# Service difficulty reports: N584JB

A list on [N584JB](https://openairdocs.org/aircraft/N584JB.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 · 55 reports

- [SDR YENA2026090800735](https://openairdocs.org/sdr/YENA2026090800735.md): Apu · contaminated · Sep 7, 2026 · N584JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT 1371, LGA-FLL. APU BLEED STRONG OIL ODOR IN FLIGHT DECK AND AFT CABIN. COMPLIED WITH INFO NOTICE 2017-T015 N AS TYPE 1 AND 2 IDENTIFIED ODOR AS TYPE 1 APU. DECONTAMINATION LEVEL B WAS ACCOMPLISHED IAW AMM 21-00-00-615-803. ACFT OK FOR SVC.
- [SDR YENA2025080100791](https://openairdocs.org/sdr/YENA2025080100791.md): Unknown · odor · Jul 31, 2025 · N584JB · Airbus A320232 · Air Distribution System
  > FLT#495, HPN-MCO. AFT FLIGHT ATTENDANTS REPORTED SMELL/ODOR OF GAS ON TAKEOFF AND LANDING; ACCOMPLISHED INFO-NOTICE 2017-T015L LEVEL 1 DEC. R&R HEPA FILTERS AS REQUIRED PER 21-26-43, LEAK CK GOOD. PERFORMED INSPECTION ON APU FOR SIGNS OF LEAKAGE, NO LEAKS FOU
- [SDR YENA2024081201114](https://openairdocs.org/sdr/YENA2024081201114.md): Door · out of adjust · Aug 11, 2024 · N584JB · Airbus A320232 · Passenger/Crew Doors
  > FLT#984, PHX-BOS. ' L1 DOOR DOES NOT LINE UP PIN WHEN CLOSED.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024070300931](https://openairdocs.org/sdr/YENA2024070300931.md): Girt Bar · failed · Jul 3, 2024 · N584JB · Airbus A320232 · Emergency Equipment
  > FLT#613, HPN-FLL. 'L2 DOOR GIRT BAR STAYS ENGAGED; REMOVED AND REPLACED L2 DOOR GIRT BAR IAW AMM 52-13-22. OPS CHECK GOOD.'
- [SDR YENA2024040500494](https://openairdocs.org/sdr/YENA2024040500494.md): Unknown · odor · Apr 3, 2024 · N584JB · Airbus A320232 · Air Distribution System
  > FLT#1711, EWR-RSW. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) 'DIRTY SOCKS SMELL FROM REAR OF A/C SMELL MOVED TO FRONT AND COCKPIT; PERFORMED DECONTAMINATION OF ECS IAW AMM 21-00-00-615-802,NO FURTHER DEFECTS NOTED.A/C OK FOR CONT. SVC. C/W INFO NOTICE 2017-
- [SDR YENA2024020600246](https://openairdocs.org/sdr/YENA2024020600246.md): Unknown · odor · Feb 4, 2024 · N584JB · Airbus A320232 · Air Distribution System
  > FLT#1927, EWR-MCO. 'MODERATE TO STRONG MUSTY DIRTY SOCK ODOR BELOW 10000FT TIL LANDING. ODOR STRONGEST IN COCKPIT BUT ALSO PERCEIVED IN CABIN. TURNED PACKS OFF AFTER LANDING; INSPECTION OF THE '' APU '' UPON ODOR IN THE CABIN; COMPLIED WITH INFORMATION NOTICE
- [SDR YENA2023005020495](https://openairdocs.org/sdr/YENA2023005020495.md): Pressure Switch · failed · May 4, 2023 · N584JB · Airbus A320232 · Aircraft Fuel Distribution System
  > FLT#361, JFK-BGI. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' ENG #1 FUEL FILTER CLOG MESSAGE DURING CLIMBOUT; SYSTEM TROUBLESHOOT IAW TSM 73-00-00-810-857-A. REMOVED AND REPLACED ENGINE FUEL FILTER IAW AMM 73-12-42 AND REMOVED AND REPLACED ENGINE FUEL FILT
- [SDR YENA2023030900223](https://openairdocs.org/sdr/YENA2023030900223.md): Slide Raft · failed · Mar 8, 2023 · N584JB · Airbus A320232 · Emergency Lighting
  > FLT#573, EWR-TPA. 'FAILED EMERGENCY LIGHT TEST ( ESCAPE SLIDE LIGHTING); REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-62-44. OPS CHECK GOOD.'
- [SDR YENA2022081800808](https://openairdocs.org/sdr/YENA2022081800808.md): Unknown · odor · Aug 16, 2022 · N584JB · Airbus A320232 · Air Distribution System
  > FLT#1179, JFK-MBJ. 'REPEAT ITEM: 3430029 3466939 DIRTY SOCK SMELL UPON ARRIVAL WHEN APU SUPPLYING BLEED AIR. THROUGHOUT CABIN AND COCKPIT. SMELL INITIATED WHEN APU BLEED SELECTED ON DURING TAXI IN. THE CABIN SMELL WAS REPORTED STRONG AT THIS POINT AND GETTING
- [SDR YENA2022050600453](https://openairdocs.org/sdr/YENA2022050600453.md): None · none · May 3, 2022 · N584JB · Airbus A320232 · Air Conditioning System
  > FLT#1733, DCA-PBI. ' AT GATE INFLIGHT CREWMEMBERS ADVISED OF ODOR WAS IN THE CABIN THAT STARTED ON INITIAL DESCENT OF THE PREVIOUS LEG I ALSO PRECEDED AN ODOR THAT SMELLS POSSIBLY LIKE A TINGE OF OIL; ACCOMPLISHED TSM 05-50-00-810-831 ISOLATED CONTAMINATION TO
- [SDR YENA2021110100734](https://openairdocs.org/sdr/YENA2021110100734.md): Ulb · failed · Oct 30, 2021 · N584JB · Airbus A320232 · Central Computers
  > FLT MCO-MZJ.SSFDR ULB REQ R/R AFTER FAILED OPS TEST; R/R ULB OF SSFDR IAW AMM 31-33-55. OPS CKS PASSED
- [SDR YENA2021110100733](https://openairdocs.org/sdr/YENA2021110100733.md): Cvr · failed · Oct 30, 2021 · N584JB · Airbus A320232 · Central Computers
  > FLT MCO-MZJ. CVR ULB REQ R/R AFTER FAILED OPS TEST; R/R ULB ON CVR IAW AMM 23-71-35 OPS CKS PASSED
- [SDR YENA2021011200035](https://openairdocs.org/sdr/YENA2021011200035.md): Fan · failed · Jan 8, 2021 · N584JB · Airbus A320232 · Air Distribution Fan
  > FLT 38, SJO-FLL. ON GROUND, DURING CLIMB, DURING CRUISE NOISE STARTED AND VIBRATION.IT WAS FELT & HEARD IN THE COCKPIT AND FWD GALLEY. ELECTRIC BURN SMELL STARTED TURNING BLOWER OFF STOPS VIBRATION, NOISE AND SMELL, AVIONICS VENT FAN BLOWER, VIBRATING, BEARI
- [SDR YENA2021010800027](https://openairdocs.org/sdr/YENA2021010800027.md): Bearing · failed · Jan 8, 2021 · N584JB · Airbus A320232 · Air Distribution Fan
  > ON GROUND DURING CLIMB, DURING CRUISE NOISE STARTED AND VIBRATION. IT WAS FELT & HEARD IN THE COCKPIT AND FWD GALLEY. ELECTRIC BURN SMELL STARTED TURNING BLOWER OFF STOPS VIBRATION, NOISE AND SMELL. AVIONICS VENT FAN BLOWER, VIBRATING, BEARING FAILING, GRIN
- [SDR YENA2020032080246](https://openairdocs.org/sdr/YENA2020032080246.md): Wire Splice · damaged · Mar 18, 2020 · N584JB · Airbus A320232 · Light System Wiring
  > FLT 2918, JFK-BOS. RED EMERGENCY LIGHT IN FORWARD PARTITION NOT ILLUMINATING; REPLACED WIRE SPLICES 7441VSA REF A320 ESPM 20-43-11. OPS CHECK GOOD.
- [SDR YENA2019101170591](https://openairdocs.org/sdr/YENA2019101170591.md): Skin · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, INSPECTION OF EXISTING REWORKS ON THE RH WING TOP SKIN LOWER SURFACE WAS ACCOMPLISHED, WITH LIGHT CORROSION FOUND BETWEEN RIBS 6-8,14-16,17-18, AND 21-22. THE CORROSION WAS BLENDED OUT AND AIRBUS WAS CONTACTED FOR REPAIR DISPOSITION.
- [SDR YENA2019101170589](https://openairdocs.org/sdr/YENA2019101170589.md): Anchor Fitting · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Wing, Landing Gear Attach Fittings
  > DURING HEAVY MAINTENANCE, LMG RETRACTION ACTUATOR FITTING (ANCHORAGE) HAS CORROSION; LOCATED AND DRILLED REPLACEMENT FITTING IAW SRM 51-44-11 & AIRBUS DWG D57259160. REF HAECO NR 32565 FOR ADDITIONAL DETAILS. LOCATED AND DRILLED REPLACEMENT FITTING IAW SRM 51-
- [SDR YENA2019101170588](https://openairdocs.org/sdr/YENA2019101170588.md): Threshold · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON AFT CARGO DOOR THRESHOLD IN SEVERAL AREAS. REMOVED AND REPLACED AFT CARGO DOOR THRESHOLD IAW A320 SRM 51-72-11 / 51-74-00
- [SDR YENA2019101170587](https://openairdocs.org/sdr/YENA2019101170587.md): Floor Support · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON AFT CABIN FLOOR SUPPORT -Y1182 FR 68 STR 23R; REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED CABIN FLOOR SUPPORT AT -Y1162 FR 68 STR 23R IAW A320 SRM 53-00-14-283-001 AND SRM 51-72-11 REFERENCE
- [SDR YENA2019101170586](https://openairdocs.org/sdr/YENA2019101170586.md): Door Sill · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON BULK CARGO DOOR SILL FR 66 STR 38R; REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM REMOVED AND REPLACED BULK CARGO DOOR SILL FR 60- FR 62 STR 38R. IAW A320 SRM 53-41-49-283-001 AND 51-72-11.
- [SDR YENA2019101170585](https://openairdocs.org/sdr/YENA2019101170585.md): Door Sill · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON L2 DOOR SILL FWD AND AFT IB CORNERS FR 66 - FR 68 STR 23L; REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED L2 DOOR SILL FR 66 TO FR 68 STR 23L IAW A320 SRM 53-41-14-283-002 AND 51-72-11.
- [SDR YENA2019101170584](https://openairdocs.org/sdr/YENA2019101170584.md): Threshold · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON AFT CARGO DOOR THRESHOLD PLATE IN SEVERAL AREAS; REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED AFT CARGO DOOR THRESHOLD PLATE IAW A320 SRM 51-74-00 / 51-72-11.
- [SDR YENA2019101170583](https://openairdocs.org/sdr/YENA2019101170583.md): Floor Support · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOOR SUPPORT Y765 FR 68 STR 23L; REMOVED CORROSION ON FLOOR SUPPORT FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT Y765, FR 68, STR 23L IAW SRM A320-53-00-14-283-002 SRM 51-72-11
- [SDR YENA2019101170582](https://openairdocs.org/sdr/YENA2019101170582.md): Dummy Rail · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOOR SUPPORT DUMMY RAIL AT FR 16, Y503, STR 23L; REMOVED CORROSION 1.0" L X 1.5" W X.055" D FROM ORIG, THICKNESS OF.160" FOUND TO BE OUT OF LIMITS PER SRM 53-11-14-283-004 REMOVED AND REPLACED FLOOR SUPPORT DUMMY RAIL
- [SDR YENA2019101170581](https://openairdocs.org/sdr/YENA2019101170581.md): Floor Support · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOOR SUPPORT Y512 FR 66 STR 23L; REMOVED CORROSION 1.704" L X 2.383" W X.042" D FROM ORIG THICKNESS OF.163" FOUND TO BE OUT OF LIMTS PER SRM. REMOVED AND REPLACED FLOOR SUPPORT AT Y512 FR 66 STR 23L IAW A320 SRM 53-00
- [SDR YENA2019101170580](https://openairdocs.org/sdr/YENA2019101170580.md): Floor Support · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOOR SUPPORT -Y465 FR 66 STR 23R; REMOVED CORROSION 1.262" L X 1.238" W X.031" D FROM ORIG THICKNESS OF.163" FOUND TO BE OUT OF LIMTS PER SRM. REMOVED AND REPLACED FLOOR SUPPORT AT -Y465 FR 66 STR 23R IAW A320 SRM 53-0
- [SDR YENA2019101170579](https://openairdocs.org/sdr/YENA2019101170579.md): Door Sill · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON R2 DOOR SILL FWD AND AFT I/B CORNERS FR 66 TO FR 68 STR 23R; REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED R2 DOOR SILL AT FR 66 TO FR 68 STR 23R IAW A320 SRM 51-72-11 AND SRM 53-41-14-283-002. REFEREN
- [SDR YENA2019101170578](https://openairdocs.org/sdr/YENA2019101170578.md): Floor Support · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOOR SUPPORT AT Y1292, FR 16, STR 23L; REMOVED CORROSION ON FLOOR SUPPORT REMOVED.055" FROM ORIGINAL THICKNESS OF.085" FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND REPLACED FLOOR SUPPORT BEAM AT FR 16 Y1292 STR 23L.
- [SDR YENA2019101170577](https://openairdocs.org/sdr/YENA2019101170577.md): Floor Support · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOOR SUPPORT Y1292 AT FR 66 LAV MOUNT HOLE STR 23L; REMOVED CORROSION 100% MATERIAL LOSS OF.110" ORIG. THICKNESS. OUT OF LIMITS PER SRM. REMOVED AND REPLACED FLOOR SUPPORT BEAM AT Y1292 FR 66 STR 23L IAW SRM 51-72-11 RE
- [SDR YENA2019101170576](https://openairdocs.org/sdr/YENA2019101170576.md): Shear Web · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION AFT SHEAR WEB SUPPORT FRAME FR 69 - FR 70 STR 23R; REMOVED CORROSION FOUND TO BE OUT OF SRM LIMITS. REMOVED AND REPLACED AFT CABIN SHEAR WEB SUPPORT FRAME FR 69- FR70 STR23R IAW A320 SRM 53-41-14-05-A AND SRM 51-72-11. CLASS
- [SDR YENA2019101170575](https://openairdocs.org/sdr/YENA2019101170575.md): Shear Web · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON RH AFT SHEAR WEB FR 60 - FR 70 STR 23R; REMOVED CORROSION FOUND TO BE OUT OF SRM LIMITS. REMOVED AND REPLACED AFT CABIN SHEAR WEB FR 69- FR70 STR23R IAW A320 SRM 53-41-14-05-A AND SRM 51-72-11 REFERENCE HAECO NR 440586-32
- [SDR YENA2019101170574](https://openairdocs.org/sdr/YENA2019101170574.md): Shear Web · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON LH AFT SHEAR WEB FR 69 -FR70 STR 23L; REMOVED CORROSION FOUND TO BE OUT OF SRM LIMITS. REMOVED AND REPLACED AFT CABIN SHEAR WEB IAW A320 SRM 53-41-14-05-A AND SRM 51-72-11 REFERENCE HAECO NR 440586-32435 FOR ALL WORK ACC
- [SDR YENA201910117573](https://openairdocs.org/sdr/YENA201910117573.md): Frame · corroded · Oct 7, 2019 · N584JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CORROSION ON FR71 FRAME STIFFENER BETWEEN STR27R - 33R; REF HAECO N/R 440586-33096 REMOVED AND REPLACED FRAME STIFFENER ANGLE AT FRAME 71 BETWEEN STR17R - 33R IAW SRM 51-72-11-911-001.
- [SDR YENA201904117186](https://openairdocs.org/sdr/YENA201904117186.md): Battery Pack · failed · Apr 7, 2019 · N584JB · Airbus A320232 · Emergency Lighting
  > FT # 391, EMER. AFT L/H BATT. FAULT; R & R AFT L/H BATT. IAW AMM 33-51-38. OPS CHECK GOOD.
- [SDR YENA2019040520174](https://openairdocs.org/sdr/YENA2019040520174.md): Power Supply · failed · Apr 2, 2019 · N584JB · Airbus A320232 · Emergency Lighting
  > FT # 2824, 1C AND 5C SEAT MOUNTED CLEAR LENS EMERGENCY LIGHTS INOP ( FLOOR PROX EMERG ESCAPE PATH MARK SYS - INCANDESCENT LIGHTING SYS - NOT APPLICABLE TO (N703 AND UP)); REPLACED EPSU FIN# 10EL PER AMM 33-51-38. PERFORMED EMER LIGHTS SYS TEST PER JETBLUE JO
- [SDR YENA201809280411](https://openairdocs.org/sdr/YENA201809280411.md): Battery · failed · Sep 28, 2018 · N584JB · Airbus A320232 · Emergency Lighting
  > FLT 2044, PBI-EWR. PSU EMERG LIGHT TEST FAIL. R&R FWD LT EMERG LIGHT BATTERY (10WL) IRW AMM 33-51-38. OPS CHECK SAT.
- [SDR YENA201710160839](https://openairdocs.org/sdr/YENA201710160839.md): Cable · no test · Oct 16, 2017 · N584JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, RT OVERWING SLIDE CABLE FAILED TO TEST. R & R THE OVERWING SLIDE CABLE. OPS CHECKED GOOD IAW AMM 25-62-43.
- [SDR YENA201710160838](https://openairdocs.org/sdr/YENA201710160838.md): Cable · no test · Oct 16, 2017 · N584JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, THE LT OVERWING SLIDE CABLE FAILED TO TEST. R & R THE OVERWING SLIDE CABLE. OPS CHECKED GOOD IAW AMM 25-62-45.
- [SDR YENA201707260601](https://openairdocs.org/sdr/YENA201707260601.md): Control Unit · failed · Jul 26, 2017 · N584JB · Airbus A320232 · Autopilot System
  > RETURN TO FIELD. FD V SPEED REMAINS IN 0 IN CLIMB CRZ APP, AFC PANEL V/S FPA SELECTION KNOB. R & R FCU IAW AMM 22-81-12, OPS CHECKED GOOD, VERIFIED FD NOT LOCKED IN VERTICAL BY CYCLING V/S SELECT KNOB AND FD SWITCHES.
- [SDR YENA201706250523](https://openairdocs.org/sdr/YENA201706250523.md): Pump · leaking · Jun 25, 2017 · N584JB · Airbus A320232 · APU Oil System
  > SEVERAL REPORTS OF STRONG FOUL ODOR IN CABIN. ACCOMP APU INLET DUCT WASH FROM RESIDUAL OIL. PERFORMED ECS DECONTAMINATION, ALL CHECKED NORMAL IAW 21-00-00615-004A. INSTALLED APU BLEED AIR DUCT IAW AMM 49-11-11, NO TRACE OF OIL FOUND IN THE DUCT. FOUND SOME O
- [SDR YENA201705060357](https://openairdocs.org/sdr/YENA201705060357.md): Filter · failed · May 6, 2017 · N584JB · Airbus A320232 · Air Distribution System
  > A STRONG MUSTY MOLD ODOR DESCENDING THROUGH 7000 FT. REMOVED AND REPLACED THE NR 1 AND 2 RECIIRCULATION FILTERS IAW AMM 21-21-41. REMOVED AND REPLACED THE OZONE FILTERS IAW AMM 21-51-41. LEAK CHECKED GOOD.
- [SDR YENA201705060356](https://openairdocs.org/sdr/YENA201705060356.md): Filter · failed · May 6, 2017 · N584JB · Airbus A320232 · Air Distribution System
  > A STRONG MUSTY MOLD ODOR DESCENDING THROUGH 7000 FT. REMOVED AND REPLACED THE 1 AND 2 RECIIRCULATION FILTERS IAW AMM 21-21-41. REMOVED AND REPLACED THE OZONE FILTER IAW AMM 21-51-41. LEAK CHECKED GOOD.
- [SDR YENA201703240215](https://openairdocs.org/sdr/YENA201703240215.md): Filter · failed · Mar 24, 2017 · N584JB · Airbus A320232 · Air Distribution System
  > FT # 1459, BDL-FLL. CABIN ODOR RETURNED ON DESCENT OILY SEWAGE ODOR. REMOVED AND REPLACED THE 1 AND 2 PACK OZONE FILTERS IAW AMM 21-51-41, OPS AND LEAK CHECKED GOOD.
- [SDR YENA201703240214](https://openairdocs.org/sdr/YENA201703240214.md): Filter · failed · Mar 24, 2017 · N584JB · Airbus A320232 · Air Distribution System
  > CABIN ODOR RETURNED ON DESCENT OILY SEWAGE ODOR. REMOVED AND REPLACED THE NR 1 AND 2 PACK OZONE FILTERS IAW AMM 21-51-41, OPS AND LEAK CHECKED GOOD.
- [SDR YENA20160919805](https://openairdocs.org/sdr/YENA20160919805.md): Power Supply · failed · Sep 19, 2016 · N584JB · Airbus A320232 · Emergency Lighting
  > FORWARD LT EPSU FAILS BATTERY SYSTEM TEST REF T/C A320-33-51-00-710-003. R & R FORWARD LT EPSU IAW AMM 33-51-38. OPS CHECK OK.
- [SDR YENA20160203096](https://openairdocs.org/sdr/YENA20160203096.md): Floor Support · corroded · Feb 3, 2016 · N584JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOORBEAM FRAME 66-FRAME 68 AND -Y765 HAS CORROSION; R & R FLOORBEAM -Y765 AT FRAME 64-FRAME 66 IAW SRM 51-72-11 AND REMOVED CORROSION AT FRAME 68 -Y765 AND FOUND TO BE WITHIN LIMITS IAW SRM 51-74-00. REMOVED.015 MAX ALLOWANCE.016. FLOORBEAM -Y765 AT
- [SDR YENA20150517127](https://openairdocs.org/sdr/YENA20150517127.md): Controller · failed · May 17, 2015 · N584JB · Airbus A320232 · Cabin Pressure Controller
  > ACFT DIVERTED, AT CRUISE, CABIN PR1 FAULT WHEN LEVELED AT 36,000 ACFT THEN DISPLAYED EXCESSIVE CABIN ALT, ALL SECONDARY INDICATIONS WERE NORMAL CAB ALT WAS 6400, NO EXCESSIVE RAE AND NORMAL DELTA P. R & R CPC 1 & CPC 2 IAW AMM 21-31-34.
- [SDR YENA20150517126](https://openairdocs.org/sdr/YENA20150517126.md): Controller · failed · May 17, 2015 · N584JB · Airbus A320232 · Cabin Pressure Controller
  > ACFT DIVERTED, AT CRUISE, CABIN PR1 FAULT WHEN LEVELED AT 36,000. AC THEN DISPLAYED EXCESSIVE CABIN ALT, ALL SECONDARY INDICATIONS WERE NORMAL CAB ALT WAS 6400. NO EXCESSIVE RAE AND NORMAL DELTA P. R & R CPC 1 & CPC 2 IAW AMM 21-31-34.
- [SDR YENA20150517125](https://openairdocs.org/sdr/YENA20150517125.md): Outflow Valve · failed · May 17, 2015 · N584JB · Airbus A320232 · Pressure Regulator/Outflow Valve
  > DIVERTED, AT CRUISE CAB PR1 FAULT WHEN LEVELED AT 36,000. AC THEN DISPLAYED EXCESSIVE CABIN ALT, ALL SECONDARY INDICATIONS WERE NORMAL CABIN ALT WAS 6400 NO EXCESSIVE RAE AND NORMAL DELTA P. R & R OUTFLOW VALVE ASSY IAW AMM 21-31-51. OPS CHECK NORMAL ALSO PR
- [SDR YENA20150517124](https://openairdocs.org/sdr/YENA20150517124.md): Controller · failed · May 17, 2015 · N584JB · Airbus A320232 · Cabin Pressure Controller
  > DIVERTED, CABIN PRESSURE LOSS, ALTITIDE 33,000 FT, SYSTEM 1 FAULT, AUTOMATIC CABIN PRESSURE CONTROL SYSTEM- CPC1, AUTOMATIC CABIN PRESSURE CONTROL SYSTEM- CPC1, R & R CPC 1 IAW AMM 21-31-34. OPS CHECK GOOD IAW AMM 21-31-00-710-002-A. OPS CHECK OF OUT FLOW VAL

Next page: https://openairdocs.org/aircraft/N584JB/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 = 'N584JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N584JB/reports

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