N591JB
Service difficulty reports · 51
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 = 'N591JB' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR YENA2025052000525Frame · crackedDURING 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 ESDR YENA2025052000524Frame · crackedDURING 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 YENA2025052000523Frame · crackedDURING 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 UPSDR YENA2025052000522Frame · crackedDURING 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 APSDR YENA2025052000521Skin · corrodedDURING 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 TSDR YENA2025052000520Power Supply · no testDURING 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 YENA2025052000519Stop Fitting · crackedDURING 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: ONSDR YENA2025052000518Attach Angle · crackedDURING 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 YENA2025052000517Skin · damagedDURING 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 8SDR YENA2025052000516Firewall · damagedDURING 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 YENA2025052000515Skin · corrodedDURING 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 YENA2025052000514Stringer · corrodedDURING 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 YENA2025052000513Stringer · corrodedDURING 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 YENA2025052000512Stringer · corrodedDURING 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 YENA2025052000511Stringer · corrodedDURING 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 CSDR YENA2025052000510Floor Support · corrodedDURING 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 YENA2024082601166Unknown · odorFLT#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 YENA2024011800069Oxygen Bottle · failedFLT#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 IAWSDR YENA2023080300892Unknown · unknownFLT#268, PUJ-JFK. (AIRCRAFT DIVERTED TO FLL) 'DURING CRUISE ECAM SEC1 FAULT.' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR YENA2023012300071Shear Pin · not reportedFLT#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 YENA2022011900030Connector · looseFLT # 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 1SDR YENA2021112900789Apu · fault messageFLT 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 OSDR YENA201912241708Fan · failedFLT 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 YENA201907130404Battery · dischargedFLT 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 YENA201907130403Battery · dischargedFLT 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 YENA201907130402Battery · dischargedFLT 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 YENA2019062480338Connector · brokenCONNECTOR 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 YENA2019061840329Power Supply · no testDURING 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 YENA2019061840327Stringer · corrodedDURING 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 ACSDR YENA2019061840326Stringer · corrodedDURING 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 FURSDR YENA2019061840325Stringer · corrodedDURING 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 CATEGSDR YENA2018111930779Battery Pack · failedFT # 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 YENA201710210862Skin · corrodedDURING 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 YENA201709250788Battery · dischargedFT 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 YENA201709250787Battery Pack · failedFT # 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 YENA201709250786Battery Pack · no testEMERGENCY LIGHT FAILED TO TEST. R & R EMERGENCY LIGHT BATTERIES. BITE AND OPS CHECKED GOOD IAW AMM 33-51-38.SDR YENA201708100656Outflow Valve · failedFUMES 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 YENA201706070469Reheater · failedTURBINE 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 ACTIVATSDR YENA201706070468Filter · failedTURBINE 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 ESDR YENA20161102966Line · loosePILOT 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. TORQUEDSDR YENA20161027960O-Ring · damagedPILOT 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 ASDR YENA20160927873Filter · odorFT 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 YENA20150317050Flap System · lockedCREW 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 YENA20141017219Pickup · failedDURING 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 GOOSDR YENA20140831173Seal · leakingDIVERTED, 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 YENA20140531105Switch · failedTHE 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 NSDR YENA20130828193Coffeemaker · odorBURNING ODOR DISCOVERED ENROUTE, COMING FROM FRONT COFFEEMAKERS. CIRCUIT BREAKERS PULLED. COFFEEMAKER WAS REMOVED AND REPLACED IAW AMM 25-35-15. OPS CHECKED OK.SDR YENA20130729164Servo Control · failedCREW 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 YENA20130529115Epsu · failedDURING MAINTENANCE, RIGHT EPSU BATTERY FAULTED DURING LIGHT TEST. REPLACED RIGHT EMERGENCY ROW EPSU BATTERY IAW 33-51-38, OPS CHECKED NORMAL.SDR YENA20100811112Fcu · failedFLT 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.
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