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 ASAA2013072495671Anti-Ice Valve · inoperativeRIGHT ENGINE ANTI-ICE VALVE NOT RESPONDING TO SWITCH POSITION. ACFT GROUNDED. RAN ENGINE CYCLED ANTI-ICE VALVE OPERATES NORMALLY GROUND VERIFICATION CHECK OK REF 30-21-00-710-801.SDR ASAA2013072295655Unknown · unknownON ARRIVAL, THE F/O FD BARS DISAPPEARED AS THE ILS WAS CAPTURED. THE CAPTAIN`S FD BARS WERE NORMAL. THE F/O FMA SHOWED LOC AND GS CAPTURE HOWEVER THE BARS DISAPPEARED. ACFT GROUNDED. PERFORMED DFCS BITE TEST REF FIM 22-11, TASK 801. NO FAULTS FOUND. CURRSDR ASAA2013071095546Fmc · false indicationFMC DISAGREE ON TAXI. ACFT GROUNDED. ACCOMPLISHED QRC PROCEDURE, OPS RESTORED.SDR ASAA2013062395264Unknown · unknown300 AGL, ACFT DRIFTED TO LT EDGE OF RUNWAY. DID NOT CORRECT. CRITICAL AREA WAS CLEAR. ACFT GROUNDED. CAPTAIN MANUALLY DISCONNECTED AUTOPILOT. DID NOT SPECIFY HOW FAR ACFT DRIFTED. NO HISTORY 30 DAYS. PERFORMED FAULT REVIEW, NO FAULTS. PERFORMED LAND VESDR ASAA2013061695118Unknown · unknownSATCOM PROMPT IS MISSING FROM CDU MENU PAGE. ACFT GROUNDED. COULD NOT DUPLICATE. SATCOM PROMPT PRESENT AND SYS OP CHECKS NORMAL REF AMM 23-15-00-730-801.SDR ASAA2013060895040Circuit Breaker · openCREW REPORTS LT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. FOUND LT SIDE WINDOW CIRCUIT BREAKER OPEN, PERFORMED CIRCUIT BREAKER RESET IAW AMM 20-60-01, NO FAULTS NOTED IAW SAME REFERENCE. PERFORMED WINDOW HEAT SYS OPS CHECK IAW AMM 30-41-00, GROUNSDR ASAA2013060494991Lens · brokenEMERGENCY LIGHT EXIT SIGN ON NR 1 GALLEY ADJACENT TO R1 DOOR HAS BROKEN LENS. ACFT GROUNDED. R & R LENS AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.SDR ASAA2013052194865Unknown · unknownON APPROACH, THE AUTOTHROTTLES DISENGAGED ON THEIR OWN AND WOULD NOT RE-ENGAGE. ACFT GROUNDED. COULD NOT DUPLICATE.SDR ASAA2013051894837Warning Light · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. RAN QRH PROCEDURE NORMAL OPERATIONS RESTORED.SDR ASAA2013051794842Connector · dirtyWHILE INTERROGATING NR 2 ENG CDU FAULTS , FOUND FAULT 77-20862. BOTTOM LT EGT SIGNAL IS OUT OF RANGE. ACFT GROUNDED. R & R LOWER LEFT EGT PROBE IAW MM 77-21-01-000-801-F00, & MM 77-21-01-400-801-F00. PERFORMED EEC TEST IAW MM 73-21-00-700-804-F00, FAULT CSDR ASAA2013030194060Scavenge Pump · making metalON INSPECTION ON FWD OIL SUMP SCAVENGE SCREEN FOR NR 2 ENGINE, FOUND SILVER FLAKING ON CHIP DETECTOR. ACFT GROUNDED. SILVER FLAKING FOUND NOT TO BE ASSOCIATED WITH MAGNETIC BEARING MATERIAL. ACFT IS OK FOR ENGINE OPERATION BUT CHIP DETECTOR INSPECTION INTERSDR ASAA2013011193663Warning Light · false activationFMC DISAGREE LIGHT ON GROUND. ACCOMPLISHED QRH PROCEDURE. NORMAL OPS.SDR ASAA2012122293519Lens · missingF/A REPORTS, ON TAKEOFF, METAL PLATE ON L1 DOOR WHICH COVERS EMERGENCY EXIT LIGHTING, FELL OFF & GLASS LENS BROKEN. NOTE PART ON FED PEDESTAL ON FLT DECK. R & R L1 ENTRY DOOR LIGHT ASSY IAW AMM 33-29-00.SDR ASAA2012120493412Sensor · malfunctionedAPU CTSATP TREND DATA SHOWS MES EGT IS AT OR NEAR THE ESTABLISHED THRESHOLD. INDICATION ERRORS ARE SUSPECT. R & R APU INLET TEMP (T2) SENSOR IAW AMM 49-61-31. REMOVED CLEANED AND RE-INSTALLED APU INLET PRESSURE (P2) SENSOR IAW AMM 49-52-31. PERFORMED APU OPSDR ASAA2012102793189Control Panel · defectiveLIGHT IN APP BUTTON BURNED OUT. CONFIRMED APP SWITCH (REAR SOCKET) DEFECTIVE. R & R DFCS MCP REF AMM TASK 22-11-34. OPS CK NORMAL REF AMM 22-11-34/501 GP32 DFCS LRU INTERFACE TEST, AMM 22-11-00/201 GP49 LAND VERIFY TEST, AND SMM 34-36-00 HGS TEST.SDR ASAA2012091892908Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. FOLLOWED QRH, OPS NORMAL.SDR ASAA2012081992756Wire Harness · brokenNR 1 ENGINE FIRE LOOP B DOES NOT TEST. FOUND RT CORE LOOP TERMINAL BROKE. R & R NR 1 ENGINE CORE FIRE DETECTION HARNESS GROUND VERIFICATION SUCCESSFUL.SDR ASAA12511677Eec · failedAUTOTHROTTLES WOULD NOT ARM FOR TAKEOFF. ACFT GROUNDED. OPS TEST FAILED DUE TO "NO EEC DATA" FAULT. HAD NR 1 ENG EEC WITH ACTIVE FAULT ON RECENT HISTORY PAGE SAYING CANNOT ACCESS CHANNEL "B". ALSO, LOGGED INTERNAL EEC FAULT CODE 73 10101. REPLACED NR 1 ENGSDR ASAA12511658Duct · splitDURING CLIMB FL 180 PRESSURIZATION LT DUCT PRESSURE 15 R 41 N1'S 97.5 PERCENT. IN CRUISE 88 PERCENT N1 FL 380' L 40, R 40. IN DESCENT 35 PERCENT N1 FL240, L21, R22. GROUNDED YES. ACCOMPLISHED T/C NG 36WC 00001 ON NR 1 ENGINE NO DEFECTS NOTED. REPLACED NR1 PSDR ASAA12511605Switch · failedNR 2 ENGINE FUEL FILTER BYPASS LIGHT CAME ON AFTER TAKEOFF. LIGHT REMAINED ON DURING CLIMB AND LEVEL OFF/ CRUSE AT 10 000. LIGHT EXTINGUISHED DURING DECENT AND REMAINED OFF THRU LANDING. ACFT GROUNDED. DIV TIME 15 MIN. NO 90 DAY HISTORY. ACCOMP TASK 73-00-SDR ASAA12511604Sensor · unknownDUCT PRESSURE SPLIT CONSISTENT 30 PSI WITH LEFT AT 16 PSI AND RIGHT AT 46 PSI. ACFT GROUNDED. ACCOMPLISHED T/C NG 36WC 00001. NO DEFECTS FOUND. R & R NR 1 (450 DEG.) THERMOSTAT AS A PRECAUTIONARY. REF AMM 36-11-05, LEAK CHECKED GOOD.SDR ASAA12511598Sensor · malfunctionedDURING CLIMB, DUCT PRESS SPLIT : L10 PSI R40 PSI. NORMAL DURING CRZ DUCT PRESS L42 PSI R 42PSI. NORMAL DURING DESC DUCT PRESS L21PSI R21 PSI GROUNDED YES. IAW FIM TASKS 36-10-00-810-807& 36-10-00-810-810. REPLACED PCV SENSOR IAW AMM 36-12-03-000-801 & 36-12-SDR ASAA12511538Controller · faultedDURING CRUISE FL 380 CABIN PRESSURE DIFFERENTIAL NEEDLE IN ORANGE CAUTION RANGE AT 8.55 PSI NO FAULT LIGHTS ON. ACFT GROUNDED. PERFORMED GROUND VERIFICATION TEST OF NR1 & NR2 DIGITAL CABIN PRESSURE CONTROLLERS BITE CHECK IAW FIM TASK 21-31-00-810-801. OPS CSDR ASAA12511529Control Valve · failedDURING CLIMB, DUCT SPLIT NOTED THROUGH FL 320 N1 RPM 101 NO WING OR ENGINE ANTI ICE ISOLATION VALVE AUTO LT AND RT PACKS. AUTO RIGHT DUCT INDICATING 42 PSI AND LEFT DUCT INDICATIONG 19 PSI. DURING CRUISE AT FL 360 N1 RPM 90.3 NO WING, NO ENGINE ANTI ICE ISOLSDR ASAA12511486Valve · failedFL 370, DUCT SPLIT LEFT 24 PSI RIGHT 44 PSI. PERFORMED NR 1 ENG BLEED AIR SYS HEALTH CHECK IAW MM 36-11-00. FOUND SEAL AND COUPLING AIR LEAK WHERE PRECOOLER UPSTREAM DUCT CONNECTS TO PRECOOLER. REPLACED SEAL. LEAK CHECKED GOOD IAW MM 36-12-01. DURING HEALTH SDR ASAA12511428Battery · failedACFT AUX BATTERY SHOWED +2 AMPS FOR ENTIRE 5 HR FLIGHT. VOLTS WERE NORMAL AT 27. NO OTHER ABNORMAL ELECTRICAL INDICATIONS NOTED. REPLACED NR 1 AND NR 2 BATTERY MAIN IAW AMM 24 31 11. OPS CHECKED GOOD. GROUND FUNCTIONAL CHECKED GOOD IAW AMM 24-31-11 NR 2 BATTSDR ASAA12511397Computer · malfunctionedMCP INOPERATIVE. ACFT GROUNDED. REBOOTED MCP REF. MM 22 11 34. MCP POWERED NORMALLY. TESTED REF MM 22-11-34 AND 22-11-00 BITE GRP. NR 32 AND NR 49. TESTS OK. TESTED HGS REF SMM 34-36-00. TESTED OK.SDR ASAA12511341Warning Message · false activationFMC DISAGREE. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.SDR ASAA12511340Transceiver · malfunctionedUNABLE TO READ RADIO ON HF1 CLEARLY, CHECK WAS GOOD HE COULD READ US LOUD AND CLEAR VERY SCRATCHY SWITCHED TO HF2 AND IT WAS CLEAR USED HF FOR DATA NR 1 ON (EEP) SOUNDED BETTER. UNABLE TO CONFORM. GROUND CHECK OPS NORMAL. AS PRECAUTION REPLACED NR 1 HF TRANSDR ASAA12511286Unknown · malfunctionedCONT CAB ZONE TEMP LIGHT ON MASTER CAUTION RECALL. MASTER CAUTION RESET EXTINGUISHES LIGHT. NR 2 CTRLR SHOWS FLT DECK TRIM VALVE FAULT ON PREV FLT. RESET & FAULT DID NOT RETURN BITE TEST NR 2 CTRLR GOOD. REF FIM 21 62 /T832. NO HISTORY 60 DAYS.SDR ASAA12510987Sensor · faultyAPU CT5ATP EGT HAS HISTORY OF INDICATING LOW AND ERRONEOUS. INDICATION ERRORS ARE SUSPECT. REPLACED APU INLET TEMP SENSOR (T2) IAW AMM 49 61 31. OPS CHECK GOOD.SDR ASAA12510962Unknown · malfunctioned"FMC DISAGREE' ANNUNCIATED ON GROUND. ACCOMPLISHED QRH PROCEDURE. RESET SUCCESSFUL.SDR ASAA12510921Keyboard · intermittentMCDU L3 KEY IS INTERMITTENTLY NOT WORKING. VERIFIED F/O'S MCDU L3 KEY INTERMITTENT. REPLACED KEYPAD. MCDU TESTS GOOD.SDR ASAA11510606Connector · dirtyWHILE ACCOMPLISHING T/C 78273000, INTERROGATE THE FMC CDU FOR ENGINE FAULTS. FOUND FAULT CODE 75-10831 THE T3 SIGNAL IS OUT OF RANGE. (LONG TIME FAULT). ACFT GROUNDED. FAULT NOT ACTIVE NO RECENT OR FAULT HISTORY. VERFIED T3 CHANNEL A & CHANNEL B DATA DISPLSDR ASAA1159934Unknown · malfunctionedFMC DISAGREE MESSAGE DISPLAYED AND FMC DISAGREE LIGHT ILLUMINATED DURING TAXI. QRH PROCEDURE CLEARED MESSAGE LIGHT REMAINED OUT.SDR ASAA1159642Warning System · malfunctionedON INITIAL TAXI OUT GOT FMC DISAGREE WARNING PROMPTS ON NAV DU'S. PERFORMED QRH PROCEDURE FMC'S RETURNED TO OPS NORMAL. FLIGHT RESUMED.SDR ASAA1159454Controller · defectiveDURING CRUISE IT WAS OBSERVED CABIN ALTITUDE TO BE FREQUENTLY OSCILLATING BETWEEN 500 FPM RATE OF CLIMB AND 300 FPM RATE OF DESCENT. REMOVED AND REPLACED NR 1 CABIN PRESSURE CONTROLLER IAW AMM 21 31 01 AND OPS CHECK GOOD IAW AMM 21 31 00 700 802.SDR ASAA1159055Unknown · malfunctionedDURING CRUISE AT FL370 NEAR COAST IN CABIN PRESSURE RATE OF CLIMB BEGAN TO VARY BETWEEN 1000FPM CLIMB AND 500FPM DESENT. AFTER TWO MINUTES CABIN STABILIZED AT 8000 AND RATE SETTLED. PERFORMED GROUND TEST BITE PROCEDURE ON NR 1&2 DIGITAL CABIN PRESSURE CONTROSDR ASAA1158966Filter · dirtyAFTER START DURING RECALL RECEIVED A ZONE TEMP LIGHT CONTROL CABIN ZONE TEMP RESETS WITH MASTER CAUTION RESET. ACCOMPLISHED FIM TASK 21 62 TASK 801. FLT DECK CABIN SENSOR LOGGED ON BOTH PACK ZONE TEMP CONTROLLERS. FAULTS CLEARED ON RESET. TESTED EACH 2 MOR
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