N557AS
Service difficulty reports · 525
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 = 'N557AS' 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.
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 = 'N557AS' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2023032342583Blade · unknownWHILE PERFORMING #2 ENGINE BLADE LUBE, FOUND SEAL TORN ON BLADE PLATFORM #21. GROUNDED - YES. REPLACED #2 ENGINE BLADE PLATFORM #21 REF ASA T/C 78472010 SUB TASK 839-033.SDR ASAA2023032342582Blade · unknownWHILE PERFORMING #2 ENGINE BLADE LUBE FOUND #1 SEAL MISSING ON BLACK PLATFORM. GROUNDED - YES. REPLACED BLADE PLATFORM REF. ASA T.C 78472010 SUBTASK 839-033.SDR ASAA2023031842414Regulator · faultyPERFORMED TASK CARD NG-36WC-00001 BLEED AIR SYSTEM HEALTH CHECK. FOUND BLEED REGULATOR FAIL AT ENG#2. GROUNDED - YES. R/R ENG 2 BAR IAW B737-800 AMM 36-11-03. OPS CHK GOOD.SDR ASAA2023031342344Unknown · unknownAFTER START CONT CABIN ZONE TEMP LIGHT ON RECALL (RESETS WITH MASTER CAUTION RESET). GROUNDED - YES. PERFORMED PZTC BITE REF B737-800 FIM 21-62 TASK 801. #2 CONTROLLER FAULTED FLIGHT DECK TRIM VALVE. FOUND FLIGHT DECK TEMP SENSOR DIRTY. CLEANED SENSOR REF B737SDR ASAA2023031142357Bleed Valve · faultedCLIMB OUT OF 9000' LEFT DUCT PRESSURE WAS 38PSI. RIGHT DUCT 26PSI. FL 360 CRUISE FLT L DUCT 38 RIGHT DUCT 28PSI FL 360 N1 89%. GROUNDED - YES. ON DEFERRAL.SDR ASAA2023030842247Indicator · faultyWHILE WORKING MEL 28-12B- FOUND #1 REFUEL TANK IND. NOT GOING INTO TESTS MODE. GROUNDED - YES. RMVD AND INSTALLED NEW REFUEL #1 TANK IND. REF 28-21-00-211-801. NO DEFECTS FOUND. ACCOMPLISHED INSTALL TES PER STEP G. REF 28-41-61-400-801. ALL TESTS PASSED.SDR ASAA2023030642210Indicator · faultyCENTER FUEL TANK INDICATION DISPLAY IS SHOWING FAIL INTERMITTENTLY ON RE FUEL PANEL. GAUGE IN COCKPIT OPS NORMALLY. GROUNDED - YES. REMOVED AND INSTALLED NEW CENTER TANK REFUEL INDICATOR. PERFORMED WIRING INSPECTION REF B737-800 WDM 28-21-00-211801. NO DEFECTSSDR ASAA2023022042025Unknown · unknownSINGLE FMC MESSAGE AFTER LANDING. GROUNDED - YES. PERFORMED BITE PROCEDURE OF FLIGHT MANAGEMENT COMPUTER SYS PER B737-800 FIM 34-61 TASK 801 FOR BOTH FMC'S. ALL SENSORS READ OK . NO ACTIVE FAULTS CURRENTLY IN SYS.SDR ASAA2023021842030Cover · leakingREF ASA T/C 78472000 DURING INSPECTION FOUND #1 ENG S/N 895405 OIL LEAKAGE AND COKE AT OIL SCAVENGE TUBE TO TRF INTERFACE. GROUNDED - YES. REMOVED AND REPLACED TURBINE REAR FRAME (TRF) OIL INLET COVER REF B737-800 AMM 72-56-00.SDR ASAA2023021541950Unknown · unknownDURING WX RADAR SELF TEST DISPLAY INDICATES WXR FAIL AND TEST PATTERN PATTERN DOES NOT DISPLAY ALSO WXR RANGE DISAGREE MESSAGE. GROUNDED - YES. PER BITE PROC B737-800 FIM 34-43-00-810-801 PULLED AND RESET C/B P6-1 D13 RESET OPS NRML.SDR ASAA2023013141750Not Entered · not enteredTONE SOUND KEEPS REPEATING EVERY 7 SECONDS. GROUNDED - YES. TONE IN QUESTION IS ALT ALERTER. DFCS BITE GRP TEST 11.61 PASS - NO FAULTS. DFCS MCP INSTALL TEST GOOD REF B737-800 AMM 22-11-34. W/ MCP ALT SELECTED ABOVE FIELD ELEV, TONE STOPPED. ETOPS GND VERIFICASDR ASAA2023012841715Unknown · unknownUPON SELECTING LNAV, FMA SHOWS NO LNAV OR A FLASHING LNAV INDICATION. WILL NOT INDIDCATE SOLID ARMED LNAV. GROUNDED - YES. ACCOMPLISHED FMC BITE PER B737-800 FIM 34-61-801 TASK. NO FAULTS FOUND. ACCOMPLISHED DFCS BITE CHK PER TASK FIM 22-11-801. NO FAULTS FOUNSDR ASAA2023012741719Unknown · unknownAFTER CONSULTATION WITH THE FLIGHT OPS DUTY OFFICER AND DETERMINING LNAV/VNAV SHOULD ENGAGE ON THE GROUND, LNAV/VNAV WILL NOT ENGAGE. LNAV/VNAV LIGHTS WERE VERIFIED OPERATIONAL. GROUNDED - YES. ACCOMPLISHED FMC BITE PER B737-800 AMM 34-61-801 TASK. NO FAULTS FSDR ASAA2022120240997Modulating Valve · faultedON RECAL ZONE TEMP CONT CAB ILLUMINATED EXTINGUISHES ON RESET. GROUNDED - YES. REPLACED CONTROL CABIN TRIM AIR VALVE OPS CHECK / BITE CHECK GOOD IN REF TO B737-800 AMM 21-61-21.SDR ASAA2022111840858Fmc · failedFMC DISAGREE. GROUNDED - YES. PERFORMED FMC DISAGREE QRH CHECKLIST FOR MAP DISPLAY.SDR ASAA2022110840697Drive Assy · malfunctionedDURING CLIMB OUT, "PWS" FLAG ILLUMINATED ON ND'S THEN CLEARED AFTER APPROXIMATELY 3 MINS. GROUNDED - YES. INITIAL EVALUATION, NO MSG ON ND AT POWER UP AFTER ALIGN AND WXR SELECTED. PERFORMED WXR BITE IAW B737-800 FIM 34-43 TASK 801, NO FAULTS FOUND. PERFORMED SDR ASAA2022110840692Autothrottle Sys · malfunctionedDURING T/O IN V-NAV, CLIMB THRUST WAS NOT COMMAND AT 800' AGL. CLIMB THRUST WAS MANUALLY SELECTED BY PUSHING "N1" - THEN F/DS HAD TO BE CYCLED TO BE ABLE TO SELECT MODES NORMALLY. GROUNDED - YES. PERFORMED DFCS FAULT REVIEW IAW B737-800 AMM 22-11-00-740-801, NSDR ASAA2022103140551Warning Message · false activationDURING CLIMBOUT APPROXIMATELY 10,000 MSL TO 25000 MSL, PWS FAIL ANNUNCIATOR APPEARED ON MFD. GROUNDED - YES. PERF B737-800 FIM 34-43 TASK 801, FOUND NO SYS FAULTS, TEST PASSED.SDR ASAA2022102240456Modulating Valve · fault messageCONT CAB ZONE TEMP ANNUN ILLUM WHEN 6-PACK PUSHED. MASTER CAUTION RESETS THE LIGHT OUT. TEMP CONTROLS NORMALLY WHEN KNOB ROTATED HOT OR COLD. GROUNDED - YES. INITIAL EVALUATION, CONT CAB ZONE TEMP ON MASTER RECALL AT OVERHEAD. PERFORMED PZTC IAW B737-800 FIM 2SDR ASAA2022092640065Sign · detachedCEILING EXIT SIGN BETWEEN EXIT ROWS OVERWING DETACHED. GROUNDED - YES. REINSTALLED MID CABIN OVERHEAD AISLE EXIT SIGN LENS REF B737-800 AMM 33-51-01.SDR ASAA2022091939999Overheat Sensor · warning lightAPU DET INOP LIGHT ILLUMINATED IN FLIGHT. GROUNDED - YES. REMOVED AND REPLACED APU OVERHEAT DETECTOR ASSEMBLY (TAILCONE) REF B737-800 AMM 26-15-01.SDR ASAA2022090939917Overheat · warning lightLEFT FWD WINDOW OVERHEAT LIGHT ILLUMINATED. GROUNDED - YES. FOUND LEFT FRONT WINDSHIELD SENSOR SWITCH IN SPARE POSITION PERFORMED WINDOW TEMP SENSOR RESISTANCE CHECK IAW B737-800 AMM 30-41-21-760-801 PRIMARY SENSOR CHECK GOOD , SPARE SENSOR CHECKED OPEN PLACEDSDR ASAA2022090639894Skin · corrodedREF DEFECT 60413749 CORROSION FOUND ON SKIN AT LAV VENT HOLE. GROUNDED - YES. DAMAGE FOUND TO BE 100% THRU, CUT OUT DAMAGE & REPAIRED SKIN IAW B737-800 SRM 53-70-01-2R-3 THIS IS A CAT B REPAIR WITH AN INSP THRESHOLD OF 67, 260 CYCLES TOTAL & 5,000 CYCLE INTERVSDR ASAA2022090339785Unknown · unknownLEFT FWD WINDOW OVERHEAT LIGHT ILLUMINATED ON DESCENT. X LIST COMPLIED LIGHT STAYED ILLUMINATED. GROUNDED - YES. PERFORMED WHCU BITE PROCEDURE L1 WINDOW IAW B737-800 FIM 30-41 TASK 801, BITE CHECK OK FAULT LIGHT OFF.SDR ASAA2022080139292Datalink · failedATC LOGON W/CPDLC SHOWS FAIL WHEN LOGGING ON. GROUNDED - YES. VERIFIED, NO FAULTS ON FMC BITE, ACARS TEST NORMAL. CYCLED FMC CMPTR 1 & 2, CMU-1 AC & DC, VHF-3 C/B, FAIL MSG CLEARED FROM CPDLC LOGON PAGE. ACCOMPLISHED CPDLC FUNCTIONAL TEST REF B737-800 AMM 34-6SDR ASAA2022072539197Dfgs · burned outMAIN PANEL LIGHTS (FO SIDE MCP) BURNED OUT. GROUNDED - YES. REMOVED AND REPLACED MCP IAW B737-800 AMM 22-11-34-000/400-801.SDR ASAA2022071239052Sign · missingEXIT ROW CEILING AFT "EXIT SALIDA" SIGN FACIA MISSING. GROUNDED - YES. REINSTALLED EXIT SIGN ON EMERGENCY EXIT ROW 16 A,B,C - D,E,F. LENS SECURED. REF B737-800 AMM 33-51-01. OK FOR SERVICE.SDR ASAA2022052038390Harness · faultyGE DIAGNOSTICS REPORTS THE #2 ENGINE EXPERIENCED AN EGT EXCEEDANCE DURING TAKEOFF THAT MAY HAVE EXCEEDED THE TRANSIENT AREA LIMITS. PEAK EGT RECORDED ON REPORT 06 WAS 982 DEGREES DURING TAKEOFF (FLIGHT PHASE 4.) PRI: AOG.ETOPS SIGNIFICANT SYSTEM. GROUNDED - YESDR ASAA2022040437894Unknown · unknownPROBE HEAT A SWITCH IN AUTO THE L ALPHA VANE ANNUNCIATOR DOES NOT ILLUMINATE. GROUNDED - YES. L AOA VANE HEATS GOOD. ANNUCIATOR NOT ILLUM. SUSPECT CONTROL PANEL. REMOVED AND REPLACED WINDOW/PITOT HEAT MODULE REF B737-800 REF AMM 30-41-41. OPS CHECK GOOD.SDR ASAA2022040237877Unknown · unknownFAIL FLAGS ON HF1. GROUNDED - YES. IAW B737-800 FIM 23-11 TASK 801, HF COM SYS BITE PROCEDURE C/OUT, BITE TEST PASSED. HF 1 SYS FAIL MSG UNLATCHED. NO FAIL MSG ON HF 1. HF TEST GND VERIFICATION PASSED.SDR ASAA2022022037507Unknown · unknownUPON REACHING CRZ ALT, R-FMC FAILED (VTK, NO MAP INFO). COMPLIED WITH FMC FAIL QRH. DUAL FMC OPS RESTORED. OPS NORMAL. GROUNDED - YES. PERFORMED B737-800 FIM 34-61 TASK 836. CYCLED FMC'S C/B'S . NO DEFECTS NOTED.SDR ASAA2022021937500Unknown · unknownWITH HF-1 SELECTED "FAIL" LIGHT INDICATED ON BOTH COMM PANELS. GROUNDED - YES. ACCOMP B737-800 FIM 23-11 TASK 803 FOR HF TRANSCEIVER FAIL PROBLEM. PULLED & RESET HF-1 C/B, "FAIL" INDICATIONS EXTINGUISHED IN BOTH RTP FREQ WINDOWS AND HF TUNING FREQS APPEARED WISDR ASAA2022021237412Unknown · unknownEMERGENCY EXIT SIGN FROM CABIN CIELING FELL OFF IN FLIGHT. GROUNDED - YES. EMERGENCY EXIT SIGN COVER REINSTALLED REF B737-800 AMM 33-51-00.SDR ASAA2022011037115Control Panel · faultyF/O RADAR IN AUTO/WX+T MODE SHOWING GROUND CLUTTER CA SIDE NORMAL,CA DISPLAY MATCHES F/O DISPLAY WHEN GC BUTTON HELD. GROUNDED - YES. REPLACED WX RADAR CONTROL PANEL. OPS NORMAL REF B737-800 AMM 34-43-91.SDR ASAA2022010737088Modulating Valve · faultyCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL AFTER START. LIGHT OUT ON MASTER CAUTION RESET. GROUNDED - YES. CONFIRMED FAULT, #2 PACK/ZONE TEMP CONTROLLER BITE TEST SHOWS HARD FAIL "FLIGHT DECK" TCV (V143). REMOVED & REPLACED SAME PER B737-800 AMM 21-61SDR ASAA2021102936456Guard · looseEMER EXIT LIGHT SWITCH COVER LOOSE. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY EXIT LIGHT SWITCH GUARD IAW ASA B737-800 SOPM 20-11-05.SDR ASAA2021102936455Lamp · inoperativeEMERGENCY EXIT LIGHT MISSING BULB FORWARD LEFT OVERWING EXIT. GROUNDED - YES. RELAMPED EMERGENCY EXIT LIGHT AT FORWARD LEFT OVERWING EXIT AND OPS CHECK GOOD IAW ASA B737-800 AMM 33-51-01.SDR ASAA2021100236239Angle · corrodedAFTER REMOVING THE RIGHT AFT PIT DOOR SURROUND SHIELD, THE ATTACH ANGLE IS FOUND TO BE CORRODED. GROUNDED - YES. REMOVED AND REPLACED AFT PIT DOOR SURROUND SHIELD ATTACH ANGLE PER B737-800 SRM 51-40-05, 51-40-02, AND BOEING DWG 146A8123 REV:- NO ALLOWABLE LIMISDR ASAA2021100136366Track · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT, RH TIE-DOWN FITTING HAS CORROSION AT BS727F.DOT:V664. GROUNDED - YES. REMOVED CORROSION FROM AFT CARGO FLOOR SUPPORT TIE DOWN AT BS727F PER B737-800 SRM 53-00-53-1A-2; REMOVED 0.050 MAX DEPTH ALLOWED 0.040;FOUND TO BE OUTSDR ASAA2021100136273Floorbeam · corrodedRH MAIN CABIN FLOOR SUPPORT BEAM UPPER CHORD HAS CORROSION, BS320, RBL-56 DOT:V657. GROUNDED - YES. BLENDED OUT CORROSION, ORIGINAL THICKNESS 0.125 IAW B737-800 SRM 53-10-51.REMOVED 0.037,REMAINING THICKNESS 0.088.AREA OUT OF LIMITS.REPAIRED AREA IAW B737-800 SDR ASAA2021100136243Shield · corrodedFWD PIT RH TRANSITION PANEL HAS CORROSION ON UPPER SURFACE AT STA 427, RBL 24 (MARKED). DOT:P466. GROUNDED - YES. REMOVED CORROSION FROM R/H SHIELD AT STA 427 PER B737-800 SRM 53-30-15-1A-1. ORIG THICKNESS .032. REMOVED .019 REMAINING .013. FOUND TO BE OUT OF SDR ASAA2021100136241Transition Panel · corrodedFWD PIT RH TRANSITION PANEL HAS CORROSION ON UPPER SURFACE ST STA 419, RBL 24(MARKED). DOT:P465. GROUNDED - YES. REMOVED CORROSION FROM R/H TRANSITION PANEL ON STA 419 IAW B737-800 SRM 53-00-53-1A-2. ORIGINAL THICKNESS IS 0.040 REMOVED 0.018 REMAINING THICKNESSDR ASAA2021093036396Track · gougedAFT CARGO COMPARTMENT LH TIE DOWN FITTING IS WORN AND GOUGED APPROXIMATELY AT STA 787.DOT: C533. GROUNDED - YES. EVALUATED AFT CARGO COMPARTMENT LH TIE DOWN FITTING AT STA 737; REMAINING TIE DOWN LIP IS 0.207 AND IS FOUND TO BE OUT OF LIMITS PER B737-800 SRM SDR ASAA2021093036395Track · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT IS CORRODED BETWEEN STA787 TO 827 AT RBL14.DOT:C530. GROUNDED - YES. REMOVED CORROSION FROM TRACK ORIG MATERIAL 0.070: REMOVED 0.010; 0.060 REMAINING AND FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-00-53-1A-2; REPAIRED TSDR ASAA2021093036394Track · gougedAFT CARGO COMPARTMENT RH TIE DOWN FITTING IS WORN AND GOUGED APPROXIMATELY AT STA 727H.DOT: C538. GROUNDED - YES. EVALUATED AFT CARGO RH TIE DOWN FITTING AT STA 727H, REMAING MATERIAL 0.201 AND FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-00-53-1A-2-4-B-(2)SDR ASAA2021093036355Skin · crackedFOUND CRACK ON THE L/H H-STAB LOWER SKIN BETWEEN STA STA. 138.70 AND 147.90 APROX. 1" LONG.MARKED ENDS OF CRACK AND CRACK LOCATION IN BLACK. GROUNDED - YES. ACCOMPLISHED DOUBLER REPAIR AS REQUIRED IAW B737-800 SRM 55-10-01-2R-11.REPAIR IS A CATEGORY "B" REPAIRSDR ASAA2021093036354Skin · noneFOUND CRACK ON THE L/H H-STAB LOWER SKIN BETWEEN STA STA.92.7 AND 101.90 APROX. 1" LONG. MARKED ENDS OF CRACK AND CRACK LOCATION IN BACK. GROUNDED - YES. ACCOMPLISHED DOUBLER REPAIR AS REQUIRED IAW B737-800 SRM 55-10-01-2R-11. REPAIR IS A CATEGORY B REPAIR WITSDR ASAA2021093036339Transition Panel · corrodedAFT CARGO COMPARTMENT RH TRANSITION PANEL IS CORRODED AT APPROXIMATELY STA 727D+10 TO 727. DOT: C540. GROUNDED - YES. REMOVED DAMAGE R/H TRANSITION PANEL STA 727D+10 TO 727. ORIGINAL MAT: .040 REMOVED: .019 REMAINING: .021,FOUND TO BE OUT OF LIMITS PER B737-8SDR ASAA2021093036338Transition Panel · corrodedAFT CARGO COMPARTMENT RH TRANSITION PANEL IS CORRODED AT APPROXIMATELY STA 727G+10 TO 727D+1 DOT:C539. GROUNDED - YES. REMOVED DAMAGE R/H TRANSITION PANEL STA 727G+10 TO 727D+10, 100% MAT LOSS & IS FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-00-53-1A-2-4-A-(SDR ASAA2021093036337Transition Panel · corrodedAFT CARGO COMPARTMENT RH TRANSITION PANEL IS CORRODED AT APPROXIMATELY STA 727I+10 TO 727G+10. DOT:C537. GROUNDED - YES. REMOVED DAMAGE R/H TRANSITION PANEL STA 727I+10 TO 727G+10, 100% MAT LOSS IS IS FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-00-53-1A.2.4
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