N513AS

Service difficulty reports · 437

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 = 'N513AS' 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 ASAA2018060624946Seal · debondedDURING ACCOMPLISHMENT OF T/C 78472002, FOUND 21 PLATFORMS WITH DISBONDED ELASTORMER SEALS ON THE NR 2 ENGINE. ACFT GROUNDED. REPLACED THE PLATFORMS IAW T/C 78472002.Jun 6, 2018 · N513AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018060764945Stop Pin · damagedDURING ACCOMPLISHMENT OF T/C 78472002, ON THE NR 2 ENGINE, FOUND THE ELASTOMER STOP PINS ON THE RETAINING FLANGE DAMAGED. ACFT GROUNDED. REPLACED THE ELASTORMER STOP PINS.Jun 6, 2018 · N513AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018060764944Blade · damagedDURING THE ACCOMPLISHMENT OF T/C 78472002, ON THE NR 2 ENGINE, FOUND THEN NR 7 FAN BLADE AFT SHANK CU-NI COATING DAMAGE BEYOND LIMITS ON CONCAVE SIDE. ACFT GROUNDED. REPLACED THE NR 7 AND 19 BLADES.Jun 6, 2018 · N513AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018060424873Control Panel · failedAUTOTHROTTLE WILL NOT ENGAGE. ACFT GROUNDED . AUTOTHROTTLE CURRENT STATUS TEST PASSED. MULTIPLE AUTOTHROTTLE 28 VDC POWER INVERTER FAULTS LOGGED ON DIFFERENT LEGS. IAW SSM 22-31-51 VERIFIED GOOD VOLTAGE AT MCP CONNECTOR D301. REMOVED AND REPLACED MODE CONMay 31, 2018 · N513AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2018040124105Light · inoperativeTHE LIGHT ON THE VNAV BUTTON AND THE A/T ARM LIGHT ON THE MCP WERE INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED DFCS MODE CONTROL PANEL IAW AMM 22-11-34. MCP INSTALLATION TESTED GOOD IAW AMM 22-11-34. LRU REPLACEMENT TESTED FOR MCP, BITE TEST GROUP 32, TApr 1, 2018 · N513AS · Boeing 737890 · Autopilot SystemSDR ASAA2018030923809Circuit Breaker · openFORWARD LEFT WINDSCREEN OVERHEAT LIGHT ILLUMINATED. ACFT GROUNDED. IAW FIM 30-41 / 801. PERFORMED A BITE CHECK OF WINDOW HEAT CONTROL SYSTEM. LOGGED BUSS POWER FAULT, FOUND THE CIRCUIT BREAKER AT P6-12 OPEN IAW AMM 20-60-01. INSPECTED THE CIRCUIT BREAKERMar 9, 2018 · N513AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2018030923806Hf Comm · malfunctionedCAPTAIN`S AND FIRST OFFICER`S COMMUNICATION PANELS DISPLAY FAILED WHEN HF 2 IS SELECTED. ACFT GROUNDED. CYCLED THE HF 2 CIRCUIT BREAKER P6-1 D2, SYSTEM RESTORED TO NORMAL. ACCOMPLISHED HF OPS TEST IAW AMM 23-11-00-710-801. GROUND VERIFICATION TEST PASSED, NOMar 9, 2018 · N513AS · Boeing 737890 · HF Communications SystemSDR ASAA2018021923576Control Valve · failedZONE TEMP CONT CAB ILLUMINATES ON RECALL GOES OUT WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED PACK TEMP CONTROL BITE IAW FIM 21-62 TASK 801. NR 1 CONTROLLER SHOWS FLT DECK TRIM VALVE ON BITE, PREVIOUS FLT AND VERIFY. REMOVED & REPLACED THE CONTROFeb 19, 2018 · N513AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2018020423485Pump · leakingFUEL LEAK FROM THE NR 2 ENGINE. ACFT GROUNDED. ACCOMPLISHED TEST 3A AT IDLE POWER, LEAK CHECKED IAW AMM 71-00-00-700-801-F00. FOUND LEAK FROM FUEL PUMP PAD DRAIN. LEAK IS AT 38 DROPS PER MINUTE. REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-1Feb 4, 2018 · N513AS · Boeing 737890 · Engine Fuel PumpSDR ASAA2018013023335Apu · shutdownAFTER APU START, RAN FOR 2 MINUTES THEN SHUTDOWN ON ITS OWN. GROUNDED - YES. FOUND CDU CODE 49-41011, NO FLAME SHUTDOWN, STARTED APU OPS NORMAL.Jan 30, 2018 · N513AS · Boeing 737890 · APU Core EngineSDR ASAA2018011023136Lens · missingDURING A PRE-FLIGHT INSPECTION, LENS ON INTERIOR EXIT LIGHT AT SEAT 17A, MISSING. ACFT GROUNDED. REPLACED THE LENS IAW EA-19797.Jan 10, 2018 · N513AS · Boeing 737890 · Emergency LightingSDR ASAA2017122723022Satcom · malfunctionedUSED SATCOM DURING FLIGHT, RECEIVED OK, UNABLE TO TRANSMIT ON BOTH SAT 1 OR SAT 2, ATTEMPTED NUMEROUS TIMES. ACFT GROUNDED. RAN THE SYSTEM TEST IAW AMM 23-15-00, SYSTEM OP CHECKED GOOD.Dec 27, 2017 · N513AS · Boeing 737890 · Communications SystemSDR ASAA2017121622925Autoland Sys · malfunctionedDURING AUTOLAND FLARE NOSE OF A/C PITCHED LEFT RESULTING IN A TOUCHDOWN APPROX 45' LEFT OF CENTERLINE AND NOSE POINTING LEFT. ONCE MAIN GEAR TOUCHED, RIGHT RUDDER NEEDED APPLICATION TO KEEP FROM CONTINUING OFF RUNWAY. ACFT GROUNDED. ACCOMPLISHED DFCS BITE PDec 16, 2017 · N513AS · Boeing 737890 · Autopilot SystemSDR ASAA2017120622796Warning Light · false activationON DEPARTURE AUTO FAIL LIGHT ALONG WITH ALTN LIGHT ILLUM FOLLOWED QRH AND RAN PRESSURIZATION IN ALT POSITION. PRESSURE NORMAL. GROUNDED - YES. FOUND "CABIN RATE HI" FAULT LOGGED ON #1 CPC. PERFORMED BITE TEST PER B737-800 AMM TASK 21-31-00-700-802 GND BITE TESDec 6, 2017 · N513AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2017112722765Bulkhead Web · crackedREF LP #11707357, R/H W/W FWD BULKHEAD PRESSURE DECK APPROX STA 663.75 WL 195 RBL 41 HAS CRACK IN ALUMINUM WEB. GROUNDED - YES. ACCOMPLISHED A CATEGORY "B" REPAIR ON R/H W/W FWD BULKHEAD PRESSURE DECK APPROX STA 663.75 WL 195 RBL 41 IAW 737-800 SRM 57-10-10-2RNov 27, 2017 · N513AS · Boeing 737890 · Fuselage Main, BulkheadSDR ASAA2017111822622Warning System · false activationRIGHT FWD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED AT FL380 SWITCH PLACED IN OFF POSITION FOR 5 MINUTES. WHEN PLACED TO ON POSITION NORMAL OPS. GROUNDED - YES. ACCOMPLISHED WHCU BITE, NO CURRENT FAULTS. HISTORY SHOWED NUMEROUS REPEATS ON WINDOW HEAT SENSOR FAIL.Nov 18, 2017 · N513AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017100822150Display · failedISFD FAILURE DURING CLIMB OUT. SHOWED A TURNING DECENT. ACFT GROUNDED. REMOVED AND REPLACED ISFD IAW AMM 34-24-02-400-801. OPS TESTED NORMAL.Oct 8, 2017 · N513AS · Boeing 737890 · Attitude and Direction Data SystemSDR ASAA2017100722141Connector · looseDURING TROUBLESHOOTING, FOUND THE NR 2 ENGINE CONNECTOR DP0803 TO BE LOOSE. ACFT GROUNDED. REMOVED, INSPECTED, CLEANED, INSTALLED, AND TESTED THE CONNECTOR DP0803. ALL TESTS PASSED.Oct 7, 2017 · N513AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2017100722140Wire Harness · damagedNR 1 ENGINE FILTER BYPASS LIGHT ILLUMINATED. ACFT GROUNDED. IAW WDM 73-31-11 WHILE SHAKING DOWN HARNESS NEAR DP0803 NR 1 ENG FUEL FILTER BYPASS LIGHT ON P5-2 FLICKERS ON & OFF. ACCOMPLISHED EEC TEST FOR THE NR 1 ENGINE, FOUND 73-31071. REMOVED, REPLACED ANDOct 7, 2017 · N513AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2017100522129Pump · failedCENTER, RIGHT FUEL PUMP SHOWING LOW PRESSURE, CTR TANK SHOWS 2340 LBS. ACFT GROUNDED. REMOVED AND REPLACED THE FUEL PUMP IAW AMM 28-22-41. OPS CHECKED FAILED. HAS A HUMMING SOUND. NO VISIBLE DEFECTS NOTED ON CONNECTOR OR WIRING. PRIMMED THE BOOST PUMP IAW Oct 5, 2017 · N513AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2017100122111Pump · failedDURING PREFLIGHT, RIGHT CENTER TANK FUEL BOOST PUMP LOW PRESSURE LIGHT REMAINS ILLUMINATED WITH PUMP SWITCH ON. ACFT GROUNDED. ACCOMPLISHED A BOOST PUMP REMOVAL AND REPLACEMENT IAW AMM 28-22-41-000-801, AND AMM 28-22-41-400-801. ACCOMPLISHED AN OPS TEST IAOct 1, 2017 · N513AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2017100122083Warning Light · false activationRIGHT FWD WINDOW OVERHEAT LIGHT ILLUMINATED. TURNED SWITCH OFF FOR 5 MINUTES IAW QRH. OPS NORMAL AFTER TURNING BACK ON. ACFT GROUNDED. ACCOMPLISHED WINDOW HEAT SYS. OPS TEST & BITE TEST OF RT FWD WINDOW HEAT CONTROL UNIT. SYS OPS TESTED GOOD & NO FAULTS DETECOct 1, 2017 · N513AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017092622059Control Unit · failedOVERHEAT LIGHT ILLUMINATED ON RIGHT SIDE WINDOW HEAT. RAN QRH PROCEDURE. LIGHT EXTINGUISHED. CONTINUED NORMAL OPS. ACFT GROUNDED. PERFORMED WHCU BITE IAW FIM 30-41, TASK 801. FOUND WHCU LRU AND WINDOW POWER FAULTS IN FAULT HISTORY. REMOVED AND REPLACED THE RSep 26, 2017 · N513AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017090921875Attach Fitting · looseL1 DOOR RELEASE LATCH STUCK WITH DOOR OPEN. ACFT GROUNDED. LUBRICATED THE L1 DOOR HOLD OPEN LATCH, BUT STILL STICKS. A LOUD POP WHILE CLOSING DOOR FROM UPPER HINGE AREA. L1 DOOR GUIDE ARM ATTACH FITTING LOOSE. TORQUED THE FITTING. NO MORE POPPING IAW CMM 52Sep 9, 2017 · N513AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2017090321796Warning Message · false activationON SHORT FINAL, RIGHT SIDE WINDOW OVERHEAT ILLUMINATED. PERFORMED THE QRH. TURNED AFFECTED WINDOW HEAT OFF (RIGHT SIDE WINDOW) WAITED 5 MINUTES & TURNED AFFECTED WINDOW HEAT ON. OVERHEAT LIGHT STAYED EXTINGUISHED. ACFT GROUNDED.Sep 3, 2017 · N513AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017081521648Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL. THE LIGHT EXTINGUISHED ON MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED FIM 21-62, TASKS 848, & 801. NO FAULTS FOUND.Aug 15, 2017 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017081121626Start Valve · failedAFTER STARTING ENG NR 2, START VALVE SWITCH TRIPPED OFF BUT START VALVE OPEN LIGHT REMAINED ILLUMINATED. PERFORMED QRH PROCEDURE AND VALVE REMAINED OPEN. CB VERIFIED IN. GROUNDED - YES. REMOVED NR 2 ENG START VLV REF AMM 80-11-030-000-801-F00. INSTALLED START Aug 11, 2017 · N513AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2017072221439Motor · failedON DEPARTURE NEITHER YOKE WOULD WORK, REFERENCED QRH, AUTOPILOT WAS ENGAGED AND AUTOPILOT TRIM WOULD NOT WORK. RAN QRH AND LANDED UNEVENTFULLY. ACFT GROUNDED. VERIFIED TRIM MOTOR INOP NO C.B.'S OUT, REMOVED & REPLACED STAB TRIM MOTOR AMM 24-41-71 PULLED & RESJul 22, 2017 · N513AS · Boeing 737890 · Stabilizer Control SystemSDR ASAA2017071721423Valve · failedAPPLIED TAKEOFF POWER, LEFT PACK BLEED TRIPPED OFF LIGHT ILLUMINATED. LOW SPEED 10KTS, ABORTED, PULLED OFF RUNWAY. COMPLETED BLEED TRIP OFF QRC. CALLED MAINTENANCE CONTROL, RETURNED TO GATE. ACFT GROUNDED. ACCOMPLISHED FIM 36-10 TASK 811. FOUND THE LT HIGH Jul 17, 2017 · N513AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2017071521390Valve · faultedAPU FAULT LIGHT ON ATTEMPTED START. STAYED ILLUMINATED, NO RESTART ATTEMPTED. ACFT GROUNDED. REMOVED AND REPLACED APU SHUTOFF VALVE IAW AMM 28-25-02, APU OPS CHECKED GOOD AND APU CURRENT STATUS SHOWS NO FAULTS. VERIFIED INSTALLED APU SHUTOFF VALVE.Jul 15, 2017 · N513AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2017070721321Warning Light · false activationDURING A BLEEDS OFF TAKEOFF, LEFT BLEED TRIP OFF LIGHT ILLUMINATED. RAN QRH BLEED TRIP OFF CHECKLIST, LIGHT EXTINGUISHED. CABIN PRESSURIZATION NORMAL AND NO DUCT PRESSURE SPLIT. ACFT GROUNDED. PERFORMED FIM 36-10 TASK 801 BLEED TRIP OFF CAN COME ON IF BLEED Jul 7, 2017 · N513AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2017060921001Actuator · failedRIGHT PACK LIGHT ILLUMINATED INFLIGHT, WOULD NOT COOL DOWN. SHUTOFF PACK IAW QRH PROCEDURES. ACFT GROUNDED. CONFIRMED FAULT, RT PACK-ZONE TEMP CONTROLLER BITE TEST SHOWS HARD FAIL FOR THE RT RAM AIR ACTUATOR, WOULD NOT RESET. LT PACK-ZONE TEMP CONTROLLER SHOJun 9, 2017 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017060820980Control Valve · faultedCONTROL CABIN ZONE TEMP ILLUMINATES ON MASTER CAUTION RECALL, EXTINGUISHES ON RESET. ACFT GROUNDED. CONFIRMED FAULT, RT PACK - ZONE TEMP CONTROLLER BITE SHOWS HARD FAIL FOR FLIGHT DECK TCV. REMOVED & REPLACED TCV (V143) IAW AMM 21-61-21, LEAK & GROUND FUNCTIOJun 8, 2017 · N513AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017052420872Engine · hung startNR 1 ENGINE HUNG START. FUEL FLOW AND EGT NORMAL. HUNG 45% N2. ACFT GROUNDED. PERFORMED FIM TASK 74-21, TASK 806, NO FAULTS NOTED. PERFORMED FIM TASK 73-00, TASK 801. NO DEFAULTS. NO RECENT FAULTS. NO FAULT HISTORY. PERFORMED NR 1 ENGINE RUN FOR 5 MINUMay 24, 2017 · N513AS · Boeing 737890 · Ignition Harness (Distribution)SDR ASAA2017041820480Control Panel · failedATTEMPTED TEST CALL ON SAT 1 & SAT 2. WE COULD HEAR DISPATCH BUT THEY COULD NOT HEAR US. ACFT GROUNDED. REMOVED AND INSTALLED A NEW SATCOM TRANSFER PANEL IAW AMM 23-15-00. PERFORMED SYSTEM TEST IAW AMM 23-15-00-730-801, SYSTEM CHECKED NORMAL. PERFORMED HF OPApr 18, 2017 · N513AS · Boeing 737890 · Communications SystemSDR ASAA2017041720474Transceiver · malfunctionedUNABLE TO RECEIVE VOICE COMMS ON SAT 1 OR 2. CALLING PARTY COULD HEAR US, BUT WE COULDN'T HEAR THEM. ACFT GROUNDED. UNABLE TO DUPLICATE. REMOVED, REPLACED, AND TESTED SATCOM TRANSCEIVER IAW AMM 23-15-00. TEST PASSED. ETOPS SIGNIFICANT SYSTEM GROUND VERIFICATApr 17, 2017 · N513AS · Boeing 737890 · Communications SystemSDR ASAA2017041620472Fmc · malfunctionedFMC DISAGREE AFTER LANDING. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC OPS RESTORED NORMAL.Apr 16, 2017 · N513AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017033020300Control Valve · failedDURING CLIMBOUT ABOVE FL 200, THE RT PACK LIGHT ILLUMINATED. SUCCESSFULLY RESET SEVERAL TIMES ONLY TO HAVE LIGHT ILLUMINATE AGAIN WITHIN TWO MINUTES. ONCE AT CRUISE ALTITUDE, IAW QRH, TURNED THE RT PACK OFF WITH ISOLATION VALVE CLOSED. ACFT GROUNDED. ACCOMMar 30, 2017 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017031120117Satcom · malfunctionedUNABLE TO RECEIVE AUDIO TRANSMISSIONS ON SATCOM 1 OR 2. COULD TRANSMIT. ACFT GROUNDED. RESET SYSTEM, OPS CHECKED GOOD IAW AMM 23-15-00-730-801.Mar 11, 2017 · N513AS · Boeing 737890 · Communications SystemSDR ASAA2017022019885Lens · brokenFWD ENTRY FLOOR LIGHT BY L1 DOOR LENS BROKEN. ACFT GROUNDED. REPLACED THE LENS.Feb 20, 2017 · N513AS · Boeing 737890 · Emergency LightingSDR ASAA2017012519551Pin · brokenL1 DOOR WOULD NOT OPEN. HANDLE ROTATED AND DOOR CAME IN BUT WOULD NOT TURN AND OPEN OUT. OPENED AFTER ABOUT 5 MINUTES WITH CAPTAIN ON INSIDE AND MECHANIC ON THE OUTSIDE WORKING THE DOOR FREE. ACFT GROUNDED. FOUND THE L1 DOOR GUIDE PIN MOUNT BROKEN OFF. REJan 25, 2017 · N513AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2017010519397Floorboard · corrodedFWD PIT NR 1 FLOORBOARD 120AF IS CORRODED. GROUNDED - YES. FABRICATED NEW FLOOR PANEL IAW SRM 51 30 01 0G 0 AND 51 30 05 0G 0 W 2.5 O. 071 R 0 L 20 D .071.Jan 5, 2017 · N513AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2017010419398Skin · crackedLEFT HORIZONAL STAB LOWER SKIN CARCKED AT HSS 111.1, 11 INCHES FROM T/E. ACFT GROUNDED. REPAIRED IAW SRM 55-10-01-2R-11 REP 11.Jan 4, 2017 · N513AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2016123119194Warning System · false activationLEFT PACK ILLUMINATED. RESET WITH MASTER CAUTION. GROUNDED - YES. LT PACK LOGGED TCV FAULT LAST FLIGHT. PERFORMED B737-800 FIM 21-62 TASK 830 & FAULT CLEARED. GROUND FUNCTIONAL CHECK GOOD.Dec 31, 2016 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016121619054Radio · inoperativeNR 1 HF RADIO INOPERATIVE. ACFT GROUNDED. VERIFIED THE NR 1 HF HAS POWER CIRCUIT BREAKERS. ACCOMPLISHED GROUND VERIFICATION OF NR 1 HF SYSTEM. TRANSMIT AND RECEIVE WAS NORMAL IAW AMM 23-11-21. NO HISTORY 60 DAYS.Dec 16, 2016 · N513AS · Boeing 737890 · HF Communications SystemSDR ASAA2016121519065Solenoid · faultedUSED ENGINE ANTI ICE DURING DECENT AND LANDING. ON LANDING NOTICED A NR 1 ENGINE COWL VALVE OPEN LIGHT APPEARED BURNED OUT. REPLACED THE BULBS DID NOT FIX, LIGHT WOULD NOT TEST. ACFT GROUNDED. REMOVED AND REPLACED THE LEFT GROUND WING THERMAL ANTI-ICING SOLENODec 15, 2016 · N513AS · Boeing 737890 · Airfoil Anti/De-ice SystemSDR ASAA2016121219017Control Valve · faultedLEFT PACK LIGHT ON, AFTER AFTER START FLOW LIGHT GOES OUT AFTER MASTER CAUTION. ACFT GROUNDED. TROUBLE SHOOTING COMMENTS CALL OUT THE LT TEMP CONTROL VALVE AND THE AFT ZONE TRIM MODULATING VALVE. THE BITE ON NR 1 TEMP CONTROLLER CALLS OUT THE LH TEMP CONTROLDec 12, 2016 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016121119011Hinge · dirtyFLIGHT ATTENDANT REPORTS L1 DOOR IS VERY DIFFICULT TO OPEN & CLOSE. GROUNDED - YES. CLEANED/LUBRICATED L1 DOOR HINGES. OPS CHECK NORMAL, REF AMM 52-11-00.Dec 11, 2016 · N513AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2016120418927Autothrottle Sys · malfunctionedAUTOTHROTTLES INOPERATIVE. CIRCUIT BREAKER IS IN. ACFT GROUNDED. VERIFIED CIRCUIT BREAKER. ACCOMPLISHED AUTOTHROTTLE OPS TEST, PASSED, IAW AMM 22-31-00/501, AND 22-0-01-730-801.Dec 4, 2016 · N513AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016100818231Warning Light · illuminatedLEFT PACK LIGHT ILLUMINATED ON RECALL AND DID EXTINGUISH WHEN MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED PACK TEMP CONTROL BITE IAW FIM 21-62 TASK 801, ZONE TEMP CONT NR 1 FAULTED TCV AND ZONE TEMP CONT #2 FAULTED ZONE TRIM VALVE, CLEARED BOTH FAULTS ROct 8, 2016 · N513AS · Boeing 737890 · Cabin Cooling System
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