N518AS
Service difficulty reports · 480
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 = 'N518AS' 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 = 'N518AS' 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 ASAA2014081708870Warning Light · illuminatedCOWL ANTI-ICE LIGHT ILLUMINATED AFTER LANDING, TAXI IN, AND NR 2 ENGINE. SHUTDOWN ENGINE AND COWL ANTI-ICE REMAINED ILLUMINATED, COMPLETED QRH CHECKLIST. ACFT GROUNDED. OPENSDR ASAA2014081408847Warning Light · illuminatedNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE, LIGHT STAYED ON. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, NR 2 ENG FIRE DETECTION OPS NORMAL IAW MM 26-11-00. DUE TO HISTORY, R & R UPPER FAN DETECTOR ASSY, IAW MM 26-11-01. REPLACED LOWER SDR ASAA2014080908781Warning Light · inoperativeAUTOTHROTTLE ARM LIGHT INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED AUTOTHROTTLE SYS OPS TEST REF AMM TASK 22-31-00-710-801. AUTOTHROTTLE ARM LIGHT OPERATED NORMAL. COULD NOT DUPLICATE. PERFORMED LWMP AUTOTHROTTLE OPS TEST IAW 22-31-00/501. TEST PASSED. ACFTSDR ASAA2014080308747Warning Message · false activationFMC DATALINK FULL MESSAGE APPEARED. ACFT GROUNDED. PERFORMED QRH PROCEDURE, OPS NORMAL.SDR ASAA2014073108731Control Module · malfunctionedNR 2 ENGINE OVERHEAT ILLUMINATED AFTER STARTING AND STABLIZED NO HOT START THE OVER HEAT LIGHT REMAINED ON FOR TWO MINUTES AND 53 SECS. ACFT GROUNDED. CLEANED ALL TERMINAL GROUND LUGS ON A AND B FIRE LOOPS ON NR 2 ENG IAW POWER PLANT BUILDUP MANUAL 71-00-02 ASDR ASAA2014071908605Heater · leakingNR 1 ENGINE FUEL HEATER, SERVO, UPPER GASKET AT FWD LT CORNER LEAKING FUEL, ACTIVE SPRAY. ACFT GROUNDED. REMOVED NR 1 ENGINE FUEL HEATER SERVO. INSTALLED NEW FUEL HEATER SERVO IAW AMM 73-11-07-400-801-F00 UP TO PAR 3(3) STEP (E). COMPLETED SERVO HEATER INSTASDR ASAA2014070608465Satcom · malfunctionedNO SATCOM PROMPT ON GROUND. ACFT GROUNDED. ACCOMPLISHED SATCOM GROUND LOCK-UP QRH PROCEDURE SATCOM PROMPT WAS RESTORED.SDR ASAA2014070508457Eec · faultedWHILE PERF T/C 78273000 FOUND NR 1 ENG FAULT MSG 75-20371 "SHORT TIME" FAULT, HMU VSV CONTROL CURRENT OUT-OF-RANGE. ACFT GROUNDED. BASED ON FINDINGS: REPLACED AND TESTED NR 1 ENG EEC IAW MM 73-21-60-400-801-F00. TESTS PASSED, INCLUDING FIM REPAIR CONFIRMATISDR ASAA2014061108158Warning Light · illuminatedOVERHEAD ELECTRICAL LIGHT CAME ON AFTER GROUND POWER DROPPED OFF A COUPLE TIMES. ACFT GROUNDED. PERFORMED FIM 24-31, TASK 801, BITE SHOWS SPOOL FAULT BUT ELECTRICAL LIGHT REMAINS. PERFORMED FIM 24-34 TASK 801 FAULT CLEARED BITE SHOWS NO FAULT. ELECTRICAL LIGSDR ASAA2014061108157Warning Message · false activationDURING TAXI OUT, RECEIVED AN FMC DISAGREE MESSAGE. ACFT GROUNDED. PERFORMED QRH PROCEDURE. MESSAGE CLEARED.SDR ASAA2014060808102Connector · dirtyNR 2 ENGINE OVERHEAT ILLUMINATED. ACFT GROUNDED. BITE CHECKED ENGINE/APU FIRE DETECTOR MODULE, NO FAULTS LOGGED. GVI ENGINE AND DUCT, NO DEFECTS NOTED. INSPECTED FIRE/OVERHEAT DETECTOR CONNECTIONS. FOUND LOWER AFT GROUND CONNECTION DIRTY. CLEANED AND SECURSDR ASAA2014060107999Fire Detector · malfunctionedDURING NR 2 ENGINE START, OVERHEAT LIGHT ILLUMINATED EGT WAS NORMAL. OUTSIDE TEMP 100 DEGREE LIGHT WENT OUT ON SHUTDOWN, MOTORED ENGINE AND LIGHT CAME BACK ON. ACFT GROUNDED. PERFORMED ENG/APU FIRE DETECTION CONTROL MODULE BITE PROCEDURE NO FAULTS NOTED. REFSDR ASAA2014060107998Control Module · failedNR 2 ENGINE START, ENGINE OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. R & R FIRE-OVERHEAT CONTROL MODULE IAW FIM TASK 26-10-01-400-801. OPTS CK IAW FIM 26-11-00-710-801 & FIM TASK 26-15-00-701-801. OPTS CK OK.SDR ASAA2014042607572Satcom · malfunctionedSATCOM LOCKED UP ON GROUND. ACFT GROUNDED. QRH PROCEDURE ACCOMPLISHED. SATCOM PROMPT ON FMC MENU REGAINED.SDR ASAA2014042007550Satcom · malfunctionedSATCOM INOPERATIVE. ACFT GROUNDED. SATCOM PROMPT PRESENT ON MCDU. PERFORMED SATCOM COMMUNICATIONS TEST IAW AMM 23-15-00-730-801, ALL TESTS PASS. NO HISTORY LAST 30 DAYS.SDR ASAA2014041707494Warning Light · false activationAUTO FAIL AND ACTN LIGHTS ARE ILLUMINATED ON PRESSURIZATION PANEL. ACFT GROUNDED. CYCLED CONTROL SWITCH TO MANUAL AND BACK, LIGHTS WENT OUT. PERFORMED AUTO FAIL LIGHT ON FAULT ISOLATION IAW FIM 21-31, TASK 827 AND BITE TEST FIM 21-31, TASK 801. NO CURRENT FSDR ASAA2014031007127Drive Assy · failedRIGHT PACK LIGHT ILLUMINATED. ACFT GROUNDED. FOUND RT RAM AIR DOOR LINKAGE DRIVE AND ARM ASSY DEFECTIVE. R & R RT RAM AIR DOOR LINKAGE DRIVE AND ARM ASSY. OPS CK NORMAL REF AMM 21-51-22.SDR ASAA2014030807116Acoustic Panel · damagedFOUND NR 6 AFT ACOUSTICAL PANEL FWD INBD FASTENER ATTACHMENT DAMAGED. ACFT GROUNDED. INSTALLED NEW NR 6 AFT ACOUSTICAL PANEL ON NR 2 ENGINE IAW AMM TASK 72-23-02-400-801-F00.SDR ASAA2014030807115Panel · damagedNR 2 ENGINE INLET AND FAN BLADES, DETAIL INSPECTION FOUND NR 5 STRUT PANEL LT MIDDLE FASTENER ATTACHMENT DAMAGED. ACFT GROUNDED. R & R STRUT PANEL ON NR 2 ENGINE IAW AMM 72-23-07.SDR ASAA2014030507094Turbine Wheel · crackedNR 1 ENGINE REAR TURBINE AFT FLANGE ASSY INTERMEDIATE HOLES ARE CRACKED AT SEVERAL LOCATIONS. ACFT GROUNDED. REMOVED PLUG ASSY & AFT FLANGE ASSY, INSTALLED NEW AFT FLANGE ASSY IAW MM 72-56-00-400 3.F 2 & 3. REINSTALLED PLUG ASSY IAW MM 78-11-02-400.SDR ASAA2014030507093Turbine Wheel · crackedNR 2 ENGINE REAR TURBINE AFT FLANGE ASSY CRACKED AT SEVERAL LOCATIONS. ACFT GROUNDED. REMOVED PLUG ASSY & AFT FLANGE ASSY, INSTALLED NEW AFT FLANGE ASSY IAW MM 72-56-00-400, 3.F.2 & 3. REINSTALLED PLUG ASSY IAW MM 78-11-02-400.SDR ASAA2014030207052Button · malfunctionedON HF/SAT SELECT PANEL ON CENTER CONSOLE HF/SAT TRANSFER HF 1 SELECT BUTTON LIGHT INOPERATIVE. ACFT GROUNDED. PERFORMED MASTER DIM AND LIGHT TEST REF AMM 33-18-00-710-802 AND OPERATED HF/SAT TRANSFER 1 & 2 SELECTOR BUTTON OPS CHECK GOOD UNABLE TO DUPLICATE.SDR ASAA2014021706880Warning Light · illuminatedRIGHT PACK LIGHT ILLUMINATED. QRH PROCEDURE COMPLIED WITH. PACK LIGHT EXTINGUISHED ON RESET. NO OPS RESTORED. ACFT GROUNDED. BITE CHECKED RT PACK-ZONE TEMP CONTROLLER, NO FAULTS NOTED NO HISTORY PAST 30 DAYS. OK FOR SERVICE.SDR ASAA2014011112370Apu · malfunctionedAPU START SWITCH TO STRT EGT BEGAN TO RISE THEN APU FAULT LIGHT ILLUMINATED AND APU SHUTDOWN. ACFT GROUNDED. ACCOMPLISHED BITE CHECK, VERIFIED IN FAULT HISTORY MAINT MSG 49-41012. NO APU ROTATION SHUTDOWN. INSPECTED MAGNETIC DRAIN PLUG, NO CONTAMINATION NOTSDR ASAA2013122812252Circuit Breaker · trippedAT FL330, WINDSHIELD HEAT CIRCUIT BREAKER TRIPPED. OVERHEAT LIGHT FOR RT SIDE CAME ON. R2 WINDOW DID NOT FEEL OVERHEATED. CIRCUIT BREAKER ALSO DID NOT FEEL HOT. ACFT GROUNDED. INSPECTED CIRCUIT BREAKER, NO LOOSE CONNECTIONS OR DISCOLORATION FOUND. RESET CSDR ASAA2013121196871Warning Light · illuminatedRT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. PERFORMED QRH PROCEDURES AND OVERHEAT LIGHT ILLUMINATED IMMEDIATELY AFTER SWITCH HAD BEEN IN THE OFF POSITION FOR 5 MINUTES. IN CRUISE, FL400 FOR 3 HRS. SAT -66 DEGREES CENTIGRADE. ACFT GROUNDED. FOUND CIRCUIT BREASDR ASAA2013121196836Warning Light · false activationAFTER ENGINE START, LEFT PACK ANNUNCIATOR ILLUMINATED. ANNUNCIATOR EXTINGUISHED WHEN MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED PACK-ZONE TEMPERATURE CONTROLLER BITE PROCEDURE FOR NR 1 CONTROLLER, IAW FIM 21-62, TASK 801. TEST PASSED. NO FAULTS NOTED.SDR ASAA2013121196832Exciter · failedNR 1 ENGINE FAILED TO START, DUE TO NO FUEL FLOW. ENGINE VALVE CLOSED ANNUNCIATOR ILLUMINATED. ACFT GROUNDED. REPLACED LT EXCITER BOX IAW AMM 74-11-01. COMPLETED IGNITION SYS AUDIBLE TEST IAW 74-00-00. OPS CHECKED GOOD IAW AMM 74-11-01.SDR ASAA2013121096714Sensor · failedWHEN ENGAGING A AND B AUTOPILOT BOTH YOKES WOULD BUMP AND KICK 1 UNIT LT ON CONTROL WHEEL. ACFT GROUNDED. DFCS LAND VERIFIY GRP 49 FAILS TEST 49.35. DUAL TEST ALL POS FAIL, AIL POS SENSOR 1, MS622.11145. R & R AILERON POSITION SENSOR IAW MM 22-11-29 PERFORMSDR ASAA2013121096713Control Valve · failed15,000 FEET, DURING PACK HIGH FLOW INHIBIT TEST ON LT PACK WITH LT PACK OFF, FLAPS 1 SELECTED CABIN RATE F/O CLIMB DID NOT RATE UP. ACFT GROUNDED. R & R LT FLOW CONTROL VALVE IAW MM 21-51-01, PERFORMED OPS CHECK/LEAK TEST, CHECKED GOOD.SDR ASAA2013113096627Transition Panel · corrodedAFT CARGO TRANSITION PANEL CORRODED BS 727F-727I. ACFT GROUNDED. R & R TRANSITION PANEL IAW SRM 53-00-53-2R-5 AND 51-40-02.SDR ASAA2013113096621Channel · corrodedAFT PIT, RT TRANSITION PANEL CORRODED AROUND NUTPLATE HOLES STA 727D-727E. ACFT GROUNDED. R & R RT TRANSITION PANEL FROM STA. 727D-12 TO STA. 767 IAW SRM 53-00-53-2R-5 AND 51-40-02.SDR ASAA2013113096620Channel · corrodedAFT PIT, RT TRANSITION PANEL CORRODED AROUND NUTPLATE HOLES, STA 727I - 767. ACFT GROUNDED. R & R RT TRANSITION PANEL FROM STA 727D12 TO 767 IAW SRM 53-00-53-2R-5 AND 51-40-02.SDR ASAA2013113096618Transition Panel · puncturedAFT CARGO, LT TRANSITION PANEL C PUNCTURED, BS 727J. ACFT GROUNDED. R & R LT TRANSITION PANEL FROM STA 727-779 IAW SRM 53-00-53-2R-5 AND 51-40-02.SDR ASAA2013113096617Channel · corrodedAFT CARGO, LT TRANSITION PANEL CORRODED AROUND NUTPLATE HOLES, BS 747-787. ACFT GROUNDED. R & R LT TRANSITION PANEL FROM STA 727-779 IAW SRM 53-00-53-2R-5 AND 51-40-02.SDR ASAA2013113096616Channel · corrodedAFT CARGO, LT TRANSITION PANEL CORRODED AROUND NUTPLATE HOLES, STA 727G -727JG. ACFT GROUNDED. R & R LT TRANSITION PANEL FROM STA 727-779 IAW SRM 53-00-53-2R-5 AND 51-40-02.SDR ASAA2013113096615Channel · corrodedAFT CARGO, LT TRANSITION PANEL CORRODED AROUND NUTPLATE HOLES, STA 727A -727G. ACFT GROUNDED. R & R LT TRANSITION PANEL FROM STA 727-779 IAW SRM 53-00-53-2R-5 AND 51-40-02.SDR ASAA2013112996633Seat Track · crackedSEAT TRACK BS 727B, LBL 45.5 INBD FLANGE CRACKED. REPAIRED SEAT TRACK IAW REO-G16953, REV A AND EA 800-57EA-11748.SDR ASAA2013112396490Computer · failedSINGLE FMC OPERATION WITH F/O FLAGS. ACFT GROUNDED. VERIFIED NR 2 FMC FAILED REF AMM 23-61-00-710-801. REPLACED NR 2 FMC. ETOPS SIGNIFICANT SYS GROUND VERIFICATION COMPLETED SUCCESSFULLY, REF AMM 34-61-02.SDR ASAA2013112196489Computer · failedF/O FMC FAILED WITH WITH SINGLE FMC OPERATION MESSAGE IN FOS CDU SCRATCH PAD AND VTK AND MAP MESSAGE DISPLAYED ON FOS NAV MAP. CONDUCTED QRH CHECKLIST, UNABLE TO RESTORE. ACFT GROUNDED. REPLACED NR 2 FMC REF MM 34-61-02-400-801.SDR ASAA2013111696428Circuit Breaker · trippedAUTO THROTTLE INOPERATIVE CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. INSPECTED AND RESET AUTOTHROTTLE CIRCUIT BREAKER IAW MM 20-60-01. SWAPPED FCC A & B WITH NO CHANGE, PUT BACK TO ORIGINAL POSITION AND OPS CHECKED BOTH A & B. CHECKED GOOD IAW MM 22-11-33. ACSDR ASAA2013110996351Start Valve · failedDURING ATTEMPTED START OF NR 2 ENGINE, NEGATIVE ROTATION. ACFT GROUNDED. REPLACED NR 2 ENGINE START VALVE IAW AMM 80-11-03. START VALVE OPS CHECKS GOOD.SDR ASAA2013101896199Fire Loop · failedNR 2 FIRE WARNING SWITCH WILL NOT ILLUMINATE DURING FIRE PROTECTION SYS TEST, DURING PREFLIGHT. ACFT GROUNDED. REPLACED NR 2 ENGINE UPPER FAN LOOP, AMM 26-10-00. TESTS GOOD, AMM 26-11-00.SDR ASAA2013100696126Transceiver · malfunctionedSATCOM INOPERATIVE, NO CDU DISPLAY PAGES. ACFT GROUNDED. RESET SAT COMM TRANSCEIVER REF FIM 23-15 TASK 801 & GROUND VERIFICATION CK GOOD.SDR ASAA2013100396102Autopilot Sys · malfunctionedCHANNEL A AND B WHEN ENGAGING AUTOPILOT A LARGE CONTROL BUMP. ALL OTHER AUTOPILOT FUNCTIONS NORMAL. ACFT GROUNDED. PERFORMED PREV FLIGHT FAULT REVIEW, CURRENT STATUS & DFCS LAND VERIFY TEST ALL IAW AMM 22-11-00. ALL OPS NORMAL, NO DEFECTS NOTED. A/P A & B SDR ASAA2013092296036Valve · failedPRIOR TO DESCENT ENGINE ANTI-ICE TURNED ON AND OPERATED NORMALLY. WHEN THRUST REDUCED FOR DESCENT FROM FL 380, NR 2 ENG ANTI-ICE LT CAME ON BRIGHT BLUE. REMAINED ON UNTIL POWER ADVANCED AT 6,000 FT, THEN EXTINGUISHED FOR REST OF FLIGHT THROUGH LANDING. ACFTSDR ASAA2013092196030Warning Light · false activationNR 2 ENGINE ANTI-ICE COWL VALVE OPEN LIGHT STAYS BRIGHT WHEN ANTI-ICE ON. GOES OUT WHEN ANTI-ICE OFF. ACFT GROUNDED. PERFORMED OPS CHECK OF NR 2 ANTI-ICE COWL VALVE AND FOUND IT TO BE OPERATING NORMAL, NO DEFAULTS & NO HISTORY. PERFORMED OPS CHECK OF NR 1 ENSDR ASAA2013082295872Fmc · malfunctionedFMC DISAGREE FAULT, ACFT GROUNDED. RESET IAW QRH.SDR ASAA2013070895506Circuit Breaker · trippedON PREFLIGHT, BOTH PACK LIGHTS AND ALL 3 ZONE TEMP LIGHTS ARE ILLUMINATED. APU IS RUNNING AND SUPPLYING BLEED AIR. ACFT GROUNDED. FOUND CIRCUIT BREAKER HOT AND TRIPPED. INSPECTED BREAKER AREA, NO DEFECT NOTED. RESET CIRCUIT BREAKER IAW AMM 20-60-01. PFM DSDR ASAA2013070495473Fmc · false indicationFMC DISAGREE ANNUNCIATED DURING TAXI OUT. ACFT GROUNDED. NORMAL OPERATIONS RESTORED AFTER COMPLETION OF QRH PROCEDURE.
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