N184JB
Service difficulty reports · 50
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 = 'N184JB' 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 = 'N184JB' 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 YENA2023110801362Unknown · unknownDURING HEAVY MAINTENANCE: RH BEAM CORRODED BETWEEN FR 86 AND FR 89 Y+10.5; BLENDED RH BEAM BETWEEN FR 86-89 IAW EMB 190 SRM 51-10-03. FOUND TO BE OUT OF LIMITS REF EMB 190 SRM 53-23-10/AD52. REMOVED AND REPLACED RH BEAM PN 170-65669-004 BETWEEN FR86 AND FR89 YSDR YENA2023110801361Unknown · unknownDURING HEAVY MAINTENANCE: LH BEAM CORRODED FR 86 AND FR 87 Y-10.R MARKED IN RED; BLENDED LH BEAM AT FR 86-87 IAW EMB 190 SRM 51-10-03 PART HAS 100% MATERIAL LOSS PART REMOVED AND REPLACED LH BEAM PN 170-65669-003 AT FR 89Y-10.5 PER EMB -190 SRM 51-40-08 ALL WOSDR YENA2023110801360Unknown · unknownDURING HEAVY MAINTENANCE: FWD WET AREA FLOOR STRUCTURE TRACK RIGHT SUPPORT AT FRAME 1714 AND 13 Y+10.5 HAS CORROSION MARKED IN RED; BLENDED CORROSION ON RH SEAT TRACK AT FR-14 PER EMB 190 SRM 51-10-03 BLENDED AREA AT FR -13 MEASURES MATERIAL LOSS .019 ALLOWED SDR YENA2023110801359Unknown · unknownDURING HEAVY MAINTENANCE: FWD WET AREA FLOOR STRUCTURE TRACK LEFT SUPPORT @FRAME 19Y-10.5 HAS CORROSION MANRED IN RED; BLENDED CORROSION ON RH SEAT TRACK AT FR -14PER EMB 190 SRM 51-10-03 DAMAGE MEASEURES L=.800 W=.600 H=.52 ORIGINAL THICKNESS IS .07 AND REMAISDR YENA2022021800075None · noneFLT # 2028, MCO-EWR. ON DEPARTURE AT 1000 FT AGL BOTH RADIO ALTIMETERS TURNED AMBER. FO'S HUD PROVIDED ERRONEOUS DATA ; COMPLIED WITH INFO NOTICE 2022-T001, NO DEFECTS NOTED, OK FOR SERVICE SUSPECT 5G INTERFERENCE. MCC DAVID NOTIFIED PER AMM 34-31-00-710-801-ASDR YENA2021121300833Slide · deployedFLT 1274, CHS-JFK. WHILE T/C C2514012-01 "DOOR SLIDE FIRING CABLE TENSION", THERE WAS A INADVERTENTLY SLIDE DEPLOYMENT ON L2 DOOR ; R/R L2 DOOR SLIDE IAW AMM 25-65-01.SDR YENA2021021900127Battery · no testFLT # 1141, BDL-PBI. R1 EPSU FAILED OPS TEST ; R & R R1 SVC DOOR POSITION EPSU W/SERVICEABLE ASSY PER AMM 33-50-01. OPS TEST OK (CORRECT REGISTRATION NUMBER AND DATE)SDR YENA202003020206Rib · crackedDURING HEAVY MAINTENANCE, RH WING LEADING EDGE RIB 17 HAS CRACK; REF AEROMAN 2020-56275: R & R RIB 17 ON LEADING EDGE RH WING IAW E190 SRM 51-40-08 & DRAWING 190-31005-405.SDR YENA201906270373Unknown · odorSUPPLEMENTAL INFORMATION: FLT 1037, SJU-SDQ. RETURNED TO FIELD. OVERWHELMING DIRTY SOCK ODOR AFTER TAKEOFF. WE BOTH FELT NAUSEOUS AND HAD HEADACHES. INFLIGHT DID NOT SMELL IT IMMEDIATELY, BUT DID AFTER ABOUT 5 MINS; PERFORMED OPERATIONAL CHECK REF 71-00-01 ALSSDR YENA201901010003Uplock · faultyFT 1210, JAX-MCO. NOSE GEAR INDICATES UP, THEN EVERY 5 SECONDS AMBER, THEN UP. WE CAN FEEL IT MOVING. R&R NLG UPLOCK PER AMM 32-32-03. OPS CK GOOD.SDR YENA2018111950780Power Supply · failedFT # 1354, DCA-BOS. LH LOWER EXTERNAL EMERGENCY EXIT LIGHT INOP; R & R POWER SUPPLY #6, OPS NORMAL REF AMM 33-50-01.SDR YENA201710230858Seal · contaminatedLOUD SQUEAL NOISE FROM OVERWING EXIT AT 12D. OCCURRED ENTIRE FLIGHT ABOVE 10,000 FT. REMOVED & REINSTALLED THE RT OVERWING ESCAPE HATCH IAW AMM 52-21-00/400. INSPECTED DOOR LOCK MECHANISM SEAL IAW AMM 52-21-20/600 & FOUND BUILD UP OF DEBRIS ON THE SEAL. REMOVSDR YENA201710110837Processor · failedEMERGENCY DECLARED ON APPROACH. CARGO SMOKE AFT EICAS. RAN QRH. BOTTLE WAS DISCHARGED. AVNX MAU 3B FAULT. AFT CARGO SMOKE MESSAGE DETERMINED TO BE CAUSED BY FAULTY GIO 3B & NIC PROC 6, MAU 3, NIC 2.SDR YENA201710110836Processor · failedEMERGENCY DECLARED ON APPROACH HAD A CARGO SMOKE AFT ON THE EICAS. RAN QRH. BOTTLE WAS DISCHARGED. AVNX MAU 3B FAULT, CARGO AFT SMOKE MESSAGE DETERMINED TO BE CAUSED BY FAULTY GIO 3B & NIC PROC 6 MAU 3 NIC 2.SDR YENA201709150767Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION DISCOVERED ON THE FLOOR SUPPORT FRAMES 86 TO 89. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-03, AND DRAWING 170-65660-433.SDR YENA201709150766Floor Support · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, FRAMES 86 TO 89. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-03, AND DRAWING 170-65660-433.SDR YENA201612021037Shear Tie · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON SHEAR TIE AT FRAME 16, BETWEEN STRINGERS 27 AND 28R. R & R THE SHEAR TIE IAW SRM 51-42-02 AND 51-43-03.SDR YENA201612021036Shear Tie · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON SHEAR TIE AT FRAME 17 BETWEEN STRINGERS 27 - 28R. R & R THE SHEAR TIE IAW SRM 51-41-02, AND 51-43-03.SDR YENA20160606544Engine · vibrationFLIGHT CREW REPORTED HIGH ENGINE VIBRATION ON DEPARTURE. ACFT DIVERTED DUE TO HIGH VIBRATION AND ENGINE EXCEEDANCE ON NR 1 ENGINE. NR 1 ENGINE R & R.SDR YENA20150629238Connector · malfunctionedCOCKPIT EMERGENCY LIGHT INOPERATIVE. RESET CONNECTOR AT RT EMERGENCY LIGHT BATTERY PACK. EMERGENCY LIGHT SYSTEM OK.SDR YENA20150425093Display · failedDURING FLIGHT, ODOR OF HOT PLASTIC "MFD 2 OVHT". PERFORMED AND COMPLIED WITH INSPECTION FOR ABNORMAL ODOR OF SMOKE IAW 21-20-00-810-801-A. R & R NR 2 MFD IAW AMM 31-61-01. OPS CHECK GOOD.SDR YENA20150225030Shear Tie · corrodedON MAINTENANCE CHECK, FOUND FRAME 81 BETWEEN STR 27 & 28R HAS ONE CORRODED SHEAR CLIP. REF EAMS NR 4490-1611, REMOVED DAMAGE SHEAR CLIP, PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED NEW SHEAR CLIP. ALL WORK ACCOMPLISHED IAW EA E15-146-01.SDR YENA20140707127Circuit Card · failedAIRCRAFT DIVERTED DUE TO AN INTERMITTENT FIRE INDICATION ON NR 1 ENGINE ITT GAUGE, NO ORAL WARNINGS, FIM 26-11-00-810-807A FAULT CODE 26110014UT1 GENERIC I/O MODULE 1, MAU 1 MOD 11/12, FAILED. R & R GEN I/O MOD MAU 1 SLOT 11/12. ACCOMPLISHED SUCCESSFUL TARGESDR YENA20130824185Pressure Switch · warning messagePARKING BRAKE NOT RELEASED MESSAGE ILLUMINATED. QRH COMPLETED STAYED ILLUMINATED. DECLARED EMERGENCY AND BRACED FOR LANDING. PERFORMED FIM TASK 32-41-00-810-852-A. FAULT CODE 32400001UT1. R & R EMERGENCY PARK BRAKE PRESSURE SWITCH SYS 1 IAW AMM 32-44-09. ASDR YENA20130824184Valve · warning messagePARKING BRAKE NOT RELEASED MESSAGE ILLUMINATED. QRH COMPLETED STAYED ILLUMINATED. DECLARED EMERGENCY AND BRACED FOR LANDING. PERFORMED FIM TASK 32-41-00-810-852-A. R & R DUAL EMERGENCY PARK BRAKE VALVE IAW AMM 32-44-01. ALL OPS AND LEAK CHECKED OK.SDR YENA20130725161Light · inoperativeDURING MX L1 AND L2 LOW LEVEL EMERGENCY LIGHT IDENTIFIERS HAS SECTIONS INOPERATIVE. R & R BOTH L1 AND L2 EXIT IDENTIFIERS LIGHT ASSY IAW AMM 33-50-15. OPS CHECK OK.SDR YENA20130725159Power Supply · failedDURING MX, RT OVERWING EMERGENCY LIGHT FOUND INOPERATIVE. R & R EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-01, OPS CHECKED GOOD.SDR YENA20120818582Hydraulic Line · rupturedFLT 1678 KIN-FLL, CREW DECLARED EMERGENCY DUE TO HYD 2 ELEC PUMP FAIL FOLLOWED BY HYD 2 LO QTY. QRH CALLED FOR CREW AWARENESS. QTY WAS 0 BUT PRESS WAS 2900. PHONE PATCH TO MX, ASKED CREW TO PUT HYD 2 ELEC SW TO ON. AT THAT POINT HYD 2 SYS FAILED. TROUBLESSDR YENA20120803570Hydraulic Line · leakingFLT 1055 JFK-PIT, HYDRAULIC SYSTEM 2 FAIL - FLUID ZERO QUANTITY AFTER NORMAL GEAR EXT / NO HYD OVERHEAT MSG. PERFORMED DETAIL VISUAL INSPECTION AND FOUND RETRACT/EXT HOSE ASSY LEAKING. REMOVED AND REPLACED HOSE ASSY IAW AMM 20-10-03. HYDRAULIC QTY LOW SERVISDR YENA20120522506Power Supply · inoperativeFLT 746 SJU-MCO FOUND OVERHEAD EMERGENCY LIGHT INOP ABOVE ROW 1. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW AMM 33-50-00, OPS CHECK NORMAL.SDR YENA20111126388Bypass Valve · failedFLT 974 FLL-BOS, AIRCRAFT DIVERTED TO MCO DUE TO CABIN AND FLIGHT DECK TEMPERATURE UNCONTROLLABLE, TEMP WAS MODULATING BETWEEN HOT AND COLD. REMOVED AND REPLACED NR 2 PACK BYPASS VALVE PER AMM 21-51-10-04 OPS CHECK OF TEMP CONTROL OK.SDR YENA20110928351Converter · faultyFLT 1080 CLT-JFK, BURNING OIL SMELL IN COCKPIT ON TAKEOFF. DUE TO HISTORY WITH RECIRCULATION FILTERS ALREADY REPLACED, THE TECHNICIAN REMOVED AND REPLACED LT OZONE CONVERTER PER AMM 36-30-00. LEAKS CHECK OK.SDR YENA20101010138Detector · shortedFLT 522 MCO-EWR, AIR TURNBACK TO MCO DUE TO NR 2 ENG BLEED LEAK EICAS MESSAGE WHILE CLIMBING THROUGH FL300. CREW PERFORMED QRH PROCEDURE AND MESSAGE EXTINGUISHED. FOUND LOOP 5 LEAK DETECTOR SHORTED. REMOVED AND REPLACED AS PER AMM 36-21-02.SDR YENA20101009137Warning System · false activationFLT 590 PBI-HPN, FLT CREW DECLARED EMERGENCY AND A/C DIVERTED TO MCO DUE TO BLEED 2 LEAK MSG IN FL 310. QRH PROCEDURE COMPLETED. BLEED 2 SELECTED OFF (XBLEED) CAS MSG EXTINGUISHED. INTERROGATED CMC FOUND BLEED 2 LEAK, ODS PACK LOOP 5 (RT BLD) [C1] /WRG FAULSDR YENA20100326043Turbine Blades · damagedFLT JB1224 LGB-PDX FLIGHT FROM LONG BEACH TO PORTLAND OREGON DIVERTED TO OAK DUE TO ENGINE NR 1 FIRE DETECTION FAIL MESSAGE DURING CRUISE. PERFORMED QRH PROCEDURES AND LANDED UNEVENTFUL. INSPECTION OF NR 1 ENGINE FOUND LOW PRESSURE TURBINE BLADE DAMAGE LPT STSDR YENA20091211170Connector · looseFLT JB1401 FLL-AUS "STEER FAIL" AMBER EICAS MESSAGE DISPLAYED AT GEAR EXTENSION, LOSS OF NOSE WHEEL STEERING ON LANDING AIRCRAFT TOWED TO GATE. MX PERFORMED TROUBLESHOOTING NO FAULT CODE FOUND, RESET AIRCRAFT AND ACCOMPLISHED STEERING ELECTRONIC SYSTEM INSPECSDR YENA20091113155Actuator · failedFLT JB78 - MCO-JFK "SLAT FAIL" AT ZERO DURING DESCENT FOR LANDING, SLATS SELECTED AND FAILED TO MOVE. CREW NOTIFIED ATC, AIRCRAFT LANDED SAFELY. MX TROUBLESHOT PER AMM FIM 27-81-00 FOUND RIGHT WING SLAT ACTUATOR NR 4 AT FAULT, REMOVED AND REPLACED RT WING NRSDR YENA20090913112Bleed Air Sys · leakingFLT 1326 BWI-BOS - DEPARTED BWI WITH LEFT ENGINE BLEED DEFERRED. ON CLIMBOUT AT 19000FT THE NR 2 ENGINE BLEED LEAK EICAS MESSAGE APPEARED. LEVELED OUT AT 20000FT TO EVALUATE SITUATION. CONFIRMED BLEED LEAK INDICATION REQUESTED DESCENT TO 10000FT. AT 12000SDR YENA20090906110Hinge · looseFLT 1119 - COCKPIT DOOR UNATTACHED FROM DOOR FRAME. FOUND UPPER HINGE LOOSE, SECURED UPPER HINGE AND INSTALLED COCKPIT DOOR AS PER AMM 52-51-01. OPS CHECK GOOD.SDR YENA20090901107Pin · damagedFLT 1417, AT FLT 280. BLEED 2 LEAK. REMOVED AND REPLACED LEAK DETECTOR CERAMIC PINS AT (P2146) AND (J2148) LOCATED FWD TOP PYLON IAW AMM 36-20-01. CHANNEL NR2 OPS CHECK GOOD.SDR YENA20090728081Computer · failedFLT 1068, AUS-JFK, DIVERTED TO BNA, "AVNX MAU 1A FAIL" IN FLIGHT AT 370, AUTO PILOT DISCONNECT AND MULTIPLE ASSOCIATED FAILURES ON EICAS. TROUBLESHOT MAU 1A FAIL FAULT CODE 45452143CMC IAW EMB 190 FIM 45-45-00-810-939-A00. MAU1 NIC PROC 1 CHECKS FAULTY, REMOVSDR YENA20090616062Sensor · failedFLT 462, RSW-BOS - THE BLEED 2 LEAK MSG APPEARED ALONG WITH LEAK ROW ON 2 BUTTON. RAN QRH, ALL INDICATIONS REMAINED THE SAME. DIVERTED TO MCO. PERFORMED FIM TASK 36-21-00-810-804A, FOUND FAILURE OF LEAK DETECTOR LOOP 5 SEGMENT 1RT0186 CHANNEL 1. REMOVED & SDR YENA20090522052Controller · failedFLT 1402, AUS-SFO, CLIMBING THRU FL 280, BLEED 2 LEAK AMBER EICAS MESSAGE ILLUMINATED (ENGINE BLEED SYS-SINGLE-NO ICING). RETURN TO AUS DUE NR 1 BLEED ON MEL. REF FIM 36-21-00-810-804A. REMOVED AND REPLACED BOTH AMS CONTROLLER PROCESSOR MODULES (CH A&B) AS PSDR YENA20090512046Module · failedFLT 1068, AUS-JFK, STEER FAIL ON APPROACH WHEN DOWN LANDING GEAR. DECLARED EMERGENCY, FOLLOWED QRH. REMOVED AND REPLACED NR 2 STEERING FEEDBACK SENSOR NR 2 FOR TROUBLESHOOTING. REMOVED & REPLACED STEERING MODULE PER AMM 32-53-01. PERFORMED ADJUSTMENT & FEESDR YENA20090410033Warning System · malfunctionedFLT 337, IAD-MCO, "SLAT FAIL" EICAS MESSAGE ON SLAT EXTENSION, 220 KIAS AT 6000FT (SPD BRK EXT) LANDED FLAPS "2" SLAT "0" PER QRH. APP SPEED 166 KIAS BRAKE TEMP PEAKED AT 315 DEG. FAULT DETERMINED TO BE TRANSITORY CONDITION PER E190 FIM 27-81-00-810-802-A. SDR YENA20090306023Indication Sys · malfunctionedFLT 5110, BNA-JFK - AIR RETURN TO BNA, ENG 1 FUEL LO PRESS, AMBER MSG AT 8000FT AFTER DEPARTURE, ACCOMPLISHED OPS TEST OF FUEL PRESS. SYSTEM PER 73-31-00-801-803-A. OPS TEST GOOD. ACCOMPLISHED ENG FEED EJECTOR PUMP OPS CHECK PER AMM 28-21-13, REF FIM 28-21-SDR YENA20090217013Unknown · smokeFLT 115 JFK-MSY - SMOKE IN COCKPIT AFTER TAKEOFF. SMELL THROUGHOUT A/C. DOME LIGHT TURNED ON, SMOKE CONFIRMED. ACCOMPLISHED MX PROCEDURES. PERFORMED POWER ASSURANCE TEST ON BOTH ENGS PER AMM 71-00-00 AND BLEED TEST PER AMM 36-11-00, NO ODOR OR SMOKE PRESENSDR YENA2008087Unknown · odorSTRONG PLASTIC BURNING ODOR, AFTER TAKEOFF UNTIL 3000 FEET. ODOR RETURNED ON DOWN WIND AT 3000 FEET UNTIL TOUCHDOWN. PERFORMED FIM TASK 21-20-00-801A. NO FURTHER DEFECT NOTED. RAN AIR CONDITIONER (CREW) CAN NOT DUPLICATE ON THE GROUND. ACFT OK TO CONTINUE. (SDR YENA2007056Battery · overtempON TAKEOFF ROLL BATTERY NR 2 OVERTEMP EICAS MESSAGE. T/S TSM 24-36-810-804-A. REMOVED AND REPLACED NR 2 MAIN BATTERY, GROUND CHECK OK.SDR YENA200605Pitot Head · unknownAIRCRAFT EXPERIENCED LOSS OF ADS SYSTEM NR 3 & NR 4. CMC SHOWED NR 3 & NR 4 (SMART PROBES) PITOT/STATIC AOA SENSOR. REMOVED & REPLACED NR 3 AND NR 4 INTEGRATED PITOT/STATIC AOA SENSOR IAW AMM 34-13-01, OPS CHECK. NO FAULT NOTED.
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