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 ASAA11510808Transceiver · failedPWS FAIL ILLUMINATED. REPLACED WXR RECEIVER / TRANSMITTER REF MM 34 43 11. WEATHER RADAR SYSTEM OPERATIONAL TEST PASSED REF MM 34 43 00.SDR ASAA11510806Unknown · malfunctionedSPEED TRIM FAIL LT ON RECALL. PERFORMED LAND VERIFY TESTS SYS TESTS GOOD. REF MM 22 00 01 730 801.SDR ASAA2011121410810Valve · failedZONE TEMP DURING RECALL "CONT CAB". ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE REF MM 21-62-00-810-801. RT CONTROLLER LOGS FLT DECK TRIM VALVE ON ALL PREVIOUS FLIGHTS. REPLACED THE FLT DECK ZONE TRIM VALVE PER AMM 21-61-21-000-801. BITE CHECK GOOD. LEAKSDR ASAA11510803Windshield · crackedON CLIMBOUT THROUGH 24K FEET COPILOT'S WINDSHIELD HAD A LOUD POP AND CRACKED (OUTER PANE) PANE WITH CRACKS GOING ACROSS AND ALL THE WAY TO THE OTHER SIDE. A MINUTE LATER THE "OVERHEAT" ANNUNICATOR CAME ON. RAN QRH FOR WINDOW DAMAGE AND RETURNED TO HNL. DIVESDR ASAA11510778Antenna · failedDURING CRUISE PWS FAIL IN TERR MODE AND WXR FAIL IN WXR MODE. REPLACED WXR ANTENNA REF MM 34 43 11 400 800 34 43 11 000 801 & OPS CHECK OK REF MM 34 43 00 710 802 001.SDR ASAA11510761Unknown · malfunctionedWEATHER RADAR OPERATED NORMALLY FOR OCEANIC CRUISE. AT END OF OCEANIC PORTION OF FLIGHT WEATHER RADAR WAS TURNED OFF AND TERRAIN WAS SELECTED FOR DISPLAY. "ANS FAIL" WAS ANNUNCIATED ON BOTH NAV DISPLAYS WEATHER RADAR WAS TURNED BACK ON AND "WXR FAIL" WAS ANNSDR ASAA11510760Fmc · malfunctionedWHILE FLYING AN RTA ARRIVAL OVER OLM FMCS DISAGREED WITH EACH OTHER BY 2 MINUTES. THE RTA WAS 2336Z FMC 1 SHOWED 2336Z FMC2 SHOWED 2328Z. FMC 2 ALSO SHOWED DIFFERENT SPEED AND DESCENT POINT ONCE FMC 2 POINT WAS REACHED IT THEN STAVED TO FMC 1 INFORMATION. VSDR ASAA11510711Screw · looseREF T/C 78472000 NR 2 ENG INLET & FAN BLADES DETAILED INSP FOUND STRUT PNL BETWEEN STRUTS 8 & 9 POS HAS LWR FWD FAST LOOSE. TORQUED BOLT TO 61 IN LBS PER AMM 72 23 07 400 801. OK FOR SERVICE.SDR ASAA11510695Transceiver · faultyWEATHER RADAR "SPOKING" THROUGHOUT FULL SWEEP IN VARIOUS RANGES & INTENSITIES. UNDERLYING WEATHER RETURNS UNRELIABLE. REPLACED WXR R/T REF MM 34 43 41 000 801 & 34 43 41 400 801. OPS NORMAL REF MM 34 43 00 710 802 001. ETOPS GROUND VERIFICATION TEST SUCCESSDR ASAA11510656Fmc · malfunctionedFMC CLOCK IS SHOWING 5HRS BEHIND CORRECT ZULU TIME. ACARS TIMES ARE REPORTING INCORRECTLY. PERFORMED FMCS OPS TEST TASK 34 61 00 710 801 OPS CHECK GOOD FMC'S ARE SHOWING CORRECT TIMES.SDR ASAA11510586Engine · overtempDUE TO APU EGT ABOVE THE THRESHOLD. REMOVED APU AND INSTALLED SERVICEABLE APU. OPS & LEAK CHECKED OK.SDR ASAA11510389Valve · failedDURING CLIMBOUT NOTICED A DUCT PRESSURE SPLIT LEFT READ 29 PSI RIGHT READ 44PSI AFTER LEVEL OFF NEEDLES PAIRED AT 34 PSI. FOUND PRE COOLER VALVE NEED REPLACEMENT REPLACED PER AMM 36 12 01. COMP ENG NR 1 BLEED AIR SYS HEALTH CK PER AMM 36 11 00 700 801. FOUNSDR ASAA11510339Hmu · failedFOUND FAULT CODE 73 20341 FMV OUT OF RANGE ON NR 1 ENG SHORT TERM FAULT. ACCOMP FIM 73 25 803 & 75 34 819 CONTINUITY AND RESISTANCE CHECKS NORMAL. EEC BITE CTRL LOOPS INPUT MONITORING SHOWS NO FMV DATA CHANNEL B. ELECTRICALLY SLAVING IN SERVICEABLE HMU CAUSSDR ASAA1150251Valve · failedNR 2 ENGINE OIL QTY SIGHT GAUGE SHOWS NO OIL YET ENGINE WAS SERVICED TO FULL DURING RON. PERFORMED NR 2 ENGINE IDLE RUN FOR 12 MIN. OIL QTY RETURNED TO FULL THEN DECREASED AGAIN. REF MM 71 00 00 201. REPLACED OIL ANTI LEAK VALVE PER MM 79 21 09 401. ALL TSDR ASAA11510229Sign · detachedEMERGENCY EXIT SIGN HAS BECOME DETACHED FROM CEILING MOUNT BETWEEN AFT BATHROOMS/LAVS. REPLACED EMERGENCY EXIT SIGN AT AFT ENTRY OPS CHECK GOOD.SDR ASAA11510233Unknown · malfunctionedFMC DISAGREE LIGHT ILLUM. PERFORMED QRH PROCEDURE. OPS NORMAL.SDR ASAA1159668Warning System · malfunctionedLEFT PACK LIGHT ILLUMINATED TRIP RESET EXTINGUISHED LIGHT PER QRH. COULD NOT DUPLICATE. PERFORMED FIM 21 53 00 810 803, OPS CHECK NORMAL.SDR ASAA1159663Unknown · malfunctionedON PUSHBACK HNL GOT FMC DISAGREE LIGHT. FOLLOWED QRH PROCEDURE EVERYTHING NORMAL CONTINUED FLIGHT NORMALLY.SDR ASAA1159641Exciter · faultyON NR 1 LEFT SIDE ENG START ATTEMP GOT NORMAL START INDICATIONS UNTIL FUEL LEVER RAISED TO IDLE. FUEL FLOW MOMENTARILY WENT TO 1200 1100 PPH THEN DROPPED TO 550 PPH THEN DROPPED TO 0 ZERO. DID NOT GET ANY EGT RISE NO LIGHT OFF. QRC/QRH ACCOMPLISHED. REPLACSDR ASAA1159568Regulator Valve · failedIN CLIMB N 98 PERCENT LEFT PACK OFF ENG NR 1 BLEED OFF ISOLATION VALVE CLOSED LEFT DUCT PRESSURE 30 PSI. AT CRUISE POWER 87 PERCENT SAME SWITCH POSITIONS LEFT DUCT PRESSURE 20 PSI. REPLACED NR 1 ENGINE PRSOV IAW B737 MM 36 11 04. LK TEST GOOD IAW B737MM 36 SDR ASAA1159559Shutoff Valve · failedWITH ISOLATION VALVE CLOSED AND NR 1 BLEED OFF LEFT DUCT PRESSURE DROPS TO 15 PSI THEN CLIMBS UP TO 19 PSI ETOPS FLT CHECKLIST 9A (8) A. ON GROUND WITH ENGINE NR 2 SHUT DOWN APU BLEED OFF L DUCT PRESSURE STARTS AT 0 AND CLIMBS TO 9 PSI. REPLACED NR 1 ENG PRSSDR ASAA1159590Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL 120DF HAS SEVERAL AREAS OF LIGHT SURFACE CORROSION REMOVED CORROSION IAW ASA EA 2550 01425 FWD AND AFT CARGO PIT ALUMINUM FLOOR PANELS BOEING CPM 20 40 03 FOUND TO BE OUT OF LIMITS IAW B737 400 SRM 53 30 53 FIG 101 DETAIL 5 ORSDR ASAA1159589Floor Support · corrodedFORWARD CARGO COMPARTMENT AT AFT BULKHEAD FLOOR SUPPORT/AFT BULKHEAD ATTACH ANGLE CORRODED ENTIRE LENGTH. SUPPORT ANGLE CORRODED BEYOND SRM 53-30-53 LIMITS. REMOVED ANGLE SUPPORT IAW SRM 51-40-02. RECEIVED NEW ANGLE SUPPORT PART NUMBER 143A9485Y35 PO 708634SDR ASAA1159279Fuel Control · faultyAPU WILL NOT START FAULT LIGHT ON. ACCOMPLISHED APU BITE TEST. FOUND FAULT CODES: 49 31175 49 52192 49 31160 49 31168 & 49 52188. REPLACED APU FUEL CONTROL UNIT REF MM 49 31 11 000 801 / 49 31 11 400 80. PERFORMED FUEL CONTROL UNIT INSTALLATION TEST NO DEFSDR ASAA1159248Charger · inoperativeELEC LIGHT CAME ON AT TOUCHDOWN. ACCOMP FIM 24 31 TASK 829 BAT CHARGER INOP MSG ON P5 13 MODULE. REPLACED BATT CHARGER M5 REF MM 24 31 21. FAILED OPS CHECK. FOUND EVIDENCE OF OVERCHARGING ON MAIN BATT. VERIFIED WIRING IS GOOD REPLACED MAIN BATTERY REF MM SDR ASAA1159247Unknown · malfunctionedAPU FAULT NO ROTATION 49 41012. PERFORMED FIM 49 40 TASK 803. NO CORRESPONDING FAULTS RECORDED. ATTEMPTED START WITH SUCCESSFUL START. NO FAULTS RECORDED. OPS CHECK NORMAL.SDR ASAA1159086Warning System · intermittentAFTER PARKING AT GATE SWITCHED TO GROUND POWER. POWER SUBSQUENTLY DROPPED OFF AND AIRCRAFT WENT TO NO POWER. DURING BATTERY START OF APU EGT WENT TO 1,000 DEGREES AND HUNG UP THERE. WE SHUT IT OFF AND TRIED A SECOND TIME. SECOND START WAS SUCCESSFUL AFTER SDR ASAA1159074Blade · damagedWHILE PERFORMING T/C 78472002 ON NR 1 ENGINE FOUND NR 17 BLADE PLATFORM WITH TORN RUBBER STRIP. REPLACED NR 17 PLATFORM P/N OFF 340 001 816 0 & INSTALLED PLATFORM P/N 340 001 816 0 PER T/C 78472002. PERFORMED FAN BLADE SURVEY PER T/C 78472002 STEP 55 CHECKS SDR ASAA1159052Filter Element · defectiveAPU WILL NOT START. REMOVED AND REPLACED APU LUBE FILTER ELEMENT AND LUBE FILTER HOUSING PER AMM 49 91 12 000 802. SERVICED APU OIL TO FULL IAW AMM 49 91 13 PB 301. ACCOMPLISHED GROUND OPS CK PER AMM 49 11 00 710 801.SDR ASAA1159030Unknown · malfunctionedAFTER START "ELEC" LIGHT ILLUMINATED. PERFORMED RIM TASK PER 24 31 00 810 801. FOUND BATT INOP FAULT. CLEARED FAULT PERFORMED M/M MAIN BATT CHARGER OPERATIONAL CHECK PER MM 24 31 710 801. ALL OPS CHECK PASSED GROUND VERIFICATION GOOD.SDR ASAA1159029Unknown · malfunctionedDURING RECALL CONTROL CABIN "ZONE TEMP" LIGHT ILLUMINATES. LIGHT EXTINGUISHES AT MASTER CAUTION RESET. BITE OF NR 2 CONTROLLER SHOWS FLT DECK TCV FAULT IN HISTORY. ACCOMPLISHED BITE AND RESET FAULT. BITE TEST NORMAL REF AMM 21 61 00.SDR ASAA1158963Sensor · failedRIGHT FORWARD WINDOW HEAT " OVERHEAT " ILLUMINATED. ACCOMPLISHED QRH PROCEDURE LIGHT REMAINED ON. PUT SENSOR IN THE OTHER POSITION BITE CK'D WHICH NO FAULTS OPS CHECK WINDOW HEAT SYS PER AMM 30 41 00, OP NML.SDR ASAA1158722Idg · failedCREW REPORTED NR 2 ENG GENERATOR DRIVE LIGHT WILL NOT ILLUMINATE UPON ENGINE SHUTDOWN. LIGHT TEST WORKS GOOD. REPLACED NR 2 ENG IDG REF MM 24-11-11. OPS NORMAL.SDR ASAA1058575Warning System · false activationFMC DISAGREE LIGHT CAME ON DURING TAXI. PERFORMED QRH LIGHTS WENT OUT. OPS NORMAL.SDR ASAA1058299Warning Light · false indicationFMC DISAGREE LIGHT ILLUMINATED. RAN QRH NO FURTHER ISSUES AFTER RESET.SDR ASAA1058293Shim · damagedDURING NR 2 ENGINE FAN BLADE LUBE FOUND ALL 24 FAN BLADE SHIMS MISSING PROTECTIVE COATING. REPLACED ALL 24 FAN BLADES SHIMS P/N 340 252 307 0 REF. T/C 78472002.SDR ASAA1058261Idg · malfunctionedNR 1 IDG DELTA P "POPPED" SEAMC NOTIFIED. TSR ISSUED DUE TO HISTORY OF NR 1 IDG DPI EXTENSIONS. ACCOMPLISHED STEP NR 1 OF TSR IDG OIL CHANGE AND FLUSH FILTER HAS NO CONTAMINATION AMM 12 13 21 600 802. REPLACED IDG PER STEP NR 2 OF TSR PER AMM 24 11 11 00 80SDR ASAA1058242Switch · faultyNR 2 ENGINE LOGGED FAULT NR 73 30312 THE START SWITCH SIGNAL AND ARINC BUS DATA DISAGREE FOUND WHILE ACCOMPLISHING T/C 78273000 INTERROGATE THE FMC CDU FOR ENGINE FAULTS. REMOVED AND REPLACED NR 2 ENGINE START SWITCH. CONFIRMED CORRECTED REF FIM TASK 73 24 0SDR ASAA1058103Filter · defectiveNR 1 IDG DELTA P "POPPED". SEAMC NOTIFIED. ACCOMPLISHED NR 1 IDG ENGINE DPI FAULT ISOLATION REF AMM 24 11 00 810 803. REMOVED AND REPLACED NR 1 ENG IDG SCAVENGE AND CHARGE FILTERS REF AMM 24 11 41 200 801. PERFORMED ENG RUN AND LEAK CHECKED GOOD. NO DISCRSDR ASAA1058017Indicator · warning lightPRIOR TO PUSHBACK F/O FD FLAG CAME ON. CYCLED POWER F/O FD FLAG RESOLVED, OPS NORMAL.SDR ASAA1058013Housing · brokenL 1086 EXIT LOCATOR SIGN STA 303 LENS ASSY TAB IS BROKEN (P/N 82000 48301) REF 33 27 11 REMOVED & REPLACED FWD EXIT LOCATOR SIGN W/ FWD F/A MASTER CALL LIGHT MODULE REF AMM 33 51 01, OPS NORMAL. FWD F/A CALL LIGHTS OPS NORMAL REF 23 43 00 & 33 27 00.SDR ASAA1057922Linkage · out of adjustRT RAM AIR DEFLECTOR DOOR FOUND OUT OF RIG WILL NOT LOCK OPEN. ADJUSTED RT RAM AIR INLET DOOR LINKAGE REF M/M 21 55 22 400 803 RIG IS NOW GOOD DOOR LOCKS OUT CORRECTLY REF M/M 21 51 22 400 803. PACK/ZONE TEMP CONTROLLER BITE CK GOOD REF M/M 21 61 00 700 806 SDR ASAA1057921Linkage · out of adjustLEFT RAM AIR DEFLECTOR DOOR FOUND OUT OF RIG WILL NOT LOCK OPEN. ADJUSTED LT RAM AIR INLET DOOR LINKAGE REF M/M 21 55 22 400 803 RIG IS NOW GOOD DOOR LOCKS OUT CORRECTLY REF M/M 21 51 22 400 803. PACK/ZONE TEMP CONTROLLER BITE CHECK GOOD REF M/M 21 61 00 700SDR ASAA1057508Radar · malfunctionedPWS FAIL WXR FAIL ANT DISPLAYED DURING WEATHER RADAR. CYCLED WXR PWR. WXR OPS CHECK NORMAL REF MM 34 43 00. NO HISTORY 60 DAYS.SDR ASAA1057474O-Ring · cutDISCOVERED CUT IN NR 2 ENG OIL CAP O-RING. REMOVED AND REPLACED NR 2 ENG OIL CAP O-RING.SDR ASAA1057413Valve · failedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATES ON RECALL. ACCOMPLISHED FIM 21 62 00 810 832 FOUND CONTROL CABIN TRIM AIR VALVE BAD. REPLACED TRIM AIR VALVE PER AMM 21 61 21 00 801 21 61 21 400 801 LEAK & OPS CHECKS GOOD. RE-ACCOMPLISHED FIM 21 62 00 810 832, NO SDR ASAA1057408Wire · brokenFD FLAG APPEARS ON CAPTAINS PFD. FOUND BROKE WIRE NEXT TO BB C1049 REPAIRED WIRE FRF SWPM 20 30 12. REMOVED AND REINSTALLED "A" FCC AND THE INTEGRATED FLIGHT SYSTEM ACCESSORY UNIT FOR TROUBLESHOOTING REF MM 22 11 33/401 AND MM 22 11 37/401 CHECKED GOOD. ACCSDR ASAA1057263Detector · faultyWHILE TURNING FINAL APU OFF APU DET INOP LIGHT ILLUMINATED. REMOVED AND REPLACED APU OVERHEAT DETECTOR TAIL CONE SECTION. PS TEST GOOD. REF MM 26 15 01. FAULT WAS CONFIRMED TO TAIL CONE DETECTOR USING FIM 26 10 00 810 801.SDR ASAA1057252Unknown · malfunctionedDURING AFTER START CHECKLIST THE LT PACK LIGHT ILLUMINATED ALONG WITH M/C AND AIR CONDITIONING DURING RECALL CHECK. PRESSING M/C CANCELLED THE THREE WARNINGS. DURING FLIGHT THE RECALL CHECK PRODUCED NO WARNINGS, NORMAL OPS. PERFORMED OPERATIONS CHECK PER FISDR ASAA0957074Start Valve · malfunctionedNR 1 ENG NO ROTATION START VALVE DID NOT OPEN ON ENGINE START. REPLACED NR 1 ENG START VLV REF AMM 80 11 03, OPS CHECK GOOD.
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