N570AS
Service difficulty reports · 547
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 = 'N570AS' 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 = 'N570AS' 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 ASAA201902047996Valve · failedLEFT PACK ZONE TEMP ILLUMINATES ON RECALL. GROUNDED - YES. REMOVED AND REPLACED LH (FLT DECK) ZONE TRIM AIR VALVE. REF AMM 21-61-21. OPS CHK GOOD.SDR ASAA2019011927880Start Valve · failedON RESTART NO N2 ROTATION NR 2 ENG. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG START VALVE REF AMM 80-11-03 NO DEFECTS NOTED AT THIS TIME. OPS CHK NORMAL.SDR ASAA2019011227746Warning System · false activationCONT CABIN ZONE TEMP ILLUMINATES ON RECALL LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. LEFT AND RIGHT PACK TEMP CONTROLLERS BITE AND OPS NORMAL REF FIM 21-62 TASK 801 AND 842. NO CURRENT FAULTS.SDR ASAA2019010427689Display · inoperativeCAPT MCDU "NEXT PAGE" PUSHBACK HAS NO TACTILE FEEDBACK. GROUNDED - YES. REPLACED CAPT CDU REF AMM 34-61-01-400-802 OPS CK OK. SOFTWARE CK OK REF AMM 34-61-00-750-802.SDR ASAA2018122927614Drain Mast · crackedAPU SHROUD DRAIN MAST POSSIBLE CRACK AT TOP SEAM. GROUNDED - YES. REMOVED AND REPLACED APU SHROUD DRAIN MAST REF B737-800 AMM 28-25-07.SDR ASAA2018122527581Lead · failed#1 ENGINE FAILED TO START USING "L" IGNITION. GROUNDED - YES. ACCOMPLISHED #1 ENGINE EEC BITE PROCEDURE, B737-800 FIM 73-00 TASK 801. NO FAULTS NOTED. PER FIM 74-21 TASK 806 STEP B.(2), REPLACED #1 ENG LEFT IGNITER PLUG REF B737-800 AMM 74-21-02. NO HELP. REPLSDR ASAA2018122127497Panel · damaged#2 ENGINE LPTACC SCOOP FAN DUCT PANEL HAS AFT TWO FASTENERS PULLED THROUGH PANEL. GROUNDED - YES. REPLACED LPTACC FAN DUCT PANEL REF B737-800 AMM 72-23-07-400-801-F00.SDR ASAA2018121727473Not Reported · malfunctionedFUEL IMBALANCE GOT PROGRESSIVELY WORSE DURING SHORT FLIGHT FROM SFO TO PDX, ABOUT 1+30 200 POUND IMBALANCE ON THE GROUND, 400 POUND IMBALANCE AT LEVEL OFF, 600 POUND IMBALANCE DURING DESCENT AND LANDING NR 2 TANK HIGH QTY. GROUNDED - YES. ACCOMPLISHED FUEL QTYSDR ASAA2018121727448Valve · intermittentTECH SERVICE REQUEST. FOLLOW-UP TO REPORTS OF FUEL IMBALANCE. GROUNDED - YES. REMOVED ENGINE CROSSFEED VALVE ACTUATOR REF AMM 28-22-21. ACCOMPLISHED CROSSFEED VALVE ALIGNMENT CHECK REF AMM 28-22-21-820-801. REINSTALLED CROSSFEED VALVE ACTUATOR REF AMM 28-22-21SDR ASAA2018121197311Compensator · out of limits#1 FUEL TANK IMBAL 4.38AND #2 FUEL TANK AT 5.59NO IMBALANCE ISSUES PRIOR TO THIS . HAPPENED VERY QUICKLY DESCENDING THRU 11,000 FEET INTO PDX LANDED WITH 4.06 IN #1 AND 5.37IN #2. GROUNDED - YES. ON TANK NO. 1, PERFORMED TANK & COMP. UNITS TEST REF B737-800 AMSDR ASAA2018121077262Unknown · multiple failWHILE IN CRUISE FL360 FMC P/RST SWITCH LIGHTS ILLUMINATED AND NO SCRATCHPAD MESSAGE WAS DISPLAYED. LOST BOTH LNAV AND VNAV. CHECKED QRH. REENGAGED LNAV AND VNAV AFTER APPROXIMATELY 2 MINUTES. NO FURTHER FAILURES. ALSO VTK WAS NEVER DISPLAYED. GROUNDED - YES. PSDR ASAA2018121077261Bonding Jumper · brokenWHILE ACCOMPLISHING T/C 78472000 FOUND ENGINE COWL TAI VALVE BONDING JUMPER BROKEN. GROUNDED - YES. REMOVED AND REPLACED TAI VALVE BONDING STRAP, REF B737-800 AMM 30-21-11.SDR ASAA2018103126682Unknown · malfunctionedIN CRUISE FLIGHT, RIGHT NAV DISPLAY LOST GUIDANCE AND DISPLAYED VTK MSG FOR APPROX 15 SECONDS. NORMAL OPERATION RESTORED W/OUT CREW INTERVENTION. GROUNDED - YES. PERFORMED FIM 34-61 TASK 836. R/H FMC OP'S NORMAL AND NO OTHER DEFECTS NOTED. A/C OK FOR SERVICE.SDR ASAA2018091226100Warning System · false activationHF 2 INDICATING "FAIL". GROUNDED - YES. RECYCLED POWER. ACCOMPLISHED OP CHECK PER AMM TASK 23-11-00-710-801. NO FAULTS NOTED. NO HISTORY LAST 60 DAYS.SDR ASAA2018081375721Actuator · leakingDURING BLOCK IN, NOTICED FUEL DRIPPING FROM THE BOTTOM OF THE NR 2 ENGINE COWLING. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE LT VSV ACTUATOR IAW AMM 75-31-01-000-801-F00, AND AMM 75-31-01-400-801-F00. PERFORMED VSV ACTUATOR TEST IAW AMM 75-31-01-7SDR ASAA2018073025561Blade · damagedWHILE ACCOMPLISHING T/C 78472002 ENG NR 2 S/N 894523 FOUND NR 4 FAN BLADE C/C SIDE CU-NI-IN COATING CHIPPED & MISSING MEASURED AT 1.2. FOUND PLATFORM ELASTOMER SEALS TORN & UNBONDED TOTALING 45 INCHES. FOUND 10 SPACERS WITH DISBONDED ELASTOMER STRIPS. GROUNDEDSDR ASAA2018062625205Indicator · malfunctionedUNDER WING REFUEL PNL NR 2 TANK IND INOP. REPORTED BY REFUELER. GROUNDED - YES. CYCLED 3 CBS. INDICATOR ON NR 2 TANK RETURNED TO NML. NO HISTORY. PERFORMED OPS TEST STEP G OF AMM 28-41-61.SDR ASAA2018062225165Coupler · failedNR 1 HF RADIO RECEIVES BUT WILL NOT TRANSMIT FROM CAPTAINS OR FO'S AUDIO PANELS. GROUNDED - YES. REMOVED & REPLACED NR 1 HF COUPLER IAW AMM 23-11-61. GROUND VERIFICATION SUCCESSFUL REF AMM 23-11-61.SDR ASAA2018061985112Switch · inoperativeN1 PUSHBUTTON SWITCH ON THE MODE CONTROL PANEL WAS INOPERATIVE. ACFT GROUNDED. REMOVED, REPLACED AND TESTED DFCS MODE CONTROL PANEL IAW AMM 22-11-34. MCP INSTALLATION TEST PASSED. PERFORMED LRU REPLACEMENT TEST FOR MCP IAW AMM 22-11-34/501 AND LAND VERIFY SDR ASAA2018061125047Sensor · false activationNR 2 WINDOW OVERHEAT LIGHT ILLUMINATED DURING APPROACH. ACFT GROUNDED. TROUBLESHOT IAW FIM 30-41, TASK 811. CURRENTLY FAULT LIGHT WAS NOT ON. PERFORMED A WINDOW HEAT CONTROL UNIT BITE IAW FIM 30-41 TASK 801, TEST PASSED. PREVIOUS LEG FAULTED WINDOW SENSOR. SDR ASAA2018052324749Cover · leakingNR 1 ENGINE HAS REPORTS OF OIL DRIPPING THE AFT FLAME ARRESTOR AFTER SHUTDOWN. GROUNDED - YES. REMOVED AND REPLACED OIL INLET COVER AT NR 1 ENGINE, ALSO ACCOMPLISHED INSPECTION OF REAR VENT TUBE TEETH FOR WEAR REF AMM 72-56-00-400-801 LEAK CHECK. LUBE UNIT WASSDR ASAA2018052224769Blade · damagedREF T/C 78472002 NR 1 ENG, DURING ACCOMP STEP 34 FOUND CU-NI-IN COATING OUT OF LIMITS ON BLADES 2 & 6 CONVEX SIDE AND BLADES 13,14,20,& 22 ON THE CONCAVE SIDE. GROUNDED - YES. BLADES 2,6,13,14,20, & 22 REMOVED AND REPLACED REF T/C 78472002 CFM 56-7 FAN BLADE LSDR ASAA2018052024710Eec · failedWHILE PERFORMING TASK CARD 78273000, FOUND A NR 1 ENGINE FAULT 73-11271, THE ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE. SHORT TIME FAULT 50-HR DEFERRAL. ACFT GROUNDED. FOUND EEC ALTERNATOR STATOR PINS SHORTED TO CASE. REMOVED EEC ALTERNATOR STATOSDR ASAA2018051744624Eec · faultedDURING INTERROGATION OF FMC, CDU ENGINE FAULTS. FOUND CODE 73-21271 ON THE NR 1 ENGINE, ALTERNATOR VOLTAGE INPUT TO THE EEC IS OUT OF RANGE, LEG 0. SHORT TIME. ACFT GROUNDED. PERFORMED A RESISTANCE CHECK ON THE NR 1 ENGINE EEC ALTERNATOR AND J7 HARNESS FOR FSDR ASAA2018042024324Warning Light · false activationLEFT PACK LIGHT COMES ON DURING RECALL. ACFT GROUNDED. THE LT PACK PRIMARY TEMP CONTROL INOPERATIVE. PERFORMED A BITE TEST IAW AMM 21-61-00. OPS TESTED NORMAL, NO FAULTS.SDR ASAA2018041424284Fault Code · false activationWHILE ACCOMPLISHING T/C 78273000, FOUND LONG TIME FAULT. CODE/MSG NUMBER: 73-21072 - THE FUEL FILTER SIGNALS DISAGREE ON NR 2 ENGINE. ACFT GROUNDED. ACCOMPLISHED FIM 73-05 TASK 801 FOR FAULT 73-21072 AND PERFORMED EEC TEST FOR THE NR 2 ENGINE IAW FIM 73-00 TSDR ASAA2018040624162Warning Light · false activationAPU FAILED CSS AT FL 360. FAULT LIGHT ON START ATTEMPT. ACFT GROUNDED. PERFORMED FIM 49-30/803. NO FAULTS FOUND. OK FOR SERVICE.SDR ASAA2018040324121Coupler · failedNR 2 HF RADIO WILL NOT TEST. UNABLE TO GET TONE WHEN TUNING A NEW FREQ. UNABLE TO GET A TONE OR TIME HACK ON FREQ 5000 OR 10.000. ACFT GROUNDED. REMOVED AND REPLACED NR 2 HF ANTENNA COUPLER IAW AMM 23-11-61-401, INSTALLATION TESTED GOOD. RESET 2.SDR ASAA2018032724059Coupler · failedNR 2 HF MAKES RANDOM KEYING SOUND DURING FLIGHT. CANNOT TRANSMIT ON THR NR 2 HF. RANDOM KEYING SOUND ONLY WHILE IN DATA MODE. ACFT GROUNDED. CONFIRMED THE NR 2 HF FAULT. REMOVED AND REPLACED HF ANTENNA COUPLER IAW AMM 23-11-61. PERFORMED AN HF SYSTEM TESDR ASAA2018031723932Hf Comm · unknownHF RADIO INOPERATIVE. ACFT GROUNDED. NR 2 HF GROUND VERIFICATION TESTED SUCCESSFUL IAW AMM 23-11-00-710-801.SDR ASAA2018031323865Warning System · false activationAFTER PUSH IN, L SIDE WINDOW OVERHEAT ILLUMINATED. GROUNDED - YES. RAN QRH CHECKLIST, LIGHT EXTINGUISHED.SDR ASAA2018030223746Adapter · leakingNR 1 ENGINE OIL CONSUMPTION TRENDING HIGHER THAN EXPECTED, FAILS TEST 3B OIL LEAK PRESENT AT STARTER QAD ADAPTER 6 O'CLOCK POSITION. ACFT GROUNDED. REMOVED LEAKING STARTER DRIVE PAD. REINSTALLED DRIVE PAD WITH NEW O-RINGS IAW CFM SHOP MANUAL 72-63-00-430-3. SDR ASAA2018013123352Wire Harness · brokenNR 1 ENGINE OVERHEAT DETECTOR LOOP B, NOT TESTING CORRECTLY. FAULT LIGHT ILLUMINATED. ACFT GROUNDED. FOUND BROKEN TERMINATION AND CHAFING ON UPPER LEFT DETECTOR NR 2 WIRING. REPLACED THE NR 1 ENGINE FAN HARNESS, UPPER & LOWER FAN FIRE DETECTORS, AND ORE SDR ASAA2018012823320Filter · dirtyCONTROL CABIN ZONE TEMP ILLUMINATED WITH MASTER CAUTION RECALL AND DOES RESET. ACFT GROUNDED. PERFORMED A PACK TEMPERATURE CONTROL BITE PROCEDURE IAW FIM 21-62, TASK 801. RIGHT PACK/ZONE TEMPERATURE CONTROLLER LOGGED A FLT DECK TRIM VALVE FAULT FOR BITE ANDSDR ASAA2018012623301Warning Light · false activationSPEED TRIM FAIL LIGHT ILLUMINATED BRIEFLY DURING DESCENT, THEN EXTINGUISHED. ACFT GROUNDED. ACCOMPLISHED DFCS BITE LIBRARY TEST 32, ALL SURFACE TESTS PASSED.SDR ASAA2018012523290Fire Detector · no testDURING A FIRE WARNING TEST, THE NR 1 ENGINE B LOOP WAS FOUND INOPERATIVE. ACFT GROUNDED. UNABLE TO DUPLICATE THE DEFECT, NR 1 ENGINE FIRE DETECTION TEST PASSED WITH LOOP SELECTOR ON NORMAL, VISUALLY INSPECTED ALL LOOP TERMINALS FOR SECURITY AND TERMINATIONSDR ASAA2018012323266Fire Loop · malfunctionedNR 1 ENGINE FIRE LOOP DOES NOT TEST FOR B. ACFT GROUNDED. MOVED LOOP SELECTOR SWITCH TO NORMAL. NR 1 ENG FIRE DETECTION OPS TEST NORMAL IAW AMM 26-11-00. ACCOMPLISHED ENGINE FIRE DETECTION LOOP RESISTANCE CHECK IAW AMM 26-11-00, TOTAL RESISTANCE VALUES ARSDR ASAA2018012223267Fire Detector · faultedDURING PREFLIGHT FIRE TEST NR 2 ENGINE FIRE HANDLE LIGHT DID NOT ILLUMINATE. ACFT GROUNDED. PERFORMED FIM 26-10 TASK 801. FOUND THE NR 2 ENG LOOP A CORE RIGHT DETECTOR FAULTED. REMOVED AND REPLACED THE CORE RIGHT LOOP A FIRE DETECT ELEMENT IAW AMM 26-11-00.SDR ASAA2018011623196Sensor · failedRIGHT FWD WINDOW HEAT OVERHEAT LIGHT ILLUMINATES WHEN IN ON POSITION. QRH PROCEDURES RUN. OVERHEAT LIGHT WILL NOT EXTINGUISH. GROUNDED - YES. ACCOMPLISHED RT FWD WINDOW HEAT CONTROLLER BITE IAW B737-800 FIM 30-41 TASK 801. TEST SHOWS RT FWD WINDOW HEAT SENSOR SDR ASAA2017121622920Control Module · failedPRESSURIZATION PANEL "AUTO FAIL" LIGHT AND "ALTN" LIGHT IS ILLUMINATED. GROUNDED - YES. AFTER MOVING MODE SWITCH TO "MANUAL" THEN BACK TO "AUTO", "ALTN" AND "AUTO FAIL" LIGHTS EXTINGUISHED. BUT FOUND LCD DISPLAYS STAYED FULL BRIGHT WITH "LIGHTS" SWITCH IN BRIGSDR ASAA2017112622750Bleed Valve · failedSHORTLY AFTER T/O IN CLB POWER LEFT DUCT PRESSURE FLUCTUATING BETWEEN 30-35, RT 50 PSI. AS WE CONTINUED TO CLIMB LEFT SIDE FLUCTUATED LESS AND LESS UNTIL CRUISE RT DID NO FLUCTUATE AT ALL BUT STILL HAD A SPLIT LEFT 38 PSI, RT 45 PSI. GROUNDED - YES. DUCT SPLITSDR ASAA2017112622704Fmc · malfunctionedLEFT FMC INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED AN OPS CHECK IAW AMM 34-61-00. OPS NORMAL. FMC SWITCH MOVED BACK TO NORMAL.SDR ASAA2017112022655Indicator · failedNR 2 TANK REFUEL INDICATOR LOWER HALF OF INDICATOR SHOWS TEST PATTERN. QUANTITY SHOWS SAME KNOWN QUANTITY. ACFT GROUNDED. REMOVED AND REPLACED IAW AMM 28-41-61-000-801 AND 28-41-61-400-801. OPS CHECKED NORMAL.SDR ASAA2017110522430Lens · detachedOVERHEAD PLASTIC EXIT SIGN ABOVE EXIT ROW 15 OFF. GROUNDED - YES. REINSTALLED LENS.SDR ASAA2017102522314Packing · leakingDURING FUEL NOZZLE IDLE LEAK CHECK, FOUND THE NR 2 ENGINE FUEL SERVO LEAKING. ACFT GROUNDED. REPLACED THE PACKING IAW CMM 73-11-77 P701-703. ACCOMPLISHED IDLE LEAK CHECK PER TEST 3A IAW AMM 71-00-00-700.SDR ASAA2017102522313Wire Harness · damagedFOUND THE NR 2 ENGINE FIRE DETECTION HARNESS TERMINAL DAMAGED. ACFT GROUNDED. REPAIRED THE DETECTOR HARNESS TERMINAL IAW AMM 26-11-02-960-802. FIRE DETECTION OPS TESTED IAW AMM 26-11-02-960-802.SDR ASAA2017102422308Panel · looseWHILE ACCOMPLISHING A NR 2 ENGINE INLET INSPECTION, FOUND THE NR 1 FAN DUCT PANEL LOOSE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE, NR 1 FAN DUCT PANEL IAW AMM 72-23-07-400-801-F00.SDR ASAA2017102422307Link · wornWHILE ACCOMPLISHING A NR 2 ENGINE INLET INSPECTION, FOUND A LINK WORN ABOVE HIGH STAGE VALVE. ACFT GROUNDED. REMOVED AND REPLACED THE WORN LINK ABOVE HIGH STAGE VALVE IAW AMM 36-11-01-400-802, AND 71-00-02.SDR ASAA2017101822258Fault Message · false activationWHILE ACCOMPLISHING T/C 78273000, FOUND THE NR 2 ENGINE FAULT 73-21372. FAULT MESSAGE UPPER EGT SECTORS READING HIGH. ECONOMIC FAULT. ACFT GROUNDED. PERFORMED BITE ON THE NR 2 ENGINE. NO FAULTS UNDER RECENT OR FAULT HISTORY.SDR ASAA2017092622061Lens · detachedEXIT SIGN LENS AT THE R2 DOOR DETACHED. ACFT GROUNDED . REPLACED THE LENS IAW AMM 33-51-14.
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