N588AS
Service difficulty reports · 577
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 = 'N588AS' 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 = 'N588AS' 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 ASAA2022051538339Indicator · failedTANK #1 REFUEL INDICATOR LOWER SEGMENTS SHOW TEST MODE. GROUNDED - YES. VERIFIED FAULT, CYCLED REFUEL IND TEST SWITCH TO TEST & IND WENT TO NML INDICATION. ACCOMP TEST AGAIN ALL REFUEL IND TEST PASS REF B737-800 AMM 28-41-61-710-001.SDR ASAA2022040838047None · degradedON T/O IN SAN WITH 27K BUMP T/O, EGT ENG #1 EXCEEDED MAX LIMIT FOR 4-5 SECONDS WITH PROPER T/O SETTING. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE T49.5 S4 PROBE PER B737-800 AMM 77-21-01. PERFORMED EEC TEST PER AMM 73-21-00-700-804-F00,(AS REQUESTED PER PSDR ASAA2022032537882Unknown · inoperative#1 ENGINE EGT TREND DATA SHOWS RECENT INCREASE IN DELTA EGT/DECREASE IN EGTHDM. (#PRI2/ETOPS) TASK CARD 78273000CNR 20220325005. GROUNDED - YES. ALL LAST 10 FLTS AND FLT 0 SHOWS FAULT 77-20861 THE BOTTOM LEFT EGT SIGNAL (T495S3) OUT OF RANGE. AFTER CLEANING OFSDR ASAA2022011637161Anti-Ice Valve · stuckACCOMPLISHING AFTER TAKE OFF CHECK LIST, NOTICE LEFT WING VALVE BRIGHT BLUE LIGHT ILLUMINATED RAN QRH. CONTINUED TO DESTINATION SNIGLE PACK OPERATION CABIN PRESSURE 7.7 PSI, CABIN ALT 7800 FEET, RT PACK 42 PSI. ACFT ALT 370 WING ANTI-ICE SWITCH OFF POSITION. SDR ASAA2021120936884Start Valve · faultyWITH #1 START SWITCH IN GROUND POSITION NO N2 ROTATION NOTED. GROUNDED - YES. CYCLED #1 START CONTROL VALVE. PERFORMED NORMAL START - OPS GOOD. REF B737-800 AMM 71-00-00. REMOVED AND REPLACED #1 ENGINE START VALVE PER AMM 80-11-03. OPS CHECK NORMAL. PERFORMED SDR ASAA2021111836636Acm · inoperativeREF LOG 60152528 LEFT PACK TRIP. GROUNDED - YES. REF B737-800 FIM TASK 21-53 TASK 820 STEP 820 F 4 REMOVED L/H ACM REF 21-51-04-000-802-002 M C. 50340 11/17/2021 INSTALLED L/H ACM PER AMM REF 12-51-04-400-802-002 THROUGH PG. 7 STEP (I). ALSO INSTALLED HIGH PRESDR ASAA2021111636625Switch · inoperativeLEFT PACK LIGHT ILLUMINATED ON CLIMB OUT THROUGH 18500. UNABLE TO RESET THE SECOND TIME. GROUNDED - YES. PERFORMED BITE CHECK OF L/H PACK ZONE TEMP CONTROLLER AND PERFORMED OPS CHK OF L/H PACK W/ NO FAULTS NOTED. REPLACED DISCHARGE O/H SWITCH PER B737-800 AMM SDR ASAA2021111636624Oil System · leakingAIR CONDITIONING SYSTEM DELIVERS "STINKY SOCK" SMELL. GROUNDED - YES. OPERATED PACKS WITH ENG. SUPPLIED AIR NO SMELL NOTED. OPERATED PACKS WITH APU AIR AND FOUND STINKY SOCK SMELL TO BE INTERMITTANT IN CABIN AND CONSTANT LIGHT OIL SMELL IN FLIGHT DECK. ACCOMPSDR ASAA2021102636400Oil Cooler · noneAPU OIL MONITORING DATA SHOWS OIL CONSUMPTION TO BE TRENDING HIGHER THAN EXPECTED. GROUNDED - YES. PERFORMED THOROUGH GVI OF APU, FOUND BACKSIDE OF APU OIL COOLER SATURATED WITH OIL. REMOVED AND REPLACED APU OIL COOLER REF AMM 49-91-41. LEAK CHECK GOOD. THIS CSDR ASAA2021102236386Lens · missingEXIT PLACARD SIGN LOWER AT OVERWING EXIT LEFT AFT MISSING. GROUNDED - YES. REPLACED LENS OVERWING EXIT LEFT AFT REF B737-800 AMM 33-50-00.OPS CK OK.SDR ASAA2021100536209Unknown · unknownR1 DOOR UNABLE TO CLOSE PROPERLY. VERY HARD TO CLOSE. GROUNDED - YES. TRANSFERED TO AAR MIG 5 W/O 1019605 / 8000/ 0001 S/N OK282474.SDR ASAA2021091536092Skin · crackedLEFT HORIZONTAL STAB LOWER SKIN IS CRACKED @ STA 147.90. (MARKED). GROUNDED - YES. REMOVED EXISTING REPAIR DOUBLER. REPAIRED LH HORIZONTAL STAB LWR SKIN WITH NEW REPAIR DOUBLER IAW B737-800 SRM 55-10-01-2R-11, REPAIR 11. THIS REPAIR 11 IS A CATEGORY B REPAIR &SDR ASAA2021090935895Light · inoperativeF/A REPORTS A/C R ROW 23 FLOOR TRACK LIGHTING INOP. GROUNDED - YES. REMOVED AND REPLACED FLOOR TRACK LIGHTING STRIP AT A/C R ROW 23 AS REQ.SDR ASAA2021090335847Extractor · faultedUPON USING APU BLEED AIR, THE FLIGHT DECK WAS INUNDATED WITH ICE PELLETS AND AIR COMING THROUGH THE VENTS AT APPROX 5-10X NORMAL VOLUME AFTER TWO CYCLES WE TURNED OFF APU BLEED AIR AND CALLED MX. GROUNDED - YES. REMOVED AND REPLACED 2 EACH WATER EXTRACTOR ON LSDR ASAA2021090335849Sensor · inoperativeRIGHT PACK TEMP NOT SHOWING A READING. GROUNDED - YES. REMOVED AND REPLACED R/H PACK TEMP SENSOR AND TEMP BULB SENSOR. OPS CHECK GOOD. REF B737-800 AMM 21-51-60, 21-51-52, AND B737-800 FIM 21-61 TASK 588. OK FOR SERVICE.SDR ASAA2021081235701Warning Light · false activationINFLIGHT RIGHT SIDE WINDOW LIGHT OVERHEAT ILLUMINATED. QRH ACCOMPLISHED LIGHT REMAINED ON. GROUNDED - YES. REPLACED BLOWN RIGHT SIDE WINDOW AND PITOT HEAT PANEL BULB PER B737-800 WDM 30-41-11. INSTALLED W0210-1001-20 FROM TERMINAL #2 TO TERMINAL #1 PER WDM 30-SDR ASAA2021072935585Warning Message · false activationHF RADIO #1 IS DISPLAYING FAIL IN BOTH ACTIVE AND STANDBY. GROUNDED - YES. VERIFIED #1 HF SHOWS FAIL FAIL NO HISTORY PERFORMED BITE ON HF #1 TRANSCEIVER BITE IS NORMAL AND #1 HF OPS NORMAL. GRD VERIFICATION SUCCESSFUL. REF B737-800 FIM 23-11 TASK 801.SDR ASAA2021080235580Actuator · faultyLEFT "RAM DOOR FULL OPEN" REMAINED ILLUMINATED ENTIRE FLIGHT, PRESSURE NORML, PACK LIGHT ILLUMINATED UPON RECALL AT TOP OF DESCENT CLEARED WITH RESET. GROUNDED - YES. ACCOMPLISHED BITE OF #1 & #2 ZONE TEMP CONT. #1 FAULTED RAM AIR ACTUATOR-CYCLED 1/2 WAY AND SSDR ASAA2021070535296Actuator · out of rigLT PACK LIGHT ILLUMINATES ON RECALL, EXTINGUISHES ON RESET. GROUNDED - YES. PZTC BITE SHOWS NO FAULTS. FOUND LEFT RAM AIR ACTUATOR OUT OF RIG-ADJUSTED PER INSTALLATION B737-800 AMM 21-51-21 OP CK GOOD. RAN LEFT PACK WITH NO DEFECTS NOTED.SDR ASAA2021070435362Actuator · inoperativeTECH SERVICE REQUEST. FOLLOW UP TO REPORT OF #2 ENG SPAR VALVE CIRCUIT BREAKER FOUND POPPED. GROUNDED - YES. REMOVED & REPLACED #2 ENG FUEL SPAR VALVE ACTUATOR REF 28-22-11. ACCOMPLISHED #2 SPAR VALVE ELECTRICAL CONTROL AND INDICATION TEST. TEST PASSES REF B7SDR ASAA2021070335246Circuit Breaker · tripped#2 ENG SHUTDOWN JUST PRIOR TO ENG STARTER CUTOUT ON GRND. SECOND ATTEMPT GOT NO FUEL FLOW. GROUNDED - YES. FOUND SPAR VALVE #2 ENG C/B POPPED ON P 6-3 B3. RESET C/B & STARTED #2 ENG @ GATE. GOOD START, NO DEFECTS NOTED. REF MM 20-60-01. SEAMC STEVE NOTIFIED.SDR ASAA2021070235231Control Valve · failedWITH POWER INCREASE UNUSUALLY HIGH AIRFLOW IN THE FLT DECK LEFT PACK GOES TO ABOUT 50 PSI AT 40% N1 WITH RIGHT STAYING ABOUT 32 PSI. GROUNDED - YES. REPLACED L/H PACK FLOW CONTROL VALVE REF B737-800 AMM 21-51-02 NO LEAKS NOTED, AT 40% N1 L PACK AT 31 PSI, R PASDR ASAA2021061735112Warning Light · illuminatedR FWD WINDOW OVERHEAT LIGHT ILLM. GROUNDED - YES. QRH PROCEDURE LIGHT EXT.SDR ASAA2021061235084Control Valve · inoperativeFLIGHT DECK TEMP EXCESSIVELY HOT, SHOWING 62'C ON CONT CAB. FOLLOWED MEL PROCEDURE WITH NO EFFECT. GROUNDED - YES. REMOVED & REPLACED LEFT AC PACK TEMPERATURE CONTROL VALVE REF B737-800 AMM 21-51-10, OP CHECKS FOR INSTALLATION OK.SDR ASAA2021060735061Blade · damagedREF T/C #7847001 SPECIAL DETAIL INSPECTION (SDI) (BORESCOPE) - CFM56-7 HPC #2 ENG. STAGES 2,4,6,8 BLADES. GROUNDED - YES. FOUND DAMAGE ON AFT SIDE STG 3 BLADES, DAMAGE TO STG 4 I/B CHANNEL, & DAMAGE ON L/E OF STG 8 BLADE. FURTHER EVALUATION OF BLADES 3 THRU 9 SDR ASAA2021060235009Control Valve · faultyLEFT PACK LIGHT ILLUMINATED ON RECALL AND EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. (RESOLVED ON W/O: 1874103 TASKCARD: N/R-00002 ) PZTC#1 (M1442) FAULTS TCV THIS PACK. REPLACED LEFT TEMP CONTROL VALVE (V139) BITE CHECK PASSES NO LEAKS NOTED. 3C/SDR ASAA2021052534905Warning Light · illuminatedLEFT PACK LIGHT ILLUMINATES ON MASTER RECALL. LIGHT EXTINGUISHES ON RESET. GROUNDED - YES. INITIAL BITE TEST SHOWED TCV FAULT ON L PACK. FAULT CLEARED. BITE TEST ACCOMPLISHED PER B737-800 AMM 21-61-00-700-806-002.SDR ASAA2021042334650Warning Light · false activationFO'S RIGHT SIDE WINDOW INDICATED OVERHEAT CONDITION QRC FOLLOWED LIGHT SWITCH REMAINED OFF. GROUNDED - YES. ACCOMPLISHED FIM BITE PROCEDURE NO FAULTS LOG ON WHCU B737-800 FIM 30-41 TASK 801, PERFORMED WINDOW HEAT SYSTEM OPS TEST GOOD B737-800 AMM 30-41-00-710-SDR ASAA2021042234644Coupler · inoperativeAS PER MCDU ACARS-HFDR MAINT PAGE #2 HF COUPLER NOT INSTALLED, #2 HF INOP. #1 HF OPS CHECK GOOD VOICE AND DATA. GROUNDED - YES. REMOVED & REPLACED HF1 & HF2 COUPLERS ON TSR71057. OPS CHECK GOOD. B737-800 AMM 23-11-61.SDR ASAA2021042234632Indication Sys · unknownWITH CENTER TANK FUEL QUANTITY AT 200 LBS, CTR FUEL PUMPS WERE TURNED ON AT CRUISE. BOTH CTR FUEL PUMP LIGHTS IMMEDIATELY ILLUMINATED AND REMAINED ON WITH NO APPARENT DECREASE IN CENTER FUEL QUANTITY. ONCE FUEL QUANTITY DECREASED BELOW 4500 LBS IN NUMBER 1 TANSDR ASAA2021042134631Transceiver · faultedAIRBORNE. NEITHER HF1 OR HF2 WILL TRANSMIT. (FOR ABOUT 10 MINUTES HF1 WAS BARELY AUDIBLE-BUT CAME BACK) BOTH CAPT, F/O SIDE. HANDMIKES DO NOT TRANSMIT EITHER ON HF 1 OR 2. HF1 SAT XFER-BOTH IN HF. GROUNDED - YES. DIVERSION TIME 63 MINUTES - INITIAL TESTING, #2SDR ASAA2021040834532Blade · damagedPER T/C 78472010 # 2 ENG. FAN LUBE #9 PLATFORM ELASTORMER IS TORN ON ONE SIDE. GROUNDED - YES. REF T/C 78472010 # 2 ENG FAN LUBE, #9 PLATFORM REPLACED AND NEW PLATFORM INSTALLED DURING LUBE.SDR ASAA2021040834531Spinner · damagedPER T/C 78472010 #2 ENG. FAN BLADE LUBE FRONT SPINNER CONE MISSING ANODIZED COATING BEYOND LIMITS. GROUNDED - YES. INSTALLED NEW FRONT SPINNER CONE REF B737-800 AMM 72-21-01/401.SDR ASAA2021032034416Skin · corrodedLAP AT STR-23L HAS MULTIPLE AREAS OF CORRONSION BETWEEN STA 727F AND STA 887 GROUNDED - YES. EVALUATED STE 23L STA 727F TO 887 AND REMOVED CORROSION AND REPAIRED IAW ALASKA AIRLINES EA NO 800-53EA-23333. THIS IS A CAT B REPAIR. THIS REPAIR IS APPROVED FIRST SSDR ASAA2021031934415Skin · corrodedSKIN CORRODED AT LAP FS-917 STR 23L GROUNDED - YES. REMOVED CORROSION AT STA 917 STR 23L AND REPAIRED IAW ALASKA AIRLINES EA 800-53EA-23333. THIS IS A CAT B REPAIR THIS REPAIR IS APPOVED FIRST STAGE APPROVAL (APPROVAL FOR STATIC STRENGTH AND INSPECTION THRESHSDR ASAA2021030934277Fire Detector · no testPILOT REPORTS #1 ENG FIRE DET SYS WON'T TEST. GROUNDED - YES. PER B737-800 FIM 26-10 TASK 801 AND 805 INITIAL EVALUATION: FIRE DETECT CTR MODULE BITE SHOWS ENG 1 LOOP B OPEN. FOUND WIRES LOOSE IN LUGS AT DETECTOR 4 AFT (HARNESS MW0326). REPAIRED BOTH TERMINAL SDR ASAA2021030534249Connector · detachedWHILE ACCOMPLISHING TC 78273000 # 1 ENG. MAINT. FAULT 73-30901 T12 SIGNAL DISAGREE. SHORT TIME FAULT. GROUNDED - YES. ACCOMPLISHED T/S FOR FAULT 73-30901 PER B737-800 FIM 73-26 TASK 805 - INITIAL EVALUATION (EEC TEST) CONFIRMED FAULT AND INPUT MONITORING SHOWESDR ASAA2021030134235Blade · damagedON FINAL IN SEA AT 300' AGL FOR 16R FULLY CONFIGURED AT FLAPS 30 DEGREES NOTICED SOUNDS OF COMPRESSOR STALL ON NO. 1 ENG AS WELL AS NI ON NO.1 ENG FLUCTUATION. SHUTDOWN NO.1 ENG EGT EXCEEDENCE. GROUNDED - YES. STARTED ACCOMP OF B737-800 FIM 71-05 TASK 805, ACCSDR ASAA2021012733955Harness · mislocatedNR 2 ENGINE CONNECTOR DP0502 HARNESS GROMMET MISLOCATED FROM CLAMP AT 3 O'CLOCK. GROUNDED-YES. REALIGNED DPO502 HARNESS GROMMET WITH CLAMP, NO FURTHER DEFECTS NOTED, REF. B737-800 AMM 73-21-06-400-801-F00.SDR ASAA2021011633902Fault Message · false activationWHILE ACCOMPLISHING TC 78273000 # 1 ENG MAINT FAULT 75-30401; THE VSV POSITION SIGNAL DISAGREE. SHORT TIME FAULT. GROUNDED - YES. PER B737-800 FIM 75-31 TASK 804 INITIAL EVALUATION L & R ACTUATORS GVI GOOD AND ELECTRICAL CHECKS PASS. NO FAULTS IN ENG HISTORY. SDR ASAA2020121033681Exciter · faultyWHILE ACCOMPLISHING APU DEPRESERVATION APU WOULD NOT START. GROUNDED-YES. APU BITE SHOWED MESSAGE 49-41011, NO FLAME SHUTDOWN. INITIATED B737-800 FIM 49-40 TASK 802. IGNITER NOT AUDIBLE. REPLACED IGNITER AND IGNITER LEADS, REF B737-800 AMM 4-41-51 AND 49-SDR ASAA2020120233627Battery Pack · inoperativeEMERGENCY LIGHTS AT L1 DOOR ARE INOPERABLE. GROUNDED-YES. REPLACED BATTERY PACK, PER B737-800 AMM TASK 33-51-06-960-805. OPERATIONS GOOD.SDR ASAA2020022863307Cover · brokenLIGHTED EXIT SIGN IN FWD GALLEY A/C RIGHT COVER IS BROKEN OFF. GROUNDED - YES. REMOVED AND REPLACED LIGHTED EXIT SIGN ASSY. OPS NML.SDR ASAA2020021853186Control Valve · failedAFTER PUSHBACK RIGHT PACK LIGHT & ASSOCIATED AIRCON LIGHT ILLUMINATED ON RECALL AFTER ENGINE START. GROUNDED - YES. PERFORMED BITE TEST OF PACK ZONE TEMP CONTROLLER, FLAGGED TCV. REMOVED AND REPLACED RH TCV REF B737-800 AMM 21-51-10. BITE TEST AND PACK FLOW TESDR ASAA2020012631978Controller · failedPERFORMED RECALL AFTER PUSHBACK ACCOMPLISHED AFTER START CHECKLIST AND GOT AIR CONDITION LIGHT AND ASSOCIATED RIGHT PACK LIGHT. PRESSED MASTER CAUTION LIGHT, PACK LIGHT AND AIR CONDITION LIGHT EXTINGUISHED, INIDICATING PRIMARY OR SECONDARY PACK CONTROLLER FAISDR ASAA2020012161894Warning Light · false activationPACK LIGHT ON MASTER CAUTION RECALL. GROUNDED - YES. FIM 21-53 TASK 821, BOTH PZTC'S HAVE NO PREVIOUS FLT FAULTS LOGGED. OPS CHECKED RIGHT PACK WITH NR 2 ENG BLEED, UNABLE TO DUPLICATE FAULT. VERIFIED RIGHT PACK OPS CHECKED NORMAL ON GND WITH ENGINE AND APU BSDR ASAA2019122643705Eec · failedDURING APU START UP WHILE TAXING INTO THE GATE. APU FAULT LIGHT ILLUMINATED. WE DISCONTINUED THE APU START AND ATTEMPTED RESTART WHEN THE APU FAULT LIGHT WENT OUT. THIS WAS REPEATED THREE TIMES. GROUNDED - YES. PERFORMED APU BITE PROCEDURE REF B737-800 FIM 49-SDR ASAA2019122433692Lamp · inoperativeEXIT LIGHT OUTSIDE L2 DOOR INOP. GROUNDED - YES. RELAMPED EMERGENCY EXIT LIGHT AT L2 DOOR REF AMM 33-51-04, OPS CHECK GOOD.SDR ASAA201912231679Probe · inoperativeCLIMBING THROUGH FL 280 R ELEV PITOT LIGHT CAME ON. CHECKED AND C/B WAS POPPED. GROUNDED - YES. ALTERNATE DEACTIVATION PERFORMED IAW CHAP 5 TABLE 3 ITEM 1. DISCONNECTED PLUG D638. VERIFIED SHORT OF 7.8 OHMS TO GROUND FROM PIN 40. DISCONNECTED PLUG D4826 AND VESDR ASAA2019122493690Fuel Sys · out of balanceWITH FUEL IN CENTER TANK AND ALL FUEL PUMPS ON, FUEL STARTED FEEDING OUT OF NR 1 MAIN TANK CREATING AN IMBALANCE. GROUNDED - YES. ON DEFERRAL.
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