N536JB

Part: FILTER — ODOR (ZONE 100) · airframe 84,638 hrs · 30,535 cycles

FLT#321, BOS-PBI. ON DESCENT THROUGH 8,000 FT - LEVEL 1 DIRTY SOCK SMELL IN COCKPIT ONLY; COMPLIED WITH TSM 05-50-00-810-831-A, REPLACED RECIRCULATING FILTERS IAW AMM 21-21-41, COMPLIED WITH INFO NOTICED 2017-T015, ISOLATED FAULT TO TYPE 10, PER TSM 05-50-00-810-085, INPECTED APU, FOUND NO OIL LEAK, AIRCRAFT IS OK FOR SVC.

Part: UNKNOWN — ODOR (CABIN) · airframe 84,593 hrs · 30,515 cycles

FLT#1891, PVD-RSW. DIRTY SOCK ODOR IN AFT CABIN REPORTED BY INFLIGHT DESCENDING THROUGH 10,000 FT. NO ODOR OBSERVED IN COCKPIT.

Part: PRESSURE SWITCH — FAULTED (HYD SYSTEM) · airframe 81,786 hrs · 29,413 cycles

FLT#210, SDQ-JFK. (AIRCRAFT DIVERTED TO FLL). 'DURING CLIMB RECEIVED HYD B LO LEVEL CAUTION MESSAGE; INVESTIGATED AND FOUND LEAK COMING FROM THE BLUE ELECTRIC PUMP PRESSURE SWITCH (2074 GJ). REPLACED PRESSURE SWITCH AND SEAL IAW AMM 29-12-17. SERVICES HYDRAULICS IRW 12-12-29. ALL OPS CHECK OK. NO LEAKS NOTED. A/C OK TO CONTINUE SERVICE.'

Part: FRAME — CRACKED (FRM 68) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 68 FRAME WEB AFT FACE HORIZONTAL FLANGE L OWER RADII LEVEL OF STR 22R. CRACK L= 0.960 INCH; (RESOLVED ON W/O: 1259323 TASKCARD: NR-00036) REF AEROMAN WO 2023 365/1 NR 2023-768633 ACCOMPLISHED REPAIR PER EC A24-143-01, AEROMAN EA 53-0508-23 REV 0 (COVER PLUS PARTS 1 AND 2), AND AIRBUS RDAF 81333240/003/2024#A. ACCOMPLISHED BY AEROMAN TECH 8672020 RII BY QC C CHACON 217.

Part: SPIGOT — CORRODED (LT PYLON) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON LH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING ON LH PYLON IAW A320 SRM 54-51-12-283-002 AND A320 SRM 54-51-12-300-002. TOOL USED: DIGITAL CALIPER P/N: 500-197-30, S/N: A21043111, DUE DATE: JUL-20-2024.WORK ACCOMPLISHED ON AEROMAN WO2023 365/1 NRC 2023.(CONSIDERED A MAJOR REPAIR)

Part: FRAME — CRACKED (FRM 16) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 7 AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 9 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00032) REF AEROMAN WO 2023 365/1 NR 2023-768522 ACCOMPLISHED THE REPAIR OF THE DOUBLE JOGGLE AREA AT FR 16 RH IAW AEROMAN EA 53-0507-23 REV. 0 (COVER PLUS PART 1-5), AIRBUS RDAF 81334175/010/2024#A. AND EC NO. A24-144-01. THIS REPAIR IS CAT B. INSP THRESHOLD FROM REPAIR EMBODIMENT (OR INSP START POINT) IS: 78000 FC (FH NOT RELEVANT), INTERVAL AND METHOD OF INSP ARE: TBD IAW AIRBUS RDAF 81334175/010/2024#A. ACCOMPLISHED BY AEROMAN TECH 8659418 RII BY AEROMAN QC Y CALDERON 238.

Part: FRAME — CRACKED (FRM 20) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE IN OPEN FASTENER HOLE H6 AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, AT FWD GALL EY AREA (2 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00041) PERFORMED PERMANENT REPAIR LOCATED ON DOOR FRAME 20 RH AT UPPER DOUBLE JOGGLE AREA ON HOLE 6 IAW A320 SRM 53-11-12-300-012. THIS REPAIR IS CATEGORY B. INSPECTION OF REPAIR IAW SRI 53-11-12-205-008, TABLE 002 ARE: INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN AT 60000 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS UNTIL 60000 FC / FH NOT RELEVANT AT 4700 FC (FH NOT RELEVANT) INSPECTION METHOD FOR LEADER HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01 AND NTM 51-10-18. INSPECTION METHOD FOR ASSOCIATED HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01.WORK ACCOMPLISHED ON AEROMAN WO:2023 365/1 NRC: 2023-768517 FUR-A320-53-01159.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: DEBONDED OB FLAP SURFACE ON RH WING; REPAIRED OB FLAP LOWER SURFACE ON RH WING IAW EC# A24-129-01, EA# 57-0022-24 REVISION 0 AND EA# 57-0022-24 PART 1. TOOL USED: DIGITAL CALIPER: P/N 500-197-30, S/N A21043111, DUE DATE: JUL/20/2024. CALIPER PN: 600-464, SN: B1730933, DUE DATE: NOV/07/2024. EDDY CURRENT INSTRUMENT P/N: NORTEC 600D, S/N: 210138503, DUE DATE: JUL-21-2024 CALIPER: P/N: 500-197-30 S/N:A18135081 DUE DATE:JUL-21-2024. EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 200053402, DUE DATE: AUG-24-2024 CALIPER PN: 500-197-30, SN: 15120589, DUE DATE: FEB/13/2024 POWER PACK PE 1068 S/N PE 0118-94826 DUE DATE JUN 20 2024, MULTIMETER P/N FLUKE 87 S/N 58610350 DUE DATE NOV 15 2024 SCALE P/N CR5200 S/N 8343110765 DUE DATE FEB/20/2024. HOT BONDER PN:HCS9200B-AV SN:18196126 DUE DATE MAR/26/2024 SCALE PN:CR5200, SN: 8343110878 DUE DATE FEB/21/2024 WORK ACCOMPLISHED ON AEROMAN WO: 2023 365/1 NRC 2023-768622 TECH: M. CALDERON INSP RII: R. NOVALES QC 79.

Part: FRAME — CRACKED (FRM 16) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE A AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, AT FWD GALLE Y AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00033) REF AEROMAN WO 2023 365/1 NR 2023-768523 ACCOMPLISHED THE REPAIR OF THE DOUBLE JOGGLE AREA AT FR 16 RH IAW AEROMAN EA 53-0507-23 REV. 0 (COVER PLUS PART 1-5), AIRBUS RDAF 81334175/010/2024#A. AND EC NO. A24-144-01. REPAIR IS CAT B. INSP THRESHOLD FROM REPAIR EMBODIMENT (OR INSP START POINT) IS: 78000 FC (FH NOT RELEVANT), INTERVAL AND METHOD OF INSP TBD IAW AIRBUS RDAF 81334175/010/2024#A ACCOMPLISHED BY AEROMAN TECH 8659418 RII BY QC Y CALDERON 238.

Part: FRAME — CRACKED (FRM 16) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 6 AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00031) REF AEROMAN WO 2023 365/1 NR 2023-768521 ACCOMPLISHED THE REPAIR OF THE DOUBLE JOGGLE AREA AT FR 16 RH IN ACCORDANCE WITH AEROMAN EA 53-0507-23 REV. 0 (COVER PLUS PART 1-5), AIRBUS RDAF 81334175/010/2024#A. AND EC NO. A24-144-01.

Part: ATTACH FITTING — CRACKED (PRESSURE BLKHD) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STGR 30L PRESSURE BULKHEAD ATTACHMENT HOLES / CRACKS - TEMPORARY REPAIR (CONSIDERED A MAJOR REPAIR)

Part: FRAME — CRACKED (PRESSURE BLKHD) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 35 LH SIDE FWD FACE TO THE PRESSURE BULKHEAD ATTACHMENT AROUND FASTENER LOCATED 1.5 INCH BELOW STR 30L. CRACK L= 0.120 INCH; ACCOMPLISHED REPAIR OF CRACKS FOUND ON FR35 AND STR30L PRESSURE BULKHEAD ATTACHMENT HOLE IN ACCORDANCE WITH AEROMAN EA# 53-0503-23, COVER AND P1-P8 , AIRBUS RDAF#81338512/004/2024, ISSUE A AND EC# A24-177-01. REF AEROMAN W/O#2023-365/1 NR 2023-768736.

Part: SPIGOT — CORRODED (RT NACELLE) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON RH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING IAW A320 SRM 54-51-12-283-002, A320 SRM 54-51-12-300-002, AND AMM 54-51-41-400-001-A TOOL USED: CALIPER: P/N: 500-197-30 S/N: A21043111, D.D: JUL-20-2024.WORK ACCOMPLISHED ON AEROMAN WO: 2023 365/1 NR 2023-768. (CONSIDERED A MAJOR REPAIR)

Part: SHEAR TIE — CRACKED (FRM 65) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC FR65 BTW STR 43L TO STR 44 IN AFT CARGO COMPARTMENT (CPCP RELATED, REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00030) REF AEROMAN WO 2023 365/1 NR 2023-768737 REMOVED AND REPLACED SHEAR TIE AND FASTENERS LOC ON FR 65 BTW STR 43L TO STR 44 IN AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11 AND DRAWING # D53480054.

Part: DOUBLER — CRACKED (FRM 16) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / RHS FR16 DOUBLE JOGGLE AREA HOLE #6, #7, #A, AND #C / CRACKS - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)

Part: DOOR FRAME — CRACKED (FRM 16) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME AT FWD GALLEY AREA (1 EA) (FRAME 16 LH IN OPEN FASTENER HOLE C AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 3 OCLOCK); RESOLVED ON W/O: 1259323 TASKCARD: NR-00040) PERFORMED PERMANENT REPAIR LOCATED ON DOOR FRAME 16 LH AT UPPER DOUBLE JOGGLE AREA ON HOLE C IAW A320 SRM 53-11-12-300-012. THIS REPAIR IS CATEGORY B. INSPECTION OF REPAIR IAW A320 SRI 53-11-12-205-008, TABLE 001 ARE: INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN AT 60000 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS UNTIL 60000 FC / FH NOT RELEVANT AT 5900 FC (FH NOT RELEVANT) INSPECTION METHOD FOR LEADER HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01 AND NTM 51-10-18. INSPECTION METHOD FOR ASSOCIATED HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01.WORK ACCOMPLISHED ON AEROMAN WO: 2023 365/1 NRC 2023-768744 FUR-A320-53-01158.

Part: STRINGER — CORRODED (FRM 56-57 S43L) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC BTW FR 56 TO FR 57 AFT CARGO COMPARTMENT (C PCP RELATED, REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00028) REF AEROMAN WO 2023 365/1 NR 2023-768643 REMOVED AND REPLACED STRINGER 43L LOC BTW FR 54 TO FR 60 LH SIDE AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11 AND DRAWING #D53470345

Part: ATTACH FITTING — UNKNOWN (PRESSURE BLKHD) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STGR 30L PRESSURE BULKHEAD ATTACHMENT HOLES / CRACKS - PERMANENT REPAIR (TBD) (CONSIDERED A MAJOR REPAIR)

Part: CLEAT — CORRODED (FRM 31) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CORROSION CLEAT LOC. BTW STR 40R AND STR41R AT FR31 IN FWD CARGO COMPA RTMENT; REMOVED AND REPLACED CLEAT AND FASTENERS LOC ON BTW STRINGER 40R AND STRINGER 41R ON FRAME 31 IN FWD CARGO COMPARTMENT I.A.W. A320 SRM 51-42-11 AND DWG D53231375.WORK ACCOMPLISHED ON AEROMAN WO: 2023 365/1 NRC 2023-768556 TECH:O. CABALLERO 8632212 INSP: M. MELENDEZ QC320.

Part: STOP FITTING — DAMAGED (FRM 68 S22) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)

Part: CLEAT — CORRODED (FRM 30) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CORROSION CLEAT LOC. BTW STR41R AND STR42R AT FR30 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED CLEAT AND FASTENERS LOC ON FRAME 30 BETWEEN STRINGER 41R TO STRINGER 42R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DRAWING D53231586.WORK ACCOMPLISHED ON AEROMAN WO: 2023 365/1 NRC 2023-768556 TECH: O. CABALLERO 8632212 INSP: M. MELENDEZ QC320.

Part: FRAME — CRACKED (FRM 20) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE IN OPEN FASTENER HOLE A AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 9 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00042) PERFORMED PERMANENT REPAIR LOCATED ON DOOR FRAME 20 RH AT UPPER DOUBLE JOGGLE AREA ON HOLE A IAW A320 SRM 53-11-12-300-012. THIS REPAIR IS CATEGORY B. INSPECTION OF REPAIR IAW SRI 53-11-12-205-008, TABLE 002 ARE: INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT IS TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN AT 60000 FC (FH NOT RELEVANT), SUBSEQUENT INSPECTION AT INTERVALS UNTIL 60000 FC / FH NOT RELEVANT AT 5900 FC (FH NOT RELEVANT) INSPECTION METHOD FOR LEADER HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01 AND NTM 51-10-18. INSPECTION METHOD FOR ASSOCIATED HOLE IS ROTATING PROVE TEST IAW NTM 51-10-01.WORK ACCOMPLISHED ON AEROMAN WO: 2023 365/1 NRC 2023-768520 FUR-A320-53-01160.

Part: FRAME — CRACKED (FRM 16) · airframe 78,802 hrs · 28,265 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE C AT UPPER DOUBLE JOGGLE AREA, CRACK DIRECTION IS 3 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1259323 TASKCARD: NR-00034) REF AEROMAN WO 2023 365/1 NR 2023-768525 ACCOMPLISHED THE REPAIR OF THE DOUBLE JOGGLE AREA AT FR 16 RH IAW AEROMAN EA 53-0507-23 REV. 0 (COVER PLUS PART 1-5), AIRBUS RDAF 81334175/010/2024#A. AND EC NO. A24-144-01. REPAIR IS CAT B. INSP THRESHOLD FROM REPAIR EMBODIMENT (OR INSP START POINT) IS: 78000 FC (FH NOT RELEVANT), INTERVAL AND METHOD OF INSP TBD IAW AIRBUS RDAF 81334175/010/2024#A. ACCOMPLISHED BY AEROMAN TECH 8659418 RII BY QC Y CALDERON 238.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 77,798 hrs · 27,873 cycles

FLT#1464, SJD-LAX. 'DISTINCT CABIN ODOR (MOSTLY AFT GALLEY) ON DESCENT. ODOR ALSO VERY DISTINCT IN COCKPIT AFTER TAXI AFTER TRANSITIONING TO APU BLEED. NO OUTSIDE FACTORS SUCH AS SMOKE NOTICED OR SEEN. ODOR SUBSIDES WITHOUT APU BLEED. ( APU BLEED AIR SUPPLY SYSTEM ).' (SUPPLEMENTAL TO FOLLOW)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 75,651 hrs · 27,027 cycles

FLT#725, JFK-SAT. (AIRCRAFT PERFORMED AN AIR TURNBACK TO JFK) 'ENG 1 BEARING 4 OIL SYS- HI PRESSURE ECAM RECEIVED AFTER TAKEOFF; REF TSI 499867 & PERFORMED HIGH POWER ASSURANCE TEST IAW 71-00-00-710-013-C #4 BEARING OIL HIGH-PRESSURE FAULT NOT FOUND AT THIS TIME. AIRCRAFT IS OK FOR SERVICE.'

Part: ACTUATOR — FAILED (YAW DAMPER 1) · airframe 75,107 hrs · 26,814 cycles

FLT#799, FLL- HAV. AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL, AUTO FLT YAW DAMPER 1, YAW DAMPERS - SYSTEM 1. INSTALLED NEW YAW DAMPER SERVO ACTUATOR IAW AMM 27-26-51. REQUIRES OP CHECK AND LEAK CHECK. REF LOG PAGE 3586051, FOR REMOVAL AND REPLACEMENT OF YAW DAMPER SERVO ACTUATOR. REF LOG PAGE 3586051, ITEM 2 PERFORMED OP CHECK OF YAM DAMPER ACTUATOR IAW AMM 27-26-51. OP CHECK IS GOOD. NO LEAKS WERE NOTED FOR THE OP CHECK AND THE LEAK CHECK WAS GOOD.

Part: NONE — NONE · airframe 72,645 hrs · 25,900 cycles

FLT # 1796, CUN-FLL. BOTH AFT CABIN ENTRY DOOR EMERGENCY LIGHTS ILLUMINATED WITH SEATBELT SWITCH; FOUND EXIT AND EMERGENCY LIGHTS ASSY CROSS-CONNECTED LEADING TO WRONG CONFIG WITH LIGHT SWITCH. REPAIRED AND INSTALLED CORRECTLY IAW AMM 33-51-00. NORMAL CONFIG

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,072 hrs · 25,358 cycles

FT # 543, EWR-PBI. ROWS 1 AND 5 LH AISLE EMERGENCY LIGHTS INOP; R & R FWD LH EPSU AND BATTERY IAW AMM 33-51-38. ALL OPS OK.

Part: EPSU — FAILED (CABIN) · airframe 71,072 hrs · 25,358 cycles

FT # 543, EWR-PBI. ROWS 1 AND 5 LH AISLE EMERGENCY LIGHTS INOP; R & R FWD LH EPSU AND BATTERY IAW AMM 33-51-38. ALL OPS OK.

Part: GROUND WIRE — CUT (EMERGENCY LIGHTS) · airframe 70,592 hrs · 25,168 cycles

FLOOR EMERGENCY LIGHTS, FOUND A GROUND WIRE TERMINAL CUT. CRIMPED NEW TERMINAL TO GROUND WIRE IAW ESPM 20-56-22. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (ROW 1ABC) · airframe 70,513 hrs · 25,144 cycles

FT # 2830, SDQ-BOS. EMERGENCE LIGHTING 1C LOOSE; R & R ROW 1 ABC EMERGENCY LIGHT IAW AMM 33-51-19. OP CHECKS GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 69,159 hrs · 24,626 cycles

FT # 272, EMERGENCY FLOOR LIGHTING ROW 1 C LENS MISSING, HOUSING DETACHED FROM BASE. INSTALLED NEW CLEAR EMERGENCY LIGHT LENS IAW 36-50-00. OPS CHECKED OK.

Part: LENS — UNSECURE (CABIN) · airframe 64,327 hrs · 22,820 cycles

FLT 566, FLL-ORD. FLOOR PATH LIGHTING ON SEAT 1 C IS HANGING DOWN. REPLACED ISLE EMERGENCY LIGHTING LENS AT 1C AS REQUIRED. PERFORMED OPS CHECK OF EMERG LIGHTING SYS REF AMM 33-51-00. OK FOR SERVICE. (FILED BY EMAIL ON 5/14/2018).

Part: FLOORBEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 62,820 hrs · 22,231 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM - Y1292 AT LEVEL FR 20 IN PASSENGER CABIN; REPLACED FLOOR BEAM -1292 AT LEVEL FR 12 TO FR 24 IN PASSENGER CABIN IAW A320 51-72-11 AND DRAWING D 531 12812 AND D531-10900.

Part: FLOORBEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 62,820 hrs · 22,231 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y765 AT LEVEL FR 20 IN PASSENGER CABIN; REPLACED FLOOR BEAM -Y765 AT LEVEL FR 12 TO FR 24 IN PASSENGER CABIN IAW SRM A320 51-72-11 AND DRAWING B 531 12812 AND D 531 - 10900.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 61,744 hrs · 21,804 cycles

EPSU 12WL FAILED TEST. R & R THE EPSU BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 61,744 hrs · 21,804 cycles

EPSU 10WL FAILED TEST; R & R THE EPSU BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 61,744 hrs · 21,804 cycles

EPSU 10WL, 13WL FAILED TO TEST. R & R THE EPSU BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: BATTERY — FAILED (POWER SUPPLY) · airframe 61,744 hrs · 21,804 cycles

EPSU FAILED TEST. R & R THE EPSU BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: RECEIVER — FAILED (NR 2) · airframe 60,841 hrs · 21,475 cycles

NAV LS TUNING DISAGREE IN FLIGHT ( ILS NAVIGATION SYSTEMS ) DIVERTED. R & R THE MMR NR 2 IAW AMM 34-36-31. OPS CHECKED OK.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 57,192 hrs · 20,161 cycles

DURING A MAINTENANCE CHECK, CORROSION WAS FOUND ON MAIN CABIN FLOORBEAM AT Y1292 FRAME 68. REMOVED AND REPLACED THE FLOORBEAM.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 57,192 hrs · 20,161 cycles

DURING A MAINTENANCE CHECK, CORROSION WAS FOUND ON AFT WET AREA LONGITUDINAL FLOOR SUPPORT AT FRAME 66 Y 512. REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOORBEAM — CORRODED (FRAME 67) · corrosion level 2 · airframe 57,192 hrs · 20,161 cycles

DURING A MAINTENANCE CHECK, CORROSION WAS FOUND ON MAIN CABIN FLOORBEAM Y1292 FRAME 67 + 12. REMOVED AND REPLACED THE FLOORBEAM.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 57,192 hrs · 20,161 cycles

DURING A MAINTENANCE CHECK, CORROSION WAS FOUND ON AFT WET AREA R2 PAX DOOR SILL AT FRAME 68 STR 23RT. REPAIRED AFT WET AREA R2 DOOR PAX DOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 57,192 hrs · 20,161 cycles

DURING A MAINTENANCE CHECK, CORROSION WAS FOUND ON AFT WET AREA FLOOR SUPPORT Y765 AT FRAME 68. REMOVED AND REPLACED THE FLOOR SUPPORT.

Part: AVIONICS UNIT — BROKEN · airframe 54,396 hrs · 19,211 cycles

RETURNED TO DEPARTURE; UNABLE TO EXECUTE DIRECT TO FUNCTION ON EITHER MCDU. UNABLE TO GET MAP ON F/O'S SIDE. SWAPPED 2 AND 3 ADIRU'S NORMAL CONDITION NOTED. SEE MDDR 265912 FOR S/N SWAP. ADVISED MCC.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,995 hrs · 17,698 cycles

DURING MAINTENANCE, FOUND EPSU AT 12WL BATTERY INOPERATIVE. R & R EPSU BATTERY AT 12WL IAW 33-51-38. OPS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYSTEM) · airframe 41,099 hrs · 14,563 cycles

FLT 462 RSW-BOS, BRAKES SYSTEM 2 FAULT ON ECAM DISPLAYED IN FLIGHT AFTER ONE HOUR. PER TSM 32-42-00-810-913A, RESET BSCU C/B AND FAULT CLEARED.

Part: THERMOSTAT — FAILED (BLEED AIR SYS) · airframe 40,773 hrs · 14,453 cycles

FLT 717 JFK-SJU, AT FL 370 WITH PACK 2 MEL OFF, BLEED 1 OVERHEAT RESULTING IN LOSS OF PRESSURIZATION. EMERGENCY DESCENT TO 10000 FEET BLEED 1 MAX TEMP 265, MAX CABIN ALTITUDE 12000FT SAFETY VALVE OPENED. REMOVED AND REPLACED THERMOSTAT FAN AIR VALVE CONTROL (7170HM1) IAW 36-11-43 ALL NORMAL.

Part: VALVE — FAILED (BLEED AIR SYS) · airframe 40,773 hrs · 14,453 cycles

FLT 717 JFK-SJU, AT FL 370 WITH PACK 2 MEL OFF, BLEED 1 OVERHEAT RESULTING IN LOSS OF PRESSURIZATION. EMERGENCY DESCENT TO 10000 FEET BLEED 1 MAX TEMP 265, MAX CABIN ALTITUDE 12000FT SAFETY VALVE OPENED. REMOVED AND REPLACED FAN AIR VALVE (9HA1) IAW 36-11-54. ALL NORMAL.

Part: FLEX LINE — RUPTURED (LT MLG) · airframe 37,521 hrs · 13,335 cycles

FLT 369 LGA-PBI, AFTER LANDING, HYD G RSVR LO LVL, A/C TOW TO GATE. REMOVED AND REPLACED FLEX LINE TO THE BRAKE SELECTOR VALVE LT MLG AND ALL OPS CHECK GOOD PER AMM 32-42-77.

Part: LINE — MISINSTALLED (LAVATORY) · airframe 33,837 hrs · 11,998 cycles

FLT 41 JFK-MCO, PUTRID ODOR COMING FROM AIR VENT AT CABIN ROWS 15 AND AFT, STRONGEST ODOR FROM AFT GALLEY GASPER AIR VENT. FOUND AT LAV 'D', THE AIR OUTLET SUPPLY LINE AND THE WASTE WATER DRAIN LINES TO BE INSTALLED BACKWARDS, INSTALLED CORRECTLY AND DRAINED RESIDUAL WATER FROM DUCTING AS REQUIRED. OPS CHECK OK.

Part: PROBE — FAILED (PITOT/STATIC SYS) · airframe 29,710 hrs · 10,523 cycles

FLT 378 - FLL-LGA - DIVERTED TO TPA, LOST CAPTAINS INSTRUMENTS, DATA, AUTO THRUST, ALTITUDE. F/O LOST ALTITUDE IN FLT. ACCOMPLISHED TSM 34-13-00-810-998-A. FUNCTIONAL TEST OF THE ALTITUDE AND AIRSPEED DATA SHOWED COMPARISON OF CAPT AND F/P DATA THE SAME, LEAK CHECK OF THE MAIN AIR DATA SYSTEM WITHIN LIMITS. REPLACED PITOT TUBE 9DA1 IAW AMM 34-11-15 AND ADM 19FP5 AND ADM FP4 IAW AMM 34-11-17-04 PER TSM 34-13-00-810-938, ALL TESTED GOOD. OK FOR SERVICE.

Part: PROBE — FAILED (NR 1) · airframe 29,646 hrs · 10,496 cycles

FLT 715, JFK-SJU, CAPTAIN SIDE PFC LOSES ALL AIRSPEED INFOR AND ALT DIFFERENCES OF 500 FT BETWEEN CAPT AND F/O'S NAV ALT. DISCREPANCY ON ECAM ON DESCENT CAPT AIRSPEED AT 0 IN CRUISE FROM 0 TO 302 FLT LEVEL 29000 FT. TSI ISSUED DUE NUMEROUS WRITE UP, REMOVED AND REPLACED ADIRU NR 1 IAW AMM 34-12-34, OPS CHECKS OK. REMOVED AND REPLACED SEC NR 1 IAW AMM 27-94-3404, OPS CHECKS GOOD. FINAL FIX, REMOVED AND REPLACED PHC-PROBE HEAT COMPUTER NR 1 (6DA1) REF 30-31-34, OPS CHECK GOOD.

Part: PROXIMITY SENSOR — INTERMITTENT (LANDING GEAR) · airframe 27,821 hrs · 9,827 cycles

FLT 5036, RME-RME, AIR RETURN, GEAR WOULD NOT RETRACT AFTER TAKEOFF, RECYCLED GEAR, GEAR RETRACTED, ASSOCIATED FAULTS INCLUDED. POST FLIGHT REPORT SHOWS PROX SENSOR 23GA FAULT. REMOVED AND REPLACED 23GA SENSOR IAW A320 AMM 32-31-73. PERFORMED NORMAL GEAR EXTENSION AND RETRACTION IAW A320 AMM 32-31-00-720-002. GEAR PERFORMED SATISFACTORY IAW A320 3231-00. NO FAULTS OR GEAR SYSTEM DISAGREE NOTED. SWUNG ALL 3 GEARS (18) COMPLETE CYCLES NO FAULTS, NO DISAGREE FAULTS NOTED. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 19,017 hrs · 6,779 cycles

ON FINAL APPROACH, L/G WAS EXTENDED ECAM -LGCIU1 FAULT- ILLUMINATED. DECIDED TO GO AROUND AND ATTEMPTED TO RESOLVE ISSUE. RETRACTED L/G LGCIU FAULT AND LGCIU 2 FAULT ILLUMINATED. APPLIED ECAM ACTION OF GPNS, OFF AND MANUAL GEAR EXTENSION. LANDING AND TAXI WAS MADE W/O FURTHER INCIDENT. PERFORMED TSM 32-31-00-810-807- LGCIU 1 FAULT 40GA L/G SEL VALVE. REMOVED AND REPLACED 40 GA IAW AMM 32-31-12-04. REMOVED AND REPLACED LGCIU 1 & 2 AS PRECAUTIONARY MEASURE PERFORMED BITE TEST OF BOTH LGCIU'S IAW 32-69-00. TEST OK. PERFORMED (2) ADDITIONAL RETRACTS OF L/G SYS, NO FAULTS NOTED. TSIN 536T07165 ACCOMPLISHED IAW TSM 32-31-00-810-802. OPS NORMAL. A/C OK FOR SERVICE.

Part: ELECTRICAL BOX — MALFUNCTIONED (LT ENGINE) · airframe 15,285 hrs · 5,444 cycles

EGT IND FLUCTUATED BETWEEN 190-490 DEGREES AFTER TAKEOFF, WENT AS LOW AS 75 DEGREES DURING RETURN. T/S IAW AMM 77-21-43-05. REPLACED JUNCTION BOX IAW 77-21-43-04. OPERATED LEFT ENG AT VARIOUS POWER SETTINGS, ALL EGT PARAMETERS NORMAL. OK FOR SERVICE.

Part: PITOT TUBE — BLOCKED (F/O) · airframe 14,568 hrs · 5,221 cycles

AIRSPEED INDICATION ON F/O SIDE QUIT WORKING AT 90 KTS APPROX AIR RETURN TO JFK. REMOVED AND REPLACED F/O'S ADM IAW 34-11-17. ALL OPS CHECK GOOD. LEAK CHECK OF F/O'S PITOT FOUND OK. REMOVED AND REPLACED F/O'S PITOT PROBE IAW AMM 34-11-15. ALL OPS CHECK GOOD. PITOT LEAK CHECK OK. REMOVED AND REPLACED PRECAUTIONARY NR 2 ADR IAW AMM 37-12-34. ALL OPS CHECK GOOD.

Part: SUPPORT BRACKET — DAMAGED (NLG) · airframe 14,228 hrs · 5,099 cycles

AFTER TAKEOFF, THE NOSE LANDING GEAR (NLG) DID NOT RETRACT AND WHEELS WERE OFFSET AT A 90 DEGREE ANGLE. THE AIRCRAFT WAS DIVERTED, WHERE IT LANDED WITH THE NLG AT ABNORMAL STEERING ANGLE. PRILIMINARY BORESCOPE INSPECTION FINDINGS INDICATE NLG UPPER SUPPORT ASSY (P/N D59831) TANGS HAVE FAILED.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG) · airframe 14,219 hrs · 5,096 cycles

ON TAKE OFF, AT APPROXIMATELY 1500, AGL GOT ECAM. F/O PERFORMED ECAM ACTION, SHOCK ABSORBER FAULT, THAT CLEARED AND THEN GOT ECAM GEAR NOT LOCKED IN UP POSITION. PERFORMED THAT ECAM WHICH CLEARED ALL PROBLEM WITH NO STATUS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FLOWN BACK UNDER MEL 32-31-00. T/S 24GA AT FAULT. REPLACED 24GA PROXIMITY SENSOR IAW AMM 32-31-73-04 AND BITE CK OK.

Part: ELECTRICAL BOX — ODOR (CABIN) · airframe 13,457 hrs · 4,862 cycles

BURNING ODOR FROM OVERHEAD AT A/C RIGHT ROW 19 RUBBER TYPE OF SMELL. ACCOMPLISHED INFO NOTICE 2004-T023TR. NO ABNORMALITIES FOUND. REPLACED SEB AT SUSPECT ROW 19DEF PER INFO NOTICE IAW 23-39-00. LIVE TV SYSTEM OPERATION CHECKED NORMAL.

Part: FAN — FAILED (E/E BAY) · airframe 8,144 hrs · 3,025 cycles

IN CRUISE AT FL 350 A GRINDING NOISE WAS COMING FROM UNDER FORWARD LAV FOLLOWED BY A BURNING ODOR SHORTLY THEREAFTER ECAM VENT EXTRACT FAULT ILLUMINATED. BOTH THE SOUND AND ODOR WENT AWAY. CONTINUED TO OAK NO OTHER PROBLEM NOTED. ITEM WAS CONTINUED UNDER MEL 21-26-02. LATER AT LGB REMOVED AND REPLACED EXTRACT FAN PER 21-26-51. AEVC TEST CHECKS GOOD PER 21-26-51.

Part: APPU — OUT OF ADJUST (TE FLAPS) · airframe 7,683 hrs · 2,837 cycles

ON APPROACH FLIGHT CONTROL LOCKED - ALIGNMENT PROBLEM - SLATS 2 & FLAPS < 1. PERFORMED FLAP RIGGING IAW MM 27-54-00-501 AND ADJUSTED RT ASYMMENTRY POSITION PICKOFF UNIT (APPU )IAW MM 27-51-18-401. PERFORMED OPERATIONAL CHECK, CHECKS NORMAL.

Part: COMPUTER — MALFUNCTIONED (SLATS) · airframe 7,681 hrs · 2,837 cycles

FLAPS LOCKED WITH ALIGNMENT FAULT BETWEEN 0 & 1; SLATS NORMAL EXTENSION. RESET BOTH SFCC'S AND PERFORMED TSM TASK 27-51-00810-818 PAR 4. A. (5), NO FAULTS NOTED. AIRCRAFT IS SATISFACTORY FOR SERVICE.