# Service difficulty reports: N507JT

A list on [N507JT](https://openairdocs.org/aircraft/N507JT.md).

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

Page 1 of 2 · 61 reports

- [SDR YENA2025062500647](https://openairdocs.org/sdr/YENA2025062500647.md): Hook And Loop · melted · Jun 24, 2025 · N507JT · Airbus A320232 · Air Distribution System
  > FLT#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 I
- [SDR YENA2025061700630](https://openairdocs.org/sdr/YENA2025061700630.md): Door Frame · cracked · Jun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, Structure
  > DURING 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: N
- [SDR YENA2025061700629](https://openairdocs.org/sdr/YENA2025061700629.md): Door Frame · cracked · Jun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, Structure
  > DURING 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: N
- [SDR YENA2025061700628](https://openairdocs.org/sdr/YENA2025061700628.md): Door Frame · cracked · Jun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, Structure
  > DURING 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:
- [SDR YENA2025061700627](https://openairdocs.org/sdr/YENA2025061700627.md): Door Frame · cracked · Jun 13, 2025 · N507JT · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 TASK
- [SDR YENA2025061700626](https://openairdocs.org/sdr/YENA2025061700626.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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 ON
- [SDR YENA2025061700625](https://openairdocs.org/sdr/YENA2025061700625.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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
- [SDR YENA2025061700624](https://openairdocs.org/sdr/YENA2025061700624.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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
- [SDR YENA2025061700623](https://openairdocs.org/sdr/YENA2025061700623.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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
- [SDR YENA2025061700622](https://openairdocs.org/sdr/YENA2025061700622.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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 LIMITS
- [SDR YENA2025061700621](https://openairdocs.org/sdr/YENA2025061700621.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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 SU
- [SDR YENA2025061700620](https://openairdocs.org/sdr/YENA2025061700620.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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 RIB
- [SDR YENA2025061700619](https://openairdocs.org/sdr/YENA2025061700619.md): Skin · corroded · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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 SK
- [SDR YENA2025061700618](https://openairdocs.org/sdr/YENA2025061700618.md): Skin · damaged · Jun 13, 2025 · N507JT · Airbus A320232 · Wing, Plate/Skin
  > DURING 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 8159
- [SDR YENA2025021700157](https://openairdocs.org/sdr/YENA2025021700157.md): Unknown · odor · Feb 14, 2025 · N507JT · Airbus A320232 · Air Distribution System
  > FLT#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
- [SDR YENA2025012900120](https://openairdocs.org/sdr/YENA2025012900120.md): Filter · odor · Jan 28, 2025 · N507JT · Airbus A320232 · Air Distribution System
  > FLT#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.'
- [SDR YENA2025012800113](https://openairdocs.org/sdr/YENA2025012800113.md): Apu · odor · Jan 25, 2025 · N507JT · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#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 DECONT
- [SDR YENA2024103001413](https://openairdocs.org/sdr/YENA2024103001413.md): Radar · failed · Oct 30, 2024 · N507JT · Airbus A320232 · Weather Radar System
  > FLT#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.'
- [SDR YENA2024070500940](https://openairdocs.org/sdr/YENA2024070500940.md): Engine · failed · Jul 3, 2024 · N507JT · Airbus A320232 · Engine (Turbine/Turboprop)
  > FLT#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 BI
- [SDR YENA2023122801658](https://openairdocs.org/sdr/YENA2023122801658.md): Unknown · unknown · Dec 19, 2023 · N507JT · Airbus A320232 · Hydraulic System, Main
  > FLT#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.'
- [SDR YENA2023070300753](https://openairdocs.org/sdr/YENA2023070300753.md): Servo Control · failed · Jun 30, 2023 · N507JT · Airbus A320232 · Aileron Control System
  > FLT#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
- [SDR YENA2022110401088](https://openairdocs.org/sdr/YENA2022110401088.md): None · none · Nov 2, 2022 · N507JT · Airbus A320232 · Air Conditioning System
  > FLT#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 BR
- [SDR YENA2022100601005](https://openairdocs.org/sdr/YENA2022100601005.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)
  > DURING 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) RE
- [SDR YENA2022100601004](https://openairdocs.org/sdr/YENA2022100601004.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING 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 FI
- [SDR YENA2022100601003](https://openairdocs.org/sdr/YENA2022100601003.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING 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 CONTINUITY
- [SDR YENA2022100601002](https://openairdocs.org/sdr/YENA2022100601002.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)
  > DURING 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
- [SDR YENA2022100601001](https://openairdocs.org/sdr/YENA2022100601001.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 INTERCOST
- [SDR YENA2022100601000](https://openairdocs.org/sdr/YENA2022100601000.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 REPLACE
- [SDR YENA2022100600999](https://openairdocs.org/sdr/YENA2022100600999.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 INTERCOST
- [SDR YENA2022100600998](https://openairdocs.org/sdr/YENA2022100600998.md): None · none · Oct 6, 2022 · N507JT · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 CONTINUITY
- [SDR YENA2021090800560](https://openairdocs.org/sdr/YENA2021090800560.md): A/C Pack · contaminated · Sep 1, 2021 · N507JT · Airbus A320232 · Cabin Cooling System
  > FLT 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 RESTORE
- [SDR YENA2021061400366](https://openairdocs.org/sdr/YENA2021061400366.md): Oil System · overserviced · Jun 9, 2021 · N507JT · Airbus A320232 · APU Oil System
  > FLT 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 O
- [SDR YENA2021061400365](https://openairdocs.org/sdr/YENA2021061400365.md): Computer · failed · Jun 9, 2021 · N507JT · Airbus A320232 · Flight Control System
  > FLT 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 A
- [SDR YENA2021052500332](https://openairdocs.org/sdr/YENA2021052500332.md): Skin · debonded · May 21, 2021 · N507JT · Airbus A320232 · Trailing Edge Flaps
  > DURING 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"" REPAIR
- [SDR YENA2021052500331](https://openairdocs.org/sdr/YENA2021052500331.md): Epsu · no test · May 21, 2021 · N507JT · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EMERGENCY LIGHT FAILS TEST; R & R EPSU AND EPSU BATTERY AT 12WL PERFORMED OPERATIONAL TEST IAW AMM 33-51-38-400-001.
- [SDR YENA2021052500330](https://openairdocs.org/sdr/YENA2021052500330.md): Epsu · no test · May 21, 2021 · N507JT · Airbus A320232 · Emergency Lighting
  > DURING 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.
- [SDR YENA2020030610213](https://openairdocs.org/sdr/YENA2020030610213.md): Slide Raft · failed · Mar 1, 2020 · N507JT · Airbus A320232 · Life Raft
  > DURING 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 33
- [SDR YENA2020030610212](https://openairdocs.org/sdr/YENA2020030610212.md): Skin · saturated · Mar 1, 2020 · N507JT · Airbus A320232 · Elevator, Plate/Skin
  > DURING 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 STR
- [SDR YENA2020030610211](https://openairdocs.org/sdr/YENA2020030610211.md): Battery Pack · discharged · Mar 1, 2020 · N507JT · Airbus A320232 · Emergency Lighting
  > DURING 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-
- [SDR YENA2020030610210](https://openairdocs.org/sdr/YENA2020030610210.md): Threshold · corroded · Mar 1, 2020 · N507JT · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING 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 (
- [SDR YENA2019061720322](https://openairdocs.org/sdr/YENA2019061720322.md): Lens · unsecure · Jun 12, 2019 · N507JT · Airbus A320232 · Emergency Lighting
  > FT # 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.
- [SDR YENA201903090120](https://openairdocs.org/sdr/YENA201903090120.md): Light · inoperative · Mar 9, 2019 · N507JT · Airbus A320232 · Emergency Lighting
  > FLT 1043, EWR-PBI. MULTIPLE EXIT SIGNS WITH BULBS BURNED OUT; RELAMPED AS REQUIRED OPS CK NORM MM 33-51-16.
- [SDR YENA20181102724](https://openairdocs.org/sdr/YENA20181102724.md): Unknown · odor · Oct 31, 2018 · N507JT · Airbus A320232 · Air Distribution System
  > COCKPIT/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 THROUG
- [SDR YENA201806070236](https://openairdocs.org/sdr/YENA201806070236.md): Battery Pack · inoperative · Jun 7, 2018 · N507JT · Airbus A320232 · Emergency Lighting
  > DURING 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. OPEN
- [SDR YENA201710080829](https://openairdocs.org/sdr/YENA201710080829.md): Lens · missing · Oct 8, 2017 · N507JT · Airbus A320232 · Emergency Lighting
  > LENS FOR EMERGENCY EXIT LIGHT SEAT 3C MISSING. REPLACED THE EMERGENCY LIGHT LENS.
- [SDR YENA201709170771](https://openairdocs.org/sdr/YENA201709170771.md): Battery Pack · no test · Sep 17, 2017 · N507JT · Airbus A320232 · Emergency Lighting
  > DURING 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.
- [SDR YENA201709170770](https://openairdocs.org/sdr/YENA201709170770.md): Battery Pack · no test · Sep 17, 2017 · N507JT · Airbus A320232 · Emergency Lighting
  > DURING 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.
- [SDR YENA201704250310](https://openairdocs.org/sdr/YENA201704250310.md): Filter · odor · Apr 25, 2017 · N507JT · Airbus A320232 · Air Distribution System
  > TURBINE 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 REPLAC
- [SDR YENA201704250309](https://openairdocs.org/sdr/YENA201704250309.md): Engine · odor · Apr 25, 2017 · N507JT · Airbus A320232 · Engine (Turbine/Turboprop)
  > TURBINE 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 REPLAC
- [SDR YENA20160913794](https://openairdocs.org/sdr/YENA20160913794.md): Floor Support · corroded · Sep 13, 2016 · N507JT · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED FRAMES 12 - 16, -Y1379.5. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-1-14.

Next page: https://openairdocs.org/aircraft/N507JT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N507JT/reports

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