N323JB, cancelled Jun 3, 2026
Service difficulty reports · 89
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 = 'N323JB' AND deregistration_id = 'N323JB-2026-06-03' 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 = 'N323JB' AND deregistration_id = 'N323JB-2026-06-03' 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 YENA2025021100146Psu · out of adjustFLT#760, PHL-BOS.' (AIRCRAFT DIVERTED TO JFK AND DECLARED AN EMERGENCY) FLAP FAIL EICAS MSG WHILE RETRACTING 1 TO 0 ORH C/W. MSG DID NOT CLEAR; FLAPS INDICATED 0 IN AMBER; REF LOGPAGE 4274864 ITEMS 1 (PERFORMED TROUBLESHOOTING AS PER FIM 27-51-00-810-801-A. FOSDR YEN2024F00000Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / WINDSHIELD FRAME / CENTER POST LH UPPER FASTENERS AREA / CRACK - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9001-24 COVER REV.0 & PART 1-4 /2/ AIRBUS SB A320-53-1331 (REF. FAA AD 2020-17-03) /3/ SDR YENA2024061800890Pressure Blkhd · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE BULKHEAD @ FR 35 & STR 30L CRACKS AT FASTENER HOLES – TIME LIMITED REPAIR; AEM EA 53-9002-24 REV 0 (COVER & PARTS 1-5) RDAF 81405207/004/2024#A, 81405207 /4/ AIRBUS TECHNICAL DISPOSITION TD/8SDR YENA2024061800873Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE BULKHEAD @ FR 35 & STR 30L / CRACKS AT FASTENER HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEM EA 53-9002-24 REV 0 (COVER & PARTS 1-5) /2/ AIRBUS STAGE 1 RDAF 81405207/004/2024#A /3/ AIRBUS DOSSSDR YENA2024061800872Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / SKIN BETWEEN FR 11-12 & STGR 17L-19L / DENTS & CRACK - TEMPORARY REPAIR; /1/ STS EA 125-2024-048 REV. IR /2/ ETD2024-190-016478 REV / WITH ANAC 8165205 /3/ PREVIOUS EC E24-692-01 DURING CURRENT DROP-IN CHECK,SDR YENA2024062100890Skin · crackedDURING CURRENT DROP-IN CHECK, 2 DENTS, ONE OF WHICH HAS A CRACK DAMAGE, ON THE FWD SKIN BETWEEN FR 11-12 & STGR 17L-19L, WAS EVALUATED AFTER THE A/C WAS FERRIED WITH A TEMPORARY REPAIR. PREVIOUS EC, FOR ORIGINAL DAMAGE AND MX FERRY TEMP REPAIR ACCOMPLISHMENTSDR YENA2024052100769Sensor · failedFLT#984, RDU-BOS. 'STEER FAIL; REMOVED AND REPLACED STEERING FEEDBACK SENSOR #2 IAW AMM 32-53-09. FAULT CLEARED. FUNCTIONAL TEST GOOD IAW AMM 32-53-09. A/C OK FOR CONT. SVC.'SDR YENA2024031200397Shear Tie · corrodedDURING HEAVY MAINTENANCE: CPCP CORROSION ON SHARE CLIP BTW FR88 STGR 28RH-29RH AT AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00007) REF: TOMX W/O 2482 N/R 00270 REPLACED PER EMB 190 SRM 51-41-02 SRM 51-41-01 AND SRM 51-43-03.SDR YENA2024031200396Shear Tie · corrodedDURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR87 STGR 28RH-29RH AFT CARGO; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00013) REF: TOMX W/O 2482 N/R 00272 REPLACED PER EMB 190 SRM 51-41-02 AND SRM 51-41-01.SDR YENA2024031200395Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR75 AND STRG28/27 RH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200394Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR82 AND STRG28/27 RH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200393Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200392Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/27 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200391Skin · gougedDURING HEAVY MAINTENANCE: GOUGES ON EXTERNAL FORWARD FUSELAGE LOWER SKIN PANEL BTW FR 20 TO X=6232.5 AND STGR 28L-27L; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00037) FUR-E190-53-01188 CREATED, REF TOMEX WO 2482, NR 00025, EXTERNAL FORWARD FUSELAGE LOWER SKIN PSDR YENA2024031200390Spar · unknownDURING HEAVY MAINTENANCE: IN REF NRC 00365:REPLACE INBD UPPER SPAR AT RH PYLON; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00039) REF TOMEX WO 8619, NRC 00394, INBD UPPER SPAR AT RH PYLON WAS REPLACED PER EMB--190 S.R.M. 51-43-03, S.R.M. 51-43-04.SDR YENA2024031200389Skin · unknownDURING HEAVY MAINTENANCE: DENT ON EXTERNAL DOUBLER OF PREVIOUS REPAIR AND FUSELAGE SKIN BTW FR 23-24 AND STGR 15L-16L AT CENTER FUSELAGE I EXTERNAL SIDE SKIN; (RESOLVED ON W/O: 1288392 TASKCARD: NR-00041) REF TOMEX WO 2482, NRC 00022, EXTERNAL DOUBLER OF PREVISDR YENA2024031200388Floor Support · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM BTW FR13 AND FR 14, Y= 280RH (W1); CMOR: REMOVE CORROSION, EVALUATE AND IF IT IS NECESSARY REPAIR PER EMB 190 SRM 51-10-03, SRM 51-12-01, SRM 53-10-10 ASDR YENA2024031200387Stringer · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON STRINGER BTW FR76/78 AND STRG 29 RH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION, EVALUATE AND IF IT IS NECESSARY REPLACE PER EMB-190 SRM 51-12-01 SRM 51-10-03, SRM 53-23-03 AD 5SDR YENA2024031200386Frame · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FRAME 80 BTW STRG28/27 RH ON AFT CARGO COMPARTMENT STRUCTURE; CMOR:REMOVE CORROSION, EVALUATE AND IF IT IS NECESSARY REPAIR PER EMB-190 SRM 51-12-01, SRM 51-10-03, ETI-190-24-036. REV. 2SDR YENA2024031200385Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/27 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200384Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR76 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200383Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR77 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200382Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR79 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REMOVE CORROSION AND EVALUATE PER EMB-190 SRM 51-10-03, SRM 51-12-01, SRM 51-75-16 AND REPLACE IF NECESSARY PER ESDR YENA2024031200381Shear Tie · corrodedDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON SHEAR CLIP BTW FR82 AND STRG28/29 LH ON AFT CARGO COMPARTMENT STRUCTURE; REF: TOMX W/O 2482 N/R -00237 REPLACED PER EMB 190- SRM 51-41-01 AND 51-41-02. (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200380Shear Tie · corrodedDURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR87 STGR 28RH-29RH AFT CARGO; REF: TOMX W/O 2482 N/R 00272 REPLACED PER EMB 190 SRM 51-41-02 AND SRM 51-41-01. (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200379Shear Tie · corrodedDURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR87 STGR 27RH-28RH AFT CARGO; REF: TOMX W/O 2482 N/R 00272 REPLACED PER EMB 190 SRM 51-41-02 AND SRM 51-41-01. (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200378Shear Tie · corrodedDURING HEAVY MAINTENANCE: CPCP CORROSION ON SHARE CLIP BTW FR85 STGR 27RH - 28RH AFT CARGO; REF: TOMX W/O 2482 N/R 00278 REPLACED PER EMB 190 SRM 51-41-01 AND 51-41-02. (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200377Shear Tie · corrodedDURING HEAVY MAINTENANCE: CPCP- CORROSION ON SHARE CLIP BTW FR86 STGR 27RH-28RH AFT CARGO; REF: TOMX W/O 2482 N/R -00275 REPLACED PER EMB 190- SRM 51-41-01 AND 51-41-02. (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200376Shear Tie · corrodedDURING HEAVY MAINTENANCE: CPCP CORROSION ON SHARE CLIP BTW FR88 STGR 27RH-STGR 28RH AFT CARGO COMPARTMENT STRUCTURE; REF: TOMX W/O 2482 N/R 00271 SHARE CLIP REPLACED PER EMB 190 SRM 51-41-02 AND SRM 51-43-03. (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200375Seat Track · corrodedDURING HEAVY MAINTENANCE: CPCP CORROSION ON FLOOR STRUCTURE SEAT TRACK BEAM FR17 AND FR18 AND Y=300RH (W1); REF: TOMX W/O 2482 N/R 00182 REPAIRED PER EMB 190 SRM 53-10-10 REP 56. (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200374Seat Track · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE / RH FLOOR TRACK / BTWN FR13-14 & Y=273 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200373Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / SKIN / BTW FR 23-24 & STGR 15L-16L / PREVIOUS DOUBLER / DENT - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200372Frame · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 80 / BTWN STR 27R-28R / CORROSION - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)SDR YENA2024031200371Skin · gougedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / LOWER SKIN / BTWN FR20-21 & STR 27LH-28LH / GOUGES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR YENA2023061900673Shutoff Valve · failedFLT#1082, RIC-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO RIC) 'BLEED (1) ONE FAIL ON CLIMBOUT; REMOVED AND REPLACED #1 NAPRSOV IN REF AMM 36-11-03. OPS CHECK GOOD AND FOUND HP CHECK VALVE MISALIGNED KEY. REINSTALLED IN THE RIGHT POSITION AND LEAK-CHECK THE LSDR YENA2022121601259Connector · damagedFLT#2324, MCO-DCA. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO MCO) ' SLAT FAIL MSG AFTER BIRD STRIKE. THE FLAP HANDLE WAS NOT MOVED. RETURNED TO THE AIRPORT FOR AN UNDERWEIGHT LANDING; FOUND RH SLAT SKEW SENSOR #4 SKEW CONNECTION DAMAGEDSDR YENA2022120901235Lever · out of adjustFLT#1132, LGA-BOS. L1 DOOR ARMING LEVER RAISES APPROX 1/2 INCH IN-FLIGHT, RESULTING IN ARMING INDICATION TO NOT BEING VISIBLE; ADJUSTED ARMED/DISARMED VISUAL INDICATION ROD END IN REF WITH AMM 52-11-22. THE ARMING LEVER NOW ARMS AND DISARMS SMOOTHLY AND INDICASDR YENA2022090100848Slide · failedFLT#8583, JFK-MCN. 'WHILE WORKING L2 DOOR INDICATION MDDR FOUND DOOR SLIDE BUSTLE PIN LANYARD DISCONNECTED (TOO SHORT TO REATTACH); REF EAMS N/R 00007, REMOVED AND REPLACED L2 EMERGENCY EVACUATION SLIDE ASSEMBLY PER E-190 AMM TASK 25-65-01-400-801-A. 'SDR YENA2022090100849Skin · dentedFLT#8583, JFK-MCN. 'W/O 1198428 ASSIGNED, AFT JACK PAD AREA DAMAGE REPAIR, W/O 1198975. ENCOMPASSED IN EAMS WO H8790; ACFT REG:323JB ACFT SN: 19000384, ACFT TAT: 30828.31, ACFT TAC:20363, COMPLIED WITH THE FOLLOWING INSPECTIONS: MISC WORK/ AIRCRAFT DROP IN PERSDR YENA2022022500092None · noneFLT # 1899, FLL-HAV(AIR TURNBACK TO FLL). DURING ALL PHASES OF FLIGHT AN ABNORMAL AMOUNT OF RUDDER PRESSURE AND TRIM WAS REQUIRED TO KEEP AIRCRAFT IN COORDINATED FLIGHT. DURING CLIMB OUT RUDDER TRIM NEEDED TO BE CONTINUALLY ADDED TO THE AIRCRAFT. LEFT RUDDER TSDR YENA2021062900408Skin · gougedFLT 6102, BNA-BOS. FUSELAGE / CENTER FUSELAGE I / EXTERNAL SKIN FR23-24 & STGR15L-16L / DENT & GOUGE - PERMANENT REPAIR (EC E21-714-01); CLASSIFIED AS MAJOR REPAIR.SDR YENA2020081700428Pintle Pin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON HOLES SHOCK STRUT REAR PINTLE PINS ON RH MAIN LANDING GEAR; REMOVED AND REPLACED SHOCK STRUT REAR PINTLE PIN ON RH MLG 2821-0025 SN L1361 FOR A SERVICEABLE PINTLE PIN PN 2821-0025 SN L2285 AS PER AMM 32-11-01-400-8SDR YENA2020081700427Pintle Pin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON HOLES LEG FWD PINTLE PIN ON LH MAIN LANDING GEAR; REMOVED AND REPLACED FWD PINTLE PIN ON LH MLG 2821-0067 SN L1413 FOR A NEW PINTLE PIN PN 2821-0067 SN L2381 AS PER AMM 32-11-01-000-801-B STEP 21(13) (A) (B) (E) (I) (J) SDR YENA2020081700426Pintle Pin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON HOLES LEG FWD PINTLE PINS ON LH MAIN LANDING GEAR; REMOVED AND REPLACED REAR PINTLE PIN ON LH MAIN LANDING GEAR PN 2821-0025 SN L1377 FRO NEW PINTLE PIN PN 2821-0025 SN 2285 IAW E190 AMM 32-11-01-000-801-BSDR YENA2020081700425Pintle Pin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON HOLES LEG FWD PINTLE PINS ON TH MAIN LANDING GEAR; REMOVED SHOCK STRUT FWD PINTLE PIN PN 2821-0067 SN L1390 AND INSTALLED SERVICABLE SHOCK STRUT FWD PINTLE PIN PN 2821-0067 SN L2385 ON RH MAIN LANDING GEAR IAW E190 AMM 32SDR YENA201909020497Wire Harness · damagedSUPPLEMENTAL INFORMATION: FLT 860, PHL-BOS. EMERGENCY DECLARED. RETURNED TO FIELD. ENG 2 FIRE INDICATION IN FLIGHT; REF LOG PAGE 2702474 ITEM #1, FOUND W8C HARNESS WITH HEAT DAMAGE AND NEEDS REPLACEMENT. REPLACED HARNESS PER EMM 72-00-00 ON #2 ENG W9B HARNESS.SDR YENA2018121840856Battery Pack · failedFT # 112, ORD-BOS. EMERGENCY LIGHT POWER UNIT #6 FAILED FUNCTIONAL TEST; REPLACED ELPU #6 IAW AMM 33-50-01. ACFT OK FOR SERVICESDR YENA2018121840855Battery Pack · failedFT # 112, ORD-BOS. EMERGENCY LIGHT POWER UNIT #1 FAILED FUNCTIONAL TEST; REPLACED ELPU #1 IAW AMM 33-50-01. ACFT OK FOR SERVICESDR YENA201709220781Power Supply · no testFOUND THE MID, RT FAIRING EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE POWER SUPPLY IAW AMM 33-50-01.SDR YENA20161022943Windshield · failedDURING CLIMB OUT THROUGH 16,500 FT, PILOT REPORTED HEARING A POP ON F/O SIDE. IMMEDIATELY AFTER HEARING THE POP, A RUSH OF AIR WAS HEARD, WHICH CONTINUED THROUGHOUT THE REST OF THE FLIGHT. AFTER THE POP SOUND, THE ACFT PRESSURE BEGAN TO CLIMB TO APPROX 4500-50
Back to N323JB, cancelled Jun 3, 2026