N559AS
Service difficulty reports · 540
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 = 'N559AS' 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 = 'N559AS' 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 ASAA2017102222276Blade · wornWHILE ACCOMPLISHING TC 78472002 ON THE NR2 ENGINE, FOUND THE FAN BLADES 18 & 22 COATING OUT OF LIMITS IAW AMM 72-21-02. ACFT GROUNDED. REPLACED THE FAN BLADES 18 AND 22, WELL AS 180 DEGREES OPPOSITE 6 AND 10 IAW AMM 72-21-02-000-802-F00.SDR ASAA2017101422198Terminal · brokenAPU FIRE DETECTOR LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED FIM 26-10, TASK 802. FOUND TERMINAL LUG STUD BROKEN. REMOVED AND REPLACED APU TAILPIPE OVHT DETECTOR IAW AMM 26-15-01-000-802, AND AMM 26-15-01-400-802. OPS CHECKED NORMAL. SUCCESSFUL GROUND VERSDR ASAA2017092822068Wire · damagedOVERHEAT, FIRE TEST SWITCH WHEN PUSHED ACTIVATES FAULT LIGHT. ACFT GROUNDED. ON GVI, FOUND GROUND TERMINALS AT THE NR 2 ENGINE FIRE DETECTOR ASSEMBLY DAMAGED. TERMINATED BOTH WIRES AT THE CONNECTOR ASSEMBLY IAW AMM 26-11-02-960-802 AND WDM 26-11-11, PG 1.SDR ASAA2017090821853Warning Light · false activationDURING PREFLIGHT, DISCOVERED PRESSURIZATION AUTO FAILED AND ALTERNATE LIGHTS ON. ACFT GROUNDED. THE MODE SELECTOR SWITCH REPOSITIONED TO MAN AND BACK TO AUTO, AUTO FAIL LIGHT EXTINGUISHED. NO PREVIOUS HISTORY LAST 30 DAYS, CHECKED GOOD FOR SERVICE.SDR ASAA2017082721724Power Unit · failedAPU FAULT LIGHT ILLUMINATED DURING START. PERFORMED APU BITE TEST. DISPLAYED MESSAGE 49-41255 START POWER UNIT SHOWS HIGH TEMPERATURE. NO APU ROTATION SHUTDOWN. ACFT GROUNDED. TROUBLESHOT IAW FIM 49-40 TASK 815. COULD NOT DUPLICATE DISCREPANCY. FOUND SAME MESSDR ASAA2017082621715Autoland Sys · malfunctionedAUTOLAND UNSATISFACTORY. FINAL APPROACH WAS SQUIRLY, LEFT OF COURSE & RIGHT OF COURSE. IT CORRECTED AT ABOUT 500 FEET THEN FLEW FINE UNTIL 10 FT AGL WE GOT APPROACH WARN AND WERE ABOUT 15-20 FT RIGHT OF CENTERLINE. A/P STAYED ENGAGED UNTIL TOUCHDOWN AND WAS SDR ASAA2017070321265Fuel Heater · leakingNR 2 ENGINE FUEL SERVO HEATER LEAKING AT IDLE. ACFT GROUNDED REMOVED THE NR 2 ENGINE FUEL SERVO HEATER & INSTALLED SERVICEABLE FUEL SERVO HEATER IAW AMM 73-11-07-000-801-F00, & 73-11-07-400-801-F00. ACCOMPLISHED IDLE LEAK TEST & NO LEAKS NOTED IAW AMM 71-00SDR ASAA2017062621193Probe · out of limitsFOUND THE NR 2 TANK UNITS, 2 AND 3 FOUND OUT OF LIMITS. ACFT GROUNDED. REPLACED THE TANK UNITS F2R AND F3R IAW AMM 28-41-21/401. LEAK CHECKED GOOD. FQIS NOW CHECKED GOOD IAW AMM 28-41-21-710-801, AND 28-41-00-710-801. COMPARISON CHECKED WITHIN LIMITS IAW ASDR ASAA2017061521068Packing · leakingNR 1 IDG FREQUENT SERVICING. ACFT GROUNDED. FOUND EXTERNAL STATIC LEAK ON CAP IAW CMM 24-11-85. REPLACED THEPACKING. RAN ENGINE FOR 10 MINUTES NO LEAKS NOTED.SDR ASAA2017052420859Elec Connector · damagedDURING UNDERCOWL INSPECTION, DISCOVERED THE J7 HARNESS FROM EEC WITH A ROTATING BACKSHELL AT THE STATOR MOTOR CONNECTION. ACFT GROUNDED. REMOVED AND REPLACED THE WIRE HARNESS IAW AMM 71-51-03-000-801-F00 AND 71-51-03-400-801-F00. PERFORMED REQUIRED INSTALLSDR ASAA2017041920484Warning Light · false activationRIGHT PACK LIGHT ILLUMINATES ON RECALL CHECK. LIGHT IS RESETTABLE. ACFT GROUNDED. PERFORMED FIM 21-62, TASK 801. NO FAULTS FOUND. NO PACK LIGHT ON RECALL.SDR ASAA2017033020302Control Valve · failedDURING START, THE RIGHT PACK LIGHT ILLUMINATED ON MASTER RECALL. CLEARED WITH RESET. ACFT GROUNDED. CONFIRMED THE FAULT, THE NR 2 PACK/ZONE TEMP CONTROLLER BITE FAILS TCV NR 2 (V141) . REMOVED & REPLACED THE NR 2 TCV, IAW AMM 21-51-10. GROUND FUNCTIONAL CSDR ASAA2017032920293Controller · failedPRESSURIZATION AUTO FAIL LIGHT ILLUMINATED AFTER LANDING. ACFT GROUNDED. ACCOMPLISHED GVI NR 2 CABIN PRESSURE CONTROLLER (CPC), FOUND COPPER TAPE SEAL AT THE EDGES & FRONT OF THE CPC TORN & NUMEROUS HOLES. REMOVED & REPLACED THE NR 2 CPC IAW AMM 21-31-01. SDR ASAA2017032120241Switch · malfunctionedNR 1 START VALVE FAILED TO CLOSE AFTER START. MANUALLY SHUT OFF. ACFT GROUNDED. ACCOMPLISHED START SWITCH TEST OF NR 1 ENGINE START SWITCH IAW AMM 80-11-00. OPS CHECKED NORMAL.SDR ASAA2017031520181Warning Light · false activationRT PACK ILLUMINATED DURING AFTER START CHECK. RT PACK LIGHT EXTINGUISHED WHEN PRESSED AND RESET MASTER CAUTION. ACFT GROUNDED. ACCOMPLISHED PACK TEMP CONTROL BITE TEST IAW FIM 21-62 TSK 801. FOUND FAULT PACK TCV. RESET FAULT, ACCOMPLISHED BITE, NO FAULTS NOTEDSDR ASAA2017022119893Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2017011219364Unknown · malfunctionedSAT PROMPT DISAPPEARED WITH POWER TRANSFER. GROUNDED - YES. ACCOMPLISHED RESET PROCEDURE PER QRH. SATCOM RESTORED NORMAL.SDR ASAA2016121719070Shim · wornNR 1 ENGINE, 24 EACH FAN BLADE SHIMS REQUIRE REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENGINE FAN BLADE SHIMS REF ASA T/C 78472002.SDR ASAA2016121119006Satcom · malfunctionedSATCOM NOT DISPLAYED ON MCDU MENU. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE PER QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2016120418929Indicator · failedNR 2 TANK REFUEL PANEL QUANTITY INDICATOR INOPERATIVE. ACFT GROUNDED. CONFIRMED. REPLACED THE NR 2 REFUEL INDICATOR IAW AMM 28-41-61.SDR ASAA2016112618840Connector · corrodedAFTER STARTING THE NR 1 ENGINE THE FILTER BYPASS LIGHT ON THE FUEL PANEL ILLUMINATED. ACFT GROUNDED. VERIFIED ALL C/B'S ARE CLOSED AND PERFORMED EEC BITE AND FOUND MAINTENANCE MESSAGE 73-31071. OPENED NR 1 ENGINE FAN COWL AND PERFORMED FIM TASK 73-05 TASK 80SDR ASAA2016112418812Clamp · brokenNR 2 MAIN TANK REFUEL INDICATOR INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED TEST IAW AMM SUBTASK 28-41-61-710-003. NO FAULTS NOTED. AS PRECAUTIONARY CLEANED INDICATOR CONNECTOR WITH CONTACT CLEANER. FOUND CLAMP THAT HOLDS INDICATOR BROKEN, WOULD NOT TIGHTEN. ISDR ASAA2016111918743Fmc · malfunctionedLT FMC FAILED ENROUTE. GROUNDED - YES. ACCOMPLISHED B737-800 FIM TASK 34-61 TASK 836. SUCCESSFUL GROUND VERIFICATION TEST. FMC OPERATION NORMAL. FMC SWITCH IN NORMAL POSITION.SDR ASAA2016102718494Warning Light · false activationAUTO FAIL LIGHT ILLUMINATED APPROX 2 MINUTES AFTER LANDING ON PRESSURIZATION CONTROL PANEL. ACFT GROUNDED. ACCOMPLISHED FIM TASK 21-31-801, NO CURRENT FAULTS SHOWING, AUTO FAIL LIGHT IS EXTINGUISHED. AIRCRAFT OK FOR CONTINUED SERVICE.SDR ASAA2016091918097Transceiver · failedNR 1 HF FAIL ILLUMINATION ON ACTIVE & STBY. ACFT GROUNDED. COULD NOT DUPLICATE ISSUE. REMOVED AND REPLACED THE NR 1 HF RECEIVER/TRANSMITTER IAW AMM 23-11-21-400-801. AS A PRECAUTION. OPS CHECKED OK.SDR ASAA2016091618040Control Valve · failedCONTROLLER CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. CONFIRMED FAULT, NR 2 PACK ZONE TEMP CONTROLLER BITE, REF AMM TASK 21-61-00-700-806-002 SHOWS FLIGHT DECK TCV FAIL. NR 1 PACK ZONE TEMP CONTROLLER SHOWS NO FAULTS. R & R FLIGHT DECK TCV, SDR ASAA2016081717736Control Valve · failedRIGHT PACK LIGHT ILLUMINATED ON DESCENT, RESET IAW QRH, LIGHT EXTINGUISHED WHEN MASTER CAUTION RESET. ACFT GROUNDED. NR 2 ZONE TEMP CONTROLLER SHOWS THIS PACK ACTIVE FAULT, REF FIM 21-62. R & R RT PACK TEMPERATURE CONTROL VALVE IAW AMM 21-51-10-400-801. LESDR ASAA2016081517709Warning Light · false activationMASTER CAUTION RECALL, RT PACK ILLUMINATED, GOES OUT ON RECALL. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-61-00. FOUND NR 2 CONTROLLER WITH RED "TCV THIS PACK" FAULT LIGHT FOR PREVIOUS FLIGHT. CONTINUED WITH VERIFY PORTION OF TSDR ASAA2016080817641Satcom · malfunctionedSATCOM PROMPT UNAVAILABLE. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE PER QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2016072617524Modulating Valve · failedRIGHT PACK LIGHT ILLUMINATED ON WITH RECALL, EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. REMOVED & REPLACED THE NR 2 AFT ZONE TRIM MODULATION VALVE IAW AMM TASKS 21-61-21-000/400. OPS CHECKED GOOD IAW AMM TASK 21-61-00-700-806-002 PACK/ZONE TEMPESDR ASAA2016072117460Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE PER QRH. SATCOM RESTORED NORMAL.SDR ASAA2016072117453Warning Light · illuminatedDURING RECALL, RIGHT PACK LIGHT ILLUMINATED. QRH FOLLOWED. ACFT GROUNDED. ACCOMPLISHED BITE TEST IAW AMM TASK 21-61-00-700-806-002. BITE PASSED. RAN BOTH PACKS FOR 15 MINUTES FOR GROUND VERIFICATION. NO FAULTS NOTED. RAN BITE AGAIN FOR BOTH CONTROLLERS.SDR ASAA2016070917319Pressure Switch · faultedIAW T/C 78273000, FOUND NR 1 ENGINE CDU MESSAGE 73-31071, FUEL FILTERS SIGNALS DISAGREE, FLIGHT LOGGED 3,5,7 LONG TERM FAULT. ACFT GROUNDED. PERFORMED FIM 73-05 TASK 801. FOUND FROM DP0808 PIN L, K WITH 18 OHMS. HARNESS CHECKED GOOD. REMOVED AND REPLACED FFDPSSDR ASAA2016062717186Warning System · false activation2 FAULTS ARE SHOWN ON THE FMC CDU 73-31631 AND 73-31632. ACFT GROUNDED. PERFORMED FIM 73-28, TASK 802, ADIRU TOTAL PRESSURE DATA IS MISSING FROM A DEU-FAULT ISOLATION. EEC 1 AND EEC 2 PASS WITH NO MAINTENANCE MESSAGES AND BOTH SHOW A VALID TOTAL PRESSURE FRSDR ASAA2016061117071Skin · dentedDURING WALK AROUND, FOUND DENT AT FUSELAGE STA 382, STR 16 LT RVSM AREA. ACFT GROUNDED. REPAIRED SKIN AND STR IAW SRM 53-00-03 AND 53-00-01.SDR ASAA2016052816870Probe · failedREFUELER REPORTED BOTH QTY INDICATOR DROPPED RAPIDLY AFTER COMPLETING REFUEL. ACFT GROUNDED. PERFORMED A FQIS OPS TEST IAW AMM 28-41-00-710-801. FOUND COMPENSATOR DATA BAD ON BOTH MAIN TANKS. PERFORMED A TANK AND COMPENSATOR UNITS TEST IAW AMM 28-41-21-710-SDR ASAA2016052816859Warning Light · false activationPRESSURIZATION AUTOFAIL LIGHT AND ALTN LIGHT ILLUMINATED AFTER LANDING. ACFT GROUNDED. MOMENTARILY SELECTED PRESSURIZATION MODE SELECTOR TO MANUAL THEN BACK TO AUTO. AUTO FAIL LIGHT EXTINGUISHED. PERFORMED DCPC BITE IAW FIM 21-31, TASK 801, NO FAULTS NOTED.SDR ASAA2016052116810Bleed Valve · failedDURING SINGLE PACK CONFIDENCE CHECK, LT DUCT PRESSURE DID NOT DROP BELOW 10 PSI, IT MAINTAINED 15 PSI. ACFT GROUNDED. R & R BAR AND PRSOV IAW AMM 36-11-03 & 36-11-04 AND PERFORMED INSTALLATION TEST IAW AMM 36-11-03 & 36-11-04 AND INSTALLATION TEST & LEAK CHESDR ASAA2016042816672Floor Panel · corrodedFWD CARGO BAY FLOOR PANEL 120AF CORRODED ON ALL EDGES. ACFT GROUNDED. FABRICATED A NEW FLOOR PANEL IAW DWG 453A1610, REV F, ALODINED IAW AMM 51-21-41. PRIMED IAW AMM 51-21-72.SDR ASAA2016042816664Cargo Track · gougedFWD CARGO BAY CARGO TRACK FITTING GOUGED AT LBL18 BS 500+4. ACFT GROUNDED. CHECKED LIMITS & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 103, SHEETS 1. REMOVED DAMAGE IAW FIG 103, SHEET 6K. ALODINED IAW SRM 51-20-01 PRIMED IAW AMM 51-21-73.SDR ASAA2016042716651Floor Panel · corrodedFWD CARGO FLOOR PANEL 120DF CORRODED AND GOUGED. ACFT GROUNDED. FABRICATED NEW FWD CARGO FLOOR PANEL 120DR IAW BAC DWG 453A1610-19, REV:F ALODINED IAW AMM 51-21-41 AND PRIMED IAW AMM 51-21-72.SDR ASAA2016042616650Floor Panel · corrodedAFT CARGO FLOOR PANEL 140BF HAS DEEP GOUGES AND CORRODED UNDER CAP STRIPS. ACFT GROUNDED. EVALUATED PANEL FOR GOUGES AND CORROSION, ORIGINAL MATERIAL THICKNESS WAS 0.71; MATERIAL REMOVED 0.030; MATERIAL REMAINING IS 0.041, FOUND TO BE OUT OF LIMITS IAW SRMSDR ASAA2016042616648Attach Bracket · crackedKEEL BEAM PANEL 192E HAS 4 EA ATTACH BRACKETS BROKEN. ACFT GROUNDED. REMOVED 4 EA BROKEN BRACKETS IAW SRM 51-40-02, PARA 7. DRILLED TO FIT NEW BRACKETS 4 EA IAW SRM 51-40-05. INSTALLED 4 EA BRACKETS IAW SRM 51-40-02, PARA 7.SDR ASAA2016042416647Shear Tie · gougedLOWER FUSELAGE MAIN EQUIPMENT COMPARTMENT DOOR CUT-OUT AFT BAYONET FITTING GOUGED. ACFT GROUNDED. R & R BAYONET FITTING IAW SRM 51-40-02 & BAC DWG 141A8505-9 DOT REMOVED.SDR ASAA2016041616409Warning Light · false activationRIGHT PACK LIGHT ILLUMINATES. CLEARS ON MASTER CAUTION RESET. ACFT GROUNDED. HAD PACK SENSOR FAULT ON INITIAL BITE. RESET SYS, GROUND FUNCTIONAL CHECK GOOD IAW AMM 21-61-00-700-806-002, NO HISTORY LAST 10 DAYS.SDR ASAA2016040316232Switch · failedON LANDING THE TAKEOFF CONFIGURATION LIGHT AND HORN ACTIVATED WHEN ACTIVATING THE REVERSE THRUST. HORN AND LIGHT EXTINGUISHED WHEN STOWING THE REVERSERS. REF LOG PAGES 11451962 AND 11451963. ACFT GROUNDED. REF PSEU BITE FIM 32-09, TASK 801, NO EXISTING FSDR ASAA2016040216200Sensor · faultedRIGHT SIDE WINDOW OVERHEAT LIGHT ON. ACFT GROUNDED. ACCOMPLISHED RT SIDE WINDOW BITE CHECK IAW FIM 30-41, TASK 811, VERIFIED WINDOW SENSOR FAULT, CLEANED AND SECURED SENSOR CONNECTION. OVERHEAT LIGHT EXTINGUISHED AND FAULT CLEARED. OPS CHECK GOOD.SDR ASAA2016033116192Valve · failedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. EXTINGUISHES WHEN MASTER CAUTION SYS WAS RESET. ACFT GROUNDED. R & R TRIM MODULATING VALVE FOR FLIGHT DECK WITH A SERVICEABLE UNIT IN REF TO AMM 21-61-21/401. OPS CHECKS AND LEAK CHECK GOOD AT THIS TIME.SDR ASAA2016032716106Fmc · false indicationDUAL FMC FAILURE, RESTORED ITSELF IN ABOUT 30 SECS. ACFT GROUNDED. PERFORMED FAULT ISOLATION IAW FIM 34-61, TASK 836, FOUND NO INFLIGHT FAULTS. OPS CHECK NORMAL FOR BOTH FMC.SDR ASAA2016031315912Arm · out of adjustUPON TAKEOFF AND CLIMB OUT CABIN ALTITUDE WAS CLIMBING AT 2000 FPM. F/A CALLED TO REPORT AN EXTREME WIND NOISE FROM THE L1 DOOR. DOOR ACFT WAS NOT PRESSURIZING. ACFT GROUNDED. UPON ACFT ARRIVAL, FOUND L1 DOOR AFT UPPER AND LOWER ROLLERS NOT ENGAGED IN TRACK
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