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.

SDR ASAA2017052420870Duct · damagedNR 1 ENGINE ADJUSTABLE SUPPORT LINK C/T THE INTERSECTION MANIFOLD DUCT ASSEMBLY HAS A BAD LOWER ROD END BEARING. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE INTERSECTION MANIFOLD DUCT ASSEMBLY, IAW POWERPLANT BUILDUP MANUAL 71-00-02, FIG 16-1. LEAK CHMay 24, 2017 · N419AS · Boeing 737990ER · Pneumatic Distribution SystemSDR ASAA2017052420869Support · failedNR 1 ENGINE SUPPORT LINK C/T INTERSECTION MANIFOLD DUCT HAS A FAILED BEARING. ACFT GROUNDED. REMOVED AND REPLACED THE DUCT SUPPORT LINK ASSEMBLY AT MANIFOLD DUCT ASSEMBLY, JUST ABOVE AND FWD OF HIGH STAGE VALVE, IAW AMM 36-11-01-000-802, AND AMM 36-11-01-400May 24, 2017 · N419AS · Boeing 737990ER · Pneumatic Distribution SystemSDR ASAA2017052020833Fmc · malfunctionedVTK DISPLAYED INTERMITTENTLY ON BOTH ND'S WHILE BOTH CDUS BLANKED INTERMITTENTLY AS WELL AFTER LANDING. ACFT GROUNDED. ACCOMPLISHED FAULT REVIEW OF FMC LT AND RT. FOUND LEFT FMC INTERMITTENT ON GROUND. CYCLED FMC LT CIRCUIT BREAKER IAW AMM 20-60-01 AND OPERATMay 20, 2017 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2017051820829Ignition Sys · failedAPU FAILED TO START WITH A FAULT LIGHT. ACFT GROUNDED. ACCOMPLISHED AMM 49-40, TASK 802. REMOVED AND REPLACED THE IGNITION UNIT IAW AMM 49-41-31 AND IGNITER PLUG IAW AMM 49-41-51 OPS CHECKED GOOD.May 18, 2017 · N419AS · Boeing 737990ER · APU Start/Ignition SystemSDR ASAA2017051020710Autothrottle Sys · malfunctionedAUTOTHROTTLE DISENGAGED WHEN TOGA BUTTON DEPRESSED FOR TAKEOFF. ACFT GROUNDED. NO FAULTS LOGGED IN HISTORY. ACCOMPLISHED A/T OPS CHECK IAW MM 22-31-00,TEST PASSED.May 10, 2017 · N419AS · Boeing 737990ER · Autopilot SystemSDR ASAA2017050920705Control Panel · failedWEATHER RADAR DOES NOT WORK IN THE AUTO POSITION. GROUNDED - YES. CONFIRMED. REMOVED & REPLACED WEATHER PANEL, REF AMM 34-43-91. OPS NORMAL PER SAME. ETOPS GROUND VERIFICATION TEST SUCCESSFUL.May 9, 2017 · N419AS · Boeing 737990ER · Weather Radar SystemSDR ASAA2017042120505Insulation · missingSEVERAL SECTIONS OF BRAIDED SHEATH MISSING FROM NR 2 ENG CORE FIRE DETECTION HARNESS MW0325. GROUNDED - YES. REMOVED AND REPLACED MW0325 HARNESS PER AMM 26-11-02 ENG FIRE DET OPERATIONAL TEST GOOD PER AMM 26-11-00.Apr 21, 2017 · N419AS · Boeing 737990ER · Fire DetectionSDR ASAA2017031220146Fmc · malfunctionedAT FL 340, THE VTK FLAG APPEARED ON CAPTAIN`S NAVIGATION DISPLAY WITH SIMULTANEOUS BLANKING OF BOTH FMC DISPLAYS. RAN FMC FAIL QRH CHECKLIST TO RESUME NORMAL OPS. ACFT GROUNDED. KNOWN ISSUE WITH U11.0 SOFTWARE. VERIFIED BOTH FMCS ONLINE AND OPS NORMAL. NO FAMar 12, 2017 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2017022619947Lever · malfunctionedWITH AUTOTHROTTLE ARMED TOGA BUTTON PRESSED, THE NR 2 THRUST LEVER WOULD NOT MOVE & AUTOTHROTTLE WOULD NOT DISENGAGE. ACFT GROUNDED. PERFORMED OPS TEST OF AUTOTHROTTLE SYSTEM IAW AMM 22-31-00, NO FAULTS NOTED.Feb 26, 2017 · N419AS · Boeing 737990ER · Auto Throttle SystemSDR ASAA2017022119897Fmc · intermittentLOST BOTH FMC DURING CRUISE, FOR A FEW MINUTES THEN CAME BACK. LOST BOTH AT THREE DIFFERENT TIMES AND EACH TIME CAME BACK AFTER A FEW MINUTES. ACFT GROUNDED. ACCOMPLISHED FAULT REVIEW ON FMC, APPEARS TO HAVE HAD POWER INTERRUPTIONS. CURRENT STATUS IS GOOD, COFeb 21, 2017 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2017011919485Control Valve · failedDUCT PRESS SPLIT IN CLIMB AND CRUISE 18L 42 R. GROUNDED - YES. ACCOMPLISHED NR 1 ENG BLEED AIR SYSTEM HEALTH CHECK REF T/C NG-36WC-00001. REMOVED & REPLACED NR 1 ENG PRECOOLER CTRL VALVE & NR 1 ENG BAR REF MM 36-12-02 & 36-11-03. LEAK & OPS CHECKED GOOD REF MMJan 19, 2017 · N419AS · Boeing 737990ER · Pneumatic Distribution SystemSDR ASAA2017011819444Shutoff Valve · leakingDUCT PRESSURE DIFFERENTIALS EXCEEDS 20 PSI DURING CLIMB AND IN CRUISE DUCT RIGHT PSI 40 DUCT LEFT PSI 17 DUCT PRESSURES WERE MATCHED DURING DESCENTS. ACFT GROUNDED. ACCOMPLISHED FIM TASK 36-00-00-860-807. FOUND PRSOV LEAKING EXCESSIVE AIR, R & R PRSOV IAW AMJan 18, 2017 · N419AS · Boeing 737990ER · Pneumatic Distribution SystemSDR ASAA2017010319241Software · defectiveAFTER LANDING ALL FMC DATA DISAPPEARED. LEFT FMC CDU CHANGED TO MENU PAGE AND WHEN PERF INIT WAS SELECTED ONLY BLANK SQUARES WERE PRESENT. GROUNDED - YES. KNOWN ISSUE WITH U11.0 SOFTWARE. VERIFIED LT FMC ONLINE & OPS NORMAL. GROUND VERIFICATION GOOD, REF AMM 3Jan 3, 2017 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2016122619163Fmc · malfunctionedDURING DESCENT, GOT SINGLE FMC OPS SCRATCHPAD MESSAGE AND MAP FLAG FIRST OFFICERS NAV DISPLAY. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE PER QRH. FMCS RESTORED NORMAL.Dec 26, 2016 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2016120318921Sensor · faultedNR 2 ENGINE N2 SIGNAL FLUCTUATES DURING TAKEOFF, FOUND ON OIP REPORT 07. ACFT GROUNDED. PERFORMED EEC BITE NR 2 ENGINE IAW AMM 73-21-00-740-803-F00. NO FAULTS FOUND. INSPECTED N2 SENSOR HARNESS CONNECTORS DP1201, DP0506 AND DP0603. NO DEFECTS FOUND. REMOVED ADec 3, 2016 · N419AS · Boeing 737990ER · Engine RPM Indicating SystemSDR ASAA2016110718592Warning Light · false activationAFTER LANDING, INTERMITTANT VTK ON FO'S SIDE WITH ASSOCIATED AMBER FMC PRST LIGHT. ACFT GROUNDED. NO LOGGED FAULTS, SYS TESTED GOOD IAW AMM TASK 34-61-00-860-801.Nov 7, 2016 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2016092818148Support · corrodedAFT CARGO BAY RT TRANSITION PANEL IS CORRODED FROM BS 727G TO 727I RBL 21.0. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO TRANSITION PANEL IAW SRM 53-00-53. FOUND TO BE OUT OF LIMITS. REPAIRED TRANSITION PANEL IAW SRM 53-00-53-2R-5 REPAIR 5. REMOVED ASep 28, 2016 · N419AS · Boeing 737990ER · Fuselage Miscellaneous StructureSDR ASAA2016092018081Warning Light · illuminatedRIGHT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. PACK ZONE TEMP BITE CHECKS GOOD IAW FIM 21-62 TASK 848 AND FIM 21-62 TASK 801, NO FAULTS NOTED AT THIS TIME.Sep 20, 2016 · N419AS · Boeing 737990ER · Cabin Cooling SystemSDR ASAA2016092018086Slide · out of adjustL1 DOOR SLIDE DIFFICULT TO PLACE BAR INTO BRACKET. ACFT GROUNDED. REMOVED THE L1 DOOR SLIDE AND COVER IAW AMM TASK 25-66-01-000-801. ADJUSTED PACK. REINSTALLED L1 DOOR SLIDE PACK AND COVER IAW AMM TASK 25-66-01-400-803.Sep 20, 2016 · N419AS · Boeing 737990ER · Escape SlideSDR ASAA2016091618059Fmc · faultedAT CRUISE BOTH FMC SCREENS WENT BLANK WITH A BLANK NAV SCREEN AND VTK ON CAPTAIN`S DISPLAY. AFTER 10-15 SECONDS FMC DISPLAYS RETURNED TO NORMAL DISPLAY AND SHORTLY VTK MESSAGE DISAPPEARED AND NAV DISPLAY RETURNED TO NORMAL, THEN HAPPENED AGAIN. RAN CHECKLISTSep 16, 2016 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2016082717805Autothrottle Sys · malfunctionedAUTOTHROTTLES WILL NOT REMAIN ENGAGED. ACFT GROUNDED. AUTOTHROTTLE BITE CURRENT STATUS SHOWS NO FAULTS, IAW FIM 22-31 TASK 801. LEG 04 OF INFLIGHT FAULTS LOGGED FAULT MESSAGE 22-31687 ASM-1 RATE MONITOR. ACCOMPLISHED IAW FIM 22-32 TASK 819 AUTOTHROTTLE SERVO Aug 27, 2016 · N419AS · Boeing 737990ER · Auto Throttle SystemSDR ASAA2016080917662Cover · detachedVESTIBULE (L1) EMERGENCY LIGHT COVER DETACHED. ACFT GROUNDED. ATTACHED THE COVER. OPS NORMAL.Aug 9, 2016 · N419AS · Boeing 737990ER · Emergency LightingSDR ASAA2016063017213Actuator · faultedRT PACK LIGHT ILLUMINATES ON RECALL. ACFT GROUNDED. REMOVED AND REPLACED RT PACK RAM AIR DOOR ACTUATOR IAW AMM 21-51-21. ALL TESTED GOOD.Jun 30, 2016 · N419AS · Boeing 737990ER · Cabin Cooling SystemSDR ASAA2016061417042Switchpack · failedPSEU ILLUMINATED ROLLOUT, EXTINGUISHED ON TAXI. ACFT GROUNDED. BITE OF PSEU HAS NO CURRENT FAULTS. FLIGHT HISTORY IS SHOWING NUMEROUS FLIGHTS WITH MESSAGE 32-62101, LT THRUST LEVER RESOLVER ANGLE IS NOT LESS THAN 44 WHILE LANDING. REF TASKS AMM 32-09-00-810Jun 14, 2016 · N419AS · Boeing 737990ER · Auto Throttle SystemSDR ASAA2016060316940Sensor · failedLEFT SIDE WINDSHIELD HEAT, OVERHEAT LIGHT ON & NOT EXTINGUISH AFTER 2.5 MINUTES COOLING PERIOD. TURNED OFF IAW QRH. ACFT GROUNDED. CONFIRMED FAULT, CAPTAIN'S SLIDING WINDOW, PN 5610002-3, SN 12324H7354, HEAT INOPERATIVE, OVERHEAT LIGHT ON. ACCOMPLISHED FIM 3Jun 3, 2016 · N419AS · Boeing 737990ER · Windshield/Door Rain/Ice RemovalSDR ASAA2016060316932Control Valve · failedRIGHT "PACK" LIGHT ILLUMINATED DURING MASTER RECALL ON DESCENT, CHECK LIGHT EXTINGUISHES WHEN MASTER CAUTION RESET. ACFT GROUNDED. CONFIRMED FAULT, RT PACK/ZONE TEMPERATURE CONTROLLER BITE, REF AMM TASK 21-61-00-700-806-002 SHOWS HARD FAILURE, TCV NR 2, V141,Jun 3, 2016 · N419AS · Boeing 737990ER · Cabin Temperature Control SystemSDR ASAA2016032116049Sensor · failedRIGHT FWD WINDSHIELD OVERHEAT. QRH FOLLOWED, DID NOT RESET. ACFT GROUNDED. PERFORMED BITE REF AMM 30-41-11-710-801, SHOWED SENSOR FAULT RT FWD. SELECTED WINDSHIELD SENSOR SW S1079 TO POSITION NR 2. PERFORMED BITE, NO FAULT NOTED. PERFORMED WHCU SYSTEM TESTMar 21, 2016 · N419AS · Boeing 737990ER · Windshield/Door Rain/Ice RemovalSDR ASAA2016031615966Fire Loop · damagedWHILE INSPECTING NR 1 ENGINE FIRE DETECTOR LOOP FOUND MW0325 WIRE HARNESS DAMAGED. ACFT GROUNDED. R & R MW0325 HARNESS IAW AMM REF 26-11-02. OPS CHECKS GOOD.Mar 16, 2016 · N419AS · Boeing 737990ER · Fire DetectionSDR ASAA2016031415906Transmitter · failedRIGHT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED ON TAXI IN. ACFT GROUNDED. R & R NR 2 SCAVENGE FILTER REF AMM 79-21-06. NO CONTAMINATION NOTED. R & R SCAVENGE FILTER CLOGGING TRANSMITTER REF AMM 79-21-07. PERFORMED ENGINE RUN LEAK CHECK REF AMM 71-00-00,Mar 14, 2016 · N419AS · Boeing 737990ER · Turbine Engine Oil SystemSDR ASAA2016031115870Wire Harness · damagedNR 2 ENGINE BOTH LT AND RT CORE FIRE DETECTOR HARNESSES OUTER SHEATHING MISSING IN SEVERAL LOCATIONS. PN CA243-01 & CA244-01. ACFT GROUNDED. R & R NR 2 ENGINE LT AND RT CORE FIRE DETECTOR HARNESSES, REF AMM 26-11-02. OPS CHECKED NORMAL, REF AMM 26-11-00.Mar 11, 2016 · N419AS · Boeing 737990ER · Fire Protection System WiringSDR ASAA2016020215271Fmc · failedON TAKEOFF ROLL AT V1, TO VR F/O'S V SPEEDS DID NOT APPEAR ON SPEED TAPE, ONCE AIRBORNE F/O'S FLIGHT DIRECTOR WORKED. FLIGHT DIRECTOR ON F/O'S SIDE WOULD NOT WORK IN VNAV OR LNAV, BUT WORKED IN LEVEL CHANGE, VERTICAL SPEED, ALT HOLD, AND HDG SELECT. ON THE CDUFeb 2, 2016 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2016012414978Satcom · malfunctionedWHILE ATTEMPTING TO DO T/C CMPT-23E0-13295- NEW SATCOM TRANSCEIVER WOULD NOT LINK WITH ACARS DATA. ACFT GROUNDED. TRIED 2 NEW RECEIVERS WITH SAME RESULT. SUSPECT TRANSCEIVERS NOT ACTIVATED. INSTALLED ORIGINAL SATCOM TRANSCEIVER & TESTED NORMAL REF AMM 23-1Jan 24, 2016 · N419AS · Boeing 737990ER · Communications SystemSDR ASAA2015122314462Warning Message · false activationFMC PERFORMANCE DATA INVALID NEEDS REBOOT MOST LIKELY FMC DISAGREE. ACFT GROUNDED. QRH REF ACCOMPLISHED, OPS RESTORED.Dec 23, 2015 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015112613980Keyboard · malfunctionedCAPTAIN`S FMC CDU L6 KEY INOPERATIVE. ACFT GROUNDED. REPLACED LT FMC CDU KEYBOARD REF AMM 34-61-01. OPS NORMAL.Nov 26, 2015 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015112413957Control Panel · failedWINDOW ON DFCS MCP HAS LED "DOTS" IN BACKGROUND. NRS ARE READABLE. ACFT GROUNDED. R & R MODE CONTROL PANEL AMM 22-11-34. INSTALLATION TEST PASSED REF AMM 22-11-34-740-801. ACCOMPLISHED ADDITIONAL TESTING REF AMM 22-00-01 DFCS LRU INTERFACE FOR MCP, LAND VENov 24, 2015 · N419AS · Boeing 737990ER · Autopilot SystemSDR ASAA2015112313941Windshield · failedRIGHT FORWARD WINDOW OVERHEAT LIGHT ILLUMINATED. DID THE CHECKLIST AND THE LIGHT CAME BACK ON. ACFT GROUNDED. BITE CHECK OF RT FRONT WHCU FAULTS "WINDOW SENSOR" PRIMARY SENSOR FAILED. RESISTANCE CHECK OF BOTH SENSORS FAILED OPEN. RIGHT FRONT SENSOR SWITCHNov 23, 2015 · N419AS · Boeing 737990ER · Windshield/Door Rain/Ice RemovalSDR ASAA2015101313488Actuator · malfunctionedRIGHT PACK LIGHT ILLUMINATED ON RECALL DURING BEFORE LANDING CHECKLIST. PACK LIGHT EXTINGUISHED AFTER PRESSING MASTER CAUTION. ACFT GROUNDED. REMOVED RT RAM AIR ACTUATOR REF AMM 21-51-21-000-801. INSTALLED RT RAM AIR ACTUATOR REF AMM 21-51-21-400-801. ACCOMOct 13, 2015 · N419AS · Boeing 737990ER · Cabin Cooling SystemSDR ASAA2015101013413Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. THE PACK LIGHT EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED BITE IAW FIM 21-62, TASK 801. NOTED RAM AIR ACTUATOR FAULT IN PREVIOUS FLT. HIT VERIFY & RECEIVED GREEN GO LIGHTS. PEROct 10, 2015 · N419AS · Boeing 737990ER · Cabin Cooling SystemSDR ASAA2015091013025Sensor · faultedAFTER NORMAL ENGINE START USING THE APU. APU WAS SHUTDOWN, OPS NORMAL. DURING TAXI OUT FAULT LIGHT ILLUMINATED. AFTER APPROXIMATELY 5 MINS APU FAULT EXTINGUISHED. ACFT GROUNDED. PERFORMED APU BITE REF FIM 49-60, TASK 801. FOUND FAULT 49-61223 CURRENT STATUSSep 10, 2015 · N419AS · Boeing 737990ER · APU ControlsSDR ASAA2015090612921Autothrottle Sys · malfunctionedAUTOTHROTTLE DISENGAGED AND WILL NOT RE-ENGAGE. ACFT GROUNDED. ACCOMPLISHED FIM TASK 22-31, TASK 801, AUTOTHROTTLE BITE GOOD WITHOUT CURRENT FAULTS, VERIFIED ALL INTERACTIVE TESTS PASSED. NO FAULTS HISTORY FOR 30 DAYS.Sep 6, 2015 · N419AS · Boeing 737990ER · Auto Throttle SystemSDR ASAA2015082418182Floor Panel · puncturedRAMP REPORTS A SMALL HOLE IN AFT PIT FLOOR 6 FEET FWD OF PIT DOOR. ACFT GROUNDED. (RESOLVED ON W/O: 331186 TASKCARD: N/R-00007 ) REMOVED DAMAGED PANEL IAW AMM 25-52-10. FABRICATED NEW PANEL IAW BAC DWG 453A2610 AND INSTALLED IAW AMM 25-52-10-400-801.Aug 24, 2015 · N419AS · Boeing 737990ER · Fuselage Floor PanelSDR ASAA2015080712782Warning Message · false activationRECEIVED AN FMC DISAGREE MESSAGE AFTER FLAP EXTENSION. ACFT GROUNDED. RESOLVED IAW QRH.Aug 7, 2015 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015072412571Indication Sys · malfunctionedDEPARTED WITH 37,000 LBS OF FUEL, WITH ALL FUEL PUMPS ON. DURING CLIMB FUEL IMBALANCE ILLUMINATED WITH APPROXIMATELY 7,500 LBS IN NR 1 TANK, NR 2 TANK FULL, AND CENTER TANK LESS THAN 17,000 LBS. RAN QRH. ACFT GROUNDED. VERBAL FROM FLIGHT CREW AFTER REBALANJul 24, 2015 · N419AS · Boeing 737990ER · Fuel Indicating SystemSDR ASAA2015072412570Control Valve · failedCONTROL CABIN TEMP CONTROL HAD NO EFFECT ON FLIGHT DECK TEMPERATURE OFF POSITION. MAINTAINED 20 DEGREES C. NO ABNORMAL INDICATIONS ON RECALL. ACFT GROUNDED. WHILE ON DEFERRAL: FWD CABIN COMPLETELY UNRESPONSIVE IN AUTO AND MANUAL SUPPLY DUCT TEMP REMAINS ATJul 24, 2015 · N419AS · Boeing 737990ER · Cabin Temperature Control SystemSDR ASAA2015072212545Filter · dirtyDURING DESCENT CONTROL CABIN TEMP WENT FULL COLD. TEMP SELECT KNOB HAD NO EFFECT ON DUCT TEMP. SELECTING KNOB TO OFF AND TEMP ROSE RAPIDLY TO HOT TEMP 60 DEG DUCT TEMP. ACFT GROUNDED. PERFORM PACK ZONE TEMP CONTROLLER BITE TEST. NO FAULTS NOTED. RAN CONTJul 22, 2015 · N419AS · Boeing 737990ER · Cabin Temperature Control SystemSDR ASAA2015070912386Fmc · malfunctionedDATA LINK FULL, MESSAGE GROUNDED. QRH FOLLOWED FMC DISAGREE ON GROUND, MESSAGE CLEARED.Jul 9, 2015 · N419AS · Boeing 737990ER · Flight Management Computing Hardware SystemSDR ASAA2015070312308Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ARM. ACFT GROUNDED. ACCOMPLISHED A/T BITE 22-31, TASK 801. FOUND 1 FAULT IN FLT HISTORY 22-31263. PERFORMED FIM 22-31, TASK 810. NO FAULTS FOUND. PERFORMED A/T OPS CK 5X NO FAULTS LOGGED. SYS CKS NORMAL. NO HISTORY IN 30 DAYS.Jul 3, 2015 · N419AS · Boeing 737990ER · Auto Throttle SystemSDR ASAA2015042411485Warning Message · false activationFUEL IMBALANCE ANNUNCIATOR APPEARED AFTER TAKEOFF. APPROX 3 MINUTES AFTER T/O ROLL NOTICED THE IMBALANCE AND SAW 700 LB IMBALANCE. DURING NEXT FEW MINUTES NOTICED INCR TO 900 LBS, MAIN TANK1 WAS 5.9, RIGHT TANK 6.6 INITIALLY. QRH PROCEDURE BALANCED FUEL TO NORApr 24, 2015 · N419AS · Boeing 737990ER · Fuel Indicating SystemSDR ASAA2015031610983Element · failedRIGHT FORWARD WINDOW SHOWS OVERHEAT, TURNED SWITCH OFF FOR 15 MIN THEN BACK ON AND STILL SHOWS OVERHEAT. ACFT GROUNDED. PERFORMED BITE CK AND FOUND SENSOR FAULT RT FRONT WINDOW. SWITCHED POSITION OF SENSOR SWITCH AND PERFORMED WINDOW HEAT, OPS CK PERFORMED Mar 16, 2015 · N419AS · Boeing 737990ER · Windshield/Door Rain/Ice RemovalSDR ASAA2015031610980Warning Light · false activationON MASTER CAUTION RECALL CONTROLLER CAB ZONE TEMP LIGHT ILLUMINATED. EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. RESET NR 2 CONTROLLER FLT DECK TRIM VALVE FAULT. BITE TEST PASS IAW MM 21-61-00. GROUND VERIFICATION SUCCESSFUL.Mar 16, 2015 · N419AS · Boeing 737990ER · Central Warning
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