N565AS
Service difficulty reports · 509
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 = 'N565AS' 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 = 'N565AS' 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 ASAA2012100593037Exciter · inoperativeATTEMPTED THREE COLD SOAK STARTS ON THE APU AT FL 400, ALL THREE ATTEMPTS RESULTED IN FAULT LIGHTS ILLUMINATING. REMOVED AND REPLACED IGNITION UNIT REF MM 49-41-31. PERFORMED FIM TASK 49-40 TASK 85. DISCONNECTED D10434 AND P13. CHECKED PINS 16/17 AND 2/1. NO SDR ASAA2012090992864Control Arm · damagedFMC CDU FAULT CODE 73-30792 FOUND. ACFT GROUNDED. R & R NR 2 ENG EEC. SOFTWARE VER 2044M25P14. EEC TEST, DISCRETES TEST, FADEC TEST, ACTUATORS TEST ALL PASSED. IDENT/CONFIG CHECKS. NO FAULTS LOGGED. REF MM 73-21-60, 71-00-00, 73-21-00.SDR ASAA2012083092807Fmc · false activationFMC DISAGREE LIGHT ILLUMINATED ON TAXI. ACFT GROUNDED. RAN CHECKLIST - LIGHT EXTINGUISHED.SDR ASAA2012082992792Connector · looseRT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED, PERFORMED QRH AND LIGHT WENT OUT THEN ILLUMINATED AGAIN. ACFT GROUNDED. PERFORMED WINDSHIELD HEAT CONTROL UNIT BITE CHECK. FOUND P9- CONTROL POWER FAULT. VERIFIED FAULT, CLEARED & PERFORMED WINDSHIELD HEAT CONTROLSDR ASAA2012082992791Control Valve · faultedLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. EXTINGUISHES ON RESET. ACFT GROUNDED. PERFORMED BITE OF NR 1 PACK ZONE TEMP CONTROLLER, TEMP CONTROL VALVE FAULT PRESENT, R & R NR 1 TEMP CONTROL VALVE IAW AMM 21-51-10, TESTED GOOD.SDR ASAA2012082492774Transceiver · contaminatedPWS FAILED APPEARED ON BOTH NDS WITH TOGA, DISAPPEARED AT ROTATION AND THEN REAPPEARED FOR 2000 FT. REAPPEARED WITH LANDING FLAP SELECTION. ACFT GROUNDED. PERFORMED WEATHER RADAR OPS TEST, NO DISCREPANCIES NOTED. ON EXAMINING WEATHER RADAR TRANSCEIVER, NSDR ASAA2012080292657Radar · malfunctionedWEATHER RADAR TILT APPEARS TO NEED CALIBRATION. NEED 4 DOWN TILT TO SHOW GROUND RETURN AT 80 MILES VERSUS 1 DOWN TILT NORMALLY. ACFT GROUNDED. PERFORMED WEATHER RADAR SYS TEST IAW AMM 34-43-00. UNABLE TO DUPLICATE DEFECT. ALL GROUND FUNCTIONAL TESTS PASS NSDR ASAA2012081292708Panel · damagedNR 1 ENGINE FAN DUCT PANELS AT 100, 300, 500 AND 1100 LOCATIONS HAVE PULLED THROUGH BOLTS, LOOSE BOLTS (2 LOC) AND LOOSE PANEL RESPECTIVELY. ACFT GROUNDED. TIGHTENED PANELS AT 100, 300 & 500. REPLACED PANEL AT 1100 IAW AMM 72-23-07-000-801-F00.SDR ASAA2012070892509Apu · malfunctionedAPU WILL NOT CARRY PNEUMATIC LOAD. PERFORMED APU BITE IAW FIM 4960-TASK 801 APU FAULTED 49-31171, FCU DISAGREES WITH COMMAND. C/W FIM 49-31-00-810-808 THROUGH F(1)(E) 1, NO FAULTS FOUND.SDR ASAA2012070792488Generator · failedNR 2 ENGINE GENERATOR OFF BUSS BLUE LIGHT AND NR 2 SOURCE OFF AMBER CAME ON IN FLIGHT WITH ASSOCIATED ELECTRICAL AMBER MASTER CAUTION LIGHT. PERFORMED QRH PROCEDURE AND NR 2 ENGINE GENERATOR OFF BUSS BLUE LIGHT REMAINED ON, AS WELL AS AMBER SOUCE LIGHT. STARTSDR ASAA2012071592551Transceiver · failedPWS FAIL WHEN WX RADAR TURNED OFF. ACFT GROUNDED. REPLACED WEATHER RADAR RT, REF MM 34-43-41. WEATHER RADAR GROUND VERIFICATION TEST NORMAL, REF MM 34-43-00.SDR ASAA2012071492540Antenna · failedPWS FAILED DURING DESCENT AS WX RADAR WAS SECURED AFTER WORKING ALL THE WAY. TURN WX OFF AND BACK ON WOULD WORK A SHORT WHILE THEN FAIL AGAIN. ACFT GROUNDED. R & R WEATHER RADAR DRIVE UNIT IAW AMM 34-43-11. OPS TEST PASSED.SDR ASAA2012071492539Transceiver · failedPWS FAIL, DISPLAYED ON NDS. ACFT GROUNDED. REF FIM TASK 34-43-00-810-815, WXR OPERATIONAL TEST SHOWS RT FAIL MSG. R & R WXR RT IAW MM 34-43-41-000-801, OPS TEST GOOD IAW MM 34-43-00-710-802-001.SDR ASAA2012071392538Transceiver · failedON GROUND PWS FAIL ANNUNCIATION. ACFT GROUNDED. REPLACED WX RADAR R/T IAW MM 34-43-41-000-801. WX RADAR AND PWS SYSTEMS GROUND VERIFICATION, OPS CHECK GOOD IAW MM 34-43-00.SDR ASAA2012071192532Connector · dirtyNR 1 ENGINE HAS EXPERIENCED A LARGE, SUDDEN INCREASE IN CRUISE DELTA EGT. FUEL FLOW AND CORE SPEED HAVE REMAINED STABLE. ACCOMPLISHED T49.5 PROBE AND EGT SYSTEM INSPECTION, REF MM 77-21-01-200-801-F00. FOUND SLIGHTLY HIGH RESISTANCE BETWEEN PIN H AND PIN LSDR ASAA2012060992332Exciter · malfunctionedAPU FAILED TO START. FAULT CODE 49-41011. MAINT MESSAGE NO FLAME SHUTDOWN. REPLACED THE APU IGNITION UNIT (EXCITER) IAW AMM 49-41-31-400-801. OPS NORMAL.SDR ASAA12511650Connector · dirtyNR 1 ENG BOTTOM RT EGT SIGNAL (T495S2) IS OUT OF RANGE. ACCOMPLISHED T49.5 PROBE AND EGT SYS INSPECTION IAW MM 77-21-01-200-801-F00. FOUND SLIGHTLY HIGH RESISTANCE BETWEEN PIN H AND PIN LOWER CASE A OF 15.6 OHMS ON CONNECTOR J9 DP0909. CLEANED CONNECTOR REFSDR ASAA2012062392396Warning Light · false activationLEFT RAM DOOR FULL OPEN LIGHT ILLUMINATED AT CRUISE ALTITUDE, FL 360. ACFT GROUNDED. ALL CIRCUIT BREAKERS ARE IN, NO FAULTS ON EITHER PACK ZONE TEMP CONTROL SYSTEM. RAN VERIFICATION ON BOTH PACK ZONE TEMP CONTROL SYSTEMS, RAN BITE ON NR 1 PACK ZONE TEMP CSDR ASAA2012061792378Exciter · inoperativeTWO APU START ATTEMPTS BOTH RESULTED IN FAULT LIGHT , NO START. ACFT GROUNDED. R & R, AND TESTED APU IGNITION UNIT IAW MM 49-41-31-400-801. TEST PASSED. APU BITE SHOWS NO CURRENT FAULTS THROUGH 3 START CYCLES. REPAIR CONFIRMATION SUCCESSFUL IAW FIM 49-40-00SDR ASAA2012061892370Start Valve · failedDURING START OF NR 1 WITH GROUND AIR SOURCE. NORMAL START BUT START VALVE OPEN. LIGHT REMAINED ON AT NORMAL IDLE. ACFT GROUNDED. R & R NR 1 ENG START VALVE REF MM 80-11-03-400-801. OPS NORMAL.SDR ASAA12511571Autoland Sys · unknownAUTOLAND & HEADINGS, LANDED LEFT OF CTR LINE OVER LEFT RUNWAY CENTER LIGHTS AT 1000FT AND CONTINUED TO DIVERGE TO THE LEFT DISCONNECTED AUTO PILOT AND RETURNED TO CENTER LINE. ACFT GROUNDED. PERFORMED SUCCESSFUL LAND VERIFY TEST IAW AMM 22-11-00-700-801. DISDR ASAA12511561Connector · dirtyWHILE ACCOMPLISHING T/C 78273000 FOR NR 2 ENG FOUND FAULT CODE 77-20862. THE BOTTOM LT EGT SIGNAL (T495S3) IS OUT OF RANGE. ACFT GROUNDED. PERFORMED FIM 77-21-00-810-803. CLEANED EGT CONNECTOR REF AMM 77-21-00. AFTER CLEANING, READING GOOD.SDR ASAA12511526Transceiver · failedRADAR PAINTING RED WHEN OUT OF CLOUDS AND NO RAIN REGARDLESS OF TILT. ACFT GROUNDED. R & R WEATHER RADAR TRANSCEIVER. OPS TESTED GOOD REF AMM 34-43-00-34-43-41.SDR ASAA12511525Lens · missingEXIT SIGN AT R2 FELL OFF. ACFT GROUNDED. R & R R2 DOOR EMER EXIT LIGHT ASSY IAW AMM 33-51-14-960-802.SDR ASAA12511500Actuator · leakingGROUND CREW NOTIFIED FLIGHT CREW OF FLUID LEAKING FROM NR 2 ENGINE DURING THE NR 2 ENGINE START. FLIGHT CREW SHUTDOWN ENGINE AFTER THIS NOTIFICATION. ACFT GROUNDED. FOUND RT VSV ACTUATOR LEAKING BEYOND LIMITS. REPLACED RT VSV ACTUATOR ON NR 2 ENGINE . REF AMSDR ASAA12511479Hmu · failedDURING NR 1 ENGINE TEST VIBRATION SURVEY, ENGINE BEGAN TO SURGE AND STALL UNCOMMANDED WHILE APPROACHING 81 PERCENT N1 FOLLOWED BY MASTER CAUTION LIGHT ENGINE INDICATION ON THE 6 PACK FOLLOWED BY LOW OIL PRESSURE INDICATION AND "ENG FAIL" ILLUM PRI ENG DISP ENSDR ASAA12511461Cone · gougedDURING NR 1 ENGINE FAN LUBE FOUND DEEP GOUGE ON MATING SURFACE OF FRONT SPINNER CONE. ACFT GROUNDED. R & R FRONT SPINNER CONE ON NR 1 ENG REF MM 72-21-01-400-801-F00.SDR ASAA12511460Shim · wornDURING NR 1 ENGINE FAN LUBE FOUND ALL BLADE SHIMS MISSING MOLYDAG COATING. ACFT GROUNDED. R & R NR 1 ENGINE 24 FAN BLADE SHIMS. REF MM 72-21-02-400-801-F00.SDR ASAA1251459Seal · tornDURING NR1 ENGINE FAN LUBE FOUND 18 OF THE 24 BLADE PLATFORMS WITH TORN OR MISSING SEALS. ACFT GROUNDED. R & R COMPLETE SET OF 24 EA BLADE PLATFORMS ON NR 1 ENG, REF MM 72-21-02-400-801-F00.SDR ASAA12511441Connector · dirtyON PREFLIGHT, FOUND ENGINE NR 2 EGT DISPLAY BOX HIGHLIGHTED IN RED VERSUS, RESET RED BOX ALERT DUE TO EGT CONNECTOR CLEANING ON NR 2 ENG REF TSR905906, EGT SENSOR CLEANING. OPS NORMAL, REF AMM 71-00-00-740-801-FOO.SDR ASAA12511132Control Valve · malfunctionedLT PACK LIGHT ILLUMINATED ON RECALL AND WOULD NOT RESET. ACCOMPLISHED FIM TASK 21 62 00 810 801 ZONE TEMP CONTROLLER BITE TEST. FOUND TCV FAULT ON NR 1 TEMP CONTROLLER. INTERMITTENT FAULT RESET. PACK OPS NORMAL. GROUND TEST VERIFIED INTERMITTENT FAULT. DUSDR ASAA12511129Warning Light · false activationLEFT PACK LIGHT ILLUMINATED AFTER PUSHBACK. QRH FOLLOWED. LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. ON ARRIVAL, PERFORMED FIM TASK 21-62-00-810-801. NR 1 CONTROLLER TCV LIGHT ON RESET NR 1 CONTROLLER RAN BITE TEST TWO MORE TIMES WITH NO ISSUES.SDR ASAA12511093Warning System · false activation"CAPT PITOT" AMBER LIGHT INDICATION REMAINS ON AFTER PLACING SWITCH TO ON. FOUND CAPT'S PITOT HEAT C/B OPEN ON THE P18 3 PANEL. RESET C/B 20 00 01 862 001. SELECTED CAPT'S PITOT TUBE HEATER SWITCH TO ON PITOT TUBE HEATER ANNUNICATOR EXTINGUISHED. PERF WATESDR ASAA12510901Terminal · damagedLEFT FWD WINDOW OVERHEAT LIGHT ILLUMINATED. FOUND TERMINAL LUGS ON THE C/B WIRE CONNECTION DISCOLORED AND CRACKED. REPLACED BOTH TERMINAL LUGS ON THE C/B REF SWPM 20 30 11. LEFT FWD WINDOW HEAT OPS CK GOOD REF MM 30 41 00. GROUND VERIFICATION TEST OPS CK SSDR ASAA11510551Unknown · malfunctionedWITH AUTO PILOT "B" ENGAGED AIRPLANE ROLLED 1/4 DEGREE LEFT TO RIGHT (INDICATED ON THE AILERON TRIM INDICATOR ON YOKE) FLIGHT ATTENDANTS NOTICED IT MID CABIN. NO ISSUES WITH AUTO PILOT "A" ENGAGED. COULD NOT DUP. DFCS FAULT REVIEW NR 20 LOG NO FAULTS LAST LSDR ASAA11510351Unknown · malfunctionedFMC DISAGREE INDICATION ON THE GROUND. PERFORMED QRH PROCEDURE. FMC RESTORED.SDR ASAA11510256Oven · smokeFORWARD OUTBOARD OVEN EMITS BLACK SMOKE SMELLS LIKE BURNED FOOD. REPLACED FWD GALLEY OVEN REF AMM 25 32 01. OPS CHECK NORMAL.SDR ASAA11510200Wire · brokenAT CRUISE ALTITUDE FL340 ENGINE FIRE / OVERHEAT DETECTOR LIGHT (FAULT) ILLUMINATED. SYSTEM TEST OF ENGINE FIRE / OVERHEAT NR 1 ENG AND APU NORMAL ENG NR 2 WILL ONLY TEST ON "B" LOOP. FAULT CODE 2614052. REPLACED ENG AND APU FIRE DET CONTROL MOD PER AMM 26 1SDR ASAA11510187Eec · warning messageACQUIRED FAULT CODE ON EEC BITE TEST. FAULT CODE 77 20862 NR 2 ENG BOTTOM LEFT EGT SIGNAL OUT OF RANGE. GROUNDED YES. NR 2 ENG SHOW NO RECENT FAULTS EEC TEST CHECKED NORMAL. NO DEFECTS NOTED AT THIS TIME DURING EGT IND CLEANING & EGT PROBS ALL WITHIN LIMITS.SDR ASAA11510036Unknown · malfunctionedELEC LIGHT ON STATIC INVERTER INOP. PROBLEM OCCURED AFTER GND PWR FAILED. WHILE TROUBLESHOOTING SYS RETURNED TO NORMAL OPS PER 24 34 TASK 801. VERIFICATION FLIGHT SUCCESSFUL.SDR ASAA1159664Regulator · failedNR 2 ENG BLEED WON'T SHUTOFF WHEN SWITCH IS OFF. PERFORMED TROUBLESHOOTING OF NR 2 ENGINE BLEED SYSTEM FOUND NR 2 ENGINE BLEED AIR REGULATOR INOP. REPLACED BLEED AIR REGULATOR IAW B737MM 36 11 03 PERFORMED LEAK AND OPERATIONAL CHECK OF NR 1 AND NR 2 ENGINE BSDR ASAA1159351Unknown · malfunctionedATTEMPTED AUTOLAND WITH HGS UNSAT. "NO AIII" AND NO "FLARE ARMED" ANNUNCIATED FOR APPROACH. DFCS SHOWS NO INFLIGHT FAULTS. CURRENT STATUS BITE GOOD BOTH AUTOPILOT A & B. DFCS OPS TEST GOOD REF MM 22 11 00. HGS CURRENT STATUS AND CAPABILITY CHECKS GOOD. HSDR ASAA1159339Coupler · defectiveWITH NR 2 HF RADIO "ACARS NO COMM" MESSAGE DISPLAYED ALL THE WAY IN CLASS IT AIRSPACE. (ETOPS AIRSPACE TOO) AFTER LANDING RADIO CHECK IN VOICE ON GROUND YIELDED NO SIDE TONE WHEN MICROPHONE KEYED. CONFIRMED FAULT UNABLE TO TRANSMIT OR RECEIVE ON NR 2 HF DATASDR ASAA1159053Button · sticksF/O FMC R 1 BUTTON STICKS. VERIFIED DISCREPANCY. REPLACED FMCS CDU KEYBOARD REF MM 34 61 01. OPS NML REF SAME.SDR ASAA1159020Screen · cloggedZONE TEMP "CONT CAB" ILLUMINATE ON RECALL. ACCOMP FIM 21 62 #801 RT ZONE CONT LOGGED TRIM AIR VALVE FAULT CLEARED SAME. INSP VALVE & CONN ALSO CLEANED TEMP SENSOR SCREEN. GROUND VERIFICATION GOOD.SDR ASAA1158998Apu · malfunctionedON CLIMB F/A IN AFT CABIN REPORTED DIRTY SOX SMELL ON CLIMB THRU 10,000 DESCENT INTO SEA FLT ATTENDANTS AGAIN REPORTED DIRTY SOX SMELL ON DESCENT BELOW 10,000. FOUND APU COMPRESSOR DRAIN CONTAMINATED WITH OIL. REMOVED AND REPLACED APU REF TASK CARD 78349010 SDR ASAA1158908Unknown · malfunctionedENGINE NR 1 DRIVE LIGHT NOT ILLUMINATED WITH ENGINE SHUT DOWN. PERFORMED OPERATIONAL TEST REF AMM 24 11 00 700 802 "E". OPERATIONAL TEST NORMAL. NO HISTORY PAST 30 DAYS. OK FOR SERVICE AT THIS TIME.SDR ASAA1158860Charger · intermittentMAIN BATTERY SHOWS 28 VOLTS AND CYCLES BETWEEN 1 AND +1 AMPS. CONFIRMED FAULT, FAULT INTERMITTENT. REPLACED MAIN BATTERY CHARGER OPS CHECK SAME GOOD REF FIM 24-31-00/824.SDR ASAA1158806Unknown · malfunctionedUPON MASTER CAUTION RECALL AIR COND ON 6 PACK AND ZONE TEMP ON CONT CAB ILLUMINATE. BOTH LIGHTS EXTINGUISHED UPON MASTER CAUTION RESET. NR 2 ZONE TEMP CONTROLLER LOGGED FLT DECK TRIM AIR VALVE FAULT LAST FLT. PERFORMED FIM 21 62 TASK 842 FAULT CLEARED A & GSDR ASAA1058687Unknown · malfunctionedF/O FLIGHT DISPLAY NOT SHOWING V SPEEDS. FOUND RT FMC INOP MAP FLAG ON F/O'S SIDE. PERFORMED FIM 34 61 TASK 807. RT FMC OPS RESTORED. ETOPS GROUND VERIFICATION TEST SUCCESSFUL.
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