N592HA
Service difficulty reports not matched to an aircraft · 188
They name N592HA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N592HA' AND registry_match IS NULL 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 = 'N592HA' AND registry_match IS NULL 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 HALA2018070700322Actuator · leakingAIR TURN BACK LEFT HYD QTY LOSS TO .70RF (STARTED FLIGHT WITH .94) REPEAT WRITEUP SEE PAGE 731445 AIR TURN BACK. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW AMM 27-21-15. OPS CHECK NORMAL.SDR HALA2018061100291Fmu · malfunctionedAIR TURNBACK, LT FMC FAILED. RAN QRH, FMC 2, LT FMC REMAINED INOPERATIVE. REMOVED AND REPLACED THE LEFT FMC IAW AMM 34-61-01-424-005. PERFORMED A CROSS LOAD IAW AMM 34-61-00-422-009-005. NO FAULT NOTED, OPS CHECKED GOOD ON GROUND, OK TO CONTINUE.SDR HALA2018060400271Fmc · malfunctionedLEFT FMC FAILED DURING CRUISE, COMPLIED WITH QRH FOR FMC FAIL, RESET FMC. NO DEFECTS DURING LANDING. PERFORMED TROUBLESHOOTING IAW FIM 34-61 FAULT TREE 849. NO FAULTS NOTED. OPS CHECKED IAW AMM 34-61-00-715-001-001. NO DEFECTS NOTED. CLEANED COOLING VENTS ASDR HALA208051700236Autopilot Sys · malfunctionedAT 2800 FT , JUST AFTER GLIDESLOPE CAPTURE FOR ILS WITH CTR AUTOPILOT ENGAGED, AUTOPILOT ABRUPTLY PITCHED DOWN TOWARD F/D, COMMAND INDICATING 8 DEG. NOSE DOWN. AUTOPILOT NAV DISCONNECTED MANUALLY TO MAINTAIN AIRCRAFT CONTROL. GLIDESLOPE INDICATION SHOWED ON GLSDR HALA2018051700234Unknown · smokeOVEN F1053 STARTED SMOKING WHEN USED. PERFORMED AN OPS CHECK IAW AMM 25-31-00. NO FAULT FOUND. OK FOR SERVICE.SDR HALA2018041600169Computer · warning messageAIR TURNBACK DUE TO A LT FMC FAIL EICAS MESSAGE. REPLACED THE LEFT FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-01, FMC DATA CROSSLOADED IAW AMM 34-61-00. OPS CHECKED GOOD. OK TO CONTINUE.SDR HALA2018041100164Warning Message · false activationDURING INITIAL CLIMB OUT THRU 5000 FT, DUCT PRESSURE DROPPED, THEN JUMPED TO APPROXIMATELY 55 PSI FOR A SHORT BURST, 20 SECONDS, THEN STABILIZED. THROTTLES AT CLIMB POWER. CONCURRENTLY FIRST FA REPORTED A DISTINCT ODOR AND POSSIBLE SMALL AMOUNT OF SMOKE. ACSDR HALA0218040900146Warning Message · false activationCABIN ALTITUDE AUTO 2 STATUS MESSAGE AFTER LEVEL OFF AT CRUISE. PERFORMED TROUBLESHOOTING PER FIM 21-31/803, NO FAULTS RECORDED. OPS CHECKED AND FOUND OK FOR SERVICESDR HALA2018040300133Slide · unwanted deployR3 OVERWING EXIT SLIDE DEPLOYED. REPLACED THE RT OVERWING SLIDE IAW AMM 25-65-05.SDR HALA2018032000113Warning Message · illuminatedRIGHT ENGINE PRV EICAS MESSAGE AND RT ENGINE BLEED ANNUNCIATOR LIGHT. DIVERTED TO THE NEAREST AIRPORT, A NORMAL LANDING WAS MADE.SDR HALA2018031300092Bleed Valve · fluctuatesRIGHT HIGH PRESSURE BLEED VALVE FLUCTUATING FROM 20-40 PSI DURING DESCENT WITH THRUST NEAR IDLE. PERFORMED AIR SUPPLY DISTRIBUTION TEST IAW AMM 36-11-00-715-149. AIR SUPPLY BITE TEST GOOD NO FAULTS NOTED, OK FOR SERVICE.SDR HALA2018031300091Switch · malfunctionedLEFT PACK TEMP ILLUMINATED, FOLLOWED QRH. AFTER 5 MINUTE COOL DOWN, ATTEMPTED A RESET. LEFT PACK TEMP WOULD NOT RESET. TURNED LEFT PACK OFF. REMOVED AND REPLACED THE LT PACK OVERHEAT SWITCH IAW AMM 21-51-18, OPS CHECKED GOOD. OK FOR SERVICE AND REPLACEDSDR HALA2018030700071Generator · leakingFOUND THE APU GENERATOR LEAKING OIL AROUND GENERATOR LEAD TERMINALS. REPLACED APU GENERATOR IAW AMM 21-21-01. SYSTEM TESTED AND LEAK CHECKED GOOD. OK FOR SERVICE.SDR HALA2018012500012Control Unit · faultyETOPS SIGNIFICANT SYSTEM - APU FAULT 1ST APU START ATTEMPT. 2ND APU START OK AFTER LANDING. BITE CHECK NO FAULT NOTED. CONDITION SAME, CHANGED IGNITER PER AMM 49-41-02-404-406, CONDITION SAME. REPLACED APU CONTROL UNIT PER AMM 49-61-05-404-008. NO FAULT NOTED.SDR HALA2018012500011Ecu · failedDURING CLIMB OUT, RECEIVED APU FAULT EICAS MESSAGE DURING AN APU VERIFICATION FLIGHT. FAILED VERIFICATION. COMPLIED WITH QRH APU STARTED. PERFORMED APU BITE TEST SHOWS P2 SENSOR ON SUMMARY, MINI FLAG 16, REMOVED AND REPLACED THE ECU IAW AMM 49-61-05-004-SDR HALA2018012300008Warning System · false activationETOPS SIGNIFICANT SYSTEM - APU FAULT EICAS QRH PROCEDURE COMPLETED. SUCCESSFUL START ON 2ND ATTEMPT. NO FAULTS NOTED. OPS CHECK GOOD. VISUAL OIL LEVEL CHECK GOOD. NOTIFIED MOC AND NO PRIOR HISTORY. AIRCRAFT OK FOR SVC.SDR HALA2017102500261Controller · unknownETOPS SIGNIFICANT SYSTEM, RIGHT ENGINE PRV EICAS IN DESCENT BETWEEN FL230 AND 17000 FT. REPLACED PRVC PER AMM 36-11-19.SDR HALA2017102000257Display · malfunctionedISFD DISPLAYING OUT OF ORDER. IAW FIM 34-24, FAULT TREE 804, REMOVED AND REPLACED ISFD IAW AMM 34-24-03. FUNCTIONAL TESTED OK. OK FOR SERVICE.SDR HALA2017082800240Sense Line · looseON DESCENT FROM FL250 TO FL230 BLEED DUCT PRESS FLUCTUATED BTN 25 TO 35 PSI. FOUND RT ENG PRSOV PRESSURE SENSE LINE LOOSE AND PACKING DAMAGED. REPLACED PACKING AND TIGHTENED SENSE LINE.SDR HALA2017082810237Sense Line · damagedETOPS / ON DESCENT FROM FL250 TO FL230 BLEED DUCT PRESS FLUCTUATED BTN 25 TO 35 PSI. FOUND RT ENG PRSOV PRESSURE SENSE LINE LOOSE AND PACKING DAMAGED. REPLACED PACKING AND TIGHTENED SENSE LINE.SDR HALA2017072400207Adc · malfunctionedRT BLEED LIGHT, FOLLOWED BY RT PRV EICAS, DURING 300FPM DESCENT FROM FL380 TO 370. ACCOMPANIED BY DUCT PRESSURE FLUCTUATION BETWEEN 20-35PSI. CHECKED AIR SUPPLY BITE MODULE, NO FAULT FOUND. CLEARED MESSAGE. PERFORMED BLEED VALVE CHECK BY ENGINE RUN IAW AMM 3SDR HALA2017072100204Pump · leakingLEFT HYDRAULIC SYSTEM FLUID QUANTITY 0.82 ON AIRCRAFT ARRIVAL. FOUND A LEAK FROM THE LEFT EDP. REPLACED THE PUMP, ENGINE IDLE RUN 5 MINUTES IAW AMM 29-11-05. NO LEAK FOUND. SERVICED HYDRAULIC FLUID TO 1.06 IAW AMM 12-12-01. OK FOR SERVICE.SDR HALA2017071900197Hf Comm · malfunctionedL HF RADIO WOULD NOT TUNE INITIALLY THE TONE WAS CONTINUOUS FOR MORE THAN 30 SEC. EVENTUALLY WAS ABLE TO TUNE AFTER MANY REATTEMPTS. PERFORMED TSK 23-11-FT 84 OPS CHECK GOOD NO FAULTS NOTED A/C OK FOR CONTINUED SERVICE.SDR HALA2017070300173Fmu · faultyIN CRUISE FLT AT FL370 WHEN THROTTLE IS RETARDED TO APPROX 1.13 EPR ON THE RT ENGINE, THE ENGINE SURGES. NOTED + - 3 EPR, + - .5 N1, ALSO RT PAC DUCT PRESSURE CYCLES FROM LOW TO HIGH FLOW 42 - 25 PSI. IN SUMMARY RT ENG SURGES AT LOW POWER SETTING. REMOVED RT FSDR HALA2017062200162Bleed Air Sys · inoperativeNR 2 ENGINE BLEED AIR INOPERATIVE. REMOVED AND REPLACED PRSOV IAW AMM 36-11-09. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2017062000160Lug · damagedEICAS MESSAGE FOR THE RT ENG FIRE NR 1 LOOP. REPLACED LUGS AT TS681-A AND TS683-A IAW WDM 26-11-21. GROUND OPS CHECKED OK IAW AMM 36-11-00. OK FOR SERVICE.SDR HALA2017050800116Unknown · odorON COMING FLIGHT ATTENDANTS REPORTED ELECTRICAL SMELL IN MID GALLEY AREA UPON BOARDING AIRCRAFT. OPERATED ALL OVENS, CHILLERS, NO ABNORMAL SMELLS, OPERATED COFFEEMAKERS NO ABNORMAL SMELLS DETECTED. RAN NR 1, NR 2 ENG INDEPENDENTLY, RAN PACKS INDEPENDENTLY, NO SDR HALA2017041000095Power Supply · inoperativeFOUND 2 EMERGENCY LIGHTS INOP. RIGHT SIDE WING SLIDE ILLUMINATION LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY (M733) PER AMM 33-51-07. OPS CHECK GOOD, OK FOR SERVICE.SDR HALA2017032800082Fan · failedELECRICAL ODOR NOTED IN THE COCKPIT, THEN CABIN CALLED REPORTING THE ODOR, QRH FOR SMOKE, FIRE, AND FUME COMPLETED. RETURNED TO DEPARTURE. R & R THE RIGHT RECIRCULATION FAN IAW AMM 21-25-01. OPS GOOD, OK FOR SERVICE.SDR HALA2017030700051Idg · faultyETOPS, L GEN OFF LIGHT UNABLE TO RESET BITE BPCU PER FIM 24-20 TREE 801. R&R LEFT IDG PER AMM 24-11-01 AND OPS CHECKED PER AMM 24-11-02-715-005. R
&R GCU PER AMM 24-22-02. OFF: PN: 729825M SN: C1467 OFF: PN: 734284F SN: 5438 ON: PN: 729825H SN: 4369 ON: PN: 7SDR HALA2016123000565Idg · faulted8:05 MINUTES INTO FLIGHT, THE LT GEN DRIVE LIGHT ILLUMINATED. REMOVED AND REPLACED THE LT IDG IAW AMM 24-11-01, REPLACED THE LEFT GCU IAW AMM 24-22-02, LEAK CHECKED OK.SDR HALA2016121500549Drive Assy · disconnectedLEFT GEN DRIVE EICAS MESSAGE LIGHT ILLUMINATED STEADY. DISCONECTED LEFT GENERATOR. REMOVED AND REPLACED THE LT GENERATOR IAW AMM 24-11-01/401 JP 827. ACCOMPLISHED OPERATIONAL CHECK IAW AMM TASK 24-11-00-715-005. SYSTEM OPERATES NORMALLY.SDR HALA2016121300541Connector · dirtyRIGHT FUEL QUANTITY INDICATION AND TOTAL FUEL QUANTITY INDICATIONS NOT DISPLAYED. EICAS MAINTENANCE MESSAGE FUEL QTY BITE. PERFORMED FUEL QTY IND SYS PER TASK 28-41 FAULT TREE, FOUND "TU12 OPEN LOZ OR HIZ WIRE G AND TU14 OPEN LOZ OR HIZ WIRE G. REMOVED CONNECTSDR HALA2016120700525Drive Assy · failedETOPS, WEATHER RADAR FAIL, ANT. REPLACED WX RADAR DRIVE ASSY. OPS CHECK OK PER AMM 34-43-05. ON: PN: 2041444-0402 SN: DAA4A-09406SDR HALA2016120600521Circuit Card · failedLT ENGINE FIRE LP 1 ON STATUS PAGE, REPLACED THE FIRE LOOP CONTROL CARD M681. FIRE DETECTION SYSTEM TESTED OK IAW AMM 26-11-00-215-001.SDR HALA2016110100379Skin · corrodedCORROSION FOUND ON INTERNAL SKIN BS 1131-1153 BETWEEN STRINGER 37 & 38R. CUT OUT DAMAGESDR HALA2016072700306Packing · damagedAIR DIVERSION, RT HYD QTY, EICAS DISPLAYED. RIGHT QTY WAS .49 WITH, RF DISPLAYED. TROUBLESHOT, FOUND LEAK CAME FROM MODULE STRUT ENGINE DRIVE PUMP PRESSURE AND CASE DRAIN FILTER DUE TO PACKING DAMAGED. REPLACED PACKING IAW AMM TASK 29-11-17-004-001. LEAK CSDR HALA2016071900278Outflow Valve · faultyCABIN ALTITUDE AUTO 1 AND 2 INOPERATIVE. T/S IAW FIM 21-31 FAULT TREE 803. FAULTED AUTO 1 AC MOTOR-STATUS AC PWR OFF VERIFIED. AUTO 2 AC MOTOR VERIFIED. DUE TO HISTORY R & R OUTFLOW VALVE ASSY IAW AMM 21-31-03.SDR HALA2016071800277Warning Message · illuminatedSTATUS MESSAGE CABIN ALTITUDE AUTO 1. PERFORMED FIM 21-31-TREE 809 NO FAULTS NOTED OK FOR SVC.SDR HALA2016060400228Warning Message · false activationRT PACK TEMP EICAS MESSAGE DISPLAYED PERIODICALLY DURING CRUISE FLIGHT BUT WOULD EXTINGUISH IN 5 SEC. REAPPEARED IN THE DESCENT. TURNED SWITCH TO AUTO-N IAW QRH. MESSAGE DID NOT APPEAR IN AUTO-N. PERFORMED PACK TEMPERATURE CONTROLLER BITE PROCEDURE IAW FIM SDR HALA2016050100169Warning Message · false activationAFTER TAKEOFF, DURING CLIMB STATUS MESSAGE, CABIN ALT AUTO 1 DISPLAYED. PERFORMED FIM 21-31, TASK 803. CABIN PRESSURE CONTROLLER BITE NO FAULTS. MESSAGE EXTINGUISHED. OK FOR SERVICE.SDR HALA2016042100117Transformer · malfunctionedAIR DIVERSION, ENROUTE-ON SD PAGE TR2 APPEARED IN AMBER. SDAC 1 AND 2 RESET IAW MCC UNSAT. R & R TR2 IAW MM 24-32-51. MSG CLEARED. OK FOR SERVICE.SDR HALA2016021900054Door · damagedFOUND ON WALK AROUND AFT CARGO INNER AFT DOOR DAMAGED BETWEEN FRAME 63 AND FRAME 63A ABOVE BEAM 5 WITH 1.25 HEIGHT 1.25. TRIMMED OUT DAMAGED AREA HFEC GOOD, VISUAL INSPECT INTERNAL AND EXTERNAL STRUCTURE, NO DEFECTS, ROB TEST INSP OPEN HOLES NO CRACKS. MATERSDR HALA2016020900032Eadi · malfunctionedCAPTAIN`S EADI HAS BEEN RUNNING AT 50 PERCENT BRIGHTNESS FOR MONTHS. PLEASE CHANGE THE UNIT. REPLACED CAPTAIN`S EADI. OPS CHECK OK IAW MM 34-22-03. PERFORMED MCDP GROUND TEST 30. TEST PASS. STATUS TO REMAIN IN, LAND 3 MODE.SDR HALA2016012400015Iru · faultedLEFT IRS FAULT. R & R LT IRU IAW AMM 34-21-01, OPS CHECKED NORMAL.SDR HALA2015102700217Warning Message · false activationON SHORT FINAL APPROACH APPROXIMATELY 1500' AGL RT PACK TEMP EICAS MESSAGE DISPLAYED. PERFORMED FIM TASK 21-51 FAULT TREE 803 PACK TEMP CONTROLLER BITE, FOUND NO FAULTS, NO 30 DAY HISTORY, OK TO CONTINUE.SDR HALA2015041800063Pump · malfunctionedATB LT AFT FUEL PUMP CB POPPED. LT AFT FUEL PUMP EICAS AT BEGINNING OF CRUISE. PERFORMED QRH, DIVERTED. R & R LT AFT FUEL PUMP IAW AMM 28-22-03-004/404-074; OPS AND LEAK CHECK OK, INFO NOTED FROM FLIGHT CREW, NO OVERWEIGHT LANDING CONDITION.SDR HALA2015041400059Circuit Card · damagedRT ENGINE BLEED PSI AT 5 PSI DURING CLIMB. IT WAS NORMAL DURING GROUND OPERATIONS. R & R RT ENGINE BLEED AIR CONTROL CARD M860 IAW AMM 36-11-12-404-026. OPS CHECKS GOOD.SDR HALA2015040200054Stiffener · crackedNR 1 ENGINE, SAILBOAT ATTACH STIFFENER, CRACKED AT FASTNER HOLE. R & R NR 1 ENGINE, SAILBOAT ATTACH STIFFNER, PN 313T3380-244 IAW SRM 51-40-02-06-0.SDR HALA2015040400053Stiffener · crackedNR 1 ENGINE, SAILBOAT ATTACH STIFFENER CRACKED AT FASTNER HOLE. R & R NR 1 ENGINE, SAILBOAT ATTACH STIFFNER IAW SRM 51-40-02-06-0.
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