# Service difficulty reports: N594JB

A list on [N594JB](https://openairdocs.org/aircraft/N594JB.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 · 62 reports

- [SDR YENA2026082600710](https://openairdocs.org/sdr/YENA2026082600710.md): Probe · damaged · Aug 26, 2026 · N594JB · Airbus A320232 · Engine Pressure Ratio (EPR)
  > FLT # 1380, FLL-GUA (AIRTURN BACK TO FLL). ENG 2 EPR MODE FAULT; FOUND #2 ENG P2/T2 PROBE WITH DEBRI FROM BIRD STRIKE. REPLACED P2T2 PROBE PER REF. AMM 73-22-11-400-010-A. ACCOMPLISHED PROBE HEAT TEST & IDLE PWR ENG RUN WITH NO FAULTS NOTED.FOUND EVIDENCE OF B
- [SDR YENA2025071100720](https://openairdocs.org/sdr/YENA2025071100720.md): Sign · detached · Jul 9, 2025 · N594JB · Airbus A320232 · Emergency Lighting
  > FLT#2931, SJU-PUJ. "R1 ABOVE DOOR EMERGENCY EXIT SIGN BROKEN / FELL OFF IN FLIGHT; REMOVED AND REPLACED R1 DOOR EXIT LIGHT LENS ALL NORMAL. REF 33-20-00, MX-4 UPDATED."
- [SDR YENA2025052700541](https://openairdocs.org/sdr/YENA2025052700541.md): Unknown · odor · May 26, 2025 · N594JB · Airbus A320232 · Air Distribution System
  > FLT#8449. SDQ-FLL. 'SMELL OF FUMES DURING DESCENT TURNED PACK 1 OFF AND SMELL DISAPPEARED WITH APU RUNNING STILL PACK 1 CAUSING ON GROUND AFTER SITTING ON GROUND SMELL CAME WITH PACK 2 ( PACKS).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024112901513](https://openairdocs.org/sdr/YENA2024112901513.md): Door · abnormal · Nov 25, 2024 · N594JB · Airbus A320232 · Passenger/Crew Doors
  > FLT#8660, MLB-JFK. 'LEFT 1 DOOR SHOWED DISARMED HALF WAY THRU FLIGHT; REPLACED L1 DOOR ARMING HANDLE PROXIMITY SWITCH + PERFORMED ADJUSTED OF PROX SWITCH TARGET. ALL WORK IAW AMM 52-73-11. OPS CHK GOOD.'
- [SDR YENA2024112901512](https://openairdocs.org/sdr/YENA2024112901512.md): Handle · broken · Nov 25, 2024 · N594JB · Airbus A320232 · Passenger/Crew Doors
  > FLT#8660, MLB-JFK. 'DOOR R4 (CAPT RIGHT) SHOWS DISARMED IN FLIGHT WITH CABIN PRESSURE LIGHT FLASHING; REPLACED R4 DOOR ARMING HANDLE PROXIMITY SWITCH + PERFORMED ADJUSTMENT OF THE PROX SWITCH TARGET. ALL WORK DONE IAW AMM 52-73-11. OPS CHECK GOOD. REFERENCE L
- [SDR YENA2024071600998](https://openairdocs.org/sdr/YENA2024071600998.md): Filter · warning message · Jul 13, 2024 · N594JB · Airbus A320232 · Smoke Detection
  > FLT#2536, STI-JFK. (AIRCRAFT PERFORMED AN AIR TURN BACK TO STI).' SMOKE DETECTION FAULT. MULTIPLE FALSE FIRE WARNINGS, LAVATORY B. ( LAVATORY SMOKE DETECTION SYSTEM); REMOVED AND REPLACED LAV FLEECES FILTER IAW AMM 26-17-00. MDDR CLEARED, MX-4 UPDATED. PLACA
- [SDR YENA2023122801662](https://openairdocs.org/sdr/YENA2023122801662.md): Unknown · unknown · Dec 28, 2023 · N594JB · Airbus A320232 · Air Distribution System
  > FLT#1668, PUJ-SJU. (AIRCRAFT PERFORMED ANA IR TURN BACK TO PUJ). 'DIRTY SOCKS SMELL IN AFT OF AIRCRAFT; ACCOMPLISHED INFO NOTICE 2017-T015 UNABLE TO LOCATE SOURCE OF ODOR BOTH PACKS TO BE PLACED ON MEL AND AIRCRAFT REPOSITIONED TO AN MX BASE FOR FURTHER TROUBL
- [SDR YENA2022103101046](https://openairdocs.org/sdr/YENA2022103101046.md): None · none · Oct 29, 2022 · N594JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#2427, FLL- MBJ. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) 'SIMILAR TO THE PREVIOUS LOGBOOK ENTRY ON CLIMB AT 11000 AT 300 KTS, NOTICEABLE VIBRATION NO ENG VIBRATION WAS NOTED. AT FL 80 RECEIVED A CALL FROM FROM FA IN REAR GAELLEY NOTING STRONG VIBRATIO
- [SDR YENA2022103101045](https://openairdocs.org/sdr/YENA2022103101045.md): None · none · Oct 29, 2022 · N594JB · Airbus A320232 · Interphone/Passenger Announcement (PA) System
  > FLT#1825, FLL-LIM. 'DURING CLIMBOUT PASSING 14, OOO A VIBRATION LIKE BUFFET WAS FELT IN THE COCKPIT AND IN THE AFT GALLEY. IT WAS INTERMITTENT. INTENSITY. AND IT HAPPENED WHEN THE A/C UP PITCH ALTITUDE. WE LEVELED OFF PAX AT 270 FOR TROUBLESHOOTING AND COMPLET
- [SDR YENA2022061700613](https://openairdocs.org/sdr/YENA2022061700613.md): Galley · odor · Jun 15, 2022 · N594JB · Airbus A320232 · Cabin Cooling System
  > FLT#163, JFK-SRQ. ' STRONG MUSTRY ODOR REPORT IN FWD GALLEYU( PACKS)'. (SUPPLEMENTAL TO FOLLOW).
- [SDR YENA2022031400176](https://openairdocs.org/sdr/YENA2022031400176.md): Accumulator · underserviced · Mar 13, 2022 · N594JB · Airbus A320232 · Master Cylinder/Brake Valve
  > FLT#2736, LAX-SFO. 'ALTERNATE BRAKE SYSTEM TEST FAILED ( BRAKE PRESSURE 1000 PSI AND ACCUMULATOR NEAR 0); FOUND BRAKE ACCUMULATOR PRESS LOW. SERVICED TO SPECIFIED LIMIT REF AMM 12-14-32. AND ACCOMPLISHED OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM FOUND SAT
- [SDR YENA2021102100712](https://openairdocs.org/sdr/YENA2021102100712.md): Web · corroded · Oct 21, 2021 · N594JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, FROM AEROMAN NR 2021-428652 CORROSION WEB LOCATED BTW FR 69 TO FR 70 STRG 23R AT AFT GALLEY AREA ( CPCP RELATED 534195-01); (RESOLVED ON W/O: 1121241 TASK CARD: NR-00015) FROM AEROMAN NR 2121-428652, WORK DONE BY H.MENDEZ 8601415, RI
- [SDR YENA2021102100711](https://openairdocs.org/sdr/YENA2021102100711.md): Web · corroded · Oct 21, 2021 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, FROM AEROMAN NR 2021-428652 CORROSION WEB LOCATED BTW FR 69 TO FR 70 STRG 23R AT AFT GALLEY AREA ( CPCP RELATED 534195-01)
- [SDR YENA2019062840355](https://openairdocs.org/sdr/YENA2019062840355.md): Angle · cracked · Jun 24, 2019 · N594JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, WHILE ACCOMPLISHING REF /4/ SB, CRACK DAMAGE WAS FOUND ON THE TI ANGLE & SHEAR PLATE LOCATED AT FR41-42 RH OF WING TO FUSELAGE STRUCTURE. REPLACED TI ANGLE WITH NEW, CUT OUT OF CRACK DAMAGE ON SHEAR PLATE, PERFORM DVI, HFEC & ROTO TES
- [SDR YENA2019062840354](https://openairdocs.org/sdr/YENA2019062840354.md): Structure · damaged · Jun 24, 2019 · N594JB · Airbus A320232 · Nacelle/Pylon, Main Frame
  > DURING HEAVY MAINTENANCE, IDENTIFIED HOLE DAMAGE ON THE LH WING PYLON SPIGOT FITTING CENTER HOLE. NOTE AT THE CURRENT CHECK THE SUBJECT AIRCRAFT IS BEING UPGRADED FROM TO WV 017 AND ALL REPAIRS MUST ENSURE WV 17 APPLICABILITY. AIB RESPONDED TO THE DAMAGE EV
- [SDR YENA2019062840353](https://openairdocs.org/sdr/YENA2019062840353.md): Fault Light · false activation · Jun 24, 2019 · N594JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU EXT AND INT LOAD FH FWD CABIN (FAULT) FOUND DURING TEST. PERFORMED TSM OF FAULT EPSU EXT AND INT LOAD FWD "L" CABIN IAW TSM 33-51-00-810-808-A. REPLACED ESCAPE SLIDE AT R1 ROOR (7501MM) IAW AMM 25-62-44-803-A. OPS TEST NORMAL IAW
- [SDR YENA201904210221](https://openairdocs.org/sdr/YENA201904210221.md): Battery · failed · Apr 21, 2019 · N594JB · Airbus A320232 · Emergency Lighting
  > FT # 225, RT EMERG BATTERY 12WL FAILED. REPLACED RT EMERGENCY BATTERY 12WL. CKS OK.
- [SDR YENA201809300480](https://openairdocs.org/sdr/YENA201809300480.md): Battery · discharged · Sep 30, 2018 · N594JB · Airbus A320232 · Emergency Lighting
  > FLT 269, BOS-FLL. DURING BLOCKING IN GATE F4 FFL GROUND POWER DID NOT CONNECT PROPERLY (TWICE). AIRCRAFT DID NOT HAVE APU RUNNING. EMERGENCY CABIN LIGHTING DID NOT ILLUMINATE DURING THESE NON-POWERED EVENTS. FOUND FWD, MID AFT EMERGENCY LIGHT BATTERIES DEAD. R
- [SDR YENA201809300479](https://openairdocs.org/sdr/YENA201809300479.md): Battery · discharged · Sep 30, 2018 · N594JB · Airbus A320232 · Emergency Lighting
  > FLT 269, BOS-FLL. DURING BLOCKING IN GATE F4 FFL GROUND POWER DID NOT CONNECT PROPERLY (TWICE). AIRCRAFT DID NOT HAVE APU RUNNING. EMERGENCY CABIN LIGHTING DID NOT ILLUMINATE DURING THESE NON-POWERED EVENTS. FOUND FWD, MID AFT EMERGENCY LIGHT BATTERIES DEAD. R
- [SDR YENA201809300478](https://openairdocs.org/sdr/YENA201809300478.md): Battery · discharged · Sep 30, 2018 · N594JB · Airbus A320232 · Emergency Lighting
  > FLT 269, BOS-FLL. DURING BLOCKING IN GATE F4 FFL GROUND POWER DID NOT CONNECT PROPERLY (TWICE). AIRCRAFT DID NOT HAVE APU RUNNING. EMERGENCY CABIN LIGHTING DID NOT ILLUMINATE DURING THESE NON-POWERED EVENTS. FOUND FWD, MID AFT EMERGENCY LIGHT BATTERIES DEAD. R
- [SDR YENA201708260700](https://openairdocs.org/sdr/YENA201708260700.md): Unknown · odor · Aug 26, 2017 · N594JB · Airbus A320232 · Air Distribution System
  > AFT F/A REPORTED A DIRTY SOCK ODOR WHEN GEAR WAS EXTENDED ON APPROACH. NOT SMELLED BY OTHER CREW, F/A LOCATION WAS AFT JUMPSEAT. ITEM WAS PLACED ON GMM 2017-TO15B. THE AIRCRAFT WAS OK TO CONTINUE IN SERVICE IAW TSI 2017-TO1513. ACCOMPLISHED TSM 05-50-00-81
- [SDR YENA201701210043](https://openairdocs.org/sdr/YENA201701210043.md): Sensor · failed · Jan 21, 2017 · N594JB · Airbus A320232 · Trailing Edge Flap Control System
  > DURING APPROACH, FLAPS FAILED BETWEEN 1 & 2. CYCLED IAW ECAM. FAILED A SECOND TIME. RECOVERED FLAP AFTER CYCLING TO 0 ON GO AROUND. R & R RIGHT APPU (30CV) SENSOR IAW AMM 27-51-18. PERFORMED SYSTEM OPS CHECK. SYSTEM OPS CHECK PASSED. ALL SELECTED FLAP POSIT
- [SDR YENA20160730672](https://openairdocs.org/sdr/YENA20160730672.md): Thermostat · failed · Jul 30, 2016 · N594JB · Airbus A320232 · Pneumatic Indicating System
  > AIR RETURN BACK TO DEPARTURE. FLIGHT CREW REPORTED AIR ENGINE 2 BLEED ABNORMAL. AIR PACK 2 FAULT OCCURRED UPON THRUST REDUCTION AFTER TAKEOFF. F/O NOTICED SLIGHT ODOR ON TAKEOFF, FOUND SENSE LINES LEAKING, BOTH IP SENSOR AND THERMOSTAT R & R IAW AMM 36-21-4
- [SDR YENA20160730671](https://openairdocs.org/sdr/YENA20160730671.md): Sensor · leaking · Jul 30, 2016 · N594JB · Airbus A320232 · Pneumatic Indicating System
  > AIR RETURN BACK TO DEPARTURE. FLIGHT CREW REPORTED AIR ENGINE 2 BLEED ABNORMAL. AIR PACK 2 FAULT OCCURRED UPON THRUST REDUCTION AFTER TAKEOFF. F/O NOTICED SLIGHT ODOR ON TAKEOFF. FOUND SENSE LINES LEAKING; BOTH IP SENSOR AND THERMOSTAT R & R IAW AMM 36-21
- [SDR YENA20151121605](https://openairdocs.org/sdr/YENA20151121605.md): Door Sill · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > R & R PAX DOOR SILL STRINGER 23R 4" FWD OF FRAME 68 AND 8" OTBD SIDE HAS 2 EA HOLES/AROUND THE HOLES HAS CORROSION. REF JB SCR 14102-1, NR 440264-32447. REMOVED CORROSION AND REPAIRED IAW 53-41-14, PG 211-212.
- [SDR YENA20151121604](https://openairdocs.org/sdr/YENA20151121604.md): Door Sill · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > R & R PAX DOOR SILL, STR 23RT, 4" FWD OF FRAME 68 AND 8" OTBD SIDE HAS 4EA HOLES AROUND THE HOLES HAS CORROSION. REF JB SCR 14104-1 NR 440264-32447. REMOVED CORROSION AND REPAIRED IAW 53-41-14, PG 211-212.
- [SDR YENA20151121603](https://openairdocs.org/sdr/YENA20151121603.md): Door Sill · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 PAX DOOR SILL STR 23 LT FRAME 68, 2" FROM OTBD SIDE, HAS CORROSION. REF NR 440264-32454, R & R L2 PAX DOOR SILL STR 23 LT FR 66-68 IAW SRM 53-41-14, FIG 21, 51-42-11 PAR 7 & 6, 51-44-11, PAR 2 REMOVED, DOT 5422.
- [SDR YENA20151121602](https://openairdocs.org/sdr/YENA20151121602.md): Door Sill · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 PAX DOOR SILL, STR 23 LT, FRAME 68, 2" FROM OTBD SIDE, HAS CORROSION. R & R L2 PAX DOOR SILL, STR 23LT FRAME 66-68 IAW SRM 53-41-14, FIG 21; 51-42-11, PAR 6 & 7; 51-44-11, PAR 2.
- [SDR YENA20151121601](https://openairdocs.org/sdr/YENA20151121601.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FRAME 64-66, STR 23RT FLOORBEAM, -Y1292 HAS CORROSION. AFT CABIN WET AREA FR 64-66, STR 23RT FLOORBEAM -Y1292 HAS CORROSION. WORK ACCOMPLISHED ON WO 741213, NR32469.
- [SDR YENA20151121600](https://openairdocs.org/sdr/YENA20151121600.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FR 69-68, STR 23RT FLOORBEAM -Y1292 HAS CORROSION. R & R AFT CABIN FLOORBEAM -Y1292 AT FRAME 68-69, STR 23R IAW SRM 51-72-11.
- [SDR YENA20151121599](https://openairdocs.org/sdr/YENA20151121599.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FR 69-68, STR 23 LT FLOORBEAM Y1292 HAS CORROSION. R & R AFT CABIN FLOORBEAM Y1292 AT FRAME 69-68 STR 23LT IAW SRM 71-72-11. WORK ACCOMPLISHED ON WO 741213, NR 32467.
- [SDR YENA20151121598](https://openairdocs.org/sdr/YENA20151121598.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOORBEAM Y1292, FR 66-64, STR 23 LT HAS CORROSION. R AFT CABIN FLOOR BEAM Y1292 AT FR 66-64, STG 23L IAW SRM 51-42-11. WORK ACCOMPLISHED ON WO 741213, NR 32473.
- [SDR YENA20151121597](https://openairdocs.org/sdr/YENA20151121597.md): Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FRAME 69-70, STR 23 RT SHEAR PLATE WEB SUPPORT HAS CORROSION. R & R SHEAR WEB PLATE WEB SUPPORT IAW SRM 51-42-11. WORK ACCOMPLISHED ON WO 741213, NR 32465.
- [SDR YENA20151121596](https://openairdocs.org/sdr/YENA20151121596.md): Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FRAME 69-70B, STR 23LT, SHEAR PLATE WEB SUPPORT HAS CORROSION. R & RT SHEAR PLATE WEB SUPPORT IAW SRM 51-42-11. WORK ACCOMPLISHED ON WO 741213, NR 32464.
- [SDR YENA20151121595](https://openairdocs.org/sdr/YENA20151121595.md): Door Sill · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > R & R PAX DOOR SILL, STR 23RT, 4" FWD OF FRAME 68 AND 8" OTBD SIDE HAS 4 EA HOLES, AROUND THE HOLES HAS CORROSION. REMOVED CORROSION AND REPAIRED IAW 53-41-14, PG 211-212.
- [SDR YENA20151121594](https://openairdocs.org/sdr/YENA20151121594.md): Door Sill · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > R & R PAX DOOR SILL STR 23, RT 4" FWD OF FRAME 68 AND 8" OTBD SIDE HAS 4 EA HOLES, AROUND THE HOLES HAS CORROSION. REMOVED CORROSION AND REPAIRED IAW SRM 53-41-14, PG 211-212 WORK ACCOMPLISHED ON WO 741213, NR 32447.
- [SDR YENA20151121593](https://openairdocs.org/sdr/YENA20151121593.md): Dummy Rail · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN LT DUMMY BEAM HAS CORROSION AT FRAME 16. R & R FWD CABIN LT DUMMY BEAM Y347 AT FR 16 IAW SRM 51-71-11 AND SRM 51-42-11 WORK ACCOMPLISHED ON WO 741213, NR32462.
- [SDR YENA20151121592](https://openairdocs.org/sdr/YENA20151121592.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR SUPPORT, Y765 FRAME 66-70, HAS CORROSION. R & R AFT CABIN WET AREA FLOOR SUPPORT IAW SRM 51-42-11. WORK ACCOMPLISHED ON WO 741213, NR 32470.
- [SDR YENA20151121591](https://openairdocs.org/sdr/YENA20151121591.md): Dummy Rail · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA DUMMY RAIL BETWEEN Y765 AND Y1292 FRAME 67-65, STR 23 LT HAS CORROSION. R & R AFT CABIN WET AREA DUMMY RAIL BETWEEN Y765 AND Y1292 FROM FR 65-FR 67 STR 23L IAW SRM 51-72-11 AND SRM 51-42-11. WORK ACCOMPLISHED ON WO 741213, NR 32471
- [SDR YENA20151121590](https://openairdocs.org/sdr/YENA20151121590.md): Dummy Rail · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA DUMMY RAIL BETWEEN Y765 AND Y254, FRAME 67-64, STR 23 LT HAS CORROSION. R & R AFT CABIN WET AREA DUMMY RAIL BETWEEN Y765 AND Y254, FR 64- FR 67, STR 23L IAW SRM 51-72-11 AND SRM 51-42-11.1 WORK ACCOMPLISHED ON WO 741213, NR 32472.
- [SDR YENA20151121589](https://openairdocs.org/sdr/YENA20151121589.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOORBEAM Y-1292, FRAME 66-64, STR 23 RT HAS CORROSION. REF N/R 440264-32556 REMOVED CORROSION ON FLOORBEAM, Y-1292, FRAME 64-5. FOUND MATERIAL LOSS OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOORBEAM IAW SRM 51-42-11, PG 25, PARA 7, 51-44-1
- [SDR YENA20151121588](https://openairdocs.org/sdr/YENA20151121588.md): Door Sill · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > R & R PAX DOOR SILL STR 23R 4" FWD OF FRAME 68 & 8" OTBD SIDE HAS 4 EA HOLES/AROUND THE HOLES HAS CORROSION. REF NR 440264-32447, REMOVED CORROSION FROM R & R PAX DOOR SILL STR 23R 4" FWD OF FR68 & 8" OTBD SIDE 4 EA HOLES. FOUND TO BE OUT OF LIMITS. REPAIRE
- [SDR YENA20151121587](https://openairdocs.org/sdr/YENA20151121587.md): Dummy Rail · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA DUMMY BEAM BETWEEN Y765 & Y254, FR 64-67, STR 23L HAS CORROSION. REF NR 440264-32472: R & R AFT CABIN WET AREA DUMMY RAIL BETWEEN Y765 & Y254 FR64-67, STR 23L IAW SRM 51-72-11 & SRM 51-42-11.
- [SDR YENA20151121586](https://openairdocs.org/sdr/YENA20151121586.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOORBEAM Y765, FR66-70, STR 23L HAS CORROSION, REF NR 440264-32470: R & R AFT CABIN WET AREA FLOORBEAM Y756, FR66-70, STR 23L IAW SRM 51-42-11.
- [SDR YENA20151121585](https://openairdocs.org/sdr/YENA20151121585.md): Dummy Rail · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA DUMMY RAIL BETWEEN Y765 & Y1292, FRAME 65-67, STR 23L HAS CORROSION. REF NR 440264-32471, R & R AFT CABIN WET AREA DUMMY RAIL BETWEEN Y765 & Y1292, FR 65-67 STR 23L IAW SRM 51-72-11 & SRM 51-42-11.
- [SDR YENA20151121584](https://openairdocs.org/sdr/YENA20151121584.md): Shear Web · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FR 69-70, STR 23R SHEAR WEB HAS CORROSION. REF NR 440264-32465: R & R SHEAR WEB SUPPORT RT CABIN BETWEEN FR 69-70 IAW SRM 51-42-11.
- [SDR YENA20151121583](https://openairdocs.org/sdr/YENA20151121583.md): Floor Support · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FR 68-69, STR 23L FLOORBEAM Y1292 HAS CORROSION REF NR 440264-32467: R & R AFT CABIN FLOORBEAM Y1292 FR 68-69 IAW SRM 51-42-11.
- [SDR YENA20151121582](https://openairdocs.org/sdr/YENA20151121582.md): Web · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FRAMES 69-70, STR 23 LT SHEAR PLATE WEB SUPPORT HAS CORROSION. REF NR 440264-32464: R & R AFT CABIN WET AREA FR69-70, STR 23L, SHEAR PLATE WEB SUPPORT IAW SRM 51-42-11 PARA 6 & SRM 51-72-11.
- [SDR YENA20151121581](https://openairdocs.org/sdr/YENA20151121581.md): Dummy Rail · corroded · Nov 21, 2015 · N594JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > FORWARD CABIN LT DUMMY BEAM HAS CORROSION AT FRAME 16 REF NR 440264-32462: R & R FWD CABIN LT DUMMY BEAM Y347 AT FRAME 16 IAW SRM 51-72-11 & SRM 51-42-11.
- [SDR YENA20141102242](https://openairdocs.org/sdr/YENA20141102242.md): Clamp · detached · Nov 2, 2014 · N594JB · Airbus A320232 · Air Intake Anti/De-Ice System
  > CREW DECLARED AN EMERGENCY AND ACFT DIVERTED DUE TO N1 MODE ECAM, FOLLOWED BY FADEC ECAM, FOLLOWED BY ENGINE 2 FAILURE ECAM. ENGINE SHUT ITSELF DOWN. APPROPRIATE ECAM, QRC, + QRH PROCEDURES RUN. ON TROUBLESHOOTING FOUND THE FAILURE OF EEC OVERHEAT THAT RESU

Next page: https://openairdocs.org/aircraft/N594JB/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 = 'N594JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N594JB/reports

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