N589AS

Service difficulty reports · 447

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 = 'N589AS' 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 ASAA12511254Unknown · malfunctionedAFTER T/O NR 1 FUEL QTY INDICATOR BLANKED. SOON AFTER TOTAL FOB INDICATOR BLANKED. BOTH SOON CAME BACK BUT NR 1 TANK WAS 400 - 500 LBS LESS THAN IT HAD INDICATED PRIOR TO T/O. AS WE LEVELED AT ATTITUDE. NR 1 TANK INCREASED BY ABOUT 500 LBS AND INDICATES WHMar 15, 2012 · N589AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA12511234Unknown · malfunctionedRECEIVED SINGLE FMC OPERATION MESSAGE. RIGHT FMC NO WORKING. FOLLOWED CHECKLIST. DUAL OPERATION RESTORED. WORKED NORMALLY FOR REMAINDER OF FLIGHT. PERFORMED OPS CHECK OF LEFT FMC PER AMM 34 61 00 710 801 OPS CHECK OK. PERFORMED OPS CHECK OF RIGHT FMC PERMar 12, 2012 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511121Control Valve · malfunctionedA/C PACK LIGHT ON RECALL. REPLACED LT PACK CONTROL VALVE REF AMM 21-51-10-000-801 & 21-51-10-400-801. INSTALLATION TESTED GOOD. BITE TESTED GOOD.Feb 16, 2012 · N589AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012021511109Warning Light · false activationLEFT PACK LIGHT ILLUMINATES ON MASTER CAUTION PRESS LIGHT GOES OUT WHEN MASTER CAUTION RESET. BITE OF TEMP CONTROLLER NR 1 SHOWS TRIM CONTROL VALVE PACK FAULT. RESET & BITE CHECKED GOOD. REF AMM 21-61-00.Feb 15, 2012 · N589AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1251097Sensor · defectiveAPU CT5ATP EGT HAS HISTORY OF INDICATING LOW AND ERRONEOUS. INDICATION ERRORS ARE SUSPECT. REMOVED AND REPLACED INLET TEMPERATURE SENSOR PER MM 49 61 31.Feb 13, 2012 · N589AS · Boeing 737890 · APU Indicating SystemSDR ASAA12511037Warning System · false activationLEFT PACK LT ILLUMINATED ON RECALL DURING LANDING CHECK. LIGHT EXTINGUISHED AFTER PUSHING MASTER CAUTION. PERFORMED PACK ZONE TEMP BITE CHECK FOR NR 2 ZONE CONTROLLER FAULTS PACK TCV. RESET FAULT. PERFORMED BITE CHECK NO FAULTES NOTED TEST PASSED. PER AMMFeb 4, 2012 · N589AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511040Detector · defectiveDURING PREFLIGHT FIRE TEST HANDLE NR 1 DOES NOT TEST PROPERLY AND FAULT LIGHT ILLUMINATES. PERFORMED FIM TASK 26 10 00 810 805 FOUND UPPER FAN DETECTOR RESISTANCE NOT WITHIN LIMITS. REPLACED UPPER FAN DETECTOR ASSY M01757 IAW AMM 26 11 01, OPS CK GOOD PER AMFeb 2, 2012 · N589AS · Boeing 737890 · Fire DetectionSDR ASAA12510976Warning System · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL LIGHT EXTINGUISHED ON MASTER CAUTION RESET. PERFORMED PACK ZONE TEMP CONTROLER BITE FOR NR 1 ZONE CONTROLLER FAULTS PACK TCV. RESET FAULT LIGHT RAN PACK NO FURTHER DEFECTS. PERFORMED PACK/ZONE TEMPERATURE CONTROLLER INSJan 20, 2012 · N589AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA11510662Filter Element · defectiveDURING THE ETOPS PDC FOUND NR 1 ENG IDG DELTA P INDICATOR WAS EXTENDED. ACCOMPLISHED FIM TASK 24 11 00 810 803. PERFORMED CHECK OF IDG SCAVENGE FILTER. VERIFIED BOTH ENG IDG DELTA P INDICATORS NOT EXTENDED.Nov 14, 2011 · N589AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA11510625Sensor · dirtyLONG TIME FAULT 77 10842 "TOP RIGHT EGT SIGNAL OUT OF RANGE" FOUND ON ALL LEGS. PERFORMED EGT CLEANING PER AMM 72 21 00 201. INITIAL S1 S4 TEMPS 57 / 21 / 21 / 50 AFTER CLEANING TEMPS READ 42 / 17 / 18 / 38.Nov 4, 2011 · N589AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA11510609Warning System · false activationPRESSURIZATION CONTROL PANEL "AUTO FAIL" LIGHT ILLUMINATED. ACCOMPLISHED PRESSURIZATION SYSTEM GROUND TEST FOR BOTH CONTROLLERS PER AMM TASK 21 31 00 700 802. PRESSURIZATION SYSTEM BITE TEST NORMAL WITHOUT FAULTS.Nov 1, 2011 · N589AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA11510605Regulator · defectiveON CLIMBOUT DUCT SPLIT OCCURRED AT 4000. N1 89.4 PERCENT LEFT DUCT PRESSURE 67 PSI RIGHT DUCT AT 42 PSI AT FL 290 N1 94.1PERCENT LT DUCT AT 48 PSI RIGHT DUCT AT 42 PSI. AT FL 380 N1 87.9 PERCENT LT AND RT DUCT AT 40 PSI. NR 1 ENG DUCT PRESSURE HIGH: ABOVE 7Oct 30, 2011 · N589AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA11510567Unknown · malfunctionedAPU PUT ON LINE TO ELECTRICALLY POWER AIRCRAFT INITIALLY HOLDS THE LOAD BUT SLOWLY SEE FREQUENCY DETRIORATE FROM 395 CPS TO AS LOW AS 375 WHEN IT TRIPPED ELECTRICALLY OFF THE LINE APU DOES NOT SUPPLY BLEED AIR FOR PACK USE. CDU SHOWED FAULT 49 41011 FOR ONE IOct 23, 2011 · N589AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA11510556Valve · failedAFTER TAKEOFF NOTICED BLEED AIR SPLIT AT CLIMB POWER. ACCOMPLISHED BLEED AIR SYSTEM HEALTH CHECK REF MM 36-11-00. HIGH STAGE VALVE FOUND TO BE INTERMITTENT DURING PRESSURE CHECK. REPLACED NR1 ENGINE HIGH STAGE VALVE REF MM 36-11-06, OPS NORMAL DURING TEST. Oct 19, 2011 · N589AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA11510549Unknown · malfunctionedNR 2 EGT FLUXUATED +50 0 IN CURISE WITH A/THDLS ON OR OFF AND EEC ON ALL OTHER GAUGES INDICATED NORMALLY NO THROTTLE MOVEMENT WITH A/THRTLS ON NO STAGGERED THOTTLES (THRUST LEVERS). PERFORMED ENG BITE TEST PER MM 73 00 00 FOR NR 2 ENG SHOW NO FAULTS RECORDED.Oct 19, 2011 · N589AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA11510542Probe · dirtyWHILE ACCOMPLISHING T/C 78273000 FOUND LONG TERM FAULT 77 10842 TOP RIGHT EGT SIGNAL OUT OF RANGE LEGS 2 5 7 AND 9 ON NR 2 ENGINE. ACCOMPLISHED FIM TASK 77 21 00 810 801 FOO CLEANED AND CHECKED TOP RIGHT EGT PROBE ON NR 2 ENG OPS NORMAL ON EEC BITE TEST (NO FOct 17, 2011 · N589AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA11510454Window · crackedR1 OUTER PANE SHATTERED AT FL 360 OVER CINNY. ACCOMPLISHED QRH PROCEDURES. DIVERSION TIME: 1 HOUR 11 MIN. REPLACED R1 WINDOW PER AMM 56 11 11 801 AND 56 11 11 400 801. REPLACED RIGHT FWD WINDOW HEAT CONTROL UNIT PER AMM 30 41 11 000 801 AND 30 41 11 400 80Sep 30, 2011 · N589AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA11510402Filter Element · faultyAPU FAULT LIGHT ILLUMINATED ON PRE FLIGHT. PERFORMED APU BITE CHECK FOUND FAULT CODE 49 94299 STARTER GENERATOR FILTER ELEMENT. REPLACED STARTER GENERATOR FILTER ELEMENT OPS AND LEAK GOOD PER AMM 49 91 12 000 803. RAN APU CURRENT STATUS NO FAILURE FOUND.Sep 19, 2011 · N589AS · Boeing 737890 · APU Oil SystemSDR ASAA1150374Unknown · malfunctionedAFTER START WHILE ON SHIP'S POWER SAW "FMC DISAGREE" LIGHTS ILLUMINATE. ACCOMPLISHED QRH PROCEDURE AND LIGHTS EXTINGUISHED. OPS CHECK NORMAL.Sep 17, 2011 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159679Circuit Breaker · trippedPWS FAIL LIGHT ILLUMINATED DU. WX RADAR CB FOUND OUT. CONFIRMED CB "WEATHER RADAR RT" OUT P6 1 D13. INSPECTED AVAIL WIRING RESET CB PERFORMED CB RESET TASK 20 60 01 860 801 WX RDR SYST OPS TEST 34 43 00 710 802 001 WX RDR SYST BITE TASK 34 43 00 810 801 ALLMay 21, 2011 · N589AS · Boeing 737890 · Weather Radar SystemSDR ASAA1159570Cdu · defectiveON F/O'S CDU 6L BUTTON STICKS WORKS INTERMITTENTLY. REPLACED F/O'S FMCS CDU IAW AMM 34 61 01 PAGE BLOCK 401. FMCS CDU BITE TEST NORMAL.May 1, 2011 · N589AS · Boeing 737890 · Central DisplaySDR ASAA1159533Unknown · malfunctionedLEFT FMC FAIL 55 MINUTES AFTER TAKEOFF. CAPTAIN'S MAP DISPLAY SHOWED VTK AND MAP FAULTS. FMC LOST FMC MENU ITEM BOTH SIDES. USED QRH TO RESTORE SINGLE FMC OPERATION BY SELECTING FMC SELECT SW TO BOTH ON RIGHT. DUAL FMC OPS WAS NOT RESTORED. CONTINUED FLIGHApr 22, 2011 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159169Idg · failedNR 1 GEN "DRIVE" LIGHT FAILS TO ILLUMINATE ON GROUND WITH ENGINE SHUTDOWN. LIGHT TEST OK. REMOVED IDG NR 1 CONN DP1206 AND RANG OUT IDG CHARGE PRESS. SW VIA PINS 5&6. SHOWS HIGH RESISTANCE OF 210 OHMS. VERIFIED FAULT NR 1 GEN DRIVE LIGHT FAILS TO ILLUMINAMar 2, 2011 · N589AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1159162Unknown · malfunctionedAFTER BRAKE RELEASE MASTER CAUTION /ELEC/ NR 2 IDG DRIVE LIGHT ILLUMINATED / NR 1 IDG LIGHT IS NOT ILLUMINATED RAN NR 1 ENG VOLTS & FREQS GOOD HOLDS A LOAD ALSO. CSD OIL LEVEL OK. NR 1 DRIVE LIGHT ILLUMINATED NORMALLY ON SHUTDOWN. NO HISTORY 90 DAYS. NR 1 Mar 1, 2011 · N589AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1159028Shim · damagedREF T/C 78472002 NR 1 ENG FAN BLADE LUBRICATION. FOUND ALL 24 EACH FAN BLADE SHIMS MISSING MOLY COATING. INSTALLED 24 EACH P/N 340 252 307 0 ON BLADES REF T/C 78472002.Feb 12, 2011 · N589AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA1159016Computer · failedFMC DISAGREE LIGHT ILLUMINATED. CONTINUOUSLY CYCLE OFF THEN ON. CONFIRMED PROBLEM. RT FMC BITE SENSOR PAGE SHOWS "MISMATCH" FOR FMC. REMOVED & REPLACED RT FMC COMPUTER REF MM 34 61 02 000 801 & 34 61 02 400 801. OPS NML PER MM 34 61 00 710 801. GROUND VEFeb 9, 2011 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159015Unknown · malfunctionedFMC DISAGREE ANNUNCIATED ON ND. RE-LOADED RIGHT FMC MEDB SOFTWARE BCG014V9 IPC REF 34 61 02 04 VERIFIED WITH MC DARREN. FMC OPS NML PER FIM 34 61 TASK 801. EXISTING SOFTWARE WAS CONFIRMED CORRECT BEFORE RE-LOAD. ALL OTHER FMC SOFTWARE ALSO CONFIRMED. USED Feb 9, 2011 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158994Computer · failedRT FMC FAILURE. VERIFIED THAT RT FMC DOES NOT OPERATE. REPLACED RT FMC COMPUTER REF MM 34 61 02. FMCS OPERATIONAL TEST NML REF MM 34 61 00.Feb 8, 2011 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158931Unknown · malfunctionedCAPT F/D INOP. AFTER ENG START ON RECALL SPEED TRIM FAIL LIGHT AND MACH TRIM FAIL LIGHT ILLUMINATED. CYCLED POWER TO "A" FCC COMPUTER. PERFORMED FCC LRU INTERFACE TEST REF MM 22 11 33/401 & LAND VERIFY TEST REF MM 22 11 00/201 BITE 49, ALL TESTS PASSED. HGJan 30, 2011 · N589AS · Boeing 737890 · Autopilot SystemSDR ASAA1158930Unknown · malfunctionedFMC DISAGREE DISPLAYED. RESET VIA QRH CHECKS OK.Jan 30, 2011 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158890Unknown · malfunctionedFMC DISAGREE IN SCRATCH PAD. QRH COMPLETED FMC DISAGREE MESSAGE NO LONGER DISPLAYED.Jan 27, 2011 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158876Unknown · malfunctionedAT CRUISE APU OPERATING. NO VOLTS OR FREQUENCY ARE DISPLAYED. PERFORMED FIM TASK 49 60 00 801. NO CURRENT FAULTS PERFORMED APU OPERATIONAL TEST 49 11 00 710 801, SYSTEM OPS NORMAL.Jan 24, 2011 · N589AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1058669Strip · brokenMAIN CABIN LT SIDE ESCAPE PATH LIGHTING HAS A PIECE BROKEN BY THE AFT LT LAVATORY. REMOVED AND REPLACED MAIN CABIN LT ESCAPE PATH LIGHTING STRIP IAW B737 MM 33 51 15 960 801.Dec 21, 2010 · N589AS · Boeing 737890 · Emergency LightingSDR ASAA1058566Hf Comm · failedHF 1 SHOWS FAIL ON BOTH ACTIVE & STANDBY. PERFORMED BITE TEST NR 1 & 2 HF SYS. OPS NORMAL REF FIM 23 11, TASK 801. HF1 OPS NORMAL WITH REF MM 23 11 00. GROUND VERIFICATION SUCCESSFUL.Nov 30, 2010 · N589AS · Boeing 737890 · HF Communications SystemSDR ASAA1058522Relay · failedDURING ACCOMPLISHMENT OF TASK CARD 78128007 FAILED STEP 1D (8). REMOVED AND REPLACED RELAY R55 BOOST PUMP CTR TANK RIGHT GFI RELAY REF WDM 28 23 11. COMPLIED WITH ACCOMPLISHMENT OF T/C 7812007. ALL STEPS PASSED. SEAMC NOTIFIED.Nov 19, 2010 · N589AS · Boeing 737890 · Fuel Boost PumpSDR ASAA1058403Bleed Valve · faultyAPU CDU FAULT VERBAL FROM FLT CREW. CDU FAULT FIM 49 52240 SHOWING. WITH APU RUNNING SET APU BLEED SWITCH TO ON NO DUCT PRESSURE REGISTERD. CHECKED AT BLEED VALVE FOUND IN CLOSED POSITION. REPLACED BLEED VALVE REF MM 49 52 11 400 801. OPS CHECKED BLEED AIOct 18, 2010 · N589AS · Boeing 737890 · APU Bleed Air SystemSDR ASAA1058270Spinner · unserviceableREF T/C 78472000 NR 1 ENGINE INLET SPINNER CONE MISSING GREATER THAN 20 PERCENT OF BLACK SULFURIC ANODIZING COATING. R & R NR 1 ENG FRONT SPINNER CONE IAW MM 72-21-01.Sep 12, 2010 · N589AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA1058211Unknown · malfunctionedHF2 SHOWS FAIL IN ACTIVE AND STANDBY WINDOWS. VERIFIED DISCREPANCY. REBOOTED HF2 AND GROUND VERIFICATION TESTS OK REF FIM 23 11 00.Aug 21, 2010 · N589AS · Boeing 737890 · HF Communications SystemSDR ASAA1058135Eec · failedA/T LIM ANNUNCIATED ON ENGINE DISPLAY. A/T INFLIGHT FAULTS LOGGED MSG 22 31413 AND 22 31513, NR 1 AND NR 2 DEU LOGGED FAULT CODE 31 68240 NR 2 ENGINE 73 21282 LOGGED IN EEC ON GROUND AND FLIGHT LEG NR 1. FOLLOWED FIM 73 27 00 810 805 F00. REPLACED NR 2 ENG Aug 6, 2010 · N589AS · Boeing 737890 · Fuel Control/Turbine EnginesSDR ASAA1057780Unknown · malfunctionedFMC DISAGREE LIGHT ILLUMINATED ON GROUND FAULT CODE 34607500. FOLLOWED QRH PROCEDURE AND LIGHT WENT OUT. PERFORMED FIM TASK 34 61 00 810 835 NO FAULTS NOTED. ALSO PERFORMED FIM TASK 34 61 00 810 801, NO FAULT NOTED.May 4, 2010 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1057719Coupler · damagedUNABLE TO TRANSMIT ON HF NR 1 AND HF NR 2 FROM BOTH THE CAPTAIN'S AND FIRST OFFICER'S POSITIONS, RECEIVES OK. REPLACED REMOTE ELECTRONICS UNIT PER MM 23 51 00 000 801. REPLACED NR 1 HF COUPLER PER AMM REF 23 11 61 000 801/23 11 61 400 801. ALL CONNECTIONS AApr 17, 2010 · N589AS · Boeing 737890 · Communications System WiringSDR ASAA1057702Wire · looseWX RADAR SPOKES INTERMITTENTLY. VERIFIED TILT CODE, +3 DURING TEST. REF FIM 34 43 TASK 806 & WDM 34 21 24 FOUND PIN W0523 2776B 24 LOOSE ON ZB5 AT TB521. WIRE SECURED WXR RT REINSTALLED REF MM 34 43 41. PERFORMED WXR OPERATIONAL TEST REF MM 34 43 00, TEST Apr 14, 2010 · N589AS · Boeing 737890 · Navigation System WiringSDR ASAA1057607Unknown · malfunctionedDURING TAXI IN, APU NOT RUNNING RIGHT ENGINE SHUT DOWN ELECTRIC POWER DID NOT TRANSFER FROM POWERED SIDE TO NON POWERED SIDE REPEAT WRITE UP. UNABLE TO DUPLICATE DEFECT PERFORMED GCU BITE IAW FIM 24 21 00, NO FAULTS. PRECAUTIONARY REPLACED BUS TIE BREAKER NRMar 25, 2010 · N589AS · Boeing 737890 · AC Generation SystemSDR ASAA1057606Unknown · malfunctionedDURING TAXI IN, SHUT DOWN NR 2 ENGINE BUS TRANSFER RELAY DID NOT TRANSFER. TRANSFER BUS OFF SOURCE OFF LIGHTS ILLUMINATED. ACCOMPLISHED GCU BITE REF FIM 24 21 00 810 801, NO FAULTS LOGGED. RAN ENGINES 1 & 2 BUS TRANSFER, OPS NORMAL.Mar 25, 2010 · N589AS · Boeing 737890 · AC Generation SystemSDR ASAA1057558Anti-Ice Valve · malfunctionedNR 1 ENG ANTI ICE COWL VLV SHOWS STUCK IN CLOSED POSITION. VERBAL FROM FLT CREW: WHEN NR 1 ENG TAI SWITCH PLACED TO ON LIGHT CAME ON BRIGHT AND REMAINED IT NEVER TRANSITIONED TO DIM. ALSO HAD AN AMBER TAI LIGHT ON THE CDS DISPLAY ABOVE THE N1 SPEED DISPLAY.Mar 18, 2010 · N589AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA1057481Unknown · malfunctionedCAN'T LOAD ROUTE INTO FMC. DOESN’T LOAD ANY ROUTE OR PERFORMANCE. CAN'T GET EXECUTE LIGHT TO ILLUMINATE. C/W FIM TASK 34 61 00 810 836. NO FAULTS NOTED.Mar 1, 2010 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0956037Floor Panel · damagedACB NR 2 FLOOR PANEL HAS A DEEP GOUGE/DENT AT AFT END LBL 10. REPAIRED IAW EA.Jun 25, 2009 · N589AS · Boeing 737890 · Fuselage Floor Panel
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