N577AS
Service difficulty reports · 610
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 = 'N577AS' 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 = 'N577AS' 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 ASAA2013092696073Seat Track · gougedCABIN SEAT TRACK GOUGED AT BS 520, LBL 24. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-4 REPAIR 4.SDR ASAA2013091996084Floor Support · corrodedMAIN CABIN, FLOOR PANEL SUPPORT ANGLE IS CORRODED AT LBL12, FROM STA 328 TO 344. BS 328-BS 344, LBL 12, BLENDED CORRODED AREA ON SUPPORT ANGLE IAW SRM 53-10-51. ALLOWABLE DAMAGE 1, ALLOWABLE DAMAGE 1, ORIG THICKNESS 0.080. REMOVED 0.014, REMAINING 0.066, FOUSDR ASAA2013091996047Floor Support · damagedIN MAIN CABIN, FLOOR PANEL SUPPORT ANGLE IS SCRATCHED/HAS TOOLING MARKS AT LBL12, FROM STA 312 TO 329. BS312 - BS329, LBL 12. ACFT GROUNDED. BLENDED DAMAGE AREA ON SUPPORT ANGLE IAW SRM 53-10-51, ALLOWABLE DAMAGE 1. ORIG THICKNESS 0.080, REMOVED 0.011, RSDR ASAA2013091996045Floor Support · crackedCABIN FLOOR SUPPORT CRACKED, BS 312-328, LBL 45. R & R FLOOR SUPPORT IAW SRM 51-40-02 & BAC DWG 141A5410, REV B.SDR ASAA2013091996043Floor Support · crackedIN MAIN CABIN, FLOOR SUPPORT IS CRACKED AT LBL12, FROM BS 344 TO 360. R & R FLOOR SUPPORT IAW SRM 51-40-02 & BAC DWG 141A5410, REV B.SDR ASAA2013091996042Floor Support · crackedIN MAIN CABIN, FLOOR SUPPORT IS CRACKED AT BL0, FROM STA 344 TO 360, BS 344 -BS 360, BL0. R & R FLOOR SUPPORT IAW SRM 51-40-02 & BAC DWG 141A5410, REV B.SDR ASAA2013091995999Floor Support · crackedCABIN FLOOR SUPPORT CRACKED, BS 312-328, RBL32. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02.SDR ASAA2013091295970Valve · faultedWHILE PERFORMING T/C 78273000, FOUND NR 2 ENGINE FAULT 75-20462 HPTACC DEMAND & POSITION DISAGREE. ACFT GROUNDED. ACCOMPLISHED TASK CARD 78273000 AGAIN, NR 2 ENGINE FAULT REMAINS ACTIVE. REPLACED HPTACC IAW AMM 75-21-01 SYSTEM OPS CHECKED GOOD IAW AMM 71-00SDR ASAA2013082695889Warning Message · false activationVTK ON CAPTAINS NAV DISPLAY. ACFT GROUNDED. COULD NOT DUPLICATE. GROUND VERIFICATION, OPS CHECKED NORMAL, REF FIM34-61/801. NO FAULTS OR FAILURES LOGGED ON FMCS. NO HISTORY 30 DAYS.SDR ASAA2013073195709Warning Light · false activationRIGHT PACK LIGHT ILLUMINATES ON RECALL. ACFT GROUNDED. RT PACK LIGHT WAS NOT ACTIVE DURING RECALL REF FIM 21-62, TASK 848. BITE BOTH PACK ZONE TEMP CONTROLLER REF FIM 21-62 TASK 801 NO FAULTS LOGGED. NO HISTORY PAST 60 DAYS.SDR ASAA2013071295573Module · faultedAFTER LANDING ATTEMPTED APU START. NO START & FAULT LIGHT ILLUMINATED IAW QRH, SHUTOFF APU, WAITED FIVE MINUTES. AFTER FAULT LIGHT WENT OUT AND TRIED ANOTHER START, ANOTHER FAULT LIGHT. ACFT GROUNDED. ACCOMP APU BITE, BITE SHOWS SEVERAL FAULTS. CLEARED ALSDR ASAA2013070995535Fmc · malfunctionedSCRATCH PAD SINGLE FMC, OPS MESSAGE APPEAR IN BOTH CDUS FOLLOWED BY F/OS DU DISPLAYING MAP (AMBER) NO VTK DISPLAYED SHORTLY AFTER CRUISE. MODE ANNUNCIATOR IN CENTER DU DISPLAY WHITE BOX AT/LIM FOLLED BY BLANKING 05 THEN RESTORING NORMAL. CAPTAINS AMBER LDG/LTSDR ASAA2013070695484Transceiver · failedWEATHER RADAR DISPLAYS A SOLID GREEN RETURN FROM APPROX 40NM TO THE OUTER EDGE OF THE DISPLAY AT ALL RANGES, IN ALL MODES, AT ALL TILT POSITIONS AND AT ANY GAIN SETTING. ACFT GROUNDED. REPLACED WXR RT UNIT REF MM 34-43-41. GROUND FUNCTIONAL TEST PASSED.SDR ASAA2013063095358Radar · malfunctionedAFTER 1 & .5 HRS OF USE, RADAR SHOWED SOLID RETURNS REGARDLESS OF TILT POSITION. ACFT GROUNDED. PERFORMED WEATHER RADAR SYSTEM BITE PROCEDURE. NO FAULTS NOTED. NO HISTORY PAST 60 DAYS REF FIM 34-43, TASK 801.SDR ASAA2013061295093Fmc · false indicationWHILE ACCOMPLISHING TC 78273000, INTERROGATED THE FMC CDU FOR ENGINE FAULTS, FAULT CODE 73-20052 WAS ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED EEC TEST NO DEFECTS NOTED IAW MM 73-21-00.SDR ASAA2013041294453Warning Light · false activationAFTER PUSHBACK, ON RECALL, THE RT PACK LIGHT STAYED ILLUMINATED, EXTINGUISHED WITH MASTER CAUTION RESET BUTTON PUSHED. PERFORMED FIM 21-62 TASK 831, RT TCV AFTER LIGHT SHOWED ON THE BITE OF THE NR 2 ZONE TEMP CONT RAN VERIFY 2 TIMES WITH GO LIGHT BOTH TIMES. SDR ASAA2013040294321Terminal · looseLT FWD AND RT SIDE WINDOW OVERHEAT LIGHTS ON, QRH PROCEDURE COMPLIED WITH NO CHANGE. FOUND BUSS SIDE WIRE THAT FEEDS CIRCUIT BREAKER C227 RT SIDE WINDOW HEAT CONTROL AND CIRCUIT BREAKER C224 LT FRONT WINDOW HEAT CONTROL TERMINAL LUG LOOSE AND OVERHEATED ON CSDR ASAA2013032094228Transmitter · malfunctionedAFTER FLT 854, PILOTS VERBALIZED NR 2 ENG F/F UP TO 300LBS/HR HIGHER THAN NR 1 ENG & FUEL USED SHOWED 1000LBS HIGHER THAN SCHEDULED BURN AFTER 4 1/2 HR FLT DURATION. ALSO, FUEL USED 28K, 10K FUEL REMAINING END-OF-FLT = 38K BUT DEPARTURE FUEL WAS 37K. OTHER SDR ASAA2013021293868Wire · damagedNR 2 COWL VALVE LIGHT GOES FROM BRIGHT, OFF AND DIM. POSITION IS INOPERATIVE. MANUALLY CYCLED RT COWL TAI VALVE, LIGHT GOES FROM BRIGHT TO DIM WITH ENG BLEED AIR, LIGHT GOES FROM BRIGHT TO OFF. REPLACED A/I VALVE REF MM 30-21-11-400, STEPS 3A-3H(5). FOUND WSDR ASAA2013021293869Warning Light · false activationON WINDOW, PITOT HEAT MODULE OVERHEAT LIGHT REMAINS ON FOR LT FWD AND RT SIDE WINDOWS. RESET SIX PACK AFTER TRYING SYS TEST AND EVERYTHING WENT TO NORMAL OPERATION. TRIED TO GET SYS TO FAIL AGAIN BUT IT WOULDNT FAIL. GROUND FUNCTIONAL GOOD IAW AMM 30-41-00SDR ASAA2013012593745Controller · malfunctionedCONTROL CAB ZONE TEMP LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. PERFORMED AN OPS CHECK OF THE PACK SYSTEMS IAW AMM 21-00-00. ALSO, PERFORMED A BITE CHECK OF THE ZONE TEMP CONTROLLERS. NO FAULTS NOTED. OK FOR SERVICE.SDR ASAA2013011793701Module · leakingDURING ETOPS PDC FOUND OIL STREAMING OUT OF APU COWLING DRAIN MAST. REPLACED APU LUBE MODULE REF AMM 49-91-11-400-802, OPS CHECKED GOOD.SDR ASAA2012122793571Terminal · looseRIGHT SIDE WINDSHIELD WINDOW OVERHEAT LIGHT ON AT 2000FT 150 IAS, 2-5 TAT WHILE ON APPROACH. RT WHCU SHOWS SENSOR FAULT. FRONT TERMINAL LOOSE -SECURED LUG FOR A H-15 WINDOW BOTH PRIMARY & SECONDARY SENSORS 100 ARE OUT OF TOLERANCE, REF MM 30-41-21, WDM 30-41SDR ASAA2012122693550Control Unit · malfunctionedON CLIMBOUT PASSING 26000 FT, RT SIDE WINDOW OVERHEAT LIGHT CAME ON. FOLLOWED QRH, RETURNED TO NORMAL OPS. REMOVED & REINSTALLED R2 WINDOW. SEALS GOOD. HISTORY SHOWS SENSOR FAULT. SENSOR OHMS GOOD & TERMINALS ARE TIGHT, REF MM 30-41-21. REPLACED R2 WISDR ASAA2012122593540Wire · inoperativeRIGHT SIDE OVERHEAT LIGHT ILLUMINATED ON SHORT FINAL, APPROX 1500 FT, AFTER LANDING ACCOMPLISHED QRH. LEFT SWITCH IN OFF POSITION. TURNED RT SIDE WINDOW HEAT ON. 10 MINUTES LATER OVERHEAT LIGHT CAME ON. PERFORMED MM 30-41-21 TO CHECK RESISTANCE OF RT SIDE SDR ASAA2012122393532Fmc · malfunctionedSINGLE FMC OPERATION ANNUNCIATED IN FLIGHT. SELECTED BOTH ON LEFT TO RESTORE COPILOTS DISPLAY. TESTED IAW FIM 34-61 TASK 807, NO FAULTS, INTERMITTENT, NO FURTHER ACTION REQUIRED.SDR ASAA2012121293455Warning Message · false activationSHORT TERM MX MESSAGE 73-20052, FOUND ON THE NR 2 ENG (INTERNAL EEC FAULT). TESTED NR 2 EEC IAW FIM TASK 73-21-00-700-804-F00. NO FAULTS INDICATED. ALSO, NO MX HISTORY FOR THE PAST 30 DAYS. THIS IS A ONE TIME ONLY INTERMITTENT FAULT.SDR ASAA2012112393335Warning Light · false activationRT PACK LIGHT ILLUMINATES ON RECALL. EXTINGUISHES ON MASTER CAUTION RESET. TROUBLESHOT PACK FAULT INTERMITTENT IAW SAME & OPS NORMAL IAW SAME.SDR ASAA2012111293289Display · inoperativeCAPTAIN`S MCDU L6 BUTTON DOESN`T CLICK WHEN PUSHED. REPLACED CAPT MCDU REF MM 34-61-01. OPS NORMAL REF SAME.SDR ASAA2012110893276Indicator · intermittentNR 1 REFUEL QTY INDICATOR AT REFUEL PANEL INOPERATIVE. UNIT IS INTERMITTENT, REPLACED NR 1 REFUEL QUANTITY INDICATIOR IN RT WING, OPS CHECK GOOD. MM REF 28-41-61. GROUND FUNCTIONAL TEST GOOD IAW AMM 28-41-61-400-801, PARA 3 H.SDR ASAA2012110393232Hmu · faultedNR 1 ENGINE FLUCTUATIONS DURING CRUISE. ENGINE FLUCTUATED BETWEEN APPROX 82 AND 96 FOR APPOX 5-10 CYCLES. FEEDING FUEL FROM MAIN TANK NR 2 FOR FUEL BALANCE. PERFORMED AN ENGINE STALL/SURGE CHECKLIST. ENGINE RETURNED TO NORMAL. ENGINE CONTROL LIGHT ILLUMINASDR ASAA2012090492825Warning Light · illuminatedAFTER ENGINE START, LIGHT ON. ACCOMPLISHED FIM TASK 24-34-00 SPCU INOP MESSAGE. FAULT CLEARED. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2012092892964Control Valve · malfunctionedRT PACK LIGHT ILLUMINATED ON RECALL. NR 2 CONTROLLER SHOWS TEMP CONTROL VALVE, RT PACK FAULT ON LAST FLT. RESET FAULT. FAULT DID NOT RETURN. VERIFY BITE TEST NR 2 CONTROLLER, PASSED. FUNCTIONAL CHECK OF RT PACK TEMP CONTROL VALVE GOOD. GROUND VERIFICATIOSDR ASAA2012092492951Gauge · false indicationFUEL PANEL TANK NR 1, LOWER GAUGE DISPLAY INDICATES 88888 AND LBS 000. PERFORMED FQS OPS TEST IAW AMM TASK 28-41-00-710-801. RESET REFUEL PANEL QTY GAUGE BY RESETTING POWER. OPS CHECKED OK.SDR ASAA2012091592901Bleed Valve · failedDUCT SPLIT DURING CLIMB PARAMETERS RECORDED AS FOLLOWS CLIMB THROUGH FL 270, L21 PSI, R 45 PSI, N1 99.9, N2 98.3, SAT-33C. CLIMB THROUGH FL 320, L22 PSI, R 46 PSI, N1 99.8, N2 97.5, SAT-44C. CLIMB THROUGH FL 340, L23 PSI, R 43 PSI, N1 100.3, N2 96.3, SAT -5SDR ASAA2012070192450Warning Light · false activationFMC DISAGREE MESSAGE ON BOTH CDU APPEARED ALONG WITH THE AMBER FMC ALERT LIGHT ON EACH PILOTS INSTRUMENT PANEL. THIS OCCURRED AFTER PUSHBACK.FOLLOWED THE QRH CHECKLIST. OPS NORMAL.SDR ASAA2012061192330Warning Light · illuminatedMINUTES PRIOR TO PUSH IN OGG FMC DISAGREE MESSAGE DISPLAYED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURES. OPS NORMAL RESTORED.SDR ASAA12511580Scavenge Pump · contaminatedSMALL AMOUNT FOUND NON MAGNETIC SILVER FLAKING MATERIAL IN REAR SUMP SCAVENGE MCD NR 2 ENG. ACFT GROUNDED. ON DEFERRAL.SDR ASAA12511510Fmc · false indicationON TAXI OUT, RECEIVED AN FMC DISAGREE MESSAGE. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. MESSAGE WENT AWAY. FMC'S OPS NORMAL.SDR ASAA2012052111496Scavenge Pump · making metalSMALL AMOUNT FOUND NON MAGNETIC SILVER FLAKING MATERIAL IN REAR SUMP SCAVENGE MCD, NR 2 ENG. ACFT GROUNDED. COMPLETED INSPECTION NR 2 ENGINE REAR SUMP, NO MATERIAL FOUND, REF AMM 79-00-00.SDR ASAA12511449Radar · malfunctionedWEATHER RADAR SHOWS "SPIKING" ALL QUADRANTS OF DISPLAY. SPIKING OCCURED AT CRUSE AS WELL AS DESCENT & AT ALL TILT & CALIBRATION SETTINGS. PREFORMED TASK 34-43-00-710-802-001, WXR SYS OPS TEST. NO PROBLEMS NOTED. OK FOR SERVICE.SDR ASAA12511453Control Panel · inoperativeF/O COURSE WINDOW INOPERATIVE, ACFT GROUNDED. CYCLED MCP NR 1 DC CIRUCIT BREAKER, DISPLAY CAME UP NORMALLY FOR A FEW SECONDS AND WENT BACK OUT AGAIN. REPLACED MCP REF MM 22-11-34, OPS CHECKED NORMAL. ACCOMPLISHED ALL MCP LWMP CHECKS PER CHECKLIST MM 22-0-01 SDR ASAA12511434Autopilot Sys · malfunctionedF/O COURSE SELECTOR WINDOW ON MCP INOPERATIVE. ON SUBSEQUENT FLIGHT TOGA BUTTON DOES NOT ACTIVATE 'PITCH GUIDANCE' UNTIL AIRBORNE. NR 1 CMD A/P WILL NOT ENGAGE. F/O CMD A/P WILL ENGAGE. DUPLICATED PROBLEMS FOUND MCP NR 1 DC C/B OUT. INSPECTED C/B & PANEL ARESDR ASAA12511430Warning Light · false activationFMC DISAGREE LIGHT ILLUMINATED ON TAXI. ACCOMPLISHED QRH. OPS NORMAL.SDR ASAA12511363Housing · leakingAPU HAS A HISTORY OF OIL SERVICING. CURRENT OIL CONSUMPTION IS STILL WITHIN LIMITS AT .02 QPH BUT IS HIGHER THAN EXPECTED. PERFORMED AMM TASK 49-95-00-810-801, APU OIL CONSUMPTION HIGH FAULT ISOLATION. FOUND LUBE FILTER HOUSING LOOSE AND LEAKING OIL. REPLASDR ASAA12511342Magnetic Seal · leakingNR 1 ENGINE HAS HISTORY OF OIL UNDER ENGINE FOUND DURING WALK AROUND. WHEN PERFORMING PART POWER LEAK CHECK FOUND NR 1 ENG IDG PAD LEAKING OUT OF SERVICABLE LIMITS. REMOVED & REPLACED MAGNETIC SEAL AMM REF 72-60-00-000-801-F00 REMOVED & RE-INSTALLED NR 1 IDGSDR ASAA12511313Fmc · malfunctionedAFTER TAXI OUT, FMC DISAGREE MESSAGE ON BOTH ND'S. ACCOMPLISHED QRH CHECKLIST. FMC DISAGREE MESSAGE DISAPPEARED.SDR ASAA12511249Controller · faultyCABIN PRESSURE AUTO FAIL LT ILLUMINATED ALTN MODE LT ILLUMINATED CABIN PRESSURE NORMAL. VERIFIED DEFECT. NR 2 CPC EXISTING FAULT SHOWS CONTRLR LRU FAIL. REMOVED AND REPLACED NR 2 CPC REF MM 21 31 01. OPS CHECK NORMAL.SDR ASAA12511211Unknown · malfunctionedAFTER T/O VNAV SELECTED A/S BUG ON BOTH PILOT FLT DISPLAYS INDICATED UP INSTEAD OF 250 KTS. FLAPS WERE FULLY RETRACTED. THIS PROBLEM CONTINUED TO LEVEL OFF AT 34 000FT WITH MULTIPLE ATTEMPTS AT VNAV & LVL CHANGE. LVL CHG WAS OK. CLIMB PAGE ANNUNCIATED 212 SDR ASAA12511149O-Ring · damagedNR 2 ENG HYD PUMP LEAKING. CK'D AND FOUND HYD CASE DRAIN UNION ON NR 2 EDP LEAKING AT BASE. REMOVED AND REPLACED O-RING ON CASE DRAIN UNION REF 29 11 11 AND AMM TASK 70 30 01 910 802 F00. LEAK CK GOOD ON ENG.
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