# Service difficulty reports: N591JB

A list on [N591JB](https://openairdocs.org/aircraft/N591JB.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 · 51 reports

- [SDR YENA2025052000525](https://openairdocs.org/sdr/YENA2025052000525.md): Frame · cracked · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK: INTERNAL STRUCTURE CONNECTION SECTION LOCATED FR68 STR23L AT AFT GALLEY AREA; REF AEROMAN NR 2025-16894 W/O:2025 82/1: R & R SECTION CONNECTION ANDFASTENERS FR68 STR23L AFT GALLEY AREA IAW A320 SRM 51-44-11, 51-21-11, AND DWG E
- [SDR YENA2025052000524](https://openairdocs.org/sdr/YENA2025052000524.md): Frame · cracked · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK: HOLE 5 FR16R UPPER DOUBLE JOGGLE AREA AT NOSE FWD FUSELAGE. D= 0.050"@ 5 O'CLOCK LOOKING FROM OUTSIDE; (RESOLVED ON W/O: 1330742 TASKCARD: NR-00020) REF AEROMAN 2025-168992 W/O:2025 82/1: PERFORMED PERMANENT REPAIR ON HOLE #5,
- [SDR YENA2025052000523](https://openairdocs.org/sdr/YENA2025052000523.md): Frame · cracked · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON HOLE C, LOCATED ON FR 16 LH SIDE UPPER DOUBL E JOGGLE AREA AT NOSE FWD FUSELAGE; WO 1330742 - NR-00022 - REF AEROMAN W/O 2025 82/1 N/R 2025-168991. PERFORMED PERM REPAIR ON HOLE C, LOCATED ON FR 16 LH SIDE UP
- [SDR YENA2025052000522](https://openairdocs.org/sdr/YENA2025052000522.md): Frame · cracked · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: MAJOR REPAIR - CRACK INDICATION FOUND AROUND FASTENER HOLE LOCATED ON FRAME 35 FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENT, BETWEEN STR30L AND STR31L ON FASTENERS HOLES #6,#2 AND #B1 FWD CARGO COMPARTMENT.CRACK LENGTH=0.300 INCHES AP
- [SDR YENA2025052000521](https://openairdocs.org/sdr/YENA2025052000521.md): Skin · corroded · May 19, 2025 · N591JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL SKIN UPPER SURFACE BOTTOM SKIN PANEL 3 AT LEVEL RIB 6 BTW REAR SPAR AND FALSE REAR SPAR ON RH WING (CPCP FINDING); (RESOLVED ON W/O: 1330742 TASKCARD: NR-00029) REF AEROMAN N/R 2025-168764, ACCOMPLISHED THE REPAIR T
- [SDR YENA2025052000520](https://openairdocs.org/sdr/YENA2025052000520.md): Power Supply · no test · May 19, 2025 · N591JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: DIDNT PASS OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNITS BY BITE-CH ECK L1 DOOR; REF AEROMAN N/R 2025-169231, REMOVED AND REPLACED ESCAPE SLIDE RAFT 831 IAW AMM 25-62-44-000-011-A AND AMM 25-62-44-400-007-A. PERFORMED OPERATIONAL
- [SDR YENA2025052000519](https://openairdocs.org/sdr/YENA2025052000519.md): Stop Fitting · cracked · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR 66 RH / DOOR STOP FITTING 7 / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0017-25 /2/ AIRBUS DOSSIER 81558284 /3/ AIRBUS RDAF 81558284/003/2025#A /4/ A320 SRM 53-41-12-300-011. DESCRIPTION: ON
- [SDR YENA2025052000518](https://openairdocs.org/sdr/YENA2025052000518.md): Attach Angle · cracked · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 35 AND STGR 30 LH / FWD FACE TO PRESSURE BULKHEAD ATTACHMENT / CRACKS – TEMPORARY REPAIR (REINFORCEMENT); /1/ AEROMAN EA 53-0011-25 REV 0 (COVER + PART 1-12) /2/ AIRBUS RDAF 81564480/003/2025 ISSUE A /
- [SDR YENA2025052000517](https://openairdocs.org/sdr/YENA2025052000517.md): Skin · damaged · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 69-70 AND STGR 30RH -33RH / AFT LAV VENT OUTLET / EXISTING REPAIR DOUBLER / OVZ HOLES – PERMANENT REPAIR; /1/ AEROMAN EA 53-0010-25 (COVER REV 0 + PART 1) /2/ AIRBUS RDAF 81550991/003/2025#A /3/ DOSSIER 8
- [SDR YENA2025052000516](https://openairdocs.org/sdr/YENA2025052000516.md): Firewall · damaged · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: FUSELAGE / TAILCONE / FIREWALL / FR 81-83 LH & RH / DEVIATIONS TO SB A320-53-1500 (FIXATION OF APU AIR INTAKE DUCT MOD) - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0014-25 REV. 0 (COVER + PART 1) /2/ AIRBUS MESSAGE 81559155/008
- [SDR YENA2025052000515](https://openairdocs.org/sdr/YENA2025052000515.md): Skin · corroded · May 19, 2025 · N591JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: WINGS / RH WING/ BOTTOM SKIN PANEL #3 /FASLE SPAR BOX AREA AT RIB 6 / INTERNAL SURFACE / CORROSION - TEMPORARY REPAIR; REFERENCES: /1/ AEROMAN 57-0018-25 (COVER + PART 1-6) /2/ AIRBUS RDAF REF. & ISSUE.: 81556615/003/2025 ISSUE A /3/
- [SDR YENA2025052000514](https://openairdocs.org/sdr/YENA2025052000514.md): Stringer · corroded · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION COUPLING STRINGER 42L LOC. BTW FR56 AND FR57 AFT CARGO COMPARTMENT(CPCP FINDING); REF AE NR 2025-169111, WO 2025-82/1 - REMOVED AND REPLACED COUPLING ON STRINGER 42L LOC. BTW FR56 AND FR57 AFT CARGO COMPARTMENT A320 SRM 51-
- [SDR YENA2025052000513](https://openairdocs.org/sdr/YENA2025052000513.md): Stringer · corroded · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR56 TO FR58 IN AFT CARGO COMPARTMENT(CPCP FINDING); FUR-A320-53-02198 REF AE NR 2025-168926, WO 2025-82/1 - REMOVED AND REPLACED PERMANENT REPAIR SECTION STRINGER 43L AND FASTENERS LOCATED BTW FR56 TO FR60
- [SDR YENA2025052000512](https://openairdocs.org/sdr/YENA2025052000512.md): Stringer · corroded · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 42L BTW FR56 TO FR59 IN AFT CARGO COMPARTMENT(CPCP FINDING); FUR-A320-53-02197 REF AE NR 2025-168925, WO 2025-82/1 - REMOVED AND REPLACED PERMANENT REPAIR ON SECTION STRINGER 42L LOCATED BTW FR56 TO FR60 AFT CARGO
- [SDR YENA2025052000511](https://openairdocs.org/sdr/YENA2025052000511.md): Stringer · corroded · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 41L BTW FR56 TO FR59 IN AFT CARGO COMPARTMENT(CPCPFINDING); FUR-A320-53-02195 CREATED - REF AE NR 2025-168923, WO 2025-82/1 - REMOVED AND REPLACED PERMANENT REPAIR STRINGER 41L LOC BTW FR 56 AND FR 60 IN AFT CARGO C
- [SDR YENA2025052000510](https://openairdocs.org/sdr/YENA2025052000510.md): Floor Support · corroded · May 19, 2025 · N591JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION: FLOOR BEAM +Y765 FR12-FR2LHS FWD GALLEY AREA; REF AEROMAN NR 2025-168931 W/O:2025 82/1: R & R FLOOR BEAM Y765 FR12-FR24LHS FWD GALLEY IAW A320 SRM 51-42-11, 51-72-11, DWG D53112812, D53110920, AND D53135201.
- [SDR YENA2024082601166](https://openairdocs.org/sdr/YENA2024082601166.md): Unknown · odor · Aug 24, 2024 · N591JB · Airbus A320232 · Air Distribution System
  > FLT#1475, BDL-SJU. 'LEVEL 2 FUME EVENT STRONG PERSISTENT DIRTY SOCK SMELL DURING DESCENT FROM 10,000FT.FUMES NOTICED BY BOTH PILOTS.ISOLATION UNSUCCESSFUL OIL ON BELLY OF AIRCRAFT NOTICED DURING PREFLIGHT; COMPLIED WITH INFORMATION NOTICE 2017-T015,SECTION B2,
- [SDR YENA2024011800069](https://openairdocs.org/sdr/YENA2024011800069.md): Oxygen Bottle · failed · Jan 17, 2024 · N591JB · Airbus A320232 · Crew Oxygen System
  > FLT#1197, PVD-FLL. 'AT CRUISE RECEIVED AN ADVISORY FOR CREW OXY LOW, PSI FLASHING AT 540 PSI. PSI CONTINUED TO DROP, WE SHUT IT OFF AT 500 PSI, PSI STAEDY WITH CREW SUPPLY SELECTED OFF * ALL CREW O2 MASKS CLOSED AND OFF; REMOVED AND REPLACED CREW O2 BOTTLE IAW
- [SDR YENA2023080300892](https://openairdocs.org/sdr/YENA2023080300892.md): Unknown · unknown · Aug 3, 2023 · N591JB · Airbus A320232 · Drag Control System
  > FLT#268, PUJ-JFK. (AIRCRAFT DIVERTED TO FLL) 'DURING CRUISE ECAM SEC1 FAULT.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023012300071](https://openairdocs.org/sdr/YENA2023012300071.md): Shear Pin · not reported · Jan 20, 2023 · N591JB · Airbus A320232 · Emergency Equipment
  > FLT#8354, EWR-BOS. 'REPLACED PERCUSSION MECHANISM DIAPHRAM SHEAR PIN AND SERVICE EMERGENCY ASSIST BOTTLE; REPLACED DIAPHRAM AND SERVICED BOTTLE PER AMM 52-10-00.'
- [SDR YENA2022011900030](https://openairdocs.org/sdr/YENA2022011900030.md): Connector · loose · Jan 15, 2022 · N591JB · Airbus A320232 · Brake Anti-Skid Section
  > FLT # 2448, SDQ-FLL. BRAKES AUTO BRAKE FAULT UPON GEAR EXTENSION. AFTER LANDING #2 MAIN BRAKE TEMP EXCEEDED 570DEG. NUMBER 1 BRAKE TEMP REMAINED AT 35DEG.; REF DEFECT 3333726 ITEM 2 R&R BRAKE FAN TECH HOUSING IAW AMM 32-48-510 OPS CHK GOOD. ACCOMPLISHED T/S 1
- [SDR YENA2021112900789](https://openairdocs.org/sdr/YENA2021112900789.md): Apu · fault message · Nov 24, 2021 · N591JB · Airbus A320232 · Smoke Detection
  > FLT 1422, MSY-FLL. SMOKE DETECTION FAULT DISPLAYED; FLT CREW INFORMED MX- A/C PUSHED FROM GATE AND FAULT SMOKE DET FAULT ON ECAM. CREW CALLED MX CONTROL FOR RESET PROCEDURE. MX CONTROL HAD CREW PULL APU ECB/APU CNTL CB. A/C LOST POWER- UNABLE TO RESTART APU O
- [SDR YENA201912241708](https://openairdocs.org/sdr/YENA201912241708.md): Fan · failed · Dec 21, 2019 · N591JB · Airbus A320232 · Air Distribution Fan
  > FLT 1968, AT ALTITUDE, SMOKE IN MID-CABIN. SMELLED ELECTRICAL. DIVERTED. AVIONICS SYSTEM FAULT, BLOWER FAN NO AVNCS SYS FAULT ECAM CAUTION. R & R BLOWER FAN IAW AMM 21-26-51. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.
- [SDR YENA201907130404](https://openairdocs.org/sdr/YENA201907130404.md): Battery · discharged · Jul 13, 2019 · N591JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERIES AT 11WL, 12WL AND 13WL; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT FIN # 11WL, 12WL AND 13WL PER AMM 33-51-38.
- [SDR YENA201907130403](https://openairdocs.org/sdr/YENA201907130403.md): Battery · discharged · Jul 13, 2019 · N591JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERIES AT 11WL, 12WL AND 13WL; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT FIN # 11WL, 12WL AND 13WL PER AMM 33-51-38.
- [SDR YENA201907130402](https://openairdocs.org/sdr/YENA201907130402.md): Battery · discharged · Jul 13, 2019 · N591JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERIES AT 11WL, 12WL AND 13WL; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT FIN # 11WL, 12WL AND 13WL PER AMM 33-51-38.
- [SDR YENA2019062480338](https://openairdocs.org/sdr/YENA2019062480338.md): Connector · broken · Jun 18, 2019 · N591JB · Airbus A320232 · Light System Wiring
  > CONNECTOR BROKEN FOR CEILING EMERGENCY LIGHT AT ROW 18; REINSTALLED WHITE CONNECTOR ON WIRE 1 OF CEILING EMERGENCY LIGHT AT ROW 18. OPS CHECK GOOD. REF AMM 33-51-11.
- [SDR YENA2019061840329](https://openairdocs.org/sdr/YENA2019061840329.md): Power Supply · no test · Jun 14, 2019 · N591JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU-EMERGENCY POWER SUPPLY UNIT DONT PASS OPERATIONAL TEST. REPLACED EPSU IAW AMM 33-51-38-400-001-A. PERFORMED OPERATIONAL TEST OF THE EPSU IAW AMM 33-51-00-710-001. TEST IS GOOD AT THIS TIME. SUPPLEMENTAL INFORMATION TO FOLLOW.
- [SDR YENA2019061840327](https://openairdocs.org/sdr/YENA2019061840327.md): Stringer · corroded · Jun 14, 2019 · N591JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION STR 43L FR 54+17 INCH IN AFT CARGO COMPARTMENT, REF WO 2019-159/1, WCC 2019-185930. PERFORMED PERMANENT REPAIR AT STR 43L BTW FR 54 TO FR 56 TO AFT CARGO COMPARTMENT IAW SRM 53-00-13. REPAIR IS CATEGORY A AND NO FURTHER AC
- [SDR YENA2019061840326](https://openairdocs.org/sdr/YENA2019061840326.md): Stringer · corroded · Jun 14, 2019 · N591JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION STR 41L AT LEVEL FR 57+7 INCH IN AFT CARGO COMPARTMENT, REF WO 2019-159/1, WCC 2019-185933. PERFORMED PERMANENT REPAIR AT STR 41L BTW FR 57 TO FR 60 IN AFT CARGO COMPARTMENT IAW SRM 53-00-13. REPAIR IS CATEGORY A AND NO FUR
- [SDR YENA2019061840325](https://openairdocs.org/sdr/YENA2019061840325.md): Stringer · corroded · Jun 14, 2019 · N591JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION STR 42L AT LEVEL FR 54+8" AND FR. 56+3" IN AFT CARGO COMPARTMENT, REF WO 2019-159/1, NR 2019-185931 PERFORMED PERMANENT REPAIR AT STR 42L BTW FR 53 TO FR 57 IN AFT CARGO COMPARTMENT IAW A320 SRM 53-00-13. THE REPAIR IS CATEG
- [SDR YENA2018111930779](https://openairdocs.org/sdr/YENA2018111930779.md): Battery Pack · failed · Nov 13, 2018 · N591JB · Airbus A320232 · Emergency Lighting
  > FT # 225, JFK-TPA. EPSU BATTERY 10WL FAILS EMERG. LIGHT SYSTEM TEST; R & R BATTERY 10WL IAW AMM 33-51-38, BATTERY AND SYSTEM OPS CHECKS GOOD.
- [SDR YENA201710210862](https://openairdocs.org/sdr/YENA201710210862.md): Skin · corroded · Oct 21, 2017 · N591JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED THE SKIN FRAMES 69- 70, STRINGERS 31-32R, AROUND THE AFT LAVATORY VENT OUTLET. REPAIRED THE SKIN IAW SRM 53-41-11-300-400. MAJOR REPAIR.
- [SDR YENA201709250788](https://openairdocs.org/sdr/YENA201709250788.md): Battery · discharged · Sep 25, 2017 · N591JB · Airbus A320232 · Emergency Lighting
  > FT 2291, BOS-TPA. EMER LIGHT FAILS TEST. R&R EMERGENCY LIGHT BATTERIES AT 12WL,11WL, AND 13WL BITE AND OPS CKS GOOD IAW AMM 33-51-38.
- [SDR YENA201709250787](https://openairdocs.org/sdr/YENA201709250787.md): Battery Pack · failed · Sep 25, 2017 · N591JB · Airbus A320232 · Emergency Lighting
  > FT # 2291, EMER LIGHT FAILS TEST; R & R EMERGENCY LIGHT BATTERIES AT 12WL,11WL, AND 13WL BITE AND OPS CKS GOOD IAW AMM 33-51-38.
- [SDR YENA201709250786](https://openairdocs.org/sdr/YENA201709250786.md): Battery Pack · no test · Sep 25, 2017 · N591JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT FAILED TO TEST. R & R EMERGENCY LIGHT BATTERIES. BITE AND OPS CHECKED GOOD IAW AMM 33-51-38.
- [SDR YENA201708100656](https://openairdocs.org/sdr/YENA201708100656.md): Outflow Valve · failed · Aug 10, 2017 · N591JB · Airbus A320232 · Air Distribution System
  > FUMES BELIEVED TO COME FROM AVIONICS. VALVE LOCKED IN THE CLOSED POSITION NOT ENOUGH AIR IN AVIONICS COMPARTMENT BEING RECYCLED CAUSING FUMES TO RISE TO CABIN AREA. RETURNED TO DEPARTURE. REPLACED THE VENT AVIONICS OUTLET VALVE AND FILTER, OPS CHECKED OK.
- [SDR YENA201706070469](https://openairdocs.org/sdr/YENA201706070469.md): Reheater · failed · Jun 6, 2017 · N591JB · Airbus A320232 · Air Distribution System
  > TURBINE OIL FUMES\DIRTY SOCK SMELL IN CKPT DURING CLIMB FROM 12,000 FT TO FL250, HP VALVES CLOSED-CL POWER, HIGH FLOW SELECTED WITH NO IMPROVEMENT, A/C IN PRECIP & CLOUDS, APU OFF PRIOR TO TAKE OFF& NO ASSOCIATED FUMES DURING GROUND OPS, DFDR EVENT P/B ACTIVAT
- [SDR YENA201706070468](https://openairdocs.org/sdr/YENA201706070468.md): Filter · failed · Jun 6, 2017 · N591JB · Airbus A320232 · Air Distribution System
  > TURBINE OIL FUMES, AND DIRTY SOCK ODOR IN THE COCKPIT DURING CLIMB FROM 12,000 FT TO FL 250, HP VALVES CLOSED, CL POWER, HIGH FLOW SELECTED WITH NO IMPROVEMENT, ACFT IN PRECIP & CLOUDS, APU OFF PRIOR TO TAKE OFF & NO ASSOCIATED FUMES DURING GROUND OPS, DFDR E
- [SDR YENA20161102966](https://openairdocs.org/sdr/YENA20161102966.md): Line · loose · Nov 2, 2016 · N591JB · Airbus A320232 · Hydraulic System, Main
  > PILOT REPORTED HYD G RSVR LOW LEVEL ECAM MESSAGE. FOLLOWED THE QRH, TURNED OFF THE PTU, ENGINE NR 1 HYRDRAULIC PUMP AND PERFORM A MLG GRAVITY EXTENSION. THE ACFT LANDED WITHOUT INCIDENT. DURING TROUBLESHOOTING, HYD PRESS LINE WAS FOUND TO BE LOOSE. TORQUED
- [SDR YENA20161027960](https://openairdocs.org/sdr/YENA20161027960.md): O-Ring · damaged · Oct 27, 2016 · N591JB · Airbus A320232 · Hydraulic System, Main
  > PILOT REPORTED VERY STRONG DIRTY SOCK ODOR ON DESCEND AND DURING TAXI IN; FOUNG HYDRAULIC FITTING ON GREEN PTU MODULE IN WHEELWELL LEAKING INTO BELLY OF KEEL BEAM AND MIGRATING TO APU INLET. REPLACED O RING FOR FITTING. CLEANED OUT ALL RESIDUAL FLUID IN KEEL A
- [SDR YENA20160927873](https://openairdocs.org/sdr/YENA20160927873.md): Filter · odor · Sep 27, 2016 · N591JB · Airbus A320232 · Cabin Cooling System
  > FT 422, FLIGHT CREW REPORTED A FOUL ODOR DURING DESCENT. R & R THE NR 2 A/C PACK OZONE FILTER IAW AMM 21-51-41. OPS AND LEAK CHECKED GOOD.
- [SDR YENA20150317050](https://openairdocs.org/sdr/YENA20150317050.md): Flap System · locked · Mar 17, 2015 · N591JB · Airbus A320232 · Trailing Edge Flap Control System
  > CREW DECLARED AN EMERGENCY ON LANDING. F/CTRL FLAPS LOCKED AFTER TAKEOFF, NEVER MOVED FLAP HANDLE. PERFORMED VISUAL INSPECTION ON FLAPS, NO DAMAGE FOUND. ACCOMPLISHED RESET OF THE WING TIP BRAKE, WTB, FLAP SYSTEM ON THE GROUND IAW AMM 27-50-00-869-006-A. NO
- [SDR YENA20141017219](https://openairdocs.org/sdr/YENA20141017219.md): Pickup · failed · Oct 17, 2014 · N591JB · Airbus A320232 · Trailing Edge Flap Control System
  > DURING APPROACH AND SELECTING FLAPS TO 2 DEGREES WITH SPEED BRAKES OUT, RECEIVED F/CTL FLAPS LOCKED WING TIP ON ECAM. COMPLETED ECAM ACTION AND LANDED UNEVENTUALLY. R & R ASYMMETRY POSITION PICK OFF UNIT ON THE LT SIDE, IAW AMM 27-51-18. OPS CHECK, FLAPS GOO
- [SDR YENA20140831173](https://openairdocs.org/sdr/YENA20140831173.md): Seal · leaking · Aug 31, 2014 · N591JB · Airbus A320232 · Cabin Cooling System
  > DIVERTED, PACK NR 2 UNABLE TO MAINTAIN CABIN TEMPERATURE IN FLIGHT AND ON THE GROUND. TROUBLESHOT AND FOUND SLEEVE AND SEALS DISLODGED ON NR 2 ACM. REPLACED SEALS AND REINSTALLED SLEEVE IAW AMM 21-52-21. NR 2 PACK LEAKS CHECK GOOD IAW AMM 21-52-00.
- [SDR YENA20140531105](https://openairdocs.org/sdr/YENA20140531105.md): Switch · failed · May 31, 2014 · N591JB · Airbus A320232 · Emergency Lighting
  > THE CREW REPORTED DURING DESCENT, EMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTING ALL CAME ON. RESET THE EMERGENCY LIGHTS FROM THE COCKPIT UNSUCCESSFUL. R & R BAD EMERGENCY EXIT LIGHT SWITCH IAW TSM 33-51-00-810-881-A. OPS CHECKED GOOD. NO FURTHER DEFECTS N
- [SDR YENA20130828193](https://openairdocs.org/sdr/YENA20130828193.md): Coffeemaker · odor · Aug 28, 2013 · N591JB · Airbus A320232 · Buffet/Galleys
  > BURNING ODOR DISCOVERED ENROUTE, COMING FROM FRONT COFFEEMAKERS. CIRCUIT BREAKERS PULLED. COFFEEMAKER WAS REMOVED AND REPLACED IAW AMM 25-35-15. OPS CHECKED OK.
- [SDR YENA20130729164](https://openairdocs.org/sdr/YENA20130729164.md): Servo Control · failed · Jul 29, 2013 · N591JB · Airbus A320232 · Landing Gear Steering System
  > CREW REPORTED NOSE WHEEL STEERING FAULT AFTER LANDING AND UNABLE TO RESET. ACCOMPLISHED TROUBLESHOOTING IAW TSM 32-51-00-810. R & R NOSE WHEEL STEERING SERVO CONTROL IAW AMM 32-51-51.
- [SDR YENA20130529115](https://openairdocs.org/sdr/YENA20130529115.md): Epsu · failed · May 29, 2013 · N591JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE, RIGHT EPSU BATTERY FAULTED DURING LIGHT TEST. REPLACED RIGHT EMERGENCY ROW EPSU BATTERY IAW 33-51-38, OPS CHECKED NORMAL.
- [SDR YENA20100811112](https://openairdocs.org/sdr/YENA20100811112.md): Fcu · failed · Aug 11, 2010 · N591JB · Airbus A320232 · Flight Controller
  > FLT 271 LAS-BUR, CREW REPORTED UNCOMMANDED RUDDER DEFLECT OF 1 DEGREE AT 8K FEET NAV/AP ON. NO LOSS OF CONTROL ON AIRCRAFT. REMOVED AND REPLACED FCU PER AMM 22-81-12-04. OPS CHECK GOOD. NO FAULTS PRESENT A/P 1&2.

Next page: https://openairdocs.org/aircraft/N591JB/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 = 'N591JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N591JB/reports

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