N656JB

Part: UNKNOWN — ODOR (CABIN) · airframe 68,873 hrs · 24,857 cycles

FLT#833, MCO-SJU. "MOMENTARY CABIN ODOR DETECTED IN ROW 15; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A. ISOLATED FAULT TO TYPE 10 AMBIENT AIR ODOR PER TSM 05-50-810-085-B/TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR SVC."

Part: A/C PACK — ODOR (NR 1) · airframe 68,295 hrs · 24,633 cycles

FLT# 696, ATL-BOS. PACK 1 FUME EVENT ON TAKE OFF PACK 1 SECURED IAW FCOM CH 7, OPEN

Part: UNKNOWN — ODOR (CABIN) · airframe 68,074 hrs · 24,549 cycles

FLT#1793, JFK-SJO. AT TOP OF DESCENT FA REPORTED TFRANSENT SMELL OF GAS. SMELL CONFIRMED BY OTHER FA. SMEI CAME AND WENT. SMELL ISOLATED TO FWD GALLEY, APU WAS OFF. PACKS 1 & 2 ON HAD BEEN INFLIGHT FOR 4 HOURS. ACCOMPLISHED INFO NOTICE 2017-7015 OPERATED BY CREW DECONTAMINATION COMPLETED NO FURTHER ACTION AT THIS TIME INSPECTED ENGINES AND APU NO OIL ACCUMULATION SEEN.

Part: ACTUATOR — FAILED (NR 2 ENGINE) · airframe 66,015 hrs · 23,758 cycles

FLT#8523, EWR-RDU. (AIRCRAFT DIVERTED TO JFK) 'DURING CLIMB OUT ENG 2 COMPRESSOR VANE ECAM MSG FOLLOWED BY ENG 2 STALL. BANG/THUD HEARD DURING STALL. ENGINE 2 RECOVERED BEFORE ECAM ACTIONS STARTED; REMOVED AND REPLACED #2 ENG LOW PRESS COMPRESSOR BLEED MASTER ACTUATOR IAW AMM 75-31-42 OPS CHECK GOOD NO DEFECTS NOTED ON HIGH POWER.'

Part: LIGHT — INOPERATIVE (RT EXIT OVEWING) · airframe 65,637 hrs · 23,621 cycles

FLT#395, HPN-MCO. 'DURING DESCENT AT 26,000 TO LANDING, STRONG ODOR FROM AFT GALLEY (STRONGEST) TO THE FORWARD CABIN (LITEST) ORDER. SOLVENT/ CLEANING SMELL, NOT DIRTY SOCK OF ENG EXHAUST SMELL; COMPLIED WITH INFORMATION NOTICE 217-T015, SECTION A, ISOLATED FAULT TO TYPE 10, (AFT LAV WASTE BIN AND CHLORINE ODOR STATED BY FLIGHT CREW) EMPTIED LAV WASTE BIN. PER TSM 05-50-00-810-085-B / 05-50-810-085-D. AIRCRAFT IS OK FOR SERVICE.'

Part: UNKNOWN — ODOR (CABIN) · airframe 65,452 hrs · 23,553 cycles

FLT#1902, FLL-JFK. 'ODOR MILD IN CLIMB, STRONG PERSISTENT ODOR IN DECENT STARTING AT 11,000 MX-270 COMPLETE; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. IDENTIFIED ODOR AS TYPE 1 LEVEL B, DECONTAMINATION LEVEL 2 WAS AACCOMPLISHED PER TSM 05-50-00-810-831-A, AIRCRAFT IS OK FOR SERVICE.'

Part: UNKNOWN — ODOR (COCKPIT) · airframe 65,383 hrs · 23,522 cycles

FLT#379, DCA-FLL. 'FUMES IN COCKPIT ON DESCENT THROUGH 10,000' FUMES IN CABIN ALSO.' (SUPPLEMENTAL INFORMTION TO FOLLOW)

Part: DOOR FRAME — CRACKED (FRM 16) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16RH DOOR STOP FITTING 7 LOWER INBOARD HOLE, CRACK DIRECTION 6 OCLOCK AND CRACK DEPTH 0.179 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00015) REF AE W/O# 2024-49/1. N/R# 2024-218389. REMOVED AND REPLACED DOOR STOP FITTING #7 AND FASTENERS LOCATED ON FRAME 16 RH SIDE IAW A320 SRM 51-42-11 AND DWG R5311 3118.

Part: CROSSBEAM — CRACKED (FRM 16) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON OPEN HOLE H1 LOC ON CROSSBEAM FR16LH. CRACK DIRECT ION 12 OCLOCK AND DEPTH =0.100 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00018) REF AE W/O# 2024-49/1. N/R# 2024-218446. PERMANENT REPAIR ON CROSSBEAM FR16 LH IAW A320 SRM 51-42-11 AND DWG R53112926, FLOWCHART 2.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CRACKS INDICATION FOUND ON FWD AND AFT FRAME SEGMENT (1 OF THE EEH 844 CRACK LENGTH 0.270 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00020) REF AE W/O# 2024-49/1. N/R# 2024-218387. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 844 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 51-42-11, A320 SRM 51-72-11. ACCOMPLISHED BY AE TECH# 8632015. AE QC INSP# 420.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CRACKS INDICATION FOUND ON FWD AND AFT FRAME SEGMENT (1) OF THE EEH 843 CRACK LENGTH 0.315 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00021) REF AE W/O# 2024-49/1. N/R# 2024-218386. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 843 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 51-42-11, A320 SRM 51-72-11.

Part: FRAME — CRACKED (FRM 16) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (CRACK INDICATION FOUND ON FRAME 16LH DOOR STOP FITTING 7 UPPER INBOARD HOLE, CRACK DIRECTION 1 OCLOCK AND CRACK DEPTH 0.152 INCH ); (RESOLVED ON W/O: 1301529 TASKCARD: NR-00017) REF AE W/O# 2024-49/1. N/R# 2024-218392. REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOCATED FR16 LH DOOR STOP FITTING 7 IAW A320 SRM 51-42-11 AND DRAWING D53112300.

Part: SUPPORT — CORRODED (FRM 66) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. FR66 UPPER SURFACE OUTBOARD FLANGE L/H SIDE AT AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1301529 TASKCARD: NR-00032) REF AE W/O# 2024-49/1. N/R# 2024 - 218667 PERFORMED REPAIR ON LOWER SILL LOC. FR66 UPPER SURFACE OUTBOARD FLANGE L/H SIDE AT AFT GALLEY AREA I.A.W. A320 SRM 53-41-14-300-001, THIS REPAIR IS CATEGORY A. AND NO FURTHER ACTION IS REQUIRED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CRACKS INDICATION FOUND ON AFT FRAME SEGMENT (1) OF THE EEH 833 CRACK LENGTH 0.350 INCH;(RESOLVED ON W/O: 1301529 TASKCARD: NR-00019) REF AE W/O# 2024-49/1. N/R# 2024-218388. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 833 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 51-42-11, A320 SRM 51-72-11

Part: FRAME — CRACKED (FRM 20) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 20RH DOOR STOP FITTING 7 LOWER INBOARD HOLE, CRACK DIRECTION 8 OCLOCK AND CRACK DEPTH 0.055 INCH; (RESOLVED ON W/O: 1301529 TASKCARD: NR-00016) REMOVED AND REPLACED DOOR STOP FITTING # 7 AND FASTENERS LOCATED ON FRAME 20 RH SIDE IAW A320 SRM 51-42-11 AND DWG R53113118. REF AE W/O# 2024-49/1. N/R# 2024-218390. ACCOMPLISHED BY AE TECH# 8622018, AE QC # 135.

Part: WEB — CORRODED (FRMS 69-70 S23L) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOC. BTW FR69 TO FR70 AT LEVEL STR23L AT AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1301529 TASKCARD: NR-00011) REMOVED AND REPLACED WEB LOC. BTW FR69 TO FR70 AT LEVEL STR23L AT AFT GALLEY AREA IAW A320 SRM 51-42-11, ARM A320 51-72-11 AND DWG D53474180. ACCOMPLISHED BY AE TECH # 8619723. AE QC# 230. REF AE WO# 2024-49/1. N/R# 2024-218558.

Part: DOOR — CORRODED (APU BAY) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CORROSION ON APU ACCESS DOOR 315AL FWD LOWER CORNER IN APU COMPARTMENT; ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON OUTER SKIN OF THE LH APU ACCESS DOOR 315AL IAW AEROMAN EA 52-0111-24 AND JETBLUE EC A24-583-01 REF AEROMAN WO# 2024 49/1 NR# 2024-218458 FOR ALL WORK ACCOMPLISHED.

Part: SUPPORT — CORRODED (FRM 66) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. FR66 UPPER SURFACE INBOARD FLANGE L/H SIDE A T AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1301529 TASKCARD: NR-00033) REF AE W/O# 2024-49/1. N/R# 2024 - 218668. PERFORMED REPAIR ON LOWER SILL LOCATED FR66 UPPER SURFACE INBOARD FLANGE L/H SIDE AT AFT GALLEY AREA I.A.W. A320 SRM 53-41-14-300-001.THIS REPAIR IS CATEGORY A. AND NO FURTHER ACTION IS REQUIRED.

Part: WEB — CORRODED (FRMS 69-70) · airframe 64,077 hrs · 23,011 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL STRUCTURE WEB LOC. BTW FR69 TO FR70 AT LEVEL STR 23 R AT AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1301529 TASKCARD: NR-00012) REF AE W/O# 2024-49/1. N/R # 2024-218550.REMOVED AND REPLACED WEB AND FASTENER LOCATED BETWEEN FR69 TO FR70 AT LEVEL STR 23R AT AFT GALLEY AREA IAW A320 SRM 51-42-11, SRM 51-72-11 AND DWG D53474180.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,066 hrs · 23,008 cycles

FLT#766, GCM-JFK. 'EMERGENCY LIGHTS ARE ON IN THE ARMED PSN. RESET UNSUCCESSFUL; REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW ESPM 20-45-51. OPS CHECK GOOD IAW AMM 33-51-00. OPS CHECK GOOD FOR CONT SVC.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 61,163 hrs · 21,886 cycles

FLT#65, JFK-ABQ. 'CABIN EMER LIGHTS CYCLING ON/OF WHEN PLACED TO ARM; PERFORMED CID DIR TEST IAW 33-51-38, FOUND OK FOR FLT SERVICE.'

Part: VALVE — FAILED (2502GM) · airframe 60,682 hrs · 21,705 cycles

FLT # 2202, FLL-JFK. (EMERGENCY DECLARED). BRAKES AUTO BRAKE FAULT; FOLLOWING TSM 32-42-00-810-808-A T/S DATA GIVES FAULT CODE 52 AND MX MSG "BRK NORM SERVOVLV4 (18GG)" R/R SERVOVALVE 18GG IAW AMM 32-41-48. OPS CHECK & LEAK CHECK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 60,325 hrs · 21,564 cycles

FLT#1112, CUR-JFK. 'EMER EXIT LTS INTERMITTENT ON & OFF WHILE ARMED; PERFORMED EMR LIGHTING SYS OPS TEST AND BITE TEST REF AMM 33-51-38. TEST OK. NO FAULTS. ALSO PERFORMED CIDS 1 TEST REF AMM 23-73-34. TEST OK NO FAULTS.'

Part: HYDRAULIC SYSTEM — OVERSERVICED (BLUE) · airframe 55,921 hrs · 19,899 cycles

FLT 610, DFW-JFK. AT 16000' JUST SOUTH OF LENDY INTERSECTION A HYD B RSRV LO AIR PR ECAM MESSAGE/ SECURED PER QRH SYSTEM PRESSURE RESTORED AT LOWER ALTITUDE.; FOUND BLUE HYD. SYS OVER SERVICED PER TSM 29-12-00-810-801-A. R/R AIR PRESSURE SWITCH IAW AMM 29-34-11-000-002-A. NO LEAKS OF HYDRAULIC CONNECTIONS. ADJUSTED BLUE HYD. FLUID TO CORRECT LEVEL. OPS CHK GOOD. A/C OK TO CONT SVC.

Part: SKIN — DENTED (LT WING SLAT) · airframe 53,957 hrs · 19,198 cycles

DURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE, SRM REPAIR SURVEY L/H WING SLAT 1 DENT LEADING EDGE; (REF AEROMAN N/R 2021-115157) PERFORMED REPLACEMENT OF EXISTING EXTERNAL REPAIR ON LH #1 SLAT AT LEVEL OF TRACK #3. THIS REPAIR IS CLASSIFIED MAJOR CAT A , NO FURTHER ACTION REQUIRED IAW EA 57-0091-21, PART 1 & PART 2, AIRBUS RDAF 80891947/003/2021 ISSUE A, EC A21-287-01

Part: FLAP TRACK — CRACKED (LT WING) · airframe 53,957 hrs · 19,198 cycles

DURING HEAVY MAINTENANCE, CRACK O/B FLAP LEADING EDGE AREA BTW FLAP TRACK 3 AND FLAP TRACK 4 ON L/H WING; (REF AEROMAN N/R 2021-115357) PERFORMED PERMANENT REPAIR ON O/B FLAP LEADING EDGE L/H WING IAW SRM A320-57-30-00-300-029 FIG 001(SHEET 5 AND 6) PROCEDURE C , PAR D. THIS REPAIR IS CATEGORY A AND NO FURTHER INSPECTION REQUIRED.

Part: SLIDE — FAILED (PAX DOOR) · airframe 53,957 hrs · 19,198 cycles

DURING HEAVY MAINTENANCE, DURING OPERATIONAL OF THE SLIDE RAFT THE SLIDE RAFT TOUCH THE FUSELAGE ON DOOR 841 AS PER AMM 25-62-44-400-803-A; (REF AEROMAN N/R 2021-115295) R & R ESCAPE SLIDE RAFT CREW DOOR 841 IAW AMM 25-62-44-000-804-A AND 25-62-44-400-803-A, PERFORMED OPERATIONAL TEST, TEST IS OK.

Part: SLIDE — FAILED (PAX DOOR) · airframe 53,957 hrs · 19,198 cycles

DURING HEAVY MAINTENANCE, DURING OPERATIONAL OF THE SLIDE RAFT, THE SLIDE RAFT TOUCH THE FUSELAGE ON DOOR 831 AS PER AMM 25-62-44-400-007-A PROCEDURE 4.B.12(B); (REF AEROMAN N/R 2021-115293) R & R ESCAPE SLIDE RAFT AT PASSENGER CREW DOOR 831 IAW AMM 25-62-44-000-012-A AND 25-62-44-400-007-A, PERFORMED OPERATIONAL TEST, TEST IS OK.

Part: SEAL — LEAKING (DE OILER) · airframe 52,730 hrs · 18,749 cycles

FLT 206, BNA-BOS. LEVEL 1 ODOR EVENT SEE CABIN ODOR FOR DETAILS; TROUBLE SHOT PER TSM 71-00-00-810-801-A, FOUND DE-OILER CARBON SEAL LEAKING. R & R DE-OILER CARBON SEAL REF AMM 72-61-49. LEAK CHECK GOOD. COULD NOT SMELL ANYTHING IN COCKPIT OR CABIN. A/C OK FOR SERVI.CE.COMPLIED WITH INFO NOTICE 21017-T036R

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 51,783 hrs · 18,355 cycles

FT # 6480, SAL-MCO. AFT L/H EPSU UNIT FAULT; R & R EPSU AFT L/H GALLEY AS PER AMM 33-51-38 UNIT TESTED OK BUT FAILED FULL TEST REF LP 2785107 ITEM #2 FOR FULL OPS CK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 50,809 hrs · 18,003 cycles

FT # 391, BOS-TPA. EPSU BATT 11WL REQUIRES REPLACEMENT; R & R EPSU BATT 11WL IAW AMM 33-51-38. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 48,940 hrs · 17,319 cycles

FLT 1417, AUS-LGB. STRONG BURNING RUBBER ODOR IN CENTRAL CABIN ON CLIMB OUT. DISSIPATED IN 3-4 MINUTES; ODOR IS DETERMINED TO BE A LEVEL 1 CONDITION. COMPLIED WITH INFO NOTICE 2017-T015D SECTION A. AIRCRAFT IS OK FOR SERVICE.

Part: LENS — MISSING (CABIN) · airframe 48,918 hrs · 17,305 cycles

FLT 679, LAS-LGB. DURING PREFLIGHT NR 1 FA NOTICED EMER EXIT LIGHT ON FWD BULKHEAD PORT SIDE MISSING COVER; INSTALLED NEW COVER LENS ON FWD BULKHEAD ROW 1 AS REQUIRED.

Part: SLIDE — NO TEST (L2 DOOR) · airframe 48,665 hrs · 17,213 cycles

FT # 391. L2 DOOR SLIDE FAIL EMERGENCY LIGHT TEST; R & R AFT L/H L2 DOOR SLIDE IAW AMM 25-62-44-400-007. TEST GOOD.

Part: REGULATOR VALVE — FAILED (CABIN HEAT) · airframe 48,050 hrs · 17,005 cycles

FT # 1158, RETURNED TO FIELD. EXCESSIVE CABIN HEAT WHILE AT ALTITUDE FWD = 116 AFT = 106; REMOVED PACK 2 PANEL. CHECKS FLOW CONTROL VALVE SENSE LINES & CONNECTORS. NO ISSUES NOTED. PANEL REINSTALLED. HOT AIR PRESSURE REGULATING VALVE REMOVED AND REPLACED. SEE LOG 2409959 ITEM 2 MDDR 378643.

Part: LIGHT — BROKEN (SEAT 1C) · airframe 46,946 hrs · 16,592 cycles

FT #319, FLL-SLC. SEAT 1C EMERGENCY EXIT LIGHT BROKEN ( FLOOR PROX EMERG ESCAPE PATH MARK SYS - INCANDESCENT LIGHTING SYS - NOT APPLICABLE TO (N703 AND UP) ); REPLACED EMERGENCY LIGHT HOUSING AT SEAT 2C, PER AMM 33-51-19. OPS CHECK OK. MX4 UPDATED, PLACARD REMOVED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 45,408 hrs · 15,988 cycles

EXIT ROW EMERGENCY LIGHT AT 1C, LENS DETACHED. SECURED THE LENS IAW AMM 33-51-19.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y 1242 ON FR18 AT FWD GALLEY AREA; REPLACED FLOORBEAM -Y1292 ON FR12 TO FR24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DRAWING D53112812 TOOL USED CALIPER PNT 500-172-30 S/N 14519392 DUE DATE MAY -23-2108 REF NRC 2018-143188.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED REF BP NON ROUTINE 2018- 143189 FLOORBEAM -Y254 ON FR18 AT FWD GALLEY AREA. REPLACED FLOORBEAM -Y254 0N FR 12 TO FR 24 IAW SRM 51-72-11 AND DRAWING D53111013.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. LOWER SILL PASSENGER DOOR 842 AT AFT GALLEY. REPLACED LOWER SILL PAX DOOR 842 PER SRM 51-72-11 AND DRAWING D53480505.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. LOWER SILL PASSENGER DOOR 842 AT AFT GALLEY. REPLACED LOWER SILL PAX DOOR 842 PER SRM 51-72-11 AND DRAWING D53480505.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NR 2018-143272. LOWER SILL PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REMOVED AND REPLACED LOWER SILL PASSENGER CREW DOOR 832 AT AFT GALLEY AREA LT SIDE IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. LOWER SILL PASSENGER DOOR 842 AT AFT GALLEY. REPLACED LOWER SILL PAX DOOR 842 AFT GALLEY AREA PER SRM 51-72-11 AND DRAWING D53480505.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NR 2018-143191 FLOORBEAM +Y254 FWD GALLEY AREA; REF BP NR 2018-143191 REPLACED FLOORBEAM +Y254 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DRAWING D53111013 TOOL USED CALIPER P/N 500-172-30 S/N 14519392 DUE DATE MAY 23 2018

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NR 2018- 143179 FLOORBEAM +Y765 BTW FR 66 AND FR 67 AT AFT GALLEY AREA; REF BP NR 2018-143179 REPLACED FLOORBEAM +Y765 BTW FR 66 AND FR 67 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DRAWING D53472815 TOOL USED CALIPER P/N 500-172-30 S/N 14514392 DUE DATE MAY 23 2018

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. LWR SILL PAX DOOR 842 AFT GALLEY AREA. REPLACED AFT LOWER SILL PAX DOOR 842 IAW SRM 51-72-11 AND DWG 53480505 P4 LOC FR66 + 4.877.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273 LOWER SILL PASSENGER DOOR 842 AT AFT GALLEY. RPL LOWER SILL PAX DOOR 842 AFT GALLEY AREA IAW SRM 51-72-11 AND DRAWING D53480505. P2 LOC FR66+4.877 IN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NR 2018- 143194 FLOORBEAM Y 503.2 ON FR 16 AT FWD GALLEY AREA; REF BP NR 2018-143194 REPLACED FLOORBEAM Y 503.2 ON FR 12 TO FR 16 AT FWD GALLEY AREA IAW SRM 51-71-11 AND DRAWING D53110984 AND D53112825 TOOL USED CALIPER P/N 500-172-30 S/N 14519392 DUE DATE MAY 23 2018

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NR 2018-143175 FLOORBEAM +Y1292 AT LEVEL FR 66 IN PASSENGER CABIN; REF BP NR 2018-143175 REPLACED FLOORBEAM +Y1292 AT LEVEL FR 64 TO FR 66 IN PASSENGER CABIN IAW SRM 51-72-11 AND DRAWING D53472815 TOOL USED CALIPER P/N 500-172-30 S/N 14519392 DUE DATE MAY 23 2018.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273 LWR SILL PAX DOOR 842 AFT GALLEY AREA. RPL LWR DOOR SILL PAX DOOR 842 AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480505. P2 LOC FR66 +4.877.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, EPSU TEST FAILED FWD LT AT FWD GALLEY AREA. REPLACED THE EPSU UNIT FWD LT AT FWD GALLEY AREA IAW AMM 33-51-38-400-001-A & PERFORMED OPS TEST. THE POWER SUPPLY UNIT TESTED OK.

Part: COUPLING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NR 2018-143247. INTERNAL STRUCTURE COUPLING BTW FR 30 TO FR 31 AT STR 41R IN FWD CARGO COMPARTMENT. REPLACED INTERNAL STRUCTURE COUPLING BTW FR 30 TO FR 31 AT STR 41R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DRAWING D532 32647.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. LWR SILL PAX DOOR 842 AFT GALLEY AREA. REPLACED LWR SILL PAX DOOR 842 AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480505 P6 LOC FR68 +.796.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. CORROSION LWR SILL PAX DOOR 842 AFT GALLEY AREA. REPLACED LWR SILL PAX DOOR 842 AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480505. P3 LOC FR66 +.488.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273 LOWER SILL PASSENGER DOOR 842 AT AFT GALLEY. REPLACED LOWER SILL PAX DOOR 842 IAW SRM 51-72-11 AND DRAWING 53480505 P1 LOC FR66+1.107.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. LWR SILL PAX DOOR 842 AFT GALLEY AREA. RPL LWR DOOR SILL PAX DOOR 842 AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480505. P2 LOC FR66 +4.877.

Part: SKIN — DEFORMED (FRAMES 73-74) · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, REAR FUSELAGE JACKING POINT AREA AT FRAMES 73 - 74, STRINGERS 30L - 30R SKIN & ANGLES DEFORMED. REPAIRED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,096 hrs · 15,871 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REF BP NON ROUTINE 2018-143273. LWR SILL PAX DOOR 842 AFT GALLEY AREA. REPLACED LOWER SILL PAX CREW DOOR 842 IAW SRM 51-72-11 AND DWG 53480505.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 40,676 hrs · 14,163 cycles

DURING HEAVY MAINTENANCE, THE EPSU 12WL AND 13WL FAILED CAPACITY CHECK. REPLACED THE EPSU IAW AMM 33-51-38-000-002-A.

Part: ENGINE — FAILED (NR 2) · airframe 30,313 hrs · 10,573 cycles

AIR RETURN TO DEPARTURE DUE TO ENGINE NR 2 FAILURE AND FIRE CLIMBING THROUGH 8000'. NR 2 ENGINE WAS R & R IAW AMM 71-00-20. ENGINE RUN OK.

Part: SWITCH — FAILED (HYD QTY) · airframe 27,065 hrs · 9,434 cycles

AIR RETURN DUE TO HYD B RESERVOIR LOW LEVEL. B SYSTEM LOW PRESSURE ECAM ON TAKEOFF. GAUGE INDICATION FULL. ECAM WARNING & CAUTION - RESERVOIR LO LEVEL. R & R LOW LEVEL SWITCH IAW AMM 29-12-41. FUNCTIONAL CHECK GOOD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 25,684 hrs · 8,973 cycles

DURING MX CHECK, FOUND FLOOR EMERGENCY LIGHT AT SEAT 15 C INOPERATIVE. R & R EMERGENCY LIGHT HARNESS ASSY AT SEAT 15C IAW AMM 33-51-21. OPS CHECK OK.

Part: SENSOR — FAILED (AC BAY) · airframe 22,074 hrs · 7,702 cycles

FLT 805 JFK-PLS, CREW DECLARED EMERGENCY AND AIRCRAFT RETURN TO JFK DUE TO AIR PACK 1 & 2 FAULT MESSAGE. PACK 2 TEMP AT 230 C. REMOVED AND REPLACED 35HH TEMP SENSOR IAW AMM 21-61-12. OPS CHECK GOOD.

Part: CABLE — FAILED (OVERWING EXIT) · airframe 21,409 hrs · 7,466 cycles

FLT 6403 JFK-LCQ, DURING HEAVY MAINTENANCE AND OPERATIONAL CHECK PER TASK CARD 52-21-00-710-003-843. RIGHT OVERWING SLIDE CABLE FAILED TO MOVE SPRING LOADED TEST TOOL TO GREEN POSITION WHEN ESCAPE LATCHES WERE MOVED. RIGHT OVERWING CABLE REMOVED AND REPLACED WITH NEW CABLE PER EC A320-53-1227-02.

Part: VIDEO DISPLAY — MALFUNCTIONED (CABIN) · airframe 14,346 hrs · 5,035 cycles

FLT 303 IAD-FLL PAX ON ROW 24DEF AND IN-FLIGHT CREW MEMBERS REPORTED A STRANGE SMELL IN THE SECTION APPARENTLY LIVE TV’S . CONFIRMED WITH IN-FLIGHT CREW SMELL EMANATING FROM ROW 24 RT AND VDU AT 24F LOST IMAGE. FOLLOWING TSM TASKS 24-00-00-810-823 AND TSM 23-39-00-810-801 SUSPECT LTV AT ROW 24DEF FAULTY. DEACTIVATED LTV SYSTEM IAW MEL 23-39-00 COND 3 CAT D PER MCC. MX-4 UPDATED. PLACARD INSTALLED. MX ACTION COMPLIED WITH. PERFORMED OPS CHECK OF ROW 24DEF AS PER TSM 23-39-00-801-810. NO ABNORMALITIES NOTED. LIVE TV SYSTEM MAY BE DEEMED OPERATIONAL. ALL OPS CHECK NORMAL IAW 23-39-00. MDDR CLEARED. VDU 24F REQUIRES REPLACEMENT, REF FLAG EVENT 404. REPLACED VDU PER 23-39-00.

Part: LIGHT — INOPERATIVE (SEAT 12E) · airframe 2,540 hrs · 828 cycles

FLT 309, IAD-SAN, APPROX BETWEEN 13:30Z-15:09Z SEAT 12E READING LIGHT OUT. PAX OBSERVED SMOKE AS LIGHT WENT OUT. REMOVED OVERHEAD PANEL 12 DEF, INSP WIRING AND CIRCUIT BOARD, FOUND NO EVIDENCE OF ELECT BURNING, RESECURED PANEL. RE-SET CIDS, PERFORMED OPERATIONAL TEST OF THE PASSENGER READING LIGHT SYSTEM PER AMM 33-25-00-710-001. OPS CHECK OK.