N560AS
Service difficulty reports · 562
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 = 'N560AS' 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 = 'N560AS' 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 ASAA2018101626513Warning System · false activationLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. GROUNDED - YES. FOLLOWED QRH PROCEDURE. LIGHT REMAINED EXTINGUISHED AFTER 4 MINUTE COOL DOWN. INFO NOTED BY MX. NO HISTORY WITHIN THE PAST 30 DAYS. A/C OK FOR SERVICE.SDR ASAA2018091526161Satcom · malfunctionedSATCOM VOICE APPEARS INOP. DATALINK STILL WORKS FINE. GROUNDED - YES. ACCOMPLISHED SATCOM COMMUNICATIONS SYSTEM TEST PER AMM 23-15-00-730-801, TEST PASSED.SDR ASAA2018090425989Unknown · malfunctionedON NUMEROUS OCCASIONS TRYING TO SEND OR RECEIVE MESSAGES ON THE ATC PORTION OF THE FMC WAS VERY SLOW OR UNABLE (POSSIBLE JUST SATCOM). GROUNDED - YES. ACCOMPLISHED LEFT FMC BITE REF FIM 34-61 TASK 801. FOUND PGM FAULT, AND ETHERNET FAULTS LOGGED. PERFORMED FIMSDR ASAA2018082425899Warning Light · false activationLEFT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED DURING CLIMB OUT, QRH PROCEDURE FOLLOWED, LIGHT OPS NORMAL. ACFT GROUNDED. AS PRECAUTION, ACCOMPLISHED A WINDOW HEAT CONTROL UNIT BITE IAW AMM 30-41-11, NO FAULTS FOUND.SDR ASAA2018062725225Seal · missingWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENG T/C 78472002, FOUND MISSING PLATFORM SEALS. GROUNDED - YES. REMOVED AND REPLACED ALL 24 FAN PLATFORMS ON NR 1 ENG (SN 894241) REF T/C 78472002.SDR ASAA2018061875088Bolt · wornDURING T/C 78472002 OF THE NR 2 ENGINE FRONT SPINNER CONE HAD SIX BOLT THREADS WORN. GROUNDED. REMOVED AND REPLACED THE BOLTS IAW AMM 72-21-01-400-801-F00.SDR ASAA2018060544915Fault Message · false activationPERFORMED FMC CDU CARD 78273000, THE NR 1 ENGINE HAD FAULT 73-20171, LONG TERM FAULT, INTERNAL EEC. ACFT GROUNDED. PERFORMED FIM 73-21, TASK 801, EEC TEST PASSED IAW AMM 73-21-00-700-804-F00, FAULT NO LONGER ACTIVE.SDR ASAA2018052824843Satcom · malfunctionedRECEIVE ONLY ON SAT-COM. NO XMIT ON ONE OR TWO BOTH CALLS OUT AND RECEIVED. GROUNDED - YES. ACCOMPLISHED SATCOM COMMUNICATION SYSTEM VOICE TEST ON BOTH SAT COM 1 AND 2. REFERENCE AMM 23-15-00. TRANSMIT AND RECEIVE VOICE QUALITY NORMAL AND CLEAR. NO HISTORY 30 SDR ASAA2018051924709Eec · faultedWHILE ACCOMPLISHING T/C 78273000 FOUND FAULT CODE 73-20171 INTERNAL EEC FAULT LONG TIME FAULT FOR NR 1 ENGINE. VERIFIED FAULT 73-20171 STILL CURRENT IAW FIM 73-21TASK 801. REPLACED THE NR 1 ENGINE EEC IAW AMM 73-21-60. GROUND VERIFICATION SUCCESSFUL IAW AMMSDR ASAA201805214659Warning Light · false activationON RECALL, THE LEFT PACK LIGHT ILLUMINATED, RESET WITH THE MASTER CAUTION. ACFT GROUNDED. RESET THE SYSTEM AND RAN PACKS FOR 15 MINUTES, RAN PACK/ZONE TEMP CONTROL BITE TEST IAW AMM 21-61-00-700-806-002. OPS CHECKED GOOD.SDR ASAA201804254367Fmc · malfunctionedDURING FLIGHT AT FL410, LOST BOTH FMC DISPLAYS VTK DISPLAYED ON CAPTAINS ND. MAP FLAG ALSO DISPLAYED ON CAPTAINS ND. AFTER APPROXIMATELY TWO MINUTES FMC'S RECOVERED AND DISPLAYS RETURNED TO NORMAL. ACFT GROUNDED. C/W FIM 34-61 TASK 804. FMC 1 & 2 BIT PASS REF SDR ASAA2018042224340O-Ring · leakingDURING PDC WALK, FOUND OIL LEAKING FROM THE NR 2 ENGINE. ACFT GROUNDED. FOUND OIL SEEPING FROM THE NR 2 ENGINE GEARBOX HAND CRANKING PAD COVER. REMOVED AND REPLACED THE O-RINGS FOR CRANKING COVER. LEAK CHECKED IAW AMM 71-00-00-800-811-F00, TEST 3A, AND AMM SDR ASAA2018042024328Circuit Breaker · openLEFT FORWARD WINDOW OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. FOUND THE CIRCUIT BREAKER FOR THE LEFT FWD WINDOW OPEN ON P6-11 PANEL. OPENED P6-11 PANEL &I NPSECTED THE CIRCUIT BREAKER. NO DEFECTS NOTED. CLOSED P6-11 PANEL. CLOSED THE CIRCUIT BREAKER. PERFORSDR ASAA2018033124096Battery Pack · failedBATTERY PACK FOR LEFT FORWARD OVERWING HATCH OUTSIDE EMERGENCY EXIT LIGHT FAILED. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK M2335 IAW AMM 33-51-06-960-805, AND OPS CHECKED GOOD IAW AMM 33-51-06-960-805 STEP 4D5.SDR ASAA2018031524015Floorbeam · crackedFLOOR SUPPORT FROM BL0 TO LBL24 STA 540 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 BL0 TO LBL24 IAW SRM 51 40 02 0G 0.SDR ASAA2018030724077Door Frame · corrodedL1 DOOR FWD LOWER FRAME AT BS 303 HAS CORROSION AT FLOOR LEVEL. ACFT GROUNDED. REPAIRED THE DOOR FRAME IAW EA 53EA 20029.SDR ASAA2018030723991Floor Support · corrodedAFT WET AREA FLOOR SUPPORT STA 947.5 LBL 25 TO 45 HAS AREAS OF CORR. GROUNDED - YES. REMOVED CORR ON AFT WET AREA FLOOR SUPPORT STA 947.5 LBL 25 TO 45, OUT OF LIMITS IAW SRM 53 70 51 1A 1. INSTALLATION ACCOMPLISHED ON MIG5 S/N OK74070 WO 1015401 - 2000 0024 W SDR ASAA2018030723989Door Sill · corrodedL1 DOOR MOP SILL HAS CORR FOUND ACCESSING 303 FRAME. GROUNDED - YES. REMOVED CORR ON L1 DOOR MOP SILL OUT OF LIMITS, REMOVED AND INSTALLED NEW MOPSILL IAW SRM 51 40 02 0G 0, 53 10 15 1A 1 W 1 O .090 R 0 L 4 D .090.SDR ASAA2018030723988Floorbeam · corrodedAFT WET AREA 947 FLOORBEAM UPPER CAP HAS AREAS OF CORR FROM LBL 25 RB 45. GROUNDED - YES. REPAIRED BEAM UPPER CAP IAW SRM 53 70 51 2R 5 REPAIR 5 W .5 O .180 R .0 L 0 D .180.SDR ASAA2018030723897Floor Support · crackedFWD WET AREA FLOOR SUPPORT BS 312 - 328, LBL 48 CRACKED AT FASTENER HOLE. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, FIG 6, STEP D6.SDR ASAA2018030723895Floor Support · crackedFWD WET AREA FLOOR SUPPORT AT BS 312 - 328, RBL 40 CRACKED AT FASTENER HOLE. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, FIG 6, STEP D6.SDR ASAA2018030523987Frame Splice · corrodedAFT CARGO COMP LOWER FRAME SPLICE IS CORRODED AT STA 727H ABOVE 25R. GROUNDED - YES. REMOVED AND REPLACED SPLICE IAW SRM 51 40 02 0G 0 W 1 O .071 R 0 L .5 D .071.SDR ASAA2018030523985Web · corrodedAFT CARGO COMP WEB AT DOOR ENTRY HAS CORROSION. GROUNDED - YES. BLENDED AFT CARGO COMP WEB AT DOOR ENTRY, OUT OF LIMITS, REMOVED AND INSTALLED NEW WEB IAW SRM 51 40 02 0G 02, 53 60 15 1A 1 W 1 O .045 R .039 L 3 D .006.SDR ASAA2018030523968Frame Splice · corrodedAFT CARGO BAY LOWER FRAME SPLICE IS CORRODED AT BS 7271 ABOVE STRINGER 25R. ACFT GROUNDED. REMOVED AND REPLACED THE FRAME SPLICE IAW SRM 51-40-02-0G.SDR ASAA2018030424054Battery Pack · no testRIGHT AFT EMERGENCY LIGHT FAILED A CHECK. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-06-960-806.SDR ASAA2018030424053Battery Pack · failedLEFT AFT ENTRY EMERGENCY LIGHT BATTERY FAILED A CHECK. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-06-960-806.SDR ASAA2018022423667Actuator · faultedAT TOP OF DESCENT ON MASTER CAUTION RECALL, SAW MASTER CAUTION AND RIGHT PACK LIGHT. LIGHT EXTINGUISHED WHEN CANCELLING MASTER CAUTION. ACFT GROUNDED. REMOVED AND REPLACED THE RT RAM AIR EXHAUST ACTUATOR IAW AMM 21-51-21, STILL FAULTY. CHECKED FOR POWER SDR ASAA2018022123649Warning Light · false activationDURING DESCENT BELOW 10,000 FT, RIGHT PACK LIGHT ILLUMINATED. PACK LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED A PACK TEMP CONTROL BITE CHECK IAW FIM 21-62, 801. BITE CHECKED GOOD, GO ON ALL PHASES OF BITE, NO FAULTS NOTED ON RIGHSDR ASAA2018020723460Warning Light · false activationPRIOR TO DESCENT PUSHED MASTER CAUTION RECALL & THE PACK LIGHT ILLUMINATED. RAN QRH PROCEDURES, & THE LIGHT EXTINGUISHED. ACFT GROUNDED. PERFORMED A PACK TEMP CONTROL BITE CHECK IAW FIM 21-62 TASK 801. FOUND THE LEFT RAM AIR ACTUATOR LIGHT ILLUMINATED ON BSDR ASAA2018013123368Warning Light · false activationRT PACK LIGHT ILLUMINATED ON TOUCHDOWN. GOES OUT WHEN M/C IS RESET. ACFT GROUNDED. PERFORMED A PACK TEMP CONTROL BITE IAW FIM 21-62, TASK 801. RAM AIR ACTUATOR SHOWED ON BITE AND PREVIOUS FLT, VERIFY GO,. AFTER RESET, RAN BITE TWICE MORE, ALL GO. INTERMITTENSDR ASAA2018010823101Display · abnormalYELLOW FD FLAG ON CAPTAIN`S PFD. ACFT GROUNDED. ACCOMPLISHED DFCS BITE IAW AMM 22-11-00. NO FAULTS FOUND. PERFORMED DFCS OPS TEST IAW AMM 22-11-00. SYS CHECKED NORMAL. CYCLED FCC A CIRCUIT BREAKER. RETURNED TO NORMAL. ACCOMPLISHED FCC A OPS TEST IAW AMSDR ASAA2017122122977Warning Light · false activationLEFT PACK LIGHT ILLUMINATED. COMPLIED WITH QRH PROCEDURES, TURNED LEFT PACK OFF. ACFT GROUNDED. ACCOMPLISHED FIM 21-53, TASK 801. INITIAL EVALUATION SHOWS AN INTERMITTENT FAULT, ACCOMPLISHED TEMP CONTROLLER NR 1 PACK BITE TEST IAW AMM 21-51-00. NO FAULTS NSDR ASAA2017121722929Probe · failedDURING ETOPS PDC WALK AROUND FOUND TAT PROBE BURNED AND CRACKED. GROUNDED - YES. REPLACED TAT PROBE, OPS NORMAL REF B737-800 AMM 34-21-06-400-801 AND 30-31-00-730-801.SDR ASAA2017121322888Elastomer · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON #2 ENGINE FOUND ALL STOP ELASTOMERS WORN ON SPINNER REAR CONE. GROUNDED - YES. REPLACED ALL STOP ELASTOMERS ON SPINNER REAR CONE REF IPC 72-21-00 & TASK CARD 78472002.SDR ASAA2017121322884Drain Mast · crackedWHILE ACCOMPLISHING APU DRAIN MAST INSP PER T/C NG-28FCD-18312-1, FOUND MAST CRACKED. GROUNDED - YES. REMOVED AND REPLACED APU FUEL FEED LINE SHROUD DRAIN MAST, REF B737-800 AMM 28-25-07.SDR ASAA2017120522788Shim · damaged#1 ENG ALL BLADE SHIMS HAS MOLYDAG COATING LOSS MORE THAN 25% NO WEAR TO BASE MATERIAL, #1 BLADE SHIM HAS A CRACK AND AXIAL RETENTION DISTORTION, AND BLADE SHIMS #2, #14, #16 HAS AXIAL RETENTION DISTORTION. REF B737-800AMM 72-21-02-200-801 STEP 2L. GROUNDED -SDR ASAA2017120422771Fuel Nozzle · malfunctionedAPU CT5ATP EGT TREND DATA SHOWS EGT HAS SHIFTED ABOVE THE MAINTENANCE THRESHOLD OF 593 GROUNDED - YES. REMOVED AND REPLACED 10 EA APU FUEL NOZZLES AND SHROUDS, OPS AND LEAK CHECKED GOOD REF B737-800 AMM 49-31-14.SDR ASAA2017112522694Starter · failedNO ROTATION ON NR 2 STARTER. ACFT GROUNDED. REMOVED & REPLACED THE NR 2 STARTER IAW AMM 80-11-01-000-801-F00, & 80-11-01-400-801-F00. OPS & LEAK CHECKED GOOD.SDR ASAA2017110622460Lens · missingEMERGENCY EXIT SIGN AT THE L2 DOOR IS MISSING THE LENS. ACFT GROUNDED. REPLACED THE LENS AND TESTED IAW AMM 33-51-01-960-801. OPS NORMAL.SDR ASAA2017103022363Pump · failedDURING LEVEL FLIGHT AT 37000 FEET, WITH 1300 POUNDS OF FUEL IN CENTER TANK, TURNED ON LEFT CENTER FUEL PUMP, THEN TURNED ON THE RIGHT CENTER FUEL PUMP. LEFT PUMP LOW PRESSURE LIGHT EXTINGUISHED QUICKLY. RIGHT CENTER TANK PUMP LOW PRESSURE REMAINED ILLUMINATEDSDR ASAA2017100422112Controller · failedLEFT FWD WINDOW OVERHEAT. COMPLIED WITH QRH. LIGHT REMAINED ILLUMINATED. ACFT GROUNDED. FOUND THE CIRCUIT BREAKER C228 TRIPPED. OPENED THE CIRCUIT BREAKER PANEL AND FOUND TERMINALS DISCOLORED. REPLACED THE TERMINALS AND CIRCUIT BREAKER IAW SWPM 20-30-11. SDR ASAA2017093022084Circuit Breaker · openLEFT FWD WINDOW HEAT, OVERHEAT LIGHT CAME ON, COMLIED WITH QRH. THE LIGHT ILLUMINATED AGAIN IMMEDIATELY WHEN SWITCH WAS TURNED BACK ON IAW THE QRH. ACFT GROUNDED. FOUND THE WINDOW HEAT POWER LEFT FRONT CIRCUIT BREAKER OUT ON THE P6-11 PANEL. ACCOMPLISHED SDR ASAA2017092922092Igniter · damagedNR 2 ENGINE SPAR VALVE DIDN'T OPEN. ACFT GROUNDED. VERIFIED OPERATION OF THE NR 2 ENGINE SPAR VALVE IAW AMM 28-22-00-701-801, PAR 4 C, STEP 4. TROUBLESHOT TO THE RIGHT IGNITION INOPERATIVE ON NR 2 ENGINE. REPLACED THE NR 2 ENGINE RT EXCITER BOX IAW AMM 74SDR ASAA2017080721568Wire Harness · failedOVERHEAT, FIRE TEST FOR THE NR 2 ENGINE B LOOP FAILED. ACFT GROUNDED. ACCOMPLISHED FIM 26-10-805. NO FAULTS. REMOVED AND REPLACED THE NR 2 DETECTORS IAW AMM 26-11-01, REMOVED AND REPLACED THE CORE HARNESS IAW AMM 26-11-02. DETECTORS AND CORE HARNESS OPS CHESDR ASAA2017080421536Fire Detector · faultedWHILE ACCOMPLISHING ENGINE/APU FIRE DETECTION CONTROL MODULE BITE TEST. NR 2 ENGINE FAULTED UPPER FAN B LOOP. ACFT GROUNDED. REMOVED AND REPLACED NR 2 ENGINE UPPER FAN FIRE DETECTOR ASSEMBLY IAW AMM 26-11-01. GROUND VERIFICATION TEST PASSED IAW AMM 26-11-00-7SDR ASAA2017072221438Fire Loop · malfunctionedNUMBER 2 ENGINE FIRE-OVERHEAT TEST FAILED IN LOOP B TEST OK IN LOOP A. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT. WITH NR 2 ENGINE LOOP SELECT SWITCH SET TO BOTH, ENGINE FIRE DETECTION, OPS TESTED IAW AMM 26-11-00-710-801 PASSED WITH NO FAULTS. OPENED THE SDR ASAA2017071821422Fmc · malfunctionedDURING TAXI TO THE GATE, LEFT FMC FAILED. INTERMITTENTLY CYCLES ON/OFF IN THE MCDU. ACFT GROUNDED. ACCOMPLISHED FMC BITE IAW FIM 34-61-TSK 801. OPS CHECKED NORMAL, NO FAULTS IAW AMM 34-61-00.SDR ASAA2017070421266Pump · leakingNR 1 ENGINE FUEL PUMP DRAIN AT GEARBOX LEAKING 40 DROPS PER MINUTE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP IAW AMM 73-11-01.SDR ASAA2017062021143Idg · failedAFTER BOTH ENGINES STARTED, ATTEMPTED TO PUT THE NR 1 GENERATOR ONLINE, BUT IT WOULD NOT GO ONLINE. JUST BLUE GEN OFF BUSS LIGHT REMAIN ILLUMINATED. THE NR 1 GEN SHOWED ZERO AMPS AND ZERO VOLTS. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 IDG IAW AMM 24-11SDR ASAA2017061721111Fmc · malfunctionedDUAL FMC FAILURE ON LANDING, DATA DUMPED, BUT FMC'S CAME BACK. ACFT GROUNDED. REBOOTED FMC IAW FIM 34-61, TASK 804, OPS CHECKED OK.
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