N613JB
Service difficulty reports · 96
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 = 'N613JB' 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 = 'N613JB' 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 YENA2026080300642Apu · odorFLT 1098, MCO-BOS (AIRTURN BACK). DIRTY SOCK ODOR IN CABIN AND FLIGHT DECK, APU BLEED HAD BEEN ON FOR APPROX 10 MINS, ODOR BEGAN APPROX 5 MIN AFTER RAIN STARTED, ( APU BLEED AIR SUPPLY SYSTEM ) FUME EVENT COCKPIT & AFT CABIN TRIED ISOLATION CHECKLIST BUT COUSDR YENA20260210001Skin · corrodedDURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - ASDR YENA2026021100194Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 14 INCHES BELOW LH SIDE STRI NGER AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00006) REF AE WO # 2025-414/1 NR # 2025-717347 EVALUATED DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 1SDR YENA2026021100193Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR40L AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00007) REF AE WO # 2025-414/1 NR # 2025-717348 EVALUATED DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR4SDR YENA2026021100192Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR70 TO FR71 BTW STR31R TO STR32R AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00008) REF AE WO # 2025-414/1 NR # 2025-717299 PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOT FOUND DENT ONLY SDR YENA2026021100191Skin · dentedDURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00009) REF AEROMAN WO # 2025=414/1 NR # 2025-717302 EVALUATED DENT ON EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE AND FOUND WITHIN LIMITS I.A.W A320 SRSDR YENA2026021100190Skin · bulgedDURING HEAVY MAINTENANCE: BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19L TO STR20L ON UPPER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00010) REF AEROMAN WO # 2025-414/1 NR # 2025-717282 EVALUATED BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19LSDR YENA2026021100189Skin · dentedDURING HEAVY MAINTENANCE: DENT SKIN LOCATED LOWER AREA DOOR R2 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00011) REF AEROMAN WO # 2025-414/1 NR# 2025-717349 EVALUATED DENTS LOCATED LOWER SKIN AREA DOOR R2 AT LOWER FUSELAGE AND FOUND WITHIN LIMITSDR YENA2026021100188Frame · crackedDURING HEAVY MAINTENANCE: CRACK NDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 8, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.120INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/O:SDR YENA2026021100187Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE A, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.110 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/SDR YENA2026021100186Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 20 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 6, CRACK DIRECTION AT 11 O CLOCK LOOKING INBOARD, D=0.125 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON SDR YENA2026021100185Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.105 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00038SDR YENA2026021100184Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 5 POSITION, CRACK DIRECTION IS 7 OCLOCK, CRACK DEPTH IS 0.090 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00039SDR YENA2026021100183Skin · deformedDURING HEAVY MAINTENANCE: DEFORMATION LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE; REF AEROMAN N/R 2025-717439, PERFORMED PERMANENT REPAIR LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE, THIS REPAIR IS CATEGORY A,SDR YENA2026021100182Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1425349 TASKCARD: SDR YENA2026021100181Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 2 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCSDR YENA2026021100180Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 3 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCSDR YENA2026021100179Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, AT AFT GALLEY AREA ( 1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00045) REF AE WO # 2025-414/1 NR # 2025-717399 PESDR YENA2026021100178Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, TRANSVERSAL FLANGE ARE A FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00046) REF AE WO # 2025-414SDR YENA2026021100177Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, CRACK DEPTH IS 0.115 INCH, AT AFT GALLEY AREA (2 EA); REF AEROMAN N/R 2025-717397, ACCOMPSDR YENA2026021100176Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA RH SIDE. CRACK L= 0.109 INCH. CRACK DIRECTION 11 O CLOCK; REF AEROMAN N/R 2025-717306, ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMISDR YENA2026021100175Window Frame · crackedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVESDR YENA2026021100174Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVESDR YENA2026021100173Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE AT LEVEL RIB 8 TO RIB 9 TRAILING EDGE ON RH WNG; REF AEROMAN WO 2025-414/1 NR # 2025-716950 ACCOMPLISHED REPAIR OF CORROSION DAMAGE AT RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB7-RIB9 I.A.W EA 57-0135-2SDR YENA2026021100172Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER AREA BTW RIB8 TO RIB 9 ON RH WING; REF AEROMAN WO # 2025-414/1 NR # 2025-717170 PERFORMED PERMANENT REPAIR ON TRAILING EDGE UPPER SKIN LOWER AREA ON RIB 8 RH WING IAW EA # 57-0135-25 (COVER ANDSDR YENA2026021100171Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING; REF AEROMAN WO #2025-414/1 NR # 2025-717174, PERFORMED PERMANENT REPAIR ON TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING IAW EA 57-0135 -25 (COVER PARTSDR YENA2026021100170Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE/ REAR FUSELAGE/ FR68 RH DOOR STOP FITTING #1/ CRACK/ PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0101-25 (COVER, PART 1+2) /2/ AIRBUS DOSSIER 81714674 /3/ AIRBUS RDAF 81714674/003/2025#A /4/ A320 SRM 53-41-12-300-011. DESSDR YENA2026021100169Skin · corrodedDURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - ASDR YENA2026021100168Window Frame · crackedDURING HEAVY MAINTENANCE, WINDSHIELD FRAME CENTER POST, LOWER NODE AREA CRACKED. REFERENCE: EA 53-0097-25, SB A320-53-1331, RDAF 81709993/003/2025 A, MESSAGE 81709993/010, REPAIR INSTRUCTION R53113430, ISSUE G, REPAIR INSTRUCTION R53112919 ISSUE K, REPSDR YENA2025032400301Thermostat · failedFLT#2121, FLL-LAX. (AIRCRAFT DECLARED AN EMERGENCY).' ON CLIMB OUT 2 TIMES AIR ENG 1 BLEED ABNORMAL MSG CLEARED ITSELF 3RD TIME WE COMPLIED WITH QRH TAKEOFF WAS A TOGA BLEEDS OFF AND PSI WAS 22 / 215 C. ENG ONE #1 . WHEN WE STARTED GETTING THE BLEED ABNORMAL MSDR YENA2025032400300Hydraulic System · lowFLT#2121, FLL-LAX. (AIRCRAFT DECLARED AN EMERGENCY).' APPROX 3 HOURS INTO FLIGHT PERFORMING SYSTEMS CHECKS. THE HYD STATUS PAGE SHOWED AMBER LINE FROM GREEN SYSTEM RESERVOIR TO GREEN ENG PUMP AND RESERVOIR INDICATOR WAS AMBER 3000 GREEN; ACCOMPLISHED VISUAL ISDR YENA2025031900274Pump · faultedFLT#2096, CUN-FLL. (AIRCRAFT DECLARED AN EMERGENCY INTO FLL) 'HYD G RSVR LO LVL ECAM MSG. EMG 1 PUMP AND PTU OFF ACCORDING TO ECAM.' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR YENA2025021000140Unknown · odorFLT#667, HPN-PBI. 'OBVIOUS OIL FUMES ODOR IN FLT DECK AND FRONT OF A/C TURNED PACK 1 OFF. STILL BAD SEVERAL MINUTES LATER. OPENSDR YENA2025012200094Bleed Air Sys · odorFLT#743, JFK-AUA. 'DIRTY SOCK SMELL REPORTED BY FLIGHT ATTENDANT FROM MID TO AFT CABIN ( APU BLEED AIR SUPPLY SYSTEM ); REF LP # 4219340, ITEM 2 OR WO # 1387703 TSI . THIS CLEARS THIS MDDR. MDDR CLEARED. MX-4 UPDATED. PLACARD RMVD. MCC NOTIFIED.'SDR YENA2024101801371Filter · odorFLT#791, BOS-TPA.' ODOR SMELL IN CABIN AT ROW 3 & 4 . APU BLEED ON; COMPLIED WITH INFO NOTICE 2017-T015 SECTION A. ISOLATED FAULT TO TYPE 10 AMBIENT AIR ODOR PER TSM 05-50-00-810-085-B/ TSM 05-50-00-810-085-D. A/C IS OK FOR SERVICE. REMOVED & REPLACED RECIRC. SDR YENA2024020800250Engine · stalledFLT#1510, PAP-FLL. (AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO SDQ). 'ENG 2 FAIL/STALL ON CLIMB OUT.' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR YENA2023082100962Safety Valve · failedFLT#2276, MCO-PVD. (AIRCRAFT PERFORMED AN AIR TURN BACK) ' GREEN HYDRAULIC FAILURE CLIMBING THRU 4,000 MANUAL GEAR EXTENSION NORMAL LANDING; FOUND L/G SAFETY VALVE DETACHED FROM MANIFOLD AND LEAKING. REF L/P 3755398, ITEMS 1 (INSTALLED NEW L/G SAFETY VALVE (49SDR YENA2023011200034Door · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 833 (FWD LH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022 287/1 NR 2002-679963. PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 833 IAW EC A320-52-1144 TASK CARD A320-52-1144-01 DOORS / EMERGSDR YENA2023011200033Door · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 (FWD RH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022 287/1 NR 2022 - 679964. PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 843 IAW EC A320-52 1144 TASK CARD A320-52-1144-02 DOORS / EMERSDR YENA2023011200032Door · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 (AFT LH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022-287/1 NR2022-679965. PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 834 IAW EC A320-52-1144 TASK CARD A320-52-1144-03 DOORS / EMERGSDR YENA2023011200031Door · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 (AFT RH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022-287/1 NR2022-679966 PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 844 IAW EC A320-52-1144 TASK CARD A320-52-1144-04 DOORS / EMERGENCSDR YENA2022080300743Drive Unit · failedFLT#2603, EWR- TPA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) WEATHER RADAR FAILURE ON CLIMB OUT; REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-41-33. DUE TO BITE TEST FAILURE. REF LOG PAGE 3476359, ITEM 1 (REMOVED AND REPLACED WX RADAR ANTENNA & DRISDR YENA2022080300742Transceiver · failedFLT#2603, EWR- TPA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) WEATHER RADAR FAILURE ON CLIMB OUT; REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-41-33. DUE TO BITE TEST FAILURE. REF LOG PAGE 3476359, ITEM 1 (REMOVED AND REPLACED WX RADAR ANTENNA & DRISDR YENA2022071800673Bleed Air Sys · odorFLT#153, DEN-LGA. ' FOUL ODOR WITH APU BLEED AND PACKS ON, DISSIPATED DURING CLIMB AFTER 5-7 MINS, CABIN ODOR FORM COMPLETED( APU BLEED AIR SUPPLY SYSTEM).' (SUPPLEMENTAL TO FOLLOW)SDR YENA2022071800672Ecs · odorFLT#571, LGA-FLL. ' DIRTY SOCK SMELL IN DESCENT THE SMELL DISSIPATED WITH PACK 1 OFF; PREFORMED LEVEL A DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM IAW AMM 21-00-00-615-802-A, USING ENG BLEED. NO ODOR PRESENT UPON COMPLETION.'SDR YENA2022022800102Bleed Valve · failedFLT # 1691, JFK-LIR(DIVERTED TO MCO). ENGINE 1 STALL AT CRUISE 34000, LOUD SHAKE NO ECAM PRESENT DIVERT TO MCO; PER TSM 71-00-00-810-808-A, ACCOMPLISHED HPC BORESCOPE OF #1 ENG HPC STG'S 3,6 AND 7 IAW AMM 72-00-00-200-016-B01 AND BORESCOPE INSPECTION OF HPC SDR YENA2021100400641Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITANCE TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + T/C A320 - 33-51-00-710 .SDR YENA2021100400640Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITANCE TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + T/C A320 - 33-51-00-710 .SDR YENA2021100400639Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITY TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + TC A320 - 33-51-00-710 .SDR YENA2021100400638Battery · no testFLT 576, MSY-JFK. BATTERY CAPACITY TEST REQ ; R/R EPSU BATTERY IAW AMM 33-51-00 + TC A320 - 33-51-00-710 .
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