY BATTERY EPSU 10WL, 11WL, 12WL, 13WL WERE DISCOVERED IN PASSENGER CABIN. R & R THE BATTERY EPSU 10WL, 11WL, 12WL, 13WL IAW AMM 33-51-38-400-001-A. TESTED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,696 hrs · 15,858 cycles

DURING A HEAVY CHECK, LOW CAPACITY BATTERY EPSU 10WL, 11WL, 12WL, 13WL WERE DISCOVERED IN PASSENGER CABIN. R & R THE BATTERY EPSU 10WL, 11WL, 12WL, 13WL IAW AMM 33-51-38-400-001-A. TESTED OK.

Part: DOOR SILL — CORRODED (FRAME 61-62) · corrosion level 2 · airframe 45,696 hrs · 15,858 cycles

DURING A HEAVY CHECK, CORROSION WAS DISCOVERED ON AFT CARGO DOOR SILL. REPAIRED THE AREA IAW EA 53-0130-17, REV 1 & EC A17 247-01. MAJOR REPAIR.

Part: SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 45,696 hrs · 15,858 cycles

DURING A HEAVY CHECK, CORROSION WAS DISCOVERED ON THE LOWER SUPPORT AT FRAME 66 AND STRINGER 23L AT AFT GALLEY AREA PERFORMED PERMANENT REPAIR IAW SRM 51-42-11, AND 53-41-14-300-001 PRINCIPLE 9.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 45,696 hrs · 15,858 cycles

DURING HEAVY CHECK, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT Y503.2, BETWEEN FRAMES 12 - 16 IN PAX CABIN. R & R THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53112825.

Part: PRESSURE PANEL — CRACKED (FRAME36) · airframe 45,696 hrs · 15,858 cycles

DURING HEAVY CHECK, THERE WAS A CRACK INDICATION FOUND IN PRESSURE PANEL ATTACHMENT HOLE ON FRAME 36 LOCATED 13.25 INCHES INBD FROM Y1292 AT 12 O`CLOCK. PERFORMED A REPAIR IAW EC 53-1263.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 36,153 hrs · 12,491 cycles

DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FAILED THE FUNCTIONAL TEST. R & R BATTERY PACK 13WL AND 12WL IAW AMM 33-51-38. EMERGENCY LIGHT CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 36,153 hrs · 12,491 cycles

DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FAILED THE TEST. R & R BATTERY PACK 13WL AND 12WL IAW AMM 33-51-38. EMERGENCY LIGHT CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,959 hrs · 11,459 cycles

DURING HEAVY MAINTENANCE CHECK, PERFORMED A CABIN EMERGENCY LIGHT CHECK. SEVERAL LIGHTS NOT WORKING. TROUBLESHOT AND REPLACED LAMPS INOPERATIVE EMERGENCY LIGHTS. OPS CHECKED GOOD IAW AMM 33-51-00-710-001-A.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 30,583 hrs · 10,655 cycles

DURING MX CHECK, FOUND ROW 25 SEAT EMERGENCY WHITE LIGHT INOPERATIVE. FOUND CONNECTOR PIN LOOSE FROM WIRE. CRIMPED NEW PIN IAW ESPM 20-44-00. OPS CHECKED OK.

Part: SAFETY VALVE — FAILED (BRAKE SYSTEM) · airframe 28,072 hrs · 9,859 cycles

FLT 390 MCO-LGA, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO JFK DUE TO BRAKES HOT ECAM ILLUMINATED. ON TAKEOFF AT ROTATION THE LEFT BRAKES WERE SHOWING 125C WHEN CLEARED FOR TAKEOFF AND SPIKE TO 300C INSTANTANEOUSLY ON ROTATION. BRAKE TEMPS WERE NORMAL ON LANDING ROLLOUT. REMOVED AND REPLACED SAFETY VALVE IAW MM 32-42-36. OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAILED (NR 1 ENGINE) · airframe 25,892 hrs · 9,084 cycles

FLT 1557 FLL-BOG, AIRCRAFT DIVERTED TO MCO DUE TO G ENGINE 1 PUMP ON ECAM IN CLIMB. FOUND NR 1 ENGINE PRESSURE SWITCH AT FAULT. REMOVED AND REPLACED IAW 29-32-12-04. OPS CHECK OK.

Part: BRAKE ASSY — MALFUNCTIONED (NR 2) · airframe 20,807 hrs · 7,282 cycles

FLT 462 RSW-BOS, AIR RETURN TO RSW - CREW DECLARED EMERGENCY DUE TO AFTER LIFT-OFF LEFT SIDE BRAKES OVERHEAT FROM 45 DEGS TO OVER 600 DEGS ON INDICATION IN 15 SECS. GEAR REMAINED EXTENDED. PERFORMED A/C TAXI AND ALL IND NORMAL. REMOVED AND REPLACED NR 2 BRAKE ASSY AS PER AMM 32-42-27. OPS CHECK NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,770 hrs · 6,902 cycles

FLT 1784 BOG-MCO, AIR TURNBACK TO BOG DUE TO FLT CONTROL AIL 1 AND 2 FAULT ON ECAM. FLT CONTROL ALT LAW LOST. RESET ELAC 1 C/B B11 AND A01. PERFORMED OPS TEST REF AMM 27-14-00-710-001. AILERON HYD ACTUATION NO FAULTS FOUND. MCC VERIFIED ONE TIME OCCURENCE VIA AIRMAN, NO PRIOR 30 DAY HISTORY.

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 19,038 hrs · 6,645 cycles

FLT 809 JFK-SDQ A/C DIVERTED TO MCO, AT CRUISE A MOMENTARY 10 SEC AROMA OF ELECTRICAL FUMES AND DISSIPATED RAPIDLY. CABIN CREW REPORTED AROMA AT ROW 5 AND MOVED AFT TO CABIN. TURNED OFF CABIN FANS AND FUME AROMA REPORTS STOPPED 20 MIN LATER. FOUND FAN INTERMITTENTLY EXERT LOUD RUMBLING VIBRATION AND NOTED FRICTION SMELLING. REMOVED AND REPLACED AVIONICS EXTRACTION FAN 18 HQ.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 8,133 hrs · 2,756 cycles

EMERGENCY LIGHTING A ROW 7 INOP. WIRES PULLED FROM CONNECTOR. ITEM IS (OPEN) PLACED ON MEL 33-50-03, CAT C UNDER CONTROL NUMBER L01907.