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 ASAA2016030215723Heat Exchanger · crackedRIGHT PLENUM AND HEAT EXCHANGER FOR THE PRIMARY BROKEN AND CRACKED. ACFT GROUNDED. R & R PRIMARY RT PLENUM AND HEAT EXCHANGER ASSY REF AMM 21-51-03-000-804-002 AND AMM 21-51-03-804-002, 21-51-03-400. PERFORMED HEAT EXCHANGER AND PLENUM/DIFFUSER INSTALLATION Mar 2, 2016 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016022015593Engine · faultedWHILE ACCOMPLISHING TASK CARD 78273000, ENGINE 2 LOGGED ECONOMIC FAULT 73-31372, UPPER EGT SENSORS READING HIGH. ACFT GROUNDED. ACCOMPLISHED FAULT ISOLATION IAW FIM 73-11, TASK 801. RAN ENGINE NR 2 AT IDLE FOR 5 MIN, ALL T49.5 PARAMETERS WERE IN RANGE, DIDFeb 20, 2016 · N558AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016022015579Control Valve · malfunctionedPACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL. EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. ZONE TEMP CONTROLLER BITE TEST FAULTED THE LT PACK TEMP CONTROL VALVE AND WOULD NOT RESET. R & R THE LT PACK TCV IAW AMM 21-51-21. ZONE TEMP CONTROLLER BFeb 20, 2016 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016021915576Warning Light · false activationLEFT PACK LIGHT ILLUMINATES DURING RECALL, EXTINGUISHES WHEN MASTER CAUTION IS RESET. ACFT GROUNDED. LEFT PACK, ZONE TEMP CONTROL BITE SHOWS RAM AIR ACTUATOR FAULT WITH BIT SWITCH. VERIFY SWITCH TEST PASSES. REF FIM 21-62, TASK 801. RESET FAULT AND OPERATEFeb 19, 2016 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016021815575Warning Light · false activationLEFT PACK LIGHT ON RECALL. ACFT GROUNDED. PREVIOUS FLIGHT LOGGED RAM AIR ACTUATOR FAULT ON NR 1 CONTROLLER. RESET FAULT. ACCOMPLISHED NR 1 PACK/ZONE TEMP CONTROLLER GROUND VERIFICATION TEST REF AMM 21-61-00. NO DEFECTS FOUND.Feb 18, 2016 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016021615476Actuator · failedDURING CLIMBOUT LT PACK LIGHT, LT PACK TEMP 100 DEGREES, RAN QRH, RESET PACK. LT PACK LIGHT RE-ILLUMINATED. CONTACTED MAINT CONT RESET PACK, PACK LIGHT ILLUMINATED. LT PACK TEMP COOLED ONLY WITH LT PACK OFF. ACFT GROUNDED. REPLACED LT RAM AIR DOOR INLET ACFeb 16, 2016 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016021315417Valve · failedON RECALL THE CONTROLLER CABIN ZONE TEMP LIGHT ILLUMINATES ALONG WITH THE MASTER CAUTION AN AIR CONDITION ANNUNCIATOR. ACFT GROUNDED. PERFORMED BITE TEST OF BOTH PACK/ZONE TEMP CONTROLLERS, REF AMM 21-61-00. RT CONTROLLER FAULTED FLIGHT DECK TRIM MODULATINGFeb 13, 2016 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016013015177Egt Indication · reads highWHILE ACCOMPLISHING TC 78273000 NR 2 ENGINE UPPER EGT SECTOR READ HIGH. ECONOMIC FAULT. ACFT GROUNDED. ACCOMPLISHED FAULT ISOLATION IAW FIM 73-11, TASK 801. RAN ENGINE NR 2 AT IDLE FOR 5 MIN. ALL T49.5 PARAMETERS WERE IN RANGE, DID NOT FLUCTUATE. ELECTRJan 30, 2016 · N558AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2016012715064Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED. ACFT GROUNDED. RAN PACK/ ZONE TEMP CONTROL BITE TEST WITH NO FAULTS IAW AMM 21-61-00-700-806-002.Jan 27, 2016 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016012615032Lamp · failedEMERGENCY EXIT LIGHT INOPERATIVE ON FUSELAGE NEAR L1 DOOR. ACFT GROUNDED. RELAMPED L1 SLIDE LIGHT AND TESTED LAMP IAW AMM 33-51-04, LAMP TEST GOOD.Jan 26, 2016 · N558AS · Boeing 737890 · Emergency LightingSDR ASAA2016011414834Regulator · failedNR 1 ENGINE BLEED AIR REGULATOR FAILED HEALTH CHECK. ACFT GROUNDED. R & R NR 1 ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03. LEAK AND OPS CHECK GOOD.Jan 14, 2016 · N558AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2016011214789Doubler · corrodedAFT CARGO COMPARTMENT FLOOR AREA TRANSITION PANEL LOWER PLATE UPPER SURFACE HAS CORROSION AT BS 727I+6 , STR 25R AND STR 26R. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO COMPARTMENT TRANSITION PANEL LOWER PLATE UPPER SURFACE BS727I+6, STR 25R AND 26R. ORIJan 12, 2016 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016011014846Floorbeam · corrodedFWD PIT CENTER FLOOR SUPPORT CORRODED, FROM TRANSITION PANEL TO TRANSITION PANEL, BS 500I. ACFT GROUNDED. REMOVED CENTER SUPPORT CORRODED IAW SRM 51-40-02, RECEIVED NEW SUPPORT ANGLE, PN 143A9485, REV F, INSTALLED CENTER SUPPORT ANGLE IAW SRM 51-40-02 PO 854Jan 10, 2016 · N558AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016011014791Channel · corrodedFWD PIT RT SIDE TRANSITION PANEL CORRODED BS 500F-BS 500I. ACFT GROUNDED. REMOVED DAMAGE CHANNEL SECTION BS 500F TO 500I IAW SRM 51-40-02, MATERIAL ID FOR FABRICATION. BAC 1496-444 IAW SRM 53-30-53-01, FIG 2, TABLE 2, FABRICATED NEW SECTION IAW SRM 53-00-53Jan 10, 2016 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016010914930Floor Panel · crackedPARTS RACK, AFT PIT FLOOR PANEL 140BF CRACKED IN 2 AREAS. ACFT GROUNDED. FABRICATED AFT PIT FLOOR PANEL 140BF IAW BAC DWG 453A2610, REV C ALODINED & PRIMED IAW SRM 51-20-01.Jan 9, 2016 · N558AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016010914929Floor Panel · corrodedFWD CARGO FLOOR PANEL 120AF CORRODED IN SEVERAL AREAS. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL 120AF IAW DWG 453A1610, REF F. ALODINE TREATED AND RESTORED PRIMER FINISH IAW SRM 51-20-01 AND AMM 51-21-72.Jan 9, 2016 · N558AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016010914788Floor Panel · corrodedFWD CARGO FLOOR PANEL 120DF CORRODED IN SEVERAL AREAS. ACFT GROUNDED. FOUND TO BE OUT OF LIMITS EXCEEDED 3" MAXIMUM ALLOWED IAW SRM 53-00-53. MATERIAL ID IS 2024-T3, .071 IAW DWG 453A1610, REV T, PO 856649-1, FABRICATED NEW FLOOR PANEL IAW DWG 453A1610, REV FJan 9, 2016 · N558AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016010914787Floor Panel · crackedFWD CARGO FLOOR PANEL 120CF CRACKED AND CORRODED IN SEVERAL AREAS. ACFT GROUNDED. AFTER FURTHER INVESTIGATION, CORROSION EXCEEDS ALLOWABLE LIMITS OF 3" CRACKS NOT ALLOWABLE REPAIRS OUT OF LIMITS IAW SRM 53-00-53, MATERIAL ID FOR NEW PANEL 2024-T3 0.071 IAWJan 9, 2016 · N558AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016010914785Floor Panel · corrodedPARTS RACK, AFT PIT FLOOR PANEL 140AF CORRODED IN SEVERAL AREAS. ACFT GROUNDED. MATERIAL ID FOR PANEL IS 2024T3 .071 PO 851953.2 IAW BAC DWG 453A2610 FABBED FLOOR PANEL IAW DWG 453A7610, ALODINED & PRIMED IAW SRM 51-20-01. REMOVED DOT H193 PART MARKED IAW DJan 9, 2016 · N558AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2016010714786Skin · crackedCRACK INDICATION AT BS 129.50 RT LOWER HORIZONTAL SKIN PANEL 16" FORWARD OF REAR SPAR. MARKED IN RED. ACFT GROUNDED. REMOVED RT L/E PANEL AND STAB TIP CAP ASSY IAW AMM 27-41-21. ROUTED OUT DAMAGED AREA AND REPAIRED IAW SRM 55-10-01-2R-11. INSTALLED RT L/E Jan 7, 2016 · N558AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015122614470Warning Light · illuminatedAT CRUISE, THE "ENGINE VALVE CLOSED", LIGHT ILLUMINATED BRIGHT BLUE FOR NR 2 ENGINE ALL ENGINE INSTRUMENTS WERE NORMAL. ALL ASSOCIATED CB WERE IN, AND NONE TRIPPED. LIGHT STAYED ON FOR REST OF FLIGHT. ACFT GROUNDED.Dec 26, 2015 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015121914337Warning Message · false activationFMC FAULT NR 2 ENGINE MESSAGE NR 73-31372, UPPER EGT SECTORS READING HIGH, FLT LEG 2. ECONOMIC FAULT. ACFT GROUNDED. ACCOMPLISHED TROUBLESHOOTING IAW FIM 73-11, TASK 801, NO FAULTS NOTED.Dec 19, 2015 · N558AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2015121214220Warning Light · illuminatedNR 2 "ENGINE VALVE CLOSED" LIGHT ILLUMINATED BRIGHT BLUE IN FLIGHT. LIGHT WENT OUT 160NM FROM OAKLAND AIRPORT ETOPS FLIGHT. LIGHT ILLUMINATED AGAIN AFTER LANDING & PUTTING APU ON BUSS. ACFT GROUNDED. R & R HPSOV SWITCH IN NR 2 HMU REF AMM 73-21-09-000, 400Dec 12, 2015 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015120914174Warning Light · false activationON TAXI IN RT ENGINE VALVE CLOSED LIGHT CAME ON. ENGINE STILL RUNNING. ACFT GROUNDED. ON NR 2 ENGINE PERFORMED ENGINE RUN AND OPS CHECK IAW AMM 73-21-09, NO FAULTS NOTED.Dec 9, 2015 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015113014049Indicator · failedFUELER REPORTS FUEL GAUGES AT REFUEL PANEL INOPERATIVE, ALL GAUGES. ACFT GROUNDED. CONFIRMED FAULT, WHEN REFUELING PANEL WAS OPENED, FUEL FUELING IND C/B AT P6-3 TRIPPED. TROUBLESHOT REF W/D 28-41-11-2 TO DEFECTIVE NR 1 TANK REFUEL QUANTITY INDICATOR. R & RNov 30, 2015 · N558AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2015102713543Engine · faultedNR 2 ENGINE ECONOMIC FAULT CODE 73-31372 GENERATED ON FLT 2 ONLY OF LAST 10 FLTS. UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. ON DEFERRAL.Oct 27, 2015 · N558AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015102713540Battery Pack · failedDURING EMERGENCY LIGHTS TEST T/C 78233001, THE INTERIOR LIGHTS AT ALL 4 OVER WING EXITS FAIL TO REMAIN ILLUMINATED FOR FIFTEEN MINUTES. ACFT GROUNDED. REPLACED OVERWING EXIT BATTERY PACKS, M1695 AND M1694 AND OPS CHECKED GOOD IAW AMM 33-51-06-960-805.Oct 27, 2015 · N558AS · Boeing 737890 · Emergency LightingSDR ASAA2015102013485Battery · dischargedBOTH MAIN ACFT BATTERIES ARE DEAD. ACFT GROUNDED. R & R MAIN & AUXILIARY BATTERIES REF MM 24-31-11. INSTALLATION TEST NORMAL IAW SAME.Oct 20, 2015 · N558AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2015102013479Warning Message · false activationZONE TEMP, CONT CABIN, ON RECALL. ACFT GROUNDED. NR 2 TEMP CONTROLLER SHOWED FLIGHT DECK TCV FAULT LOGGED. RAN BITE OF CONTROLLER, REF 21-61-20. FAULT CLEARED. NO PREVIOUS HISTORY.Oct 20, 2015 · N558AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015101213479Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. COMPLIED WITH QRH PROCEDURE. OPS NORMAL.Oct 12, 2015 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015092213163Satcom · faultedNO SATCOM PROMPT. ACFT GROUNDED. RAN SATCOM LOCKUP QRH PROCEDURE, SATCOM RESTORED.Sep 22, 2015 · N558AS · Boeing 737890 · Communications SystemSDR ASAA2015072812615Control Valve · malfunctionedLEFT PACK LIGHT ILLUMINATED DURING MASTER RECALL. ACFT GROUNDED. REPLACED LT PACK TEMP CONTROL VALVE IAW MM 21-51-10, COMPLETED LEAK AND OPS CHECK.Jul 28, 2015 · N558AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015072712605Warning Message · false activationFMC DISAGREE MESSAGE ON GROUND. ACFT GROUNDED. COMPLETED FMC DISAGREE CHECKLIST 11.2. CONDITION CLEARED, OPS NORMAL.Jul 27, 2015 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015071512479Warning Light · false activationFMC DISAGREE LIGHT ILLUMINATED. ACFT GROUNDED. QRH CHECK LIST PERFORMED, NORMAL OPS RESTORED.Jul 15, 2015 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015062712223Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. QRH RESOLVED ISSUE.Jun 27, 2015 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015061012057Fuel Sys · malfunctionedINITIALLY SHOWED A NR 800 LB DIFFERENCE IN FUEL QUANTITY BETWEEN THE FUEL TOTALIZER AND THE FMC FUEL QUANTITY. THE LT, RT, AND CENTER QUANTITY ADDED UP TO EQUAL THE FUEL TOTALIZER QUANTITY OF 18.4. HOWEVER THE FMC ACTUAL FUEL SHOWED 17.6. ACFT GROUNDED. CYCJun 10, 2015 · N558AS · Boeing 737890 · Aircraft Fuel SystemSDR ASAA2015060611983Satcom · lockedSATCOM LOCK-UP WITH POWER TRANSFER. ACFT GROUNDED. QRH PROCEDURE COMPLETED SUCCESSFULLY.Jun 6, 2015 · N558AS · Boeing 737890 · Communications SystemSDR ASAA2015060411964Beam · gougedRT CENTER WING BEAM SPANWISE LOWER CHORD DAMAGED BY ECS DOOR LATCH. ACFT GROUNDED. REPLACED LOWER CHORD.Jun 4, 2015 · N558AS · Boeing 737890 · Wing Main, Frame StructureSDR ASAA2015052711880Fmc · failedWHILE LOADING NAV DATABASE SOFTWARE RT FMC WOULD NOT RESTART. ACFT GROUNDED. REPLACED RT FMC WITH SERVICEABLE ONE. ACCOMPLISH FMC CROSS LOAD. VERIFIED BOTH FMC'S MATCH SOFTWARE. ACCOMPLISH FMC OPS TEST, TEST PASS. ACCOMPLISH FMC SYS TEST, TEST PASSED ACCOMay 27, 2015 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015043011606Keyboard · damagedCAPTAINS FMC CDU L-6 BUTTON COVER MISSING. ACFT GROUNDED. REPLACED CAPTAINS CDU KEYBOARD REF AMM 34-61-01. OPS CHECKS NORMAL.Apr 30, 2015 · N558AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015032511094Pump · leakingON ENGINE CHECK, OBSERVED FUEL UNDER NR 1 ENGINE. ACFT GROUNDED. RAN NR 1 ENGINE FOR APPROXIMATLELY 10 MINUETS FOUND LEAK TO BE AT 14 DROPS A MINUTE. RUNNING AT IDLE. FOUND FUEL COMING FROM FUEL PUMP DRAIN. FOUND TO BE WITHIN LIMITS BUT WILL REQUIRE CHANGE Mar 25, 2015 · N558AS · Boeing 737890 · Engine Fuel PumpSDR ASAA2015032211070Warning Light · illuminatedRIGHT ENGINE VALVE CLOSED, LIGHT REMAINS ILLUMINATED BRIGHT. ACFT GROUNDED.Mar 22, 2015 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015030110820Door · noneF/A REPORTS L1 DOOR VERY STIFF AND HARD TO CLOSE. ACFT GROUNDED. PERFORMED FWD L1 DOOR SYS TEST IAW AMM 52-11-00-700-904, OPS CHECK GOOD CLOSE AND OPEN WITHIN LIMITS, NO HISTORY 30 DAYS.Mar 1, 2015 · N558AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2015022310755Light · illuminatedNR 2, ENGINE VALVE CLOSED, LIGHT IS ILLUMINATED BRIGHT BLUE. ALL OTHER PARAMETERS INDICATING NORMAL, LIGHT WENT OUT, EXTINGUISHED FORTY MINUTES AFTER FIRST OBSERVATION. ACFT GROUNDED, ON DEFERRAL.Feb 23, 2015 · N558AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2015020710576Warning Light · illuminatedENROUTE AT CRUISE, NR 2 ENGINE VALVE CLOSED LIGHT ILLUMINATED AND STAYED ON BRIGHT. ALL ENGINE PARAMETERS AND FUEL FLOWS WERE NORMAL. NR 1 ENG FF 2.65, NR 2 ENG FF 2.63. ENGINE PERFORM NORMALLY AND NO OTHER INDICATIONS ABNORMAL. DISPATCH AND MX CONTROL NOTIFeb 7, 2015 · N558AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2015020610574Warning Light · false activationENROUTE AT CRUISE THE NR 2 BLUE "ENG VALVE CLOSED" LIGHT ILLUMINATED AND STAYED ON BRIGHT BLUE NR 1 ENG FUEL FLOW 2.64, NR 2 ENG FUEL FLOW 2.63 ALL ENGINE PARAMETERS NORMAL NO OTHER INDICATION OF ANY ENGINE ABNORMALITY. MAINTENANCE & DISPATCH NOTIFIED VIA SATFeb 6, 2015 · N558AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015013010482Autopilot Sys · inoperativeUNABLE TO ENGAGE B AUTOPILOT. A AUTOPILOT FUNCTIONS PROPERLY. ACFT GROUNDED. OPENJan 30, 2015 · N558AS · Boeing 737890 · Autopilot SystemSDR ASAA2015012210391Satcom · malfunctionedSATCOM DROPPED OFF AFTER PWR TRANSFER, ACFT GROUNDED. RESTORED IAW QRH ON GROUND.Jan 22, 2015 · N558AS · Boeing 737890 · Communications SystemSDR ASAA2015011210238Warning Light · false activationBLUE MAINTENANCE LIGHT ILLUMINATED DURING APU START. ACFT GROUNDED. PERFORMED BITE TEST IAW FIM 49-60, TASK 801. NO FAULT FOUND, NO HISTORY 30 DAYS. STARTED APU, APU STARTED WITH NO FAULT, CONTACTED MAINTENANCE CONTROL, OK FOR SERVICE.Jan 12, 2015 · N558AS · Boeing 737890 · Central WarningSDR ASAA2015011110223Valve · failedRT ENGINE TAI VALVE DID NOT CLOSE AFTER LANDING. ACFT GROUNDED. VERFIED BOTH LIGHT ON P5-11 AND ON UPPER DU. T/S IAW FIM 30-21, TASK 801. VERIFIED OVERPRESSURE SWITCH S806 GOOD, VERIFIED WIRING FROM P5-11 TO OVER PRESSURE SWITCH GOOD. TRIED NEW P5-11, PANELJan 11, 2015 · N558AS · Boeing 737890 · Air Intake Anti/De-Ice System
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