N589AS

Service difficulty reports · 447

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 = 'N589AS' 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 ASAA2013071195563Fmc · unknownFMC DISAGREE. ACFT GROUNDED. PERFORMED QRH PROCEDURE. FMC DISAGREE NO LONGER DISPLAYED.Jul 11, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013070995533Fmc · false indicationFMC DISAGREE MESSAGE AFTER ENGINE START. ACFT GROUNDED. CLEARED AFTER FOLLOWING QRH.Jul 9, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013060495031Probe · out of limitsDIAGNOSTICS REPORTS NR 2 ENGINE TREND DATA SHOWS A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. ACCOMPLISHED T49.5 PROBE AND EGT SYS INSPECTION. FOUND T495 S1 EGT TEMP PROBE RESISTANCE VALUES OUT OF LIMITS AMMJun 4, 2013 · N589AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2013052394895Smoke Detector · dirtyAFT CARGO FIRE LIGHT FAILS TEST. LIGHT DOES ILLUMINATE WITH GENERAL LIGHTS TEST. ACFT GROUNDED. CLEANED FIRE WARNING SENSORS IN AFT PIT. OPS CHECKS GOOD.May 23, 2013 · N589AS · Boeing 737890 · Smoke DetectionSDR ASAA2013052294874Autothrottle Sys · malfunctionedAUTOTHROTTLE DISENGAGED DURING CLIMB WITHOUT WARNING (NO A/T ANNUNCIATION ON PANEL). UPON LEVEL OFF WE GOT AN OVERSPEED CLACKER FOR APPROX 1-2 SECONDS AT MACH .80. ACFT GROUNDED. OVSPD INSP OF AIRFRAME NOT REQD IAW AMM 05-51-04-210-801, ITEM 2.G(2). CREW STAMay 22, 2013 · N589AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013052294873Switch · inoperativeAUTOPILOT B WILL NOT ENGAGE IN CMD OR CWS. ACFT GROUNDED. REF WDM 22-11-12 FOUND F/OS S232 A/P DISC SWITCH INOP. REPLACED S232 SWITCH REF MM 22-11-41, OPS CHECK NORMAL.May 22, 2013 · N589AS · Boeing 737890 · Autopilot SystemSDR ASAA2013051394807Fmc · inoperativeFMC DISAGREE ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED QRH, OPS NORMAL.May 13, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013050594711Valve · intermittentNR 1 COWL VALVE OPEN LIGHT ILLUMINATES INTERMITTENTLY WITH ENGINE ANTI-ICE SWITCH OFF. ACFT GROUNDED. REPLACED NR 1 ENG COWL TAI VALVE REF MM 30-21-11. LEAK CHECK AND OP CHECK GOOD, OK FOR SERVICE.May 5, 2013 · N589AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2013050594710Connector · unsecureLEFT BLUE COWL VALVE OPEN LIGHT FLICKERS CONTINUOUSLY WITH ENGINE ANTI-ICE SWITCH OFF IN FLIGHT. ACFT GROUNDED. RESEATED CONNECTOR PLUG ON LT ENGINE COWL TAI VALVE, SHOOK DOWN WIRE BUNDLES FOR VALVE AND FOR PANEL IN COCKPIT, NO FLICKERING NOTED. RAN ENGINE May 5, 2013 · N589AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2013042994652Fmc · failedNO FMC DATA ON F/O FMC. ACFT GROUNDED. REPLACED NR 2 FMCS COMPUTER REF MM 34-61-02-000-801 OPS CK GOOD. REM/REPL NR 2 FMCS CDU REF MM 34-61-01-000-802, OPS CK GOOD.Apr 29, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013042794621Circuit Breaker · faultedAFTER LANDING, SHUTTING DOWN NR 2 ENGINE, ACFT MAIN ELECTRICAL BUSS POWER WOULD NOT ACCEPT GROUND POWER. STARTED APU TO ESTABLISH ELECTRICAL POWER ACFT GROUNDED. FOUND CIRCUIT BREAKER MAIN BUSS 2 INSIDE P-92 PANEL OUT. RESET BREAKER, DURING TAP TEST AROUNDApr 27, 2013 · N589AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2013042694639Start Valve · failedPUSHED BACK, STARTED NR 2 ENG , NORMAL START. PERFORMED AN ISOLATE/VENTALATE PROCEDURE ON NR 2 ENG . NOTICED NR 2 ENG START VALVE OPEN AND BOTH LIGHT BELOW IT (NO WORDS) FLASHING. PERFORMED QRH 7.11 THRU STEP NR 7, SHUTDOWN ENGINE. ACFT GROUNDED. REPLACEApr 26, 2013 · N589AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2013042394607Pressure Switch · failedRT NR 2 FILTER BYPASS LIGHT CAME ON AFTER LANDING. CAPTAIN STATED IT WAS A FUEL FILTER BYPASS LIGHT. NR 2 ENG DISPLAYS MX MESSAGE 73-31072. REPLACED NR 2 ENG FUEL FILTER REF MM 73-11-02. NO DISCREPANCIES NOTED & LEAK CHECKED GOOD. INSPECTED NR 2 FILTER BYPAApr 23, 2013 · N589AS · Boeing 737890 · Engine Fuel Indicating SystemSDR ASAA2013042394606Warning Light · false activationDURING PREFLIGHT, SINGLE FMC ANNUNCIATION WITH MAP AND VTK ANNUNCIATION OF F/OS ND. PERFORMED FIM TASK 34-61 TASK 836. RT FMC FUNCTIONS NORMAL. GROUND VERIFICATION SUCCESSFUL. NO CURRENT FAULTS.Apr 23, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013041394462Display · malfunctionedNR 1 FUEL QTY INDICATOR AND TOTAL QTY INDICATOR WENT BLANK FOR APPROX 5 SECONDS 2 TIMES DURING FLIGHT. ON ARRIVAL AT GATE, FUEL QTY DISPLAYS NORMAL. ACCOMPLISHED FQIS BITE PROCEDURE IAW FIM 28-41, TASK 813 AND TASK 801. CURRENT STATUS SHOWS NO FAULTS AND TESTApr 13, 2013 · N589AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2013040794386Start Valve · inoperativeAFTER PUSH BACK ATTEMPED TO START ENG NR 2 WITH SWITCH IN GROUND NO N2 OR N1 OR OTHER IND THAT STARTER WAS ROTATING ENG. RAN ENGINE FOUND START VALVE INOPERATIVE, REPLACED START VALVE ON NR 2 ENGINE REF AMM 80-11-03. GROUND VERIFICATION CHECK SUCCESSFUL ACFTApr 7, 2013 · N589AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2013040494332Fuel Nozzle · failedAPU CT5ATP EGT TREND DATA SHOWS EGT HAS SHIFTED ABOVE THE ESTABLISHED THRESHOLD. REMOVED FUEL NOZZLES IAW TASK 49-31-14-000-801, ITEM 2AE, 1-3 12292. DURING REMOVAL OF NOZZLES, 3 FASTNERS SHEARED AT 5, 7, 8 O`CLOCK POSITION REINSTALLED HARDWARE AND LINES IAWApr 4, 2013 · N589AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2013032994285Warning Light · false activationSINGLE FMC OPS MESSAGE DISPLAYED DURING PREFLIGHT. MESSAGE CLEARED FOLLOWING RESET PROCEDURE. OPS NORMAL.Mar 29, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013032494250Smoke Detector · failedCARGO FWD ARM DOESN`T ILLUMINATE RED ON TEST. R & R FWD CARGO TWO AFT DETECTORS AND CARGO SMOKE DETECTION. TEST OPS CHECKED GOOD REF MM TASK 26-16-00-710-80.Mar 24, 2013 · N589AS · Boeing 737890 · Smoke DetectionSDR ASAA2013032094218Fmc · failedLEFT FMC FAILED. R & R LT FMC IAW AMM 34-61-02. FMC GROUND VERIFICATION SATISFACTORY.Mar 20, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013031994201Compensator · malfunctionedCRUISE LEVEL FLIGHT, LT MAIN TANK 7.96, R MAIN TANK 8.54. BEGAN CROSSFEED, AFTER 5 MINUTES FUEL QTY INCREASED IN LT MAIN TANK TO 8.27, RT MAIN TANK 8.44. FQUIS BITE TEST GROUND TEST FAILED. TANK 1 COMPENSATOR DATA BAD. INFLIGHT FAULTS LOGGED FAULT CODE 28-4Mar 19, 2013 · N589AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2013031794190Warning Light · false activationON F/OS CDU GOT SINGLE FMC WARNING & MAP LIGHT ON NAV DISPLAY. PUT BOTH FMC ON 1 AND RETURNED TO NORMAL - OPS NOW NORMAL. REF 34-61-00 AND FIM TASK 801 FIM 34-61, NO FAULTS.Mar 17, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013031394160Fmc · failedBOTH FMCS FAILED AFTER TAKEOFF. VTK DISPLAYED ON BOTH SIDES. RESTORED AFTER ABOUT 30 SECONDS. ALSO THE INITIAL POINT ON THE LEGS PAGE WAS REPLACED BY A DICO ON LIFTOFF. MAY HAVE BEEN THE FMCS STARTING TO FAIL. FMCS BITE SHOWS NR 1 AND 2 FMC FAIL REMOVED ANMar 13, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013030694086Circuit Breaker · failedON TAXI IN, AFTER SHUTTING DOWN NR 2 ENGINE, NO POWER TRANSFER. TRANSFER BUS OFF AND SOURCE OFF LIGHT ILLUMINATED. ACFT WOULD NOT ACCEPT GROUND POWER. APU STARTED AND POWER APPLIED NORMALLY. ACFT GROUNDED. RAN BOTH ENGINES AND TOGGLED NR 2 ENGINE GENERATOMar 6, 2013 · N589AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2013030494080Pressure Switch · failedAFTER LANDING NR 1 FUEL FILTER BYPASS LIGHT ILLUMINATED ON TAXI IN. PERFORMED FIM TASK 73-05, TASK 801 AND TASK 802 FOR NR 1 ENG. CDU FAULT MESSAGE 73-31071 NOTED. R & R NR 1 ENG FUEL FILTER IAW AMM 73-11-02 AND R & R NR 1 FUEL FILTER DIFFERENTIAL PRESSUREMar 4, 2013 · N589AS · Boeing 737890 · Engine Fuel Indicating SystemSDR ASAA2013030394056Warning Light · false activationAFTER ENGINE START, FMC DISAGREE MESSAGE APPEARED. ACCOMPLISHED QRH ITEMS - MESSAGE CLEARED.Mar 3, 2013 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013011193662Fuel Cell · contaminatedNR 2 FUEL QTY INDICATION VARIED 400 LBS. SUMPED NR 2 MAIN TANK IAW MM 12-11-00, FOUND & REMOVED WATER FROM TANK. PERFORMED FQIS OPS CHECK IAW MM 28-41-00. NO FAULTS FOUND. GROUND VERIFICATION SUCCESSFUL. PERFORMED FUEL COMPARISON CHECK IAW MM 28-41-00 & FJan 11, 2013 · N589AS · Boeing 737890 · Fuel StorageSDR ASAA2012121893508Thermocouple · malfunctionedAPU TREND DATA SHOWS A SHIFT IN EGT. INSPECTED APU INLET AND PLENUM REF AMM 49-11-00-200-801. NO OBSTRUCTIONS FOUND. PERFORM APU BITE CHECK IAW AMM 49-61-00-700-801. NO MX MESSAGE FOUND. R & R THE INLET TEMP SENSOR T2 IAW M/M 49-61-31-401. REPLACED BOTH Dec 18, 2012 · N589AS · Boeing 737890 · APU ControlsSDR ASAA2012121893482Fire Detector · intermittentWHEN TESTING CARGO FIRE, THE FWD LIGHT WILL NOT TEST. LIGHT DOES COME ON WITH THE LIGHTS TEST. PERFORMED FIM 26-16 TASK 806 FWD CARGO FIRE DETECTION FAULT ISOLATION. FAULT RESET & FWD CARGO A & B FIRE LOOP OPS NORMAL.Dec 18, 2012 · N589AS · Boeing 737890 · Fire DetectionSDR ASAA2012121393466Warning Light · unknownDURING LANDING CHECK, RT PACK LIGHT ILLUMINATED DURING RECALL AND EXTINGUISHED WITH MASTER CAUTION RESET. FOUND RIGHT PACK CONTROL AC CIRCUIT BREAKER OUT ACCOMPLISHED BITE RT CABIN CONTROL COMPUTER, FOUND NO FAULTS RESET CIRCUIT BREAKER.Dec 13, 2012 · N589AS · Boeing 737890 · Central WarningSDR ASAA2012120693417Valve · failedDURING CRUISE, PRIOR TO EEP, ATTEMPTED TO CYCLE FUEL CROSSFEED. NO LIGHT INDICATING VALVE MOVEMENT. LIGHT DID NOT TEST WITH PRESS TO TEST. REPLACED BOTH LIGHT BULBS WITH NEGATIVE RESULTS. ON CHECKING P-6-3 PANEL, FOUND FUEL CROSSFEED VALVE CIRCUIT BREAKER Dec 6, 2012 · N589AS · Boeing 737890 · Fuel Transfer ValveSDR ASAA2012110393230Warning Light · false activationAFTER ENGINE START, FMC DISAGREE LIGHT ILLUMINATED ON BOTH ND. CHECKLIST FOR ON GROUND SITUATION WAS ACCOMPLISHED. OPS NORMAL.Nov 3, 2012 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012102093159Exciter · malfunctionedON APU START THE FAULT LIGHT CAME ON AND SMOKE WAS OBSERVED COMING OUT OF THE APU EXHAUST. ACCOMPLISHED FIM TASK 49-40, TASK 802, NO FLAME SHUTDOWN, MAINT MESSAGE 49-41011. REPLACED IGNITER PLUG AND IGNITION EXCITER REF MM 49-41-51 AND 49-41-31.Oct 20, 2012 · N589AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2012100893121Floor Support · corrodedFWD CARGO BAY, BS 500I AFT BULKHEAD, FLOOR SUPPORT STRUCTURE RBL 22 CORRODED. FLOOR SUPPORT CORRODED OUT OF LIMITS IAW SRM 51-10-02. LOCATED DRILLED, COUNTER SUNK AND DEBURRED IAW SRM 51-40-05. INSTALLED IAW SRM 51-40-02.Oct 8, 2012 · N589AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2012100493023Indicator · faultedFAULT LIGHT ILLUMINATED ON APU START. ACCOMPLISHED FIM 49-90-00-810-809. REMOVED AND INSPECTED STARTER GENERATOR FILTER, NO DEBRIS FOUND. INSTALLED NEW FILTER ELEMENT FOR STARTER GENERATOR IAW MM 49-91-12-400-803. CONTINUED FIM, R & R OIL FILTER INDICATOR. Oct 4, 2012 · N589AS · Boeing 737890 · APU Oil SystemSDR ASAA2012090792849Eec · faultyNR 1 ENGINE HAD AN INTERMITTENT FAULT 73-20011 INTERNAL EEC FAULT SHORT TERM, INTERMITTENT FAULT 73-11281, EEC CHANNEL NOT ENERGIZED SHORT TERM, INTERMITTENT FAULT 73-20041 INTERNAL EEC FAULT LONG TERM. ACCOMPLISHED FIM TASK 73-21-00-810-801-F00. REPLACED NRSep 7, 2012 · N589AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012090392820Regulator · failedLEFT BLEED TRIP OFF LT ILLUMINATED, ATTEMPTED RESET IAW QRH, LT WENT OUT FOR ABOUT 10 SEC, DUCT PRESSURE SPLIT L 22 PSI RT 45 PSI, RE-ILLUMINATED. ACFT GROUNDED. DIVERSION TIME - 23 MINUTES. PCV FAILS CONTROL PRESSURE REGULATION TEST, CONTROL PRESS READS OFF-SSep 3, 2012 · N589AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2012092192930Panel · looseWHILE ACCOMPLISHING ENG INLET & FAN BLADE INSPECTION ON NR 1 ENG, T/C 78472000, FOUND FAN DUCT PANEL NR 3 WITH LOOSE FASTENER. R & R FAN DUCT PANEL NR 3 IAW MM 72-23-07-400-801.Sep 2, 2012 · N589AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2012091192868Warning Light · false activationON TAXI OUT GOT A FMC DISAGREE MESSAGE. ACFT GROUNDED. ACCOMPLISHED CHECKLIST, MESSAGE CLEARED UPON CHECKLIST COMPLETION. BOTH FMC GROUND VERIFIED GOOD REF FIM TASK 34-61-00-810-835.Sep 1, 2012 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012081792736Eec · malfunctionedNR 1 ENGINE (SN 802109) HAS SHORT TIME FAULT, MSG. 75-20571 HMU TBV CONTROL CURRENT IS OUT OF RANGE. REMOVED EEC IAW AMM REF 73-21-60-000-801. INSTALLED EEC IAW AMM 73-21-60-400-801. PERFORMED EEC TEST IAW AMM 73-21-60-400-801-F00, TEST PASSED. PERFORMED EAug 1, 2012 · N589AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012081392714Unknown · leakingFOUND OIL LEAKING FROM MIDDLE DRAIN OF APU IAW 05-60-00-280-801CSTEP A.(2) (C) APU REQS REPLACEMENT. BLACK LIGHT TEST OF SWABS FROM LOAD COMPRESSOR DRAIN DID NOT PROVIDE CONCLUSIVE EVIDENCE OF OIL CONTAMINATION. RAN APU WITH RT PACK ON FOR 30 MINUTES. NO AAug 1, 2012 · N589AS · Boeing 737890 · Standard Practices/StructuresSDR ASAA2012071792555Warning Light · false activationRECEIVED A FAULT LIGHT DURING IN-FLIGHT APU START. STARTED APU & RAN 5 MINUTES, VOLTS & FREQS NORMAL. FAULT CODE 49-31016 OVER TEMP SHUTDOWN CLEARED IAW FIM TASK 49-30-803, TASK OPS GOOD.Jul 1, 2012 · N589AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2012060992331Control Valve · faultyCONT CAB ZONE TEMP ILLUMINATED ON RECALL. LIGHT EXTINGUISHED ON RESET. ACFT GROUNDED. BITE TEST SHOWS ON NR 2 AUTOTEMP CONTROLLER LOGGED FLT DECK TCV FAULT. R & R FLT DECK TCV (V143) DUE TO HISTORY, REF AMM TASK 21-61-21, OPS CK NORMAL.Jun 9, 2012 · N589AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA12511657Fmc · failedF/O'S FMC BRIGHT/DIM KNOB MOVES SIDE TO SIDE WHEN ROTATED THE SCREEN BLACKS OUT. VERIFIED DISCREPANCY. R & R F/O FMC CDU REF MM 34-61-01-000-802 & 34-61-01-400-802. TESTS OK IAW SAME REF.Jun 5, 2012 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511661Switch · failed#2 ENGINE FILTER BYPASS LIGHT ON LANDING. R & R NR 2 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH REF AMM TASK 73-34-01, GROUND VERIFICATION OPS CK NML, REF AMM TASK 73-21-00 EEC TEST, 71-00-00-700-801-F00 IDLE POWER LEAK CK AND AMM TASK 73-34-01 INSTALLATIJun 4, 2012 · N589AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012061992385Keyboard · inoperativeCPTS FMC/CDU L6 BUTTON INOPERATIVE. ACFT GROUNDED. R & R FMCS MCDU KEYBOARD, REF MM 34-61-01-000-801 AND MM 34-61-01-400-801. OPS NORMAL.Jun 1, 2012 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511620Warning Light · false activationON RECALL "AIR COND" ILLUMINATED ON MASTER CAUTION WITH OVERHEAD "CONT CAB" LIGHT RESET OFF. ACFT GROUNDED. TESTED PACK/ZONE TEMP CONTROLLER IAW MM 21-60-00. SYS OP CHECKED GOOD.May 31, 2012 · N589AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511487Control Valve · malfunctionedLEFT PACK ILLUMINATED ON RECALL EXTINGUISHES W/MASTER CAUTION RESET. ACFT GROUNDED. PACK CONTROLLER BITE SHOWS TCV FAULT. TROUBLESHOT IAW FIM 21-62, TASK 848. VERIFICATION TEST OF NR 1 TEMP CONTROL VALVE NORMAL.Apr 30, 2012 · N589AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511454Knob · inoperativeF/O FMC BRT ADJUST KNOB NOW WORKING PROPERLY WHEN YOU TOUCH IT CDU SCREEN GOES TO FULL BRIGHT OR FULL DIM. COULD NOT DUPLICATE WRITE UP. ADJUSTED UP AND DOWN F/O'S BRIGHT KNOB ON FMC CDU. SYS IS WORKING NML. NO HISTORY. PERFORMED LAMP TEST REF 34-61-01. SYS Apr 24, 2012 · N589AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511384Starter · leakingFOUND NR 2 ENGINE STARTER ASSY LEAKING OIL FROM EXHAUST HOUSING. REPLACED NR 2 ENGINE STARTER ASSY REF MM 80-11-01-400-801, OPS AND LEAK CHECKED NORMAL.Apr 10, 2012 · N589AS · Boeing 737890 · Engine Starter
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