N589JB
Service difficulty reports · 53
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 = 'N589JB' 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 = 'N589JB' 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 YENA2024112201492Unknown · odorFLT#779, JFK-MBJ. CREW INFLIGHT AND FLIGHT NOTICED PUNGENT DIRTY SOCKS FUMES IN THE DESCENT CAUSING ORAL AND THROAT IRRITATION PERSISTENT; C/W NOTICE 2017 -J015 SECTION A . ISOLATED ODOR FAULT . IDENTIFIED AND DETERMINED TO BE AN AMBIENT SMELL. T/C PERFORMED PSDR YENA2024090301222Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE H1(UPPER INBOARD POSITION) ON DOOR STOP FITTING 7 FR 16 LH SIDE. CRACK DIRECTION 5 OCLOCK D1-D2+0.120 INCHES; (RESOLVED ON W/O: 1311036 TASKCARD: NR-00013) EVALUATED CRACK ON FRAME 16 LH SIDE, DOOR SDR YENA2024090301221Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION. CRACK DIRECTION IS 5 OCLOCK, CRACK DEPTH IS 0.114 INCH APPROX. AT FWD GALLER AREA; (RESOLVED ON W/O: 1311036 TASKCARD: NR-00020) REMOVED ANSDR YENA2024090301220Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK FOUND IN OPEN HOLE H3 (LOWER INBOARD LOCATION) ON DOOR STOP 7 FR16 RH SIDE, CRACK DIRECTION 6 OCLOCK, D1-D2+0.065 INCH; (RESOLVED ON W/O: 1311036 TASKCARD: NR-00029) REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS ON FRAMSDR YENA2024090301219Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR66 LH DOOR STOP FITTING Ñ1 AREA AT LOWER I NB HOLE. CRACK DIRECTION 5 OCLOCK VIEW LOOKING FWD. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1311036 TASKCARD: NR-00036) FUR-A320-53-01648, REF AEROMAN N/R 2024-4582SDR YENA2024090301218Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR66 LH DOOR STOP FITTING Ñ1 AREA AT LOWER I NB HOLE. CRACK DIRECTION 5 OCLOCK VIEW LOOKING FWD. CRACK D= 0.170 INCH; REF AEROMAN N/R 2024- 458267, PERFORMED REPAIR ON FR66 LH DOOR STOP FITTING #1 AREA AT AFTSDR YENA2024090301217Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE B FRAME 16 R/H SIDE AND CONFIRM INDICATION USING BOROSCOPE VIEW AS PER REF NTM 51-90-00; REF AEROMAN N/R 2024-458273, PERFORMED REPAIR HOLE B ON FRAME LAYER LOC ON DOUBLE JUGGLE AREA FRAME SDR YENA2024090301216Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 RH DOOR STOP FITTING Ñ1 AREA AT LOWER I NB HOLE. CRACK DIRECTION 6 OCLOCK VIEW LOOKING AFT. CRACK D= 0.155 INCH; REF AEROMAN 2024-458266, PERFORM REPAIR OF THE LWR INB HOLE CRACK ON THE DOOR STOP FITTINGSDR YENA2024090301215Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH DOOR STOP FITTING Ñ1 AREA AT UPPER I NB HOLE. CRACK DIRECTION 6 AND 11 OCLOCK VIEW LOOKING AFT. CRACK D= 0. 165 INCH; REF AEROMAN N/R 2024- 458268, ACCOMPLISHED REPAIR OF CRACK FOUND ON DOOR STOP FITTSDR YENA2024090301214Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH DOOR STOP FITTING Ñ1 AREA AT LOWER I NB HOLE. CRACK DIRECTION 6 AND 1 OCLOCK VIEW LOOKING AFT. CRACK D= 0.1 65 INCH; REF AEREOMAN N/R 2024- 458269, ACCOMPLISHED REPAIR OF CRACK FOUND ON DOOR STOP FITTSDR YENA2024090301213Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH DOOR STOP FITTING Ñ1 AREA AT LOWER O B HOLE. CRACK DIRECTION 6 AND 12 OCLOCK VIEW LOOKING AFT. CRACK D= 0.1 65 INCH; REF AEROMAN N/R 2024- 458270, ACCOMPLISHED REPAIR OF CRACK FOUND ON DOOR STOP FITTISDR YENA2024090301212Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TOP SKIN UPPER SURFACE RIB 20 LEADING EDGE RH WING; REF AEROMAN NR 2024-448430 WO 2024 262/1 ACCOMPLISHED THE REPAIR OF THE CORROSION ON THE RH WING TOP SKIN PANEL 2 UPPER SURFACE, FRONT SPAR LEVEL AND BETWEEN RIBS 19-20 BONSDR YENA2024090301211Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TOP SKIN UPPER SURFACE OVERHAND LOC RIB 17 RH WING; REF AEROMAN NR 2024-448504 WO 2024 262/1 ACCOMPLISH THE REPAIR OF THE CORROSION ON THE RH WING TOP SKIN PANEL 2 UPPER SURFACE, FRONT SPAR LEVEL AND BETWEEN RIBS 19-20 BONDISDR YENA2024090301210Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH / DOOR STOP FITTING #1 / HOLE LWR INB / CRACK - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-9027-24 (COVER + PART 1) /2/ DOSSIER 81437902 /3/ AIRBUS RDAF 81437902/003/2024#A DESCRIPTION: DURING CURRSDR YENA2024090301209Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / UPPER SURFACE / FRONT SPAR & RIBS 19-20 / BONDING SPIGOT /CORROSION DAMAGE – PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-9051-24 REV. 0 (COVER + PARTS 1-2) /2/ AIRBUS MESSAGE 81443224/008 /3/ ASDR YENA2024090301208Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH / DOOR STOP FITTING #1 / CRACK DAMAGE - TIME-LIMITED REPAIR, A CRACK WAS FOUND ON DOOR STOP FITTING #1 AT FR68 AT THE L2 DOOR. 3 HOLES WERE AFFECTED TO THE FRAME LAYER. CRACKED HOLES WERE REAMED TOSDR YENA2024020800251Cabin Pressure · faultedFLT#426, TPA-JFK. (AIRCRAFT PERFORMED AN AIR TURN BACK TO TPA). 'ON CLIMB OUT V/S INDICATED EXCESSIVE CABIN CLIMB. CABIN ALTITUDE STARTED TO CLIMB ABOVE NORMAL LIMITS. APOUND 18,000 FT RECIEVED EXCESSIVE CABIN ALTITUDE ECAM WARNING. EXECUTED EMERGANCY DESCENT SDR YENA2023122001599Unknown · unknownFLT#1975, JFK-YVR. 'DURING FLIGHT CABIN CREW REPORT A BURNING ODOR FROM SEAT ROW 7 TO 13 MID CABIN. THE LTV SYSTEM WAS DEACTIVATED PER QPH PROCEDURE. AFTER THAT ODOR DISSIPATED ( THALES AVANT IFE (ENTIRE SYSTEM) )." (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR YENA2023005020498Light · failedFLT#2534, PBI-DCA. 'DURING EMERGENCY LIGHT CK OF WEEKLY, FOUND FWD GALLEYS LIGHT - INOP; REMOVED AND REPLACED FWD EPSU BATTERY PACK IAW AMM 33-51-38. OPS CHECKS GOOD.'SDR YENA2022091900926None · failedFLT#41, FLL-MDE. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' IN-FLIGHT FMGC 1 FAILED AND BLANKED CAUSING AP1 TO TRIP. CAME BACK AND THEN FAILED WITH 2FD2 DISPLAYED ON PFD PATCH WITH DISPATCH AND MTC MADE JOINT DECISION TO RETURN TO FLL; REMOVED AND REPLACEDSDR YENA2022090900884None · noneFLT#2119, ORH-FLL. 'DIRTYSOCK SMELL REAR CABIN LANDING & FRONT; "COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810-085-B/ TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR SERVICE.'SDR YENA2022060600552Actuator · failedFLT#1327, FLL-MBJ. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' ENG 2 COMPRESSOR VANE IN FLIGHT AND AFTER LANDING. DID NOT LAND OVERWEIGHT (145,200 #); REMOVED AND REPLACED 2.5 ACTUATOR R/H ENGIN.E IDLE LEAK CHECK OK AMM 75-31-42. SEE DEFECT 3371893-2 (PERFOSDR YENA2022051300465None · noneFLT#819, JFK-ATL. 'BELOW 10,000 CABIN ODOR / FUME DIRTY SOCK SMELL ( APU SYSTEM ); PERFORMED APU CLEANING PROCEDURE AND INSP APU AREA FOR LEAKS. GAINED ACCESS TO APU BLEED AIR DUCT AND BORESCOPE WAS PERFORMED. NO CONTAMINANTS WERE NOTED. OPERATED APU PER AMM 4SDR YENA2022031600229Door · false indicationFLT#2312, CUN-SMF. 'DOOR 2L ON ECAM SHOWING DOOR SLIDE ARMED ERRONEOULY (SLIDE INDICATIONS ON ECAM - PAX DOOR ARMED IND); PERFORMED OPS TEST OF LS DOOR AMM 52-10-00 NO FAULTS FOUND AT TIME OF INSPECTION MDDR CLEARED MX-4UPDATED PLACARD REMOVED.'SDR YENA2021042700284Ecs · contaminatedFLT 512, AUS-FLL. STRONG DIRTY SOCK ODOR FROM PACKS WHEN ON APU BLEED OR ENGINE BLEED. *REPEAT WRITE UP. (4-10-21); INSP APU COMP & FOUND MINOR OIL SATURATION AT INLET SEAL AND PLENUM SEAL. CLEANED APU COMP PER 49-00-00. INSP ENG 1 & 2 AND FOUND NO LEAKS. INSPSDR YENA2020122100625Epsu · failedDURING HEAVY MAINTENANCE, INOPERABLE EPSU, EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN. R & R EMERGENCY POWER SUPPLY UNIT EPSU FIN (12WL), IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. PERFORMED OPERATIONAL CHECK OF THE EPSU, IAW AMM 33-51-0SDR YENA2020122100624Slide · faultedDURING HEAVY MAINTENANCE, EPSU EXTERNAL LOAD FAULT INDICATION ON EPSU 10WL IN FWD CABIN, REF AEROMON NR 2020-359485 W/O 2020 160/1. PERFORMED TSM FAULT ISOLATION ON EPSU EXTERIOR LIGHTS FAULT INDICATION IN EPSU 10WL, IAW TSM 33-51-00-810-808-A STEP 4B (2)(C).SDR YENA2020122100623Power Supply · no testDURING HEAVY MAINTENANCE, REF N/R 2020-359482 W/O 2020 160/1, INOPERABLE EPSU-EMERGENCY POWER SUPPLY UNIT 11WL IN PASSENGER CABIN. R & R EMERGENCY POWER SUPPLY UNIT EPSU FIN (11WL), IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. PERFORMED OPERATIONAL SDR YENA2020122100622Door Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON EMERGENCY EXIT DOOR 833, INNER FRAME SEGMENT 1, IN PASSENGER CABIN, REF AEROMAN NR 2020-359259 W/O 2020 160/1. ACCOMPLISHED TASK CARD A320-52-1144-03 DOORS EMERGENCY EXIT OVERWING EMERGENCY EXIT HATCH (FWD LT EEH)SDR YENA2020122100621Door Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON EMERGENCY EXIT DOOR 843 INNER FRAME SEGMENT 1, IN PASSENGER CABIN, REF AEROMAN NR 2020-359258 W/O 2020 160/1. ACCOMPLISHED TASK CARD A320-52-1144-02 DOORS EMERGENCY EXIT OVERWING EMERGENCY EXIT HATCH (FWD RT EEH) SDR YENA2020122100620Door Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON EMERGENCY EXIT DOOR 844, INNER FRAME SEGMENT 1, IN PASSENGER CABIN, REF AEROMAN NR 2020-359260 W/O 2020 160/1. ACCOMPLISHED TASK CARD A320-52-1144-04 DOORS EMERGENCY EXIT OVERWING EMERGENCY EXIT HATCH (AFT RT EEH)SDR YENA2020122100619Door Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON EMERGENCY EXIT DOOR 834 INNER FRAME SEGMENT 1 IN PASSENGER CABIN, REF AEROMAN NR 2020-359260 W/O 2020 160/1. ACCOMPLISHED TASK CARD A320-52-1144-03 DOORS, EMERGENCY EXIT, OVERWING EXIT HATCH (AFT RT EEH) FRAME. RSDR YENA2020122100618Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION LOWER SILL FR 66RT AFT GALLEY AREA (CPCP RELATED 534147-01). REMOVED AND REPLACED LOWER SILL LOCATED ON RT SIDE AT LEVEL OF STR 23R BETWEEN FR 66 TO FR 68, IAW A320 SRM 51-72-11 AND DWG NR D53480505. WORK STEPS PERFORMED SDR YENA2020062800381Sensor · failedFLT 647, RETURNED TO FIELD. ON CLIMB OUT, AP 1 ENGAGED FL 280, ACFT PITCHED DOWN, SAT & TAT SHOWED EXTREME NEG NUMBERS. DISENGAGED AP, LEVELED AT FL 320. SAT & TAT AMBER XX. DURING DESCENT, FO WOULDN`T FOLLOW PROFILE AGAIN, EXTREME NEG SAT NOTED. CHECKED TATSDR YENA2020062600379Fcu · failedFLT 533, BDL-TPA. EXPERIENCED TWO UNCOMMANDED PITCH DOWNS DURING CLIMB ON AP1. DISCONNECTED AP BOTH TIMES TO RECOVER. TAT, SAT & ISA ALL SHOWED -80C DURING EVENT THEN WENT BACK TO NORMAL. AT TIMES DURING CRUSE AT FL340 TAT AND SAT SHOWED AMBER X'S THE FIRSSDR YENA2019060620301Battery · failedFT 225, DURING EMERGENCY CABIN BITE TEST, BATTERY FAULT. FOUND THE BATTERY FAULT AT 10WL & 13WL. REMOVED AND REPLACED ESPU BATTERY AT 10WL & 13WL IAW AMM 33-51-38. CHECKED GOOD.SDR YENA2019060620300Battery · failedFT 225, DURING EMERGENCY CABIN BITE TEST, BATT FAULT. FOUND BATTERY FAULT AT 10WL & 13WL. REMOVED AND REPLACED ESPU BATTERY AT 10WL & 13WL IAW AMM 33-51-38. CHECKED GOOD.SDR YENA2019041730198Light · detachedFT # 668, PSE-MCO. EMERGENCY EXIT LIGHT NEAR FLOOR AND BETWEEN L1 DOOR AND FWD FA JUMPSEAT HAS DETACHED FROM WALL; ATTACHED LIGHT MOUNT PLATE TO PANEL AMM 25-00-00. SECURED EMERGENCY LIGHT ASST IAW AMM 33-51-00, OPS OK.SDR YENA201708170666Unknown · odorAT FL 350, DURING CRUISE, APPROXIMATELY 42 MIN INTO FLIGHT, A DISTINCT ODOR PERSISTED WHILE IN CRUISE, SMELLED LIKE DIRTY LAUNDRY. STRONG IN COCKPIT. CABIN REPORTED NO ODOR. ACCOMPLISHED TSM 05-50-00-810-831-A. RAN APU AND ENGINES AND PACKS. ENGINES AT HISDR YENA20161004898Battery Pack · inoperativeAFT EMERGENCY LIGHTING FAULTED DURING CIDS EMERGENCY TEST. R & R THE BATTERY PACK 13WL IAW AMM 33-51-38, TEST PASS, OPS CHECKED GOOD.SDR YENA20150107001Fairing · unsecureAIR RETURN TO DEPARTURE DUE TO A VIBRATION DURING CLIMB. FOUND SPEED TAPE PARTIALLY OFF FROM WTB PANEL 191BT. APPLIED NEW SPEED TAPE IAW SRM 53-35-00.SDR YENA20130714146Transducer · failedCREW DECLARED AN EMERGENCY AFTER LANDING GEAR EXTENSION DUE TO ECAM BRAKES /A-SKID/NWS FAULT. ACCOMPLISHED TROUBLESHOOTING IAW TSM 32-42-00, AND FOUND BRAKE PRESSURE TRANSDUCER FAULTING BSCU. R & R BRAKE PRESSURE TRANSDUCER IAW AMM 32-42-00. ACCOMPLISHED NORSDR YENA20130224050Battery · failedFLT 866 PUJ-JFK, DURING MAINTENANCE LEFT AFT EPSU FAILED BATTERY CAPACITY TEST. REMOVED AND REPLACED BATTERY FOR THE LEFT EPSU AFT POSITION. OPS CHECK NORMAL PER AMM 33-50-00.SDR YENA20120714557Battery · failedFLT 654 SJU-TPA, DURING MAINTENANCE THE RIGHT EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED BATTERY FOR RIGHT EPSU IAM AMM 33-51-38. OPS CHECK GOOD.SDR YENA20120428487Release Cable · faultyFLT 6407 JFK-LCQ, ON HEAVY MAINTENANCE CHECK FOUND RT SIDE OPERATIONAL TEST OF EMERGENCY EXIT HATCHES FAILED TRAVEL REQUIREMENTS. RIGHT SIDE SLIDE RELEASE FLEX CABLE FOR EMERGENCY EXIT HATCH REPLACED. RIGGED AND OPS CHECK PER A320-53-1227-02, NO FURTHER ACTISDR YENA20110613272Control Unit · bindingFLT 139 BUF-JFK, THE FLIGHT CREW EXECUTED A GO AROUND AT 2000 FEET DUE TO FLAP HANDLE BINDING FROM POSITION 1 TO POSITION 2. THE F/O WAS ABLE TO RECOVER OPERATION OF THE JAMMED HANDLE. TECHNICIAN REPLACED FLAP CONTROL UNIT ASSY AS PER AMM 27-51-43-04. ALL OSDR YENA20110203191Cooling Fan · failedFLT 1783 MCO-BOG, A/C DIVERTED TO KIN - THE CREW DECLARED EMERGENCY DUE TO AFT AVIONICS BAY ALARM CAME ON. THERE WAS NO SIGN OF SMOKE EITHER IN CABIN OR IN COCKPIT. PERFORMED A VISUAL INSPECTION OF AFT AVIONICS BAY FOR EVIDENCE OF SMOKE/FIRE NO DEFECTS NOTEDSDR YENA20100605077Epsu · failedFLT 526 MCO-EWR ON GROUND MAINTENANCE CHECK - RT EPSU (EMERGENCY POWER SUPPLY UNIT) FAILED OPERATION CHECK ON EMERGENCY LIGHTS SYSTEM. REMOVED AND REPLACED RT EMER EPSU IAW AMM 33-51-38. OPS TEST GOOD.SDR YENA20100328045Module · intermittentFLT JB477 BOS-OAK AIRCRAFT HAD 3 UNCOMMANDED PITCH DOWNS WITH LOSS OF 100 FT NO ASSOCIATED ECAMS/FLIGHT CONTROL FAULTS. AIRCRAFT WAS AT CRUISE AT FL360/.78MACH WITH AUTO PILOT 2 ENGAGED STRAIGHT AND LEVEL IN SMOOTH AIR, MANUAL THS PITCH TRIM WHEEL MOVED RAPIDSDR YENA2007019A/C Pack · odorAPRX 1645Z, NO VISIBLE SMOKE (BURNING RUBBER SMELL) DURING APPROACH QRH COMPLIED WITH MID CABIN. EMERGENCY DECLARED. SMELL SUBSIDED UPON EXITING TAXIWAY. EVACUATION WAS DEEMED NOT REQUIRED. PERFORMED TROUBLESHOOTING IAW TSM 24-00-00-810-823 AND TSM 23-39-00-81
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