N585AS

Service difficulty reports · 564

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 = 'N585AS' 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 ASAA2018102326572Shroud · wornNR 1 ENG ABRADABLE SHROUD HAS GROOVES COMPLETELY AROUND THE SHROUD. MAX WIDTH WAS 2.9 IN. OUT OF LIMITS PER AMM 72-24-02 F.(1)(E). GROUNDED - YES. INSTALLED NEW COMPOUND TO THE ABRADABLE SHROUD IAW AMM 72-24-02-200-802. 2.A.-F.(1)-(10). COMPLETED NR 1 ENG ABRAOct 21, 2018 · N585AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018101526498Start Valve · failedRIGHT ENGINE START SWITCH FAILED TO ENGAGE THE START MODE IN MEX. AFTER MULTIPLE ATTEMPTS START MODE WAS SUCCESSFUL ONLY AFTER HOLDING THE START SWITCH HARD OVER AND HOLDING IN THERE. GROUNDED - YES. REMOVED AND REPLACED RIGHT ENGINE START SWITCH REFERENCE AMMOct 15, 2018 · N585AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2018092626270Warning System · false activationAFTER ENGINE START RIGHT PACK LIGHT ILLUMINATED. EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED PACK TEMP CONTROL BITE REF FIM 21-62 TASK 801. FOUND TCV PACK LAST LEG. ACCOMPLISHED VERIFY, NO CURRENT FAULTS. RESET FAULT, RT PACK TEMP CONTSep 26, 2018 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018092226224Pressure Switch · failed#1 FUEL FILTER BYPASS LIGHT IS ON WHEN ENGINE IS RUNNING. GROUNDED - YES. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH REF B737-800 AMM 73-34-01. REMOVED AND REPLACED FUEL FILTER, REF AMM 73-11-02. ACCOMPLISHED TEST 3A DIFF PRESS SWITCH AND FISep 22, 2018 · N585AS · Boeing 737890 · Engine Oil Indicating SystemSDR ASAA2018091726159Guide Vane · damagedWHILE ACCOMPLISHING T/C 78472022 NR 1 ENGINE FOUND 1 STAGE 1 LPT NGV BURNED WITH MISSING MATERIAL. BLADE LOCATED APPROX AT 12:00 POSITION 1. ALSO FOUND 4TH STAGE 1 LPT NGV CRACKED APPROX 3/4 WAY THROUGH ALL ON DIFFERENT SEGMENTS APPROX 12:00 TO 3: 00 POSITION.Sep 17, 2018 · N585AS · Boeing 737890 · Turbine SectionSDR ASAA2018091126085Warning System · false activationDURING CRUISE, LEFT PACK LIGHT ILLUMINATED WITH MASTER CAUTION RECALL. COMPLIED WITH QRH PROCEDURE AND LIGHT EXTINGUISHED INDICATING SINGLE CONTROLLER FAILURE. GROUNDED - YES. ACCOMPLISHED PACK/ZONE TEMPERATURE CONTROLLER BITE REF AMM 21-61-00 OPS CHECK NORMALSep 9, 2018 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018082105865Valve · malfunctionedAT TOP OF THE DESCENT, CROSSFEED VALVE, CHECK VALVE OPENED BUT FAILED TO CLOSE. QRH 12-2 ACCOMPLISHED. ACFT GROUNDED. ACCOMPLISHED FIM 28-22, TASK 808. CROSSFEED VALVE OPS CHECKED GOOD.Aug 20, 2018 · N585AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2018070225249Wire Harness · defectiveNR 2 ENGINE TREND DATA HAS NOT RECOVERED TO EXPECTED EGT AND HDM LEVELS AFTER LAST EGT INDICATION SYSTEM. GROUNDED - YES. ENGINEERING REQUEST, REMOVED AND REPLACED CJ10 HARNESS REF AMM 73-21-06/401. REMOVED AND REPLACED J10 HARNESS REF AMM 73-21-06/401. FADEC Jul 1, 2018 · N585AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2018061825113Connector · disconnectedNR 2 ENGINE COWL VALVE OPEN LIGHT ILLUMINATED WITH A TAI INDICATION. FOLLOWED QRH. ACFT GROUNDED. FOUND THE NR 2 ENGINE COWL VALVE ELECTRICAL CONNECTOR DISCONNECTED. RECONNECTED AND PERFORMED AN OPS CHECK IAW AMM 30-21-11-400-801, OPS TESTED GOOD.Jun 18, 2018 · N585AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2018061875085Bleed Valve · failedWHILE PERFORMING A NR 2 ENGINE IDLE RUN, WITH ALL ENGINE BLEEDS OFF AND ISOLATION VALVE CLOSED, THE RT DUCT PRESSURE READ APPROXIMATELY 20 PSI. ACFT GROUNDED. FOUND THE NR 2 ENGINE BLEED AIR REGULATOR HAD FAILED. REMOVED AND REPLACED THE NR 2 ENGINE BAR IAJun 17, 2018 · N585AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2018061865096Wire Harness · damagedAFTER ENGINE SHUTDOWN, NR 2 EGT WAS BLANK, BUT HAS RED BOX WHERE THE TEMP WOULD BE. ACFT GROUNDED. ACCOMPLISHED AN ENGINE EXCEEDANCE PAGE CHECK IAW AMM 71-00-00-800-804-F00. EXCEEDANCE VALUES WERE, RED AT 950 WITH A PEAK OF 961. FOR 9.4 SECONDS. EEC BITE Jun 16, 2018 · N585AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2018061835095Probe · failedA MOMENTARY EGT EXCEEDANCE OCCURRED ON THE NR 2 ENGINE ON INITIAL CLIMBOUT. ACFT GROUNDED. ACCOMPLISHED AN ENGINE EXCEEDANCE PAGE CHECK IAW AMM 71-00-00-800-804-F00. EXCEEDANCE VALUES WERE RED AT 950 WITH A PEAK OF 961. FOR 9.4 SECONDS. EEC BITE SHOWS NO FAJun 13, 2018 · N585AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2018061125031Battery Pack · dischargedEMERGENCY LIGHTS BY R1 DOOR INOP. GROUNDED - YES. REMOVED AND REPLACED M1674 EMERGENCY EXIT LIGHT BATTERY PACK, OPS CHECK GOOD IAW AMM 33-51-00.Jun 11, 2018 · N585AS · Boeing 737890 · Emergency LightingSDR ASAA201805214687Skin · corrodedFUSELAGE SKIN, BS 917, STRINGER 19L, AROUND THE AFT LAVATORY VENT WAS FOUND CORRODED. ACFT GROUNDED. REMOVED THE CORROSION, AND FOUND THE SKIN TO BE ACCEPTABLE FOR CONTINUED SERVICE IAW EA 800-53EA-20323.May 17, 2018 · N585AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA201805184685Blade · damagedWHILE ACCOMP T/C 78472002, FOUND ELASTOMER DAMAGE TO ALL PLATFORMS BEYOND MM LIMITS. ACFT GROUNDED. NEW PLATFORMS INSTALLED IAW CARD 78472002, SUB TASK 839-045.May 17, 2018 · N585AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA201805184684Blade · damagedWHILE ACCOMP T/C 78472002, FOUND 10 PAIRS OF BLADES WITH CU-N1 COATING DAMAGED BEYOND Y DIMENSION LIMITS. ACFT GROUNDED. REPLACED THE FAN BLADE SETS IAW AMM 72-21-02-900-801-F00.May 17, 2018 · N585AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018050624560Unknown · malfunctionedFOUND RECENT FAULT ON ENGINE NR 2. FAULT 77-10852, THE BOTTOM RIGHT EGT SIGNAL (T49552) IS OUT OF RANGE. ECONOMIC FAULT. DEFERRED PER T/C 78273000. GROUNDED - YES. REFB737-800 FIM 77-21 TASK 802 FOR TROUBLESHOOTING. NO RECENTS FAULTS STORED. EEC TEST PASSED. PMay 6, 2018 · N585AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2018021923642Pump · failedNR 1 AFT FUEL PUMP LOW PRESSURE ILLUMINATED DURING CRUISE. ACCCOMPLISHED QRC PROCEDURE. ACFT GROUNDED. REPLACED THE NR 1 TANK AFT PUMP IAW AMM 28-22-41.Feb 19, 2018 · N585AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2018021823607Seal · missingWHILE ACCOMPLISH T/C 78472002 ON THE NR 1 ENGINE, FOUND THE NR 4 PLATFORM CONCAVE SIDE MISSING SEAL. ACFT GROUNDED. REMOVED AND REPLACED THE PLATFORM IAW AMM 72-21-02-000-802.Feb 18, 2018 · N585AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2018021823606Spinner · damagedWHILE ACCOMPLISHING TASKCARD 78472002, FOUND THE FRONT SPINNER CONE MISSING BLACK SULFURIC ANODIZING. ACFT GROUNDED. REMOVED AND REPLACED THE SPINNER CONE IAW AMM 72-21-01-401.Feb 18, 2018 · N585AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2018021823605Blades · damagedWHILE ACCOMPLISH T/C 78472002 ON THE NR 1 ENGINE, FOUND FAN BLADES NR 5, 15, AND 20 MISSING CU-NI-IN COATING BEYOND AREA X ALL ON CONCAVE SIDE. ACFT GROUNDED. THE FAN BLADES WERE REPLACED IAW AMM 72-21-02-000-802-F00. VIBRATION SURVEY FOUND TO BE WITHIN LIMFeb 18, 2018 · N585AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2018021323542Connector · failedDURING FLIGHT, THE NR 1 FUEL TANK, AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. ACFT GROUNDED. FOUND THE LT AFT FUEL PUMP CIRCUIT BREAKER TRIPPED. LEFT AFT PUMP INOPERATIVE. REMOVED AND REPLACED THE PUMP CONNECTOR D70 IAW SWPM 20-61-11. REPLACED THE WIRFeb 13, 2018 · N585AS · Boeing 737890 · Fuel System WiringSDR ASAA2018020623432Autopilot Sys · malfunctionedWHEN ENGAGING SECOND AUTOPILOT FOR AUTOLAND APPROACH B, THE AUTOPILOT DISENGAGED, ENGAGED AUTOPILOT A, ATTEMPTED TO ENGAGE B AGAIN, SAME RESULT. UNABLE TO ATTEMPT APPROACH. ACFT GROUNDED. ACCOMPLISHED DFCS BITE IAW FIM 22-11 TASK 801 CURRENT STATUS, AUTOFeb 6, 2018 · N585AS · Boeing 737890 · Autopilot SystemSDR ASAA2018020323390Wire · chafedNR 1 MAIN TANK, AFT LOW PRESSURE ILLUMINATED DURING CRUISE WITH 8500 LBS OF FUEL IN THE NR 1 MAIN TANK. ACFT GROUNDED. ACCOMPLISHED WIRING CHECKS IAW TSR 701389 AND FOUND W1136-3601B-16 CHAFED CAUSING ARCING BY D70 CONNECTOR ON THE NR 1 TANK AFT BOOST PUMP. Feb 3, 2018 · N585AS · Boeing 737890 · Fuel System WiringSDR ASAA2018020323389Pump · failedNR 1 FUEL TANK AFT PUMP LOW PRESSURE LIGHT ILLUMINATED WITH PUMP ON AND 5000 LBS FUEL IN THE TANK. GROUNDED - YES. REMOVED AND REPLACED NR 1 TANK AFT FUEL PUMP IAW AMM 28-22-41. C/W OPERATIONAL TEST OF THE NR 1 TANK AFT FUEL PUMP IAW AMM 28-22-41. OPS TEST GOOFeb 3, 2018 · N585AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2018012923328Transceiver · failedHF 2 RECEIVES BUT DOES NOT TRANSMIT. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 HF TRANSCEVER IAW AMM 23-11-21, OPS CHECKED NORMAL.Jan 29, 2018 · N585AS · Boeing 737890 · HF Communications SystemSDR ASAA2018012623304Satcom · malfunctionedSATCOM INOPERATIVE DURING A MEDLINK EVENT. NO NUMBER WAS DISPLAYED AT BOTTOM OF SCREEN AND THERE WAS A CONTINUED BUSY TONE HEARD. ACFT GROUNDED. VERIFIED NO NUMBER & BUSY TONE, AFTER CYCLING THE SATCOM CIRCUIT BREAKER, THE SYSTEM RESTORED TO NORMAL. ACCOMPLJan 26, 2018 · N585AS · Boeing 737890 · Communications SystemSDR ASAA2018010823111Impeller · failedNR 1 AFT FUEL LOW PRESSURE LIGHT ILLUMINATED ON PUSHBACK. ACFT GROUNDED. FOUND R18 GFI RELAY WITH RESET BUTTON TRIPPED. RESET THE R18 IAW FIM 28-22 TASK 803. DISCONNECTED THE NR 1 AFT FUEL PUMP CONNECTOR D70. INSPECTED FOR DAMAGE. NO DEFECTS NOTED IAW FIM.Jan 8, 2018 · N585AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2017122923061Indication Sys · out of toleranceFOUND A NR2 ENGINE FAULT MESSAGE 77-10852, THE BOTTOM RIGHT EGT SIGNAL IS OUT OF RANGE, ECONOMIC FAULT, ACFT GROUNDED. PERFORMED EEC BITE IAW FIM 73-00, TASK 801. NO FAULTS FOUND IN RECENT FAULTS OR FAULT HISTORY. PERFORMED INITIAL EVAL PER FIM 77-21 TASKDec 29, 2017 · N585AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2017122723070Apu · oil consumptionAPU HAS A HISTORY OF GREATER THAN EXPECTED OIL CONSUMPTION. PREVIOUS TROUBLESHOOTING HAS FOUND NO EVIDENCE OF EXTERNAL LEAKAGE. ACFT GROUNDED. REPLACED THE APU IAW T/C 78349010. LEAK AND OPS CHECKED GOOD.Dec 27, 2017 · N585AS · Boeing 737890 · APU Oil SystemSDR ASAA2017120122749Link · worn#1 ENGINE PNEUMATIC DUCT SUPPORT LINK ASSY'S ARE WORN AT BOTH ROD ENDS OF SUPPORT LINKS. GROUNDED - YES. REMOVED & REPLACED #1 ENGINE PNEUMATIC DUCT SUPPORT LINK ASSYS REF B737-800 AMM 36-11-01.Dec 1, 2017 · N585AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2017112022643Idg · inoperativeNR 1 GENERATOR INOPERATIVE. ACFT GROUNDED. REMOVED & THE NR 1 IDG IAW AMM 24-11-11. OPS TESTED GOOD. LEAK CHECKED GOOD.Nov 20, 2017 · N585AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2017102122309Warning Message · false activationFOUND MAINTENANCE MESSAGE FOR THE NR 2 ENGINE. THE BOTTOM RIGHT EGT SIGNAL IS OUT OF RANGE . ECONOMIC FAULT. ACFT GROUNDED. PERFORMED ENG 2 EEC TEST IAW AMM 73-21-00-700-804-F00. TEST PASSED WITH NO FAULTS.Oct 21, 2017 · N585AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2017102022268Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED IN FLIGHT, EXTINGUISHED ON MASTER CAUTION RESET. ACFT GROUNDE. ACCOMPLISHED CONTROLLER BITE. BITE & LAST FLIGHT FAULT WAS TCV. RESET AND RERAN BITE. CLEARED FAULT. OPS GOOD IAW AMM 21-61-00-700-807-002.Oct 20, 2017 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017092522039Panel · damagedNR 2 ENGINE FAN DUCT PANEL NR 3 HAS FASTENER PULLED THRU. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FAN DUCT PANEL NR 3, IAW AMM 72-23-07.Sep 25, 2017 · N585AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017092122017Heat Exchanger · leakingNR 2 ENGINE OIL-FUEL HEAT EXCHANGER LEAKS AT FUEL PUMP GASKET INTERFACE. ACFT GROUNDED. REMOVED MAIN OIL FUEL HEAT EXCHANGER AMD SERVO FUEL HEATER IAW AMM 79-21-02-000-801-F00 AND 73-11-07-000-801-F00. INSTALLED NEW NR 2 ENGINE OIL-FUEL HEAT EXCHANGER IAW ASep 21, 2017 · N585AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA2017092121998Pin · migratedNR 2 ENGINE, FOUND ANTI-ROTATION PIN MIGRATING AT THE THIRD STAGE STATOR SEAL SEGMENT, 9 O'CLOCK. ACFT GROUNDED. REMOVED & REPLACED THE NR 2 ENGINE.Sep 21, 2017 · N585AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2017091621953Warning Message · false activationDURING ACCOMPLISHMENT OF T/C 78273000, NR 2 ENGINE HAS ECONOMIC FAULT MESSAGE 73-31372, UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. NO FAULTS LOGGED AT THIS TIME.Sep 16, 2017 · N585AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2017083121772Fault Message · illuminatedWHILE ACCOMPLISHING TASK CARD 78273000, FOUND MAINTENANCE MESSAGE 73-31372 FOR UPPER EGT SECTORS READING HIGH, ECONOMIC FAULT NR 2 ENGINE. ACFT GROUNDED.Aug 31, 2017 · N585AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2017082121693Warning Light · false activationRIGHT FWD WINDOW HEAT OVERHEAT CAUTION LIGHT ILLUMINATED AT 2145Z. QRH PROCEDURE FOLLOWED. ACFT GROUNDED. COMPLIED WITH A BITE CHECK OF WHCU WITH NO DEFECTS NOTED IAW FIM 30-41TASK 801.Aug 21, 2017 · N585AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017073121591Channel · corrodedCARGO BAY FLOOR, LT TRANSITION ANGLE, FROM FWD PIT TO BS 847 IS CORRODED AT SEVERAL PLACES. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-00-53-1A-2 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED IAW SRM 53-00-53-28-5, FABRICATED A NEW TRANSIJul 31, 2017 · N585AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017070421262Lens · detachedMID-CABIN OVERHEAD EXIT ROW SIGN DAMAGED. ACFT GROUNDED. FOUND BOTH MID-CAIN CEILING EXIT SIGN LENS COVERS OFF. CHECKED CONDITION OF BOTH LENS COVERS AND HOLDER OK. REINSTALLED LENS IAW AMM 33-51-01-960-801.Jul 4, 2017 · N585AS · Boeing 737890 · Emergency LightingSDR ASAA2017062821224Warning Message · illuminatedFOUND NR 2 ENGINE ECONOMIC FAULT MESSAGE 73-31372. UPPER EGT SECTORS READING HIGH. ACFT GROUNDED.Jun 28, 2017 · N585AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2017062821218Light · intermittentAUTOTHROTTLE ARM LIGHT INOPERATIVE. ACFT GROUNDED. CYCLED ACFT POWER. AUTO ARM LIGHT ILLUMINATES NORMAL IAW FIM 22-31-801.Jun 28, 2017 · N585AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2017062721206Unknown · malfunctionedF/O MASTER, A/P ENGAGED. AT LOC CAPTURE F/O LOC FLIGHT DIRECTOR BAR REMOVED FROM VIEW. AT GS INTERCEPT, GS FD BAR ALSO REMOVED. AUTOPILOT REMAINED ENGAGED, CONTINUED CORRECT GUIDANCE. A/P MANUALLY DISENGAGED, CYCLED FLIGHT DIRECTORS (BOTH) CA FD REMAINED IN VIJun 27, 2017 · N585AS · Boeing 737890 · Autopilot SystemSDR ASAA2017052920877Actuator · failedRT PACK LIGHT ON AFTER RECALL PUSHED. FOLLOWED QRH, LIGHT OUT AFTER MASTER CAUTION PUSHED. ACFT GROUNDED. ON WALK AROUND FOUND R/H RAM DOOR DOOR IN FULLY OPEN POSITION. ROD ON RT RAM AIR DOOR ACTUATOR IS STUCK OUT, REPLACED RT RAM AIR DOOR ACTUATOR IAW AMM 21May 29, 2017 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017052820933Wire Harness · shortedAFTER ENGINE SHUTDOWN AT THE GATE, A RED BOX SHOWED ON THE NR 2 EGT. ACFT GROUNDED. ACCOMPLISHED A NR 2 ENGINE EGT CONNECTOR CLEANING IAW AMM 77-21-00-140-801. PRE-CLEANED TEMPS WERE S1-153, S2-113, S3-112, S4-146. POST-CLEANED TEMPS WERE S1-31, S2-17, S3-17,May 28, 2017 · N585AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2017051820803Control Valve · failedPRIMARY FLIGHT DECK TEMP CONTROLLER INOPERATIVE. ACFT GROUNDED. NR 2 TEMP CONTROLLER LOGGED FLIGHT TCV FAULT. REMOVED AND REPLACED CONTROL CABIN TRIM AIR VALVE V143. OPS NORMAL IAW AMM 21-61-21-400-801. LEAK CHECKED GOOD.May 18, 2017 · N585AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017051620797Warning Light · false activationDURING TOP OF DESCENT, THE RIGHT PACK ANNUNCIATOR LIGHT ILLUMINATED. WENT OUT WHEN THE MASTER CAUTION LIGHT WAS RESET. QRH PROCEDURE ACCOMPLISHED. ACFT GROUNDED. PERFORMED FIM 21-62, TASK 801, PACK TEMP CONTROL BITE, NO FAULTS OR FAILURES NOTED. DEEMED TO May 16, 2017 · N585AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017050220611Unknown · malfunctionedON DESCENT RECALL CHECK RIGHT PACK LIGHT ILLUMINATED. LIGHT RESETS WITH MASTER CAUTION RESET. GROUNDED - YES. ACCOMPLISHED RIGHT PACK TEMP CONTROLLER BITE TEST, REF AMM 21-61-00. FOUND ACTUATOR FAULT ONE TIME. PERFORMED ACTUATOR OPS TEST, REF 21-51-21. SYSTEM May 2, 2017 · N585AS · Boeing 737890 · Cabin Cooling System
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