N533AS
Service difficulty reports · 389
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 = 'N533AS' 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 = 'N533AS' 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 ASAA2021052634931Transmitter · malfunctioned#1 HF WILL NOT TRANSMIT OR RECEIVE & HAS NO SIDE TONE. GROUNDED - YES. ACCOMPLISHED HF BITE IAW B737-800 FIM 23-11 TASK 801. SYSTEM RESET AND OPS CHECK NORMAL. AIRCRAFT OK FOR SERVICE.SDR ASAA2021052334923Actuator · faultyWHILE ACCOMPLISHING T/C 78273000 FOUND SHORT TIME FAULT MSG NBR: 75-20401 THE VSV POSITION SIGNALS DISAGREE DURING FLIGHT LEG 1. DEFERRED PER T/C 78273000. GROUNDED - YES. #1 ENG SHOWS LEG 4 AND 9 FAULTING 75-20401. RH AND LH VSV RANG OUT: LH IS SIGNIFICANTLY SDR ASAA2021051634828Trans Rectifier · failedTR & ELEC LT ILLUM ON P5-13 WHILE TOWING A/C ON APU PWR. GROUNDED - YES. BITE CK OF ELEC LT SHOWS BAT CHARGER INOP 1, FAULT CLEARS & RETEST SHOWED NO FAULTS. ACCOMP MAIN BATT CHARGER OPS TEST REF B737-800 AMM 24-31-21-710-801 OPS CK OK. PRECAUTIONARY OPS CK OFSDR ASAA2021050334742Fmc · malfunctionedFMC DISAGREE GROUNDED - YES. RAN QRC - FMC DISAGREE WENT OUT.SDR ASAA2021043034729Spinner · wornREF T/C 78472000 #2 ENG FRONT SPINNER CONE ANODIZED COATING AND WHITE ANTI-EROSION PAINT WORN TO LIMITS. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FRONT SPINNER CONE REF B737-800 AMM 72-21-01.SDR ASAA2021043034722Sign · brokenAFT R/H OVER WING EXIT, SIDEWALL LOCATING EXIT SIGN IS BROKEN. GROUNDED - YES. REMOVED AND REPLACED EXIT SIGN ASSY. OPS CHECK GOOD IAW B737-800 AMM 33-51-01.SDR ASAA2021042534694Fault Code · false activationFOUND FAULT CODE 75-10401 (VSV POSTION SIGNALS DISAGREE) SHORT TIME FAULT DEFERRED PER T/C 78273000 #1 ENG. GROUNDED - YES. PER B737-800 FIM 75-31 TASK 804 INITIAL EVALUATION: PERFORMED #1 ENG EEC TEST. TEST PASSED NO FAULTS. PERFORMED ACTUATORS TEST. NO FAULTSDR ASAA2021042234636Connector · brokenDURING FUEL PUMP INSTALL FOUND CONNECTOR DP1207 BROKEN ON HMU #1 ENG. GROUNDED - YES. ON THE #1 ENG, REMOVED AND REPLACED MW0312 HARNESS REF B737-800 AMM 71-51-03/401. ALL OPS TEST PASS. ETOPS GROUND VERIFICATION SUCCESSFUL.SDR ASAA2021041434582Selector Knob · out of toleranceHEADING SELECT KNOB AND HEADING BUG ARE INTERMITTENTLY OUT OF SYNC WHEN ATTEMPTING TO SELECT A HEADING. GROUNDED - YES. VERIFIED SELECTED HDG WILL INTERMITTENTLY PAUSE & THEN JUMP A COUPLE DEGREES AS HDG IS ADJUSTED. SAME RESPONSE WITH EITHER FCC A OR B AS MASSDR ASAA2021041334609Pump · leakingWHILE ACCOMPLISHING T/C 78472022 FOUND FUEL LEAKING FROM FUEL PUMP PAD DRAIN ON #1 ENG. GROUNDED - YES. ACCOMPLISHED LEAK CHECK REF B737-800 AMM 71-7100-801-F00 FOUND LESS THAN 90 DPM. REMOVED AND REPLACED #1 ENG FUEL PUMP REF AMM 73-11-01-400-801-F00. COMPLETSDR ASAA2021041034567Actuator · leakingENG #2 FUEL LEAK GREATER THAN 90 DROPS PER MIN FROM RH VSV DRAIN. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE RIGHT HAND VSV REF B737-800 AMM 75-31-01-400-802 OPS CHECK AND LEAK GOOD REF AMM 75-31-01-790-801.SDR ASAA2021040934550Heat Exchanger · leakingON WALK ALROUND FOUND FUEL LEAK UNDER #2 ENGINE. GROUNDED - YES. FOUND FUEL LEAKING AT #2 ENGINE MAIN OIL/FUEL HEAT EXCHANGER PAD DRAIN AT 27 DROPS PER MIN IAW B737-800 AMM 71-71-00-200-801. REMOVED AND REPLACED MAIN OIL/FUEL HEAT EXCHANGER, LEAK CHECK GOOD. RSDR ASAA2021033034476Warning Light · false activationL 'PACK' ILLUMINATED ON RECALL. GROUNDED - YES. BITE OF NR 1 CONTROLLER SHOWS TCV FAULT. TEST OF CONTROLLER REF B737-800 AMM 21-61-20-400-801 PASS FAULT CLEARS AND OPS NORMAL.SDR ASAA2021031634340Actuator · faultedWHILE ACCOMPLISHING T/C 78273000 FOUND MAINTENANCE MESSAGE 75-30401 THE VSV POSITION SIGNALS DISAGREE. SHORT TIME FAULT DEFFERED PER T/C 78273000. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE RIGHT VSV ACTUATOR PER B737-800 AMM 75-31-01 OPERATIONAL LEAK CHECSDR ASAA2021031434293Actuator · leakingFUEL RUNNING FROM RH VSV ACTUATOR DRAIN LINE ON #1 ENG WHILE ACTUATING THE VSV MANUALLY REF B737-800 AMM 75-31-00-790-801. GROUNDED - YES. REMOVED AND REPLACED #1 ENG R/H VSV ACTUATOR REF B737-800 AMM 75-31-01-000-802-F00 AND AMM 75-31-01-400-802-F00 AND AMM 7SDR ASAA2021020534054Sensor · faultedLEFT FWD WINDOW (CAPT #1) OVERHEAT LIGHT ILLUMINATED AND WILL NOT EXTINGUISH. GROUNDED - YES. PRIMARY AND SPARE SENSORS READ OPEN FROM WINDOW HEAT CONTROLLER CONNECTOR. REMOVED AND REPLACED L1 WINDOW REF B737-800 AMM TASK 56-11-11-000-801 AND TASK 56-11-11-400SDR ASAA2021020434011Sensor · faultyAPU FAILED START DURING 2 ATTEMPTS AT FL400 AND 1 ATTEMPT AT FL340. APU FAULT LIGHT ILLUMINATED ON ALL 3 ATTEMPTS. GROUNDED - YES. R & R INLET TEMP SENSOR PER B737-800 FIM 49-30 TASK 803. NO DEFECTS NOTED NO FAULTS CODES. CLEARS MEL 49-1B C/N 05021533 MELSDR ASAA2021013033980Heater · malfunctionedLEFT FORWARD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED B737-800 FIM 30-41 TASK 801, FOUND SENSOR FAULT. NO HELP ON RESET, SWITCHED TO ALT SENSOR, NO HELP. GVI OF L1 WINDOW SENSORS FOUND SOME CRACKING IN BETWEEN BOTH SENSORS . FOLLOWED FSDR ASAA2021012233931Flow Divider · faultyFAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL400. SUCCESSFUL CSS ACCOMPLISHED AFTER FAULT LIGHT EXTINGUISHED. GROUNDED-YES. REMOVED AND REPLACED APU FUEL FLOW DIVIDER, REF B737-800 AMM 49-31-15. GROUND VERIFICATION SUCCESSFUL. NO LEAKS NOTED.SDR ASAA2021012133936Fault Light · false activationFAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL410. SUCCESSFUL CSS ACCOMPLISHED AT FL330 AFTER FAULT LIGHT EXTINGUISHED. APU STARTED OK ON GROUND ALSO. GROUNDED-YES. ACCOMPLISHED APU BITE, IAW B737-800 FIM 49 33 TASK 803 FAULT CODES 49-31295 AND 49-SDR ASAA2021011933913Warning Light · false activationZONE TEMP LIGHT FOR CONT CAB ILLUMINATES ON RECALL. EXTINGUISHES ON RESET. GROUNDED-YES. ACCOMPLISHED B737-800 AMM 21-61-00 ZONE TEMP CONTROL AND INDICATION ADJUSTMENT TEST, BIT SHOWS FLT DECK TRIM VALVE FAULT. ACCOMPLISHED FLT DECK TRIM VALVE FAULT ISOLATSDR ASAA2021011833901Exciter · inoperative2 ATTEMPTS AT STARTING APU RESULTED IN THE FAULT LIGHT ILLUMINATING BOTH TIMES. GROUNDED-YES. FOUND APU TO HAVE NO IGNITION. REPLACED IGNITION UNIT, IAW B737-800 AMM TASK 49-41-31-000-801 AND 49-41-31-400-801. REPLACED IGNITER PLUG LEAD, IAW AMM TASK 49-41SDR ASAA2021011033871Fault Code · activated#2 ENGINE LONG TIME FAULT. THE T3 SIGNAL IS OUT OF RANGE. MSG NBR: 75-20832. DEFERRED PER T/C 78273000. GROUNDED - YES. NO RECENT OR IN FLT FAULT HISTORY ON EEC BITE. INPUT MONITORING PAGE SHOWS HALF DEGREE DIFFERENCE BETWEEN CH A & CH B FOR T3 SENSOR. NO HISTSDR ASAA2020122633749Charger · inoperativeELEC LIGHT AFTER ENGINES START. GROUNDED-YES. PERFORMED B737-800 FIM 24-31 TASK 801 AND HAD BATTERY CHARGER 1 INOPERABLE, FAULT CLEARED. PERFORMED FIM 24-31 TASK 829. FAULT CLEARED AND PERFORMED FIM 24-31 TASK 801 WITH NO FAULTS.SDR ASAA2020122533767Blade · faultyWHILE ACCOMPLISHING T/C 78472010. NR 1 ENGINE, BLADE NR 1 FAILED BLADE ROOT ULTRASONIC INSPECTION, PER SBCFM56-7B-72-1033-1. REQUIRES BLADE AND BLADE PAIR CHANGE. GROUNDED-YES. REMOVED AND REPLACED THE FAN BLADES NR 1 AND NR 13 ON NR 1 ENGINE, REF T/C 7847SDR ASAA2020122533762Spacer · debondedWHILE ACCOMPLISHING T/C 78472010. NR 1 ENGINE, FOUND 10 FAN BLADE SPACERS WITH DISBONDING ELASTOMER MATERIAL. GROUNDED-YES. REMOVED AND REPLACED, ON NR 1 ENGINE, 10 EA FAN BLADE SPACERS, REF T/C 78472010.SDR ASAA2020122433748Coupler · inoperativeAFTER DEPARTURE HF-1 INOPERABLE. NO INCOMING AUDIO, NO TRANSMIIT OR SIDE TONE. GROUNDED-YES. VERIFIED DEFECT, NR 1 HF WILL NOT TUNE, NO SIDE TONE. REMOVED AND REPLACED NR 1 HF COUPLER, REF B737-800 AMM 23-11-61. GROUND VERIFICATION TEST PASSED.SDR ASAA2020111033541Blade · wornPER T/C 78472010 NR 2 ENGINE FAN LUBE NR 7 AND NR 12 BLADES CU-NI-IN COATING MISSING BEYOND LIMITS. GROUNDED-YES. NR 2 ENGINE S/N 804633 REPLACED 2 SETS OF FAN BLADE PAIRS, IN REF TO B737-800 AMM 72-21-02-000-802-F00 AND T/C 78472010.SDR ASAA2020111033540Blade · wornPER T/C 78472010 NR 2 FAN BLADE LUBE NR 13 FAN BLADE CU-NI-IN COATING MISSING BEYOND LIMITS. GROUNDED-YES. NR 2 ENGINE S/N 804633 REPLACED THE FAN BLADE PAIR, IN REF TO B737-800 AMM 72-21-02-000-802-F00 AND T/C 78472010.SDR ASAA2020111033539Spacer · debondedPER T/C 78472010 NR 2 FAN LUBE SPACERS NR 3, 7, 8, 10, 13, AND 15 ELASTOMERS ARE DISBONDED. GROUNDED-YES. NR 2 ENGINE S/N 804633 REPLACED FAN BLADE SPACERS NR'S 3, 7, 8, 10, 13, AND 15, REF T/C 78472010.SDR ASAA2020111033532Actuator · faultyRT PACK INLET DOOR ACTUATOR CONTINUOUSLY RUNNING. GROUNDED-YES. REMOVED AND REPLACED RT RAM AIR DOOR INLET ACTUATOR, REF AMM 21-51-21/401. THREE C/B'S OPENED, TAGGED, AND RESET. OPERATIONS TEST PASS. ETOPS GROUND VERIFICATION SUCCESSFUL. SEAMC SCOTT NOTSDR ASAA2020110933523Fmc · malfunctionedON TAXI VTK SHOWS CAPT SIDE. LT FMC NOT RESPONDING. GROUNDED-YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 836. RESET FMC'S WITH C/B CYCLE. FMC'S OPERATIONS NORMAL.SDR ASAA2020090833141Hf Comm · failedHF NR 1 INDICATES FAILURE ON FREQUENCY CONTROL PANEL. GROUNDED - YES. UPON A/C POWER UP, FOUND RTP'S NO LONGER SHOWS A HF NR 1 FAILURE. PERFORMED B737-800 FIM 23-11 TASK 801 HF BITE, RTP FIM 23-13 TASK 815 AND B737-800 AMM 23-12-41-800-802, ALL GOOD. GROUNSDR ASAA2020090331131Shimmy Dampener · leakingHYDRAULIC A QUANTITY WENT TO ZERO. GROUNDED - YES. FOUND MANIFOLD ON LEFT MLG SHIMMY DAMPER DETACHED WITH ALL 3 MOUNTING BOLTS SHEARED OFF AND LEAKING HYDRAULIC FLUID. REMOVED MANIFOLD AND CAPPED HYD LINE. REMOVED LT MLG SHIMMY DAMPER, REF B737-800 AMM 32-SDR ASAA2020083193109Warning Light · false activation"ELEC" ANNUNCIATOR LIGHT IS ILLUMINATED ON P5-13 ELECTRIC METER PANEL. GROUNDED - YES. PERFORMED P5-13 ELEC LIGHT MESSAGE BIT, PER B737-800 FIM 24-631 TASK 801. FOUND FAULT MSG "BAT CHGR INOP 1" WOULD NOT RESET. VERIFIED C/B'S J9 A4 IS CLOSED AND P92 E1 ISSDR ASAA2020082533076Connector · disconnectedDURING TAXI AFTER LANDING, FUEL FILTER BYPASS LIGHT ILLUMINATED ON NR 1 SIDE. NR 1 ENGINE OPERATING NORMALLY. GROUNDED - YES. PERFORMED B737-800 FIM 73-05 TASK 801 FAULT ISOLATION PROCEDURE, FOUND ELECTRICAL CONNECTOR FOR FUEL FILTER DIFFERENTIAL PRESS SWITSDR ASAA2020081873034Warning Message · false activationDURING CRUISE WHILE TRANSFERRING FUEL, NOTICED THE NR 1 AFT LOW PRESS LIGHT FAILED TO ILLUM WHEN NR 1 FUEL PUMP SWITCH (AFT) WAS PLACED TO OFF POSITION. ALL OTHER PUMP LOW PRESS LIGHTS ILLUM NORMALLY. FUEL FLOW FOR BOTH ENGINES MATCHED AND ONCE BALANCED FUELSDR ASAA2020070832878Switch · out of rigAPU WILL NOT CRANK. GROUNDED - YES. REMOVED AND REPLACED BOTH AIRCRAFT BATTERIES REF AMM 24-31-11. APU STILL WILL NOT START ON JUST BATTERY POWER. APU STARTS ONLY ON GROUND POWER. AFTER FAILED BATTERY START APU BITE SHOWS MSG 49-15004 (INLET DOOR SHUTDOWN)SDR ASAA2020070632868Unknown · malfunctionedAPU FAILED START AT FL400, FL400, FL300 AND FAILED START ON THE GROUND. GROUNDED - YES. DURING INIT EVALUATION "APU FAULT" LIGHT CAME ON WHEN TRYING TO START, 3 TIMES. APU BITE TEST SHOWED "49-15004 INLET DOOR SHUTDOWN." ACCOMPLISHED FIM TASK 49-10 TASK 80SDR ASAA2020062232824Battery · failedLEFT OVERWING EMERGENCY EXIT LIGHTS FAIL BATTERY TEST. GROUNDED - YES. EMERGENCY BATTERIES REMOVED/REPLACED AND TESTED (M2335 & M1670) S/N 82039 IAW AMM 33-51-06.SDR ASAA2020061972811Battery Pack · no testRIGHT OVERWING EMERGENCY EXIT LIGHTS FAIL BATTERY TEST. GROUNDED - YES. REMOVED & REPLACED EMERGENCY LIGHT BATTERIES M1671 & M1676. OPS CHECK GOOD.B737-800 AMM 33-51-06.SDR ASAA2020061972810Battery Pack · no testR2 DOOR INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS FAILS BATTERY TEST. GROUNDED - YES. EMERGENCY BATTERIES REMOVED/REPLACED AND TESTED (M1672) IAW B737 AMM 33-51-06.SDR ASAA2020062963844Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN SHOWING CRACK INDICATIONS BETWEEN STAB STA 175.50 & 184.70, RUNNING PARALLEL WITH STAB STA 184.70. GROUNDED - YES. REPAIRED THE DAMAGED AREA ON THE HORIZONTAL STAB IAW SRM 55-10-01-2R-11. PERMANT CATEGORY "B" REPAIR SDR ASAA2020062953843Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN SHOWING CRACK INDICATIONS BETWEEN FWD AND AFT, BETWEEN STAB STA 120.30 AND 129.50. GROUNDED - YES. REPAIRED THE DAMAGED AREA ON THE LT HORIZONTAL STAB IAW SRM 55-10-01-2R-11, PERMANENT CATEGORY B REPAIR INSPECTION THRESHSDR ASAA2020032732565Connector · loose#1 ENG ESN 804627 HMU CHANNEL B CANNON PLUG LOOSE BACKSHELL. GROUNDED - YES. REMOVED & REPLACED J6 HARNESS. OPS CK GOOD. REF B737-800 IPC 73-21-06-1A & B737-800 AMM 73-21-06.SDR ASAA2020032732564Connector · loose#1 ENG HMU SOL PLUG BACKSHELL LOOSE. GROUNDED - YES. REMOVED & REPLACED MW0312 HARNESS. OPS CK GOOD. REF B737-800 IPC 71-51-03-01A & B737-800 AMM 71-51-03.SDR ASAA2020022652272Hf Comm · malfunctionedHF #1 INOP. GROUNDED - YES. CYCLED AIRCRAFT POWER, PERFORMED OPERATIONAL CHECK OF HF #1 RADIO TRANSMISSION PER B737-800 AMM 23-11-00, PERFORMED BITE TEST PER B737-800 FIM 23-11 TASK 801, ALL OPS CHECK NORMAL, GROUND VERIFICATION SUCCESSFULL.SDR ASAA2020021063134Ignition Sys · unknown#1 ENGINE WILL NOT START WITH IGN R SELECTED. GROUNDED - YES. RELEASED PER MEL 74-1E. #1 ENGINE RIGHT IGNITION SYSTEM IS INOP. OPENED #1 ENG INBD T/R, AND ACCOMPLISHED GVI ON R/H IGNITER LEADS AND EXCITER FOR LOOSE ITEMS, NO DEFECTS NOTED. OPS CHECK R IGN PER SDR ASAA2020012841991Wire Harness · chafedDURING TC N8420001 #2 ENGINE HARNESS GVI, FOUND J10 CHAFING JUST AFT OF DP1005. GROUNDED - YES. REPAIRED J10 HARNESS REF B737-800 AMM TASK 70-70-01-350-801-F00, GOOD UNTIL ENGINE REMOVAL.SDR ASAA2020010331744Control Panel · faultyAUTOPILOT B DISCONNECTED TWICE IN CRUISE DURING SMOOTH FLYING CONDITIONS. BOTH TIMES IT WAS REENGAGED WITH NO ISSUE. GROUNDED - YES. DFCS FAULT REVIEW SHOWS NUMEROUS FAULT MSG# 22-11607 "MCP DATA INV" & HGS FAULT REVIEW SHOWS "RALT 2" FAULT MESSAGE ON FLT 1,3,
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