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 ASAA2021012733953Fmc · fault messageCAPTAIN'S ND "FMC DISAGREE" ON GROUND. GROUNDED-YES. PERFORMED B737-800 FIM 34-61 TASK 835. FOUND MISMATCH BETWEEN FMC NR 2 COWL ANTI VALVE, REF LG PG 60083689. PERFORMED FMC BITE, PER FIM 34-61 TASK 801. OPERATIONS NORMAL.SDR ASAA2020122733773Warning Message · false activationR2 WINDOW HEAT INOPERABLE. GROUNDED-YES. B737-800 FIM 30-41 TASK 809 NO DEFECT NO CURRENT FAULTS. CW WINDOW HEAT SYSTEM OPERATIONS TEST VERIFIED R2 WINDOW HEATS WITH NO FAULTS, REF B737-800 AMM 30-41-00-710-801.SDR ASAA2020122733753Heater · malfunctionedR1 WINDOW HEAT INOPERABLE. GROUNDED-YES. PERFORMED B737-800 FIM 30-41 TASK 812 R1 WINDOW HEAT OK BITE OK.SDR ASAA2020120733664Start Valve · stickingREPORTS OF NR 1 ENGINE START VALVE IS SLOW TO OPEN OR STICKING. GROUNDED-YES. REMOVED AND REPLACED NR 1 ENGINE START VALVE, IAW B737-800 AMM 80-11-03. OPERATIONS CHECK GOOD, NO OTHER DEFECTS NOTED. GROUND VERIFICATION SATISFACTORY.SDR ASAA2020112333599Eec · faultedWHILE PERFORMING TC 7827300 FOUND NR 2 ENGINE FAULT CODE 73-30312 SHORT TIME FAULT START SIGNAL SWITCH AND ARINC BUS DATA DISAGREE. GROUNDED-YES. REMOVED & REPLACED NR 2 ENGINE EEC, PER B737-800 AMM 73-21-60/401. PERFORMED EEC TEST AFTER INSTALLATION, PER ASDR ASAA2020101633374Spacer · debondedSPACERS NR 4, NR 10, NR 23 ON ENGINE 1 FOUND LOOSE ELASTOMER, REF T/C 78472010. GROUNDED-YES. REMOVED AND REPLACED SPACERS NR 4, NR 10, NR 23 ON ENGINE 1, REF T/C 78472010.SDR ASAA2020101633373Spinner · erodedFWD SPINNER CONE PAINT EROSION ON 1 ENGINE, REF T/C 78472010. GROUNDED-YES. REMOVED AND REPLACED FWD SPINNER CONE 1 ENGINE, REF T/C 78472010.SDR ASAA2020082423056Bulb · burned outRT LOWER WING EMERGENCY LIGHT INOPERABLE. GROUNDED - YES. RT LOWER WING EMERGENCY LIGHT BULB REPLACED, IAW B737-800 AMM 35-51-04-960-801. OPS CHECK GOOD, IAW B737-800 AMM 33-51-710-001 SUBTASK.SDR ASAA2020082433050Skin · corrodedAIRCRAFT SKIN CORRODED AROUND LAV EXHAUST VENT. GROUNDED - YES. REMOVED DAMAGE AND CHECKED LIMITS. ORIGINAL THICKNESS IS .125, REMAINING IS .098, .027 WAS REMOVED. FOUND TO BE OUT OF LIMITS, REF B737-800 SRM 53-00-01-1A-1. CUTOUT DAMAGE AND REPAIRED SKIN,SDR ASAA2020082143051Battery Pack · dischargedR2 DOOR EMERGENCY EXIT LIGHTS INOPERABLE. GROUNDED - YES. REMOVED, REPLACED, AND OPS CHECK OF BATTERY PACK M1672 AND R2 DOOR EMERGENCY LIGHT, GOOD IAW B737 AMM 33-81-06-960-805.SDR ASAA2020022732326Wire · separatedFLT CREW REPORTS #2 ENGINE FIRE DETECTION DOES NOT TEST. GROUNDED - YES. PERFORMED ENGINE FIRE DETECTION RESISTANCE TEST PER B737-800 AMM 26-11-00-730-801. FAILED RIGHT CORE LOOP. DISCOVERED WIRES SEPARATED FROM TERMINAL LUGS. REPAIRED WIRES SEPARATED FROM TERSDR ASAA2020021963209Engine · out of limitsGE DIAGNOSTICS REPORTS THE #2 ENGINE EXPERIENCED AN EGT EXCEEDANCE DURING TAKEOFF THAT MAY HAVE EXCEEDED THE TRANSIENT AREA LIMITS. PEAK EGT RECORDED ON REPORT 06 WAS 960 DEGREES DURING TAKEOFF (FLIGHT PHASE 4.) #2 ENGINE TREND DATA ALSO SHOWS A SUDDEN SHIFT SDR ASAA2020021932208Sense Line · leakingEGT EXCEEDANCE ENG 1+2 GROUNDED - YES. FOR ENG #1, ACCOMPLISHED STEP F. (4), HPT BLADES BORESCOPE INSP B737-800 FIM 71-06 TASK 805 AND REF B737-800 AMM TASK 72-00-00-200-807-F00 HPT BORESCOPE INSP. ACCOMPLISHED HPT BOROSCOPE INPECTION IAW AMM 72-00-00-200-807-SDR ASAA2020013132034Starter · leakingNR 1 ENGINE OIL CONSUMPTION RATES ARE HIGHER THAN EXPECTED. ACCOMPLISH VISUAL INSPECTION OF OIL LINES AND OIL SYSTEM COMPONENTS FOR EVIDENCE OF OIL LEAKAGE. GROUNDED - YES. FOUND EVIDENCE OF OIL LEAKAGE AT STARTER DRIVE PAD AREA, CLEANED AREA AROUND STARTER ARSDR ASAA2020012401952Compensator · failedCHECK #2 (RIGHT) FUEL TANK UNIT VALUES. GROUNDED - YES. REPLACED ALL #2 TANK FQIS TANK UNITS AND COMPENSATOR UNITS ON TANK-TIGERS W/O 12046M84-R-0-8. #2 TANK COMPENSATOR RESISTANCE AND CAPACITANCE CKS GOOD IAW B737 800 AMM 28 41 21 710 801.SDR ASAA2020012403937Valve · stuckRIGHT MAIN FUEL TANK QUANTITY SLOWLY DECREASED DURING INITIAL CRUISE WHILE USING CENTER TANK FUEL. RIGHT MAIN QUANTITY STABILIZED AT 8.13 FUEL USED AGREED WITH PLANNED BURN. GROUNDED - YES. REPLACED LH AND RH CENTER TANK BOOST PUMPS, CROSSFEED VALVE BODY AND ASDR ASAA2020012283936Compensator · failedLEFT WING TANK FUEL QUANTITY READS 400 LBS MORE THAN WHAT WAS IN THE TANK CONFIRMED BY FUEL STICKING. GROUNDED - YES. REPLACED ALL NR 1 TANK FQIS UNITS AND COMPENSATOR UNITS ON WORK ORDER 12046M84-R-0-9. NR 1 TANK COMPENSATOR RESISTANCE AND CAPACITANCE CHECSDR ASAA2020012181909Fuel Tank · malfunctionedDURING CRUISE, WING TANKS BEGAN DRAINING WHILE CTR FUEL TANK STILL HAD OVER 3500 LBS WITH ALL FUEL PUMP SWITCHES ON. CTR TANK FUEL BEGAN DRAINING WITH CROSSFEED VALVE OPEN ONLY. GROUNDED - YES. PERFORMED UNWANTED FUEL TRANSFER INTO CENTER TANK IAW FIM 28-21 TASDR ASAA2020012171890Warning Light · false activationAT TOP OF DESCENT, LEFT PACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL PACK LIGHT EXTINGUISHED WHEN MASTER CAUTION WAS RESET. GROUNDED - YES. ACCOMPLISHED PACK ZONE TEMP CONTROLLER BITE IAW FIM 21-61 TASK 801, FOUND FAULT HISTORY FOR RAM AIR ACT. FAULT CLEASDR ASAA2020010631772Actuator · faultedWHEN RECALL IS PRESSED LEFT PACK LIGHT AND MASTER CAUTION LIGHT REMAIN ILLUMINATED. BOTH LIGHT EXTINGUISH WHEN MASTER CAUTION IS RESET. GROUNDED - YES. ACCOMPLISHED PACK ZONE TEMP CONTROLLER BITE REF B737-800 21-61 TASK 801, LEFT CONTROLLER LOGGED RAM AIR DOORSDR ASAA2019123081713Control Valve · intermittentLEFT PACK ILLUMINATED IN FLIGHT. GROUNDED - YES. PERFORMED PACK/ZONE TEMP CONTROLLER BITE IAW AMM 21-61-00-700-806-002. THIS PACK - TCV LIGHT ON DURING BITE OF LEFT CONTROLLER, OFF FOR PREV FLIGHT AND VERIFY TESTS. 2 OTHER OCCURRENCES LAST 60 DAYS. REMOVED ANSDR ASAA2019122651700Warning Light · false activationLEFT PACK ILLUMINATED DURING MASTER RECALL AND EXTINGUISHED DURING RESET. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 21-53 TASK 821 FOUND LEFT PACK TCV LIGHT ON WAS ABLE TO RESET FAULT. LEFT PACK OPS CK GOOD.SDR ASAA2019120651514Indicator · inoperative#2 TANK, WING REFUEL QTY GAGE INOP. GROUNDED - YES. BITE CHK SYSTEM & GAUGES, NO FAULTS, INDICATES NORMAL, REF B737-800 FIM 28-41 TASK 801. OPS NORMAL.SDR ASAA2019111271276Warning Light · false activationLEFT PACK LIGHT ILLUMINATED WHEN MASTER CAUTION IS PRESSED. PACK LIGHT EXTINGUISHES WITH MASTER CAUTION IS PUSHED. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE REF B737-800 FIM 21-62 TASK 801. NO ISSUES RT PACK TEMP CONTROLLER. L/H PACK TEMP CONTROLLER ON SDR ASAA2019110231230Starter · inoperative#2 ENGINE WOULD NOT ROTATE WHEN START SWITCH PUT TO GND. NO ROTATION AT ALL. GROUNDED - YES. REMOVED AND REPLACED #2 ENG STATER PER B737-800 AMM 80-11-01, SERVICED WITH OIL AND PERFORMED GVI, NO DAMAGE NOTED AND ALL CHECKS GOOD. STARTER IS SECURE, A/C GOOD FORSDR ASAA2019091230694Control Panel · scratchedCAPT COURSE SELECTOR WINDOW SCRATCHED UP. UNABLE TO CLEARLY READ COURSE. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL PER AMM 22-11-34. DFCS MODE CONTROL PANEL OPS CKS NORMAL PER AMM 22-11-34-740-801. DFCS, LAND VERIFY GRP 49, DFCS CURRENT STATSDR ASAA2019090730638Actuator · leakingDURING WALKAROUND NOTICED FUEL DRIPPING FROM #2 ENGINE. GROUNDED - YES. OPENED #2 ENG COWLS. FOUND FUEL DRIPPING FROM LEFT VSV DRAIN TUBE AT 3 DROPS PER MIN. HAD CREW RUN #2 ENGINE AT IDLE. NO LEAKS NOTED DURING IDLE RUN. AFTER SHUT DOWN NO LEAKS NOTED FROM DRSDR ASAA2019081973421Start Valve · inoperative#2 ENG NO ROTATION. GROUNDED - YES. REMOVED & REPLACED STARTER VALVE REF B737-800 AMM 80-11-03, OP & LK CHECK CW-NO LEAK NOTED, OP CHECK GOOD.SDR ASAA2019081233372Probe · failed# 2 ENG EGT RED BOX, DID NOT HAPPEN DURING ENGINE START. GROUNDED - YES. REPLACED T49.5 S1 PROBE ASSY IAW AMM 77-21-01 PULLED 7EA CB AND RESET 7EA CBS. GROUND VERIFICATION TEST GOOD. POWER ASSURANCE TEST #5 PASSED AT 65% N1, EGT 578 DEG, N2 88.3 OAT +16C.SDR ASAA2019080183254Actuator · faultedRAM AIR FULL OPEN LIGHT NOT ILLUMINATED (RIGHT) ON PREFLIGHT. GROUNDED - YES. CONFIRMED FAULT, R/H PACK-ZONE TEMP CONTROLLER BITE SHOWS R/H RAM AIR ACTUATOR FAULT. REMOVED & REPLACED R/H RAM AIR ACTUATOR REF B737-800 AMM 21-51-21. ACCOMPLISHED R/H PACK/ZONE TESDR ASAA2019072330186Unknown · malfunctionedHF#1 FAILED SELCAL CHECK ON 8.843 MHZ. GROUNDED - YES. PERFORMED INITIAL EVALUATION REF FIM 23-11 TASK 806. THE HF 1 COMMUNICATION SYSTEM OPERATES SATISFACTORILY, FAULT WAS INTERMITTENT. A/C OK FOR SERVICE.SDR ASAA2019070729964Transceiver · inoperativeHF #1 INOP. GROUNDED - YES. ACCOMPLISH FIM 23-11 TASK 806, HF COMM SYSTEM RECEIVE/XMIT PROBLEM. REMOVED & REPLACED #1 HF TRANSCEIVER, PER AMM 23-11-21, SUCCESSFUL GROUND VERIFICATION ACCOMPLISHED.SDR ASAA2019063029887Unknown · malfunctionedHF 1 FAILED ABOUT 90 MINUTES INTO THE FLIGHT - NO AUDIO AT ALL, SENSITIVITY AT 100%. CIRCUIT BREAKER NOT POPPED. GROUNDED - YES. ABLE TO COMMUNICATE. SYS CKS NML. NO FAULTS FOUND. PERFORMED SYS OPS TEST REF AMM 23-11-00.SDR ASAA2019062429789Valve · failedR-PACK LIGHT DURING MASTER CAUTION RESET LIGHT GOES OUT. GROUNDED - YES. R-PACK PRIMARY TEMP CONTROL INOP. PERFORMED BITE, CONFIRMED R-PACK TEMP CONTROL VALVE FAILED. REMOVED AND REPLACED R PACK TEMP CONTROL VALVE REF B737-800 AMM 21-51-10. TEMP CONTROL VALVE SDR ASAA2019051329319Elastomer · missingNR 1 ENGINE ESN 894137 TC 78472010 FOUND MULTIPLE PLATFORMS MISSING ELASTOMER SEALS. OUT OF LIMITS PER TASK AMM 72-21-02-200-801-F00. REQUIRES REPLACEMENT OF 24 PLATFORMS. GROUNDED - YES. REPLACED ALL 24 PLATFORMS REF T/C #78472010.SDR ASAA2019051329322Shim · wornNR 1 ENGINE ESN 894137 TC 78472010 FOUND ALL FAN BLADE SHIMS WORN OUT OF LIMITS AMM TASK 72-21-02-200-801-F00. GROUNDED - YES. REPLACED ALL FAN BLADE SHIMS. REF T/C 78472010.SDR ASAA2019051329321Spacer · debondedNR 1 ENGINE ESN 894137 TC 78472010 FOUND 3 SPACERS DISBONDED. POSITIONS 19, 21, AND 23. GROUNDED - YES. REPLACED 3 EA. SPACERS @ POSITIONS 19, 21, AND 23. REF T/C #78472010.SDR ASAA2019051329320Blade · wornNR 1 ENGINE ESN 894137 TC 78472010 FOUND SIX FAN BLADES FAILED INSPECTION FOR CUNI MISSING. POSITIONS 2, 3, 8, 14, 15 AND 20. GROUNDED - YES. REPLACED 6 EA. BLADES. REF T/C #78472010.SDR ASAA2019043029210Sign · unsecureR1 EMERGENCY EXIT SIGN FELL OFF. GROUNDED - YES. RESECURED EXIT SIGN FOR R1 DOOR. OPS NORMAL.SDR ASAA2019042659141Indicator · inoperativeAT REFUEL PANEL FOUND #1 TANK FUEL QTY INDICATOR NOT PRESENTING LBS DISPLAY AND NOT PASSING INDICATOR SELF TEST. GROUNDED - YES. REMOVED AND REPLACED #1 TANK FUEL QTY INDICATOR PER B737-800 AMM 28-41-61-000-801/28-41-61-400-801.SDR ASAA2019041078936Warning Light · false activationL "PACK" LIGHT ILLUMINATED DURING RECALL @ CRUISE FL 340. EXTINGUISHED WHEN MASTER CAUTION RESET. PRESSURIZATION, DUCT PRESSURES, FLY DECK & CABIN TEMPS, & PACK TEMPS ALL NORMAL. GROUNDED - YES. REF B737-800 FIM TASK 21-53 TASK 809, PZTC #1 PREV FLT LOGGED RAMSDR ASAA2019040318868Filter · dirtyDIRTY SOCK SMELL ON INITIAL CLIMB FROM OMA. TURNED OFF RECIRC FANS, SMELL WENT AWAY. KEPT FANS OFF. GROUNDED - YES. ACCOMPLISHED F.I.M TASK 21-00 TASK 804. REMOVED AND REPLACED RECIRCULATION AIR FILTERS REF. AMM 21-25-01. FILTERS FOUND VERY DIRTY. PERFORMED OPSDR ASAA2019031428616Link · wornNR 2 ENGINE START DUCT/VALVE FWD SUPPORT LINK WORN. GROUNDED - YES. REPLACED LINK. REF AMM 80-11-03.SDR ASAA2019031428613Link · wornNR 2 ENGINE, SUPPORT LINK @ HIGH STAGE VALVE/DUCT WORN. (INBD. FWD AREA). GROUNDED - YES. REPLACED LINK. REF. AMM 36-11-01.SDR ASAA2019031328599Actuator · leakingNR 1 ENG DRIPPING FUEL FROM THE RIGHT VSV DRAIN @ 15DPM. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG RT VSV ACTUATOR REF AMM 75-31-01. OPS AND LEAK CHECK GOOD REF AMM 75-31-01.SDR ASAA2019030928563Exciter · inoperativeAFTER STARTING ENGINE NR 2 WITH IGNITION ON RIGHT SIDE WE ATTEMPTED TO START ENG NR 1 AND NO START INDICATIONS. GROUNDED - YES. REMOVED & REPLACED NR 1 ENG RT IGNITION EXCITER REF AMM 74-11-01 OPS CK GOOD. REMOVED MEL 74-1E.SDR ASAA2019030228424Card · dirtyUNABLE TO MAKE VOICE CALLS ON SATCOM. BOTH 1&2 SAY NOT READY. SCRATCH PAD SAYS SATCOM VOICE UNAVAILABLE. GROUNDED - YES. REMOVED SATCOM TRANSCEIVER, REMOVED, CLEANED, AND RESEATED BOTH SIM CARDS IN THE CIM MODULE. REINSTALLED SATCOM TRANSCEIVER REF AMM 23-15-0SDR ASAA2019021728212Bolt · looseF/O'S WINDOW DIFFICULT TO CLOSE. GROUNDED - YES. FOUND LOWER AFT AFT TRACK GLIDE BEARING BOLT LOOSE. REPLACED GLIDE BOLT REF CMM 56-10-02 OPS CHECKS NORMAL.SDR ASAA2019020628080Satcom · malfunctionedSAT 1 AND SAT 2 UNAVAILABLE DURING FLIGHT (NOT READY). GROUNDED - YES. PERFORMED GOOD RESET OF SATCOM SYSTEM PER FIM 23-15-00-23-801. PERFORMED GOOD OPS TEST OF SATCOM NR 1 AND NR 2 PER AMM 23-15-00-730-801.SDR ASAA2019010627694Transceiver · failedSATCOM VOICE INOP. GROUNDED - YES. REMOVED AND INSTALLED NEW SATCOM XCEIVER REF AMM 23-15-00. PERFORMED OPS TEST REF AMM 23-15-00/501. SYS CKS NML.
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