N564AS
Service difficulty reports · 539
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 = 'N564AS' 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 = 'N564AS' 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 ASAA0957011Engine · oil consumptionPER PAT, ENGINE NR 1 AND ENGINE NR 2 OIL CONSUMPTION LIMITS HAVE BEEN EXCEEDED FOR ETOPS FLIGHT. ENGINE NR 1 OIL CONSUMPTION .75 ENGINE NR 2 OIL CONSUMPTION .60 ACFT GROUNDED. PERFORMED GENERAL VISUAL INSPECTION OF ENGINE NR 1 AND ENGINE NR 2 PER ETOPS MANUASDR ASAA0957004Radar · malfunctionedWX RADAR WAS INTERMITTENT. WX FAIL ILLUMINATED FOR 90 SECONDS FIRST TIME AND 15 SECONDS THE SECOND TIME. ACFT GROUNDED. ACCOMPLISHED FIM 34 43T801 WXR SYSTEM BITE. GROUND VERIFICATION SUCCESSFUL NO DEFECTS NOTED. NO HISTORY LAST 90 DAYS.SDR ASAA0957009Drain Line · leakingLEFT HIGH PRESSURE WATER SEPARATOR FWD UPPER WATER EXTRACTOR DRAIN LINE HOSE OUTBOARD LOCATION LEAKING GROUNDED YES. REMOVED AND REPLACED DRAIN HOSE OF HIGH PRESSURE WATER SEPARATOR PER MM 21 51 14 400 801. OPS AND LEAK CHECKS GOOD.SDR ASAA0956962Control Valve · failedRT STANDBY TEMP CONTROL VALVE FAILED OPS CHECK. REPLACED THE RT STBY TEMP CONTROL VALVE PER MM 21 31 11 400 801 STEPS F (1) THRU (7). LEAK AND OPS CHECK DUE 65613. ACCOMPLISHED INSTALLATION TEST OF RT STBY TEMP CONTROL VALVE PER MM 21 51 11 400 801. OPS ANSDR ASAA0956898Seal · out of limitsWHILE ACCOMPLISHING THE APU CHANGE FOUND THE INLET SEAL (SIGMA) OUT OF LIMITS. REMOVED & REPLACED APU INLET SEAL REF 49 15 11.SDR ASAA0956894Apu · malfunctionedDURING CLIMB DIRTY SOCK (MELTED CRAYON) SMELL VERY PROMINENT IN CABIN AIR. INTENSITY INCREASED DURING CLIMB AND CRUISE AND CONTINUED DURING DESCENT. TROUBLESHOOTING DETERMINED THAT ODOR IS COMING FROM APU SUSPECT LOAD COMPRESSOR SEAL. WHILE PERFORMING FIM TSDR ASAA0956872Warning System · malfunctionedAUTO FAIL LIGHT ILLUMINATED AT TOP OF DESCENT. FOLLOWED QRH NO ABNORMAL PRESSURIZATION CHANGE NOTICED. PERFORMED FIM TASK 21 31 00 810 801. FOUND CODE 078 OFV LRU FAIL. PERFORMED FIM TASK 21 31 00 810 82. FAULT MESSAGE CLEARED INTERMITTENT FAULT GROUND VESDR ASAA0956871Warning System · intermittentPRES AUTO FAIL LIGHT ON. AUTO FAIL LIGHT ON & FOUND EXISTING "OFV WIRING" & "OFV LRU FAIL" FAULTS. PERFORMED FIM TASK 21 31 00 810 802. DETERMINED FAULTS INTERMITTENT PER FIM TASK 21 31 00 810 802 & 21 31 00 810 802. ALL FAULTS CLEARED. SEAMC NOTIFIED.SDR ASAA0956822Eec · faultedTHE "A/T LIM" DISPLAYED ON ENGINE INSTRUMENT AUTO THROTTLE MODE. A/T COMPUTER LOGGED MSG 22 31411 AND 22 31511 NR 1 EEC LOGGED FAULT CODE 73 21281. FOLLOWED FIM 73 27 TASK 805 REQUIRES EEC REPLACEMENT. REPLACED NR 1 ENG EEC PER MM 73 21 60 000 801 AND 73 21SDR ASAA0956794Warning System · malfunctionedFMC DISAGREE LIGHT ON DURING TAXI. GROUNDED YES. FLIGHT CREW PERFORMED QRH PROCEDURE OPS NORMAL.SDR ASAA0956614Ecu · malfunctionedAPU INOP. VERIFIED APU INOP WITH APU ECU INTERFACE MESSAGE DURING APU BITE. REMOVED AND REPLACED APU ECU PER MM 49 61 12. OPS NORMAL REF SAME. VERIFIED P/N & SOFTWARE NUMBER PER SEAMC. GROUND VERIFICATION CHECKS GOOD. SEAMC NOTIFIED.SDR ASAA0956517Hmu · malfunctionedNR 2 ENGINE CONTROL LIGHT ILLUMINATED ON TAXI OUT. CHECKED FAULT HISTORY AND FOUND FAULT CODES 75 20582 (TBV DEMAND AND POS SIGNAL DISAGREE) AND 75 20532 (LPTACC DEMAND AND POSITION SIGNALS DISAGREE). ACCOMPLISHED FIM TASK 75 22 00 810 801 F00 (FOR 75 20532)SDR ASAA0956516Warning System · malfunctionedPACK LIGHT ILLUMINATED ON RECALL. PERFORMED FIM TASK 21 53 00 810 812 AND FOUND TCV FAULT LATCHED ON RT ZONE TEMP CONTROLLER. RAN SATISFACTORY BITE CHECK ON SAME AND TCV FAULT CLEARED. PACK LIGHT NO LONGER ILLUMINATES ON RECALL.SDR ASAA0956493Battery · dischargedFOUND AFT RT ATTENDANTS STATION O/B EMERGENCY FLASHLIGHT TO BE INOP. REMOVED DEAD BATTERY AND INSTALLED NEW.SDR ASAA0956474Flap · chafedCHAFING ON LEFT WING I/B AFT FLAP O/B END. REPAIRED AFT FLAP.SDR ASAA0956477Angle · corrodedCORROSION ON FWD CARGO BAY AFT CENTER BULKHEAD PANEL LOWER ANGLE. REPLACED ANGLE.SDR ASAA0956476Fitting · crackedRT WING REAR SPAR STA 289 I/B FIXED T/E SEAL BULKHEAD CRACKED ON FWD SIDE AT FASTENERS. REMOVED AND REPLACED FITTING.SDR ASAA0956475Skin · gougedDENT WITH GOUGE IN E&E DOOR EXTERNAL SKIN FWD OF HANDLE. COMPLIED WITH EA.SDR ASAA0956460Seat Track · gougedCAPTAINS I/B AFT SEAT TRACK IS GROOVED ON UPPER SURFACE AND AFT HOLES ARE ELONGATED. REPLACED I/B AFT SEAT TRACK.SDR ASAA0956459Seat Track · gougedCAPTAINS O/B AFT SEAT TRACK IS GOUGED. REMOVED AND REPLACED CAPTAINS AFT O/B SEAT TRACK.SDR ASAA0956458Seat Track · damagedF/O OUTBOARD AFT SEAT TRACK HOLE IS ELONGATED. REMOVED AND REPLACED F/O AFT SEAT TRACK.SDR ASAA0956457Seat Track · damagedF/O INBOARD AFT SEAT TRACK I/B RAIL AFT HOLE IS ELONGATED AND TRACK IS GOUGED. REMOVED AND REPLACED F/O OUTBOARD AFT SEAT TRACK I/B RAIL.SDR ASAA0956456Wedge · chafedLEFT WING NR 3 SLAT TRAILING EDGE WEDGE HAS A SMALL CHAFED AREA ON THE LOWER SKIN I/B CORNER. REPAIRED CHAFE ON NR 3 SLAT LOWER SKIN I/B CORNER.SDR ASAA0956455Skin · dentedDENT WITH GOUGE IN E/E DOOR EXTERNAL SKIN FWD F HANDLE.SDR ASAA0956427Connector · disconnectedRIGHT SIDE WINDOW OVERHEAT LIGHT COMES ON IMMEDIATELY WHEN WINDOW HEAT IS TURNED ON. DUPLICATED MALFUNCTION. FOUND COILED CONNECTOR TO F/O'S SLIDER WINDOW NOT LOCKED & CAME OFF. SECURED CONNECTOR & COMPLETED GROUND VERIFICATION REF AMM 30 41 00 710 801. SESDR ASAA0956398Control Valve · faultedON LANDING "RECALL" LEFT PACK LIGHT ILLUMINATES "AIR COND" LIGHT ILLUMINATES ON 6 PACK AND BOTH RESET WITH MASTER CAUTION. PERFORMED BITE CK REF FIM 21 62 TASK 801. FOUND LEFT ZONE TEMP CONT FAULTED LEFT TCV. REMOVED AND REPLACED LEFT TCV REF MM 21 51 10. SDR ASAA0956383Chain · brokenWHILE SERVICING OILS NR 2 ENG, FOUND OIL CAP CHAIN BROKEN. INSTALLED NEW OIL CAP CHAIN PER AMM 79 11 01.SDR ASAA0956380Oil Cooler · leakingAPU OIL COOLER IS LEAKING OIL. REMOVED AND REPLACED APU OIL COOLER REF MM 49 91 41, LEAK CHECK GOOD ROTABLE PART VERIFIED BY SEAMC.SDR ASAA0956286Wire · not seatedUNABLE TO TRANSMIT ON HF 1 RECEIVE WAS OK. DIVERSION TIME 1 HR 2 MIN. REF WDM FOUND WIRE W0811 2534B 24 NOT SEATED AT TB812 YB7. SEATED WIRE 2534B 24 AT TB812. WHILE ACCOMPLISHING CONTINUITY CHECK FOUND CONNECTOR D8509P NOT COMPLETELY SEATED AT E8 1 SHELF.SDR ASAA0956210Shroud · damagedNR1 ENG FAN FRAME JUST FWD OF ABRADABLE SHROUD IS MISSING .25 WIDE 360 DEG OF COATING GROUNDED, YES. REPAIRED IAW 70 62 14 USING ALT METHOD STEP 4.DSDR ASAA0956120Coupler · failedINTERMITTENT COMM SELECTION ON NR 2 COMM SELECTOR. NR 1 HF AND NR 2 VHF INTERMITTENT ON NR 2 RTP. AFTER CYCLING SWITCHES SEVERAL TIMES OPS CK GOOD FOR REMAINDER OF FLIGHT. ACFT GROUNDED. REPLACED NR 2 RADIO TUNING PANEL, OPS NORMAL REF MM 23-12-41-400-801/8SDR ASAA0956090Transceiver · intermittentHF NR 1 INTERMITTENTLY CUTS OUT DURING TRANSMISSION, BOTH CAPTS AND F/O'S MIC. ACFT GROUNDED. AFTER NUMEROUS TEST DUPLICATED PROBLEM NR1 HF CUTS OUT ABOUT EVERY 7 TIMES. REPLACED NR1 HF TRANSCEIVER REF MM 23-11-21-000-801 OPS CHECK NORMAL IAW MM 23-11-21-40SDR ASAA0956014Antenna · malfunctionedWXR GENERATED RANDOM SPIKES ON BOTH DISPLAYS AT RANGES GREATER THEN 40 MILES. GROUNDED YES. UNABLE TO DUPLICATE. DUE TO HISTORY REMOVED AND REPLACED WXR R/T OPS TEST GOOD REF MM 34 43 41 400 801. VERIFICATION FLIGHT FAILED. REMOVED AND REPLACED WXR DRIVE UNIT SDR ASAA0956005Radar · malfunctionedALTHOUGH RADAR APPEARED TO OPPERATE NORMALLY IT GENERATED RANDOM SPIKES THAT WERE IDENTICAL ON BOTH DISPLAYS THE RADAR WAS ON FOR MOST OF THE FLT BUT ONLY STARTED SPIKING DURING THE LAST 1.5 HOURS AND ONLY ON RANGES GREATER THEN 40 MILES GROUNDED YES. COULD NSDR ASAA0955971Computer · faultyRT FMC FAILED. DID NOT RESTORE WITH BOTH FMC'S ON LT. VERIFIED FAULT. RT FMC INOP. PERFORMED FIM 34 61 00 810 807. FMC RT TESTS OK. FMC XFER SWITCH SET TO NORMAL. CONFIRMED INTERMITTENT FAULT.SDR ASAA0852546Stiffener · damagedDRILL START MARK ON STIFFENER ANGLE IN AIR CON BAY AT BS 663 RBL 40. REPLACED IAW EA5310 02768.SDR ASAA0752009Structure · damagedLT WINGLET DAMAGED DUE CONTACT WITH AIRCRAFT N784 AT GATE. REMOVED AND REPLACED WINGLET ASSY PER AMM 57 20 21.SDR ASAA0751411Frame · bentAFT INNER FRAME UPPER CORNER OF THE L1 DOOR IS BENT AND CRACKED DUE TO CONTACT WITH JETWAY. ACCOMPLISHED EA5210 01220 REPAIR ANGLE.SDR ASAA071411Door Frame · bentAFT INNER FRAME UPPER CORNER OF THE L1 DOOR IS BENT AND CRACKED DUE TO CONTACT WITH JETWAY. ACCOMPLISHED EA5210 01220 REPAIR ANGLE.
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