N519AS

Service difficulty reports · 485

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 = 'N519AS' 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 ASAA2014102609508Satcom · malfunctionedNO SATCOM PROMPT ON MCDU MENU PAGE AFTER POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED QRH FOR SATCOM LOCKUP ON GROUND, SYSTEM RETURNED TO NORMAL AFTER 60 SECONDS.Oct 26, 2014 · N519AS · Boeing 737890 · Communications SystemSDR ASAA2014102409467Warning Message · false activationFMC DISAGREE ON TAXI OUT OUT. ACFT GROUNDED. QRH PROCEDURES COMPLIED WITH - NORMAL OPS.Oct 24, 2014 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014102309486Transmitter · malfunctionedDURING LANDING THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ACFT GROUNDED. REPLACED NR 2 ENGINE SCAVENGE OIL FILTER CLOGGING TRANSMITTER IAW AMM 79-21-07. R & R SCAVENGE OIL FILTER IAW AMM 79-21-06. LEAK AND OPS CHECK GOOD IAW AMM 73-21-00 AND 71-00Oct 23, 2014 · N519AS · Boeing 737890 · Engine Oil Indicating SystemSDR ASAA2014091709149Anti-Ice Valve · failedNR 1 COWL VALVE OPEN LIGHT REMAINED ILLUMINATED BRIGHT BLUE WITH TAI AMBER LIGHT DURING FLIGHT WITH ENGINE ANTI-ICE SWITCH TURNED ON. ACFT GROUNDED. REPLACED NR 1 ENGINE ANTI-ICE VALVE, OPS CK FAILED. R & R VALVE AGAIN REF MM 30-21-11. LEAK & OPS CK GOOD RESep 17, 2014 · N519AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2014081308836Indicator · failedFUEL QTY INDICATOR FOR TANK 2 ON THE REFUELING PANEL INOPERATIVE. ACFT GROUNDED. REPLACED NR 2 FUEL QTY INDICATOR, ALL OPS NORMAL, REF MM 28-41-61.Aug 13, 2014 · N519AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2014081008803Button · intermittentCAPTAIN'S FMC L2 BUTTON WORKS INTERMITTENTLY. ACFT GROUNDED. REPLACED CAPTAIN'S FMC CDU REF MM 34-61-01, OPS CHECKED GOOD.Aug 10, 2014 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014070608462Control Panel · failedTHE AUTOPILOT SELECTED, DISCONNECTED TWICE DURING THE FLIGHT, ONCE DURING CLIMBOUT AND ONCE IN LEVEL FLIGHT AT 38,000 FT. THE AIR WAS SMOOTH IN BOTH CASES. WHEN THE AUTOPILOT DISCONNECTED IN CRUISE, AUTOTHROTTLES WORKED FINE. ACFT GROUNDED. FCC A & B LOGGEJul 6, 2014 · N519AS · Boeing 737890 · Autopilot SystemSDR ASAA2014062908387Selector Panel · failedTHE ALTITUDE SELECTOR ON THE MCP WILL NOT CHANGE ALTITUDES. ACFT GROUNDED. CONFIRMED FAULT, MCP ALTITUDE NUMBERS FROZEN. PULLED AND RESET "MCP DC2" CIRCUIT BREAKER AT P6-2 PANEL, MCP ALTITUED SELECTOR WILL FUNCTION FOR A WHILE THEN FREEZES UP. REPLACED DFCJun 29, 2014 · N519AS · Boeing 737890 · Autopilot SystemSDR ASAA2014062608378Warning Message · false activationFMC DISAGREE LIGHTS CAME ON DURING TAXI. ACFT GROUNDED. PULLED AND RESET FMCS COMPUTER CIRCUIT BREAKERS AND RESTORED FMC DATA.Jun 26, 2014 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014061908290Selector · malfunctionedMCP ALTITUDE SELECTOR INOPERATIVE, NUMBERS IN ALTITUDE WINDOW FROZEN. ACFT GROUNDED. MCP CHECKED NORMAL IAW FIM 22-11TASK 80, ALT SELECTOR. OPS CHECKED NORMAL.Jun 19, 2014 · N519AS · Boeing 737890 · Autopilot SystemSDR ASAA2014051307801Acars · malfunctionedACARS DATALINK IS FULL AND IT IS VERY SLOW IN ITS COMMUNICATION FUNCTIONS. ACFT GROUNDED. PERFORMED FIM TASK 34-61-00-810-839. RESET DATA LINK. DATA FULL MESSAGE DO NOT SHOW ON EITHER DIPLAY AFTER 5 MIN INITIAL DISCREPANCY INTERMITTENT FAULT IAW FIM TASK.May 13, 2014 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014041907514Starter · failedNR 1 ENGINE STARTER BLOWING OIL FROM STARTER AIR EXHAUST. ACFT GROUNDED. REPLACED NR1 ENGINE STARTER WITH NEW IAW AMM 80-11-01. NR 1 ENGINE STARTER VERIFIED EFFECTIVE.Apr 19, 2014 · N519AS · Boeing 737890 · Engine StarterSDR ASAA2014041807505Anti-Ice Valve · failedTHE LT ANTI-ICE VALVE LIGHT REMAINS BRIGHT BLUE, WHEN THE SWITCH IS POSITION TO ON. THE TAI LIGHT ON THE ENGINE DISPLAY IS GREEN WHEN SWITCH IS POSITION ON. ACFT GROUNDED. REPLACED NR 1 ENGINE NOSE INLET COWL TAI VALVE REF MM 30-21-11. OPS CK OK.Apr 18, 2014 · N519AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2014040907498Anti-Ice Valve · failedTOOK SEVERAL ATTEMPTS TO GET NR 1 ENGINE ANTI-ICE VALVE TO OPEN. ACFT GROUNDED. R & R NR 1 ENG COWL ANTI ICE VALVE IAW MM 30-21-11-000-801 AND MM 30-21-11-400-801 THRU STEP 3H(3)(F)(2). ACCOMPLISHED STEPS 3H(3)(F) 3&4. ACCOMPLISHED STEPS 3H(3)(F) 5 THRU J(1Apr 9, 2014 · N519AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2014032607323Warning Light · false activationLEFT ENG ANTI-ICE INTERMITENT ON DECENT. ACFT GROUNDED. PERFORMED ENGINE COWL ANTI-ICING, OPS CHECK LT ENG IAW MM 30-21-00-701-801. OPS CHECKED GOOD.Mar 26, 2014 · N519AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2014031707224Warning Message · false activationAPU FAULT LIGHT ILLUMINATED ON START, SECOND START NORMAL. ACFT GROUNDED. PERFORMED APU BITE IAW FIM 49-60, TASK 801. FOUND IN FAULT HISTORY CODE 49-61157. PERFORMED FIM TASK 49-60, TASK 804 FOUND TO BE INTERMITTENT FAULT. APU STARTED NORMAL. GROUND VERMar 17, 2014 · N519AS · Boeing 737890 · APU ControlsSDR ASAA2014022807029Control Unit · malfunctionedELECTRICAL LIGHT ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. PERFORMED BITE CHECK IAW FIM TASK 24-31, TASK 801. SPCU INOPERATIVE FAULT STORED. PERFORMED FIM TASK 24-34, TASK 802. FAULT CLEARED, SEAM C. R & R SPCU IAW MM TASKS 24-34-11-000-801/24-34-11-4Feb 28, 2014 · N519AS · Boeing 737890 · DC Generating SystemSDR ASAA2014022707030Battery · dischargedMAIN ACFT BATTERIES DEAD. ACFT GROUNDED. R & R BOTH MAIN ACFT BATTERIES REF AMM 24-31-11. OPS CHECKED GOOD REF SAME. VERIFIED PN SEAM C.Feb 27, 2014 · N519AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2014021706883Fmc · intermittentLOST LEFT FMC AT 37,000 FT, FOLLOWED QRH, LT FMC REMAINED FAILED. ACFT GROUNDED. RESET FMC CICUIT BREAKERS IAW AMM 20-60-01-860-801. ACCOMPLISHED FMC FAULT ISOLATION PROCEDURE, IAW FIM 34-61, TASK 836. FMC OPS NORMAL, INTERMITTENT FAULT, NO HISTORY PAST Feb 17, 2014 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014020106731Autothrottle Sys · malfunctionedAFTER TAKEOFF, AUTOTHROTTLE DROPPED OFF AFTER SELECTING TAKEOFF MODE. DURING CLIMBOUT, AUTOTHROTTLE WOULD ENGAGE FOR 5-10 SECONDS THEN DROP OFF. ACFT GROUNDED.Feb 1, 2014 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2014020106729Autothrottle Sys · malfunctionedDURING DEPARTURE, AUTO THROTTLE DISENGAGED. WOULD NOT RE-ENGAGE. ACFT GROUNDED. ACCOMPLISHED AUTO THROTTLE SYS OPS TEST, IAW AMM 22-31-00-710-801. AUTO THROTTLE TEST OK.Feb 1, 2014 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013121912202Handle · obstructedR1 DOOR HANDLE VERY STIFF AT FIRST DETENT WHEN OPENING. ACFT GROUNDED. REPOSITIONED R1 DOOR LINER IAW MM 52-41-31.Dec 19, 2013 · N519AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2013111496419Light · brokenEMERGENCY LIGHT ON LT SIDE OF CENTER AISLE AT ROW 20ABC BROKEN. ACFT GROUNDED. INSTALLED NEW LIGHT STRIP AMM 33-51-15.Nov 14, 2013 · N519AS · Boeing 737890 · Emergency LightingSDR ASAA2013100396098Autothrottle Sys · malfunctionedINFLIGHT, AUTO-THROTTLES FAIL LIGHT ILLUMINATED AND AUTO THROTTLES DISENGAGED. WOULD ENGAGE FOR A FEW SECONDS THEN DISENGAGE. ACFT GROUNDED. COULD NOT DUPLICATE. A/T FAULT, REVIEW LOGGED NR 1 ASM FAULT NR 22-31687 ON FLT 14, 4 TIMES ONLY. ACCOMP FIM 22-3Oct 3, 2013 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013092396040Starter · failedON ENGINE START, ENG NR 1 START VALVE OPENED NORMALLY BUT NO ROTATION. ACFT GROUNDED. FOUND NR 1 ENG STARTER WOULD NOT TURN W/START VALVE OPEN, REF 80-11-01-00-801. REPLACED NR 1 ENG STARTER IAW AMM 80-11-01-000-801-F00 & 80-11-01-400-801-F00. OPS & LEAK CSep 23, 2013 · N519AS · Boeing 737890 · Engine StarterSDR ASAA2013091996014Wire Harness · damagedDURING T/C N8420001, RT ENGINE EXTERNAL HARNESS GVI, FOUND WIRE DAMAGE FOR UPPER FAN B LOOP, FIRE DETECTOR MW0316, REF WDM 26-11-21. ACFT GROUNDED. REPLACED WIRE HARNESS MW0316 (B LOOP), REF AMM TASK 26-11-021-000-801 AND 26-11-02-400-801. ACCOMPLISHED ENG FSep 19, 2013 · N519AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2013090195909Anti-Ice Valve · stuckDURING DESCENT, NR 1 COWL ANTI-ICE VALVE STUCK OPEN. ACFT GROUNDED. COMPLIED WITH OP TEST OF THE NR 1 ENGINE COWL ANTI-ICING IAW AMM TASK 30-21-00-710-801. OPS TEST THE ENG ANTI-ICE 1 SWITCH SEVERAL TIMES- OP TESTS GOOD. ACFT OK FOR CONTINUED SERVICE.Sep 1, 2013 · N519AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2013082295871Valve · failedFORWARD CABIN ZONE TEMP ILLUMINATED DURING RECALL. LIGHT EXTINGUISHED WHEN MASTER CAUTION RESET IAW QRH 215. ACFT GROUNDED. NR 2 ZONE TEMP CONTROLLER BITE REF FIM 21-62, TASK 801 SHOW ZONE TRIM VALVE FAULT. FOUND AFT COMPARTMENT PASS. ZONE TRIM AIR MOD VALVEAug 22, 2013 · N519AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013080295731Indicator · activatedWHILE ACCOMPLISHING TASK CARD N8005001, FOUND APU OIL FILTER INDICATOR POPPED. ACFT GROUNDED. R & R APU OIL FILTER ELEMENT, AND SERVICED FILTER INDICATOR IAW AMM 49-91-13. OPS AND LEAK CK GOOD, NO DEFECTS NOTED.Aug 2, 2013 · N519AS · Boeing 737890 · APU Oil SystemSDR ASAA2013052894933Transceiver · failedWEATHER RADAR IS SPOKING ALL QUADRANTS ALL RANGES. ACFT GROUNDED. VERIFIED DISCREPANCY. NOTICED SPOKING ON RADAR DISPLAY. REPLACED RADAR RT. PERFORMED SYS OPS TEST REF 34-43-00. SYS CHECKED NORMAL.May 28, 2013 · N519AS · Boeing 737890 · Weather Radar SystemSDR ASAA2013051094769Circuit Breaker · trippedCAPT FD ILLUMINATED ON ADI, SPEED TRIM & MACH TRIM LIGHTS ILLUMINATED. A/T WOULD NOT ENGAGE. ACFT GROUNDED. FOUND AFCS SYS A WARN LIGHT C/B P18-1 PANEL OPEN. RESET C/B IAW AMM 20-60-01. ACCOMPLISHED LAND VERIFY TEST IAW AMM 22-11-00-700-801. OPS CK NORMAL AMay 10, 2013 · N519AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2013042994651Indication Sys · malfunctionedNR 2 MAIN FUEL TANK READS 8.50. A FEW MINUTES LATER IT IS READING 8.14. TOTAL WAS READING 41.3. NOW IT IS READING 40.9. APU HAS NOT BEEN RUNNING. ACFT GROUNDED. TASK CARD NG-28WC-00001 ACCOMPLISHED. CURRENT STATUS GOOD, REF FIM 28-41-807.Apr 29, 2013 · N519AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2013032494244Engine · vibrationON TAKE OFF AND CLIMB, F/A AND PAX REPORTED LOUD VIBRATION FROM LT ENGINE AND ODOR OF OIL & SMOKE IN CABIN. SOUND REDUCED WITH POWER 70 N1. ALL ENGINE INDICATIONS NORMAL VIBRATION INCREASED DURING DESCENT WITH POWER AT IDLE. ALL C/P INDICATIONS NORMAL. NOMar 24, 2013 · N519AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2013032194235Floorbeam · damagedAFT CARGO COMP CARGO FLOORBEAM HOLED ON UPPER FLANGE STA NR 765 & RBL 8.10. REPAIRED CARGO FLOORBEAM IAW SRM 53-00-53, REPAIR 4.Mar 21, 2013 · N519AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2013030594214Floor Panel · damagedAFT CARGO FWD OF DOOR FLOOR PANEL REPAIR DOUBLER MISSING RIVET AND CORNER DAMAGED. ACCOMPLISHED E.A 800-25EA-9885.Mar 5, 2013 · N519AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2013012693746Warning Light · false activationCONT CABIN AMBER ZONE TEMP LIGHT ILLUMINATED, MASTER CAUTION RESETS LIGHT. PERFORMED BITE CK ON NR 1& NR 2 ZONE TEMP CONTROL. NR 2 SHOWED TRIM VALVE FAULT RESET CONTROLLER, NO FAULT, GROUND VERIFICATION TEST OK IAW AMM 21-61-00-700-806-002.Jan 26, 2013 · N519AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013012493742Control Valve · malfunctionedRT PACK LIGHT ILLUMINATED. MASTER CAUTION RESET EXTINGUISHED LIGHT IAW QRH 2.7. ACFT GROUNDED. NR 2 TEMP CONTROLER SHOWS THIS PACK-TCV FAULT. R & R NR 2 TEMP. CONT VALVE REF AMM 21-51-10-000-801. LK & OPS CKD GOOD. BITE TEST PASS REF AMM 21-61-00-700-8Jan 24, 2013 · N519AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013010493623Warning Light · illuminatedON RECALL, RT PACK LIGHT ILLUMINATES, GOES OUT WHEN RESET. ACCOMPLISHED BITE TEST OF RT TEMP CONTROLLER IAW PLACARD ON FRONT PANEL. RESET TCV FAULT AND BITE TEST GOOD. NO LIGHT ILLUMINATES ON RECALL.Jan 4, 2013 · N519AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012120393401Warning Light · false activationFMC DISAGREE MESSAGE DISPLAYED DURING TAXI. ACFT GROUNDED. FOLLOWED QRH PROCEEDURE AND FMC DISAGREE WAS CLEARED.Dec 3, 2012 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012112393353Warning Light · false activationON TAXIOUT RECEIVED A FMC DISAGREE. ACCOMPLISHED FMC FAIL QRH PROC AND IT RETURNED TO NORMAL.Nov 23, 2012 · N519AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012111693310Indicator · false indicationUPPER MFD FUEL QUANTITY RT SIDE AND TOTAL FUEL, INTERMITENTLY DISAPPEAR AND REAPPEAR. C/W FIM 28-41 TASK 813 NO FAULTS FOUND & FQIS BITE PASS.Nov 16, 2012 · N519AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2012101993157Regulator · failedON PUSHBACK, NOTICED BLEED AIR VALVE LT CB POPPED P64 A7. ACFT GROUNDED. CONFIRMED FAULT WITH CIRCUIT BREAKER. RESET BREAKER IAW AMM 20-60-01-860-801. R & R NR 1 BLEED AIR REGULATOR IAW AMM 36-11-03-000-801 AND 36-11-03-400-801. LEAK AND OPS CHECK PERFORMEOct 19, 2012 · N519AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2012101993156Circuit Breaker · trippedOPEN CIRCUIT BREAKER FOUND ON PREFLIGHT P6-4 (A) BLEED AIR VALVES LEFT. RESET BREAKER REF AMM 20-60-01-860-801, BREAKER REMAINS CLOSED. NO DEFECTS NOTED.Oct 19, 2012 · N519AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2012101593116Autothrottle Sys · malfunctionedON CLIMB OUT, AUTO THROTTLE DISENGAGED & WOULD NOT RESET. CYCLED AUTO THROTTLE SYS. AUTO THROTTLES OPS CHECKED GOOD WITH CURRENT STATUS TEST, AUTO THROTTLES TEST, REPLACE TEST IAW BITE GROUP 35, AND HGS MM 34-36-00.Oct 15, 2012 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012100793038Modulating Valve · faultedAFTER ENGINE START, RECALLED PUSHED, CONTROL CABIN-ZONE TEMP ILLUMINATED. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE, NR 1 CONTROLLER, NO FAULTS. CONTROLLER NR 2 HAS TWO FAULTS. V 143 & V141. CLEARED V143. FOUND RT PACK FAULTING THE TEMP CONTROL VALVE. Oct 7, 2012 · N519AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012100192984Controller · failedRT PACK LIGHT ILLUMINATED ON RECALL, EXTINGUISHED WITH MASTER CAUTION RESET INDICATION, FAILURE OF PRIMARY CONTROLLER. PERFORMED BITE CHECK REF FIM TASK 21-53-00-810-810, CHECKED GOOD.Oct 1, 2012 · N519AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012090492826Indicator · inoperativeNR 1 FUEL GAUGE IN REFUELING PANEL ON WING INOPERATIVE. VERIFIED DISCREPANCY NR 1 REFUEL QTY INDICATOR INOPERATIVE. REMOVED & INSTALLED NR 1 TANK REFUEL IND REF MM 28-41-61-00-801 AND 28-41-61-400-801. PERFORMED OPS CHECKED IAW MM 28-41-61-00-801 AND 28-41-Sep 4, 2012 · N519AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2012081592724Circuit Breaker · malfunctionedAUTOTHROTTLE INOPERATIVE. ACFT GROUNDED. CYCLED AUTOTHROTTLE CIRCUIT BREAKER. AUTOTHROTTLES OP CHECKED NORMAL. THROTTLE TESTS, REPLACE TEST IAW BITE GROUP NR 35, & HGS SMM 34-36-00.Aug 1, 2012 · N519AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012070592501Exciter · failedAPU FAULT LIGHT ILLUMINATED ON START ATTEMPT. WAITED 5 MIN, FAULT LIGHT EXTINGISHED ATTEMPTED SECOND START, FAULT LIGHT ILLUMINATED AGAIN. R & R APU IGNITION UNIT, IGNITER PLUG, AND IGNITION LEAD IAW AMM 49-41-31, 49-41-51 AND 49-41-52. PERFORMED APU STARTIJul 5, 2012 · N519AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2012072592592Indicator · inoperativeNR 2 TANK GAUGE INOPERATIVE. R & R NR 2 MAIN TANK REFUEL QUANTITY INDICATOR. OPS TEST GOOD REF AMM 28-41-61-400-801.Jul 2, 2012 · N519AS · Boeing 737890 · Fuel Indicating System
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