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 ASAA2019122081658Indicator · failed#1 FUEL TANK QUANITY INDICATOR BLANK IN COCKPIT. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 28-41. TASK 813 SYSTEM REPORTS FAULT CODE 28-41103. FQIS BITE PER 28-41 TASK 801 REPORTS SAME. GROUND TEST SUGGEST TANK OVER FULL TRANSFERRED 500 LBS TO CENTER TANK. FAUSDR ASAA2019112031452Wire Harness · faultedWHILE PERFORMING T/C 78273000 FOUND ECONOMIC TERM FAULTS ON THE #1 ENG, FAULTS 75-10411/75-20411(THE HPTACC POSITION SIGNALS DISAGREE). ALSO HAS HISTORY OF ECONOMIC TERM FAULTS 75-20461/75-10461(THE HPTACC DEMAND AND POSITION SIGNALS DISAGREE), 75-10361(THE HPSDR ASAA2019112031415Fault Code · false activationWHILE ACCOMPLISHING T/C 78273000, FOUND A SHORT TIME FAULT ON THE #2 ENG, FAULT # 75-10452 "THE VBV POSITION SIGNALS DISAGREE". GROUNDED - YES. PERFORMED B737-800 FIM 75-32 TASK 803 NO FAULTS PRESENT AND APPEARS TO BE A ONE TIME FAULT, SYSTEM OP CHECKS GOOD.SDR ASAA2019110731340Fault Message · activatedWHILE ACCOMPLISHING T/C #78273000 FOUND NO. #1 ENGINE ECONOMIC FAULT (75-30411) THE HPTACC POSITION SIGNALS DISAGREE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019110431248Control Valve · failedRIGHT PACK LIGHT ILLUMINATES DURING MASTER CAUTION RECALL. EXTINGUISHES WITH RESET. GROUNDED - YES. BOX FAULTED R/H TCV RESET BOX AND RAN BITE CHECK (HARD FAULTED.) REMOVED AND REPLACED R/H TCV AND RAN BITE CHECK. NO FAULTS NOTED LEAK CHECK GOOD REF B737-800 ASDR ASAA201911051239Warning Light · false activationRH PACK LITE ILLUMINATED ON RECALL AND EXTINGUISHES WITH RESET. GROUNDED - YES. ACCOMPLISHED B737-800 AMM 21-61-00 PACK ZONE TEMP CONTROLLER BITE GRD VERIFICATION SUCCESSFUL THIS CLEARS MEL 21-32B.SDR ASAA2019111531341Fault Code · activated#1 ENG FAULT CODE 75-10361, THE HPTACC POSITION SIGNAL IS OUT OF RANGE. 500 FLT HRS ECOMOMIC FAULT. DEFERRED PER T/C 78273000. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019103091173Slide · low pressureL2 ESCAPE SLIDE INDICATING PSI NEAR LOWER LIMIT. GROUNDED - YES. AFTER L2 ESCAPE SLIDE PACK INFLATION CYLINDER CHECK FOUND PRESSURE OUT OF LIMITS. REMOVED AND REPLACED L2 ESCAPE SLIDE PACK ASSY WITH A SERVICEABLE UNIT PER AMM 25-66-01/401.SDR ASAA201910231082Sensor · failedLEFT SIDE WINDOW OVERHEAT ILLUMINATED, FOLLOWED QRH PROCEDURE LIGHT EXTINGUISHED. GROUNDED - YES. REMOVED AND REPLACED LH SIDE SLIDE WINDOW (#2) IAW B737-800 AMM 56-12-11. OPS CK AND LEAK CK GOOD. NO DEFECTS NOTED. THIS CLEARS MEL 30-11E.SDR ASAA201910231077Warning Light · false activationLEFT SIDE WINDOW OVERHEAT ILLUMINATED. GROUNDED - YES. FOLLOWED QRH PROCEDURE LIGHT EXTINGUISHED.SDR ASAA2019102203175Warning Message · false activationDURING APPROACH L SIDE WINDOW HEAT OVER HEAT LIGHT ILLUMINATED. GROUNDED - YES. TURNED L/H SIDE WINDOW HEAT ON & GREEN "ON" LIGHT ILLUMINATED. ACCOMP WINDOW HEAT CONT UNIT BITE TEST, TEST SHOWS OK. ACCOMP FAULT HISTORY BITE SHOWS SENSOR FAULT FOR L/H SIDE. REFSDR ASAA2019100743931Warning Light · false activationLEFT CENTER FUEL PUMP CAME ON WITH 1080 LBS. GROUNDED - YES. FUELED CENTER TANK TO 14000 LBS. BOTH L/CENTER AND R/CENTER LOW PRESS LIGHTS CAME ON THEN OFF IMMEDIATELY. CLASSED AS INTERMITTENT FAULT. OK FOR SERVICE, REF B737-800 FIM 28-22 TASK 801.SDR ASAA2019092430806Wire · disconnectedWHILE ACCOMPLISHING TASK CARD 78233008 FOUND EMERGENCY EXIT AISLE AREA LIGHT AT ROW 23ABC INOP. GROUNDED - YES. RE-CONNECTED WIRE W3152-0356-20 TO GROUND BLOCK GD3756DC, REFERENCE WDM 33-51-13 AND SWPM 20-90-15. PERFORMED OPERATIONAL EST OF EMERGENCY EXIT AREASDR ASAA2019092130762Unknown · malfunctionedUNABLE TO RECEIVE SATCOM CALLS FROM DISPATCH. OUTBOUND CALLS ON SAT-2 & SAT-1 ARE OPS NORMAL. GROUNDED - YES. ACCOMPLISHED INCOMING CALL TEST, WAS ABLE TO RECEIVE INBOUND CALLS. REF AMM 23-15-00-730-801 STEP A(2).SDR ASAA2019091430708Power Supply · inoperativeRIGHT OVERWING EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED LIGHT OVERWING EMERGENCY LIGHT POWER SUPPLY S/N 39707, OPS CHECK GOOD IAW AMM 33-51-06-960-806.SDR ASAA2019082130709Skin · crackedLT HORIZONTAL LOWER SKIN HAS A CRACK AT STA 147 APROX 32" AFT OF FRONT SPAR. (MARKED). GROUNDED - YES. REPAIRED LT HORZ STAB LOWER SKIN IAW SRM 55-10-01-2R-11. THIS REPAIR IS CAT B REPAIR AND REQUIRED INTERVAL REPEAT INSPECTION EVERY 9000 FLIGHT CYCLES AND INSSDR ASAA2019082130567Door Sill · corrodedR-2 DOOR MOP SILL IS CORRODED BETWEEN FS 947 TO FS 990. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED AND REPLACED MOP SILL IAW SRM 51-40-02-0G-0W 1.5 O .080 R .040 L 3.0 D .040.SDR ASAA2019082130566Panel · crackedBREAK PANEL ON L/S FS 540 I/B FWD AND AFT SIDE IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED PANEL IAW SRM 51-40-02-0G-0.SDR ASAA201908123358Warning Light · false activationAFTER ENGINE START, CONT CABIN ZONE TEMP ILLUMINATED ON RECALL. QRH PROCEDURE FOLLOWED. LIGHT EXTINGUISHED WHEN MASTER CAUTION SYSTEM RESET. GROUNDED - YES. PERFORMED B737-800 FIM TASK 21-62 TASK 842 AND CONT CABIN ZONE TEMP LIGHT EXTINGUISHED, NO FAULT LIGHTSSDR ASAA2019052129446Lens · missingFLIGHT ATTENDANT REPORTS- MID CABIN EXIT SIGN ONE SIDE OF EXIT SIGN MISSING. GROUNDED - YES. REPLACED MID CABIN EXIT SIGN HOUSING & LENS PER AMM 33-51-01-960-801.SDR ASAA2019051729363Sensor · defectiveFOLLOW-UP TO REPORTS OF APU OIL BEING "FULL" WITH CDU REFLECTING "ADD" .PRI 2-. GROUNDED - YES. REMOVED AND REPLACED APU OIL LEVEL SENSOR IN REFERENCE TO AMM 49-94-11. OPS CHECKS GOOD.SDR ASAA2019050629256Spacer · debondedPER T/C 78472010 NR 2 ENGINE FAN LUBE SPACERS NR 3,5,8,910,11,13,14,16,17,18,19,20,21,22,23, AND 24 ELASTOMER STRIPS DISBONDED. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE FAN LUBE SPACERS NR3,5,8,9,10,11,13,14,16,17,18,19,20,21,22,23, AND 24 ELASTOMER STSDR ASAA2019043099185Warning Light · false activationLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. EXTINGUISHES WHEN CLEARED. GROUNDED - YES. ACCOMPLISHED LEFT PACK BITE I/A/W B737-800 FIM 21-62 TASK 801. FOUND TCV FAULT. WAS ABLE TO RESET TCV. LEFT PACK OPS CHECK GOOD IAW FIM 21-62 TASK 830.SDR ASAA2019042959137Control Module · failedLEFT PACK LIGHT ILLUMINATES ON RECALL CLEARS ON M/C RESET. GROUNDED - YES. REMOVED AND REPLACED RAM AIR INLET ACTUATOR IAW B737-800 AMM 21-51-21 BITE TEST GOOD IAW 21-61-00 FOUND TEMPERATURE CONTROL VALVE FAILED. REMOVED AND REPLACE TEMPERATURE CONTROL VALVE ISDR ASAA2019040428919Bracket · gougedREF T/C # 78472000 #1 ENG INLET AND FAN BLADES - DETAILED INSP FOUND MOUNT BRACKET ON FWD DUCT FOR TAI VALVE GOUGED BY TURNBUCKLE. GROUNDED - YES. REMOVED & REPLACED #1 ENG COWL TAI VALVE FWD DUCT REF CFM56-7 PPBM 71-00-02 FIG 27-1 SHT 2,4,5,6 & 7.SDR ASAA2019040428918Bracket · gougedREF T/C # 78472000 #1 ENG INLET AND FAN BLADES - DETAILED INSP FOUND LWR O/B MOUNT BRACKET ON ENG FLANGE FOR TAI VALVE GOUGED FROM TURNBUCKLE. GROUNDED - YES. REMOVED & REPLACED #1 ENG COWL TAI VALVE FWD DUCT MOUNT BRACKET REF CFM56-7 PPBM 71-00-02 FIG 6-1 SHTSDR ASAA2019040848917Bearing · defectiveREF T/C # 78472000 #1 ENG INLET AND FAN BLADES - DETAILED INSP FOUND AFT TURNBUCKLE FOR START VALVE HAS BAD ROD END BEARING. GROUNDED - YES. REMOVED & REPLACED AFT TURNBUCKLE FOR #1 ENG START VALVE LOWER DUCT REF CFM56-7 PPBM 71-00-02 FIG 25-1 SHT 2 & 4.SDR ASAA2019040168834Probe · out of toleranceON FMC/CDU TASKCARD # 78273000, FOUND LONG TERM FAULT CODE 79-11101. #1 ENGINE OIL TEMPERATURE SIGNAL IS OUT OF RANGE. APPLY PLT DEFERRAL PER T/C 78273000. GROUNDED - YES. PER B737-800 FIM 79-21 TASK 802 ELECTRICAL CONNECTOR DP0602 GVI GOOD. REMOVED AND REPLACSDR ASAA2019031628646Eec · faultyON DESCENT INTO ANC NR 1 OIL TEMP INDICATION BECAME INTERMITTENTLY BLANK SEVERAL TIMES. INDICATION WAS NORMAL PRIOR TO SHUTDOWN. GROUNDED - YES. REMOVED CONNECTOR TO OIL TEMP SENSOR AND INSPECTED, NO DEFECTS NOTED. RE-ATTACHED CONNECTOR REF AMM 79-34-02. PERFOSDR ASAA2019030928554Control Unit · malfunctionedON LANDING ELEC LIGHT ILLUMINATED. GROUNDED - YES. RAN FIM 24-31 TASK 801 SPCU FAULT LOGGED. RAN FIM 24-34 TASK 802, RESET SPCU. TEST OK. OK FOR SERVICE.SDR ASAA2019030628501Warning System · false activationAFTER LANDING ELEC LIGHT ILLUMINATED. GROUNDED - YES. BITE SHOWS SPCU FAULT. ACCOMPLISHED FIM 24-34 TASK 802. CYCLED SPCU NORMAL AND SPCU STANDBY C/B'S ON M01720. FAULT CLEARED AND BITE TEST NORMAL REF FIM 34-31 TASK 801.SDR ASAA2019022028337Wire Harness · faultyWHILE PERFORMING T/C 78273000, FOUND MAINT MESSAGE 79-11101, THE ENGINE OIL TEMPERATURE SIGNAL (TEO) IS OUT OF RANGE, LONG TERM FAULT. GROUNDED - YES. ON DEFERRAL. REMOVED AND REPLACED J6 FAN WIRING HARNESS ON NR 1 ENGINE PER AMM 73-21-06/401, NO EEC FAULTS. ASDR ASAA2019012827976Control Valve · inoperativeAFTER T/O AND DURING CLIMB THE LEFT DUCT PRESSURE WAS LOW. PASSING 10,000' PRESSURES WERE 41 AND 13. WHEN WE LEVELED OFF THE DUCT PRESSURES EVENED OUT. WHEN WE INCREASED THE POWER THE SPLIT WOULD COME BACK. GROUNDED - YES. AIR TURNBACK - DIVERSION TIME 24 MINUSDR ASAA2018122227569Wire Harness · defectiveGE DIAGNOSTICS REPORTS #1 ENGINE TREND DATA SHOWS A DELTA EGT INCREASE AND EGTHDM DECREASE. EGT INDICATION ERRORS ARE SUSPECT. GROUNDED - YES. FOUND J10 HARNESS BAD. REMOVED AND REPLACED J10 HARNESS IAW B737-800 AMM 73-21-06. REMOVED AND REPLACED EGT PROBE S3 SDR ASAA2018120227187Probe · failedFAULT CODE MSG 79-11101 ENGINE OIL TEMP OUT OF RANGE NR 1 ENGINE LONG TIME FAULT DEFERRED PER TC 78273000. GROUNDED - YES. ON DEFERRAL. REPLACED OIL TEMP SENSOR T432 PER AMM 79-34-02/401. LEAK TEST GOOD PER AMM TASK 71-00-00-700-801-F00. EEC TEST GOOD PER AMM SDR ASAA2018120317168Control Valve · failedAFTER BOTH ENGINES STARTED L PACK LIGHT CAME ON. L PACK LIGHT WOULD NOT GO OUT ON RECALL, DID NOT GO OUT ON TRIP RESET. RAN QRH AND RETURNED TO THE GATE. AFTER RETURN TO THE GATE ENGINES OFF PACK LIGHT WENT OFF. GROUNDED - YES. R & R L PACK TEMPERATURE CONTROLSDR ASAA2018110926833Oil Cooler · failedNR 2 ENG MAIN OIL/FUEL HEAT EXCHANGER FAILED RUN ON TORQUE CHECK FOR FUEL TUBE (7) REF AMM 79-21-02-400-801-F00 STEP 3 G (3) (H),3. GROUNDED - YES. REPLACED NR 2 ENG MAIN OIL/FUEL HEAT EXCHANGER PER AMM 79-21-02. LEAK CHECK GOOD. GROUND VERIFICATION GOOD.SDR ASAA2018110826834Hmu · failedON NR 2 ENGINE START, AFTER START LEVER RAISED TO IDLE. ENGINE HUNG UP AT APPROXIMATELY 40% N2, EGT 505*, ABORTED START. RAN CHECKLIST. 2ND ATTEMPT AT START NORMAL. GROUNDED - YES. HUNG START ON FIRST ATTEMPT, 2 OTHER STARTS SUCCESSFUL. REMOVED AND REPLACED NRSDR ASAA2018110826821Check Valve · defectiveNR 2 ENGINE HAS REPORTS OF HUNG STARTS WITH LOW EGT AND LOW N2. GROUNDED - YES. REPLACED NR 2 ENGINE 5TH STAGE BLEED AIR CHECK VALVE REF AMM 36-11-02-400-801 AND ACCOMPLISHED INSTALLATION TEST. TEST OK, NO LEAKS NOTED. REMOVED AND REPLACED NR 2 ENGINE SPAR VALSDR ASAA2018110726788Engine · hung startAFTER RAISING START LEVER TO IDLE, ENG #2 N2 HUNG UP AT APPROX 45% EGT FLASHING ABORTED ENGINE START. GROUNDED - YES. PERFORMED B737-800 AMM TASK 28-22-00-710-801 ELEC CONTL AND END TEST TO #2 ENG FUEL SPAR VALVE. IND AND FUNC TEST GOOD. PERFORMED B737-800 FIMSDR ASAA2018110976787Engine · hung startAFTER RAISING START LEVER TO IDLE ON ENGINE START (#2) ENGINE HUNG UP AT APPROX 47% N2 EGT APPROX 574 DEG. GROUNDED - YES. AIRCREW RAN ENGINE @ GATE AND ALL PARAMETERS NORMAL. INTERROGATED FMC FOR ENGINE #2 FAULTS + NO FAULTS NOTED. NO HISTORY. OK FOR CONTINUESDR ASAA2018110626736Control Valve · malfunctionedLEFT PACK ILLUMINATED AFTER ENGINE START EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. PERFORMED AMM 21-61-00 LT ZONE TEMP CONT VLV THIS PACK, RESET AND PERFORMED BITE, ALL PASS "GO".SDR ASAA2018110326721Exciter · failedENG NR 2 FAILED TO START USING LEFT IGNITION SYS, RIGHT IGN SYS WORKED. GROUNDED - YES. REMOVED AND REPLACED IGNITION EXCITER PER AMM 74-11-01. OPS CHECK GOOD.SDR ASAA2018101526460Warning System · false activationON TAXI OUT LEFT PACK LIGHT ILLUMINATED. GROUNDED - YES. FOUND "TCV" FAULT ON NR 1 CONTROLLER. ACCOMPLISHED BITE TEST PER AMM TASK 21-61-00-700-806-002. THIS RESET THE FAULT. RAN BITE SEVERAL TIMES. FAULT IS CLEARED.SDR ASAA2018091026076Wire Harness · defectiveNR 1 ENGINE TREND DATA SHOWS EGT INDICATION TO HAVE GREATER THAN EXPECTED SCATTER. INDICATION ERRORS ARE STILL SUSPECT. GROUNDED - YES. CW SB 73-0142 REMOVED CJ9 HARNESS NR 1 ENG PN 325-045-201-0 AND INSTALLED PN 325-045-502-0 REF AMM 73-21-06. FADEC SYSTEM TESDR ASAA2018090425996Fault Message · false indicationAPU BITE CURRENT STATUS SHOWS FAULT MSG 49-61259 SPEED SENSOR 1 SHOWS OPEN CIRCUIT. GROUNDED - YES. ACCOMPLISHED FIM 49-60 TASK 817 UP TO PG 7 PA 7, FAULT CLEARED FROM CURRENT STATUS ON APU BITE.SDR ASAA2018082125891Igniter · inoperativeENGINE #2 FAILED TO START, NO EGT 15 SEC. AFTER START LEVER RAISED TO IDLE. RAN QRC, QRH. IGNITOR LEFT WAS SELECTED. CALLED SEA MX AND STARTED ENGINE W/ RIGHT IGNITOR THEN MEL VIA FLIGHT CREW PLACARD APPLIED AND PROCEDURE APPLIED. GROUNDED - YES. REL PER MEL 7SDR ASAA2018080125614Guide Arm · out of adjustRAMP REPORTS R1 DOOR DIFFICULT TO CLOSE. GROUNDED - YES. C/W GALLEY SERVICE DOOR ADJUSTMENT PER AMM 52-41-00, ADJUSTED GUIDE ARM AND PINS. OPS CHECKED GOOD.SDR ASAA2018073025567Start Valve · failedNR 1 START VALVE WOULD NOT OPEN FOR START. GROUNDED - YES. C/W FIM TASK 80-07 TASK 804. CONFIRMED 28V AT CONNECTOR DP1202 ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 START VALVE PER AMM 80-11-03. OPS AND LEAK CHECKS GOOD.SDR ASAA2018071225361Wire Harness · chafedWHILE ACCOMPLISHING T/C N8420001, FOUND A WIRE CHAFED BEYOND LIMITS ON THE CORE FIRE DETECTOR NR 4 AFT MW0325 ON NR 2 ENG. GROUNDED - YES. R&R NR 2 ENG FIRE DETECTOR HARNESS MW0325 REF MM 26-11-02. OPS CH3ECK GOOD.
Back to N588AS