N590AS
Service difficulty reports · 440
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 = 'N590AS' 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 = 'N590AS' 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 ASAA2016020215268Satcom · lockedSATCOM LOCK-UP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURES IAW QRH. SATCOM OPS NORMAL.SDR ASAA2016012014931Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.SDR ASAA2016011414835Control Valve · failedAT CRUISE MASTER CAUTION FOLLOWED BY A NR 2 BLEED TRIP OFF LGHT. FOLLOWED QRH RESUMED NORMAL OPS. ACFT GROUNDED. TROUBLESHOT IAW FIM 36-10, TASK 801. NO DEFECTS FOUND. NOTE: REPLACED PRECAUTIONARY NR 2 ENGINE PRECOOLER CONTROL VALVE IAW AMM 36-12-02. VERIFSDR ASAA2016011014719Warning Message · false activationFMC DISAGREE ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.SDR ASAA2016010814690Actuator · failedDURING ENGINE NR 1 START THE SPAR VALVE CLOSED LIGHT REMAINED BRIGHT WHILE START LEVER WAS IN IDLE DETENT. AFTER STARTER CUTOUT ENGINE VALVE CLOSED LIGHT WENT BRIGHT THEN DIM. THE ENGINE SHUTDOWN AT THAT TIME. SPAR VALVE LIGHT REMAINS BRIGHT WITH THE START SDR ASAA2015122014352Servo Control · failedAUTOTHROTTLE WILL NOT STAY ENGAGED. ACFT GROUNDED. AUTOTHROTTLE INFLIGHT FAULTS SHOWED 8 FAULTS OF ASM 1 RATE MONITOR. AUTO THROTTLE SERVO MOTOR TEST FAILED ASM 1. R & R ASM 1 IAW AMM 22-31-91-020-801/22-31-91-400-801. OPS CHECKS GOOD. PERFORMED ADDITIONASDR ASAA2015120314107Battery Pack · failedWHILE PERFORMING TASK CARD 78233001. THE EMERGENCY LIGHTS NEAR SEATS 16ABC, AND 25ABC, SEATS 16 THRU 24DEF, AND THE AFT GALLEY CENTER LOWER CEILING PANEL WENT OUT BEFORE THE 15 MIN LIMIT. AFTER A DEEP CYCLE CHARGE. ACFT GROUNDED. REMOVED, REPLACED, AND TESSDR ASAA2015112114238Power Supply · failedR2 DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. ACFT GROUNDED. RELAMPED R2 DOOR EGRESS LIGHT-NO HELP, REF AMM 33-51-04. R & R RT AFT EMERGENCY LIGHT POWER SUPPLY REF AMM 33-51-06. OPS CK GOOD.SDR ASAA2015111313760Satcom · malfunctionedSAT PHONE WILL CONNECT AND RECEIVE BUT WILL NOT TRANSMIT ON RADIOS 1 OR 2. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2015102913558Satcom · malfunctionedSATCOM PROMPT WAS MISSING. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE SATCOM LOCK-UP AND SATCOM WAS RESTORED. REF FIM 23-15, TASK 801, VERIFIED SATCOM PROMPT IN VIEW ON MENU PAGE. OPS NORMAL.SDR ASAA2015101513500Idg · malfunctionedNR 2 IDG FREQUENT SERVICING. ACFT GROUNDED. PERFORMED STATIC LEAK CHECK. NO PRESSURE DROP OR LEAKS DETECTED, IAW AMM 24-11-00-700-801. ALSO, OIL LEVEL WAS NOT WITHIN SIGHT GAUGE. IAW TSR, NR 2 IDG DUE REPLACEMENT. INSTALLED NEW IDG, OPS AND LEAK CHECK GOSDR ASAA2015100713393Idg · failed1 ENGINE DRIVE LIGHT ILLUMINATED. RAN CHECKLIST AND DISCONNECTED NR 1 DRIVE. ACFT GROUNDED. BITE CHECK OK, NO FUEL FOUND IN OIL. NO OIL IN SIGHT GLASS, EVIDENCE OF LEAKAGE FROM THE AIR/OIL COOLER IN THE C-DUCT, REF FIM 24-11, TSK 801, STEPS A-F. 4, A. REPLSDR ASAA2015091213023Warning Message · false activationDURING TAXI OUT FMC DISAGREE MESSAGE ILLUMINATED. ACFT GROUNDED. QRH PROCEDURE ACCOMPLISHED, FMC DISAGREE MESSAGE NO LONGER DISPLAYED.SDR ASAA2015083012961Servo · not reportedAUTOTHROTTLE WILL NOT ARM. ACFT GROUNDED. ACCOMPLISHED AUTOTHROTTLE SYSTEM OPS TEST, NO FAULTS NOTED, REF MM 22-31-00. DURING AUTOTHROTTLE SYS FAULT REVIEW FOUND 1 FLIGHT LEG WITH 24 INSTANCES OF MAINT MESSAGE 22-31501. AS PRECAUTION, REPLACED NR 1 AUTOTHRSDR ASAA2015082512901Fmc · malfunctionedDATALINK FULL MESSAGE. ACFT GROUNDED. FOLLOWED QRH IN 6.110, P19 AND FMC QRH ANOMALY CLEARED.SDR ASAA2015081812926Circuit Breaker · openSPAR VALVE ENGINE NR 1 CIRCUIT BREAKER OPEN. ACFT GROUNDED. CHECKED ENGINE, NR 1 SPAR VALVE C/B NO DAMAGE NOTED - RESET C/B, REF AMM 20-60-01. C/B REMAINS CLOSED, OK FOR CONTINUED SERVICE.
SDR ASAA2015081212858Warning Message · false activationFWD LT WINDOW HEAT OVERHEAT LIGHT ILLUMINATED AND REMAINS ILLUMINATED AFTER PERFORMING QRH CHECKLIST. ACFT GROUNDED. RECYCLED WINDOW HEAT BREAKER. LT WINDOW HEAT OPS CHECK GOOD IAW AMM 30-41-11.SDR ASAA2015072112532Control Valve · malfunctionedLEFT A/C PACK LIGHT ILLUMINATED ON RECALL, CANCELS WITH RESET. ACFT GROUNDED. PERFORMED PACK BITE TEST. FOUND FAULT WITH LT TEMP. CONTROL VALVE. REPLACED LT TEMP CONTROL VALVE REF AMM 21-51-10. OPS CHECK GOOD. PERFORMED PACK BITE TEST, NO FAULTS FOUND.SDR ASAA2015070312326Warning Message · false activationAFTER PUSHBACK AND ENGINE START FMC DISPLAYED FMC DISAGREE MESSAGE. ACFT GROUNDED. QRH PROCEDURE RESOLVED DISCREPANCY.SDR ASAA2015061012056Satcom · lockedSATCOM LOCK UP AFTER POWER CHANGE. ACFT GROUNDED. PERFORMED QRH PROCEDURE. SAT RESTORED.SDR ASAA2015052511847Hf Comm · malfunctionedCAPTAIN REPORTED HF NR 1 FAIL LIGHT ON WINDOW. HF1 OPS NORMAL. ACFT GROUNDED. RESET CONTROL HEAD FOR CAPTAIN VHF NR 1, HF NR 1 COMM BY RESETTING C/B'S P18-2-D11 AND P18-2-E11. PERFORMED GROUND VERIFICATION. OPS CHECK HF1, VHF1 RADIO. OPS CHECK NORMAL. NOSDR ASAA2015031010911Shim · wornREF T/C 78472002, NR 2 ENG FAN BLADE LUBRICATION . FOUND ALL 24 EA FAN BLADE SHIMS HAVE THE MOLYDAG COATING MISSING AND WORN TO BASE METAL. ACFT GROUNDED. INSTALLED 24 NEW FAN BLADE SHIMS, PN: 340-252-307-0 IAW TASK CARD NR 78472002 ON NR 2 ENGINE FAN BLADESSDR ASAA2015030410849Warning Message · false activationFMC DISAGREE AFTER PUSHBACK. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. MESSAGE CLEARED.SDR ASAA2015011510282Warning Message · illuminatedFMC DATALINK FULL MESSAGE IN FLIGHT. ACFT GROUNDED. FMC DISAGREE QRH RAN ON GROUND. OPS NORMAL.SDR ASAA2015011110224Lamp · failedCREW REPORTS EMERGENCY LIGHT LENS MISSING AT THE SIDE WALL OF THE RT FWD OVERWING EXIT. ACFT GROUNDED. REPLACED THE LAMP AND TESTED EMERGENCY LIGHT EXIT LOCATOR SIGN AT RT FORWARD OVERWING EXIT IAW MM 33-51-01-960-801. OPS NORMAL.SDR ASAA2015010610168Lens · missingROW 16 DEF, EMERGENCY EXIT LENS MISSING. ACFT GROUNDED. REPLACED THE LENS.SDR ASAA2015010310124Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ENGAGE DURING TAXI FOR T/O. ACFT GROUNDED. OPENSDR ASAA2014121509959Circuit Breaker · trippedCIRCUIT BREAKERS ON P6-2 ROW B, NR 2 AND 3 TRIPPED. ACFT GROUNDED. RESET CIRCUIT BREAKER`S AFCS SYS B MACH TRIM DC AND FCC DC IAW AMM 20-60-01. PERFROMED FCC B INSTALLATION TEST IAW AMM 22-11-33-400-801. ALL TEST PASSED.SDR ASAA2014120809896Warning Message · false activationAUTO FAIL LIGHT ILLUMINATED AFTER 80 KNOTS ON TAKEOFF. COMPLETED QRH AND SYS OPERATED NORMALLY IN ALTERNATIVE. ACFT GROUNDED. NR 2 CABIN PRESSURE CONTROLLER HAD FAULT CODE 57 LOGGED. ACCOMPLISHED SYSTEM TEST & CLEAR TEST. OPS NORMAL. FAULT WENT AWAY. ALL SDR ASAA2014120709890Servo · failedAUTOTHROTTLE WILL NOT STAY ARMED. ACFT GROUNDED. VERIFIED ASM-1 BAD. FAILS SERVO MOTOR TEST EVERY TIME REF MM 22-31-00 SYSTEMS TEST. REPLACED ASM NR 1. OPS NORMAL REF MM 22-31-91. VERIFIED SERVO MOTOR TEST OPS NORMAL REF MM 22-31-00 SYSTEMS TEST.SDR ASAA2014120209840Autothrottle Sys · malfunctionedAUTO THROTTLE WILL NOT STAY ARMED. ACFT GROUNDED. AUTOTHROTTLE CURRENT STATUS TEST PASSED. RAN SERVO TEST NUMEROUS TIMES ALL PASSED REF MM 22-31-00. REVIEWED FLT HISTORY, ASM 1 RATE MONITOR ONLY SHOWS ON FLT LEG 15 WITH NO OTHER OCCURRENCE, NO HISTORY PASTSDR ASAA2014112009717Lens · missingEMERGENCY LIGHT LENS MISSING AT SEAT ROW 16. ACFT GROUNDED. REPLACED EMERGENCY LIGHT LENS, OPS CHECKED GOOD IAW AMM 33-51-00.SDR ASAA2014111509674Warning Message · false activationFMC ANOMALY DATA LINK FULL ON GROUND. ACFT GROUNDED. PERFORMED FMC DISAGREE QRH PROC IAW F/A RUN. OPS CHECKED NORMAL.SDR ASAA2014111009629Warning Light · false activationAFTER RECALL, ZONE TEMP LIGHT FOR COCKPIT ILLUMINATED. ACFT GROUNDED. BOTH CONTROLLERS LOGGED COCKPIT TRIM VALVE FAULT. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE PROCEDURES IAW FIM 21-62, TASK 801 AND CLEARED FAULT. BOTH TEMP CONTROLLERS, OPS CHECKED GOOSDR ASAA2014102109447Servo · failedAUTOTHROTTLE DISENGAGES WITHIN APPROXIMATELY 10 SECONDS AFTER ENGAGING. ACFT GROUNDED. REPLACED NR 1 ASM IAW MM 22-31-91. GROUND CHECKS GOOD.SDR ASAA2014091109119Apu · faultedAPU CSS COMPLETED LESS THAN ONE HOUR PRIOR TO TOP OF DESCENT. FIRST ATTEMPT AT FL380 WAS UNSUCCESSFUL WITH A FAULT LIGHT. SECOND ATTEMPT AT FL380 WAS UNSUCCESSFUL WITH THE FAULT LIGHT. THIRD ATTEMPT AT FL310 HAD A SUCCESSFUL START. ACFT GROUNDED. REPLACED SDR ASAA2014090809084Converter · malfunctionedAPU FAULT LIGHT ILLUMINATED DURING APU START AT FL380. CSS REQUIRED ON DISPATCH RELEASE. ACFT GROUNDED. REPLACED APU START CONVERTER UNIT REF MM:49-41-61, OPS CK NORMAL.SDR ASAA2014090509063Circuit Breaker · trippedAUTOTHROTTLE FAILED, CIRCUIT BREAKER FOUND OPEN. ACFT GROUNDED. NO 90 DAY HISTORY. REVERSED SPECIAL PROCEDURES NR 2, REMOVED COLLAR AND CLOSED CIRCUIT BREAKER P18-1 E1 IAW SWPM 20-00-10. AUTOTHROTTLES OPS NORMAL IAW SYSTEM TEST, REF TASK 22-31-00-710-802.SDR ASAA2014083009008Warning Light · illuminatedFAULT LIGHT ILLUMINATED DURING APU START ATTEMPT AT FL400 SECOND START ATTEMPT AT FL 3200 SUCCESSFUL. ACFT GROUNDED. OPEN.SDR ASAA2014082208929Flow Divider · failedCSS PERFORMED AT 380, 4+ HRS INTO FLT. START FAILED APU FAULT LIGHT CAME ON. ONLY 1 ATTEMPT WAS MADE. ACFT GROUNDED. COMPLETED APU HARNESS & APU TO FIREWALL CONNECTOR GVI. NO DEFECTS NOTED. REPLACED APU FUEL FLOW DIVIDER & SOLENOID VALVE IAW AMM 49-31-15. SDR ASAA2014082008906Control Unit · leakingAPU FAULT LIGHT TWICE ON CSS START FLT 380+ FLT 310. ACFT GROUNDED. FUEL LEAKING FROM FUEL CONTROL DRAIN AT 2 DROPS IAW SECOND. R & R APU FUEL CONTROL UNIT OPS/LEAK CHECKS NORMAL REF AMM 49-31-11. PERFORMED APU BITE, NO FAULTS IN LAST RUN CYCLE, REF FIM TASDR ASAA2014072808810Skin · crackedCRACK NOTED ON LOWER SKIN OF RT HORIZONTAL STABILIZER. CRACK APPROXIMATELY ONE INCH LONG AND LOCATED JUST FWD OF REAR AT APPROXIMATELY STAB STA 96.5. ACFT GROUNDED. REPAIRED SKIN IAW SRM 55-10-01, REPAIR II.SDR ASAA2014072808798Skin · crackedCRACK NOTED ON LOWER SKIN OF RT HORIZONTAL STABILIZER. CRACK IS ONE INCH LONG AND LOCATED APPROX SEVENTEEN INCHES FWD OF REAR SPAR JUST INBD OF STABILIZER STA 138.7. CRACK IS CIRCLED IN RED. ACFT GROUNDED. REPAIR THE LOWER SKIN OF THE LOWER SKIN RT HORIZONSDR ASAA2014072408825Seat Track · crackedCRACK INDICATION FOUND LBL 24.75 OTBD FLANGE AFT HOLE, IN SEAT TRACK BS 727B. ACFT GROUNDED. REPAIRED FLANGE IAW EA SB737-53-1296-NG-120 .SDR ASAA2014072408824Seat Track · crackedCRACK INDICATION FOUND RBL 45.50 INBD FLANGE FWD & OTBD FLANGE FWD AND AFT HOLES IN SEAT TRACK BS 727B. ACFT GROUNDED, REPAIRED FLANGES IAW EA SB737-53-1296-NG-120.SDR ASAA2014072408823Seat Track · crackedCRACK INDICATION FOUND LBL 45.5 INBD FLANGE IN SEAT TRACK, BS 727B. ACFT GROUNDED. REPAIRED SEAT TRACK IAW EA SB 737-53-1296-NG-120 .SDR ASAA2014072308752Reveal · crackedAFT CARGO BAY DOOR SURROUND REVEAL PANEL 142KW HAS EDGE NICKS AND BARE METAL. ACFT GROUNDED. REMOVED THE EDGE DAMAGE; FOUND OUT OF LIMITS IAW SRM 53-60-15-01-1, FIG 103, SHEET 4. REPLACED THE NEW REVEAL PANEL 142-KW PN 146A9403-237, PO 810374.2 IAW SRM 51-10SDR ASAA2014072308751Reveal · crackedFWD CARGO BAY AFT DOOR SURROUND REVEAL PANEL 122DW HAS AN EDGE CRACK. ACFT GROUNDED. REPLACED THE REVEAL PANEL NR 122-DW, PN 143A9403-188, PO 817402.1 IAW SRM 53-30-15-01-1 AND 51-10-02-06-0.SDR ASAA2014071208530Seal · damagedNR 1 ENG OUTLET GUIDE VANE INBD SEAL TORN MISSING MATERIAL AT 9 O'CLOCK. ACFT GROUNDED. R & R OGV SEAL IAW AMM 72-23-01.SDR ASAA2014070808492Pressure Switch · malfunctionedNR 1 ENGINE FILTER BYPASS LIGHT ILLUMINATED DURING TAXI TO GATE. SHUTDOWN NR 1 ENGINE IMMEDIATELY. FILTER BYPASS LIGHT IMMEDIATELY EXTINGUISHED AND REMAINED OUT. ACFT GROUNDED. R & R FUEL DIFFERENTIAL PRESSURE SWITCH. PERFORMED EEC TEST NO FAULTS FOUND. R
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