N584AS
Service difficulty reports · 569
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 = 'N584AS' 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 = 'N584AS' 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 ASAA2019042904151Floorbeam · corrodedPASSENGER COMPARTMENT FLOOR WET AREA AT STA 947.5 HAS CORROSION. GROUNDED - YES. REPAIRED 947.5 FLOOR BEAM IAW B737-800 SRM 53-70-51-2R-5 AND ALASKA AIRLINES EA 800-53EA-21558.SDR ASAA2019042904150Floorbeam · corrodedPASSENGER COMPARTMENT FLOOR BEAM STA 294 HAS EVIDENCE OF CORROSION. GROUNDED - YES. REPAIRED FLOOR BEAM AT STA 294 IAW ALASKA E.A 800-53EA-21495W:1" O:.094" R:.065" L:1" D: .029".SDR ASAA2019042549134Floorbeam · corroded986 FLOOR BEAM AT LEFT GIRT BAR ATTACH HOLE HAS AREA OF CORR. GROUNDED - YES. REPAIRED 986 FLOOR BEAM L/H SIDE IAW B737 800 SRM 53 70 51 2R 4 REPAIR 4 W 1.5 O .150 R .057 L 2 D .093.SDR ASAA2019042242958Floor Support · crackedPAX COMPARTMENT FLOOR STA 312-STA 328 RBL 31 INTERCOTAL CRACKED ON UPPER SURFACE. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT PAX COMPARTMENT FLOOR STA 312 STA 328 RBL 31 IAW B737 800 SRM 51 40 02 0G 0.SDR ASAA2019041749011Floorbeam · corrodedPAX COMPARTMENT FLOOR WET AREA AT STA 312 HAS EVIDENCE OF CORR. GROUNDED - YES. REPAIRED FLOOR BEAM IAW 737 800 SRM 53 10 51 2R 15 W 1" O .125" R .099" L 2" D .026".SDR ASAA2019041749008Floor Support · crackedINTERCOSTAL CRACKED STA 312-328 LBL46. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT STA 312-328 LBL46 IAW B737 800 SRM 51 40 02 0G 0 PG 6 STEP D 1-6.SDR ASAA2019041749006Floor Support · crackedPAX COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 280 AND STA 400 AT BUTT LINE 14L HAS CRACKS IN 2 LOCATIONS ON UPPER SURFACE. GROUNDED - YES. REMOVED AND REPLACED PAX COMPARTMENT FLOOR STRUCTURE INTERCOSTAL UPPER CHORD BETWEEN STA 380 AND STA 400 AT BUTSDR ASAA201904179003Floor Support · crackedPAX COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 380 AND STA 400 AT BUTT LINE 10R HAS CRTACKS AT 3 LOCATIONS ON UPPER SURFACE. GROUNDED - YES. REMOVED AND REPLACED 1EA. PAX COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BTWN STA 380 AND 400 RBL 10 IAW B737 800SDR ASAA201904179002Floor Support · crackedPAX COMPARTMENT FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 380 AND STA 400 AT BUTT LINE 0 HAS CRACKS AT 4 LOCATIONS ON UPPER SURFACE. GROUNDED - YES. REMOVED AND REPLACED 1EA. PAX COMPARTMENT FLOOR STRUCTURES INTERCOSTAL BTWN STA 380 AND 400, BL0 IAW B737 800 SRMSDR ASAA2019042239060Channel · corrodedR/H R-2 MOP SEAL HAS CORR IN AREAS AROUND NUT PLATES AND AT LWR DOOR CUTOUTS. GROUNDED - YES. REMOVED AND REPLACED 1EA. R/H MOPSILL AND NUTPLATES IAW B737 800 SRM 51 40 02 0G 0 PG 2 STEP 4.B AND PG 6 STEP D W 1" O .080" R .052" L 1" D .028".SDR ASAA2019041739009Floor Support · crackedAREA AFT OF AFT CARGO COMPARTMENT L/H SIDE FLOOR SUPPORT BRACKET AT STA 867 BEHIND BULKHEAD PANEL 141PW IS CRACKED. GROUNDED - YES. REMOVED,LOCATED AND DRILLED INSTALLED IAW B737 800 SRM 51 40 02.SDR ASAA2019041739005Floorbeam · crackedPAX COMPARTMENT STA 540 BL 0 BL 24.82L PANEL BREAK CRACKED. GROUNDED - YES. REMOVED AND REPLACED 1EA PANEL BREAK AT STA 540 BL 0 BL 24.82 IAW B737 800 SRM 51 40 02 0G 0 PG 6 STEP D 1-6.SDR ASAA2019041138958Angle · crackedFWD CARGO COMPARTMENT (AFT SIDE) LEFT SIDE, BAFFLE CLIP FWD OF STA 500H IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW B737 800 SRM 51 40 02 0G 0 STEP 7 D L.SDR ASAA2019041729007Angle · crackedFWD CARGO COMPARTMENT (AFT SIDE) LEFT SIDE, BAFFLE CLIP FWD OF STA 500G IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW B737 800 SRM 51 40 02 0G 0 AND B737 800 SRM 51 40 05 0G 0.SDR ASAA2019042219063Transition Panel · corrodedAFT CARGO LEFT FLOOR TO SIDEWALL TRANSITION PANEL HAS 3EA. CORRODED NUTPLATE HOLES FROM STATION 727F TO 727I ON UPPER AND LOWER SURFACE. GROUNDED - YES. REPAIRED TRANSITION PANEL IAW B737 800 SRM 53 00 53 2R 5 REPAIR 5 W .5 O .040 R .030 L 1.5 D .010.SDR ASAA2019042219062Angle · corrodedAFT CARGO RH TRANSITION STRIP 727I-727H CORRODED AROUND NUTPLATES LOWER SURFACE. GROUNDED - YES. REPAIRED R/H TRANSITION STA 727H TO 767 IAW B737 800 SRM 53 00 53 2R G 6 REPAIR 6 W 1.1 O .040 R .039 L 1.5 D .010.SDR ASAA2019042212959Attach Angle · corrodedAFT CARGO RH TRANSITION STRIP ATTACH ANGLE CORRODED AT STA 767 TO STA 787 STR 25. GROUNDED - YES. REMOVED AND REPLACED SHIELD AND ANGLE IAW B737 800 SRM 51 40 02 0G 0 FIG 8 AND PARA 5 AND PARA 7 W .5 O .050 R .035 L 1.1 D .015.SDR ASAA2019041729010Shield · corrodedAFT CARGO RH TRANSITION STRIP STA 727I TO 807 CORRODED ON UPPER SURFACE AND LOWER SURFACE AROUND NUTPLATES. GROUNDED - YES. REMOVED CORR AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737 800 SRM 53 60 15 01 1 FIG 5 ORDERED NEW SHIELD 9TRANSITION STRIP), LOSDR ASAA2019032228752Bushing · migratedWHILE ACCOMPLISHING T/C 78472000 NR 2 ENGINE FOUND LWR SUPPORT LINK BUSHING MIGRATED ON INTERSECTION MANIFOLD DUCT. GROUNDED - YES. REPLACED SUPPORT LINK AS NEEDED REF AMM 36-11-01.SDR ASAA2019031428651Heat Exchanger · leakingDURING IDLE PWR RUN, FOUND NR 2 ENG MAIN OIL/FUEL HEAT EXCHANGER PAD DRAIN LEAKING AT A RATE OF 8 DROPS PER MIN. (LEAKING FUEL). GROUNDED - YES. REMOVED & REPLACED OIL/FUEL HEAT EXCHANGER REF AMM 73-11-04. LEAK CHECKED GOOD.SDR ASAA2019031428614Actuator · leakingDURING IDLE PWR RUN, FOUND NR 2 ENG. MAIN OIL / FUEL HEAT EXCHANGER PAD DRAIN LEAKING AT A RATE OF 8 DROPS PER MIN. (LEAKING FUEL). GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG RT VSV ACTUATOR REF AMM 75-31-01-000-802-F00 AND 75-31-01-400-802-F00. LEAK CHECK SDR ASAA2019030928558Lens · detachedEXIT SIGN LENS AT MID CABIN OVER AISLE FELL OFF. GROUNDED - YES. RE-INSTALLED EXIT SIGN AT MID CABIN, NO FURTHER DEFECTS NOTED.SDR ASAA2019022828389Modulating Valve · failedAFTER ENGINES STARTED WITH PACKS ON RESPECTIVE ENGINES CABIN CONTROL ZONE LIGHT ILLUMINATED. CHECKLIST WOULD NOT SOLVE PROBLEM. GROUNDED - YES. PERFORMED PACK/ZONE TEMP CONTROLLER BITE REF AMM 21-61-21, FAULT LIGHT FOR PRIMARY FLT DECK TRIM AIR VALVE ILLUMINATSDR ASAA201902258321Warning Light · false activationTOP OF DESCENT PRIOR TO DCA RIGHT SIDE DATA DISAPPEARED FROM RIGHT EADI. MAP YELLOW WARNING ILLUMINATED. FMC R REMAINED ILLUMINATED GREEN. GROUNDED - YES. ACCOMP B737-800 FIM 34-61 TASK 836 RESET FMC CB'S AND OPS CK NORMAL.SDR ASAA2019021628207Sign · unsecureEMERGENCY EXIT SIGN FELL FROM CEILING OVER AISLE AT OVERWING EXIT ROW. GROUNDED - YES. REINSTALLED LENS OK FOR SERVICE.SDR ASAA2019012428380Probe · failedREF T/C 78273000- NR 2 ENG MAINT MSG 73-31372 "UPPER EGT SECTORS READING HIGH ECONOMIC FAULT- ETOPS A/C. GROUNDED - YES. REPLACED T49.5 PROBE S4 DUE TO A COLD TEMP OF 221.84 DEG. VS S1- 39.34. REF AMM 77-21-01-400-801-F00. ACCOMPLISHED EEC TEST REF. AMM 71-00-SDR ASAA2019011227751Unknown · malfunctionedNR 1 HF RADIO UNABLE TO TRANSMIT OR RECEIVE. GROUNDED - YES. PERFORMED FIM 23-11 TASK 806 FOR HF NR 1 RADIO NO DEFECTS NOTED.SDR ASAA2019010327657Circuit Breaker · openNR 1 ENGINE DID NOT START (NO LITE OFF). GROUNDED - YES. FOUND NR 1 ENGINE L & R IGNITION C/B'S OPEN, PERFORMED C/B RESET OF NR 1 ENGINE L & R C/B'S PER AMM 20-60-01. PERFORMED NR 1 ENGINE NORMAL START PROCEDURES FOR L & R IGNITION PER AMM 71-00-00, OPS CHECK SDR ASAA2018112527106Warning System · false activationHF 1 FAIL ANNUNCIATED. GROUNDED - YES. RESET PWR TO HF 1 BY PULLING, THEN RESETTING HF 1 C/B. "FAIL" EXTINGUISHED IN RTP'S REPLACED BY SET FREQUENCIES AS NORMAL. HF 1 OPS NORMAL PER AMM 23-11-00. GND VERIFICATION SUCCESSFUL.SDR ASAA2018111386804Switch · inoperativeAUTOPILOT A WOULD NOT ENGAGE. AUTOPILOT B OPERATED NORMALLY. GROUNDED - YES. PERFORMED DFCS BITE PER B737-800 FIM 22-11 TASK 801. FAULT 22-11281 A/P DISC S/W-1 IS STILL ACTIVE. REMOVED CAPTS AUTOPILOT DISCONNECT SWITCH PER B737-800 AMM 22-11-41-000-801. INSTALSDR ASAA2018110426725Warning System · false activationON CLIMB OUT THE CONT CAB LIGHT ILLUMINATED. CK LIST WAS ACCOMP. WITH THE CONT CAB LIGHT REMAINING ON. TRIED PRESSING THE CAPT RECALL AND MC AND CONT CAB LIGHT REMAINED ON. LATER IN THE FLIGHT THE FO RECALL WAS PRESSED AND THE AIR COND LIGHT STAYED ON. PRESSEDSDR ASAA2018091026061Anti-Ice Valve · failedIN CRUISE NR 2 N1 "TAI" INDICATION AMBER ON, OVERHEAD BLUE LIGHT OUT WITH SWITCH OFF N1 NR 1 AND NR 2 ARE MATCHED. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE COWL TAI VALVE REF AMM 30-21-11/401, OPS CHECK AND LEAK CHECK GOOD. NO OTHER DEFECTS NOTED.SDR ASAA201808205847Wire Harness · looseNR 1 ENGINE, STATOR GENERATOR WIRE BUNDLE DP0702 WAS LOOSE. ACFT GROUNDED. REMOVED AND REPLACED THE J7 HARNESS IAW AMM 73-21-06/401. EEC TEST AND ACTUATORS TEST PASSED. ETOPS GROUND VERIFICATION SUCCESSFUL.SDR ASAA2018081725835Control Valve · failedDURING DESCENT, THE COCKPIT TEMPERATURE BECAME UNCOMFORTABLY WARM AND WE WERE UNABLE TO CONTROL IT WITH THE CONT CABIN TEMP SELECTOR. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 TCV IAW AMM 21-51-10.SDR ASAA201808202812Control Valve · failedLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL, CLEARED DURING MASTER CAUTION RESET. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 TCV IAW AMM 21-51-10. OPS CHECKED GOOD. FAULT CLEARED.SDR ASAA2018081395728Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON PRESSING THE MASTER CAUTION RECALL SIX PACK. LIGHT EXTINGUISHED WHEN MASTER CAUTION RESET. ACFT GROUNDED. COMPLETED A PACK ZONE TEMP CONTROLER BITE CHECK IAW AMM 21-61-00, OPS CHECKED GOOD, NO FAULTS GENERATED.SDR ASAA2018072425524Probe · out of toleranceDURING ACCOMPLISHMENT OF NR 1 MAIN TANK FQIS TEST REF NG-28FCD-18088-1, FOUND PROBES F3, F5, AND F6 OUT OF TOLERANCE REF AMM TASK 28-41-21-710-801. GROUNDED - YES. REMOVED AND REPLACED PROBES F3, F5, AND F6 OF THE NR 1 MAIN TANK. FQIS SYSTEM TEST PASS. ETOPS GSDR ASAA2018072425515Unknown · malfunctionedON LANDING ROLLOUT BOTH ND'S DISPLAYED VTK AND BOTH MCDUS REVERTED TO THE MENU PG BOTH MISSING FMC PROMPTS, DURING TAXI IN VTK MESSAGES CLEARED, AND FMC PROMPTS RETURNED TO BOTH MCDU'S. GROUNDED - YES. ACCOMPLISHED FMC BITE PROCEDURES ON BOTH FMC'S, IAW FIM 34SDR ASAA2018071625396Unknown · malfunctionedAUTOLAND UNSUCCESSFUL, PLANE SLOWED 5 KNOTS TO REF AND SEEMED NOT TO TRIM AT APPROXIMATELY 75 FEET. GROUNDED - YES. PERFORMED FIM 22-11 TASK 801. NO FAULTS LOGGED EITHER DFCS LAST FLIGHT. PERFORMED LAND VERIFY BITE 49 -GOOD. NO HISTORY LAST 90 DAYS PLUS.SDR ASAA2018070525301Cover · missingL2 DOOR EXIT SIGN COVER MISSING. GROUNDED - YES. REMOVED AND REPLACED L2 DOOR EXIT SIGN LIGHT ASSEMBLY REFERENCE AMM 33-51-01.SDR ASAA2018070325270Unknown · malfunctionedON PRE FLIGHT FO NAV DISPLAY REPEATEDLY SHOWS "VTK" INTERMITTENTLY. GROUNDED - YES. RECYCLED POWER. REALIGNED ADIRU'S AND PERFORMED GROUND OPS CHECK PER AMM 34-61-00, NO FAULTS INDICATED. NO HISTORY IN LAST 30 DAYS.SDR ASAA2018061185001Display · defectiveNR 1 FMC SCREEN HAD SEVERAL WHITE LINES RUNNING HORIZONTALLY ON THE TOP OF THE SCREEN. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 MCDU, OPS NORMAL IAW AMM 34-61-01-400-802.SDR ASAA2018052524774Start Valve · failedNR 2 ENGINE STARTER VALVE INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE ENGINE START VALVE ASSY IAW AMM 80-11-03, OPS GOOD.SDR ASAA2018051184683Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON THE NR 2 ENGINE IAW T/C 78472002, FOUND ALL SHIMS WORN INTO PARENT MATERIAL. ACFT GROUNDED. REPLACED THE SHIMS.SDR ASAA201805184682Spinner · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON THE NR 2 ENGINE IAW T/C 78472002, FOUND THE SPINNER DAMAGED ON THREADS FOR TACK BOLT, AND MISSING PAINT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENG SPINNER CONE IAW AMM 72-21-01-000-801-F00 STEP 2F(1), AND 72-21-0SDR ASAA2018042024336Fmc · malfunctionedAFTER LANDING, TEMPORARY VTK FLAG ON CAPTAIN'S NAV DISPLAY. ACFT GROUNDED. RESET SYSTEM, GROUND FUNCTIONAL CHECKED GOOD IAW AMM 34-61-00-710-801, NO HISTORY LAST 30 DAYS.SDR ASAA2018040424143Satcom · lockedSATCOM LOCK UP. GROUNDED - YES. PERFORMED QRH PROCEDURE SAT RETURNED.SDR ASAA2018032524032Fmc · malfunctionedON ARRIVAL, WHEN BRINGING FLT INTO SCRATCH PAD RECEIVED MESSAGE ON CDU INVALID ENTRY. ACFT GROUNDED. BITE TESTED THE LT AND RT FMC IAW FIM 34-61-00-810-801. NO FAULTS. NO IN FLT FAULTS. SENSORS TESTED OK. CDU KEY TEST OK. CDS FMC INTERFACE OK BOTH FMCS.SDR ASAA2018031823926Control Valve · malfunctionedZONE TEMP LIGHT ILLUMINATED ON MASTER RECALL. ACFT GROUNDED. REPLACED FLT DECK TRIM VALVE V143 IAW AMM 21-61-21. OPERATED BOTH LEFT AND RIGHT PACKS FOR APROXIMATELY 10 MINUTES. OPS CHECKED GOOD. PERFORMED PZTC BITE ON BOTH NR 1 AND 2 CONTROLLERS IAW FIM 21SDR ASAA2018031823925Warning Light · false activationAUTO FAIL AND ALT LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED FIM 21-31 / 827, AUTO FAIL LIGHT ON, CYCLED TO MANUAL THEN TO AUTO, LIGHT EXTINGUISHED, RESET FAULTS WITH NO FURTHER FAULTS LOGGED.
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