N587AS

Service difficulty reports · 482

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 = 'N587AS' 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 ASAA12511485Floorbeam · corrodedFORWARD CARGO PIT AFT FLOORBEAM CORRODED SEVERAL LOCATIONS. ACFT GROUNDED. R & R IAW SRM 51-40-05.Apr 20, 2012 · N587AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA12511444Floorbeam · corrodedFWD CARGO PIT AFT FLOOR ATTACH ANGLE CORRODED, SERVERAL LOCATIONS. R & R IAW SRM 51-40-005.Apr 20, 2012 · N587AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA12511415Control Unit · malfunctionedRT SIDE WINDOW HEAT, OVERHEAT LIGHT ILLUMINATED ON APPROACH. ACCOMPLISHED QRH PROCEDURE AND LIGHT REMAINED EXTINGUISHED. GROUNDED. DUE TO UNIT HISTORY ENGINEERING REQUESTS REPLACEMENT OF WCHU. REPLACED RT SIDE WINDOW HEAT CONTROL UNIT. OPS CHECKED GOOD, REFApr 16, 2012 · N587AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA12511414Warning Light · false activationRT WINDOW (F/O SLIDER) OVERHEAT LIGHT ILLUMINATED FL 270 ON ARRIVAL/APPROACH. ACCOMPLISHED QRH PROCEDURE. LIGHT ILLUMINATED AGAIN ON TAXI IN. GROUNDED. ACCOMPLISHED FIM TASK 30-41-00-810-801. PERFORMED WHCU BIT PROCEDURE. INTERMITTENT FAULTS. NO FAULTS NOTApr 16, 2012 · N587AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA12511307Autopilot Sys · malfunctionedSPEED CONTROL WOULD GO FROM SLOW & THE THROTTLES WOULDN'T INCREASE. MANUALLY MOVEED THOTTLES. SPEED WOULD GO TOO FAST AND HAD TO MANUALLY MOVE THROTTLES BACK. HAPPENED IN VPATH AND LEVEL CHANGE. MAINLY HAPPENED IN DESCENT. NOT AS BAD IN THE CLIMB. AUTOTHMar 31, 2012 · N587AS · Boeing 737890 · Auto Throttle SystemSDR ASAA12511166Wire Harness · chafedNR 2 ENGINE HARNESS MW0316 IS CHAFED ONE INCH FROM TERMINAL LUG AT CONNECTION TO UPPER FAN FIRE DETECTOR ASSY. REMOVED HARNESS IAW MM 26 11 02 000 801. INST HARNESS IAW MM 22 11 02 400 801. OPS CHECK NORMAL REF MM 26 11 00 710 801.Feb 28, 2012 · N587AS · Boeing 737890 · Fire Protection System WiringSDR ASAA12511082Window · crackedAT FL 260 LEFT SIDE WINDOW "OVERHEAT" LIGHT ILLUMINATED FOLLOWED BY ELECTRICAL ARCING ON L2 WINDOW FOLLOWED BY L2 CRACKING OUTER PANE. DIVERSION TIME: 2 HOURS. REPLACED LT NR 2 SLIDING WINDOW PER AMM 56 12 11 400 801, OPERATION CHECK NORMAL.Feb 9, 2012 · N587AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA12510959Warning System · false activationRIGHT PACK LIGHT ILLUMINATES ON RECALL. EXTINGUISHES WITH MASTER CAUTION RESET. PERFORMED PACK ZONE TEMP CONTROLLER BITE. FAULTED RAM AIR ACT. VERIFY TEST PASS FAULT RESET REF FIM 21 62 00 810 836.Jan 18, 2012 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1150862Unknown · malfunctionedLEFT PACK LIGHT ILLUMINATED ON GROUND. ACCOMPLISHED BITE PROCEDURE ON PACK/ZONE TEMP CONTROLLERS. A TCV FAULT SHOWED ON THE NR 1 TEMP CONTROLLER. FAULT CLEARED & TEMP CONTROLLERS SHOW NO NEW FAULTS. GROUND VERIFIED BY RUNNING APU & A/C PACKS. NO FAULTS INDec 27, 2011 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA11510754Unknown · malfunctionedON RECALL RT PACK LIGHT ILLUMINATES LIGHT RESETS DURING MC RESET. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST. NO FAULTS LOGGED. REF AMM 21 61 00 700 806 002.Dec 4, 2011 · N587AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA11510620Transceiver · defectiveRADAR SPOKES INTERMITTENTLY ALL QUADRANTS/RANGES/TILTS. CONFIRMED RADAR SPOKES. VERIFIED RECEIVER/TRANSMITTER COOL FAN OPERATES PER AMM 34 43 41 400 801 FAN CIRCULATES NORMAL. REPLACED RADAR RECEIVER/TRANSMITTER PER AMM 34 43 41 400 801. PERFORMED RADAR SYNov 3, 2011 · N587AS · Boeing 737890 · Weather Radar SystemSDR ASAA11510503Unknown · malfunctionedAFTER PUSHBACK FMC DISAGREE MESSAGE. PERFORMED PROCEDURE IN THE QRH. FMC OPERATION RESTORED.Oct 11, 2011 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA11510470Sensor · failedAFTER ENGINE START FWD WINDOW HEAT "OVERHEAT" LIGHT CAME ON. REFERRED TO QRH AND TURNED SWITCH OFF AND WAITED 2 MINUTES. PLACED SWITCH BACK ON AND OVERHEAT LIGHT CAME BACK ON. ACCOMPLISHED FIM 30 41 TASK 801. WINDOW SENSOR FAULT ILLUMINATED LAST SEVERAL LEOct 4, 2011 · N587AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA11510446Warning System · false activationWINDOW HEAT OVERHEAT LIGHT ILLUMINATED. PERFORMED BITE TEST OF WINDOW HEAT CONTROL PER FIM 30 41 00 810 801, NO FAULTS FOUND.Sep 30, 2011 · N587AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA11510376Sensor · dirtyCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON TAXI OUT. PACK/ZONE TEMP CONTROLLERS PASS BITE PROCEDURE. OPENED A/C ZONE TEMP VALVE FAN CONT FLT DECK (B3 ON P6 4 PANEL). CLEANED FLIGHT DECK TEMP SENSOR. OPERATED AIR CONDITIONING SYSTEM. ZONE TEMP LIGHT NEVESep 15, 2011 · N587AS · Boeing 737890 · Cabin Temperature SensorSDR ASAA11510375Unknown · malfunctionedAUTO FAIL AND ALTN LIGHTS ON PRESSURIZATION PANEL. VERIFIED AUTO FAIL AND ALTN LIGHTS ON. LIGHTS EXTINGUISHED BY SELECTING MANUAL AND RETURNING TO AUTO. GROUND VERIFICATION NORMAL BOTH PRESSURE CONTROLLERS OK FOR SERVICE REF MM 21 31 0.Sep 15, 2011 · N587AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA11510239Apu · oil consumptionON CLIMBOUT NOTICED APU MAINT LIGHT ON. C/W APU BITE PROCEDURE PER AMM 49 60 00 810 801. FAULT CODE 49 91227 LOW OIL QUANTITY LOGGED. SERVICED 2 QTS OF OIL IN APU. REF 12 13 31 FAULT CLEARED FROM CURRENT STATUS APU OPS NORMAL. TSR ISSUED DUE TO HISTORY OF Aug 14, 2011 · N587AS · Boeing 737890 · APU Core EngineSDR ASAA11510199Start Valve · failedAFTER LANDING IN PDX SHUTDOWN NR 2 ENGINE. NEEDED TO RESTART NR 2 AND DID NOT GET A START VALVE OPEN LIGHT. PERFORMED FIM TASK 80 07 00 810 803 F00 INST JUMPER BETWEEN PINS 9 & 5 ON DP1202. MOVED START SWITCH TO GND & START VLV OPEN INDICATES ON CDS. REPLAAug 6, 2011 · N587AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA11510212Oil Cooler · defectiveAPU OIL CONSUMPTION CONTINUES TO BE HIGHER THAN EXPECTED CURRENT CONSUMPTION. TSR ISSUED. REPLACED APU OIL COOLER REF MM 49 91 41 400 801. LEAK AND OPS CHECK GOOD.Aug 5, 2011 · N587AS · Boeing 737890 · APU Oil SystemSDR ASAA11510190Engine · making metalFOUND METAL SHAVINGS ON THE AFT SUMP MAGNETIC CHIP DETECTOR FOR THE NR 2 ENG. NON MAGNETIC. MATERIAL IS NON MAGNETIC OR METALLIC HAIR LIKE DEBRIS. OK FOR CONTINUED SERVICE REF MM 79-00-00-200-804-F00, STEP F (7) (K). REPLACED NR 2 ENGINE REF T/C 78471000.Jul 30, 2011 · N587AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA11510150Idg · failedIDG DRIVE ANNC INOP. REPLACED 1 ENG IDG PER MM 24 11 11 000 801 AND 24 11 11 400 801. LEAK AND OPS CHECK GOOD.Jul 21, 2011 · N587AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1159971Unknown · malfunctionedDURING PREFLIGHT FOUND OPEN C/B ON P18 2 (B 10) "FMCS BITE DC". RESET C/B PER MM 20 60 01 REF WDM 34 61 22. TESTED FMC REF MM 34 61 00 710 801. TESTS OK. SUCESSFUL GROUND VERIFICATION.Jul 1, 2011 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1159917Wire Harness · brokenDURING ENG FIRE TEST LIGHTS IN FIRE SWITCH HANDLE NR 2 FAILED TO ILLUMINATE. PERFORMED ENG/APU FIRE DET CONT MODULE BITE TEST PER FIM 26 10 TASK 801. FAULTED NR 2 ENG LOOP B UPPER FAN DETECTOR. FOUND WIRE AT UPPER FAN DET BROKEN OFF TERMINAL. RE-TERMINATEDJun 22, 2011 · N587AS · Boeing 737890 · Fire Protection System WiringSDR ASAA1159522Transceiver · malfunctionedNR 2 HF RADIO WILL NOT TRANSMIT MIC WILL EITHER NOT CYCLE OR RADIO STICKS IN TUNING MODE WITH A CONTINOUS TUNNING TONE. MUST CYCLE TRANSMIT SWX TO STOP. CONFIRMED FAULT. REPLACED NR 2 HF TRANSCEIVER PER AMM 23 11 21 400 801. GROUND SYSTEM VERIFICATION CHECApr 23, 2011 · N587AS · Boeing 737890 · HF Communications SystemSDR ASAA1159445Control Unit · failedF/O OUTER WINDOW FRACTURED. F/O NOTED ARCING ON UPPER RT FRAME FOLLOWED BY FRACTURE. ACCOMPLISHED CHECKLIST. NO FURTHER DETERIORATION. REMOVED AND REPLACED R FRONT WINDOW CONTROLLER PER MM 30-41-11. REPLACED F/O'S NR 1 WINDOW PER MM 56-11-11. WINDOW HEATApr 13, 2011 · N587AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA1159331Valve · malfunctionedRT BLEED TRIP OFF ILLUMINATED AT START OF DESCENT, QRH ACCOMPLISHED LIGHT EXTINGUISHED. FOUND EXPOSED WIRE ON BLEED AIR REG. REPLACED RT BLEED AIR REG. PERFORMED CHECK OF PRECOOLER SYSTEM REF MM 36 12 00 700 801, PRECOOLER VALVE TEST FAILED. CONTINUED W/ CMar 23, 2011 · N587AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1159073Display · defectiveLEFT FMC L 6 BUTTON STUCK DOES NOT RESPOND TO SELECTED INPUTS. REPLACED CAPT'S FMCS CDU PER AMM34 61 01, OPS CHECK NML.Feb 22, 2011 · N587AS · Boeing 737890 · Central DisplaySDR ASAA1159062Unknown · malfunctionedAUTOLAND UNSAT AIRCRAFT LINED UP WITH LEFT SIDE OF APPROACH END OF RUNWAY AND WANTED TO DRIFT FURTHER LEFT. TOUCHDOWN HOWEVER WAS IN TOUCHDOWN ZONE. ACCOMPLISHED DFCS LAND VERIFY GP49 TESTS REF AMM22 11 00 OPS CHECK NML. PER NEW PROCESS CHECKED FOR REPETITIFeb 21, 2011 · N587AS · Boeing 737890 · Autopilot SystemSDR ASAA1158892Wire Harness · brokenPILOT REPORTS FIRE DECTECTION TEST WILL NOT ILLUMINATE T HANDLE FOR ENGINE NR 2 IN LOOP B. FOUND WIRE BROKEN INSIDE TERMINAL AT ENG FAN UPPER LOOP B/2 WIRE MW0316. CRIMPED NEW TERMINAL END TO WIRE MW0316 PER SWPM 20 30 11. ENG 2 FIRE LOOP B TESTS GOOD.Jan 27, 2011 · N587AS · Boeing 737890 · Fire Protection System WiringSDR ASAA1158886Connector · dirtyWHILE IN E & E BAY FOUND FAULT LOGGED ON ENGINE/APU FIRE DETECTION UNIT FOR NR 2 ENGINE UPPER FAN LOOP B DETECTOR. CLEANED TERMINAL CONNECTIONS TO THE NR 2 ENGINE UPPER FAN FIRE DETECTOR ASSY AND PERFORMED ENGINE FIRE DETECTION OPERATIONAL TEST REF MM 26 11 0Jan 25, 2011 · N587AS · Boeing 737890 · Fire Protection System WiringSDR ASAA1158871Circuit Breaker · trippedFMC DISAGREE ON TAXI OUT. RESET CB AS PER QRH PROCEDURE. FMC DISAGREE EXTINGUISHED.Jan 23, 2011 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158859Fmc · failedRIGHT FMC INOP WITH " VTK" FLAG. VERIFIED DISCREP WITH FMC 2 C/B'S IN NR 2 FMC LRU GREEN "POWER ON AND FMC VALID" LIGHTS NOT ILLUMINATED. FMC CDU'S SHOW FMC RIGHT BITE INOP. REPLACED NR 2 FMC COMP REF MM 34-61-02. PERFORMED FMC CROSS LOAD REF 34-61-00. OPJan 20, 2011 · N587AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA1158789Warning System · false activationTHE "ELEC" LIGHT ON OVERHEAD PANEL ILLUMINATED. ELEC PANEL SHOWED "AUX CHARGER BATT FAULT" INSP AUX BAT CHARGER CONNECTIONS FOUND NO DISCREPANCIES. RESET THE SYSTEM PERFORMED AMM TASK 24 31 31 710 801 AUX BAT CHARGER OPS TEST. GRN VERIFICATION NORMAL.Jan 14, 2011 · N587AS · Boeing 737890 · Battery/Charger SystemSDR ASAA1158744Unknown · malfunctionedTHE "STAB OUT OF TRIM" LIGHT ILLUMINATED WITH AUTOPILOT ON. MAIN ELECTRIC TRIM WORKS NORMAL. FCC B RECORDED TWO OCCURRENCES OF FAULT CODE 22 11830 "ELEVATOR AUTHORITY LIMITED". PERFORMED DFCS GROUP NR 1 (CURRENT STATUS) NR 11 (AUTOPILOT) AND NR 49 LAND VERIJan 9, 2011 · N587AS · Boeing 737890 · Autopilot SystemSDR ASAA1158723Idg · failedGENERATOR DISCONNECT NR 2 DRIVE LIGHT NOT WORKING. BULB CHECKS GOOD. REMOVED AND REPLACED NR 2 ENG IDG IAW AMM 24-11-11-400-801. OPS CHECK GOOD PER AMM 24-11-00.Jan 3, 2011 · N587AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1158709Unknown · malfunctionedON MASTER CAUTION RECALL CONT CAB ZONE TEMP CAUTION LT ILLUMINATED. NR 2 CTRLR SHOWS "FLT DECK TRIM VALVE" FAULT ON BIT & PREV FLT TESTS. VERIFY TEST GO. RESET FAULT. FAULT DID NOT RETURN. INTERMITTENT FAULT. BITE TEST NR 2 CTRLR GOOD. GND VERIFICATION GDec 28, 2010 · N587AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA1058615Apu · malfunctionedDESCENDING THROUGH 5000 FEET SOUR "DIRTY SOCKS" SMELL PRESENT IN FLT DECK. CONFIRMED APU IS THE SOURCE OF CABIN ODOR REF TASK 05 60 00 280 801C1. ALSO RAN BOTH PACKS WITH BOTH ENGINES. SMELL ONLY RETURNED WHEN APU WAS SELECTED. REMOVED AND REPLACED APU PERDec 8, 2010 · N587AS · Boeing 737890 · APU Core EngineSDR ASAA1058553Anti-Ice Valve · failedNR 2 ENG COWL VALVE OPEN LIGHT REMAINED BRIGHT BLUE AFTER COMMANDED ON. ASSOCIATED AMBER TAI WARNING ON CTR DISPLAY. REPLACED WITH SERVICEABLE COWL ANTI ICE VALVE REF AMM 30 21 11 400 801. RAN ENGINES PROBLEM STILL EXISTS SUSPECT OVERHEAD MODULE. REPLACED Nov 26, 2010 · N587AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA1058521Pump · failedMAIN FUEL TANK NR 2 / AFT "LOW PRESSURE" LIGHT ILLUMINATED C/B CHECKED IN. FOLLOWED QRC AFT FUEL PUMP OFF. "LOW PRESSURE" LIGHT STILL ILLUMINATED (WITH 8.00 FUEL INDICATION). RANG OUT INTERNAL WIRING OF NR 2 AFT PUMP RANG BAD WDM 28 23 11. REMOVED AND REPLNov 19, 2010 · N587AS · Boeing 737890 · Fuel Boost PumpSDR ASAA1058502Actuator · malfunctionedCROSSFEED VALVE CB OPEN. ACCOMPLISHED C/B RESET PROCEDURE PER AMM 20 60 01 CB DID NOT REMAIN SET. REMOVED & REPLACED FUEL CROSSFEED VALVE ACTUATOR ASSY PER AMM 28 22 21. ACFT OK FOR SERVICE.Nov 13, 2010 · N587AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA1058475Unknown · malfunctionedPRIOR TO LANDING ON SHORT FINAL FUEL CROSSFEED "VALVE OPEN" BLUE LIGHT FLICKED BRIGHT BLUE. ON TAXI IN LIGHT FLICKERED ALSO. CROSSFEED SEL CLOSED. PERFORMED FIM TASK 28 22 00 810 807 A/C CHECKS GOOD CROSS FEED VALVE OPS CHECKS GOOD ON GROUND. VERIFICATION Nov 3, 2010 · N587AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA1058282Shim · wornDURING ACCOMPLISHMENT OF NR 2 ENG FAN LUBE DETERMINED BLADE SHIMS PRESSURE FACE COATNG WORN. REMOVED AND REPLACED 24 EA BLADE SHIMS PER T/C 78472002.Sep 16, 2010 · N587AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA1058260Warning System · malfunctioned"FMC DISAGREE" WARNING ON THE GROUND IN OGG. RAN THROUGH THE QRH CHECKLIST OF RESETTING C/B'S. "FMC DISAGREE" WARNING WENT AWAY.Sep 8, 2010 · N587AS · Boeing 737890 · Central ComputersSDR ASAA1058230Idg · faultyNR 2 IDG HAS RECENT HISTORY OF FREQUENT SERVICING. REPLACED THE NR 2 ENGINE IDG REF MM 24 11 11. ALL OPS AND LEAK CHECKS GOOD. OK FOR SERVICE.Aug 26, 2010 · N587AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1058108Valve · malfunctionedON CLIMBOUT ABOUT 18,000 FT MSL LEFT DUCT PRESSURE 42 PSI RIGHT 42 PSI, ON LEVEL OFF LEFT 42 PSI RIGHT 12 PSI AT 41 000 FT. REPLACED THE NR 2 ENG HIGH STAGE VALVE REF MM 36 11 06 000 801 AND 36 11 06 400 801 STEP E THROUGH H. (2) OPS CHECK GOOD. REPLACED THEJul 27, 2010 · N587AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058106Regulator · failedDUCT SPLIT ON CLIMBOUT. CLIMBING THROUGH FL360 RT SIDE 20 PSI LT SIDE 42 PSI. N1'S 100.9 N2'S 97.1 OAT 49C. DURING THE HEALTH CHECK THE HIGH STAGE REGULATOR FAILED THE OVERPRESSURE FUNCTION AND BACKFLOW TESTS. REPLACED NR 2 ENG HIGH STAGE REGULATOR PER MM Jul 26, 2010 · N587AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058074Sensor · failedDUCT PRESSURE DIFFERENTIAL EXCEEDS 20 PSI DURING CLIMB: FL 370 100.1 PERCENT N1 53 DEG C L. 45 PSI R. 22 PSI FL 380 99.7 PERCENT N1 54 DEG C L. 43 PSI R. 22 PSI (CLIMB PWR) FL 380 90.2 PERCENT N1 54 DEG C L. 41 PSI R. 25 PSI (CRUISE PWR). REPLACED NR 2 ENGINEJul 14, 2010 · N587AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA1058049Regulator · failedDUCT PRESSURE SPLIT L=44 PSI R= 26 PSI AT CRUISE 35000FT N1 = 89.1 N2= 93.2 AFTER 4 HOURS OF FLIGHT THE PRESSURE BUMP LEFT CABIN RATE DESCENDED 400FPM AND DUCT PRESSURE SPLIT CHANGE TO L=40 PSI AND R= 32 PSI THAN BOTH TO ORIGINAL SPLIT 44/26. PERFORMED ENGINEJul 10, 2010 · N587AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA1058039Idg · faultyNR 2 IDG HAS RECENT HISTORY OF FREQUENT SERVICING. ACCOMPLISHED IDG OIL SYSTEM STATIC LEAK CHECK REF AMM 24 11 00 700 801. NO LEAK NOTED. REMOVED AND REPLACED IDG PUSH TO VENT VALVE REF AMM 24 11 00 700 804. REMOVED AND REPLACED PRESSURE FILL HALF COUPLINGJul 8, 2010 · N587AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA1058042Sensor · out of toleranceAPU FAULT LIGHT ON START UNABLE TO START. FOUND FAULT CODE 49 61224 INLET TEMP SENSOR SHOWS OUT OF RANGE HIGH. REMOVED AND REPLACED INLET TEMP SENSOR PER MM 49 61 31 400 801. OPS CHECK GOOD.Jul 6, 2010 · N587AS · Boeing 737890 · APU Indicating System
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