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.

SDR ASAA2014081808878Warning Light · illuminatedRIGHT PACK ILLUMINATED DURING TAKEOFF, WOULD NOT EXTINGUISH AFTER COMPLETED QRH PROCEDURE. ACFT GROUNDED. OPENAug 18, 2014 · N535AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014081608845Satcom · malfunctionedSATCOM NOT ANNUNCIATED ON MENU ON FMC. ACFT GROUNDED. SATCOM LOCKED UP ON GROUND QRH PERFORMED. SAT PROMPT DISPLAYED NORMALLY.Aug 16, 2014 · N535AS · Boeing 737890 · Communications SystemSDR 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.Aug 3, 2014 · N535AS · Boeing 737890 · Cabin Cooling SystemSDR 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.Jul 3, 2014 · N535AS · Boeing 737890 · Communications SystemSDR ASAA2014061108160Warning Light · false activationDURING TAXI OUT, FMC DISAGREE LIGHT CAME ON. ACFT GROUNDED. QRH PROCEDURE EXTINGUISHED THE LIGHT.Jun 11, 2014 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR 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.May 31, 2014 · N535AS · Boeing 737890 · Smoke DetectionSDR 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.May 30, 2014 · N535AS · Boeing 737890 · Fire DetectionSDR 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 TILTMay 28, 2014 · N535AS · Boeing 737890 · Weather Radar SystemSDR L4PR20140522002Converter · damaged.5 INCH DIAMETER OF THE CENTER CORE OF CATALYTIC OZONE CONVERTER IS MISSING.May 22, 2014 · N535AS · Boeing 737890 · Humidity Control SystemSDR L4PR20140522001Converter · damaged.5 INCH DIAMETER OF THE CENTER CORE OF CATALYTIC OZONE CONVERTER IS MISSING.May 22, 2014 · N535AS · Boeing 737890 · Humidity Control SystemSDR 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 MMMay 14, 2014 · N535AS · Boeing 737890 · Standard Practices/StructuresSDR 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 8May 3, 2014 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014050207691Heat Shield · crackedNR 2 ENGINE REAR FLANGE IS CRACKED AT BOLT HOLES. ACFT GROUNDED. R & R FLANGE ASSY REF MM 72-56-00.May 2, 2014 · N535AS · Boeing 737890 · Turbine SectionSDR ASAA2014050207690Heat Shield · crackedNR 1 ENGINE REAR FLANGE IS CRACKED AT BOLT HOLES. ACFT GROUNDED. R & R FLANGE ASSY IAW MM 72-56-00.May 2, 2014 · N535AS · Boeing 737890 · Turbine SectionSDR ASAA2014041107510Warning Message · false activationON GROUND FMC DISAGREE, ACFT GROUNDED. COMPLETED CHECK LIST, FMC NORMAL.Apr 11, 2014 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014041075211Warning Message · false activationFMC DISAGREE LT ON GROUND. ACFT GROUNDED. CLEARED IAW QRH PROCEDURES. OPS NORMAL.Apr 10, 2014 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR 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.Apr 8, 2014 · N535AS · Boeing 737890 · Communications SystemSDR ASAA2014040707463Satcom · lockedSAT COM LOCKED UP DURING POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED QRH SAT COM RESTORED.Apr 7, 2014 · N535AS · Boeing 737890 · Communications SystemSDR 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.Mar 1, 2014 · N535AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR 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.Feb 23, 2014 · N535AS · Boeing 737890 · APU Core EngineSDR 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.Feb 18, 2014 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR 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.Feb 9, 2014 · N535AS · Boeing 737890 · Cabin Temperature Control SystemSDR 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.Jan 24, 2014 · N535AS · Boeing 737890 · Engine Fuel System WiringSDR 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.Jan 24, 2014 · N535AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2014011812411Satcom · faultedSATCOM PROMPT ON MENU NOT DISPLAYING. ACFT GROUNDED. RESET SATCOM SYS IAW FIM TASK 23-15-801, SYS TESTS GOOD.Jan 18, 2014 · N535AS · Boeing 737890 · Communications SystemSDR 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.Jan 10, 2014 · N535AS · Boeing 737890 · Cabin Cooling SystemSDR 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.Dec 19, 2013 · N535AS · Boeing 737890 · Central WarningSDR 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.Nov 3, 2013 · N535AS · Boeing 737890 · HF Communications SystemSDR 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.Oct 31, 2013 · N535AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR 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.Aug 23, 2013 · N535AS · Boeing 737890 · APU Core EngineSDR 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.Aug 16, 2013 · N535AS · Boeing 737890 · Communications SystemSDR ASAA2013081295782Fmc · false indicationON TAXI OUT, FMC DISAGREE. ACFT GROUNDED. QRH COMPLETE. OPS NORMAL.Aug 12, 2013 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013072595684Fmc · false activationFMC DISAGREE LIGHT ON. ACFT GROUNDED. RESOLVED WITH QRH PROCEDURE.Jul 25, 2013 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013072495670Fmc · false indicationFMC DISAGREE DURING TAXI OUT. ACFT GROUNDED. RESOLVED BY QRH PROCEDURE.Jul 24, 2013 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR 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.Jul 15, 2013 · N535AS · Boeing 737890 · Emergency LightingSDR 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 ENGINEJul 12, 2013 · N535AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013060294957Warning Message · illuminatedON GROUND AFTER ENGINE START, PUSHBACK, AMBER FMC DISAGREE ON BOTH NAV DISPLAYS. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. FMC DISAGREE, ANNUNCIATION EXTINGUISHED.Jun 2, 2013 · N535AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR 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 NUMERMay 19, 2013 · N535AS · Boeing 737890 · Communications SystemSDR 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 VERMay 3, 2013 · N535AS · Boeing 737890 · Communications SystemSDR 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 OPERATIOApr 21, 2013 · N535AS · Boeing 737890 · APU Start/Ignition SystemSDR 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 Apr 17, 2013 · N535AS · Boeing 737890 · Power Indicating SystemSDR 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 TEMar 25, 2013 · N535AS · Boeing 737890 · Cabin Temperature Control SystemSDR 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. VERIFFeb 7, 2013 · N535AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR 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 GOODFeb 6, 2013 · N535AS · Boeing 737890 · Power Indicating SystemSDR 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 AMMJan 14, 2013 · N535AS · Boeing 737890 · Fuel Indicating SystemSDR 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 FAUJan 1, 2013 · N535AS · Boeing 737890 · Cabin Temperature Control SystemSDR 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 RECENTDec 27, 2012 · N535AS · Boeing 737890 · Fuel Controlling SystemSDR 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.Dec 26, 2012 · N535AS · Boeing 737890 · Central WarningSDR 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.Dec 25, 2012 · N535AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR 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 LIGHTDec 14, 2012 · N535AS · Boeing 737890 · Central Warning
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