N562AS
Service difficulty reports · 600
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 = 'N562AS' 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 = 'N562AS' 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 ASAA1058588Unknown · malfunctionedON TAXI OUT FMC DISAGREE ANNUNCIATED. COMPLETED CMPTR1/CMPTR2 CB PULLED TIMED AND RESET AS PER QRH MESSAGE EXTINGUISHED.SDR ASAA1058518Warning System · intermittentCONT CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL. CONFIRMED. BITE CHECK OF NR 2 CTRLR SHOWS FLT DECK TRIM VALVE FAULT LAST FLT. RESET FAULT. BITE TEST NR 1 AND NR 2 CTRLR'S GOOD. FAULT DID NOT RETURN. INTERMITTENT FAULT. FUNCT CHECK FLT DECK TRIM VALVE GOSDR ASAA1058497Cover · tornON WALKAROUND OBSERVED TORN HF ANTENNA COVERING AT BASE OF RUDDER. FOUND BMS10 21 TYPE II MISSING IN SEVERAL SMALL PLACES. INSPECTED ANTENNA FOUND NO DAMAGE TO FIGERGLASS COMPOSITE STRUCTURE. APPLIED POLYUREATHANE PROTECTIVE TAPE TO AREA AND SEALED AS PER ASDR ASAA1058479Fmc · failedRT FMC FAIL MESSAGE, DISPLAYED ON GROUND IN ANC RAN CHECKLIST MESSAGE DID NOT CLEAR. CONFIRMED RT FMC IS INOP. VERIFIED FMC P/N 176200 05 01WITH SEAMC. REPLACED RT FMC WITH SERVICABLE ONE. ACCOMPLISHED SOFTWARE CROSSLOAD FROM LT TO RT. VERIFIED SOFTWARE CSDR ASAA1058480Unknown · malfunctionedFMC DISAGREE WARNING. PERFORMED QRH PROCEDURES, OPS OK.SDR ASAA1058459Warning System · false activationFMC DISAGREE LIGHTS ILLUMINATED ON GROUND. QRH PROCEDURE PERFORMED. ACCOMPLISHED FMC BITE BOTH SYSTEMS OK.SDR ASAA1058363Filter · defectiveFOUND APU LUBE MODULE DPI EXTENDED. ACCOMP OIL FILTER IND SERVICING REF M/M 49 91 13 600 801. REMOVED & REPLACED LUBE FILTER ELEMENT LK & OPS NORMAL REF M/M 49 91 12 400 802. ACCOMP MAG DRAIN PLUG INSP NO DEFECTS NOTED REF M/M 49 91 81 200 801. RESET DPI OSDR ASAA1058337Detector · failedAPU DET INOP LIGHT ON. REPLACED APU OVERHEAT DETECTOR M1925 IAW AMM 26 15 01 PAGE BLOCK 401. APU FIRE DETECTION OPS TEST NORMAL.SDR ASAA1058307Wire Harness · chafedFOUND DP1102 BACKSHELL LOOSE AND CHAFING WIRES (NR 1 ENGINE). REPLACED MW0311 HARNESS ASSY REF MM 73 21 06 000 802 F00 & MM 73 21 06 400 802 F00. ALL OPS CHECKS GOOD REF SAME. WORK ACCOMPLISHED ON NR 1 ENGINE.SDR ASAA1058298Regulator · malfunctionedON CLIMBOUT DUCT PRESSURE SPLIT WITH LEFT FLUCTUATION 10 PSI. AT 6000' N1'S LT /89.6 RT /89.6 DUCT PRES L 42 TO 50 PSI / R 30 PSI. FLUCTUATION STABILIZED 8-10 THOUSAND FT WITH ONLY SMALL SPLIT. CRUISE TO TOD APPROX 8-10 PSI SPLIT. AT IDLE DESCENT 1-2 PSI SSDR ASAA1058289Transceiver · malfunctionedACARS "NO COMM" FOR 3 PLUS HOURS. APPEARS THAT HF PORTION IS INOPERATIVE. PERFORMED HF LINK TEST IAW MM 23 27 00 730 803 004 PARAGRAPH D.8. CONFIRMED FAILURE OF HF2 DATA PORTION OF SYSTEM (HF1 WORKS IAW AMM PROCEDURE). REMOVED AND REPLACED HF2 TRANSCEIVER SDR ASAA1058238Switch · failedAFTER ENGINE START THE ENGINE NR 1 BLUE ENG VALVE CLOSED LIGHT STAYED BRIGHT BLUE. REPLACED NR 1 ENG HPSOV SWITCH REF MM 73 21 09/201. PERFORMED REPAIR CONFORMATION PER FIM 73 06 00 810 805 F00 LIGHT OPERATES. NORMALLY.SDR ASAA1058158Bonding Strap · looseAPPROX HALF WAY INTO T/O ROLL NR 1 ENG WAS CYCLING .5 PERCENT. DURING CLIMBOUT CYCLING INCREASED TO 3 TO 4 PERCENT MOSTLY LESS THAN THE COMMANDED POSITION. ALL ENGINE INSTRUMENTS WERE FOLLOWING ENGINE CYCLING AND THE N1 COMMAND SECTOR WAS RAPIDLY SHOWING THESDR ASAA1058123Warning System · malfunctionedAT LEVEL OFF FL 380 NOTICED LEFT ENG VALVE CLOSED LIGHT ILLUM DIM. NO OTHER DISCREPANCIES NOTED. ENG OPERATING 4.0 HARD TO SEA ON LTS TEST OR PRESS TO TEST ANY BRIGHTER ILLUM LOOKED UP IMMEDIATELY AFTER SENDING ACARS TO MAINT CTRL AND NOTED LIGHT EXTINGUISHESDR ASAA1058099Unknown · malfunctionedWEATHER RADAR STAB OUT OF TOLERANCE (ON DEPT TILT 11 DEGREES UP GROUND CLUTTER ENTIRE SCREEN UNTIL FL200) TRIED DIFFERENT TILT SELECTIONS TO NO AVAIL. CANNOT DUPLICATE ON GROUND IN SEA. GROUND VERIFICATION AND SYSTEM OPERATION NORMAL PER MM 34 43 00 SYSTEM TSDR ASAA1058052Inlet Bullet · out of limitsWHILE PERFORMING TC 78472000 ENG INLET & FAN BLADES DETAILED INSPECTION FOUND FORWARD SPINNER CONE OUT OF LIMITS. REMOVED AND REPLACED NR 2 FORWARD SPINNER CONE REF MM 72 21 01.SDR ASAA1058018Actuator · out of adjustRIGHT RAM AIR DOOR DEFLECTOR OUT OF RIG. RE-ADJUSTED RAM AIR INLET ACTUATOR AND RIG CHECKS NORMAL. RIGHT RAM AIR INLET DOOR OPS CHECKS NORMAL, REF M/M 21 51 21 400 801.SDR ASAA1058004Switch · failedNR 1 ENGINE "VALVE CLOSED LIGHT" REMAINS ILLUMINATED BRIGHT AFTER ENGINE START. REMOVED AND REPLACED NR 1 ENG HIGH PRESSURE SHUT OFF VALVE SWITCH ON NR 1 ENG HMU. REF MM 73 21 09 400 801 F00. PERFORMED NR 1 ENG RUN OP CK GOOD.SDR ASAA1057999Signal Cond Unit · faultyNR 2 ENGINE VIBRATION INDICATION DISAPPEARED INTERMITTENTLY DURING FLIGHT. PERFORMED FIM 77 05 00 810 805. BITE TESTED AVM REF FIM 77 31 00 810 801. SELF TEST SHOWS NO FAULTS. FAULT HISTORY HAS MULTIPLE FAULT NR 46. DIRECTS TO FIM 77 31 TASK 803 INDICATESSDR ASAA1057919Warning Light · illuminatedNR 1 CSD DRIVE LIGHT REMAINS OFF AFTER SHUTDOWN. PERFORMED OPERATIONAL TEST OF NR 1 IDG RAN ENGINE SYSTEM OPS NORMAL PER AMM 24 21 00.SDR ASAA1057694Circuit Breaker · poppedHF NR 1 CIRCUIT BREAKER POPPED. CHECKED BEHIND P18 2 PANEL FOR CONTAMINATION OR DEFECTS NONE NOTED. RESET C/B REF SWPM 20 60 01. ACCOMPLISHED GROUND VERIFICATION REF MM 23 11 21, OPS NORMAL.SDR ASAA1057588Apu · making metalAPU FAULT LIGHT ILLUMINATED AFTER LOAD APPLIED TO APU. PERFORMED APU BITE TEST. MAINT MSG 49 94299 STARTER GEN OIL FILTER CLOGGED. FOUND METAL PARTICLES FROM MAGNETIC DRAIN PLUG. REPLACED APU FER T/C 78349010 AND MM 49 11 00 400 802.SDR ASAA1057500Ram Air Door · malfunctionedFOUND RT RAM AIR DEFLECTOR DOOR INOP. SYSTEM CHECKS GOOD IAW MM 21 51 21 400 801 UNABLE TO VERIFY FAULT. RAN DEFLECTOR DOOR UP AND DOWN SEVERAL TIMES NO FAULTS ON NR 1 OR NR 2 TEMP CONTROLLERS AND BOTH "VERIFY" TESTS PASS. NO HISTORY LAST 90 DAYS.SDR ASAA1057494Unknown · malfunctionedAFTER ENGINE START NR 1 ENG VALVE CLOSED FUEL VALVE LIGHT REMAINED ILLUMINATED ALL ENGINE PARAMETERS & OPERATION NORMAL. SHUT POWER DOWN, TURN A/C POWER ON. NO FAULT NOTED ON FMC/CDU. RUN EEC TEST NO FAULTS NOTED REF AMM 73 00 00. PERFORMED SUCCESSFUL GROUSDR ASAA1057356Skin · damagedFWD ENTRY DOOR STA 345 UPPER AFT CORNER (BELOW UPPER GATE) SKIN DAMAGED. CUT OUT DAMAGED SKIN & INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 52 00 01 REPAIR 2.SDR ASAA1057186Cdu · malfunctionedTHE 1R BUTTON ON F/O'S CDU/FMC IS INTERMITTENT. REMOVED & REPLACED NR 2 MCDU. OP CHECK NORMAL. REF MM 34 61 01 000 802 & 3461 01 400 802.SDR ASAA1057192Engine · malfunctionedNR 1 ENGINE HAS FAULT 76 31361, THE START LEVER SIGNALS DISAGREE. GROUNDED ACFT. CURRENTLY FAULT SHOWS UP ON LEG 2 AND LEG 6 ONLY. REQUIRES CONTROL STAND DISASSEMBLY FOR TROUBLESHOOTING NO TIME TO PERFORM WILL REQUIRE HANGAR TIME. DEFERRED FOR 450 HOURS. NO FSDR ASAA0957143Unknown · malfunctionedFOUND LONG TERM FAULT MSG 76 31361 START LEVER SIGNAL DISAGREE LEG 1 ENG NR 1. FFR SHOWS 2 FAULTS NR 1 ENGINE MSG 76 31361. ACCOMPLISHED FIM TASK 76 11 00 & INPUT MONITORING DISCRETES TESTS ON NR 1 START LEVER SEL POS SW DEU1 DEU2 GROUND VERIFICATION TEST OPSDR ASAA0956955Fmc · malfunctionedAFTER POWER UP NR 2 FMC DISPLAY FLASHED FROM DIM TO BRIGHT FOR ABOUT 10 MIN UNTIL AIRCRAFT HIT SOME BUMPS ON THE TAXIWAY. AFTER WHICH THE DISPLAY DID NOT FLASH. NO PREVIOUS HISTORY LAST 60 DAYS. GROUND VERIFICATION CHECKS OF FMC & CDU TEST NORMAL REF AMM 34SDR ASAA0956652Vapor Barrier · crackedREFERENCE DEFECT 6190500T (RT WHEEL WELL FOUND 4 INCH CRACK IN VAPOR BARRIER) PERFORM REPAIR OF VAPOR BARRIER. REPAIRED CRACK IN VAPOR BARRIER AT RT WHEEL WELL IAW SRM 51 70 04 REPAIR 10.SDR ASAA0956626Actuator · out of rigRIGHT RAM AIR MODULATING SYSTEM INLET DOOR APPEARS OUT OF RIG. DOOR CAN BE PUSHED IN BY HAND. RIGGED & ADJUSTED RT RAM AIR DOOR ACTUATOR SYSTEM. RAM AIR SYSTEM OPS CHECK NORMAL REF 21 51 22.SDR ASAA0956515Warning System · malfunctioned"AUTO FAIL" LIGHT ILLUMINATED. VERIFIED PROBLEM. RAN BITE OF CONTROLLER. AUTO FAIL FAULT CLEARED REF AMM 21 31 00 810 806. CONFIRMED OPS CHECK NORMAL. SEAMC ETOPS DESK NOTIFIED.SDR ASAA0956497Gasket · leakingNR 1 ENG FOUND TO BE LEAKING FUEL DURING OIL SERVICING. FOUND HMU FUEL TUBE LEAKING AT GASKET, REPLACED HMU FUEL TUBE GASKET NR 34 REF MM 73 21 10. SECURED, OPS CHECK GOOD. NO LEAKS NOTED. SEAMC NOTIFIED.SDR ASAA0956431Precooler · failedDURING CLIMB AT 100.7 PERCENT NI DUCT SPLIT OF 18 PSI LEFT 17 RIGHT 35. IN CRUISE AT 41,000FT AT 88.5 PERCENT NI LEFT DUCT 16 RIGHT DUCT 34 PSI AGAIN 18 PSI SPLIT. NO CROSSOVER NOTED ON NR 1 ENGINE DURING HIGH STAGE CROSSOVER CHECK. PERFORMED ENG BLEED AIR SDR ASAA0956415Support Angle · crackedCRACKED SEAL SUPPORT ANGLE RT WING TRAILING EDGE PANEL. REMOVED AND REPLACED SEAL SUPPORT ANGLE.SDR ASAA0956414Support · crackedSEAL SUPPORT CRACKED AT L/N FIXED UPPER T/E PANEL BETWEEN NR 5 AND NR 6 SPOILER. REMOVED WEB, REPLACED SEAL SUPPORT AND RE-INSTALLED WEB PER SRM.SDR ASAA0956392Support Channel · gougedE&E DOOR CUTOUT AFT LATCH SUPPORT CHANNEL IS GOUGED. REMOVED AND REPLACED SUPPORT CHANNEL.SDR ASAA0956382Engine · oil consumptionPER SEAMC NR 1 ENG OIL CONSUMPTION IS AT .63. THIS EXCEEDS ETOPS LIMITS. ACCOMP NR 1 ENG GVI FOR OIL LEAKS REF AMM 71 71 00. NO LEAKS NOTED. A/C RESTRICTED FROM ETOPS FLIGHT UNTIL OIL FALLS BELOW .600 QPH. SEAMC NOTIFIED. PER SEAMC NR 1 ENG OIL CONSUMP HASDR ASAA0956381Charger · faultedDURING AFTER START FLOW THE 'BAT DISCHARGE' LIGHT BLINKED ON THEN OFF. UPON SELECTING BAT THE VOLTS READ 27 AND THE AMPS READ 5. OVER THE NEXT 3 MINS THE AMPS DECREASED TO 2. THE STBY PWR SWITCH WAS THEN SELECTED TO BAT STBY PWR WAS NORMAL. THE STBY PWR SWSDR ASAA0956379Inverter · inoperativeELEC LIGHT ILLUMINATED ON OVERHEAD PANEL. VERIFIED STATIC INVERTER INOP. CYCLED INVERTER REMOTE C/B STATIC INVERTER OPS NML REF TASK 24 34 21 400 801. NO HISTORY 60 DAYS. VERIFICATION FLIGHT SUCCESSFUL.SDR ASAA0956288Engine · oil consumptionPER SEAMC, AIRCRAFT RESTRICTED FROM ETOPS SERVICE DUE TO OIL CONSUMPTION RATE ON NR 2 ENG AT .62. ABOVE ETOPS LIMITS. PER SEAMC, ENG OIL CONSUMPTION RETURN TO .17 WITHIN ETOPS LEVEL. ACFT RETURN TO ETOPS SERVICE.SDR ASAA0956188Transceiver · defectiveWX RADAR HAS A "SLICING" EFFECT ON RADAR SCREEN, LOOKS LIKE SEVERAL PIECES OF PIZZA SLICES. WX+T MODE ALSO HAS THE SAME PROBLEM. COULD NOT VERIFY DEFECT ON GROUND. REMOVED & REPLACED WX RADAR RT REF MM 34 43 41. ADM PITOT QD REQ'S INSPECTION. INSPECTED ADSDR ASAA0956183A/C Pack · malfunctionedDURING GROUND AND CLIMB OPS WITH APU OR ENGINE PWR ABOVE IDLE THE T PACK OPERATES VERY LOUD WITH VERY HIGH AIR FLOW.(THIS IS THE AIRFLOW ON THE FLIGHT DECK THE PACK SOUNDS NORMAL FROM OUTSIDE) WHEN OPERATING LT PACK AND RT TOGETHER IT IS VERY LOUD. WHEN LT PASDR ASAA0956126Fan Blade · nickedWHILE ACCOMPLISHING TC 78472002, NR 2 ENG FAN LUBE ESN 894 258. FOUND 5 EA PN 340 001 814 AND 1 EA PN 340 001 816 PLATFORMS WITH NICKS AT FWD LUG FACE GREATER THAN .008 INCH GROUNDED YES. REPLACED 6 EA DAMAGED PLATFORMS WITH NEW PLATFORMS PN 340 001 816 REF. SDR ASAA0956125Shim · wornWHILE ACCOMPLISHING FAN LUBE TC 78472002 NR 2 ENG SN 894 258 FOUND EXCESS MOLYDAG COATING WORN ON ALL 24 SHIMS. REF STEP 56 ON TC GROUNDED YES. REMOVED 24 EACH FAN BLADE SHIMS PN 340 252 306 0 AND INSTALLED 24 EACH NEW SHIMS PN 340 252 307 0. REF TC 78472002 SDR ASAA0955925Idg · defectiveNR 1 ENG IDG OIL LEVEL LOW. ELECTED TO CHANGE NR 1 IDG DUE TO EXCESS HISTORY OF SERVICING PER MM 24 11 00 700 AND 24 11 11 400.SDR ASAA0955878Converter · failedBLUE "MAINT" LIGHT ILLUMINATED WHEN APU WAS STARTED. FOUND CODE 49 41244 IN CDU. ACCOMPLISHED FIM TASK 49 40 00 810 806 THRU F2E. REMOVED & REPLACED STARTER GENERATOR PER AMM 49 41 21. NO HELP FAULT CODE STILL PRESENT. REQUIRES START CONVERTER UNIT. MAINSDR ASAA0955814Circuit Breaker · trippedRIGHT FORWARD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. WINDOW IS COOL. ACCOMPLISHED QRH PROCEDURE. OVERHEAT LIGHT REMAINS ON. CHECKED, NO HISTORY. FOUND RT FRONT AC WINDOW HEAT TRL C/B OUT. RESET SAME REF MM 20 60 01. OPS CHECK R1 WINDOW HEAT GOOD. REF SDR ASAA0752058Bearing · migratedDURING DAILY CHECK, FOUND NLG RETRACT ACTUATOR ATTACH LUG BEARING MIGRATION LEFT OF CENTER OUT OF LIMITS REF EA 3230 01055. STEP 1 BEARING MIGRATION MEASURES .155 LEFT OF CENTER. PREVIOUSLY ON DEFERRAL REF L P 6264563. BEARING MIGRATION CONDITION WAS REPAIRSDR ASAA0651311Lens · meltedFWD GALLEY FLASHLIGHT INOP FLASHLIGHT DIFFICULT TO REMOVE. FOUND FLASHLIGHT LENS MELTED TO BASE UNIT. REPLACED FWD FLASHLIGHT ASSY. OP CHECKS OK.
Back to N562AS