N530AS
Service difficulty reports · 358
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 = 'N530AS' 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 = 'N530AS' 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 ASAA2014061708250Idg · contaminatedDURING ENGINE RUNS, AFTER NR 1 ENGINE CHANGE, IDG WOULD NOT PRODUCE POWER, NO INDICATIONS. ACFT GROUNDED. REMOVED NR 1 ENGINE IDG IAW MM 24-11-11-800-801. METAL CONTAMINATION FOUND IN NR 1 IDG. FLUSHED NR 1 IDG OIL COOLING CIRCUIT IAW AMM TASK 24-11-11-090-SDR ASAA2014060508083Warning Message · false activationFMC DISAGREE AFTER PUSH BACK. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE, OPS NORMAL.SDR ASAA2014051107766Coupler · malfunctionedNR 1 HF WILL NOT TRANSMIT. ACFT GROUNDED. RESET SYS POWER PERFORMED FIM TASK IAW AMM 23-11-801. BITE OF HF SYSTEM PASSED, NO FAULTS FOUND. GROUND VERIFICATION CHECKED OK NO HISTORY PAST 30 DAYS. SYSTEM RESTORED. REPLACED HF ANTENNA COUPLER #1 REF AMM TASKSDR ASAA2014032007261Satcom · malfunctionedNO SATCOM ON MENU PAGE. UNABLE TO RESTORE VIA QRH. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2014031507204Eec · faultedACQUIRED FAULT CODE ON EEC BITE TEST NR 2 ENGINE. ACFT GROUNDED.SDR ASAA2014022607003Connector · unsecureUNABLE TO TRANSMIT ON HF1 BOTH SIDES. ACFT GROUNDED. SECURED CONNECTOR D4227P TO HF1 COUPLER & OPS CHECKED GOOD, REF AMM 23-11-61.SDR ASAA2014022106943Module · faultyAPU FIRE DETECTOR INOPERATIVE LIGHT ILLUMINATED AFTER APU STARTED AND STABLE. ACFT GROUNDED. FOUND ENGINE & APU FIRE DETECTION MODULE M279 FAULTY. FOUND APU TAILPIPE OVERHEAT DETECTOR WITH HIGH RESISTANCE, 150 KOHMS. R & R M279 & APU TAILPIPE OVERHEAT DETESDR ASAA2014021706881Hf Comm · malfunctionedNR 1 HF INOPERATIVE, WOULD NOT TRANSMIT OR RECEIVE. ACFT GROUNDED. CYCLED POWER ON NR 1 HF TRANSCIEVER IAW FIM 23-11-TASK 801 & 806. BITE CHECKED GOOD. NO FAULTS NOTED. NO HISTORY 60 DAYS.SDR ASAA2014021006813Bleed Valve · failedDURING CLIMB, FL 360 LT DUCT PRESSURE 44 PSI, RT 22 PSI, N1'S WERE 100.5 - PRESSURIZATION NORMAL. DURING CRUISE AT FL 380 DUCT PRESSURES LT=34 PSI, RT=28 PSI. ACFT GROUNDED. ACCOMPLISHED TC NG-36WC-00001. PRECOOLER CONTROL VALVE FAILED, R & R PRECOOLER CONTSDR ASAA2014012312468Warning Message · false activationLEFT PACK LIGHT COMES ON AT RECALL, OUT WITH RESET MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED PACK-ZONE TEMP CONTROLLER BITE AMM 21-61-02. OPS CHECKED NORMAL, GROUNDED, VERIFICATION SUCCESSFUL.SDR ASAA2014010712341Radar · malfunctionedWEATHER RADAR INOPERATIVE, FAILED AFTER 1 HR, RADAR OPS CHECKED NORMAL. ACFT GROUNDED. WEATHER RADAR SYSTEM CHECKED GOOD IAW TASK 34-43, TASK 801. NO HISTORY IN 30 DAYS, GROUND VERIFICATION GOOD.SDR ASAA2013110796331Warning Message · false activationFMC DISAGREE OCCURRED ON TAXI OUT. ACFT GROUNDED. PERFORMED PROCEDURE FROM QRH. NORMAL OPS RESTORED.SDR ASAA2013110596303Display · malfunctionedF/O CDU BLANKED. ACFT GROUNDED. ACCOMPLISHED FIM TASK 34-61, TASK 804 CDU BITE CHECK PROCEDURE, NO FAULTS FOUND, SYS. OPS CHECKS NORMAL.SDR ASAA2013110396285Unknown · unknownCOPILOT MCDU INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED FIM 34-61, TASK 804, MCDU OPERATION NORMAL WITH NO FURTHER DISCREPANCIES.SDR ASAA2013102896248Warning Light · false activationFMC DISAGREE LIGHT CAME ON. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.SDR ASAA2013101596183Battery · dischargedBOTH MAIN & AUX BATTERIES ARE DEAD. ACFT GROUNDED. R & R MAIN & AUX BATTERIES IAW MM 24-31-11. OPS NORMAL.SDR ASAA2013091795998Warning Light · illuminatedDURING TAXI, FMC DISAGREE ANNUNCIATED IN CDU SCRATCH PAD. ACFT GROUNDED. QRH PROCEDURES WERE FOLLOWED TO SUCCESSFULLY RESET FMCS.SDR ASAA2013091795996Display · malfunctionedDURING MOMENTARY GROUND POWER LOSS, F/O MCDU BLANKED OUT. ACFT GROUNDED. SWITCHED POWER SOURCES, NO HELP, RESET FMCS MCDU 2 AND COMPUTER 2 CIRCUIT BREAKER IAW AMM 20-60-01-860-801. F/O MCDU RETURNED TO NORMAL. OK FOR CONTINUE SERVICE.SDR ASAA2013091395972Knob · inoperativeCAPTAIN`S COURSE KNOB INOPERATIVE. ACFT GROUNDED. R &R MAIN CONTROL PANEL IAW AMM 22-11-34. MAIN CONTROL PANEL OPS NORMAL. ACFT OK CONTINUE FOR SERVICE.SDR ASAA2013080895763Fmc · false indicationFMC DISAGREE ILLUMINATED AFTER ENGINE START. ACFT GROUNDED. LIGHT WENT OUT AFTER QRC PROCEDURE.SDR ASAA2013080395726Fmc · unknownGROUND POWER TRIPPED OFF. GROUND POWER APPLIED AGAIN TO ACFT, RT FMC MCDU BLANK. ACFT GROUNDED. REDET POWER, PERFORMED RT CDU BITE CHECK, LCD TEST, NO DEFECTS FOUND. DFCS BITE 22-11-801 GOOD. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2013072995701Fmc · inoperativeF/O FMC IS BLANK. ACFT GROUNDED. REBOOTED F/O FMC. OPS CHECK NORMAL.SDR ASAA2013072095640Display · malfunctionedF/O MCDU INOPERATIVE. ACFT GROUNDED. CYCLED POWER, F/O MCDU CAME ONLINE, CHECKED F/O MCDU IAW AMM 23-15-839-002. OPS NORMAL.SDR ASAA2013070995529Unknown · unknownVNAV ABNORMALLY LOW SPEED COMMANDED DURING CLIMB. VNAV WAS COMMANDING A CLIMB SPEED OF 217 KIAS AT 4000 MSL. VNAV RESPONDED NORMALLY TO SPEED INTERVENTION. THROUGH THE CLIMB REGIME TO FL 360 WHEN ENGAGING VNAV IT WOULD COMMAND APPX 217KIAS. ONCE ESTABLISHESDR ASAA2013061295086Computer · failedREF T/C 78222000 STEP 2.D.(5) FAILS. WHEN ATTEMPTING TO SELECT V/S MODE ON MCP, MINIMUM SPEED REVERSION ACTIVATES AND V/S REVERTS TO LEVEL CHANGE, WITH UNDERSPEED LIMITING CHARACTER FLASHING IN IAS/MACH DISPLAY. ACFT GROUNDED. SWAPPED FCC A & B, VERIFIED PROSDR ASAA2013060995058Cdu · failedCAPTAIN`S CDU WILL NOT POWER UP. ACFT GROUNDED. REMOVED CAPTAIN`S CDU IAW AMM 34-61-01-000-802 INSTALLED SERV CDU IN CAPTAIN`S POSITION, OPS CHECK GOOD IAW AMM 34-61-01-400-802.SDR ASAA2013051394797Autopilot Sys · malfunctionedAUTOPILOT A DISCONNECTED TWICE IN CRUISE NO OBVIOUS REASON. ACFT GROUNDED. MCP DATA INVALID MSG 22-11607- REF FIM TASK 22-11, TASK 817 & 803 MCP, OPS TEST OK. FULL MCP OVERNIGHT TEST PASSED. NO FAULTS NOTED- CURRENT STATUS OK. GROUND VERIFICATION OF MCP ACCOSDR ASAA2013042894640Transceiver · failedHF NR 1 WILL NOT TRANSMIT OR RECEIVE. ACFT GROUNDED. NR 1 HF TRANSCEIVER BITE; KEY INTERLOCK LED SEQUENCES INCORRECTLY. REPLACED NR 1 HF TRANSCEIVER IAW MM 23-11-21. INSTALLATION TEST GOOD IAW SAME. HF COMM WITH SFO GOOD REF MM 23-11-00.SDR ASAA2013042194557Lamp · inoperativeEXTERIOR EMERGENCY LIGHT AFT OF RT WHEEL WELL INOPERATIVE. REPLACED LAMP. OP CHECKED NORMAL.SDR ASAA2013030494079Panel · crackedWHILE ACCOMPLIMENT OF TC 78472000, NR 2 ENG INLET & FAN INSPECTION FOUND BLEED VALVE LOWER PANEL 530-600 POSN AFT LOOKING FWD CRACKED. REPLACED PANEL IAW AMM 72-23-07-400-801-F00.SDR ASAA2013022794016Circuit Breaker · trippedAT FL 350, ATTEMPTED OPENING OF FUEL CROSSFEED VALVE FOR FUEL BALANCING, BLUE LIGHT DID NOT ILLUMINATE EITHER BRIGHT OR DIM. PERFORMED QRH PROCEDURE, NOTICED FUEL CROSSFEED CIRCUIT BREAKER OUT P6-3, B-7 LOCATION. SUSPECT CROSSFEED VALVE REMAINED CLOSED. RESESDR ASAA2013021493916Valve · failedNR 1 ENG COWL VALVE OPEN LIGHT REMAINED BRIGHT WITH SWITCH IN THE ON POSITION TAI LIGHT ON UPPER DU WAS ILLUMINATED GREEN. ACCOMPLISHED FIM TASK 30-21, TASK 805 THRU STEP E (3)(A) PG2. LIGHT REMAINS ON BRIGHT. REPLACED ENG 1 COWL TAI VALVE NO LEAKS NOTED,SDR ASAA2013011793702Ecu · faultedWHILE PREFORMING FMC-CDU T/C FOUND FAULT CODE 76-31362 FOR THE NR 2 ENGINE, START LEVER SIGNALS DISAGREE LONG TERM FAULT. R & R NR 2 ENG EEC. REF MM 73-21-60-000-801-FOO AND 73-20-60-400-801-FOO. PERFORMED FADEC SYS TEST REF MM 73-21-00-700-802-F00. EEC SOSDR ASAA2012100393012Indicator · trippedDURING OIL SERVICE, NOTICED SMALL AMOUNT OF OIL UNDER NR 2 ENGINE PRIOR TO SERVICE. OPENED IDG ACCESS DOOR, FOUND DIFFERENTIAL PRESSURE INDICATOR PIN EXTENDED. R & R IDG SCAVENGE AND CHARGE FILTERS REF AMM 24-11-41-000-801 24-11-41-400-801. NO LEAKS NOTED -SDR ASAA2012100192986Apu · malfunctionedAPU FAULT LIGHT ILLUMINATED, APU DID NOT START. APU BITE CHECK SHOWS MSG-49-41012 NO ROTATION SHUTDOWN. ACCOMPLISHED FIM TASK 49-40-00-810-803 . FROM APU BITE CHECK. STARTED APU NUMEROUS TIMES. FAULT DID NOT RETURN. NO HISTORY 60 DAYS.SDR ASAA2012090692837Control Panel · weakMAIN CONTROL PANEL SPEED WINDOW EXTREMELY DIM. ALL OTHER MCP LIGHTS ARE NORMAL. DID GET IT TO GO BRIGHTER BY TAPPING ON LIGHT PANEL HOWEVER IT DID GO DIM AGAIN. SPEED BUG AND ALL SYSTEMS WORK NORMALLY. ACFT GROUNDED. R & R MODE CONTROL PANEL REF MM 22-11-34SDR ASAA2012080592668Control Valve · failedON MASTER CAUTION RECALL - RT PACK LIGHT ILLUMINATED, LIGHT EXTINGUISHED ON RESET. R & R NR 2 (RT SIDE) TEMPERATURE CONTROL VALVE, HAD A HARD FAULT DURING CONTROLLER BITE CHECK. MX DONE IAW AMM 21-51-10-000-801 AND 21-51-10-400-801, OPS AND LEAK CHECK GOOD.SDR ASAA2012080392656Sensor · faultedRT SIDE WINDOW OVERHEAT LIGHT ON. TURNED OFF FOR 5 MINUTES, CAME BACK ON IMMEDIATELY WHEN POWER RESTORED. SENSOR FAULT RT SIDE WINDOW HEAT CONTROL UNIT. MOVED LEAD TO SPARE WINDOW TEMP SENSOR ON RT SIDE WINDOW IAW FIM 30-41 TASK 811. RT SIDE WINDOW HEAT COSDR ASAA2012082292763Igniter · damagedLT ENGINE WOULD NOT START. ACFT GROUNDED. FOUND RT IGNITER PLUG DAMAGED. R & R IGNITION PLUG, RT REF T/C 78474000, NO FAULTS, CODES IN EEC BITE TEST. OPS CK NORMAL.SDR ASAA2012081492721Module · failedON CLIMB-OUT, LOST ALL PROBE HEAT (A) (ALL CBS IN). GEN 2 - 56 AMPS GEN 1-66 TO 95 AMPS. ACFT GROUNDED. VERIFIED DISCREPANCY WITH PROBE HEAT SWITCH ON (A) VERIFIED LIGHTS REMAIN ON WITH TEMP GUN, VERIFIED PROBES HOT WITH SWITCH ON. R & R P5-9, REF 30-41-41 SDR ASAA2012070992508Coupler · looseNR 1 AND 2 HF RADIOS TESTED UNSATISFACTORY ON BOTH HEADS. ACFT GROUNDED. NR 1 AND 2 HF RADIO CHECK LOW AND HIGH FREQUENCIES WERE 2 X 2, VISUALLY INSPECTED ANTENNA AND COUPLER ATTACHMENT POINTS, NO DEFECTS FOUND. FOUND 1 & 2 HF COAX DISCONNECTS AT E8-1 RACK LOSDR ASAA2012070292456Control Panel · failedHF1 TRANSMIT FUNCTION INOPERATIVE. AUDIO RECEPTION FUNCTIONS NORMALLY. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, NR 1 HF OPS NORMAL. R & R NR 1 HF COUPLER REF MM 23-11-61, OPS CHECK NORMAL. REQUIRES FLIGHT VERIFICATION OF NR 1 HF. FLT VERIFICATION UNSUCCESDR ASAA2012071492543Oil System · lowAPU MAINTENANCE LIGHT CAME ON AFTER APU START. ACFT GROUNDED. PERFORMED FIM TASK 49-60-00-810-801. FOUND NO FAILURES IN CURRENT STATUS & FAULT HISTORY. FOUND MAINT MESSAGE 49-91227 LOW OIL QTY IN MAINT HISTORY. PERFORMED FIM TASK 49-90-00-810-804. SERVICESDR ASAA2012071492533Display · intermittentMCP IAS/MACH WINDOW DISPLAY VERY DIM EVEN WITH MAIN PANEL BRIGHTNESS ALL THE WAY UP. ACFT GROUNDED. COULD NOT DUPLICATE. SHOOK DOWN MODE CONTROL PANEL, MCP IAS/MACH WINDOW DISPLAY CHECKED NORMAL.SDR ASAA2012062892441Transceiver · failedLOST ABILITY TO TRANSMIT USING HF 1 TRIED RECHANNELING RADIO NO EFFECT SWITCHED TO HF 2, OPS OK. ACFT GROUNDED. PERFORMED T/S REF FIM 23-11-00-810-806, FOUND NR 1 RT INOP R & R NR 1 RT IAW AMM 23-11-21-801 AND INSTALLED NR 1 RT IAW AMM 23-11-21-400-801. GROSDR ASAA2012061792376Control Valve · failedDUCT SPLIT IN CLIMB, EXCEEDED 20 PSI, DIFFERENTIAL L-N1 100.1 46 PSI, R N1 100.2 23 PSI. AFTER 10 MINUTES CRUISE AT FL 380 BOTH N1 89.7 BOTH 40 PSI. ACCOMPLISHED NR 2 ENG HEALTH CHECK IAW TASK CARD NG-36WC-00001. FOUND PRECOOLER CONTROL VALVE FAILED. R & RSDR ASAA2012061792354Idg · failedWHILE PERFORMING PDC FOUND NR 2 ENGINE DELTA P ON IDG POPPED GROUNDED - YES. PERFORMED W/O 169161 - NR 2 ENG IDG FILTER AND OIL CHANGE. THROUGH HISTORY AND IDG PLACARD THIS IS THE 3RD POP OF THE IDG. R & R NR 2 IDG IAW MM 24-11-11-000-801 AND MM 24-11-11-400SDR ASAA12511559Fmc · malfunctionedDURING TAXI OUT, FMC DISAGREE MESSAGE APPEARED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. FMC MESSAGE NO LONGER DISPLAYED.SDR ASAA12511437Switch · malfunctionedON CLIMBOUT, STAB TRIM BECAME INOPERATIVE ON RUNNING QRH PROCEDURE FOUND STAB TRIM CONTROL CIRCUIT BREAKER POPPED. DIVERSION TIME: 28 MINUTES. DISCONNECTED ELECTRONIC CONNECTOR CAPT CONTROL CUTOUT SWITCH. CIRCUIT BREAKER REMAINS CLOSED WITH ELECTRONIC STAB SDR ASAA12511403Warning Message · false indicationFMC DISAGREE. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.
Back to N530AS