N419AS
Service difficulty reports · 294
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 = 'N419AS' 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 = 'N419AS' 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 ASAA2019022828422Actuator · faultyLT PACK LIGHT ON /ON RECALL. GROUNDED - YES. REMOVED AND REPLACED LEFT PACK RAM AIR INLET ACTUATOR. OP'S CK GOOD REF AMM 21-51-21-000-801 AND 21-51-21-400-801. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST ON NR 1 AND NR 2 CONTROLLERS OP'S CK GOOD NO FAULTSSDR ASAA2019012727963Control Valve · failedRIGHT PACK LIGHT ILLUMINATED. WILL NOT RESET. GROUNDED - YES. REF AMM 21-61-00, ZONE TEMP CONT 2, ACCOMPLISHED PACK/ZONE TEMP CONT BITE TEST TWICE AND FAULTED THE PRIMARY TEMP CONT VALVE. ACCOMP GVI OF AIR COND BAY AND INSP HEAT EXCH FOR BLOCKAGE. ALL CKD GOODSDR ASAA2019012527927Actuator · failedCLIMBING THROUGH 9000 FT ON DEPARTURE FROM JFK RIGHT "PACK" LIGHT ILLUMINATED. FOLLOWED QRH 2.12. LIGHT EXTINGUISHES WITH RECALL RESET. ALSO BLUE "RAM DOOR FULL OPEN" LIGHT ON RIGHT SIDE ILLUMINATED ABOUT THE SAME TIME AS PACK LIGHT. REMAINED ON ENTIRE FLIGHT.SDR ASAA2018123177610Warning Light · false activationL PACK LIGHT ILLUMINATED ON GROUND. RESET WITH TRIP RESET BUTTON. GROUNDED - YES. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST BOTH CONTROLLERS REF B737-900 AMM 21-61-00-700-806-002 NUMEROUS TIMES, OPS CK NML, NO FAULTS NOTED.SDR ASAA2018122097479Warning Light · false activation#2 PACK LIGHT ILLUMINATED. GROUNDED - YES. FOUND RIGHT PACK TRIP. ACCOMPLISHED B737-900 FIM 21-53 TASK 802. RIGHT PACK LIGHT RESET & OPS CHECK NORMAL.SDR ASAA2018120127167Warning System · false activationON MASTER CAUTION RECALL, RIGHT PACK LIGHT ILLUMINATED WHEN MASTER CAUTION RESET PRESSED, THE RT PACK LIGHT EXTINGUISHED. GROUNDED - YES. PERFORMED RT PACK/ZONE TEMPERATURE CONTROLLER BITE TEST, NO FAULTS NOTED REF AMM CH 21-51-00-700-803.SDR ASAA2018112727131Warning System · false activationHF1 RADIO CONTROL PANEL DISPLAYS "FAIL". GROUNDED - YES. COULD NOT DUPLICATE, TRANSCEIVER BITE CK GOOD, FAIL MESSAGE NO LONGER PRESENT, RECEPTION ON MULTIPLE FREQUENCIES. SYS CKS GOOD PER AMM 23-11-00, GND VERIFICATION SUCCESSFUL.SDR ASAA2018111126861Compressor · stalledAPU COMPRESSOR STALLS OR SURGES ABOUT EVERY 5 MINUTES WITH LT PACK RUNNING. GROUNDED - YES. REPLACED APU PER ASA T/C 78349010.SDR ASAA2018102926657Warning System · false activationAFTER ENGINE START ON MASTER CAUTION RECALL THE LT PACK LIGHT ILLUMINATED AND EXTINGUISHED DURING MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST. NR 2 CONTROLLER TEST PASSED NO FAULTS NOTED. NR 1 CONTROLLER SHOWED 1 FAULSDR ASAA2018092625258Circuit Breaker · trippedGND SERV DC HOT BAT C/B IS POPPED. GROUNDED - YES. FOUND GRND SER DC HOT BATT C/B ON P6-4 OUT. NO PREVIOUS HISTORY. ACCOMPLISHED C/B RESET PROCEDURE REF B737-900 AMM 20-60-01. NO DEFECTS NOTED. CLOSED C/B AND OPS GOOD REF AMM 24-34-00-00-710.SDR ASAA2018092546235Control Valve · failedRIGHT HAND PACK LIGHT ILLUMINATED ON RECALL EXTINGUISHED WHEN MASTER CAUTION PRESSED. GROUNDED - YES. #2 CONTROLLER BITE TEST REF B737-900 AMM 21-61-00 SHOWS "THIS PACK TCV". ACCOMPLISHED B737-900 FIM 21-62 TASK 831 RIGHT TEMPERATURE CONTROL VALVE FAULT ISOLATSDR ASAA2018091926191Warning System · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL. RESET WITH SECOND PUSH. GROUNDED - YES. ACCOMPLISHED CABIN ZONE TEMP CONTROLLER BITE REF FIM 21-62 TASK 801. NR 2 CONTROLLER SHOWS "TEMP CONTROL VALVE" FAULT LAST LEG. ACCOMPLISHED VERIFY AND CLEARED FAULT. RIGHT PACK OPSDR ASAA2018091026065Connector · disconnectedRT SIDE PITOT OVERHEAT ANNUNCIATOR ILLUMINATES WHEN PITOT HEAT IS ON. GROUNDED - YES. FOUND RT SIDE WINDOW OVERHEAT ON UPON ARRIVAL, PITOT HEAT HAS NO "OVERHEAT" LIGHT. FOUND COIL CORD DISCONNECTED AT AIRCRAFT SIDE. RECONNECTED CONNECTOR SECURELY. OPS CHECK OFSDR ASAA2018090425983Warning System · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL AND RESETS W/MC RESET. GROUNDED - YES. RIGHT TEMP CONTROLLER SHOWS "THIS PACK -TCV" RED LIGHT ILLUMINATED. PERFORMED FIM 21-62 TASK 831. BITE TEST/VERIFY AND RESET PER FIM 21-62 TASK 801.SDR ASAA201808205846Tee Fitting · leakingFUEL DRIPPING FROM TEE FITTING ON THE FUEL LINE FROM THE APU FUEL CONTROL UNIT TO FUEL MANIFOLD. ACFT GROUNDED. REPLACED FUEL FLOW DIVIDER TEE, LEAK CHECKED GOOD.SDR ASAA2018080425670Warning Light · false activationAFTER START OF BOTH ENGINES. ON RECALL, SPEED TRIM FAIL LIGHT ILLUMINATED. OFF ON RESET. ACFT GROUNDED. ACCCOMPLISHED DFCS BITE LIBRARY NT 33 & 34, PSEU SHOWS NO CURRENT FAULTS. RESET THE CIRCUIT BREAKER MACH TRIM AC & DC AT P6-2, FCC DC CB AT P6-2.SDR ASAA2018073025570Warning System · false activationRIGHT PACK ILLUMINATES ON RECALL. GROUNDED - YES. PERFORMED FIM 21-62 TASK 801, PACK TEMP CONTROL BITE. CLEARED FAULT, RIGHT PACK LIGHT NO LONGER ILLUMINATES ON RECALL.SDR ASAA2018072525532Connector · disconnectedIN CRUISE R2 WINDOW OVERHEAT LIGHT ILLUMINATED. PER QRH PROCEDURE IT DID NOT RESET AFTER 5 MIN COOL DOWN. HOWEVER, LATER, FOUND CONNECTOR POWER FOR THAT WINDOW DISCONNECTED. WE DID NOT TURN THE WINDOW ON AGAIN. GROUNDED - YES. RECONNECTED R2 WINDOW COIL CORD RSDR ASAA2018070325293Floor Support · brokenMAIN CABIN FLOOR SUPPORT PANEL BREAK AT STA 540 LBL24-45 IS BROKEN. GROUNDED - YES. REMOVED AND REPLACED SUPPORT PANEL BREAK AT STA 540 LBL 24-45 IAW SRM 51-40-02 AND BAC DWG 143A0060 REV A.SDR ASAA2018071225358Transition Panel · corrodedAFT CARGO COMPT LT SIDE TRANSITION PANEL HAS CORROSION NUMEROUS PLACES BETWEEN BS727F AND BS727I+10. GROUNDED - YES. BLENDED CORROSION FROM ZEE CHANNEL LT SIDE FROM BS 727F TO 727I+10. FROM BS727H TO 727I+10 ORG MAT .040, .006 REMOVED .034 REMAINS, FOUND TO BESDR ASAA2018071225357Transition Panel · corrodedAFT CARGO COMPT RT SIDE TRANSITION PANEL HAS CORROSION NUMEROUS PLACE AS MARK BETWEEN BS727 AND 727C. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ORIG THICKNESS .040 REMOVED .007 REMAINING THICKNESS .033 IAW SRM 53-00-53-1A-2 & DWG BAC 1496-377SDR ASAA2018062925294Floor Support · gougedMAIN CABIN AFT WET AREA PANEL BREAK AT STA 950 RBL 23-RBL 16 HAS A GOUGE. GROUNDED - YES. REMOVED GOUGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1. REMOVED AND REPLACED FLOOR PANEL SUPPORT IAW SRM 51-40-02 AND BAC DWG 147A5650.SDR ASAA2018062825342Transition Panel · corrodedFORWARD CARGO COMPT FLOOR STRUCTURE STA 500C-500D RBL 22 TRANSITION PANEL HAS SPOTS OF CORROSION. GROUNDED - YES. BLENDED CORROSION FROM ZEE CHANNEL BETWEEN BS500C-500D RBL22 ORG MAT .040, REMOVED .006, .034 REMAINS. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53 SDR ASAA2018062625291Intercostal · crackedMAIN CABIN FLOOR STA 344-360 BL0 INTERCOSTAL CRACKED AT FASTENER (VIEWED FROM E&E COMPT). GROUNDED - YES. REMOVED INTERCOSTAL IAW SRM 51-40-02. LOCATED, DRILLED AND INSTALLED IAW BAC DW114A5400.SDR ASAA2018062625290Intercostal · crackedMAIN CABIN FLOOR STA 344-360 APPROX LBL 10 INTERCOSTAL HAS CRACK AT FASTENER (VIEWED FROM E&E COMPT). GROUNDED - YES. REMOVED INTERCOSTAL IAW SRM 51-40-02. LOCATED AND DRILLED INTERCOSTAL IAW BAC DWG 141A5400 REV-A. INSTALLED IAW BAC DWG 141A5400 REV A.SDR ASAA2018062625229Intercostal · crackedMAIN CABIN FLOOR STA 312-325 APPROX LBL 48 INTERCOSTAL CRACKED AT FASTENER (VIEWED FROM E&E COMPT). GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT STA 312-325 LBL 4B IAW SRM 51-40-02 AND BAC DWG 141A5400 REV.SDR ASAA2018062185146Start Valve · intermittentREPORTS OF #2 ENGINE START VALVE LIGHT FLICKERING AFTER ENGINE START. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE START VALVE IAW AMM 80-11-03.SDR ASAA2018061725120Connector · dirtyFOLLOWING ENGINE NR 2 START AND STARTER CUT-OUT, ENGINE NR 2 START VALVE OPEN LIGHT BEGAN FLASHING PRIOR TO STARTING ENGINE NR 1. GROUNDED - YES. REMOVED CLEANED AND REINSTALLED CONNECTOR FROM START VALVE PER FIM 80-07 TASK 809. PERFORMED ENGINE START OPS CHECSDR ASAA2018051744649Case · corrodedDURING A NR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION. CORROSION FOUND ON 17 NUT PLATES FOR THE AFT ACOUSTICAL PANELS FROM APPROX 1:30 TO 10:30 O'CLOCK POSITIONS. AROUND BOTTOM OTBD SIDE OF CASE. ALSO FOUND THE NR 5 FAN FRAME AT 5 O'CLOCK POSITION SDR ASAA2018042124344Connector · dirtyGE DIAGNOSTICS REPORTED THE NR 1 ENGINE TREND DATA SHOWS A SHIFT IN EGT HOT DAY MARGIN, ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT PRI: 2 ETOPS SIGNIFICANT SYSTEM. ACFT GROUNDED. ACCOMPLISHED EGT INDICATION SYSTEM TROUBLESHOOTING AND CONNSDR ASAA2018040124113Pump · leakingNR 2 ENGINE DEVELOPED A FUEL LEAK. ACFT GROUNDED. REMOVED THE NR 2 ENGINE HMU IAW TC N8473000. REMOVED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-11-11. REMOVED THE NR 2 ENG MAIN OIL HEAT EXCHANGER IAW AMM 79-21-02. REMOVED NR 2 ENGINE SERVO FUEL HEATER IAW AMMSDR ASAA2018032324034Gasket · leakingDURING TAXI IN, THE NR 2 ENGINE FOUND LEAKING FUEL. ACFT GROUNDED. FOUND THE NR 2 ENGINE FUEL PUMP TO HMU GASKET LEAKING. REMOVED AND REPLACED THE GASKET. LEAK AND OPS CHECKED GOOD.SDR ASAA2018022023609Pump · leakingAIRCRAFT HAS HAD 2 BTB FOR NR 2 ENGINE LEAKING FUEL WITH NFF AFTER ENGINE IS RERUN. SUSPECT FUEL PUMP AS THE SOURCE OF LEAK. SEE SL 737-SL-73-021 FOR ADDITIONAL DETAILS. GROUNDED - YES. ENGINEERING REQUEST - REMOVED AND REPLACED NR 2 ENG FUEL PUMP IAW AMM 73-1SDR ASAA2018020223378Control Valve · failedLH PACK LIGHT ILLUMINATES ON RECALL. RESETS WITH MASTER CAUTION RESET. GROUNDED - YES. PERFORMED LH PACK/ZONE TEMP CONTROLLER BITE TEST PER B737-900 AMM 21-61-00. BITE TEST REVEALED LH TEMP CONTROL VALVE FAILURE. REMOVED AND REPLACED LH TEMP CONTROL VALVE PER SDR ASAA2018012523312Fmc · failedLEFT FMC FAILED. ACCOMPLISHED QRH PROCEDURES. GROUNDED - YES. ACCOMPLISHED FIM 34-61 TASK 836. TEST PASSED.SDR ASAA2018011523164Fmc · intermittentDURING CRUISE FLIGHT, LEFT SIDE FMC INTERMITTANT VTK. ACFT GROUNDED. CREW REPORTED LEFT FMC OPERATED INTERMITTANT SEVERAL TIMES. REMOVED AND REPLACED THE LEFT FMC COMPUTER IAW AMM 34-61-02. PERFORMED INSTALL TEST STEP E. CROSSLOADED ALL SWITCHES FROM RT SISDR ASAA2018010223076Autothrottle Sys · malfunctionedAUTOTHROTTLE KICKED OFF AND WOULD NOT REENGAGE. GROUNDED - YES. RELEASED PER MEL 22-4B AUTOTHROTTLE SYSTEM INOP AND MEL 22-99B CAT III AUTOLAND NOT AUTHORIZED. REF A/T BITE B737-900 FIM 22-31 TASK 801 NO CURRENT FAULTS. LEG 01 SHOWS MESSAGE 22-31688. REF FIM 2SDR ASAA2017120622831Warning Light · false activationR1 WINDOW OVERHEAT ILLUMINATED AFTER START. RAN QRH PROCEDURES. IT EXTINGUISHED. DURING FLIGHT IT OVERHEATED AGAIN. WE RAN THE SAME PROCEDURES AND IT AGAIN EXTINGUISHED. GROUNDED - YES. VERBAL FROM CREW THE OVERHEAT HAPPENED 3 TIMES (SIG) COULD NOT DUPLICATE TSDR ASAA2017111822627Cover · out of positionF/A FOUND UNIDENTIFIED WHITE RECTANGULAR PIECE OF PLASTIC AT BACK OF AIRCRAFT. ROUGE PIECE BROUGHT UP TO FLIGHT DECK FOR FUTURE IDENTIFICATION. GROUNDED - YES. REINSTALLED LIGHT COVER FOR AFT CABIN AISLE EMERGENCY LIGHTS, OPS CHECKS GOOD COVER SECURE.SDR ASAA2017110422425Control Panel · failedFIRST OFFICER COURSE WINDOW BLANKED. COURSE ON ND WORKS NORMAL. ACFT GROUNDED. REMOVED AND REPLACED MCP IAW AMM 22-11-34-000-801 AND 22-11-34-400-801. PERFORMED MCP INSTALLATION TEST IAW AMM 22-11-34-400-801. DFCS LRU REPLACEMENT TEST FOR MCP IAW AMM 22-11-SDR ASAA2017102922365Fmc · malfunctionedRIGHT FMC FAILED AS INDICATED BY VTK FLAGS ON FIRST OFFICER'S ND AND LOSS OF LNAV / VNAV. CONDITION LASTED APPROXIMATELY 30 SECONDS AND NORMAL OPS RESTORED WITHOUT CREW INTERVENTION. ACFT GROUNDED. ACCOMPLISHED AN FMC BITE. VERIFIED LAST FLIGHT RIGHT FMC FAISDR ASAA2017102922353Light · brokenEMERGENCY LIGHT COVER CAME OFF AFT BULKHEAD. GROUNDED - YES. REF WDM 33-51-22-6, FOUND EMERGENCY LIGHT AFT LAV FLOODLIGHT MOUNTED ON AFT WINDSCREEN ADJACENT TO LAVATORY D TO BE BROKEN. REMOVED, REPLACED, AND TESTED LIGHT ASSEMBLY PER AMM 33-51-01-960-802 - OPSSDR ASAA2017101422199Pitot Tube · malfunctionedRIGHT ELEVATOR PITOT CAUTION LIGHT ILLUMINATED AFTER ENGINE START. REMAINED ILLUMINATED DURING POWER TRANSFER WITH PROBE HEAT SWITCHES IN AUTO AND ON POSITIONS. ACFT GROUNDED. R & R THE RT ELEVATOR PITOT PROBE. OPS & LEAK CHECKED NORMAL IAW AMM 34-11-01 & SDR ASAA2017082421728Regulator · failedLEFT BLEED AIR INDICATOR NEVER MOVED FROM 0 PSI CABIN TEMP SLOWLY ROSE. TEMP CONTROLLER AT FULL COLD TO REACH 30 DEG C BY END OF RUNWAY AND SUPPLY DUCTS HELD ABOUT 23 DEG C. AIR CONDITIONING RAM AIR VALVE LEFT CB P6-4 A7 POPPED. GROUNDED - YES. DURING INITIAL SDR ASAA2017081621650Warning Light · false activationELECTRIC LIGHT CAME ON DURING PREFLIGHT. ACFT GROUNDED. ACCOMPLISHED FIM 24-31, TASK 801. LIGHT WENT OUT AND NO FAULTS FOUND. OK FOR SERVICE.SDR ASAA2017080321540Regulator · failedRIGHT & LEFT BLEED DUCT PRESSURES SPLIT BY GREATER THAN 20 PSI IN CRUISE. RIGHT = 44 LEFT = 22 AT FL 340/ .79M, ENGINE BLEEDS ON, APU BLEED OFF, TAI OFF, PACKS AUTO. ACFT GROUNDED. PERFORMED BLEED SYSTEM HEALTH CHECK IAW TC NG-36WC-00001. FOUND BLEED AIR REGULSDR ASAA2017080121512Display · inoperativeF/O MCDU INOPERATIVE. ACFT GROUNDED. REPLACED F/O MCDU IAW 34-61-01-400-802 & ME-04 ASA-4190942.SDR ASAA2017072321451Display · failedFIRST OFFICER`S CDU INOPERATIVE. ACFT GROUNDED. REPLACED THE CDU IAW AMM 34-61-01, & ME-04, ASA-419-942. OPS NORMAL.SDR ASAA2017062121159Servo · failedAUTOTHROTTLE WILL NOT STAY CONNECTED. ACFT GROUNDED. CONFIRMED FAULT, AUTOTHROTTLE INOPERATIVE. CURRENT BITE & FAULT HISTORY SHOW ASM-1 FAULT MESSAGE 22-31687. REMOVED & REPLACED THE AUTOTHROTTLE ASM-1 IAW AMM 22-31-91. GROUND FUNCTIONAL CHECK NORMAL IAW AMSDR ASAA2017052920892Lamp · inoperativeL2 DOOR SLIDE LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP. LAMP TESTED GOOD IAW AMM 33-51-04-960-801.
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