N597AS
Service difficulty reports · 401
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 = 'N597AS' 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 = 'N597AS' 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 ASAA2013020493825Controller · malfunctionedON RECALL CONT CAB ZONE TEMP LIGHT ILLUMINATES AND EXTINGUISHES WITH PUSH TO RESET. FOUND FAULT ON NR 2 CONTROLLER FLIGHT DECK TRIM VALVE. ACCOMPLISHED RESET AND TEST PROCEDURES IAW TASK 21-61-20-400-801. FAULT CLEARED AND DID NOT REAPPEAR.SDR ASAA2013020293796Overheat Sys · malfunctionedCAPTAIN SIDE ON 6 PACK MASTER CAUTION OVERHEAT DETECTOR WILL NOT ILLUMINATE ON FIRE FAULT INOPERATIVE OR OVERHEAT FIRE SELF TEST. ACFT GROUNDED. ACCOMPLISHED MASTER CAUTION DISPLAY TROUBLESHOOTING IAW FIM TASK 31-52-00-810-802. RECYCLED OVERHEAT DETECTION MSDR ASAA2013012493753Ignition Lead · failedAPU FAILED TO START. NO FLAME SHUTDOWN FAULT CODE 49-41011. REPLACED APU IGNITION UNIT REF AMM 49-41-31. REPLACED APU IGNITER PLUG REF AMM 49-41-51. REPLACED APU IGNITER PLUG LEAD REF AMM 49-41-52. PERFORMED APU IGNITION UNIT, IGNITER PLUG AND IGNITER PLUSDR ASAA2013012093719Igniter · inoperativeAPU INOP, DUE TO NO FLAME SHUTDOWN, FAULT CODE 49-41011. ACFT GROUNDED. PERFORMED FIM TASK 49-40 TASK 802 BITE CHECKS NO CURRENT FAULTS, START/OPERATION/SHUTDOWN CHECKS GOOD, INLET PLENUM AND COMPRESSOR INLET CLEAR. BITE CHECKS GOOD 5 START CYCLES, NO HISTORSDR ASAA2013011093666Panel · wornNR 2 ENGINE FAN DUCT PANEL AT 200 POSITION LOWER MIDDLE BOLT PULLING THROUGH HOLE. R & R NR 2 ENGINE FAN DUCT PANEL IAW AMM 72-23-07-000-801.SDR ASAA2013010493616Fuel Cell · contaminatedNR 1 AND 2 FUEL TANK GUAGES ERRATIC. FLUCUATIONS UP TO 800 LBS IN NR 2 TANK AND UP TO 400 LBS IN NR 1 TANK, WHILE BURNING FROM CENTER TANK. FLUCTUATIONS CEASED ONCE LEVEL. CRUISE ALTITUDE OF FL340 AFTER APPROX 30 MIN. REMAINDER OF FLIGHT FUEL BURN PLUS TOTASDR ASAA2012122393536Apu · unknownFOLLOWING GROUND POWER INTERRUPTION APU INDICATES FAULT ON START. WILL NOT START. RESTARTED APU AFTER 5 MINUTES. APU STARTED NORMAL, NO FAULT LIGHT ILLUMINATED, NO HISTORY ON LAST 30 DAYS. OK FOR SERVICE.SDR ASAA2012112393364Modulating Valve · malfunctionedCONTROL CABIN ZONE TEMP ILLUM DURING RECALL AFTER START- EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. R & R ZONE TRIM AIR MODULATING VALVE. REF AMM 21-61-21. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE CK. NO FAULTS NOTED. LK CKD GOOD.SDR ASAA2012111993326Warning Light · false activationFMC DISSAGREE LIGHT CAME ON AFTER PUSH. ACCOMPLISHED QRH PROCEDURE. NORMAL OPS RESTORED.SDR ASAA2012111993322Warning Light · illuminatedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATES ON RECALL, LIGHT RESETS NORMALLY. NR 2 CONTROLLER LOGGED FLT DECK TRIM VALVE FAULT. NO HISTORY-FAULT RESET. RAN PACK-TEMP CONTROL NORMAL. NO CURRENT FAULTS, GROUND VERIFICATION SUCCESSFUL REF FIM 21-62, TASK 842.SDR ASAA2012111393295Controller · malfunctionedON PREFLIGHT, NOTICED PRESSURIZATION CONTROL PANEL AUTO FAIL AND ALTN LIGHTS ILLUMINATED WITH MODE SELECTOR IN AUTO POSITION. RESET CABIN PRESSURE CONTROLLER BY TURNING SELECTOR TO MANUAL THEN BACK TO AUTO. CONTROLLER RESET. PERFORMED GROUND VERIFICATION. SDR ASAA2012090992857Warning Light · false activationFMC DISAGREE ON TAXI OUT. FOLLOWED QRH PROCEDURE AND RESET 2 CBS. FMC OPS NORMAL.SDR ASAA2012090492824Filter · cloggedNR 1 IDG DPI EXTENDED. ACFT GROUNDED. THIS IS THE 2ND NR 1 ENG DPI OCCURANCE. R & R IDG SCAVENGE AND CHARGE FILTER. NO DEFECTS ON REMOVED FILTERS. RESET DPI AND SERVICED IDG. OPS AND LK CKS GOOD. ALL REF MM 24-11-41-200-801.SDR ASAA2012090392819Warning Light · false activationFMC LIGHT ILLUMINATED DURING TAXI. ACFT GROUNDED. COMPLIED WITH QRH FMC LIGHT EXTINGUISHED.SDR ASAA2012091592892Warning Light · false activationAPU FAULT LIGHT ILLUMINATED DURING APU START, LIGHT WENT OUT WHEN SWITCHED TO OFF. SECOND APU START WAS NORMAL. PERFORMED APU OPS TEST IAW AMM 49-11-00-701-801. APU CHECKS NORMAL. NO FAULTS ON CURRENT STATUS.SDR ASAA2012070792498Warning Light · false activationAFTER ENGINE START, RECEIVED AN FMC DISAGREE LIGHT. RAN QRH PROCEDURE. LIGHT CLEARED, CONTINUED NORMAL OPERATIONS.SDR ASAA2012070692483Control Valve · failedRT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL. EXTINGUISHES WHEN MASTER CAUTION RESET. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST IAW MM 21-61-00. CONFIRMED FAULT, FOUND HARD FAIL ON NR 2 CONTROLLER, THIS PACK TEMP CONTROL VALVE. R & R TEMP CONTROLSDR ASAA2012070592476Controller · malfunctionedRT PACK LIGHT ILLUMINATES ON MASTER RECALL RECALL-EXTINGUISHES WHEN MASTER CAUTION IS RESET. NR1 CONTROLLER SHOWS STANDBY CONTROLLER FAULT, NR2 CONTROLLER SHOWS TCV FAULT. BOTH FAULTS RESET,VERIFIED. RAN BOTH PACKS REF MM 21-61-00, OPS NORMAL, SAME. GROUNDSDR ASAA2012070392464Start Valve · failedNR 2 ENGINE WOULD NOT START, NO ROTATION. R & R NR 2 ENGINE START VALVE IAW MM 80-11-03-00-801-F00. OPS AND LEAK CHECKED GOOD.SDR ASAA2012072192573Seal · tornNR 2 ENG FAN BLADE LUBE FOUND 10 PLATFORMS WITH TORN RUBBER SEALS. ACFT GROUNDED. INSTALLED 10 NEW FAN BLADE PLATFORMS IAW TC 78472002. ACCOMPLISHED VIBRATION SURVEY TEST 7 IAW AMM 71-00-00, NR 2 ENG VIB WITHIN LIMITS.SDR ASAA2012071192526Line · leakingON CLIMB, RT DUCT PRESSURE 14 PSI LT DUCT PRES 39PSI AT CRUISE BOTH 38 PSI. ACFT GROUNDED. R & R NR 2 ENGINE BAR IAW MM 36-11-03-400-801 AND NR 2 ENGINE PRSOV IAW MM 36-11-04-400-801. HEALTH CHECK ACCOMPLISHED IAW MM 36-11-00-700-801. FAILED ENGINE RUN, DUSDR ASAA12511619Controller · malfunctionedRT "PACK" ILLUMINATED ON RECALL. ACFT GROUNDED. PERFORMED FIM TASK 21-53-00-810-804, RTT PACK LIGHT ON STAYS OFF AFTER RESET. FOUND NR 2 CONTROLLER LOGGED "THIS PACK TCV" FAULT. RESET CONTROLLER AND OPERATED PACK. GROUND VERIFICATION TESTS NORMAL.SDR ASAA12511558Connector · looseNR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED ON TAXI. ACFT GROUNDED. FOUND CONNECTOR PLUG FOR NR 2 ENGINE FUEL DIFFERENTIAL PRESSURE SWITCH LOOSE AND COVERED WITH SURFACE CORROSION. CLEANED CONNECTOR AND SWITCH. RESECURED CONNECTOR AND PERFORMED NR 2 ENGINE RSDR ASAA12511276Unknown · malfunctionedAUTOTHROTTLES WILL NOT REMAIN ENGAGED. PERFORMED CURRENT STATUS TEST SERVO MOTOR TEST AND TORQUE TEST. NO FAULTS AND NO HISTORY 60 DAYS.SDR ASAA12511189Autothrottle Sys · malfunctionedAUTOTHROTTLE DISENGAGED AFTER TAKEOFF UNABLE TO RE-ENGAGE NO C/B'S POPPED. UNABLE TO DUP/VERIFY DISCREP REF FIMS 22 32 TASK 806 FIM 22 31 TASK 801/805 FLT FAULT REVIEW SHOWED ASM 2 RATE MONITOR FAULT. PERFORMED A/T CURRENT STATUS BITE AND INTERACTIVE SERVO MSDR ASAA12511122Control Valve · malfunctionedAFTER ENGINE START ON GROUND CONT CAB ZONE TEMP LIGHT ILLUMINATED UPON RECALL. LIGHT CANCELS WITH MASTER CAUTION RESET PER QRH PROCEDURE. PERFORMED FIM TASK 21-62-00-810-842 CONTROL CABIN ZONE TEMP LIGHT ON AND STAY OFF AFTER RESET. CONFIRMED FAULT TCV FAULSDR ASAA12511000Filter Element · defectiveNR 1 IDG DPI RED INDICATOR EXTENDED. PERFORMED FIM TASK 24 11 00 810 803 IDG DPI FAULT ISOLATION INTERROGATED FMC CDU TC 78273000. FILTER INSP COMPLETED REF: TC 78424000 CHANGED OIL REF: TC 78424000 OPS CHECKED GOOD LEAK CHECKED GOOD.SDR ASAA1250973Apu · leakingAIRCRAFT HAS "DIRTY SOCK" SMELL ON TAKEOFF AND DESCENT. ACCOMPLISHED TASK 05 60 00 280 801C1 PARAGRAPH 2A THRU 2E RAW OIL FOUND IN THE INTERNAL AREAS OF THE DRAIN CAVITY APU REQUIRES REPLACEMENT. REPLACED APU OPS/LEAK CHECKED APU PER T/C 78349010. NO EVIDENSDR ASAA12510972Unknown · malfunctionedAUTO THROTTLE WON'T ENGAGE. A/T BITE TEST NORMAL PER MM 22 31 10 401 & FIM 22 11 T802.SDR ASAA201121210802Outflow Valve · damagedAFT ANTI SKID MATERIAL MISSING & TORN ON OUTFLOW VALVE. ACFT GROUNDED. REMOVED DAMAGED ANTI SKID FOIL FROM AFT OUTFLOW VALVE IAW AMM 21-31-03-000-801. ACCOMPLISHED EA 2130-01028.SDR ASAA11510709Window · malfunctionedCO-PILOT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. ACCOMP FIM 30 41 00 810 811 STEP G SENSOR USED RANG 390OHMS. SPARE RANG 386 OHMS. ACCOMP OPS TEST WINDOW HEAT AMM 30 41 0 710 801. WINDOW HEATED TO 150'. ON PWR TEST AFTER OVERHEAT ILLUMINATED AND ON LSDR ASAA11510698Unknown · malfunctionedON RECALL CONT CAB ZONE TEMP LIGHT ILLUMINATES EXTINGUISHES WITH MASTER CAUTION RESET. NR 2 TEMP CONTROLLER LOGGED FLT DECK TRIM VALVE FAULT. FAULT RESET OK. CURRENT STATUS NORMAL. GROUND VERIFICATION SUCCESSFUL. REF FIM 21 62 TASK 842. M/M BITE PROCEDURESDR ASAA11510370Igniter · meltedDURING NR 2 ENGINE START NO EGT. MOTORED ENGINE AT 27 PERCENT N2 FOLLOWED QRH AND SHUT IT DOWN. (IGN SWITCH IN IGN R POSITION). REMOVED NR 2 ENGINE INGNITER R PLUG IN REF AMM 74 21 02. FOUND PLUG MELTED. INSTALLED NEW SERVICE ALB IGNITER PLUG IN REF AMM 7SDR ASAA11510019Idg · failedNR 1 GEN SOURCE OFF LIGHT CAME ON IN FLIGHT WOULD NOT RESET / APU COVERED THE BUS. GCU 1 SHOWS IDG FAULT. REPLACED NR 1 ENG IDG PER MM 24 11 11 000 801 AND 24 11 11 400 801. PERFORMED OPERATIONAL TEST REF AMM 24 11 00 700 802. OPS CHECK GOOD.SDR ASAA1159879Unknown · malfunctionedAUTO THROTTLE DC 1 CIRCUIT BREAKER POPPED D 18 1 E1. RESET AUTO THROTTLE DC 1 CIRCUIT BREAKER AND TEST GOOD IAW B737NG AMM 22 31 00.SDR ASAA1159819Shutoff Valve · failedPERFORMED NR 2 ENGINE BLEED AIR HEALTH CHECK. PRSOV AND HIGH STAGE VALVE FAILED. NR 2 PRSOV REPLACED AND INSTALLATION TEST GOOD IAW B737NG MM 36 11 04. NR 2 HIGH STAGE VALVE REPLACED AND INSTALLATION TEST GOOD IAW B737NG MM 36 11 08.SDR ASAA1159725Transceiver · looseWEATHER RADAR IS "SPOKING" OTHERWISE OPERATES OK. FOUND RADAR TRANSCEIVER LOOSE IN RACK. RE-SECURED SYS TESTS GOOD.SDR ASAA1159646Starter · failedWHILE TRYING TO START ENG NR 1 IT ONLY REACHED 21 22 PERCENT AND STARTED TO ROLL BACK. THIS WAS ACCOMPANIED BY A LOUD WHINING NOISE. ALSO THE RAMP REPORTED SPARKS COMING FROM THE MOTOR. FUEL WAS NEVER INTRODUCED. REMOVED AND INSTALLED NEW STARTER ON THE NRSDR ASAA1159616Cdu · defectiveCAPTS MCDU IS VERY DIM AT MAXIMUM BRIGHTNESS SETTINGS. UNIT IS STILL USABLE DISPLAY IS NOT ABLE TO BE MADE BRIGHT ENOUGH IN A BRIGHTLY LIT COCKPIT. REPLACED CAPT MCDU. INSTALLATION TEST GOOD REF AMM 34 61 01.SDR ASAA1159499Valve · failedON TAKEOFF PASSING 2000FT W/ PWR AT 940 N1 LEFT PACK DUCT PRESSURE = 90 PSI POWER PULLED BACK TO 70.0 N1 LEFT DUCT PRESS = 70 PSI. PWR AT IDLE LEFT DUCT PRESS = 45 PSI (RIGHT=35 PSI). PWR 60.0 N1 LEFT DUCT PRESS = 60 PSI. PRESSURIZATION = NORMAL. LEFT PACKSDR ASAA1159459Servo · failedAUTO THROTTLE WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 AT SERVO MOTOR IAW AMM TASK 22 31 91 400 801, OPS CHECK NORMAL.SDR ASAA1159236Unknown · malfunctionedWX RADAR PRESENTS FALSE RETURNS AT 60, 70 DEG LEFT AND RIGHT AT APPROX 5 MILES. REF FIM 34 43 TASK 802. PERFORMED WXR OPERATIONAL TEST PER MM 34 43 00 710 802 001 NO FAULTS NOTED. ALSO PERFORMED WXR BITE PER MM 34 43 00 810 801 NO FAULTS FOUND. NO HISTORY SDR ASAA1158792Unknown · malfunctionedUPON RECALL CONT CABIN ZONE TEMP LIGHT ILLUMINATES. EXTINGUISHES W/MASTER CAUTION RESET. PERFORMED PACK/ZONE TEMPERATURE CONTROLLER BITE TEST. NO FAULTS LOGGED. PERFORMED CABIN TEMPERATURE CONTROL & INDICATION OPERATIONAL TEST. OPS CHECK GOOD. REF AMM 21SDR ASAA1158787Apu · malfunctionedON DESCENT AT APPROX 15,000 MSL THERE WAS A STRONG SMELL OF DIRTY SOCKS IN BOTH THE COCKPIT AND PASSENGER CABIN. ODOR CONTINUED THROUGH 10,000 MSL TO LANDING. DURING INITIAL EVALUATION STARTED APU AND OPERATED BOTH LEFT AND RIGHT A/C PACKS. DETERMINED THERESDR ASAA1058651Unknown · malfunctionedGOT FAIL LIGHT ON NR 2 HF. REBOOTED HF 2 PERFORMED FIM 23 11 00 810 803 BITE TESTED PER MM 23 11 00 810 801 TESTS OK, NO HISTORY.SDR ASAA1058667Gearbox · making metalWHILE ACCOMPLISHING T/C 78472040 AGB/TGB CHIP DETECTORS INSPECTION FOUND ALUMINUM DEBRIS IN NR 1 ENGINE AGB/TGB CHIP DETECTOR. NR 1 ENGINE AGB TGB CHIPS DETERMINED TO BE SILVER FLAKING NO MAGNETIC MATERIAL NOTED. CHIPS ROUTED FOR LAB ANALYSIS. ENGINE MAY COSDR ASAA1058587Unknown · malfunctionedAPU ELECTRICS DROPPED OFF LINE 2 TIMES. GVI ON APU NO DEFECT FOUND. APU GCU LRU TEST PASSED. APU BITE NO CURRENT FAULT NO RELATED FAULT FOUND ON FAULT HISTORY & NO HISTORY IN TRAX. PERFORMED OPERATIONAL TEST FOR AC GENERATION & CONTROL SYSTEM REF MM 24 21 SDR ASAA1058542Filter · defectiveNR 1 ENGINE IDG DELTA P FOUND POPPED. REMOVED & REPLACED NR 1 ENG IDG SCAVENGE FILTER. DRAINED & RESERVICED OIL. 1ST IDG DELTA P PIN POPPED & FILTER CHANGE. PLACARD MARKED TO INDICATE. LEAK & OPS CHECK GOOD AMM REF 24 11 41.SDR ASAA1058538Control Panel · failedF/O AUTOPILOT WOULD NOT ENGAGE. NR 1 ENGAGED OK. REPLACED AUTO PILOT MODE CONTROL PANEL PER MM 22 11 34/401 DFGS TEST FOR MCP LAND VERIFY & HGS SENSOR TEST FOR FCC/AT CHECKS GOOD. VERIFICATION AUTOLAND SUCCESSFUL.SDR ASAA1058470Idg · failedNR 2 DRIVE LIGHT ILLUMINATED. SHOWING 0 VOLTS 0 FREQUENCY ON GENERATOR NR 2. TROUBLESHOT PER TASK 24 11 11 01A. NO VOLTS OR FREQS. GCU BITE PER TASK 24 21 00 810 801 INDICATES FAULTY IDG. REPLACED NR 2 ENGINE IDG PER MM 24 11 11 400 801 ALL OPS CHECKS NORM
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