N506JB
Service difficulty reports · 79
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 = 'N506JB' 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 = 'N506JB' 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 YENA2026090800734Display · failedFLT#227, MCO-SJU (AIR TURNBACK TO MCO). DURING CLIMBOUT WE EXPERIENCED WHAT APPEARED TO BE AN ELECTRICAL BURNING ODOR CA MCDU WAS INOP AT THE SAME TIME; REMOVED & INSTALLED MCDU DISPLAY MONITOR IAW AMM 22-82-00. OPS CHK GOOD.SDR YENA2026060800464Lamp · burned outFLT 2424, MCO-DCA. "FOUND AFT EXIT SIGN MULTIPLE LAMP BURN; REMOVED AND REPLACED AFT EXIT SIGN LAMP IN REFERENCE A320 AMM 33-51-16.OPS CK GOOD.AC OK TO CONT."SDR YENA2025121701225Slide Raft · faultedFLT 488, MCO-ORH. DOOR 2 L SLIDE SHOWS DISARMED IN FLIGHT AFTER PRESSURIZATION. ( PASSENGER OR OVER WING DOOR SLIDE/SLIDE RAFTS (WITHOUT PASSENGERS) ); REMOVED AND REPLACED L2 DOOR SLIDE PER AMM 25-62-44. SLIDE ARM LEVER STILL SHOWS DISARMED ON ECAM. SLIDE ARMSDR YENA2025061100584Outflow Valve · failedFLT#195, HPN-MCO (AIRCRAFT DIVERTED TO JFK). 'CAB PR EXCESS CAB ALT ECAM AT FL 320 TO 10500 FT. AS WE INITIATED EMG DESCENT CABIN ALT REMAINED OVER 10000 FT AS WE MADE OUR RAPID DESCENT TO 10K; REMOVED AND REPLACED OUTFLOW VALVE IAW AMM 21-31-51. OPS CHECK GOOSDR YENA2025031700258Tachometer · failedFLT#2834, RSW-ORH. (AIRCRAFT DIVERTED TO BOS) 'BRAKES AUTO BRK FAULT BRAKE RELEASED; REMOVED AND REPLACED #4 TACHOMETER IAW AMM 32-42-57-04. OPS CHECK GOOD.'SDR YENA2024112501493Ecs · contaminatedFLT#2920, ALB-MCO. 'VERY STRONG ODOR ROWS 7-9 ON LANDING REPORTED BY INFLIGHT; C/W INFO NOTICE 2017-T015K . ACCOMPLISHED LEVEL B DECONTAMINATION OF ECS PER AMM 21-00-00-615-803-A . ACCOMPLISHED ECS TEST WITH ALL BLEED SOURCES, NO ODOR NOTED. APU WAS REPLACED, SDR YENA2024111801486Apu · unknownFLT#987, ORH-MCO. 'STRONG DIRTY SOCK ODOR FOR ABOUT 2 MINUTES AND IT THEN DISSIPATED; PERFORMED APU INSPECTION FOR OIL LEAKS AND NO LEAKS FOUND AT THIS MOMENT. R & R HEPA FILTERS PER AMM 21-21-41 LEAK CHECK GOOD. OPERATED PACKS AND NO ODOR EVENT NOTICE AS PER SDR YENA2024101801378Switch · pilot errorFLT#811, BOS-ORD. (AIRCRAFT PERFORMED AN AIR TURN BACK TO BOS) 'FLT LANDING GEAR DOWN. ECAM. VMO LIMITED TO 235 AFTER TAKE OFF; PUT L/G DOWN VMO/MMO SWITCH TO NORMAL POSITION IAW AMM 05-59-32=869-001 ECAM CLEARED.'SDR YENA2024072301029Fitting · unknownDURING HEAVY MAINTENANCE: REMOVE AND REPLACE CONTINUITY FITTING LH & RH SIDE LOCATED BTW FR 1 AND FR 2 IN COCKPIT; REF AEROMAN N/R 2024-349053, REMOVE AND REPLACE CONTINUITY FITTINGS LH AND RH SIDE LOCATED BTW FRAME 1 AND FRAME 2 IN COCKPIT IAW EC A24-844-01, SDR YENA2024072301028Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER CORNER LH SIDE. CRACK LENGTH IS 0.483 INCH; REF AEROMAN N/R 2024- 2024-348647, PERFORMED PERMANENT REPAIR ON WINDSHIELD FRAME LH LOWER RADIUS C1 AREA AND EXISDR YENA2024072301027Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE HOLE 6 AT LEVEL DOOR STOP 7. CRACK AT 1. O CLOCK. D1-D2= 0.079 INCH. CONFIRM INDICATION USING BOROSCOPE VIEW AS PER NTM 51-90-00; REF AEROMAN N/R 2024-348897, PERFORMED PERMANENT REPAIR OF CRSDR YENA2024072301026Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE HOLE C AT LEVEL DOOR STOP 7 . CRACK AT 1. O CLOCK. D1-D2= 0.118 INCH. CONFIRM INDICATION USING BOROSCOPE VIEW AS PER NTM 51-90-0; REF AEROMAN N/R 20240348898, PERFORMED PERMANENT REPAIR OF CRSDR YENA2024072301025Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / LH CTR POST LOWER NODE / CRACK + EXISTING REPAIR AT HOLE D1 LH - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-9010-24 (COVER + PARTS 1 THRU 5) REV 0 /2/ AIRBUS RDAF 80992805/026/2024#A SDR YENA2024072301024Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / RHS FR16 DOUBLE JOGGLE AREA HOLE C AND #6 / CRACKS - PERMANENT REPAIR; REFERENCES: AEROMAN EA 53-9015-24 REV. 0 (COVER + PARTS 1-3) AIRBUS SB A320-53-1373 REV. 01 AIRBUS RDAF 81411276/028/2024#A AIRBUS SDR YENA2022031400192Window Post · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.250 INCH APPROX IN COCKPIT (1EA); REMOVED AND REPLACED CONTINUITY FITTING RH (1E/A) AND FASTENERS LOC. BTW FR1 TO FR2 WISDR YENA2022031400191Pressure Blkhd · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 TO PRESSURE BULKHEAD ATTACHMENT AREA FWD FACE AT FASTENER HOLE LOCATED 1 INCH BELOW ST30LH LEVEL, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, CRACK LENGTH ARE L1=0.375 INCH APPROX, L2=0.28 0 INCH APPROX IN FWD CASDR YENA2022031400190Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.250 INCH APPROX IN COCKPIT (1 EA); ACCOMPLISHED THE REPAIR OF THE (1) CRACK IN THE LH WINDSHIELD FRAMING NEAR THE CENTERSDR YENA2022031400189None · noneDURING HEAVY MAINTENANCE, (E/C A21-1370-01) WINGS / CENTER WING BOX / UPPER SKIN PANEL / UPPER SURFACE / FRAME 41-42 / STIFF 17 / CORROSION DAMAGE - PERMANENT REPAIR (CLASSIFIED AS A MAJOR REPAIR)SDR YENA2022031400188Bulkhead · crackedDURING HEAVY MAINTENANCE, (E/C A21-1362-01) FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / BULKHEAD / CRACKS AT FASTENER HOLES – PERMANENT REPAIR (CLASSIFIED AS A MAJOR REPAIR)SDR YENA2022031400187Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN LOC. BTW FR41 TO FR42 ON STIFFENER 17 L/H SIDE IN CENTER FUEL TANK (CPCP RELATED MPD TASK; "EVALUATED REWORKED AREA LOCATED ON EXTERNAL SKIN BTW FR41 TO FR42 ON STIFFENER 17 LH IN CENTER FUEL TANK AND FOUND OUTSDR YENA2022031400186Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN LOC. AT LEVEL FR42, 1.500 IN OUTBOARD SIDE OF Y1292 IN CENTER FUEL TANK (CPCP RELATED MPD); ACCOMPLISHED REPAIR OF CORROSION AFFECTED AREA FOUND ON RH WING BOTTOM SKIN UPPER SURFACE AROUND RIB.SDR YENA2022031400185Tie Clip · corrodedDURING HEAVY MAINTENANCE, CORROSION INTERNAL STRUCTURE TIE CLIP LOCATED AT FR 32 AND BTW STR 41R AND 42R IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED TIE CLIP IAW A32O SRM 51-72-11-911-001 AND DWG D53232982SDR YENA2022031400184Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y464.8 BTW FR 64-67 AT AFT GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM -Y464.8 LOCATED BTW FR64-67 AT AFT GALLEY AREA IAW SRM A320-51-72-11 & DWG D53472040 SHEETS 2;10;12. REF. AEROMAN WO 1138762 NR 2021-499923 SDR YENA2022031400183Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y765 BTWN FR 64-66 AT AFT GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM -Y765 BTWN FR 64-66 AT AFT GALLEY IAW SRM A320-51-72-11 AND DRWG D534 72816 SHEET 2; SHEET 3; DWG D53472000 SHEET 24. REF. AEROMAN W/O 113876SDR YENA2022031400182Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM - Y1292 LOCATED BTW FR 12-24 AT FWD. GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM -Y1292 LOCATED BTWN FR 12-24 AT FWD. GALLEY AREA IAW A320 SRM 51-72-11 & DWG. D53110984 SHEET 1; DWG. D53112812 SHEET 2;D53110876 SSDR YENA2022031400181Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM +Y1292 LOCATED BTWN FR 12-24 AT FWD. GALLEY AREA (CPCP RELATED MPD TASK 531189-01); REMOVED AND REPLACED FLOORBEAM+Y1292 LOCATED BTWN FR12-24 AT FWD. GALLEY AREA IAW A320 SRM 51-42-11;SRM 51-72-11 AND DWG D5311281SDR YENA2022031400180Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM +Y503.2 LOCATED BTWN FR 12-16 AT FWD. GALLEY AREA (CPCP RELATED MPD TASK 531189-01); REMOVED AND REPLACED FLOOR BEAM +Y 503.2 LOCATED BTWN FR 12-16 AT FWD FWD. GALLEY AREA IAW A320 SRM 51-42-11 AND SRM 51-72-11 ANSDR YENA2022031400179Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOORBEAM +Y765 LOCATED BTWFR12-24 AT FWD. GALLEY AREA (CPCP RELATED MPD TASK 531189-01; REMOVED AND REPLACED FLOORBEAM +Y765 LOCATED BTWN FR12-24 AT FWD. GALLEY AREA IAW A320SRM 51-42-11;51-72-11 AND DRWG D53112812. REF. AESDR YENA2020112700542Bulb · inoperativeDURING HEAVY MAINTENANCE, EMERGENCY EXIT LIGHTS AT DOORS HAVE NUMEROUS INOPERABLE BULBS, REF FAS WO N506JB-01-01 NR-00046. R & R BAD BULB ON EMERGENCY EXIT LIGHTS AT L1, L2, R1, R2 & LT OVERWING EXIT SIGNS, IAW A320 AMM 33-51-17. OPERATIONS CHECKED GOOD ON ESDR YENA2020092400464Battery · failedFLT 70 FLL-BOS. CABIN EMERGENCY LIGHTS NOT FUNCTIONING PROPERLY. REPLACED EMERGENCY LIGHT BATTERIES, PER AMM 33-51-00. OPS CK NORMAL.SDR YENA2020031840243Battery · dischargedFLT# 905, EWR-TPA. RH EMER EXIT EPSU FAILED BITE TEST; REPLACED EPSU BATTERY PER AMM 33-51-38SDR YENA2019111840653Seal · failedFT # 1735, BOS-MSP. THE PILOT REPORTS HIGH VIBRATIONS FROM THE #2 ENGINE. THE A/C WAS JUST RETURNED TO SERVICE IN BOS FOR THE R & R OF ONE FAN BLADE ON THE #2 ENGINE THAT HAD A DENT ON IT. THE PILOT ELECTED WITH THE CONCURRENCE OF MCC TO RTF IN BOS. ENG 2 N1 SDR YENA201908126439Unknown · odorFLT 120, LEVEL II ODOR EVENT TRICRESYL PHOSPHATE (DIRTY SOCK) ODOR. BOTH PILOTS SCRATCHY THROAT SLIGHT HEADACHE. ISOLATED IN SEQUENCE BLEED 1 AND BLEED 2 ODOR DISAPATED WITH BLEED 2 OFF RESIDUAL ODOR RUNNING PACK 2 VIA CROSS BLEED AND LATER ON APU BLEED CABINSDR YENA2018122600886Fitting · crackedDURING HEAVY MAINTENANCE, CENTER WING BOX FWD SPAR LWR FLANGE LH SIDE OB FITTING FIRST TWO HOLES FORM IB END OF FITTING HAVE CRACK INDICATIONS; REF HAECO NR 440518-22392 - REPLACED LH CORNER FITTING FR36 IAW A320 SRM 51-72-11 + 51-42-11.SDR YENA2018122600885Frame · crackedDURING HEAVY MAINTENANCE, CENTER WING BOX FWD SPAR LWR FLANGE RH SIDE OB FITTING FIRST TWO HOLES FROM IB END OF FITTING HAVE CRACK INDICATIONS; REF HAECO NR 440518-22393 - REPLACED RH CORNER FITTING FR36 IAW A320 SRM 51-72-11 + 51-42-11.SDR YENA2018122600884Light · inoperativeDURING HEAVY MAINTENANCE, PAX CABIN SEAT 1C EMERGENCY PATH LIGHT LENS AND FIXTURE DAMAGED; REMOVED AND REPLACED SEAT ROW 1 LH EMERGENCY LIGHT ASSY IAW A320 AMM 33-51-18-000-001-A & 33-51-18-400-001-A. NR 440518-22312 FOR WORK PERFORMED. SUPPLEMENTAL INFORMATIOSDR YENA201710260870Light · shortedDURING AN EMERGENCY LIGHTS SYSTEM TEST, THE FWD LEFT EPSU INDICATED AN INTERIOR & EXTERIOR LOAD FAULT. PERFORMED TSM 33-51-00-810-808-A, THE FWD LEFT SLIDE LIGHTS HAD SHORTED. REPLACED SLIDE EMERGENCY LIGHTS. SYS TESTED GOOD.SDR YENA201702230111Skin · corrodedFUSELAGE SKIN FOUND CORRODED ON THE AVIONICS SKIN AIR INLET VALVE ATTACH SURFACE, FRAME 21+8, STRINGER 14L. REMOVED AND REPLACED THE SKIN DOUBLER IAW SRM 51-72-11, 51-42-11, AND 51-44-11.SDR YENA20150812349Floor Support · corrodedDURING HEAVY MAINTENANCE, FOUND RT AFT FUSELAGE FLOOR SUPPORT HAS SHEARED FASTENERS AT FRAMES 68 - 69 -Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 53-41-15.SDR YENA20150812348Floorbeam · corrodedDURING HEAVY MAINTENANCE FOUND RT AFT FUSELAGE FLOORBEAM HAS CORROSION AT SPLICE FRAME 66 Y1292. REPLACED THE FLOORBEAM IAW SRM 51-42-11.SDR YENA20150812347Floor Support · corrodedDURING HEAVY MAINTENANCE FOUND RT AFT FUSELAGE FLOOR SUPPORT CORRODED AT SPLICE FRAMES 67 - 68 -Y1292. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.SDR YENA20150812346Door Sill · corrodedDURING HEAVY MAINTENANCE, FOUND LT AFT DOOR SILL CORRODED FRAMES 68 - 68. REPLACED THE DOOR SILL IAW SRM 51-42-11.SDR YENA20150812345Floorbeam · corrodedDURING HEAVY MAINTENANCE, FOUND LT AFT FUSELAGE FLOORBEAM HAS CORROSION AT SPLICE FRAME 66 Y1292. REPLACED THE FLOORBEAM IAW SRM 51-42-11.SDR YENA20150812344Floorbeam · corrodedDURING HEAVY MAINTENANCE, FOUND AFT CABIN FLOORBEAM AT FRAME 66 Y254 CORRODED. REPLACED FLOORBEAM IAW SRM 51-42-11.SDR YENA20150812343Floor Support · corrodedDURING HEAVY MAINTENANCE, FOUND AFT CABIN FLOOR SUPPORT FROM FRAMES 66 - 68 Y1732 CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.SDR YENA20150812342Floor Support · corrodedDURING HEAVY MAINTENANCE FOUND AFT CABIN FLOOR SUPPORT AT FRAMES 66-88 -Y765 CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.SDR YENA20150812341Floor Support · corrodedDURING HEAVY MAINTENANCE FOUND AFT CABIN FLOOR SUPPORT FROM FRAMES 68 - 70; Y1732 CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.SDR YENA20150812340Floorbeam · corrodedDURING HEAVY MAINTENANCE FOUND AFT CABIN FLOORBEAM JUST FWD OF FRAME 66 AT Y765 CORRODED. REPLACED THE FLOORBEAM IAW SRM 51-42-11.SDR YENA20150812339Floorbeam · corrodedDURING HEAVY MAINTENANCE, FOUND LT AFT FUSELAGE FLOORBEAM HAS CORROSION AT FRAME 68 Y765. REPLACED THE FLOORBEAM SRM 51-42-11.SDR YENA20150812338Floorbeam · corrodedDURING HEAVY MAINTENANCE FOUND AFT CABIN FLOORBEAM AT FRAME 66 BETWEEN Y756 AND Y1292 CORRODED. REPLACED THE FLOORBEAM IAW SRM 51-42-11 AND SRM 53-00-14.
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