N535AS
Service difficulty reports · 387
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 = 'N535AS' 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 = 'N535AS' 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 ASAA2014081808878Warning Light · illuminatedRIGHT PACK ILLUMINATED DURING TAKEOFF, WOULD NOT EXTINGUISH AFTER COMPLETED QRH PROCEDURE. ACFT GROUNDED. OPENSDR ASAA2014081608845Satcom · malfunctionedSATCOM NOT ANNUNCIATED ON MENU ON FMC. ACFT GROUNDED. SATCOM LOCKED UP ON GROUND QRH PERFORMED. SAT PROMPT DISPLAYED NORMALLY.SDR ASAA2014080308744Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. PERFORMED BITE CHECK IAW MM 21-61-00-700-806-002. NO FAULTS NOTED. NO HISTORY 90 DAYS.SDR ASAA2014070308436Satcom · malfunctionedMCDU MENU PAGE DOES NOT HAVE SATCOM LISTED. ACFT GROUNDED. RESET SATCOM C/B AT P18-2 PANEL GRID D14 IAW AMM 20-60-01. SAT ON MCDU MENU PAGE NOW APPEARS.SDR ASAA2014061108160Warning Light · false activationDURING TAXI OUT, FMC DISAGREE LIGHT CAME ON. ACFT GROUNDED. QRH PROCEDURE EXTINGUISHED THE LIGHT.SDR ASAA2014053107984Warning Light · inoperativeFWD CARGO GREEN CONTINUITY LIGHT INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED CARGO BAY SMOKE DETECTION. OPS TEST IAW AMM TASK 26-16-00-710. SYS TEST OK NO FAULT DETECTED.SDR ASAA2014053007983Fire Detector · contaminatedCARGO FIRE DETECTOR FWD EXTINGUISHER LIGHT WILL NOT TEST. ACFT GROUNDED. CLEARED DUST FROM FWD CARGO DETECTORS AND OPS NORMAL REF MM 26-00-02.SDR ASAA2014052807966Control Panel · failedWEATHER RADAR AUTO MODE INOPERATIVE. LATER REPORTED AS WX RADAR - MANUAL TILT ON CAPTAIN'S SIDE AND F/O SIDE IS NOT WORKING PROPERLY. WITH ZERO MANUAL TILT SELECTED ON CAPT SIDE, ND DISPLAY SHOWS + 11M WITH -15 SELECTED ON KNOB, ND SHOWS 0M AND CAN'T BE TILTSDR L4PR20140522002Converter · damaged.5 INCH DIAMETER OF THE CENTER CORE OF CATALYTIC OZONE CONVERTER IS MISSING.SDR L4PR20140522001Converter · damaged.5 INCH DIAMETER OF THE CENTER CORE OF CATALYTIC OZONE CONVERTER IS MISSING.SDR ASAA2014051407810Unknown · unknownPRACTICE HGS A111 AUTOLAND UNSATISFACTORY, FINAL 100' SINK RATE INCREASED WITH DECREASED PITCH RESULTING IN FIRM TOUCHDOWN. TD POINT WAS ACCURATE. NO HGS WARNINGS, BUT SINK RATE NOT STABLE AT LOW ALTITUDE. ACFT GROUNDED. PERFORMED A LAND VERIFY TEST IAW MMSDR ASAA2014050307687Fmc · malfunctionedON SHORT FINAL, TWO SECONDS PRIOR TO TOUCHDOWN, FMC DISAGREE MESSAGE WITH LOSS OF AIRSPEED INDICATIONS ON CAPTAIN`S SIDE. AT LANDING, LOST AIRSPEED INDICATION ON BOTH CAPTAIN'S AND F/O'S SIDE. PFD'S ONLY. ACFT GROUNDED. PERFORMED FMC BITE IAW AMM 34-61-TASK 8SDR ASAA2014050207691Heat Shield · crackedNR 2 ENGINE REAR FLANGE IS CRACKED AT BOLT HOLES. ACFT GROUNDED. R & R FLANGE ASSY REF MM 72-56-00.SDR ASAA2014050207690Heat Shield · crackedNR 1 ENGINE REAR FLANGE IS CRACKED AT BOLT HOLES. ACFT GROUNDED. R & R FLANGE ASSY IAW MM 72-56-00.SDR ASAA2014041107510Warning Message · false activationON GROUND FMC DISAGREE, ACFT GROUNDED. COMPLETED CHECK LIST, FMC NORMAL.SDR ASAA2014041075211Warning Message · false activationFMC DISAGREE LT ON GROUND. ACFT GROUNDED. CLEARED IAW QRH PROCEDURES. OPS NORMAL.SDR ASAA2014040807477Satcom · malfunctionedSATCOM INOPERATIVE. NO FMC MENU PROMPT L-4. ACFT GROUNDED. CYCLED CIRCUIT BREAKER, SATCOM P18-2 GRID D-14 IAW AMM TASK 23-16-00-23-801. OPS CHECK GOOD.SDR ASAA2014040707463Satcom · lockedSAT COM LOCKED UP DURING POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED QRH SAT COM RESTORED.SDR ASAA2014030107031Valve · failedNR 2 ENGINE ANTI-ICE OVERHEAD LIGHT IS FLICKERING ON AND OFF. NO OTHER ABNORMAL INDICATIONS. SWITCH WAS IN THE OFF POSITION. ACFT GROUNDED. REMOVED 2 ENG TAI VALVE IAW AMM 30-21-11-000-801. INSTALLED NR 2 ENG TAI VALVE IAW AMM 30-21-11-400-801.SDR ASAA2014022306962Engine · stalledAFTER APU START COMPRESSOR STALLS CAN BE HEARD & RPM FLUCTUATES. ACFT GROUNDED. ACCOMPLISHED APU BITE CHECK, NO FAULTS NOTED. RAN APU NO STALLS NOTED, INPUT MONITORING SPEED WAS STEADY AND CONSTANT WITH AND WITHOUT LOADS.SDR ASAA2014021806897Warning Message · false activationFMC DISAGREE SCRATCH PAD. DISPLAY UNIT AMBER ANNUNCIATION AFTER ENGINE START AND GENS PUT ON BUSSES. ACFT GROUNDED. QRH PROCEDURE FOLLOWED. OPS RESTORED TO NORMAL.SDR ASAA2014020906809Valve · faultedCONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. EXTINGUISHES ON RESET. ACFT GROUNDED. PERFORMED PAC/ZONE TEMP CONT BITE IAW MM 21-61-00, PREVIOUS FLT SHOWED RT PACK, COCKPIT TRIM VALVE FAULT. VERIFY SHOWED PASS. NO HISTORY 90 DAYS.SDR ASAA2014012412485Wire Harness · chafedNR 1 ENGINE FOUND CJ9 AND CJ10 ENGINE CORE WIRE HARNESSES CHAFED TOGETHER, VSVA CONNECTOR ON CJ9, APPROX 3 O`CLOCK. ACFT GROUNDED. REPLACED CJ9 AND CJ10 CORE ENGINE WIRE HARNESS IAW AMM 73-21-06.SDR ASAA2014012412477Wire Harness · damagedNR 1 ENGINE, WIRE HARNESS FOR LT & RT CORE FIRE DETECTOR, STAINLESS STEEL INSULATION DAMAGED AND MISSING. ACFT GROUNDED. REPLACED NR 1 ENGINE LT & RT CORE FIRE DETECTOR HARNESS MW0326, REF AMM 26-11-02. ETOPS SIGNIFICANT SYS GROUND VERIFICATION SUCCESSFUL.SDR ASAA2014011812411Satcom · faultedSATCOM PROMPT ON MENU NOT DISPLAYING. ACFT GROUNDED. RESET SATCOM SYS IAW FIM TASK 23-15-801, SYS TESTS GOOD.SDR ASAA2014011012359Warning Message · illuminatedRT A/C PACK LIGHT CAME ON IN CRUISE FOLLOWED QRH PROCEDURE. DURING RECALL LIGHT ILLUMINATED. AFTER MASTER CAUTION RESET LIGHT WENT OUT, ACFT GROUNDED. PERFORMED PACK TEMP CONTROLLER BITE TEST REF AMM 21-61-00, OPS CK NORMAL.SDR ASAA2013121912182Warning Light · false activationLT PACK LIGHT ILLUMINATES WHEN RECALL. EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED PACK TEMP CONTROL BITE AMM REF 21-61-00, OPS CHECK NORMAL GROUND VERIFICATION SUCCESSFUL NO HISTORY 30 DAYS.SDR ASAA2013110396288Warning System · inaccurateNR 2 HF RADIO ANNUNCIATES FAIL BUT WORKS NORMALLY. ACFT GROUNDED. RESET ACFT POWER, FAIL MESSAGE CLEARED, PERFORMED HF SYS BITE AMM TASK 23-11-801, BITE TEST GOOD. PERFORMED RADIO OPS CHECK OK. NO HISTORY FOR PAST 30 DAYS.SDR ASAA2013103196272Shim · wornWHILE CONDUCTING FAN LUBE, ON NR 2 ENGINE, IT WAS NOTED THAT THE MOLY DAG COATING ON ALL BLADE SHIMS IS WORN OFF. ACFT GROUNDED. REPLACED ALL FAN BLADE SHIMS IAW T/C 78472002 ON NR 2 ENG.SDR ASAA2013082395874Engine · malfunctionedAPU DID NOT START ON FIRST ATTEMPT. FAULT CODE 49-41012. ACFT GROUNDED. ACCOMPLISHED FIM TASK 49-40, TASK 803, STEP E. BITE CHECK DID NOT SHOW MX MESSAGE 49-41012. IN LAST CYCLE. ONLY SHOWS 1 OCCURRENCE IN FAULT HISTORY IAW FIM TASK THE FAULT IS CORRECTED.SDR ASAA2013081695816Satcom · malfunctionedSATCOM PROMPT ON FMC. UNABLE TO INITIATE CALL. ACFT GROUNDED. PERFORMED FIM 23-15-801. SATCOM RESET & REBOOTED CORRECTLY. SATCOM PROMPT RETURNED. NO OTHER DEFECTS NOTED.SDR ASAA2013081295782Fmc · false indicationON TAXI OUT, FMC DISAGREE. ACFT GROUNDED. QRH COMPLETE. OPS NORMAL.SDR ASAA2013072595684Fmc · false activationFMC DISAGREE LIGHT ON. ACFT GROUNDED. RESOLVED WITH QRH PROCEDURE.SDR ASAA2013072495670Fmc · false indicationFMC DISAGREE DURING TAXI OUT. ACFT GROUNDED. RESOLVED BY QRH PROCEDURE.SDR ASAA2013071595614Power Supply · inoperativeL2 DOOR-SLIDE EMERGENCY LIGHT INOPERATIVE DURING T/C 78233008. ACFT GROUNDED. R & R POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD T/C 782333008 AND W/D 33-51-14.SDR ASAA2013071295575Control Valve · malfunctionedLEVELING FL390 RT BLEED TRIP OFF LIGHT ILLUMINATED BLEED RESET WITH TRIP RESET IAW QRH. CRUISE LT PRESS 39 PSI, RT PRESS 31 PSI, RT BLEED TRIP OFF LIGHT ILLUMINATED SECOND TIME DURING TOP OF DESCENT 90 N2 80 N1. BLEED RESET WITH TRIP RESET. NO WING OR ENGINESDR ASAA2013060294957Warning Message · illuminatedON GROUND AFTER ENGINE START, PUSHBACK, AMBER FMC DISAGREE ON BOTH NAV DISPLAYS. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. FMC DISAGREE, ANNUNCIATION EXTINGUISHED.SDR ASAA2013051994850Unknown · unknownSATCOM INOPERATIVE. PROMPT DOES NOT APPEAR ON THE FMC, SATCOM SWITCHES DO NOT WORK. THE SATCOM PROMT CAME BACK ABOUT 30 MIN LATER AND THE SYS WORKED CORRECTLY. ACFT GROUNDED. PERFORMED SATCOM SYS TEST REF MM 23-15-00-730-801. OPS NORMAL. CYCLED POWER NUMERSDR ASAA2013050394704Satcom · malfunctionedPILOTS UNABLE TO HEAR AUDIO SATCOM 12. DATA NORMAL DISPATCH SAYS THEY CAN HEAR PILOTS WHEN CALL IS MADE. ACFT GROUNDED. PERFORMED SATCOM NR 1 & NR 2 ADJ/TEST IAW AMM 23-15-00, BOTH SYS TRANSMITT & RECEIVE NORMAL DURING CALLS, SAN GND-TO-DISPATCH. GROUND VERSDR ASAA2013042194559Starter Gen · failedAPU FAILED TO START AND THE APU FAULT LIGHT ILLUMINATED. REPLACED STARTER GENERATOR IAW AMM 49-41-21-000-801 AND 49-41-21-400-801. R & R START CONVERTER UNIT IAW AMM 49-41-61-000-801 AND 49-41-61-400-801 STARTER APU IAW AMM 49-11-00-860-801. GROUND OPERATIOSDR ASAA2013041794509Sensor · failedDIAGNOSTICS REPORTS NR 1 ENGINE IS SENDING INTERMITTENT OIL PRESSURE ALERTS. ALL WITHIN NORMAL EXPECTED RANGE. ACCOMPLISHED TSR. PERFORMED AVM BITE IAW 77-31-00-970-803-F00. FOUND N2 SENSOR FAILED ON NR 1 ENG 31 FAULTS. REMOVED AND INSTALLED NEW NR 1 ENG SDR ASAA2013032594263Controller · malfunctionedCONT CAB LIGHT ON RECALL RESETS ON MC RECALL. CONFIRMED FAULT, CONT CABIN ZONE TEMP LIGHT ILLUMINATES ON MASTER RECALL. T/S FOUND NR 2 ZONE TEMP CONTROLLER WITH FLT DECK TRIM VALVE FAULT LIGHT ILLUMINATED AFTER INTERROGATION. PERFORMED NR 1 & NR 2 CABIN TESDR ASAA2013020793850Unknown · unknownDIAGNOSTICS REPORTS NR 1 ENGINE CORE VIBRATION DATA INTERMITTENTLY REPORTS ZEROS FROM THE FRONT AND REAR SENSORS. AAVM STILL LOGS LOSS OF N2 SIGNAL, ALSO CDS LOGGED 31-63150, ENGINE 1 N2 RPM INVALID ON BOTH DEUS AS INTERMITTENT AND ON VARIOUS FLT LEGS. VERIFSDR ASAA2013020693822Sensor · intermittentDIAGNOSTIC REPORTS NR 1 ENGINE CORE VIBRATION DATA INTERMITTENTLY REPORTS ZEROS FROM THE FRONT AND REAR SENSORS. ACFT GROUNDED. PERFORMED AAVM SYS BITE CHECK. BITE CHECK LOGGED N2 SENSOR LOSS OF SIGNAL FOR NR 1 ENG. REPLACED NR 1 ENG N2 SENSOR. OPS CK GOODSDR ASAA2013011493681Unknown · unknownINITIAL FUEL LOAD ON ACFT WAS INCORRECT, MAIN TANKS NOT FUELED TO FULL IN CENTER TANKS. PERFORMED FUEL QUANTITY OP TEST REF AMM 28-41-00-710-801, NO FAULTS FOUND, NO CURRENT FAULTS FOUND, SYS VERIFIED WITH FUEL STICK VERSUS FLT DECK IND, WITHIN LIMITS IAW AMMSDR ASAA2013010193589Warning Light · illuminatedON RECALL, AIR CONDITIONER & ZONE TEMP ILLUMINATED. EXTINGUISH ON RESET. NR 2 PACK ZONE TEMP CONTROLLER LOGGED FLT DECK TRIM VALVE FAULT. ACCOMPLISHED FIM TASK 21-62, TASK 832. FAULT CLEARED AND DID NOT COME BACK ON SUBSEQUENT TESTS. RAN PACKS WITH NO FAUSDR ASAA2012122793569Eec · faultedA/T LIM SHOWING ABOVE N1 INDICATORS AFTER SPLIT THROTTLES AND AUTO THROTTLE DISCONNECT. A/T INFLT FAULTS SHOW MANY 22-31411 AND 22-31511 EEC 1A/1B DATA INV AND THROT SPLIT 22-31525. DEUS 1 & 2 FAULT 31-68210 NO EEC-1 CH A BUSS DATA. EEC 1 & 2 SHOW NO RECENTSDR ASAA2012122693549Warning Light · illuminatedAMBER LIGHT ILLUMINATED ON OVERHEAD PANEL AFTER ENGINE START AND ON ENGINE DRIVEN GENERATORS. SPCU INOPERATIVE FAULT. RESET AND TESTS NORMAL IAW FIM 24-34, TASK 802. VERIFIED FAULT, GROUND VERIFICATION SUCCESSFUL.SDR ASAA2012122593542Apu · unknownAPU DID NOT START, FAULT LIGHT ILLUMUNATED ON GROUND. PERFORMED FIM TASK 49-31-808 STEP F, FAULT CORRECTED. STARTED APU 4 TIMES, OPERATED NORMAL.SDR ASAA2012121493465Warning Light · false activationDURING PRE-FLIGHT, STANDBY POWER OFF LIGHT ILLUMINATED. FOUND STANDBY BUSS 115 VC AC IND CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. PERFORMED GROUND OPERATION VERIFICATION OF STANDBY POWER SYS. OPS NORMAL. NO HISTORY 30 DAYS. STANDBY POWER OFF LIGHT
Back to N535AS