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 ASAA2013112996567Warning Message · illuminatedFOUND NR 2 ENGINE WITH MAINTENANCE MESSAGE 73-21352, LONG TERM. APL VOLTAGE TO EEC OUT OF RANGE. AIRCRAFT GROUNDED.Nov 29, 2013 · N558AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2013112996566Warning Message · illuminatedFOUND NR 2 ENGINE WITH MAINTENANCE MESSAGE 76-31362, LONG TERM, START LEVER SIGNALS DISAGREE. ACFT GROUNDED. OPENNov 29, 2013 · N558AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2013111996466Start Valve · failedCOULD NOT START NR 1 ENGINE. ACFT GROUNDED. CHECKED AND FOUND NR 1 ENG START VALVE STUCK CLOSED. REPLACED NR 1 ENG START VALVE IAW AMM 80-11-03. LEAK AND OPS TEST NORMAL.Nov 19, 2013 · N558AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2013111696432Door · unknownLEFT RAM AIR DOOR OPENED FOR APPROXIMATELY 5 MINUTES DURING DESCENT 350KTS CLOSED AT 13000. ACFT GROUNDED.Nov 16, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013092996076Controller · inoperativePRESSURIZATION CONTROLLER FLT ALT NRS INOP. FLICKERED THEN WENT INOPERATIVE. ACFT GROUNDED. REPLACED CABIN PRESSURE CONTROL MODULE IAW AMM TASK 21-31-02-000-801. OPS CHECKED GOOD.Sep 29, 2013 · N558AS · Boeing 737890 · Cabin Pressure ControllerSDR ASAA2013092396038Valve · warning lightON RECALL DURING LANDING CHECKLIST LT PACK LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED FIM 21-62 TASK 830 FOUND LT PACK TCV FAULT. REPLACED LT TCV REF MM 21-51-10. OPS CKS GOOD.Sep 23, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013091795993Warning Light · illuminatedAUTO FAIL AND ALTN LIGHTS ILLUMINATED ON PREFLIGHT. ACFT GROUNDED. CONFIRMED FAULT LIGHT ON. RESET CONTROLLER BREAKERS AND LIGHT WENT OUT. OPS GOOD IAW TASK 21-31-00-700-802.Sep 17, 2013 · N558AS · Boeing 737890 · Central WarningSDR ASAA2013090795934Actuator · malfunctionedLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. PACK LIGHT EXTINGUISHED DURING MASTER CAUTION RESET. ACFT GROUNDED. REPLACED THE LT RAM AIR INLET ACTUATOR ASSY, REF MM 21-51-21-400. OPS., BITES CK NORMAL.Sep 7, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013090295914Warning Light · illuminatedON SELECTING RECALL ON LANDING CHECKLIST, LEFT PACK LIGHT ILLUMINATED. PACK LIGHT RESET. ACFT GROUNDED. RESET 4 RAM ACTUATOR FAULT ON NR 1 PACK/ZONE TEMP CONTINUED BOTH PACK/ZONE TEMP. CONTS BITE TEST GOOD IAW MM 21-61-00.Sep 2, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013082495875Fmc · warning messageFMC DISAGREE MESSAGE ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE, MESSAGE DID NOT RETURN.Aug 24, 2013 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013082195859Sensor · dirtyAFT F/A SAID ITS COLD IN AFT PORTION OF CABIN. DUCT TEMP AT 20-22C W/ AFT CABIN TEMP SHOWING 30-32. TEMP KNOB MOVED TO 3-4 O`CLOCK POSITION WITH NO INCREASE IN HEAT. DISCUSSED W/ MX CONTROL VIA SAT COM. POSSIBLE AFT CABIN TEMP PROBE FAILURE/ CONTAMINATIONAug 21, 2013 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013080695742Fuel Control · faultedAPU BITE CHECK, LOGGED OVERTEMP SHUTDOWN MESSAGE 49-31016 AND FCU RESOLVER CIRCUIT SHOWS BAD 49-31175. ACFT GROUNDED. REPLACED THE FCU IAW MM 49-31-11, LEAK AND OPS CHECKED GOOD. APU BITE CHECKED GOOD IAW MM 49-61-00.Aug 6, 2013 · N558AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2013080195714Starter · inoperativeNR 2 ENGINE HAS NO ROTATION ON START. ACFT GROUNDED. R & R NR 2 ENG STARTER IAW 80-11-01.Aug 1, 2013 · N558AS · Boeing 737890 · Engine StarterSDR ASAA2013072195650Landing Gear · malfunctionedAFTER TAKEOFF, LANDING GEAR WAS RETRACTED NORMALLY. DURING AFTER TAKEOFF FLOW, WHEN LANDING GEAR HANDLE WAS PLACED TO OFF, THE RED NOSE GEAR LIGHT ILLUMINATED AND WAS ACCOMPANIED BY NOSE GEAR AIR NOISE. FOLLOWED QRH AND RAISED HANDLE TO UP. PROCEEDED TO ANJul 21, 2013 · N558AS · Boeing 737890 · Landing Gear Retraction/Extension SystemSDR ASAA2013071395588Wire Harness · faultyENG 2 OVERHEAT DOES NOT ILLUMINATE DURING OVHT/ FIRE TEST. ACFT GROUNDED. CONFIRMED. WITH LOOP A SELECTED ON NR 2 ENGINE - FIRE TEST NORMAL. BITE CHECKED FIRE DETECT MODULE. ALL 3 LIGHTS ON FOR NR 2 ENG B LOOP. WIRING OPEN OR DETECT FAULTS. REPAIRED HARNEJul 13, 2013 · N558AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2013071395587Unknown · unknownSATCOM PROMPT ON CDU IS MISSING. UNABLE TO SELECT SATCOM. SATCOM CB CHECKED IN. ACFT GROUNDED. ACCOMPLISHED SATCOM SYS TEST- NO DEFECTS. GROUND VERIFICATION SUCCESSFUL. REF AMM 23-15-00-730-801.Jul 13, 2013 · N558AS · Boeing 737890 · Communications SystemSDR ASAA2013062795351Control Valve · inoperativeLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. REPLACED LT RAM AIR INLET ACTUATOR. OPS CHECKS OK REF AMM 21-51-21-000-801 AND 21-51-21-400-801. FOLLOWUP TO REPORTS OF LT PACK LIGHT ON RECALL. REPLACED LT TCV. OPS AND LEAK CHECKS OK, REF AMM 21-51-Jun 27, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013062295235Warning Light · false activationLEFT PACK LIGHT ILLUMINATES ON RECALL DISEATED ON AFTER LANDING CHECKS. ACFT GROUNDED. ACCOMPLISHED GROUND VERIFICATION OF THE CABIN TEMP CONTROLLER BITE TEST IAW AMM 21-61-00-700-806-002, UNABLE TO CONFIRM. ACCOMPLISHED CABIN TEMP CONTROL AND INDICATION OPJun 22, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013062195238Controller · malfunctionedON RECALL OF MASTER CAUTION ILLUMINATION OF THE LT PACK LIGHT. MASTER CAUTION RESET LIGHT OUT. ACFT GROUNDED. PERFORMED ZONE TEMP CONTROLLER BITE TEST ON LT AND RT TEMP CONTROLLERS IAW AMM 21-61-00-700-806-002, OPS CHECKED GOOD, NO FAULTS NOTED.Jun 21, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013061195075Warning Light · false activationLEFT PACK LIGHT ILLUMINATED, EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED BITE TEST NR 1 CONTROLLER IAW FIM TASK 21-62, TASK 837. CHECKED GOOD, NO MX MESSAGE SHOWN.Jun 11, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013041394456Transceiver · failedHF 1 DOES NOT TRANSMIT OR RECEIVE CAN NOT HEAR SIDE TONE. ACFT GROUNDED. CONFIRMED FAILURE NO TRANSMIT OR RECEIVE & NO SIDE TONE. REPLACED NR 1 HF TRANSCEIVER IAW AMM 23-11-21-000-801. PERFORMED GROUND VERIFICATION OPS CHECK IAW AMM 23-11-00-730-801. OPS NOApr 13, 2013 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA2013041194455Circuit Breaker · trippedHF 1 LOCATED P18-2 POSITION 11 TRIPPED CIRCUIT BREAKER. TESTED THE NR 1 HF SYS IAW AMM 23-11-21-400-801, STEP F. ALSO, MADE A CLEAR RADIO CHECK USING THE NR 1 HF SYS. CHECKED THE RESET CIRCUIT BREAKER ON THE P18-2 PANEL IAW AMM 20-60-01-860-801.Apr 11, 2013 · N558AS · Boeing 737890 · HF Communications SystemSDR ASAA2013040194320Start Valve · failed1 STARTER VALVE WOULD NOT OPEN. REPLACED THE NR 1 START VALVE IAW AMM 80-11-03-000/400-801. OPS TEST AND LEAK CHECK GOOD.Apr 1, 2013 · N558AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2013040194313Indicator · malfunctionedRT FUEL QUANTITY WENT BLANK AFTER SHOWING 9200 LBS AT TOP OF CLIMB, WAS BLANK FOR ABOUT 1 HR THEN CAME BACK AND ACTED NORMALLY. COMPLETED T/C 800-28EA-10039, NO HISTORY PAST 60 DAYS, NO CURRENT FAULTS. PERFORMED FUEL STICK TO VERIFY GAUGE. GAUGE AND FUEL STApr 1, 2013 · N558AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2013022293964Shroud · crackedAPU SHROUD HAS A CRACK ON AFT BASE 2.1 LONG. ACFT GROUNDED. R & R APU DRAIN SHROUD.Feb 22, 2013 · N558AS · Boeing 737890 · APU Cowling/ContainmentSDR ASAA2013020293793Control Valve · inoperativeRIGHT PACK LIGHT CAME ON AFTER ENG START. ACFT GROUNDED. BITE CHECK SHOWED RT PACK TCV INOP. R & R RT PACK TEMP CONT VALVE. CLEARED FAULT ON RT PACK, OPS NORMAL REF AMM 21-51-10.Feb 2, 2013 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012122693552Warning Light · false activationFMC DISAGREE MESSAGE AFTER TAXI OUT. FOLLOWED QRH PROCEDURE, OPS NORMAL.Dec 26, 2012 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012112893378Control Valve · malfunctionedRT PACK LIGHT ILLUMINATES ON RECALL. BITE SHOWS TCV FAULT ON NR 2 CONTROLLER. RAN BITE & FAULT CLEARED. OPS NORMAL REF AMM 21-61-01.Nov 28, 2012 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012112293359Oil System · lowAPU MAINT LIGHT ILLUMINATED. FOUND APU OIL LEVEL LOW, SERVICED APU WITH 1 QT OIL. STARTED APU 3 TIMES MAINT LIGHT REMAINS EXTINGUISHED. AC OK FOR SERVICE.Nov 22, 2012 · N558AS · Boeing 737890 · APU Oil SystemSDR ASAA2012112093342Valve · malfunctionedON TOUCHDOWN SPAR VALVE CLOSED LIGHT ILLUMINATED AFTER 5-6 SECONDS LIGHT EXTINGUISHED. NO ABNORMAL INDICATIONS. VERIFIED WITH CREW NR 1 SPAR VALVE WAS THE AFFECTIVE UNIT. R & R NR 1 SPAR VALVE IAW AMM 28-22-11-400-804. OPS CHECK OK IAW AMM 28-22-10-710-801.Nov 20, 2012 · N558AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2012111593306Bulb · failedRT PACK TEMP INDICATION PEGS ZERO. PACK WORKS OK. CHECKED RESISTANCE AT RT PACK TEMP BULB FOUND VERY LOW RESISTANCE. REPLACED RT PACK TEMP BULB WITH NEW ONE. VERIFIED RT PACK TEMP IND NOW INDICATES REF MM 21-51-60-400-801 & WDM 21-61-51.Nov 15, 2012 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012111193275Warning Light · false activationON LANDING ROLL OUT, THE NR 1 SPAR VALVE CLOSED LIGHT ILLUMINATED (FLICKERED) ON AND OFF SEVERAL TIMES. REMOVED AND CLEANED CONNECTOR PLUG, NO CORROSION NOTED, ALL WIRES SECURE, RECONNECTED CONNECTOR PLUG, GROUND FUNCTIONAL CHECKED GOOD IAW FIM TASK 28-22 TASNov 11, 2012 · N558AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2012110793262Wire · brokenWHILE CHANGING AUX BATTERY FOUND WIRE (W2532-0531-1/0) BROKEN FROM NEGATIVE BATTERY CONNECTOR CABLE. TERMINATED WIRE W2532-0531-1/0 & W2532-220R-24. REF WDM 24-31-12 & SWPM 20-30-11, OPS CHECK NORMAL, REF MM 24-31-11.Nov 7, 2012 · N558AS · Boeing 737890 · Electrical Power System WiringSDR ASAA2012101593117Warning Light · false activationNR 1 ENGINE, WHILE PERFORMING T/C 78273000 HAD SHORT TERM FAULT 73-30311, THE START SWITCH SIGNAL AND BUSS DATA DISAGREE. ACCOMPLISHED T/C 78273000, FAULT NO LONGER ACTIVE.Oct 15, 2012 · N558AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2012090992852Warning Light · illuminatedRT PACK LIGHT ILLUMINATED. LIGHT CLEARS ON RECALL. BITE TEST OF NR 2 TEMP. CONT SHOWS FAULT TEMP CONTROL VALVE ON PACK. PERFORMED FIM 21-62-00-801. RAN RT PACK, FAULT CLEARED & DID NOT RETURN.Sep 9, 2012 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012092692949Actuator · leakingNR 2 ENGINE BLEED VALVE LEAKING FROM FUEL VENT DRAIN. R & R NR 2 ENGINE LT VBV ACTUATOR OPS & LEAK CHECKED GOOD IAW MM 75-32-02-000-801-F00, 75-32-02-400-801-F00, 71-00-00-700-807-F00 75-32-00-730-801-F00.Sep 8, 2012 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012090792840Pump · failedRT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. UNABLE TO CONFIRM DISCREPANCY. R & R RT CENTER TANK FUEL BOOST PUMP IAW AMM 28-22-41. BOOST PUMP OPS CHECKED GOOD IAW AMM 28-22-41.Sep 7, 2012 · N558AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2012090692842Warning Light · illuminatedFMC DISAGREE LIGHT ON THE GROUND IN DCA. ACFT GROUNDED. RESET FOLLOWING QRH PROCEDURE. OPS NORMAL.Sep 6, 2012 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012090592829Fmc · false activationON TAXI OUT, FMC DISAGREE MESSAGE. ACCOMPLISHED QRH, MESSAGE CLEARED.Sep 5, 2012 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012091392885Solenoid Valve · malfunctionedON INITIAL CLIMB, IN CONT LGT TURB, YAW DAMPER SWITCHED WENT TO OFF. WHEN RIDE WAS SMOOTHED, PLACED SWITCH TO ON , YAW DAMPER SWITCH STAYED ON. R & R MAIN RUDDER PCU SOLENOID VALVE AND TRANSFER VALVE, OPS CHECK AND LEAK CHECK GOOD IAW AMM 22-23-21.Sep 1, 2012 · N558AS · Boeing 737890 · Rudder Control SystemSDR ASAA2012091192866Yaw Damper · failedYAW DAMPER DISENGAGED TWICE ON APPROACH. (APPROX 1500 & 300AGL) ACFT GROUNDED. NR 1 SMYD SHOWS YD SERVO LOOP FAULT WITH MX MESSAGE 22-21006. ACCOMPLISHED FIM 22-23-809. TEST PASS & NO FAULTS UNDER EXISTING FAULTS. ON NEXT FLIGHT, ON TAKE-OFF, Y/D KICKED-OFF.Sep 1, 2012 · N558AS · Boeing 737890 · Speed-Attitude Correction SystemSDR ASAA2012073192638Indicator · false indicationON PDC WALK AROUND FOUND NR 1 ENGINE DPI ON IDG EXTENDED. REMOVED NR 1 IDG SCAVENGE FILTER IAW AMM 24-11-41-000-801. INSPECTED IAW AMM 24-11-41-200-801, NO DAMAGE OR CONTAMINATION FOUND. INSTALLED NEW FILTER AND SERVICE IDG, RUN ENGINE AND LEAK CHECKED, NO Jul 3, 2012 · N558AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA12511668Connector · unsecureRT SIDE WINDOW HEAT OVERHEAT ORH FOLLOWED RESET TO NORMAL. ACFT GROUNDED. CHECKED CONNECTOR PLUG TO SLIDER AFT PLUG NOT FULLY ENGAGED. PERFORMED FIM TASK 30-41-00-810-801. FOUND HISTORY OF TEMP SENSOR BIT TEST, OK, PASSED GREEN LIGHT. NO HISTORY 30 DAYS.Jun 8, 2012 · N558AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2012062792431Actuator · failedAFTER NR 1 ENGINE START, ENGINE ROLLED BACK. TRIED TO ENGAGE GENERATOR NR 1 AND IT DID NOT TAKE. EGT DROPPED LOWER THAN NORMAL, AFTER ROLLBACK AND FUEL FLOW DROPPED TO ZERO. CLOSED FUEL SHUTOFF VALVE AND SHUTDOWN NR 1 ENGINE. NO LIMITS WERE EXCEEDED DURINJun 2, 2012 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012062192398Window · out of limitsRT SIDE WINDOW HEAT OVERHEAT AMBER LIGHT ILLUMINATED AFTER LEVEL-OFF AT FL 350, WITH ON LIGHT GOING OFF. ACCOMPLISHED QRH. OPERATED MANUALLY THERE AFTER. FLIGHT CREW STATED WINDOW HEAT OPS NORMAL LAST 4HRS OF FLT. COMPLIED WITH FIM 30-34-00-810-801, FOUND Jun 2, 2012 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012061992379Warning Light · false activationWINDOW HEAT RT SIDE OVERHEAT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED WINDOW HEAT, OPS TEST IAW AMM 30-41-00-710-801, SYS OPS CHECKED GOOD, NO DEFECTS NOTED, OK FOR SERVICE. DUE TO HISTORY, REPLACED F/O SLIDER FLEX CORD, GROUND VERIFICATION TEST PASSED REF Jun 1, 2012 · N558AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA12511544Apu · shutdownON PUSH BACK, APU SHUTDOWN WITH FAULT LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED TROUBLESHOOTING IAW AMM 49-60-00-810-801. FAULT 49-91005 HIGH OIL TEMP SHUTDOWN. PERFORMED VISUAL INSPECTION OF OIL COOLER AND EDUCTOR, NO DAMAGES FOUND IAW AMM 49-90-00-810-May 11, 2012 · N558AS · Boeing 737890 · APU Oil SystemSDR ASAA12511515Blade · mismanufacturedCOATING MISSING FROM ALL 24 FAN BLADE SHIMS ON THE NR 1 ENGINE. ACFT GROUNDED. R & R ALL FAN BLADE SHIMS ON NR 1 ENGINE, REF MM 72-21-02.May 3, 2012 · N558AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA12511493Control Unit · failedFUEL QTY IS NOT AUTOMATICALLY UPDATING IN FMS. ATTEMPTED FQIS BITE PER FIM 28-41 TASK 801 ON MCDU. FQIS BITE INOP MESSAGE SHOWED. PERFORMED FMCS BITE PER FIM 34-61 TASK 801 FQIS FAULTED ON EVERY LEG. REMOVED AND REPLACED FUEL PROCESSOR UNIT REF MM 28-41-81 OPApr 30, 2012 · N558AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA12511471Fire Detector · inoperativeNR 2 ENG B SYSTEM, FIRE DETECTION INOPERATIVE. ACFT GROUNDED. ACCOMP ENG/APU FIRE DETECT CONTROL MODULE BITE IAW FIM TASK 26 10 00 810 801. ENG 2, LOOP B, CORE LT DETECT FAULT LOGGED. PERF FIM TASK 26-10-00-810-805. LT CORE DETECT ELEMENT RESISTANCE READSApr 27, 2012 · N558AS · Boeing 737890 · Fire Detection
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