N562JB

Service difficulty reports · 65

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 = 'N562JB' 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.

SDR YENA2026022500238Apu · contaminatedFLT #1367 HPN-PBI. "AFT INFLIGHT SMELLED DIRTY SOCK SMELL AS SOON AS WE TOUCHED DOWN AND TAXIED TO THE GATE. THIS WAS AFTER APU STARTED CLEARING THE RUNWAY.;INSPECTED APU AREA FOUND SATURATED WITH TYPE 1 DE-ICE FLUID TO INCLUDE INTAKE & PLENUM. C/W INFO NOTICEFeb 25, 2026 · N562JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR YENA2025009000905Slide · unwanted deployFLT#1567, HPN-PBI. "ACCIDENTAL DEPLOYMENT OF R1 DOOR SLIDE; REMOVED AND REPLACED R1 DOOR SLIDE FUNCTIONAL TESTS GOOD IAW AMM 25-62-44 A/C OK FOR SERV"Aug 30, 2025 · N562JB · Airbus A320232 · Escape SlideSDR YENA2024121601559Computer · failedFLT#787, JFK-SXM. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'F CTL ELAC 1 PITCH FAULT IN FLIGHT. NECESSITATED A RETURN TO JFK FLT MX; REF TSM 27-93-00-810-859-A. REMOVED AND REPLACED ELAC 1 COMPUTER IAW AMM 27-93-34. REF L/P 4133099 (AS PRECAUTION R/R ELEC Dec 14, 2024 · N562JB · Airbus A320232 · Elevator Control SystemSDR YENA2024120201516Autopilot Sys · abnormalFLT#2062,SJU-BOS. 'WHILE CLIMBING RECEIVED ECAM AUTO FLT RUD TRV LIMITER 1 ( RUDDER TRAVEL LIMITER SYSTEMS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)Dec 1, 2024 · N562JB · Airbus A320232 · Rudder Control SystemSDR YENA2024041100512Unknown · odorFLT#130, RSW-JFK. 'GETTING ON OIL SMELLS IN THE CABIN WITH ENGINES RUNNING AND NO APU ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)Apr 9, 2024 · N562JB · Airbus A320232 · Air Distribution SystemSDR YENA2023122101619Unknown · unknownFLT#2107, JFK-FLL. 'F/A REPORTED DIRTY SOCK SMELL AT 6000 FT UNTIL LANDING (AT SAME TIME WE ENTER CLOUD DECK) ( APU SYSTEM ); INSPECTED APU & NO LEAKS NOTED AFETR RECTIVATION & OPERATION OF BLEED SYSTEM AMM 21-00-00 & 36-10-00. PER INFO NOTICE 2017 T015 SUSPECDec 20, 2023 · N562JB · Airbus A320232 · Air Distribution SystemSDR YENA2023121501589Unknown · unknownFLT#1920, MSY-LGA. (AIRCRAFT DECLARED AN EMERGENCY INTO LGA), ' HYD B RESERVOIR LOW LEVEL IN FLIGHT INDICATOR SHOWED VERY LOW FLUID IN B SYSTEM; REMOVED AND REPLACED B HYD PRESS SW (10CE1) SEAL REF AMM 27-92-17. OPS CHECK OK. LEAK CHECK OK. AC OK FOR SVC.'Dec 14, 2023 · N562JB · Airbus A320232 · Hydraulic System, MainSDR YENA2023113001518Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H1, CRACK DIRECTION IS 5 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2023- 631069, PERFORMED REPAIR FR16LH AT LEVEL DOONov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2023113001517Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H3, CRACK DIRECTION IS 5 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2023- 631070, PERFORMED REPAIR FR16LH AT LEVEL DOONov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2023113001516Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H3, CRACK DIRECTION IS 10 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); PERFORMED REPAIR FR16RH AT LEVEL DOOR STOP FITTING #7 HOLE 3. IAWNov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2023113001515Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK , CRACK DEPTH: 0.128 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00012 ) FUR-A320-53-00976, REF ANov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001514Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK , CRACK DEPTH: 0.128 INCH APPROX; REF AEROMAN N/R 20232-631118, PERFORMED REPAIR ON DOOR STOP FITTING #7 FR Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001513Unknown · unknownDURING HEAVY MAINTENANCE: WEAR ON BUSHING I/B ACTUATOR HING O/B LUG ON LH ELEVATOR; AFTER REMOVAL OF THE WORN BUSHING FOUND CORROSION ON THE LUG BORE FORUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ELEVATOR ACTUATOR ATTACH FITTING O/B LH THIS IS A CAT "A" REPNov 27, 2023 · N562JB · Airbus A320232 · Elevator StructureSDR YENA2023113001512Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA LH SIDE CONTINUITY FITTING, CRACK LENGTH IS 0.180 INCH, IN COC KPIT (1 EA); ROTOTEST INSPECTION IN OPEN FASTENER 3 HOLES OF LH AND RH SIDES IAW NTM 51-10-0Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001511Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA, LH SIDE, FROM UPPER TENSION BOLT, CRACK LENGTH IS 0. 100 INCH, CRACK DIRECTION IS 2 OCLOCK, IN COCKPIT (1 EA); REMOVED AND REPLACED MIRROR FITTINNov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001510Unknown · unknownDURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 RH SIDE, FRAME 68; CRACK LOCATION: 06 OCLOCK , CRACK DEPTH: 0.145 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00024 ) PENov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001509Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 LH SIDE, FRAME 68; CRACK LOCATION: 06 AND 12 OCLOCK , CRACK DEPTH:0.187 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00025 ) PERFORMED REPAIR ON FNov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001508Unknown · unknownDURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CORROSION STRINGER 43L LOCATED BTW FRAME 62 AND FRAME 63 IN AFT CARGO COMPARTMENT (CPCP-RELATED MPD TASK 534107-01); (RESOLVED ON W/O: 1269492 TASKCARD: NR-00026 ) REMOVED AND REPLACED STRINGER 43L LOCATED BTWNov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2023113001507Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE AT UPPER JOGGLE AREA, HOLE A, CRA CK DIRECTION IS 3 OCLOCK AT FWD GALLEY AREA (1EA); REF AEROMAN NR 2023-631084 WO 2023 358/1 ACCOMPLISHED REPAIR OF THE CRACK AT FR 20 RH UPPER JOGGLE AREA HOLE A INov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2023113001506Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 AT FWD GALLEY AREA (1 EA) (CRACK INDICAT ION ON FRAME 20 LH SIDE AT UPPER JOGGLE AREA, HOLE 6, CRACK DIRECTION IS 3 OCLOCK AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2023-631085 WO 2023 358/1 ACCOMPLISHED RNov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2023113001505Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON UPPER SURFACE OF THE UPPER SKIN OF THE C ENTER WING BOX FR41 TO FR42 ON LH SIDE IN PASSENGER CABIN (CPCP RELATE D REFER MPD TASK 571157-01); REF AEROMAN NR 2023-631067 WO 2023 358/1 PERFORMED PERMANENT REPNov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001504Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER ATTACHMENT AREA AND CONTINUITY FITTING / CRACKS - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2023113001503Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / TOP SKIN PANEL / UPPER SURFACE / BETWEEN FR41-42 AT BEAM Y1292 TO Y1732 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2023012700077A/C Pack · odorFLT#953, JFK-PBI. 'AFT CABIN ODOR REPORTED BY INFLIGHT CREW. PACK 2 WAS ISOLATED, ODOR WENT AWAY; COMPLIED WITH INFO NOTICE 2017-T015J, SECTION B2. DECONTAMINATION LEVEL A ACCOMPLISHED PER TSM 05-50-00-810-831-A. IDENTIFIED PACK 2 AS A SOURCE OF ODOR. REF.Jan 23, 2023 · N562JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2022082600821Thermostat · failedFLT#8097, JFK-DEN. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'SHORTLY AFTER T/O, WE RECEIVED A AIR ENG 1 BLEED FAULT. LEVELS AT 8,000 RAN QRC ECAM & QRH PROCEDURES. NEEDED TO AVOID ICING CONDITIONS. WHICH WE WERE UNABLE TO THUS FORCING US TO RETURN TO JFK.Aug 23, 2022 · N562JB · Airbus A320232 · Pneumatic SystemSDR YENA202206270621None · noneFLT#109, BOS-JAX. 'STRONG DIRTY SOCK ODOR ON DESCENT AND ARRIVAL STARTED AT 11000 FEET. TURNED OFF PACK 1 AND IT AIDED SOME. FRESH OIL FROM THE BOTTOM OF THE TAIL SEEPING FROM SEVERAL AREAS OF APU. APU LOW OIL WRITE UP AND SERVICED 3 DAYS AGO ODOR REPORTING FOJun 26, 2022 · N562JB · Airbus A320232 · Air Conditioning SystemSDR YENA2022010400007Unknown · odorFLT 275, BDL-SJU. "TRANSIENT ENVIRONMENTAL ODOR " DETECTED DURING APPROACH PHASE. MILD TO MODERATE ODOR LASTED 10 MINUTES OF FLIGHT LOCATED AFT OF CABIN. DETECTED BY 2 AFT FLIGHT ATT. DESCRIBED AS LEVEL II. ; COMPLIED WITH INFO NOTICE 2017-T015I SECTION A(A), Dec 28, 2021 · N562JB · Airbus A320232 · Air Distribution SystemSDR YENA2021031900177Fairing · out of adjustFLT 6302, EWR- JFK. NOSE GEAR DOOR DID NOT CLOSE AFTER T/O CYCLED GEAR AND STILL DID NOT CLOSE UNTILL FIFTEEN MINUTES BEFORE LANDING ; ADJUSTED NLG LEG FAIRING IAW AMM 32-22-00; PERFORMED NORMAL EXTENSION AND RETRACTION OPERATIONAL TEST IAW AMM 32-31-00-720-00Mar 16, 2021 · N562JB · Airbus A320232 · Nose/Tail Landing GearSDR YENA2021022600134Control Unit · failedFLT 2469, BOS-FLL. WHEEL N/W STRG FAULT IN FLIGHT; R & R BSCU IAW AMM 32-42-34. PERFORMED OPS CK OF STEERING AND NO FAULT NOTED AT THIS TIMEFeb 25, 2021 · N562JB · Airbus A320232 · Landing Gear Steering SystemSDR YENA2021022600133Control Unit · failedFLT 2469, BOS-FLL. WHEEL N/W STRG FAULT IN FLIGHT; R & R BSCU IAW AMM 32-42-34. PERFORMED OPS CK OF STEERING AND NO FAULT NOTED AT THIS TIMEFeb 25, 2021 · N562JB · Airbus A320232 · Landing Gear Steering SystemSDR YENA2021022600132Control Unit · failedFLT 2469,BOS-FLL. WHEEL N/W STRG FAULT IN FLIGHT; R & R BSCU IAW AMM 32-42-34. PERFORMED OPS CK OF STEERING AND NO FAULT NOTED AT THIS TIMEFeb 25, 2021 · N562JB · Airbus A320232 · Landing Gear Steering SystemSDR YENA2021020500091Keelbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON WEB OF TI ANGLE RT HAND AT FR41-42 LOWER HOLE POSITION; (REF AEROMAN NR 2021-12/1-2021-30271 -) ACCOMPLISHED REPAIR OF THE CRACK DAMAGE, FR 41-42 ON THE KEEL BEAM RT HANDS IAW AEROMAN EA 53-0019-21 AND AIRBUS RDAS Jan 31, 2021 · N562JB · Airbus A320232 · Fuselage Main, KeelSDR YENA2020120800568Pump · failedFLT 1421, PHL-SJU. RETURNED TO FIELD. FUEL FLOW FLUCTUATION. R & R NR 2 ENGINE FUEL PUMP, REF AMM 73-12-41. OPERATIONS AND LEAK CHECK GOOD.Dec 1, 2020 · N562JB · Airbus A320232 · Engine Fuel PumpSDR YENA2020120800567Transmitter · failedFLT 1421, PHL-SJU. RETURNED TO FIELD. FUEL FLOW FLUCTUATION. R & R NR 2 ENGINE FUEL FLOW TRANSMITTER, REF AMM 73-31-17. OPERATIONS CHECK OK.Dec 1, 2020 · N562JB · Airbus A320232 · Engine Fuel Indicating SystemSDR YENA2020120700566Fmu · failedFLT 1421, PHL-SJU. RETURNED TO FIELD. ON CLIMBOUT FUEL FLOW INDICATION INDICATED A FLUCTUATION OF BETWEEN 1800-8000 LB/HR ON ENGINE NR 2. PREVIOUSLY WRITTEN UP. R & R NR 2 ENGINE FMU, REF AMM 73-22-52. OPERATIONS CHECK OK. PERFORM HIGH POWER ASSURANCE RDec 1, 2020 · N562JB · Airbus A320232 · Fuel Controlling SystemSDR YENA2020012950066Battery · no testEMER LT BAT CAPACITY TEST FAIL; PER T/C A320-33-51-00-710-003 R & R EMER LT BAT AS REQ MM 33-51-00.Jan 25, 2020 · N562JB · Airbus A320232 · Emergency LightingSDR YENA2020012925065Battery · no testEMER LT BAT CAPACITY TEST FAIL; PER T/C A320-33-51-00-710-003 R & R EMER LT BAT AS REQ MM 33-51-00.Jan 25, 2020 · N562JB · Airbus A320232 · Emergency LightingSDR YENA202001285064Battery · no testEMER LT BAT CAPACITY TEST FAIL; PER T/C A320-33-51-00-710-003 R & R EMER LT BAT AS REQ MM 33-51-00.Jan 25, 2020 · N562JB · Airbus A320232 · Emergency LightingSDR YENA201710010810Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE R2 DOOR SILL UPPER SURFACE AFT INBD CORNER FRAME 68, STRINGER 23. REPLACED THE DOOR SILL IAW SRM 51-42-11.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201710010809Door Sill · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR SILL AFT OF THE INBD CORNER UPPER SURFACE AT FRAME 68, STRINGER 23L. REPLACED THE DOOR SILL IAW SRM 53-41-14-283-002.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201710010808Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOOR SUPPORT-Y1292, FRAME 20 STRINGER 23R. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201710010803Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOOR SUPPORT Y503 FRAME 20, STRINGER 23R. REPLACED THE FLOOR SUPPORT IAW SRM 53-11-14.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201710010807Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOORBEAM Y464, FRAME 66 +10. REPLACED THE FLOORBEAM IAW SRM 51-72-11.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20171001806Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM Y1292 FR 16. REPLACED THE FLOORBEAM IAW SRM 51-72-11.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20171001805Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM -Y1732 FR 20. REPLACED THE FLOORBEAM IAW SRM 51-72-11.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20171001804Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT FLOORBEAM -Y1292 FRAME 68. REPLACED THE FLOORBEAM IAW IAW SRM 51-42-11.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20171001803Dummy Rail · corrodedCORROSION WAS DISCOVERED ON FWD CABIN DUMMY RAIL, Y503, FRAME 20. REPLACED THE DUMMY RAIL IAW SRM 53-11-14.Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201708180665Lens · brokenEMERGENCY EXIT LIGHT LENS AT SEAT 11C IS BROKEN. REPLACED THE LENS, OK FOR SERVICE.Aug 18, 2017 · N562JB · Airbus A320232 · Emergency LightingSDR YENA201705070355Control Panel · failedSMOKE PUSHBUTTON INDICATING RED SMOKE ON THE AFT AVIONICS RACK. NO AURAL WARNING. QRA COMPLETE. R & R SDCP IAW AMM 23-39-00 SECT 4000, STEP 25 AND PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW AMM 23-39-00, SECT 5000, STEP 10. NO ODOR OR FAULT NOTEMay 7, 2017 · N562JB · Airbus A320232 · Communications SystemSDR YENA20160130086Floor Support · corrodedAFT CABIN , AFT WET AREA, FLOOR SUPPORT 1292, FRAME 66. R & R THE FLOOR SUPPORT BETWEEN FRAMES 66 - 64 IAW SRM 53-72-11, 51-42-11 PARA 2D, 51-21-11, 51-23-12 & GMM 5-169.Jan 30, 2016 · N562JB · Airbus A320232 · Fuselage Miscellaneous Structure
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