N580JB
Service difficulty reports · 91
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 = 'N580JB' 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 = 'N580JB' 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 YENA2025120101133Computer · malfunctionedFLT#1970, BOS-PHX. WHILE DESCENDING AND SLOWING TO 210 KTS AT 9000 FEET, SELECTED FLAPS 1 AND RECEIVED ELAC 1 FAULT. PLANE ROLLED APPROX 15 DEGREES RIGHT. DISCONNECTED A/P AND HAND FLEW PLANE TO NORMAL LANDING; REF LG # 4520823 ITEM #2, # 4520824 ITEM #1 FOSDR YEN2025F00010Pump · failedFLT#1970, BOS-PHX. "WHILE DESCENDING AND SLOWING TO 210 KTS AT 9000 FEET, SELECTED FLAPS 1 AND RECEIVED ELAC 1 FAULT. PLANE ROLLED APPROX 15 DEGREES RIGHT. I DISCONNECTED A/P AND HAND FLEW PLANE TO NORMAL LANDING; REF LG # 4520823 ITEM #2, # 4520824 ITEM #1 FOSDR YENA2025021700155Battery · failedFLT#2126, MBJ-FLL. 'EMERGENCY LIGHT INOP; REMOVED AND REPLACED ALL 4 EPSU BATTERIES REF AMM 33-51-38-000-001-A SEE SUBSEQUENT ITEMS FOR PART TRANSACTIONS THIS ITEM CLEARED FWD EPSU BATTERY.'SDR YENA2024081301137Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 31 BTW STR 40L AND STR 41L IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00019) REF AEROMAN WO 2024 51/1 NR 2024-370753. REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCATSDR YENA2024081301136Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 31 AND BTW STR 40R AND STR 41R IN FW D CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00020) REF AEROMAN WO 2024- 51/1 NR 2024-370766. REMOVED AND REPLACED CLEAT (SHEAR TIE)SDR YENA2024081301135Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 41R AND STR 42R IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00021) REF AEROMAN WO 2024-51/1 NR 2024-370812. REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCATSDR YENA2024081301134Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 42R AND STR 43R IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00022) REF AEROMAN WO 2024 51/1 NR 2024-370813. REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCATSDR YENA2024081301133Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 42L AND STR 43L IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00023) REF AEROMAN WO 2024 51/1 NR 2024 370814 REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCATESDR YENA2024081301132Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 41L AND STR 42L IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00024) REF AEROMAN WO 2024- 51/1 NR 2024- 370815. REMOVED AND REPLACED SHEAR TIE LOCATED AT SDR YENA2024081301131Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 33 AND BTW STR 40R AND STR 41R IN FW D CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00025) REF AEROMAN WO 2024 51/1 NR 2024-370827. REMOVED AND REPLACED SHEAR TIE LOCATED ASDR YENA2024081301130Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 32 AND BTW STR 41R AND STR 42R IN FW D CARGO COMPARTMENT; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00028) REF AEROMAN WO 2024 51/1 NR 2024 370834. REMOVED AND REPLACED SHEAR TIE LOCATED AT LEVEL OF FR 3SDR YENA2024081301129Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 30 AND BTW STR 41R AND STR 42R IN F WD CARGO COMPARTMENT; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00029) REF AEROMAN WO 2024 51/1 NR 2024 370848. REMOVED AND REPLACED SHEAR TIE LOCATED AT LEVEL OF FR 3SDR YENA2024081301128Shear Tie · corrodedDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 30 AND BTW STR 41R AND STR 42R IN F WD CARGO COMPARTMENT; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00029) REF AEROMAN WO 2024 51/1 NR 2024 370848. REMOVED AND REPLACED SHEAR TIE LOCATED AT LEVEL OF FR 3SDR YENA2024081301127Shear Tie · corrodedDURING HEAVY MAINTENANCE: CRACK SHEAR TIE IN AFT CARGO COMPARTMENT (CRACK SHEAR TIE LOC ON FRAME 61 BTW STR 41 TO 42L ON AFT CARGO COMPARTMENT ); REF AEROMAN WO # 2024-51/1 NR # 2024-371091REMOVED AND REPLACED SHEAR TIE (CLIP) LOC. ON FR 61 BTW STR 41L TO STR SDR YENA2024081301126Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 42L AND FR61 IN AFT CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00044) REF AEROMAN WO # 2024-51/1 NR- 2024-370795 PERFORMED PERMANENT REPAIR LOC. FR 60 STRINGER 42L IN AFT CARGO COMPARTMSDR YENA2024081301125Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 8, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.098 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/SDR YENA2024081301124Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE A, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.096 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/SDR YENA2024081301123Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE B, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.094 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/SDR YENA2024081301122Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE C, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.075 INCHES. CRACK DIR ECTION: 1 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/SDR YENA2024081301121Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION SPIGOT FITTING ON RH PYLON (1 EA); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00051) REF AEROMAN WO # 2024-51/1 NR # 2024-371044 REPLACED LOWER SPIGOT FITTING IAW A320 SRM 54-51-12-300-002 STEP 2.A(3) TO (9).SDR YENA2024081301120Stringer · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE (2EA) ON STRINGER 2RH BETWEEN FR80 TO FR81 UPPER FUSELAGE; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00057) REF AE W/O# 2024-51/1. N/R# 2024 - 371123. ACCOMPLISHED REPAIR OF ELONGATED HOLES ON EXISTING REPAIR LOCATION ON RSDR YENA2024081301119Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / SKIN PANEL BETWEEN FR80-81 & STGR 1R-3R / ELONGATED HOLES & EXISTING REPAIR - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9033-24 COVER & P1-P2 /2/ AIRBUS RDAF 81440328/004/2024 ISSUE B /3/ AIRBUS TD/814SDR YENA2024051600750Warning Light · false activationFLT#1795, JFK-AUS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'AFTER T/O RECEIVED ENG 1 AGENT 1 DISCH LIGHT. ILLUMINATED AND REMAINED ON NO OVERWEIGHT LANDING ON RETURN TO JFK; REF TSM 26-21-00-810-815-A. FOUND FAULTY ENG 1/ AGENT 1 P/BSW. R/R ENG 1/ AGENT 1SDR YENA2022120201196Unknown · odorFLT#688, BNA-LGA. 'ODOR EVENT COMING THROUGH 10000FT; PERFORMED DECONTAMINATION OF AIRCRAFT IAW AMM 36-12-00. NO ODOR IS PRESENT. COMPLETED WITH INFORMATION NOTICE 2017-TO15, SECTION B2. DECONTAMINATION LEVEL 2 WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. AIRCSDR YENA2022030100103Fan · failedFLT # 669, JFK-SJC. VENT BLOWER FAULT ECAM IN CRUIZE SLIGHT VIBRATION AND ELECTRICAL SMELL COMING FROM VENT IN COCKPIT PRIOR TO ECAM. ( EXTRACT FAN - NO AVNCS SYS FAULT ECAM CAUTION ) ; REMOVED AND REPLACED AVX VENT EXTRACT FAN REF AMM 21-26-51. OPS CK GOOD. MSDR YENA2021091700611Skin · corrodedDURING HMV, CORROSION AROUND FASTENER ROW TOP RIGHT WING SURFACE STR 11 BETWEEN RIB 2/3 DOT 88-017 ; REMOVED CORROSION FROM AREA IAW A320 SRM 51-74-00 PERFORMED NDT INSPECTION ON AREA WITH ORIGINAL MATERIAL .210 MATERIAL LOSS OF .040 AND FOUND OUT OF LIMITS IASDR YENA2021091700610Skin · corrodedDURING HMV, CORROSION AROUND FASTENER ROW TOP RIGHT WING SURFACE STR 11 BETWEEN RIB 3/4 ; REMOVED CORROSION IAW A320 SRM 51-74-00 PERFORMED NDT INSPECTION ON AREA WITH ORIGINAL THICKNESS .210 MATERIAL REMAIN .173 WITH A LOSS OF .037 AND FOUND OUT OF LIMITS IAWSDR YENA2021091700609Skin · corrodedDURING HMV, CORROSION AROUND FASTENER TOP RIGHT-WING SURFACE STR 11 HEAR SLAT #3 DOT 88-023 ; REMOVED CORROSION FROM AREA IAW A320 SRM 57-21-11 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL THICKNESS .166 MATERIAL REMAIN .155 WITH A LOSS OF .011AND FOUND OUT OF LISDR YENA2021091700608Skin · corrodedDURING HMV, L/H WING UPPER SURFACE HAS AREAS OF CORROSION AT STA 1957 RIB 4 AND UPPER SKIN BUTT SPLICE11 DOT 008 ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .213 MATERIAL REMAIN .185 WITH A LOSS OF .028 SDR YENA2021091700607Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREA OF CORROSION AT RIB 1 3"FWD OF UPPER SKIN BUTT SPLICE 11.7 INCHES O/B OF FUSELAGE ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .210 MATERIAL REMAIN .168 WITH LOSSDR YENA2021091700606Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION AT WING WALK AREA STA 700/RIB2 32" AFT OF FRONT SPAR ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .200 MATERIAL REMAIN .155 WITH LOSS OF .045 AND FSDR YENA2021091700605Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION ABOVE FRONT SPAR AT STA 1957/RIB4 ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .260 MATERIAL REMAIN .152 WITH LOSS OF .108AND FOUND TO BE OUT OF LISDR YENA2021091700604Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION AT RIB 8 ABOVE REAR SPAR ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .311 MATERIAL REMAIN .240 WITH A LOSS OF .071 AND TO BE OUT OF LIMITS IAW A32SDR YENA2021081700522Unknown · odorFLT 2085, BDL-MIA. CABIN ODOR REPORTED BY INBOUND FLIGHT ATTENDANTS DIRTY SOCK SMELL; INFLIGHT CREW DEBRIEFED DURING GATE OPERATION AND DEPLANING WITH DOOR OPEN. ODOR EVENT OCCURED AFT AND MID CABIN . COMPLIED WITH INFORMATION NOTICE 2017-T015G SECTION A ( A )SDR YENA2021040600207Unknown · odorFLT 1533, JFK-CTG. ODOR EVENT ON TAKEOFF/CLIMBOUT. SPECIFICALLY NOTICEABLE IN THE COCKPIT. MX-270 FORM COMPLETED; COMPLIED INFO NOTICE 2017-1015F SECTION A. A/C OK FOR SERVICESDR YENA201907200414Epsu · failedFLT 430, SMF-BOS. AFT EXIT LIGHT INOP; R & R AFT EPSU IAW AMM 33-51-00 OPS CHECK AND TEST GOOD. A/C OK FOR CONT. SERVICED.SDR YENA2019060325294Line · rupturedFT # 80, AIRCRAFT WAS FOUND WITH A HYDRAULIC LEAK ON THE #1 ENGINE AFT PYLON AREA. AFTER GAINING ACCESS TO THE SUBJECT AREA, IT WAS FOUND THAT A HYDRAULIC LINE HAS RUPTURED AND CAUSED DAMAGE TO THE PYLON BOX STRUCTURE P/N D54541005000000. AFTER CLEANUP ANDSDR YENA201812310892Battery · dischargedFLT 2991, BOS-TPA. EPSU 10WL BATTERY FAILS EMERGENCY LIGHT SYSTEM TEST; R & R EPSU 10WL BATTERY IAW AMM 33-51-38, EMERGENCY LIGHT SYSTEM CHECKS OK.SDR YENA2018120490803Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM -Y450 .8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AND DRAWING # D53472816SDR YENA2018120490802Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM -Y464.8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AND DRAWING # D53472816.SDR YENA2018120490801Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM - Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM - Y464.8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AN DRAWING # D53472816SDR YENA2018120490800Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA; REF BP NR # 2018-374614 REPLACED FLOOR BEAM + Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780SDR YENA2018120490799Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA; REF BP NR # 2018-374616 REPLACED FLOOR BEAM +Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780SDR YENA2018120490798Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM - Y 1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA; REF BP NR # 2018-374620 REPLACED FLOOR BEAM - Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780SDR YENA2018120490797Web · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT WEB AT STR 23R AT AFT GALLEY AREA; REF BP NR # 2018-374680 REPLACED SUPPORT WEB AT STR 23R BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER SRM A320-51-72-11 AND DRAWING # D53474180.SDR YENA2018120490796Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y1162.5 BETWEEN FR 66-FR 68 AT AFT GALLEY AREA; REPLACED FLOOR BEAM-Y1162.5 BETWEEN FR 66-FR 68 AY AFT GALLEY AREA IAW SRM A320-51-72-11 AND DRWG D53472780. REF AEROMAN NR 2018-374619.SDR YENA2018120490795Stringer · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON STRINGER 43L LOCATED BTW FR 62 TO FR 63 IN AFT CARGO COMPARTMENT; REF BP NR # 2018-374610 REPLACED STRINGER 43L BTW FR 60 60 FR 64 IN AFT CARGO COMPARTMENT AS PER SRM A320 51-72-11 AND DRAWING # E 53470342.SDR YENA2018120490794Dummy Rail · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y503.2 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA; REF BP NR # 2018-374621 REPLACED RAIL DUMMY Y503.2 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING # 53112825SDR YENA2018120490793Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1292 LOC. BTW FR 12 TO FR 24 IN PASSENGER CABIN; REF BP NR # 2018-374613 REPLACED FLOOR BEAM LOC +Y1292 BTW FR 12 TO FR 24 IN PASSENGER CABIN AS PER SRM A32051-72-11 AND DRAWING # D53112812.SDR YENA2018120490792Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y 1292 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA; REPLACED FLOOR BEAM LOCATION -Y1292 BTW FR 12 TO 24 AT FWD GALLEY AREA AS PER SRM A320-51-72-11 AND DWG D53112812. ALL WORK ACCOMPLISHED ON AERO
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