N507JT

Service difficulty reports · 61

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N507JT' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR YENA2025062500647Hook And Loop · meltedFLT#1911, EWR-RSW."ENTERING FLIGHT DECK SMELL/ODOR OF MELTING WIRES INSULATION BURNING SMELL/ODOR SEE PREVIOUS WRITE UP ON PAGE 4301026 (FOUND OLD HOOK AND LOOP ADVISE MELTING IN THE SUN PERMEATING FAN REMOVED & CLEARED ODOR NO LONGER DETECTED); ACCOMPLISHED IJun 24, 2025 · N507JT · Airbus A320232 · Air Distribution SystemSDR YENA2025061700630Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 O'CLOCK, CRACK DEPTH IS 0.095 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKCARD: NJun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061700629Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 LH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 O'CLOCK, CRACK DEPTH IS 0.090 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKCARD: NJun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061700628Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT OPEN FASTENER HOLE UPPER OUTBOARD AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 O'CLOCK, CRACK DEPTH IS 0.095 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKCARD:Jun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061700627Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 AND 12 O'CLOCK, CRACK DEPTH IS 0.110 INCH APPROX, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1389906 TASKJun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061700626Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ON RH WING IAW (CPCP FINDING); REF AEROMAN WO 2025-180/1 WCC#2025-298913 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ONJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700625Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TIP SKIN LOWER SURFACE BETWEEN RIB 21 TO RIB 22 ON RH WING (CPCP FINDINGS); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00042) AEROMAN WO# 2025 180/1 WCC 2025-2984859 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700624Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10") TO RIB 19 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00044) AEROMAN WO 2025-180/1 NR 2025-298902 FOR WORK PERFORMED; PERFORMED BLEND OUT Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700623Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 TO RIB 17 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00053) AEROMAN WO 180/1 NR# 2025-298901 FOR WORK PERFORMED; PERFORMED PERMANENT REPAIR LOCATED Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700622Skin · corrodedDURING HEAVY MAINTENANCE: AEROMAN WO# 180/1 NR# 2025-298911 FOR WORK PERFORMED: PERFORMED PERMANENT REPAIR LOCATED ON TRAILING EDGE, TOP SKIN, LOWER SURFACE OVERHANG AREA, BTW RIB 14 (PLUS 17 INCHES) TO RIB 15, LH WING AND FOUND WITHIN ALLOWABLE DAMAGE LIMITSJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700621Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 15 (PLUS 16") TO RIB 16 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00055) REF TASK CARD 72179-01-1-575 JB WO# 1389906 PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SUJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700620Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10 INCHES) TO RIB 19 ON LH WING; TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCAION TRAILING EDGE TOP SKIN LOWER SURFACE RIB 18 PLUS 10 INCHES TO RIBJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700619Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 (PLUS 15 INCHES) TO RIB 17 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00057) TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCATED TRAILING EDGE TOP SKJun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025061700618Skin · damagedDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / TEOH BTWN RIB 15 - 19 / LOWER SURFACE / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0046-25 REV 0 (COVER AND PARTS 1 - 4) /2/ AIRBUS RDAF 81592930/005/2025#A /3/ AIRBUS DOSSIER 8159Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/SkinSDR YENA2025021700157Unknown · odorFLT#1733, DCA=PBI. 'FUMES/ODOR COCKPIT DESCENDING THROUGH 8000 THRUST IDLE. HP VALVE OPEN. PACK 1 OFF; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2 IDENTIFIED ODOR TYPE 10 TRANSITORY PRECAUTIONARY R/R 2 EA. CABIN FILTERS, DECONTAMINATION LEVEL 2 WAS Feb 14, 2025 · N507JT · Airbus A320232 · Air Distribution SystemSDR YENA2025012900120Filter · odorFLT#87, ALB-FLL. 'ODOR EVENT DESCENDING THROUGH 4000 PERSISTED 3-5 MINUTES HP VALVES OPEN; C/W INFO NOTICE 2017-TOI5J & REF TSM 05-50-00-810-831-A PERFORMED PACK BURNS NO ODOR NOTED R/R RECIRCULATION FILTERS IAW AMM 21-21-00 NO ODOR NOTICED AT THIS TIME.'Jan 28, 2025 · N507JT · Airbus A320232 · Air Distribution SystemSDR YENA2025012800113Apu · odorFLT#1817, JFK-POS. 'AROUND 14K FEET A STRONG ODOR WAS SMELLED THROUGHOUT THE WHOLE AIRCRAFT. STARTED OUT STRONG AND SWEET THEN TURNED OLD AND MUSTY (DIRTY SOCK); C/W INFO NOTICE 2017-TO15K SECTION B LEVEL 2 DETERMINE APU SOURCE OF ODOR AT THIS TIME. SYS DECONTJan 25, 2025 · N507JT · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR YENA2024103001413Radar · failedFLT#2751, TPA-SJU. (AIRCRAFT DIVERTED TO FLL) 'WX RADAR INTERMITTENT. FAILED 3 TIMES, JUST STOPPED PAINTING AND NO INDICATIONS, NO ECAMS; REMOVED AND REPLACED R.T. I.A.W AMM 34-41-33, NO FAULTS NOTED.'Oct 30, 2024 · N507JT · Airbus A320232 · Weather Radar SystemSDR YENA2024070500940Engine · failedFLT#153, JFK- PBI. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) .'AFTER T/O A/C HAD A SIGNIFICANT VIBRATION. WHILE TROUBLESHOOTING TOWER ADVISED SEVERAL A/C SAW DEBRIS COME OFF OUR A/C. WE RETURNED AND DIDAN OVERWEIGHT LANDING; FOUND #1 ENG DAMAGE CAUSED BY BIJul 3, 2024 · N507JT · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA2023122801658Unknown · unknownFLT#2475, BDL-SJU. (AIRCRAFT DECALRED AN EMERGENCY INTO SJU) ' HYD Y RSVR LVL ECAM: 45 MINUTES INTO FLIGHT C FL 340. FOLLOWED ECAM QRH. CONTACTED MCC; REMOVED AND REPLACED O-RING AT HALF COUPLING FIN# 3701GM IAW AMM 29-13-15. OPT CHECK OK. NO LEAK FOUND.'Dec 19, 2023 · N507JT · Airbus A320232 · Hydraulic System, MainSDR YENA2023070300753Servo Control · failedFLT#1393, FLL- NAS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' R AILERON IS DEFLECTED UP A LITTLE. AIR RETURN TO FLL PER CO; FOUND R/H WING BLUE AILERON SERVO CONTROL AT FAULT. REF LOGPG 3740737 -2 (ACCOMPLISHED REMOVED AND REPLACED R/H WING BLUE AIRLERON Jun 30, 2023 · N507JT · Airbus A320232 · Aileron Control SystemSDR YENA2022110401088None · noneFLT#1279, LAS-LAX. 'STRONG CHEESE ODOR REPORTED BY FA'S ON FINAL APPROACH. ISOLATION CHECKLIST DONE AFTER LANDING; DURING T/S PER TSM 05-50-00-810-831-A, FOUND GREEN SYS HYD LINE LEAKING, CORRECTED ON LOG PAGE # 3442177, ITEM#1 (FOUND GREEN HYD LINE REGULAR BRNov 2, 2022 · N507JT · Airbus A320232 · Air Conditioning SystemSDR YENA2022100601005None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 68 RH SIDE UPPER CORNER WEB JOINT AFT FACE BETWEEN UPPER FASTENER AND STRINGER 8 RADIUS, CRACK LENGTH IS 0.2 50 INCH APPROX AT AFT GALLEY AREA (1 E/A); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00014 ) REOct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)SDR YENA2022100601004None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF AEROMAN WO 2022 181/1 NR 2022-481927, REMOVED AND REPLACE CONTINUITY FIOct 6, 2022 · N507JT · Airbus A320232 · Fuselage Internal Mounting StructureSDR YENA2022100601003None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF TO AEROMAN WO 2O22 181/1 NR 2022-481928, REMOVED AND REPLACE CONTINUITYOct 6, 2022 · N507JT · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2022100601002None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16RH SIDE IN OPEN FASTENER HOLE 2 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS AREA 6 AND 8 O CLOCK AT FWD GALLEY AREA (2EA); (RESOLVED ON W/O: 1166726 TASK CARD: NR-00019 ) REF TO AEROMAN WO 2022 181/1 Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)SDR YENA2022100601001None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 8 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481996, REMOVED AND REPLACED INTERCOSTOct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)SDR YENA2022100601000None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 2 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 2, 5, 8, AND 11 OCLOCK AT THE FWD GALLEY AREA (4 EA); REF TO AEROMAN WO 2022 181/1 NR 2022-481998, REMOVED AND REPLACEOct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)SDR YENA2022100600999None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE 3 AT DOOR S TOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 1 AND 4 OCLOCK AT FWD GAL LEY AREA (2 EA); REF TO AEROMAN WO 2020 181/1 NR 2022-481999, REMOVED AND REPLACED INTERCOSTOct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)SDR YENA2022100600998None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT (1 EA); REF TO AEROMAN WO 2022-181/1 NR 2022-481927, REMOVED AND REPLACE CONTINUITYOct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)SDR YENA2021090800560A/C Pack · contaminatedFLT 2893, JFK-MIA. DIRTY SOCKS SMELL ON DECENT THROUGH 5000 FT. DISIPATED WITH PACK 1 OFF. PACK 1 ODOR ( PACKS ); ACCOMPLISHED WO 1132627 SVC CK AND CABIN ODOR TSM PER INFO NOTICE 2017 - T015 H SECT B2 AND AMM TASK 21-00-00 LEVEL A DECONTAMINATION. AC RESTORESep 1, 2021 · N507JT · Airbus A320232 · Cabin Cooling SystemSDR YENA2021061400366Oil System · overservicedFLT 543, EWR-PBI. #4 F/A SMELLED THE DIRTY SOCKS SMELL BEFORE TO OUT OF EWR F/A SAID THE SMELL WENT AWAY BUT SEVERAL PAXS COMPLAINED OF THE SMELL THE SMELL CAME BACK ON DESCENT THE F/A STATED; COMPLIED WITH INFO NOTICIE 2017-T015F SECTION B. APU BLEED PLACED OJun 9, 2021 · N507JT · Airbus A320232 · APU Oil SystemSDR YENA2021061400365Computer · failedFLT 6122, PBI-MCO. AFTER DEPARTURE WE NOTICE THE AIRPLANE IN A SLIP AND IN A 5 DEGREE BANK RIGHT TURN WITH AUTO PILOT ON. TURNING OFF THE AUTOPILOT THE PLANE 3 BANK INCREASES FURTHER & AGRESSIVELY; PERFORMED TSM TASK 27-10-00-810-842A. R & R ELAC1 (2CE1) PER AJun 9, 2021 · N507JT · Airbus A320232 · Flight Control SystemSDR YENA2021052500332Skin · debondedDURING HEAVY MAINTENANCE, LH WING / OTBD FLAP / TRAILING EDGE / RIB 6-8 / DEBOND - PERMANENT REPAIR (PN:D575710080000 , SN: 2083); THIS REPAIR HAS BEEN APPROVED VIA THE REF /2/ RDAF. THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORY ""A"" REPAIRMay 21, 2021 · N507JT · Airbus A320232 · Trailing Edge FlapsSDR YENA2021052500331Epsu · no testDURING HEAVY MAINTENANCE, EMERGENCY LIGHT FAILS TEST; R & R EPSU AND EPSU BATTERY AT 12WL PERFORMED OPERATIONAL TEST IAW AMM 33-51-38-400-001.May 21, 2021 · N507JT · Airbus A320232 · Emergency LightingSDR YENA2021052500330Epsu · no testDURING HEAVY MAINTENANCE, EMERGENCY LIGHT FAILS TEST; R & R EPSU AND EPSU BATTERY AT 10WL PERFORMED OPERATIONAL TEST IAW AMM 33-51-38-400-001-A.May 21, 2021 · N507JT · Airbus A320232 · Emergency LightingSDR YENA2020030610213Slide Raft · failedDURING HEAVY MAINTENANCE, EPSU INT LOAD AND EXT LOAD FAULT SHOW ON PTP DURING EMERGENCY LIGHT TEST; REF AEROMAN N/R 2020-44268, REMOVED AND REPLACED ESCAPE SLIDE RAFT FROM DOOR 831 IAW 25-23-42 AND PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW AMM 33Mar 1, 2020 · N507JT · Airbus A320232 · Life RaftSDR YENA2020030610212Skin · saturatedDURING HEAVY MAINTENANCE, TRAPPED WATER INDICATION ON R/H ELEVATOR HOMNEYCOMB CORE STRUCTURE TOP SKIN LOC 2"" OUTBD FROM LIGHTNING STRIP N2 AND 4"" FROM T/E ( SIZE IS L=4"", W= 3""; REF AEROMAN N/R 2020-44129, PERFORMED REPAIR ON RH ELEVATOR HONEYCOMB CORE STRMar 1, 2020 · N507JT · Airbus A320232 · Elevator, Plate/SkinSDR YENA2020030610211Battery Pack · dischargedDURING HEAVY MAINTENANCE, WHILE ACCOMPLISHING ITEM 13 OF TASK CARDS 320K8010 ENO -10 AND 320K8010-ENO 11, FOUND EMERGENCY LIGHTS 51WL AND 53WL INOP IN PASSENGER CABIN (2EA); REF AEROMAN N/R 2020-44247, REMOVED AND REPLACED GPSU BATTERY PACK 11WL IAW AMM 33-51-Mar 1, 2020 · N507JT · Airbus A320232 · Emergency LightingSDR YENA2020030610210Threshold · corrodedDURING HEAVY MAINTENANCE, CORROSION ON THRESHOLD SHEET LOCATED FR52A TO FR56 RH SIDE IN AFT CARGO COMPARTMENT; ACP ON AEROMAN W/O 2020 7/1 NON-ROUTINE 2020-44137. REMOVED AND REPLACED THRESWHOLD SHEET LOCATED FR 52A TO FR 56 RH SIDE IN AFT CARGO COMPARTMENT (Mar 1, 2020 · N507JT · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2019061720322Lens · unsecureFT # 2074, EMERGENCY FLOOR LIGHT ROW 1 HELD ON BY A BANDAID. FALLING OFF. SECURED ROW 1 EMERGENCY LIGHT LENS COVER AS REQUIRED IAW AMM 33-50-00. OK FOR SERVICE.Jun 12, 2019 · N507JT · Airbus A320232 · Emergency LightingSDR YENA201903090120Light · inoperativeFLT 1043, EWR-PBI. MULTIPLE EXIT SIGNS WITH BULBS BURNED OUT; RELAMPED AS REQUIRED OPS CK NORM MM 33-51-16.Mar 9, 2019 · N507JT · Airbus A320232 · Emergency LightingSDR YENA20181102724Unknown · odorCOCKPIT/CABIN HAD AN ODOR WHILE DESCENDING FROM 370 - 330. F/A CALLED ABOUT ODOR ROW 21-25. BURNING ELEC. METALIC ODOR IN COCKPIT. ACCOMPLISHED ODOR RECOGNITION AND ISOLATION PROCEDURE FCOM VOL-1 PACK 1 OFF 3-5 MIN. ODOR DISSIPATED, KEPT CONFIGURATION THROUGOct 31, 2018 · N507JT · Airbus A320232 · Air Distribution SystemSDR YENA201806070236Battery Pack · inoperativeDURING A CABIN EMERGENCY LIGHT TEST, FAILED FOR EMERGENCY LIGHT 12WL. REMOVED AND REPLACED THE EPSU 12WL BATTERY PACK IAW AMM 33-51-38-000-002-A, AND 33-51-38-400-002-A. OPS TESTED GOOD IAW AMM 33-54-38-805-058-A. OPENJun 7, 2018 · N507JT · Airbus A320232 · Emergency LightingSDR YENA201710080829Lens · missingLENS FOR EMERGENCY EXIT LIGHT SEAT 3C MISSING. REPLACED THE EMERGENCY LIGHT LENS.Oct 8, 2017 · N507JT · Airbus A320232 · Emergency LightingSDR YENA201709170771Battery Pack · no testDURING A WEEKLY EMERGENCY LIGHT TEST, THE SYSTEM FAILED. FOUND THE EPSU BATTERY AT FAULT 10WL AND 13WL. R & R BOTH BATTERY PACKS IAW AMM 33-51-38. OPS TESTED OK.Sep 17, 2017 · N507JT · Airbus A320232 · Emergency LightingSDR YENA201709170770Battery Pack · no testDURING A WEEKLY EMERGENCY LIGHT TEST, THE SYSTEM FAILED. FOUND EPSU BATTERY AT FAULT 10WL AND 13WL. R & R BOTH BATTERY PACKS IAW AMM 33-51-38. OPS TESTED OK.Sep 17, 2017 · N507JT · Airbus A320232 · Emergency LightingSDR YENA201704250310Filter · odorTURBINE OIL / DIRTY SOCK ODOR DURING CLIMB 7-12000 FT. INCREASED WHEN ENTERING THIN CLOUD LAYER. DURATION 3-4 MINUTES. FA REPORTED SLIGHTLY STRONGER IN FRONT. HI / LO FLOW NO CHANGE. DFDR EVENT BUTTON PUSHED. NR 1 ENGINE AND LT & RT OZONE FILTERS REPLACApr 25, 2017 · N507JT · Airbus A320232 · Air Distribution SystemSDR YENA201704250309Engine · odorTURBINE OIL / DIRTY SOCK ODOR DURING CLIMB 7-12000 FT. INCREASED WHEN ENTERING THIN CLOUD LAYER. DURATION 3-4 MINUTES. FA REPORTED SLIGHTLY STRONGER IN FRONT. HI / LO FLOW NO CHANGE. DFDR EVENT BUTTON PUSHED. NR 1 ENGINE AND LT & RT OZONE FILTERS REPLACApr 25, 2017 · N507JT · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA20160913794Floor Support · corrodedFLOOR SUPPORT CORRODED FRAMES 12 - 16, -Y1379.5. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-1-14.Sep 13, 2016 · N507JT · Airbus A320232 · Fuselage Miscellaneous Structure
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