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 ASAA11510523Probe · failedGE DIAGNOSTICS REPORTS NR 1 ENGINE TREND DATA SHOWS A SHIFT IN DELTA CRUISE AND TAKE OFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACCOMPLISHED TASK 77 21 01 200 801 F00 T49.5 PROBE AND EGT SYS INSP AND FOUND T49.5 PROBE AT SECTOR S3 TO BE OUT OF LIMITS. RSDR ASAA11510410Controller · malfunctionedRIGHT PACK LIGHT ILLUMINATE ON RECALL: RESETS WITH MASTER CAUTION. BITE TESTED ZONE TEMP CONTROLLERS AND FOUND FAULT ON NR 2 CONTROLLER TCV THIS PACK. RESET AND RAN RIGHT PACK PER FIM 21 62 00 810 831. TESTS OK. NO FAULTS.SDR ASAA11510378Filter · defectiveNR 2 ENG IDG DELTA P EXTENDED. PERFORMED FIM 24 11 00 810 803. CHANGED OIL. REPLACED CHARGE AND SCAVENGE FILTERS. OPS & LEAK CHECK GOOD NO DEFECTS NOTED.SDR ASAA11510294Window · defectiveDURING TAKEOFF ROLL NEAR 140 KTS MASTER CAUTION LGT ILLUMINATED ANTI ICE ANN. THE RIGHT SIDE WINDOW INDICATED AN OVERHEAT. PHX TEMP WAS 41 DEGREES C PER THE QRH TURNED SWITCH OFF FOR 5 MIN. TURNED WINDOW HEAT BACK ON. SYSTEM OPERATED NORMALLY REMAINDER OF SDR ASAA11510095Eec · faultedWHILE ACCOMPLISHING T/C 78273000 A FAULT WAS FOUND ON ENG 2 MESSAGE 73-10812 LONG TERM FAULT T 12 IS OUT OF RANGE. AVIONICS FOUND MULTIPLE INTERNAL EEC FAULTS REPLACED NR 2 ENG EEC REF MM 73-21-60. ALL OPS TEST GOOD.SDR ASAA11510079Unknown · malfunctionedNR 1 ENGINE TAI LIGHT ILLUMINATES AMBER 15 SECONDS AFTER THE NR 1 ENG ANTI ICE SWITCH IS PLACED TO OFF. ALL ENGINE INDICATIONS ARE THAT THE COWL ANTI ICE VALVE IS OPENING AND CLOSING NORMALLY. ACCOMPLISHED NR 1 ENG IDLE RUN. VERIFIED NORMAL GRD OPS OF CDS TSDR ASAA1150033Unknown · malfunctionedF/O SIDE WINDOW OVERHEAT LIGHT 11 000 250K SAT + 13C TAT +25C IAW CHECKLIST TURNED HEAT OFF WAITED 3 MINUTES TURNED BACK ON LIGHT DID NOT RECUR. ACCOMPLISHED WINDOW HT CTL UNIT BITE TEST PER FIM TASK 30 41 00 810 801 SYS CHECKS GOOD. OK FOR SERVICE.SDR ASAA11510014Warning System · intermittentRT PACK LIGHT REMAINS ILLUMINATED ON RECALL RESETS W/MASTER CAUTION RESET. ACCMP FIM TASK 21 53 00 810 810. FAULT FOUND TO BE INTERMTTENT ON RT PACK. BITE CHECK FOUND TO BE CLEAR. NO FAULTS. GROUND CHECK OK.SDR ASAA1159991Control Panel · inoperativeAPU GENERATOR POWER NOT AVAILABLE. ACFT GROUNDED. REPLACED APU STARTER GENERATOR AS REQUIRED OPS CHECKED BAD. AIR PRESSURE WAS GOOD NO ELECTRICAL POWER. REF AMM 49-41-21-400-810. REPLACED REMOTE APU CONTROL PANEL REF MM 26-22-03. PERFORMED TESTS MM 26-22-00-73SDR ASAA1159974Display · inoperativeF/O MCDU INOP. REPLACED F/O MCDU PER AMM REF 34 61 01 400 802/34 61 01 000 802. OPS CHECKS GOOD.SDR ASAA1159967Sensor · faultyAPU GENERATOR KICKED OFF BUS. ACCOMPLISHED FIM TASK 49 60 00 810 817 SPEED SENSOR 1 OR 2 SHOWS CIRCUIT FAILURE. FOUND NUMEROUS FAULTS ON NR 1 SPEED SENSOR. REPLACED SPEED SENSOR PER M/M 49 61 21. GROUND VERIFICATION CHECKS GOOD.SDR ASAA1159966Unknown · malfunctionedDURING ENGINE START WITH APU RUNNING AND ON APU GENERATOR POWER THE APU GENERATOR KICKED OFF BOTH SIDES BUT CONTINUED TO RUN. AFTER ENGINE NR 1 WAS STARTED APU GENERATORS WERE SUCCESSFULLY PUT BACK ON BOTH SIDES HOWEVER EEC ON ENGINE NR 1 WAS IN ALTN MODE. NSDR ASAA1159735Fmc · malfunctionedLOSS OF RIGHT FMC. VTK DISPLAYED WITH SINGLE FMC OPERATION. FOLLOWED QRH 11.3 RESTORED TO A SINGLE FMC OPS. LEFT FMC OPERATIONAL. REBOOTED RT FMC REF FIM TASK 34 61 TSK 801 NORMAL OPS RESTORED.SDR ASAA1159275Control Valve · faultyDURING RECALL AFTER START LIST LEFT PACK ILLUMINATED EXTINGUISHES W/ MASTER CAUTION RESET. PERFORMED BITE CHECK LT PACK TCV FAULT LIGHT ON. REMOVED & REPLACED LT TCV REF MM 21 51 10. BITE CHECK OK.SDR ASAA1159190Terminal · looseLT SIDE WINDOW OVERHEAT LIGHT CAME ON DID CHECKLIST AND IT CAME ON AGAIN. ACCOMP FIM TASK 30 41 00 810 801 FOUND SENSOR FAULT ON WINDOW HEAT CONTROLLER ACCOMPLISHED TSR 813838 STEPS 1 THROUGH 3. FOUND LOOSE WINDOW HEAT SENSOR TERMINAL ON L2 WINDOW SECURED SESDR ASAA1159178Light · inoperativeREF T/C 78233008: EMERGENCY LIGHT CEILING LIGHT IN FORWARD LOWERED CEILING PANEL IS INOP. RELAMP NO HELP. REF WDM 33 51 12 PAGE 4 REMOVED AND REPLACED L1417 EMERGENCY LIGHT CEILING LIGHT AND PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST PER MM 33 51 00 710 80SDR ASAA1159170Wire Harness · defectiveLEFT/SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. QRH PROCEDURE FOLLOWED. OVERHEAT LIGHT RE-ILLUMINATED. TROUBLESHOT REF FIM 30 41 00 810 811. WHCU FAULTS THE WINDOW SENSOR LAST FIVE FAULTS. BOTH SENSORS RESISTANCE CHECK GOOD (299 OHMS) WITH WINDOW COLD. LT SSDR ASAA1159165Unknown · malfunctionedON TAKEOFF OUT OF ANC CLIMBING THROUGH APPROX 500FT HAD ILLUMINATION OF LEFT SIDE WINDOW OVERHEAT LIGHT. RAN QRH CHECKLIST AFTER SWITCH OFF FOR 5 MINUTES TURNED SWITCH BACK ON. LT SIDE WHC LOGGED SENSOR FAULT SYS TESTS GOOD REF TASK 30 41 00 710 801. NO HISSDR ASAA1159082Display · faultyLEFT MCDU BUTTON 6 RIGHT DOES NOT CLICK MUSHY. REMOVED, REPLACED AND PERFORMED GOOD TEST OF LEFT MCDU PER MM'S 34 61 01 000 802 AND 34 61 01 400 802.SDR ASAA1159081Anti-Ice Valve · failedWING ANTI ICE IS NOT OPERATING PER FLT OPS CHECKLIST PG 7.000 P 33 SIMULATING DUCT OVERTEMP CONDITION. REPLACED LT ANTI ICE VALVE WING ANTI ICE TESTED GOOD PER AMM 30 11 11 000 801.SDR ASAA1159041Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 727H STR 25R. REMOVED CRACKED STRINGER CLIP FABRICATED REPLACEMENT PART AND INSTALLED IAW BOEING 737 800 SRM 51 40 02 53 60 07 AND BOEING DRAWING 146A1010.SDR ASAA1159040Baffle · crackedBAFFLE CRACKED IN FORWARD CARGO BAY. REMOVED CRACKED BAFFLE AND ATTACH ANGLES FABRICATED REPLACEMENT PARTS AND INSTALLED IAW B737 800 SRM 51 30 01 53 00 53 51 20 01 51 40 02.SDR ASAA1159039Pan · crackedAFT SERVICE DOOR PAN AFT BRACKET IS CRACKED. REMOVED CRACKED BRACKET, FABIRCATED AND INSTALLED REPLACEMENT BRACKET IAW B737 800 SRM 51 40 02.SDR ASAA1159097Floor Panel · crackedAFT CARGO NR 2 FLOOR PANEL IS CRACKED. REMOVED CRACKED FLOOR PANEL FABRICATED AND INSTALLED REPLACEMENT PART IAW BOEING DWG 453A2610 AND B737 800 SRM 53 60 53 51 40 02 51 40 08 51 20 01 AND BOEING SOPM 20 41 02.SDR ASAA1159023Unknown · unknownDURING CLIMBOUT AT FL360 N1 99.0-99.0 SAT 60 L DUCT PRESSURE STAYED AT 43 PSI RT DUCT PRESSURE DROPPED TO 23 PSI. STAYED AT 23 PSI UNTIL CRUISE THEN CAME UP TO 34 PSI. COMPLIED WITH FIM 36-10-00-810-804. FOUND NR 1 AND NR 2 ENGINE PRECOOLER CONTROL VALVES ASDR ASAA1159021Indicator · poppedFOUND NR 1 ENG DELTA P INDICATOR POPPED. FOUND NO EVIDENCE OF IDG FILTER CONTAMINATION. MARKED DECAL ON NR 1 ENG IDG THIS IS THE FIRST EVENT OF INDICATOR POPPING. ACCOMPLISHED FIM TASK 24 11 00 810 803 DELTA P INDICATOR HAS BEEN RESET.SDR ASAA1158902Unknown · malfunctionedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. COULD NOT DUPLICATE. NR 2 TEMP CONT BITE LOGGED FLT DECK TRIM VALVE FAULT BUT VERFIY CK "GO". RESET NR 2 TEMP CONT AND OPERATED LT PACK FOR SEVERAL MIN AT DIFFERENT TEMP SETTING ALL CK NML. RETESTED NR 2SDR ASAA1158716Start Valve · failedON ENG START WITH START SWITCH IN GRD NO START VALVE OPEN OR N2 INDICATION ON ENG NR 1. ENG NR 2 START NORMAL. REPLACED NR 1 ENGINE START VALVE LEAK CHECKED AND TEST GOOD IN REF AMM 80 11 03 000 801 AND AMM 71 00 00 700 821.SDR ASAA1058706Apu · faultySMELL / ODOR DETECTED IN CABIN AND FLT DECK ON CLIMB OUT RETURN TO ANC. DIVERSION TIME 10 MINUTES. PERFORMED CABIN ODOR TROUBLESHOOTING REF AMM 05 60 00 280 801C1 & ETOPS MANUAL 05 60 00. INSPECTED CABIN AND CARGO AREAS FOUND NO VISUAL CONTAMINANTS. DEBRIESDR ASAA1058628Unknown · malfunctionedNR 2 ENGINE HAS LONG TERM FAULTS: MESSAGE NR 73 10122 INTERNAL EEC FAULT MESSAGE NR 73 10812 THE T12 SIGNAL IS OUT OF RANGE. MESSAGE NR 75 10822 THE T25 SIGNAL IS OUT OF RANGE. MESSAGE NR 75 10832 THE T3 SIGNAL IS OUT OF RANGE. MESSAGE NR 77 10842 : THE TSDR ASAA1058545Start Valve · failedNO "START VALVE" LIGHT & NO ROTATION WHEN STARTING NR 1 ENGINE. REPLACED START VALVE REF MM 80 11 03. OPS CHECK NORMAL ENG ROTATED AND LIGHT OPERATED NORMALLY.SDR ASAA1058461Warning System · false activationTHE "PWS FAIL" (PREDICTIVE WINDSHEAR SYSTEM) ILLUMINATED ON BOTH CAPTAIN AND FIRST OFFICERS ND'S AFTER LANDING WENT OUT AFTER ENGINE SHUTDOWN. NO POPPED CB'S. PERFORMED FIM 34 43 TASK 815 AND MM 34 43 00. OPS NORMAL SAME. SUCCESFUL GROUND VERIFICATION. NOSDR ASAA1058419Filter · defectiveNR 2 IDG DIFF INDICATOR POPPED. FOUND DURING ETOPS PDC. REMOVED AND REPLACED IDG FILTERS & OIL ON NR 2 IDG REF T/C 78424000 OPS & LEAK CHECK GOOD.SDR ASAA1058381Warning System · intermittentON RECALL ZONE TEMP LIGHT FOR CONT CAB CAME ON. WENT OUT ON RESET. PERFORMED FIM TASK 21 62 00 810 842. APPEARS TO HAVE BEEN AN INTERMITTENT FAULT. CONTROLLER FAULT RESET. PAC OPERATION NORMAL WITH NO REOCCURRING ZONE TEMP LIGHT, HAS NO OTHER HISTORY.SDR ASAA1058322Hf Comm · malfunctionedHF NR 2 WILL NOT TRANSMIT FROM EITHER AUDIO PANEL, THE TUNING TONE & RECEPTION IS GOOD. DIVERSION TIME 65 MINUTES. ACCOMPLISHED HF BITE CHECK PER FIM 23 11 TASK 801. BITE CHECK OK. GROUND OPS CHECK ALSO OK. AS PRECAUTION REPLACED NR 2 HF TRANSCEIVER AMM 2SDR ASAA1058247Unknown · malfunctionedAUTO THROTTLES WILL NOT ENGAGE. IN FLT FAULT REVIEW LOGGED ASM NR 2 FAULTS ON LAST LEG. ACCOMPLISHED AUTOTHROTTLE ARM PROBLEM FAULT ISOLATION TESTS. REF M/M TASK 22 32 00 810 810. PASSES ALL TESTS. ACCOMPLISHED A/T BITE PROCEDURE TESTS. REF M/M FIM TASK SDR ASAA1058245Controller · malfunctionedLEFT PACK LIGHT ILLUMINATED ON RECALL DURING "LANDING CHECK". RESET WHEN MASTER CAUTION ANNUNCIATOR PUSHED. VERIFIED FAULT TEMP CONTROL VALVE ON NR 1 ZONE TEMP CONTROLLER. RESET AND TESTS NORMAL PER FIM 21 62 TASK 802. GROUND VERIFICATION OF SYSTEM OPERATISDR ASAA1058241Bleed Air Sys · malfunctionedNO APU AIR NO DUCT PRESS NO DUAL BLEED. RESTARTED APU VERIFIED GROUND OPS NORMAL BITE CHECK CDU NO CURRENT STATUS FAULT.SDR ASAA1058150Control Valve · malfunctionedLEFT PACK LIGHT ILLUMINATED ON RECALL. ACCOMPLISHED BITE CHECK ON LT ZONE TEMP CONTROLLER FOUND LT PACK TCV FAULT. REPLACED LT TEMP CONTROL VALVE PER AMM 21 51 10 00 801 AND 21 51 10 400 801, OPS BITE LEAK CHECK ALL GOOD.SDR ASAA1058088Control Unit · failedNR 4 WINDOW HEAT CONTROL UNIT (RT FWD) ON E4 2 RACK HAS FLASHING "WHCU LRU" LIGHT AND WILL NOT RESPOND TO BITE COMMANDS. ACCOMPLISHED T/S PER FIM 30 41 00 810 801 AND FIM 30 41 00 810 807. REPLACED NR 4 WINDOW HEAT CONTROL UNIT (M323) PER MM 30 41 11 000 801SDR ASAA1058030Fmc · failedNR 2 FMC DISPLAYS VTK/MAP SWITCHED TO BOTH ON NR 1 OK. VERIFIED RT FMC FAILED. REPLACED NR 2 FMC. FMC SYS TEST GOOD REF 34 61 02 400 801.SDR ASAA1058025Hf Comm · malfunctionedHF1 RADIO RECEIVER IS GARBLED AND UNUSABLE ON 4 ATTEMPTS WITH DIFFERENT FREQUENCIES. HF2 XMITTER AND RECEIVER NORMAL OPS. HF1 HAD FADING ON SFO ARINC BUT WAS SOLID RECEIVING WWV UNABLE TO VERIFY DISCREPANCY. REMOVED AND REPLACED HF NR 1 RECEIVER IAW MM 23 1SDR ASAA1058005Fmc · malfunctionedRIGHT FMC FAILURE. FMC MESSAGE LIGHT CAME ON WITH SINGLE FMC OPERATION MESSAGE IN SCRATCH PAD. THIS WAS FOLLOWED BY LOSS OF FMC DATA ON F/O'S NAVIGATION DISPLAY. VTK & MAP MODE FLAGS APPEARED. MOVING FMC SOURCE SELECT SWITCH TO LEFT RESTORED NORMAL FMC OPESDR ASAA1057964Unknown · malfunctionedWHILE PERFORMING FMC CDU TASK CARD FOUND FAULT CODE 73 10812 T12 SIGNAL IS OUT OF RANGE FOR NR 2 ENGINE. FAULT CODE 73 10812 LOGGED IN FLIGHT LEG NR 1 ONLY. FOLLOWED FIM 73 26 TASK 804 ACCOMPLISHED EEC TEST, NO FAULTS. GROUND VERIFICATION TEST PASSED.SDR ASAA1057963Unknown · malfunctionedWHILE ACCOMPLISHING FMC CDU T/C FOUND FAULT CODE 79 11102. THE ENGINE OIL TEMPERATURE SIGNAL IS OUT OF RANGE FOR NR 2 ENGINE. FAULT CODE 79 11102 WAS LOGGED IN FLIGHT LEG 1 ONLY. FOLLOWED FIM 79 21 TASK 802 ACCOMPLISHED EEC TEST, NO FAULTS. GROUND VERIFICASDR ASAA1057962Unknown · malfunctionedWHILE ACCOMPLISHING FMC CDU T/C FOUND CODE 77 10842 THE TOP RIGHT EGT SIGNAL 9T495 S1) IS OUT OF RANGE FOR NR 2 ENGINE AND 77 10852 THE BOTTOM RIGHT EGT (T49552) IS OUT OF RANGE FOR NR 2 ENG. FAULT CODES 77 10842 AND 77 10852 LOGGED IN FLIGHT LEG 1 ONLY. FOLSDR ASAA1057893Sight Gauge · defectiveMAINTENANCE REPORTS NR 2 ENGINE OIL TANK SIGHT GAUGE IS BECOMING DIFFICULT TO READ. REMOVED AND REPLACED NR 2 ENGINE OIL TANK SIGHT GLASS REF AMM 79 11 01. RAN NR 2 ENGINE TEST 3A IDLE POWER LEAK CHECK REF AMM 71 00 00. NO LEAK NOTED. RAN NR 2 ENGINE TEST SDR ASAA1057882Warning System · malfunctionedLEFT PACK LIGHT ILLUMINATED ON RECALL AFTER ENGINE START. LIGHT EXTINGUISHES WHEN RESET. LT CONTROLLER LOGGED FLIGHT DECK TCV LAST LEG. ACCOMPLISHED CONTROLLER BITE REF MM 21 61 01 AND RESET FAULT. LT PACK CONTROL OPS NORMAL.SDR ASAA1057786Warning Light · illuminatedCONT CAB ZONE TEMP LIGHT ILLUMINATES DURING MASTER CAUTION RECALL. PERFORMED FIM TASK 21 62 00, ALL SYSTEM OPERATING NORMAL. NO HISTORY PAST 60 DAYS. SEAMC NOTIFIED.SDR ASAA1057777Filter · failedDURING TAXI OUT THE NR 1 ENGINE FUEL FILTER BYPASS LIGHT CAME ON. REPLACED NR 1 ENGINE FUEL FILTER ASSY AND HOUSING O-RINGS PER MM 73 11 02, OPS AND LEAK CHECKS GOOD.
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