N534AS
Service difficulty reports · 339
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 = 'N534AS' 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 = 'N534AS' 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 ASAA2017012619564Wire Harness · damagedNR 1 ENGINE WIRE HARNESS MW0326 HAS BROKEN SHEILDING. ACFT GROUNDED. REMOVED AND REPLACED CORE FIRE DETECTION HARNESS. OPS NORMAL IAW AMM 26-11-02.SDR ASAA2016120418931Linkage · looseNR 2 ENGINE INTERSECTION DUCT LOWER ATTACH LINK ASSEMBLY LOOSE. ACFT GROUNDED. REMOVED & REPLACED THE DUCT SUPPORT LINKAGE ASSEMBLY IAW AMM 36-11-01.SDR ASAA2016101618370Start Valve · failedNR 1 ENGINE NO ROTATION UPON STARTING WITH NO START VALVE LIGHT. GROUNDED, YES. REMOVED AND REPLACED NR 1 ENGINE START VALVE, REF AMM 80-11-03. LEAK AND OPS CHECK GOOD, REF AMM 71-00-00.SDR ASAA2016101418341Battery Pack · failedDURING CLIMB, FA REPORTED FWD EMERGENCY LIGHTS ILLUMINATED. THERE WAS A BRIEF ELECTRICAL ODOR IN THE COCKPIT WHICH DISSIPATED. CIRCUIT BREAKER P18 A11 LIGHTING EMERGENCY CHARGER FWD WAS FOUND TRIPPED. ABOUT 20 MINUTES LATER, FWD EMERGENCY LIGHTS EXTINGUISHED SDR ASAA2016082617823Cone · wornNR 2 ENGINE FRONT SPINNER CONE ANTI-EROSION COATING, ROTATION INDICATOR WORN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FRONT SPINNER CONE, IAW AMM 72-21-01-00-801-F00 STEPS 2E AND 2F(1) AND 72-21-01-400-801-F00 STEPS 3F(5) AND 3G.SDR ASAA2016081617721Control Module · failedFOLLOW-UP TO REPORT OF CABIN PRESSURE CONTROL PANEL INTERMITTENT DISPLAYS, REPLACE PANEL FOR BENCH CHECK. ACFT GROUNDED. REMOVED & REPLACED CABIN PRESSURE CONTROL MODULE, IAW AMM 21-31-02. SYSTEM GROUND & MANUAL MODE TEST PASSED. REPLACED R87 AUX MASTER DIM SDR ASAA2016080217590Unknown · unknownBOTH FMC'S UNABLE TO LINE SELECT 5L INTO SCRATCHPAD ON FIX PAGE, A BEAM ONLY. IN OTHER FMC PAGES, LINE 5L WORKS NORMALLY. ACFT GROUNDED. SPOKE WITH FLIGHT CREW UPON ARRIVAL. CAPT SAID IT STARTED WORKING AFTER HE WROTE IT UP, AND CONTINUED TO OP NORMAL. TESTSDR ASAA2016080117579Control Module · failedOUTFLOW VALVE POSITION INDICATOR ERRATIC. CYCLING BETWEEN OPEN AND CLOSED. PRESSURIZATION NORMAL. GROUNDED - YES. SPOKE WITH FLIGHT CREW UPON ARRIVAL. ACCOMPLISHED FIM TASK 21-31 TASK 801. NO FAULTS ON BOTH CONTROLLERS AND NO FAULT HISTORY. REPLACED CABIN PSDR ASAA2016072917550Warning Message · false activationFRM 21312100 CABIN ALTITUDE IS AT 7000 FT AND DIFFERENTIAL PRESSURE IS AT 8.5 PSI. AIRCRAFT WAS FLOWN AT FL380. ACFT GROUNDED. PERFORMED FIM 21-33 TASK 803, OPS NORMAL.SDR ASAA2016072617522Outflow Valve · failedAT 500 FEET ON FINAL, THE AUTO FAIL LIGHT ILLUMINATED ON THE PRESSURIZATION PANEL ALONG WITH GREEN ALTN LIGHT. AT GATE WE FOLLOWED THE QRH AND WHEN I MOVED THE SWITCH TO ALTN THE AUTO FAIL LIGHT WENT OUT. GROUNDED - YES. REMOVED AND INSTALLED NEW OUTFLOW VALVSDR ASAA2016071517379Modulating Valve · failedDURING MASTER CAUTION RECALL, MASTER CAUTION AIR COND LIGHT AND CONTROL CABIN ZONE TEMP LIGHT ILLUMINATED, EXTINGUISHED DURING MASTER CAUTION RESET. ACFT GROUNDED. R & R LT PACK TEMP CONTROL MODULATING VALVE IAW AMM 21-51-10, OPS CHECK NORMAL.SDR ASAA2016071517376Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATES ON RECALL. GOES OUT ON MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED FIM 21-62 TASK 848. LIGHT DID NOT ILLUMINATE. PERFORMED BITE B737-800 FIM 21-62 TASK 801. NO FAULTS LOGGED. OPERATED PACK. NO ZONE TEMP LIGHT ILLUSDR ASAA2016071317366Exciter · failedAPU FAULT LIGHT ILLUMINATES DURING START. ACFT GROUNDED. REMOVED AND REPLACED EXCITER IGNITION UNIT IAW AMM 49-41-31.SDR ASAA2016063017221Compensator · failedNR 2 MAIN FUEL TANK AUTO SHUT OFF AT 8,260 LBS. ACFT GROUNDED. REMOVED NR 2 MAIN TANK ACCESS PANEL 632AB IAW AMM 28-11-11. REMOVED AND REPLACED NR 2 MAIN TANK COMPENSATOR PROBE IAW AMM 28-41-21. INSPECTED AREA, OK TO CLOSE ACCESS PANEL 632AB. INSTALLED ANDSDR ASAA2016061417136Floor Panel · corrodedPARTS RACK, AFT PIT FLOOR PANEL 140BF HAS CORROSION ALL AROUND. ACFT GROUNDED. CORROSION ON FLOOR PANEL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1, MATERIAL ID FOR FLOOR PANEL 2024-T3, CLAD .071 IAW DWG 453A2610, REV K FABRICATED FLOOR PANEL IAW DWG 453SDR ASAA2016061417088Skin · crackedCRACK NOTED ON RT HORIZONTAL STABILIZER JUST INBD OF STABILIZER STA 147.9. CRACK IS APPROXIMATELY 1" LONG AND IS APPROXIMATELY 8" FWD OF REAR SPAR. CRACK IS MARKED IN RED. ACFT GROUNDED. REPAIRED LOWER SKIN ON RT HORIZONTAL STABILIZER AT STA 147.9 IAW SRM SDR ASAA2016061417087Skin · crackedCRACK NOTED ON LT HORIZONTAL STABILIZER JUST INBD OF STABILIZER, STA 138.7, CRACK IS APPROXIMATELY 1.5" LONG AND IS NEXT TO DRAIN HOLE. CRACK IS MARKED IN RED. ACFT GROUNDED. REPAIRED LOWER SKIN ON LT HORIZONTAL STABILIZER AT STABILIZER STA 138.7 IAW SRM 55SDR ASAA2016043016572Warning Message · false activationDURING PREFLIGHT SAW MAP ON F/O FMC AND SINGLE FMC OPERATIVE. ACFT GROUNDED. ACCOMPLISHED OPS TEST OF FMCS IAW AMM 34-61-00-710-801. OPS CHECKED NORMAL.SDR ASAA2016032416084Warning Light · false activationON SHORT FINAL AUTOFAIL ILLUMINATED ON PRESSURIZATION PANEL. ACFT GROUNDED. PLACED CONTROL TO MANUAL & BACK TO AUTO, FAULT CLEARED NR 2 CONTROLLER FAULTED OUTFLOW VALVE. NR 1 AND NR 2 PRESSURIZATION SYS GROUND TEST, OPS CHECKS NORMAL.SDR ASAA2016021615487Unknown · odorON DEPARTURE FROM DCA FLAPS 15 BLEEDS OFF RWY 1 JUST AFTER LIFTOFF COCKPIT BEGAN FILLING WITH SMOKE AND FUMES, THICKEST SMOKE AFTER 1 MIN, DISSIPATED COMPLETELY BY 4 MIN SUSPECT MASSIVE INJECTION OF DE-ICE FLUID TYPE IV INTO AC SYS THROUGH APU INLET. ACFT GROSDR ASAA2016012014936Converter · failedAPU FAULT LIGHT ON FIRST START ATTEMPT. ACFT GROUNDED. ACCOMPLISHED FIM 49-40 TASK 821. NO CURRENT FAULTS. HISTORY SHOWS MESSAGE 49-41254. HAS HISTORY OF PRIOR OCCURRENCES. REF AMM 49-41-61-400-801, R & R APU START CONVERTER UNIT. OPS TEST NORMAL.SDR ASAA2016011214751Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.SDR ASAA2016011214750Warning Light · false activationDURING RECALL, THE CONTROLLER CABIN ZONE TEMP LIGHT STAYED ON. IT WENT OUT WHEN RESET. ACFT GROUNDED. CONFIRMED CONTROLLER CAB ZONE TEMP ANNUNCIATOR ILLUMINATED WITH MASTER CAUTION RECALL AND EXTINGUISHES WITH RESET. PERFORMED CABIN TEMP CONTROLLER BITE OSDR ASAA2016010114601Warning Message · false activationFMC DISAGREE ILLUMINATED ON THE GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC DISAGREE MESSAGE CLEARED.SDR ASAA2015121814323Battery Pack · failedLEFT AFT EMERGENCY LIGHT FAILED TEST FROM TASK CARD 78233001. ACFT GROUNDED. LEFT AFT EMERGENCY LIGHT BATTERY PACK. R & R IAW AMM 33-51-06. OPS CHECK GOOD.SDR ASAA2015112514241Lamp · failedOVERHEAD EMERGENCY AISLE SPOTLIGHT AT ROW 1 IS INOPERATIVE. ACFT GROUNDED. RELAMPED ROW 1 OVERHEAD EMERGENCY AISLE SPOTLIGHT, OPS NORMAL.SDR ASAA2015111213762Circuit Breaker · failedON ENGINE SHUTDOWN THE NR 1 TRANSFER BUS OFF LIGHT CAME ON. ACFT GROUNDED. ISOLATED TO FAULTY BUS TIE BREAKER C804. R & R C804 BUS TIE BREAKER NR 1 IAW MM 24-21-41. TESTS GOOD IAW SAME. NR 1 GCU CHECKS GOOD IAW INSTRUMENT TEST MM 24-21-81.SDR ASAA2015103113565Connector · misinstalledCAPT'S WINDOW HEAT CONNECTOR AT L2 WINDOW CLOCKED INCORRECTLY. ACFT GROUNDED. RECLOCKED CAPT'S WINDOW HEAT CONNECTOR AT L2 WINDOW. REF MM TASK 56-12-11-420-006 STEP F, 5. WINDOW HEAT CHECKED GOOD. REF MM TASK 30-41-00-710-801.SDR ASAA2015101313493Valve · failedNR 1 ENGINE ANTI-ICE COWL VALVE OPEN, LIGHT ON WHEN ANTI-ICE SWITCH IS OFF. ACFT GROUNDED. REPLACED NR 1 ENGINE COWL TAI VALVE REF MM 30-21-11-000-801 AND 30-21-11-400-801. PERFORMED OPS TEST, REF MM 30-21-00-710-801, OPS CHECKS NORMAL. ETOPS GROUND VERIFICASDR ASAA2015100513341Anti-Ice Valve · malfunctionedAFTER ENGINE SHUTDOWN, NR 1 COWL VALVE OPEN LIGHT. REMAINED ON WITH ENGINE ANTI-ICE SWITCH OFF. ACFT GROUNDED. CYCLED NR 1 ENGINE COWL VALVE SWITCH. LIGHT EXTINGUISHED. PERFORMED NR 1 ENGINE COWL ANTI-ICING OPS CHECK IAW AMM 30-21-00-710-801, OPS CHECK NORSDR ASAA2015092513201Connector · looseINTERMITTENT DIM FLASHING OF LT ANTI-ICE COWL VALVE OPEN LIGHT ON CLIMBOUT WITH ENGINE ANT-ICE SWITCH OFF. UPON ENCOUNTERING ICING CONDITIONS, THE SWITCH AND LIGHT OPERATED NORMALLY AND NO FURTHER FLASHING OCCURRED IN EITHER SWITCH ON OR OFF POSITION THE REST SDR ASAA2015091213004Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. SATCOM RESTORED IAW QRH.SDR ASAA2015090712968Static Inverter · warning lightELECTRIC LIGHT REMAINS ILLUMINATED ON OVERHEAD ELECTRICAL PANEL. ACFT GROUNDED. PERFORMED FIM 24-31, TASK 801, ELECTRIC LIGHT BITE CK. LOGGED STAT INV INOPERATIVE FAULT. IAW TECH SERVICES REQUEST, REPLACED STATIC INVERTER REF MM 24-34-21 & FAULT CLEARED. ALSSDR ASAA2015090612950Regulator · failedBLEED AIR VALVES LT CIRCUIT BREAKER TRIPPED, P6-4, NR 7. ACFT GROUNDED. GVI P6-4 CIRCUIT BREAKER PANEL NO FAULT FOUND RESET CIRCUIT BREAKER. CIRCUIT BREAKER TRIPPED AGAIN. DISCONNECT DP1102, CIRCUIT BREAKER STAYED IN. SUSPECT M1180 ENG 1 BLEED AIR REGULATOSDR ASAA2015090512933Inverter · failedLIGHT ILLUMINATED ON RECALL. ACCOCIATED ELECTRIC LIGHT ILLUMINATED OVERHEAD ELECTRICAL PANEL. ACFT GROUNDED. ACCOMPLISHED ELECTRIC LIGHT MESSAGE BITE, REF FIM24-31, TASK 801, LOGGED "SPCU INOP" FAULT, UNABLE TO CLEAR. ACCOMPLISHED FIM 24-34, TASK 802. REPLSDR ASAA2015090512932Light · false activationDURING TAXI, ELECTRONIC LIGHT ILLUMINATED, RAN QRH RETURN TO GATE. ACFT GROUNDED. PERFORMED FIM 24-31, TASK 801, ELECTRIC LT BITE CK. LOGGED STAT INV INOPERATIVE FAULT. PERFORMED FIM 24-34, TASK 801 & FAULT CLEARED, REF LOG 11411176 FOR ETOPS TOP DEFERRAL.SDR ASAA2015090412938Control Unit · failedF/O WINDSHIELD HEATS UP BUT IT WILL NOT TEST PROPERLY, THE OVERHEAT LIGHT DOES NOT LIGHT UP FOR OVERHEAT TEST AND ON FRONT OF CONTROL BOX IN ELECTRONIC EQUIPMENT, LIGHT TEST DOESN'T WORK AND BITE TEST DOESN'T WORK. ACFT GROUNDED. R & R F/O'S WINDSHIELD HEAT SDR ASAA2015090312929Light · false activationELECTRICAL LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED FIM TASK 24-31, TASK 801, FOUND TO BE AN INTERMITTENT FAULT.SDR ASAA2015080812776Control Panel · failedELECTRIC LIGHT ILLUMINATED ON GROUND PRIOR TO TAKEOFF. ACFT GROUNDED. R & R ELECTRICAL METER BATTERY PANEL 24-21-53. OPS CHECK NORMAL.SDR ASAA2015080712784Battery · failedAPU FAULT LIGHT ILLUMINATED. ACFT GROUNDED. FOUND THE FOLLOWING FAULTS ON APU MAINTENANCE FAULT HISTORY: 49-11019, 49-41012. AND 49-41-1. APU WILL START FINE WITH EXTERNAL POWER BUT WILL SHUTDOWN ALONG WITH AC LOSING ELECTRICAL POWER AS SOON AS THE APU BUSSESDR ASAA2015080712775Static Inverter · malfunctionedDURING LANDING ROLL THE ELECTRIC LIGHT ILLUMINATED. ACFT GROUNDED. TROUBLESHOT TO STATIC INVERTER. R & R STATIC INVERTER IAW AMM 24-34-21-000-801 AND 24-34-21-400-801. STATIC INVERTER OPS CHECK GOOD AND ELECTRIC LIGHT REMAINED OUT.SDR ASAA2015080712774Static Inverter · faultedELECTRONIC LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED ELECTRIC LIGHT MESSAGE BITE PROCEDURE IAW FIM 24-31, TASK 801, STATIC INVERTER 1 FAULT SHOWS. REPLACED STATIC INVERTER IAW AMM 24-34-21.SDR ASAA2015080312710Warning Message · false activationFMC DISAGREE MESSAGE ON GROUND, AFTER TAKEOFF FLAPS SELECTED. ACFT GROUNDED. PERFORMED FMC DISAGREE QRH. OPS NORMAL.SDR ASAA2015080312705Warning Light · false activationELECTRIC LIGHT ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. BITE SHOWS STATIC INVERTER INOPERATIVE, ACCOMPLISHED FIM 24-34, TASK 801, FAULT CLEARED, ELECTRIC LIGHT TEST. NO HISTORY PAST 30 DAYS.SDR ASAA2015080212685Apu · malfunctionedAPU WILL NOT START. ACFT GROUNDED. PERFORMED APU BITE PROCEDURE IAW AMM 49-61-00-700-801, NO CURRENT FAULTS. PERFORMED APU STARTING AND OPERATION IAW AMM 49-11-00-860-801. USED BATTERY ONLY FOR FOUR STARTS AND WITH GROUND POWER CONNECTED TWICE. ALL STARTS SDR ASAA2015080212681Warning Flag · false activationCAPTAIN FOUND FLAG ILLUMINATED. ACFT GROUNDED. TROUBLESHOT IAW FIM TASK 22-11-00-810-801. NO FD BOV FAULTS IN DFCS HISTORY. ALL AUTO TESTS PASS. PERFORMED DFCS ADDITIONAL TEST FOR FLIGHT DIRECTOR, BITE LIBRARY GROUP 12, REF AMM 22-11-00, ALL TESTS PASS. SDR ASAA2015080212679Computer · failedAFTER START, THE L NAV WOULD NOT ENGAGE AND THE AUTO THROTTLES WOULD NOT ARM AND ON MASTER CAUTION RECALL THE SPEED TRIM AND MACH TRIM LIGHTS ILLUMINATED. ACFT GROUNDED. FFR REVEALS MULTIPLY FCC "A" FAULTS. REPLACED FCC "A" IAW MM 22-11-33. GROUND VERIFICATSDR ASAA2015072812613Satcom · malfunctionedSATCOM RECEIVES VOICE OK BUT VOICE DOES NOT GO OUT. VERIFIED WITH DISPATCH VIA ACARS COMMUNICATION. ACFT GROUNDED.SDR ASAA2015072212546Control Valve · malfunctionedLEFT "PACK" LIGHT ILLUMINATED DURING CRUISE FLIGHT. LIGHT EXTINGUISHED WITH MASTER CAUTION PUSH TO RESET. QRH PROCEDURE ACCOMPLISHED. ACFT GROUNDED. PERFORMED BITE CHECK, FOUND LT TEMP CONTROL VALVE INOPERATIVE. REPLACED LT TEMP CONTROL VALVE. ACCOMPLISHEDSDR ASAA2015072112530Warning Light · false activationAIRBORNE NR 1 PACK LIGHT ILLUMINATED ON AIR CONDITIONING PANEL MASTER CAUTION RESET EXTINGUISHES LIGHT. ACFT GROUNDED. PERFORMED TEMP CONTROL BIT TEST REF MM 21-61-00 TCV FAULT CLEARED, NO HISTORY PAST 30 DAYS. OK FOR SERVICE.
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