N594AS
Service difficulty reports · 497
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 = 'N594AS' 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 = 'N594AS' 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 ASAA2018062625427Transition Panel · corrodedRT TRANSITION PANEL FROM STA 500A TO STA 500I HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. REMOVED CORR OUT OF LIMITS. FABRICATED AND INSTALLED NEW RT TRANSITION PANEL FROM STA 500A-500I IAW SRM 55-00-53 2R 5, 53 00 53 1A 2 W .750 R .033 O .040 L 6.00 D .007.SDR ASAA2018071625385Fitting · crackedRT STA 500H AFT BAFFLE CLIP CRACKED AT STR25. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW SRM 51 40 02 0G 0.SDR ASAA2018071625383Fitting · crackedLT STA 500H FWD BAFFLE CLIP CRACKED AT STR 25. GROUNDED - YES. REMOVED DAMGED CLIP AND INSTALLED NEW CLIP AT STA 500H STR 25L IAW SRM 51 40 02 0G 0.SDR ASAA2018071625382Fitting · crackedLT STA 500H AFT BAFFLE CLIP CRACKED STR 25. GROUNDED - YES. REMOVED DAMAGED CLIP AND INSTALLED NEW CLIP AT STA 500H STR 25L IAW SRM 51 40 02 0G 0.SDR ASAA2018071625381Fitting · crackedFWD CARGO COMPARTMENT BAFFLE CLIP CRACKED LT SIDE AFT SIDE OF STA 440. GROUNDED - YES. REMOVED DAMAGED CLIP AND INSTALLED A NEW CLIP AT STA 440 LT SIDE IAW SRM 51 40 02 0G 0.SDR ASAA2018071625380Fitting · crackedLT STA 500G FWD BAFFLE CLIP CRACKED AT STR 25. GROUNDED - YES. REMOVED DMGED CLIP AND INSTALLED NEW CLIP AT STA 500G STR 25L IAW SRM 51 40 02 0G 0.SDR ASAA2018071625379Fitting · crackedLT STA 500G AFT BAFFLE CLIP CRACKED AT STR 25. GROUNDED - YES. REMOVED DAMAGED CLIP AND INSTALLED NEW CLIP AT STA 500G STR 25L IAW SRM 51 40 02 0G 0.SDR ASAA2018071625377Fitting · crackedRT STA 500H FWD BAFFLE CLIP CRACKED AT STR25. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW SRM 51 40 02 0G 0.SDR ASAA2018062525430Threshold · corrodedAFT PIT THRESHOLD WEB IS CORRODED. GROUNDED - YES. REMOVED CORR ON AFT CARGO THRESHOLD WEB AND FOUND TO BE OUT OF LIMITS IAW SRM 53 60 15 1A. REMOVED WEB AND REPLACED WITH NEW WEB IAW SRM 51-40-02 0G 0 W 3 O .50 R .035 L 36 D .015.SDR ASAA2018071625391Transition Panel · corrodedRT TRANSITION PANEL STA 767 TO 792 IS CORRODED. GROUNDED - YES. REMOVED CORR FROM RT TRANSITION PANEL STA 767 TO 792 FOUND TO BE OUT OF LIMITS IAW SRM 53 60 15 1A 1 FIG 103 DETAIL D. REMOVED/REPLACED TRANSITION PANEL IAW SRM 51 40 02 0G 0 FIG 8 AND PARA 4 AND SDR ASAA2018062525330Transition Panel · corrodedRT TRANSITION PANEL IS CORRODED FROM ST5A 727A TO 760. GROUNDED - YES. REPLACED RT TRANSITION PANEL IAW SRM 53 00 53 2R 5 W 1 O .045 R .038 L 5 D.007.SDR ASAA2018062525329Transition Panel · corrodedLT TRANSITION PANEL HAS AREA OF CORR FROM STA 727+18 TO STA 794. GROUNDED - YES. REPLACED LT TRANSITION PANEL IAW SRM 53 00 53 2R 5 W 1 O .045 R .038 L 12 D.007.SDR ASAA2018061125030Sensor · faultedLEFT FWD WINDOW HEAT, OVERHEAT LIGHT ON. GROUNDED - YES. LEFT FWD CONTROLLER BITE SHOWS SENSOR FAULT. MOVED SENSOR SELECTOR TO ALTERNATE POSITION REF FIM 30-41 TASK 812. OPS NORMAL.SDR ASAA2018060844916Filter · warning lightFOUND A NR 1 ENGINE SHORT TIME FAULT, 77-21131. THE N2 SPEED SENSOR SIGNALS DISAGREE ON FLIGHT LEG 3. ACFT GROUNDED. THE NR 1 ENGINE WAS REPLACED DUE TO AN OIL FILTER BYPASS LIGHT ILLUMINATION DUIRNG CLIMBOUT.SDR ASAA2018060824949Engine · making metalDURING CLIMB OUT, RECEIVED A NR 1 ENGINE OIL FILTER BYPASS LIGHT. ACFT GROUNDED. ACCOMPLISHED AN EEC BITE IAW FIM 73-00, TASK 801, NO FAULT CODES NOTED. INSPECTED THE CHIP DETECTORS IAW AMM 79-21-05, THE FWD CHIP DETECTOR SHOWS SOME DEBRIS. ATTEMPTED TO SDR ASAA2018052024745Module · defectiveA/C WILL NOT ACCEPT GROUND POWER. GROUNDED - YES. CONFIRMED FAULT. FOUND GND POWER SWITCH NOT MAKING CONTACT UPON ON POSITION (BROKEN). SWITCH PN 64AT34-7E, IPC 24-21-51-02 DOES NOT SHOW IN TRAX. NOT AVAILABLE. R&R POWER GENERATION MODULE (P5-4) REF AMM 24-21-SDR ASAA2018041424239Diffuser · unserviceableRIGHT AFT PRIMARY HEAT EXCHANGER PLENUM UNSERVICEABLE. ACFT GROUNDED. REMOVED RIGHT AFT PRIMARY HEAT EXCHANGER AND PLENUM/DIFFUSER ASSY IAW AMM 21-51-03-000-805-002. INSTALLED A SERVICEABLE PLENUM/DIFUSSER ASSY, AND PRIMARY HEAT EXCHANGER IAW AMM 21-51-03, LSDR ASAA2018041324238Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED IN FLIGHT. LIGHT EXTINGUISHED ON MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED FIM 21-62 TASK 842. DURING BITE OF THE NR 2 CONTROLLER, TCV FAULT ILLUMINATED FOR PREVIOUS FLT. TCV FAULT CLEARED DURING BITE. FOLLOW UP BITE SDR ASAA2018032724050Lens · detachedOVERHEAD EXIT SIGN IN FOREWARD GALLEY FEEL OFF. ACFT GROUNDED. ADJUSTED THE TANGS ON LENS .SDR ASAA2018032624042Indicator · failedFUELER REPORTED CENTER TANK FUEL QTY INDICATOR ON REFUEL PANEL INOPERATIVE. ACFT GROUNDED. REPLACED THE FUEL QTY IAW AMM 28-41-61-000. OPS CHECKED NORMAL.SDR ASAA2018031523937Lens · detachedFLIGHT ATTENDANT REPORTED THE AFT FACING EMERGENCY EXIT COVER HAS FALLEN OFF. ACFT GROUNDED. INSTALLED THE LIGHT COVER.SDR ASAA2018031423914Warning Light · illuminatedCARGO FIRE PANEL, DISCHARGE LIGHT ILLUMINATED. ACFT GROUNDED. REPLACED THE NR 2 CARGO FIRE BOTTLE IAW T/C 78226001, OPS CHECKED GOOD AND DISCHARGE LIGHT NO LONGER ILLUMINATED.SDR ASAA2018031223829Warning System · false activationCONT CAB ZONE TEMP LIGHT ON CLIMB AND RE-ILLUMINATED ON RECALL. GROUNDED - YES. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE REF AMM 21-61-00 OPS CHECK NORMAL NO FAULTS FOUND. NO HISTORY 30 DAYS.SDR ASAA2018022123655Bushing · wornWHILE COMPLETING T/C N8420001, FOUND UPPER FAN FIRE DETECTOR TEFLON BUSHING WORN IN MULTIPLE PLACES FOR THE NR 2 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE UPPER FAN FIRE DETECTOR IAW AMM 26-11-01/401. OPERATIONAL CHECK SATISFACTORY.SDR ASAA2018022023641Bottle · malfunctionedDISCHARGE LIGHT ILLUMINATED, CARGO FIRE PANEL ILLUMINATED IN FLIGHT. NO FIRE WARNING INDICATED. ACFT GROUNDED. SHAKEDOWN OF WIRE HARNESS & MEGGING OF WIRES W5074-6003-22 & W5098-6012-22 IAW WDM 26-23-11, NO DEFECTS NOTED. NR 1 CARGO FIRE BOTTLE REPLACED IAWSDR ASAA2018021723595Connector · damagedDURING CLIMBOUT, CARGO DISCHARGE LIGHT ILLUMINATED. DURING CRUISE, THE DISCHARGE LIGHT IS EXTINGUISHED. ACFT GROUNDED. ACCOMPLISHED STEP 1 AND STEP 2 OF TSR701453. FOUND A BENT PIN 3 ON PRESSURE SWITCH FOR CARGO FIRE BOTTLE. FOUND DAMAGE TO PIN 3 ON CONNSDR ASAA2018021523596Warning Light · false activationPRIOR TO TAKEOFF, CARGO DISCHARGE LIGHT ILLUMINATED. ACFT GROUNDED. CYCLE THE CARGO FIRE CIRCUIT BREAKER. ACCOMPLISHED CARGO FIRE EXTINGUISHER TEST IAW AMM 26-23-02-860-007. OPS CHECKED NORMAL.SDR ASAA2018020523415Indicator · failedGAUGES ON RIGHT WING FUELING PANEL WENT BLANK DURING REFUELING. GROUNDED - YES. FOUND FUEL FUELING IND C/B POPPED. ACCOMPLISHED C/B RESET PROCEDURE REF AMM 20-60-01-860-801. ISOLATED TO FAULTY NR 1 TANK REFUEL INDICATOR. REF WDM 28-44-11 & 28-41-11. REMOVED & SDR ASAA2018020123356Fcu · unknownAPU HAS HISTORY OF MUILTIPLE FAILED CSS WITH FAULT 49-41010, NO ACCEL SHUTDOWN RECORD AND IS CURRENTLY ON MEL 49-99A. ACFT GROUNDED. ACCOMPLISHED APU BITE PROCEDURE IAW FIM 49-60 TASK 801 AND NO ACCELERATION SHUTDOWN FAULT ISOLATION IAW FIM 49-40 TASK 801. SDR ASAA2018012523298Warning Light · false activationILLUMINATION OF LEFT PACK. ACFT GROUNDED. BITE SHOWED LEFT TEMP CONTROL VALVE, COULD NOT VERIFY, RESET AND REVERIFIED, FAULT DID NOT RETURN. NO HISTORY 60 DAYS.SDR ASAA2018012223272Unknown · malfunctionedAPU FAILED TO START ON TAXI-IN. GROUNDED - YES. PERFORMED APU BITE PER FIM 49-60 TASK 801. NO FAULTS ON CURRENT STATUS, NO FAULTS NOTED IN FAULT. APU STARTS NORMALLY PER AMM 49-11-00.SDR ASAA2017121922992Transceiver · faultedWEATHER RADAR DISPLAYS RETURNS WHEN THERE IS NOTHING THERE IN BOTH AUTO AND MANUAL MODE STARTING AT ABOUT 80 MILE RANGE IN MAP MODE IT SHOWS RETURNS AT ALL DISTANCES THAT DONT APPEAR TO BE TERRAIN. ACFT GROUNDED. REPLACED THE WEATHER RADAR R/T IAW AMM 34-43-4SDR ASAA2018060824948Pin · migratedWHILE ACCOMPLISHING TC SBCFM56-7B-72-0986-1 FOR THE NR 1 ENGINE, FOUND THE SLAB HEADED ANTI-ROTATION PINS AT THE 3:00 AND 9:00 POSITIONS OF THE STAGE 3 TO HAVE ROTATED MORE THAN ZERO BUT LESS THAN 45 DEGREES. ACFT GROUNDED. THE NR 1 ENGINE WAS REPLACED.SDR ASAA2017101422195Bulb · failedTEMP INDICATOR IN LEFT PACK POSITION INDICATES ZERO. PRESSURE NORMAL. ACFT GROUNDED. REMOVED AND REPLACED THE LEFT PACK TEMP BULB IAW AMM 21-51-60-000-801, AND 21-51-60-400-801, OPS CHECKED GOOD.SDR ASAA2017092322009Drain · crackedFOUND APU FUEL LINE SHROUD DRAIN MAST CRACKED. ACFT GROUNDED. COMPLETED ON T/C NG-28FCD-18312-1.SDR ASAA2017091221905Lens · detachedF/A REPORTS THAT THE EXIT SIGN IN FIRST CLASS GALLEY OVER THE COCKPIT DOOR FELL OFF. ACFT GROUNDED. INSTALLED EXIT SIGN IN FIRST CLASS GALLEY OVER COCKPIT DOOR, OPS CHECK GOOD.SDR ASAA2017082021671Insert · damagedFOUND THE NR 2 ENGINE NR 3 STRUT PANEL AFT UPPER SCREW NUT CLIP ON BEARING WORN. ACFT GROUNDED. REMOVED AND PEPLACED A DAMAGED KEY LOCK INSERT AT THE NR 2 ENGINE NR 3 STRUT FAN DUCT PANEL IAW MM 70-42-13-250. INSTALLED FAN DUCT PANEL IAW AMM 72-23-07-400-80SDR ASAA2017082021672Bracket · gougedNR 2 ENGINE INLET AND FAN BLADE DETAILED INSPECTION. FOUND BOTH UPPER & LOWER ATTACH BRACKETS GOUGED FROM TURN BUCKLE ON FWD TUBE FOR TAI VALVE. ACFT GROUNDED. REPLACED TAI DUCT ON NR 2 ENGINE AND LOWER ATTACHMENT AND TURN BUCKLE IAW AMM 30-21-11. LEAK CHESDR ASAA2017082021670Panel · damagedNR 2 ENGINE INLET AND FAN BLADES DETAILED INSPECTION, FOUND ONE FASTENER COUNTERSINK ON 1 & 3 STRUT PANELS DAMAGED BY LOOSE FASTENERS. FOUND NR 2 ENG NR 3 STRUT PANEL AFT UPPER SCREW NUT CUP ON BEARING WORN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENG SDR ASAA2017082021669Link · wornNR 2 ENGINE INLET AND FAN BLADES DATAILED INSPECTION FOUND FWD SIDE OTBD BEARING ON TURNBUCKLE FOR START VALVE WORN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FWD SIDE OTBD TURNBUCKLE IAW P/P BUILDUP MANUAL 71-00-02 FIG. 25-1 PAGE 2 AND 3.SDR ASAA2017081492622Hmu · failedON PREFLIGHT FOUND NR 1 ENGINE FUEL VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE. GROUNDED - YES. REMOVED AND REPLACED THE NR 1 ENGINE HMU IAW T/C N8473000 & T/C N8473001. ALTERNATE DEACTIVATION PROCEDURE REVERSED.SDR ASAA2017072121442Fmc · malfunctionedBOTH FMCS FAILED MOMENTARILY DURING TAXI IN, AFTER LANDING. THEY RETURNED ABOUT 10 SECONDS LATER. ACFT GROUNDED. PERFORMED FMC OPS TEST IAW AMM 34-61-00-710-801. NO FAULTS FOUND, PERFORMED FMC NUISANCE FAULT IAW AMM 34-61-00-860-801, NO FAULTS NOTED. OK FORSDR ASAA2017072121434Warning Light · false activationRIGHT PACK ILLUMINATED ON RECALL AND DOES RESET WITH MASTER CAUTION. ACFT GROUNDED. TESTED THE RIGHT PACK IAW AMM 21-51-00-700-803. THE TEST PASSED, THIS WAS AN INTERMITTENT FAULT.SDR ASAA2017061121012Battery Pack · failedDURING TC 78233000 ACCOMPLISHMENT, FOUND THE EMERGENCY EXIT LIGHTS AROUND L2 DOOR, INTERIOR AND EXTERIOR, INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECKED GOOD.SDR ASAA2017060921019Duct · crackedNR 1 ENGINE COWL TAI AIR DUCT HAS APPROXIMATELY A ONE INCH CRACK NEAR 90 DEGREE BEND AT THE 12 O'CLOCK POSITION ABOVE THE CORE AND FWD OF THE PRECOOLER. ACFT GROUNDED. REMOVED TWO CLAMPS AND ONE BRACKET FROM THE NR 1 ENGINE COWL TAI DUCT. REPAIRED THE TAI DUSDR ASAA2017060821022Wire · burnedNR 1 ENGINE ELECTRICAL HARNESS THAT COMES FROM VSV AND VBV VALVES ON OUTBOARD SIDE, HAD BURNED INSULATION AND WIRES AT 12 O'CLOCK POSITION. ACFT GROUNDED. THE NR 1 ENGINE WAS REPLACED IAW T/C 78471001.SDR ASAA2017060620974Indicator · failedFUELER REPORTED REFUEL PANEL CENTER INDICATOR WILL NOT TEST. OTHER INDICATIONS NORMAL. ACFT GROUNDED. REMOVED AND REPLACED CENTER REFUEL PANEL QUANTITY INDICATOR IAW AMM 28-41-61. OPS AND TESTED GOOD.SDR ASAA2017060421016Line · crackedDUCT PRESSURE SPLIT GREATER THAN 20 PSI, RT 44, LT 18 ON CL RT 42, LT 19 AT 340 LEVEL. ACFT GROUNDED. ACCOMPLISHED T/C NG-36WC-00001 UP TO STEP L PAR 5. FOUND A CRACK IN THE CONTROL PRESSURE LINE AT HSV. REMOVED AND REPLACED THE NR 1 ENGINE HSV CONTROL PRSDR ASAA2017050420635Pcu · defectiveFOLLOW-UP TO HISTORY OF ELEC LIGHT ILLUMINATING. GROUNDED - YES. ACCOMPLISHED TSR. REPLACED SPCU REF MM 24-34-11-400-801. INSTALLATION TEST CK'D GOOD PER THE SAME. OBSERVED THAT THE TR UNIT FAULT LIGHT WAS ILLUMINATED. ACCOMPLISHED FIM 24-31 TASK 826. FOUND TRSDR ASAA2017050420633Warning System · false activationELEC CAUTION LIGHT ILLUMINATED. GROUNDED - YES. CLEARED SPCU FAULT- PERFORMED BITE TEST PER 24-31- TASK 801 FIM. OPS CHECK GOOD.
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