N583AS

Service difficulty reports · 465

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 = 'N583AS' 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.

SDR ASAA0956040Inlet Bullet · wornNR 1 ENG FRONT CONE WORN. REMOVED AND REPLACED NR 1 ENG FRONT CONE REF MM 72 21 01 400 801.Jun 27, 2009 · N583AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA0955564Sensor · defectiveFWD LEFT WINDOW OVERHEAT LIGHT ILLUMINATED. VERIFIED L1 WINDOW PRIMARY TEMP SENSOR BAD SPARE TEMP SENSOR GOOD, S1078 S/W POSITIONED FOR SPARE SENSOR REF MM TASK 30 41 00 810 812. WINDOW HEAT OPS NORMAL REF MM TASK 30 41 00 710 801.May 10, 2009 · N583AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0955402Fmc · malfunctionedNR 2 FMC INOP. PERFORMED FMC GND VERIFICATION TEST PER M/M 34 61 00 710 801, TEST OK. NO HISTORY LAST 30 DAYS. A/C RETAINS CURRENT CAT STATUS.Apr 29, 2009 · N583AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0955164Fuel Sys · malfunctionedINADVERTENT FUEL IMBALANCE GREATER THAN 1000 LBS LEFT TANK 7.35 RIGHT TANK 8.40. BALANCE WAS RESTORED. NO EVIDENCE OF FUEL LEAK. ACCOMPLISHED FIM TASK 28 41 810 820 NO DISCREPANCIES FOUND. FUEL QUANTITY TEST PASSED. GROUND TEST VERIFICATION PASSED. NO FAApr 17, 2009 · N583AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA0955152Fuse · blownRT AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP (EXTERIOR LIGHT. REPLACED BATT PACK PICO FUSE. OPS CHECK RT AFT SERVICE DOOR EMERG EXIT SLIDE LIGHT GOOD.Apr 14, 2009 · N583AS · Boeing 737890 · Emergency LightingSDR ASAA0954999Control Valve · failedAFTER STARTING ENGINES, CHECKED MC LIGHT AND GOT RIGHT PACK LIGHT. REMOVED AND REPLACED RIGHT PACK TEMP CONTROL VALVE REF MM 21 61 00, OP CHECK AND BITE CHECK GOOD REF MM 21 61 20. GROUND VERIFICATION ACCOMPLISHED PER ETOPS MANUAL. RT PACK TEMP CONTROL VALVMar 31, 2009 · N583AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0954795Warning System · malfunctionedWHEN MASTER CAUTION RECALL CHECK ACCOMPLISHED RT "PACK" LT ILLUMINATED. LT EXTINGUISHED WHEN MASTER CAUTION PUSH TO RESET BUTTON PUSHED. TROUBLESHOT PER FIM 21 62 00 810 828. RT PACK TCV FAULT LIGHT CLEARS AFTER TEMP CONTROLLER BITE. PAC OPS NORMAL RT "PACMar 15, 2009 · N583AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0954756Control Unit · overspeedFVR UNSATISFACTORY APU OVERSPEED AT FL 390 AUTO SHUTDOWN INITIATED. REMOVED AND REPLACED APU FUEL CONTROL UNIT REF MM 49 31 11 000 801 AND 49 31 11 400 801 STEPS A THROUGH AND INCLUDING H(2) OF INSTALLATION. REMOVED AND REPLACED APU ELE CONT UNIT REF MM 49 6Mar 14, 2009 · N583AS · Boeing 737890 · APU ControlsSDR ASAA0954755Sensor · malfunctionedAFTER LEVELING FL 340 APU OVERSPEED ILLUMINATED FOLLOWED BY A SHUTDOWN OF THE APU. DIVERSION TIME 83 MINUTES. PERFORMED APU BITE CHECK FOUND FAULT MSG 49 31014 (APU OVERSPEED SHUTDOWN). PERFORMED FIM 49 30 TASK 802. REMOVED AND REPLACED APU SPEED SENSOR P/Mar 13, 2009 · N583AS · Boeing 737890 · APU ControlsSDR ASAA0954637Unknown · malfunctionedJUST AFTER TAKEOFF AT 1000 AGL RECEIVED CDU SCRATCH PAD MESSAGE "VERIFY POSITION IRS FMC" FMC L 299' /0.0 FMC R 123' /0.0 GPS L 122'/0.1 IRS L068'/12 IRSR 070"/12.0 RADIO: BLANK RADIO POS 041'/0.0 DME UPDATE ON NAV STATUS PAGE NORMAL ACTIVE NAV SCR GPS 2 IRS 2Mar 4, 2009 · N583AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0954634Oil Filter · dirtyNR 1 ENG FOUND SMALL AMOUNT OF COKE PARTICLES IN AFT SUMP CHIP DETECTOR. REMOVED AND REPLACED SCAVENGE OIL FILTER PER MM 79 21 06, NO PARTICLES FOUND IN SCAVENGE FILTER. LEAK CHECK GOOD.Mar 2, 2009 · N583AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA0954438Eec · failedNO EGT AFTER START LEVER TO IDLE (ENG 1). REMOVED & REPLACED NR 1 EEC PER MM 73 21 60, OPS CHECK GOOD PER MM 71 00 00, PART VERIFICATION PER ETOPS PROGRAM VERIFIED WITH SEAMC.Feb 15, 2009 · N583AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA0954288Retainer · crackedRT WING TE PANEL 671BB SEAL RETAINER ANGLE IS CRACKED. REMOVED FABICATED NEW AND INSTALLED RETAINER ANGLE.Jan 25, 2009 · N583AS · Boeing 737890 · Wing Miscellaneous StructureSDR ASAA0954289Bracket · crackedRT WING FIXED TE SEAL BRACKET WS 289 CRACKED. R&R WITH NEW BRACKET PER SRM 51 40 02.Jan 24, 2009 · N583AS · Boeing 737890 · Wing Miscellaneous StructureSDR ASAA0954290Fairing · chafedWING TO BODY FAIRING DAMAGE 193AR CHAFFED THROUGH. REPAIRED PER SRM 51 70 05.Jan 24, 2009 · N583AS · Boeing 737890 · Aerodynamic FairingsSDR ASAA0954292Skin · dentedSKIN DAMAGE DENT. REPAIRED PER ASA EA 53EA00526.Jan 22, 2009 · N583AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA0954291Bracket · crackedLT WING FIXED TE SEAL BRACKET AT WS 289 IS CRACKED FWD WEB AFT BRACKET. R&R LT WING FIXED TE SEAL BRACKET AT WS 289 PER SRM 51 40 02.Jan 20, 2009 · N583AS · Boeing 737890 · Wing Miscellaneous StructureSDR ASAA0954196Connector · dirtyENROUTE APU OVERSPEED LIGHT ILLUMINATED ALONG WITH MASTER CAUTION. APU CONTROL SWITCH SELECTED TO OFF. OVERSPEED LIGHT EXTINGUISHED 5 MIN AND 40 SECONDS LATER. EGT WENT FROM 200* TO 0* WHEN LIGHT WENT OUT GROUNDED YES. PERFORMED APU BITE PER AMM 49 60 00 FOJan 10, 2009 · N583AS · Boeing 737890 · APU System WiringSDR ASAA0954195Sensor · malfunctionedAPU OVERSPEED LIGHT ILLUMINATED WITH MASTER CAUTION. HAPPENED AT FL350 ABOUT 2 1/2 HOURS INTO FLIGHT. SHUT DOWN APU OVERSPEED LIGHT EXT PER QRH GROUNDED YES. PERFORMED APU BITE TEST MX MSG NR 49 31014 APU OVERSPEED PRESENT. REF FIM 49 60 00 810 801. VERIFJan 10, 2009 · N583AS · Boeing 737890 · APU ControlsSDR ASAA0954157Filter Element · poppedAPU LUBE FILTER ELEMENT DELTA-P EXTENDED, GROUNDED, YES. APU LUBE FILTER REMOVED AND REPLACED IAW AMM 49 91 13 MAGNETIC CHIP DETECTOR, CHK GOOD. LEAK CHECK ON MCD AND FILTER BOWL GOOD.Jan 5, 2009 · N583AS · Boeing 737890 · APU Oil SystemSDR ASAA0854115Packing · looseWHILE SERVICING NR 2 ENG OIL SERVICING CAP PACKING VERY LOOSE GROUNDED YES. R&R PACKING OIL CAP P NR M83248 1 226Dec 27, 2008 · N583AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0854083Pcu · malfunctioned`ELEC` LIGHT ILLUMINATED ON OVERHEAD PANEL GROUNDED YES. TRIED TO CLEAR THE FAULT AND NO HELP. CYCLED NORMAL AND STANDBY SPCU C/B AND CLEARED FAULT REF MM FIM 24 34 00 810 802 SPCU. OPS CK GOOD.Dec 20, 2008 · N583AS · Boeing 737890 · DC Generating SystemSDR ASAA0854084Generator · unknownAPU GENERATORS DROPPED OFFLINE WITHOUT WARNING GROUNDED YES. NO CIRCUIT BREAKERS OPEN NO FAULTS IN COMPUTER STARTED APU SWITCHED TO APU POWER LOADED UP SYSTEM NO DEFECTS NOTED. GOOD FOR SERVICE. SEAMC BILL NOTIFIED.Dec 20, 2008 · N583AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0854037Valve · faultedON MASTER CAUTION RECALL GOT MASTER CAUTION AIR COND AND RT PACK LIGHT. IT EXTINGUISHES ON RESET GROUNDED YES. PERFORMED PACK/ZONE TEMP CONTROL BITE TEST PER FIM TASK 21-62 TASK 801. FOUND FAULT WITH TRIM CONTROL VALVE RT. R&R RT TRIM VALVE PER FIM TASK 21-Dec 13, 2008 · N583AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0853932Sensor · failedRIGHT SIDE WINDOW OVERHEAT CONDITION 10 MIN AFTER TAKEOFF TURNED HEAT OFF FOR 5 MINUTES PER QRH UPON TURNING HEAT ON THE OVERHEAT LAMP ILLUMINATED IMMEDIATELY. TURNED HEAT OFF FOR REMAINDER OF FLIGHT. RT SIDE WHCU FAULTS SENSOR. W/RT SIDE WINDOW HEATED FOUNDec 1, 2008 · N583AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853923Controller · faultedWHILE EN ROUTE RIGHT SIDE WINDOW OVERHEAT LIGHT CAME ON FOLLOWED QRH PROCEDURE AND OVERHEAT LIGHT CAME BACK ON BITE CHECKED WHCU CURRENT BIT PASSED. RT SIDE WHCU LOGGED SENSOR FAULT FOR PAST 7 LEGS. MEASURED RESISTANCE OF SENSOR REF MM 30 41 21 760 801 PRIMANov 30, 2008 · N583AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853922Controller · intermittentWHILE EN ROUTE RIGHT SIDE WINDOW HEAT OVERHEAT LIGHT CAME ON CYCLED IT OFF PER THE CHECKLIST (AND BACK ON) BUT OVERHEAT WOULD NOT EXTINGUISH. SWITCH REMAINS OFF PER THE CHECKLIST. OPS CHECK BITE CHECK INTERMITTENT SENSOR FAULT OPS CK IAW FIM 30 41 00 810 801Nov 30, 2008 · N583AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853622Controller · faultyDURING LANDING CHECK, "RIGHT PACK" LIGHT ILLUMINATED ON RECALL ACCOMPLISHED FIM TASK 21 53 810 & ZONE TEMP CONTROLLER BITE PER 21 61 00. RT CONTROLLER SHOWED PACK TEMP SENSOR FAULT. RESET & RAN PACK FOR 1 2 HOUR ON GROUND WITH NO FURTHER FAULTS.Oct 18, 2008 · N583AS · Boeing 737890 · Cabin Temperature ControllerSDR ASAA0853587Probe · malfunctionedGE DIAGNOSTICS REPORTS NR 1 ENGINE CRUISE DELTA EGT SHOWS GREATER THAN NORMAL SCATTER AND MOVEMENT. EGT INDICTION IS SUSPECT: PRI: 1 PERFORMED EGT PROBES CLEANING PER MM 77 21 00 201 PINS AND SOCKETS TENSION CHECKED NORMAL. VALUES S1 S4 PRE 205 176 176 214 POOct 7, 2008 · N583AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA0853537Starter Gen · failedBLUE MAINT LIGHT ON APU ILLUMINATED. PERFORMED FIM TASK 49 40 00 810 806 CONFIRMED FAULT REMOVED AND REPLACED STARTER GENERATOR REF MM 49 41 21 OPS & LEAK CHECK GOOD. CONFIRMED FAULT CORRECTED W CDU AND FIM TASK 49 40 00 810 806.Sep 28, 2008 · N583AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA0853532Oil Filter · faultyWHILE ACCOMPLISHING TC 78349013 FOUND APU OIL FILTER DELTA P INDICATOR EXTENDED. REMOVED AND REPLACED APU OIL FILTER, NO CONTAMINATION NOTED. INSPECTED MAGNETIC DRAIN PLUG, NO CONTAMINATION NOTED. RAN APU FOR 15 MINS. NO LEAKS NOTED. GROUND VERIFICATION SSep 25, 2008 · N583AS · Boeing 737890 · APU Oil SystemSDR ASAA0853481Position Sensor · out of adjustAUTOPILOT HAD SPOIL 4 SIQ FAILURE INDICATION. ADJUSTED SPOILER POSITION SENSOR.Sep 9, 2008 · N583AS · Boeing 737890 · Autopilot SystemSDR ASAA0853476Processor · faultedDURING CRUISE DEVELOPED 1000 LBS FUEL IMBALANCE WITH ASSOCIATE "IMBAL" ANNUNCIATOR FOR NO OBVIOUS REASON. ACFT WAS NOT BALANCED, FUEL CROSS FEED CLOSED. CENTER TANK EMPTY WITH CENTER BOOST PUMPS OFF. ALL MAIN TANK PUMPS ON. LT QTY REACHED 7100 LBS RT WAS 8Sep 7, 2008 · N583AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA0853471Oil Filter · activatedNR 1 ENG IDG DPI FOUND EXTENDED ARCTIC VERIFIED 1ST OCCURRENCE LAST 365 DAYS. ACCOMP FIM 24 11 TASK 803. REMOVED INSP & REPLACED CHG & SCAVENGE FILTERS REF MM 24-11-41. RESET DPI LK & OPS NORMAL REF MM 24-11-41. GROUND VERIFICATION SUCCESSFUL.Sep 2, 2008 · N583AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853447Fmc · malfunctionedFMC DISAGREE LIGHT ILLUMINATED. ACCOMPLISHED FMC DISAGREE QRH ON THE GROUND. PERFORMED "FMC DISAGREE MESSAGE ON CDU" FIM TASK 34 61 00 810 835. GROUND VERIFCATION SUCCESSFUL.Aug 31, 2008 · N583AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853425Fmc · malfunctionedDURING CLIMB SPEED BUG DROPPED TO CLEAN SPEED WITH V NAV ENGAGED FMC READS GOOD FOR CLIMB SPEED. AT CRUISE V NAV AND BUG APPEAR TO BE WORKING OKAY. PERFORMED FMC BITE TEST PER MM 34-61-00. PERFORMED DFGS BITE TEST PER MM 22-11-00. NO FAULTS NOTED. NO HISTAug 28, 2008 · N583AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853404Controller · inoperativeLT FWD WINDOW OVERHEAT LIGHT ILLUMINATED FOUND LEFT FRONT HEAT POWER C/B ON P6 11 OUT. RESET C/B REF PROCEDURE MM 20 60 01. BITE CHECK ON WHCU OPS NORMAL REF MM FIM 30 41 00 TASK 801. GROUND VERIFICATION CHECKS GOOD.Aug 24, 2008 · N583AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853398Fmc · faultedAT LIM ILLUMINATED IN FLIGHT ABOVE N1'S. AFTER LANDING DASHES ABOVE N1'S CURRENT STATUS & BITE CHECKS GOOD REF FIM 22 31 710 801 FMS CHECKS GOOD REF FIM 34 61 00 810 807 & FIM 73 00 00 810 801 F00, NO PREVIOUS HISTORY. GROUND VERIFICATION SUCCESSFUL.Aug 21, 2008 · N583AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853332Idg · failedNR 2 GEN OFF BUSS LIGHT ILLUMINATED FOLLOWED SHORTLY BY NR 2 DRIVE LIGHT ILLUMINATION. DISCONNECTED DRIVE AND PUT APU ON BUSS. REMOVED AND REPLACED THE NR 2 ENG IDG REF MM 24 11 11 000 801 AND MM 24 11 11 400 801 LEAK CHECK AND OPS CHECKS GOOD REF MM 24 11 0Aug 15, 2008 · N583AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853250Transceiver · faultedDURING LANDING ROLL "PWS FAIL" ILLUMINATED ON BOTH CAPT AND FO NAV DISPLAY. WEATHER RADAR OPERATED NORMAL INFLIGHT. VERIFED DISCREPANCY PWS FAIL ANNUNCIATED ON BOTH CAPT'S & FO'S DISPLAY. CYCLED WRX CB GROUND VERIFICATION TEST PASSED REF MM 34-43-00.Jul 30, 2008 · N583AS · Boeing 737890 · Weather Radar SystemSDR ASAA0853215Fmc · faultedUPON TAXI OUT FMC DISAGREE CAME ON BOTH FMC'S STAYED ON FOR 6-8 MINUTES AND BOTH WENT OFF AS WE TAXIED IN. FMC DISAGREE EXTINGUISHED BEFORE AIRCRAFT RETURNED TO GATE. PERFORMED FIM TASK 34-61-00-810-835 FOR PRECAUTIONARY PURPOSES. DETERMINED TO BE INTERMITTJul 22, 2008 · N583AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853214Controller · faultedAUTO FAIL LIGHT ALONG WITH ALTN LIGHT ILLUMINATED CLEARED NUISANCE MSG FROM NR 2 PRESS CONT SYSTEM OPS CHECK NORMAL IAW AMM 21 31 00 700 802. (GROUND TEST)Jul 22, 2008 · N583AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA0853171Start Valve · malfunctionedWHILE TRYING TO START ENG NR 2 MOVED START SWITCH TO GND DID NOT GET A "START VALVE OPEN" LIGHT OR N2 INDICATION COMPLETED FIM TASK 80 70 00 810 804 F00. DRY MOTORED ENGINE SUCCESSFUL, TWO ATTEMPTS NO FAULTS IN BITE CHECK RECENT OR HISTORICAL. NO HISTORY 30 Jul 6, 2008 · N583AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA0853106Oil System · lowNR 1 OIL AT 13 ADDED 4QTS OIL TO NR 1 AND 4QTS OIL TO NR 2.Jun 27, 2008 · N583AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853086Fmc · faultedFMC DISAGREE FLAG DISPLAYED ON TAXI OUT CONFIRMED FAULT FMC DISAGREES MONITORING PARAMETERS. RESET BOTH FMC'S AND TEST NML PER FIM 34 61 00 810 807. INSPECTION ACCOMPLISHED FOR SIMULTANEOUS MAINTENANCE.Jun 24, 2008 · N583AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853034Oil System · lowNR 1 ENG QTY AT 13 NR 2 ENG QTY AT 15 SERVICED NR 1 ENG OIL TO FULL 5.5 QTS SERVICED NR 2 ENG TO FULL.Jun 4, 2008 · N583AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853022Charger · malfunctionedAUX BATTERY SHOWS A 2 AMP CHARGE AND HAS NOT DECREASED TO ZERO. DC VOLTS SHOWS 27 CKD AUX BATT AND AUX BATT CHGR REF 24 31 31, OPS CKS OK WITHIN.Jun 3, 2008 · N583AS · Boeing 737890 · Battery/Charger SystemSDR ASAA0852830Filter · cloggedWITH FWD & CONT CABIN PACK CONTROLLERS IN 12:00 AFT CABIN CONTROLLER REQUIRED 4:00 POSITION TO MAINTAIN AFT CABIN TEMP AT 26 DEGS C. NO FAULTS LOGGED IN NR 1, 2 CONTROLLERS. FOUND AFT CABIN TEMP SENSOR FILTER CLOGGED. CLEANED FILTER. GROUND VERIFICATION PAApr 22, 2008 · N583AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0852822Modulating Valve · malfunctionedCABIN ZONE TEMPERATURE ANNUNCIATION OCCURRED. BITE TEST INDICATED RIGHTHAND PACK TRIM MODULATING VALVE AT FAULT. RESET, OP CHECKED OK.Apr 17, 2008 · N583AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA0852805Switch · faultyAUTOPILOT "A" WILL NOT ENGAGE. COULD NOT GET AUTOPILOT "A" TO ENGAGE. PERFORMED DFCS BITE SHOWED MULTIPLE DISCONNECT FAILURES. FOUND F/O'S DISCONNECT SWITCH BAD. THE "A" SIDE OF SWITCH STICKS OPEN REQUIRES NUMEROUS PRESSES OF SWITCH TO CLOSE AND ENGAGE AUTApr 4, 2008 · N583AS · Boeing 737890 · Autopilot System
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