N558AS

Service difficulty reports · 535

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 = 'N558AS' 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 ASAA0853431Control Unit · malfunctionedTHE LEFT MCDU BLANKED OUT TWICE WITHIN 10 MINUTES THE FAIL LIGHT ILLUMINATED ON THE LEFT VERTICAL SIDE OF THE NUMBER KEY PAD. THE CENTER SCRENE MESSAGE INDICATED BIT TEST BIT PASS NORMAL OPERATION WAS AUTOMATICALLY RESTORED BOTH TIMES WITHIN 10 SECONDS. UNABAug 29, 2008 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853396Fmc · faultedAFTER ENGINE START FMC DISAGREE ILLUMINATED. PERFORMED QRH PROCEDURE RESET OK, PER PROCEDURE.Aug 20, 2008 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0853344Generator · faultedAPU MAINT LIGHT COMES ON WHEN SWITCHING APU GEN SWITCH 1 TO ON. VERIFIED FAULT APU SHOWED FAILED GEN DIODE MESS 49 41244. REMOVED AND REPLACED APU STARTER GEN PER MM 49 41 21 000 801. SYSTEM CHECK GOOD PER MM 49 41 21 000 801.Aug 17, 2008 · N558AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853331Wire Harness · damagedEN ROUTE R SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. SWITCH OFF PER QRH, THEN BACK ON, NORMAL OPS FOR DURATION OF FLT. FOUND PIN 1 ON COIL CORD TO BE INTERMITTENT OPEN. REMOVED AND REPLACED COIL CORD M2675. OPS TEST GOOD REF MM 30 41 00 WDM 30 41 11.Aug 14, 2008 · N558AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA0853329Oil Filter · poppedWHILE ACCOMPLISHING TASKCARD 78349013, FOUND APU OIL FILTER DELTA P POPPED. ACCOMPLISHED OIL FILTER INDICATOR SERVICING PER MM 49 91 13.Aug 11, 2008 · N558AS · Boeing 737890 · APU Oil SystemSDR ASAA0853261Warning System · malfunctionedWX FAIL MESSAGE ILLUMINATED INTERMITTENTLY. CONFIRMED WX TRANSCEIVER SECURED IN RACK CONFIRMED WX CONTROL PANEL CONNECTORS SECURED NO OTHER FAULTS NOTED. NO HISTORY PAST 30 DAYS. PERF WX OPERATION TEST IAW 34-43-00-710-802-001. NO FAULTS NOTED AT THIS TIMEAug 2, 2008 · N558AS · Boeing 737890 · Weather Radar SystemSDR ASAA0853204Controller · faulted"AUTO FAIL" LIGHT ILLUMINATED. PERFORMED FIM TASK 21-31-00-810-801. FAULT NO LONGER EXISTS. GROUND VERIFICATION TEST SUCCESSFUL. PERFORMED TEST ON NR1 & NR 2 CONTROLLERS.Jul 19, 2008 · N558AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA0853193Filter · trippedON SCWA FOUND NR1 ENG IDG DPI POPPED ACCOMPLISHED FIM TASK 24-11-00-810-803 AND EA 2410-01025. RAN ENG AND RED BUTTON IS NOT EXTENDED. FAULT CORRECTED REF STEP F1(B).Jul 16, 2008 · N558AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0853174Oil System · lowENGINE OIL NR 1 = 12 QTS, NR 2 = 13 QTS AT TOP OF DESCENT SERVICED BOTH ENGINE OIL LEVELS TO FULL PER MM 12 13 11. NR 1 ENGINE ADDED 4.5 QTS, NR 2 ENGINE ADDED 4.0 QTS AND APU 0 ENGINE OIL ADDED INFO ENTERED INTO WEB BASED OIL MONITORING DATA BASE.Jul 10, 2008 · N558AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA0853110Controller · faultedRT SIDE WINDOW HT OVERHEAT LT ILLUMINATED COMPLETED QRH PROCEDURE OPS NORMAL REMAINDER OF FLT PERFORMED WINDOW HEAT SYS OPS TEST PER MM 30 41 00 SYSTEM CHECK GOOD.Jun 29, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0853089Controller · faultedDURING PREFLIGHT "AUTO FAIL" AND "ALTN" ILLUMINATED ON PRESSURIZATION CONTROLLER. CYCLED AUTO PRESSURE CONTROL SW IN MAN AND DROVE OF VLV DOOR CLEARED FAIL LT, PERFORMED AUTO PRESS PNL CONTROLLER BITE NR 1 PASS NR 2 LOGGED CABIN PRESS CONT FAULT CLEARED ALL AJun 25, 2008 · N558AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA0852974Oil Filter · dirtyAPU OIL FILTER DELTA P INDICATOR EXTENDED REQUIRES MAINT REF: T C 78349013. REPLACED APU OIL FILTER AND RESET DELTA P INDICATOR, OPERATED APU FOR 30 MIN AND RE-CHECKED DELTA P INDICATOR. INDICATOR REMAINS RESET AMM 49 91 13 & 49 91 12.May 20, 2008 · N558AS · Boeing 737890 · APU Oil SystemSDR ASAA0852870Warning System · malfunctionedTHE "FMC DISAGREE" MESSAGE ON CDU AND MAP DISPLAYS. ACCOMPLISHED FIM 34 61 TASK 835. THE "FMC DISAGREE" MESSAGE ERASED AND NO FURTHER DISCREPANCIES.May 4, 2008 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA0852869Warning System · malfunctionedAFTER ENGINE START "ELEC" LIGHT ON OVERHEAD PANEL CAME ON. ACCOMPLISHED FIM 24 31 TASK 801 & 24 34 TASK 802. FAULT CODE CLEARED. PER FIM FAULT WAS INTERMITTENT, OK FOR SERVICE.May 4, 2008 · N558AS · Boeing 737890 · AC Indicating SystemSDR ASAA0852804Circuit Breaker · damagedUPON LEVEL OFF AT FL370 RT FWD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED AND WINDOW HEAT POWER C/B POPPED OPEN. FOUND HEAT DAMAGE ON WIRE AND LUG AT WINDOW HEAT PWR C/B. REPLACED C/B C394 (RT WINDOW HEAT PWR). REPLACED TERM LUG TO C/B C394. WINDOW HEAT CONTROApr 2, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0852803Window · faultyRIGHT FWD WINDOW HEAT OVERHEAT ILLUMINATED ACCOMPANIED BY POPPED C/B. REPLACED R1 WINDOW AND RESET C/B.Apr 1, 2008 · N558AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA0852782Control Unit · faultedRIGHT FWD WINDOW OVERHEAT LIGHT ILLUMINATED IN FLIGHT. FOUND RT FRONT WINDOW HEAT PWR C/B OUT. VISUAL INSPECTION OF WIRING AT WINDOW AND RACK GOOD. RESET C/B. UNABLE TO VERIFY DISCREPANCY REPLACED RT FWD WINDOW HEAT CONTROLLER PRECAUTIONARY. OPS CHECK GOOMar 27, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0852705Warning System · malfunctionedLEFT SIDE WINDOW OVERHEAT LIGHT ANNUNCIATED. QRH FOLLOWED. OPS NORMAL. REPEAT WRITE UP. WINDOW HEAT CONTROLLER LOGS WINDOW SENSOR FAILURE. ACCOMPLISHED VISUAL INSPECTION OF L1 WINDOW NO CRAZING NOTED. NO VISUAL DISTORTION OR DEFECTS NOTED. CHANGED TO SPMar 10, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0852701Computer · malfunctionedCAT IIIA AUTOLAND AIRCRAFT TRACKED AND TOUCHED DOWN APPROX 35' LEFT OF CENTERLINE. NO FLIGHT FAUTLS LOGGED. CURRENT STATUS CHECKED NORMAL. PERFORMED "LAND VERIFY" TEST PG 201. TEST PASSED. PERFORMED HGS SENSOR TEST, ALL NO DEFECTS.Mar 9, 2008 · N558AS · Boeing 737890 · Autopilot ComputerSDR ASAA0852689Valve · faultyZONE TEMP ILLUMINATED ON RECALL, "CONT CAB" FOUND RT CONTROLLER FLT DECK TRIM AIR VALVE FAULT LIGHT ON. REPLACED FLIGHT DECK TRIM AIR VALVE. OP & LEAK CHECK OK. CLEARED PACK ZONE TEMP CONTROLLER FAULT.Mar 2, 2008 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0852687Warning System · malfunctionedLEFT SIDE WINDOW OVERHEAT LIGHT CAME ON. COMPLIED WITH QRH THE LIGHT EXTINGUISHED. PERFORMED CNTL CABIN WINDOW ANTI ICE SYSTEM TEST. OP CHECKS GOOD.Feb 28, 2008 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA0852683Warning System · malfunctionedBOTH ND'S DISPLAY "FMC DISAGREE" PERFORMED FIM 34 61 TASK 835. NO FLIGHT FAULTS SYSTEM FUNCTIONS NORMALLY. UNABLE TO CONFIRM ORIGINAL FAULTS.Feb 27, 2008 · N558AS · Boeing 737890 · Central WarningSDR ASAA0852643Filter · cloggedWHILE PERFORMING TASKCARD 78349013 (APU OIL FLITER DELTA P INDICATOR) FOUND THE INDICATOR EXTENDED. ACCOMPLISHED OIL FILTER INDICATOR SERVICING. LEAK CHECK OK.Feb 24, 2008 · N558AS · Boeing 737890 · APU Oil SystemSDR ASAA0852590Modulating Valve · faultyAFTER ENGINE START DURING RECALL GOT A "CNTL CAB ZONE TEMP" LIGHT. FOUND CNTL CAB ZONE TRIM MOD VALVE FAULT LOGGED ON NR 1 TEMP CONTROLLER. REPLACED CONTROL CABIN TRIM MOD VALVE. GROUND BITE TEST OK.Feb 16, 2008 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0852541Hf Comm · malfunctionedBOTH HF2 RADIOS WILL NOT GO INTO DATA MODE. UNABLE TO DUPLICATE. NR 2 HF DATA MODE OPS NORMAL (REF 23 27 00), NR 2 HF OPS NORMAL (REF 23 11 00).Feb 7, 2008 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA0852539Transceiver · malfunctionedBOTH HF2 RADIOS WILL NOT GO INTO DATA MODE. UNABLE TO DUPLICATE. NR 2HF DATA MODE OPS NORMAL (REF MM23 27 00) HF OPS NORMAL. (REF MM23 11 00)Feb 7, 2008 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA0852535Radio · malfunctionedNR 1 HF RADIO GARBLED. SELCAL CHIME AND LIGHT OK. FREQ 6673 & 3452 ATTEMPTED IN FLIGHT. HF NR 2 VOICE AND SELCAL OK. UNABLE TO VERIFY DISCREPANCY. REPLACED AND TESTED NR 1 HF ANTENNA COUPLER IAW 23 11 61 PGS 401 409. NO DISCREPANCIES NOTED.Feb 2, 2008 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA0852456Starter Gen · faultyAPU "MAINT" LIGHT ILLUMINATED. VERIFIED FAULT CODE 49 41244. ACCOMPLISHED FIM 49 40 TASKS 805 806. REPLACED STARTER GENERATOR (REF MM 49 41 21 PG 401). GROUND VERIFICATION GOOD.Jan 7, 2008 · N558AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA0752383Idg · overservicedNR 2 ENGINE IDG IS OVER SERVICED WITH OIL. RESERVICED NR 2 IDG IAW AMM12 13 21. REMOVED 0.50QT.Dec 14, 2007 · N558AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0752382Idg · overservicedNR 1 ENGINE IDG IS OVERSERVICED WITH OIL. RESERVICED NR 1 ENGINE IDG IAW AMM12 13 21. REMOVED 0.75QT.Dec 14, 2007 · N558AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA0752385Skin · puncturedLEFT WING NR 6 SPOILER PUNCTURED AT LOWER SURFACE APPROX WBL 96. REPAIRED IAW B737 800 SRM 51-70-10 REPAIR 2.Dec 12, 2007 · N558AS · Boeing 737890 · SpoilersSDR ASAA0752208Pressure Switch · faultyRIGHT CENTER TANK FUEL PUMP LOW PRESSURE LIGHT DID NOT ILLUMINATE MOMENTARILY WHEN PUMP SWITCHED ON. REPLACED LOW PRESSURE RIGHT CENTER FUEL SWITCH. SIGNIFICANT SYSTEM VERIFICATION SUCCESSFUL.Nov 4, 2007 · N558AS · Boeing 737890 · Fuel Pressure IndicatorSDR ASAA0752126Sensor · dirtyAFT CABIN TEMP CONTROLLER WILL NOT MAINTAIN TEMPERATURE. WITH KNOB AT 2 O`CLOCK TEMP INDICATES 7 DEGREES. C DUCT SUPPLY STABILIZES IN MANUAL MODE. VERIFIED TEMP CONTROL WITH TRIM AIR SWITCH SELECTED OFF. NO FAULTS LOGGED ON CONTROLLERS.Oct 17, 2007 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA0650967Converter · smokeON TAKEOFF ROLL HAD SMOKE FILL COCKPIT ACID OIL SMELL AND IRRITATION TO EYES. ABORT SPEED 130 KNOTS SMOKE CLEAR WITH ENGINES AT IDLE PERFORMED CABIN ODOR TROUGLESHOOTING PROCEDURES IAW MM 05 60 00 P101. RAN ENGINES AT IDLE AND HIGH POWER. UNABLE TO DUPLICATSep 21, 2006 · N558AS · Boeing 737890 · Air Distribution SystemSDR ASAA060967Converter · odorON TAKEOFF ROLL HAD SMOKE FILL COCKPIT ACID OIL SMELL AND IRRITATION TO EYES. ABORT SPEED 130 KNOTS SMKE CLEAR WITH ENGINES AT IDLE.Sep 21, 2006 · N558AS · Boeing 737800* · Air Distribution System
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