N517AS

Service difficulty reports · 449

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 = 'N517AS' 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 ASAA2014052307915Warning Message · false activationFMC DISAGREE MESSAGE DISPLAYED DURING TAXI. ACFT GROUNDED. COMPLETED QRH STEPS, NORMAL FMC OPERATION RESUMED.May 23, 2014 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014051507827Circuit Breaker · trippedCIRCUIT BREAKER TRIPPED - P6-2 A3, ACFT GROUNDED. PERFORMED CIRCUIT BREAKER RESET PROCEDURE IAW AMM 20-60-01. CIRCUIT BREAKER REMAINS SET. PERFORMED IFSAU OPS CHECK IAW AMM 22-11-37. BITE AND OPS TEST PASSES. ACFT OK FOR SERVICE.May 15, 2014 · N517AS · Boeing 737890 · AC Power Distribution SystemSDR ASAA2014042007549Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ENGAGE IN FLIGHT. ACFT GROUNDED. ACCOMPLISHED BITE OF AUTOTHROTTLE IAW FIM 22-31, TASK 801. FOUND LT ADIRU NO DATA FAULT 22-31004. RESET LT ADIRU CIRCUIT BREAKERS, IAW AMM 20-60-01-860-801. ACCOMPLISHED BITE TEST OF ADIRU`S LT & RT,Apr 20, 2014 · N517AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2014041807504Lamp · dirtyFWD CARGO EXTIGUISHER WILL NOT TEST. BULB OK. ACFT GROUNDED. CLEANED LAMP ASSY AND TESTS NORMAL IAW FIM 26-23, TASK 812.Apr 18, 2014 · N517AS · Boeing 737890 · Extinguishing SystemSDR ASAA2014041607481Controller · malfunctionedON RECALL LT PACK LIGHT IS ON THE LIGHT GOES OUT WHEN MASTER CAUTION IS PUSHED. ACFT GROUNDED. ONE PREVIOUS FLT FAULT OF "THIS PACK TCV" ON NR 1 ZONE TEMP CONTROLLER. PERFORMED PACK/ZONE TEMP CONTROLLER BITE REF MM 21-61-00-700-806-002 W/ NO DEFECTS NOTED. FApr 16, 2014 · N517AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2014040407442Warning Light · false activationNR 1 BLEED TRIP OFF ILLUMINATED 5 MINUTES AFTER LEVELING OFF AT FL 410. TRIP RESET IAW QRH. DESCENDED TO FL 370, 5 MINUTES AFTER LEVEL OFF, NR 1 BLEED TRIP OFF ILLUMINATED AGAIN. ONCE AGAIN RESET IAW QRH. BOTH TIMES PRESSURIZATION REMAINED AT CRUSING ALT OR 8Apr 4, 2014 · N517AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014033107381Sign · brokenFOUND EXIT SIGN BROKEN, COVER & BASE. ACFT GROUNDED. R & R SIGN ASSY. OPS CHECKED GOOD.Mar 31, 2014 · N517AS · Boeing 737890 · Emergency LightingSDR ASAA2014022306959Static Inverter · failedELEC LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED FIM TASK 24-34-TASK 801. STATIC INVERTER INOPERATIVE. WOULD NOT RESET. REMOVED STATIC INVERTER IAW AMM 24-34-21-000-801. INSTALLED NEW STATIC INVERTER IAW AMM 24-34-21-400-801. GROUND OPS CHECK GOOD.Feb 23, 2014 · N517AS · Boeing 737890 · DC Generating SystemSDR ASAA2014012612498Warning Message · false activationSINGLE FMC OPERATION ON SCRATCH PAD. SEVERAL MINUTES LATER LNAV / VNAV DISSCONNECTED POS PAGE 3 SHOWED NO DATA FROM R-FMC. FOLLOWED QRH SELECTED FMC BOTH ON LT CONTINUED NORMALLY. NO VTX ON F/O SIDE (ONLY INFO ON R-FMC WAS POS PAGE NR 3). ACFT GROUNDED. PJan 26, 2014 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014012212427Idg · damagedTHE NR 1 ENGINE IDG HAS A HISTORY OF REQUIRING FREQUENT SERVICING. ACFT GROUNDED. REMOVED NR 1 ENGINE IDG IAW TASK 24-11-11-000-801, INSTALLED NR 1 ENGINE IDG IAW TASK 24-11-11-400-801. PERFORMED OPS TEST ON NR 1 ENGINE IDG IAW TASK 24-11-00-700-802. NO LEJan 22, 2014 · N517AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2014011912406Controller · faultedRECEIVED A ZONE TEMP LIGHT, RAN QRH PROCEDURES AND UPON RESETING MASTER CAUTION, LIGHT WENT OUT. ACFT GROUNDED. AUTO TEMP CONTROLLER LOGGED COCKPIT TRIM VALVE FAULT. RAN BOTH AUTO TEMP CONTROLLERS BITE TEST IAW FIM 21-62, TASK 842 AND FAULT CLEARED AND RESETJan 19, 2014 · N517AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013121712161Control Valve · failedLEFT PACK LIGHT ILLUMINATED DURING RECALL, PACK LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. R & R LT TEMP CONTROL VALVE IN REF AMM 21-51-10. PERFORMED OPS CK IAW MM 21-51-10-400, PASSED.Dec 17, 2013 · N517AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013112896570Actuator · faultedON MASTER CAUTION RECALL RT PACK LIGHT ILLUMINATED WILL RESET. ACFT GROUNDED. LOGGED RAM AIR ACTUATOR FAULT. R & R RT RAM AIR ACTUATOR REF MM 21-51-21, GROUND FUNCTION, OPS CHECK GOOD.Nov 28, 2013 · N517AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013112896569Controller · malfunctionedDURING FINAL APPROACH, PUSHED RECALL AND RECEIVED A RT PACK LIGHT. RAN CHECKLIST, LIGHT STAYED ILLUMINATED. ACFT GROUNDED. PERFORMED BIT TEST OF BOTH PACK ZONE TEMP CONTROLLERS, NR 2 CONTROLLER SHOWED RAM AIR ACTUATOR FAULT ON BIT TEST. PREVIOUS FLT WAS GONov 28, 2013 · N517AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013111496508Skin · crackedLEFT HORIZONTAL STAB LOWER SURFACE SKIN CRACKED AT STAB STA 138.70. ACFT GROUNDED. REMOVED DAMAGE AND REPAIRED ON LT HORIZONTAL STAB LOWER SURFACE SKIN AT STA 138.20 IAW SRM 55-10-01, SRM 51-40-02. ALODINED AND PRIMED IAW SRM 51-20-01 AND TOP COATED IAW AMMNov 14, 2013 · N517AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2013111496507Floor Support · corrodedAFT CARGO, FLOOR SUPPORT CORRODED AT RBL 6 BETWEEN 727 & 727A. ACFT GROUNDED. BLENDED AREA ORIGINAL THICKNESS .63, REMOVED .009 REMAINING .054 AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 1A-2. REMOVED DAMAGE SECTION IAW SRM 53-00-53 REPAIRED. LOCATED ANov 14, 2013 · N517AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013111496481Channel · corrodedFWD CARGO FLOOR STRUCTURE, LT SIDE TRANSITION PANEL HAS CORROSION AROUND OUTER EDGE FASTENER HOLES FROM BS 500D-500F. REMOVED CORROSION ON 3 HOLE BETWEEN STA 500D-BS 500F. ORIG MATERIAL .040" MATERIAL LOSS BN HOLE NR 1 & 2 BETWEEN STA 500D & 500E .003 & .002Nov 14, 2013 · N517AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013111396524Doubler · bentEXTERNAL FUSELAGE, POWER RECEPTACLE DOOR 114AR CUTOUT INNER DOUBLER BENT AT AFT EDGE. ACFT GROUNDED. REMOVED DAMAGE, PERFORMED DVI AND HFEC INSP, VERIFIED SURFACE ROUGHNESS OF 63RA, VERIFIED THICKNESS OF .058 REFINISHED AREA IAW REO G16904, REV A AND EA 80Nov 13, 2013 · N517AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2013111396523Skin · nickedEXTERNAL FUSELAGE, POWER RECEPTACLE DOOR 114AR CUTOUT INNER DOUBLER NICKED AT UPPER FWD EDGE. ACFT GROUNDED. REMOVED DAMAGE, ACCOMPLISHED DVI, HFEC INSPECTIONS, SURFACE ROUGHNESS TEST OF 63RA, DOUBLER THICKNESS VERIFICATION OF .039 AND REFINISHED THE AREA IANov 13, 2013 · N517AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2013111396522Doubler · bentEXTERNAL FUSELAGE, POWER RECEPTACLE DOOR 114AR CUTOUT INNER DOUBLER BENT AT FWD CENTER AREA. ACFT GROUNDED. REPAIRED EXT POWER DOOR DOUBLER IAW REO G16904, REV A DATE 11-24-13 AND EA 800-53EA-11655, REV NEW DATE 25, NOV 2013.Nov 13, 2013 · N517AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2013102096207Exciter · unknownAPU FAILED TO START. RECEIVED A FAULT LIGHT AND MAINT MESSAGE 49-41180. ACFT GROUNDED. STARTED APU NUMEROUS TIMES SUCCESSFULLY. FAULT CODE DOES NOT REAPPEAR. OPS CHECKED GOOD IAW FIM 49-40, TASK 804. REMOVED AND REPLACED APU IGNITION EXCITER OPS CHECKEDOct 20, 2013 · N517AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2013100296096Warning Message · false activationFMC DISAGREE LIGHT ILLUMINATED ON GROUND. ACFT GROUNDED. PERFORMED QRH PROC LIGHT WENT AWAY.Oct 2, 2013 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013091795994Director · malfunctionedFLIGHT DIRECTOR DID NOT CAPTURE THE APPROACH, MADE IN THE LOCALIZER GUIDANCE, RAW DATA FUNCTIONED OK. ACFT GROUNDED. VERIFIED WITH FLIGHT CREW DEFECT ON F/O SIDE ACCOMPLISHED DFCS BITE TEST IAW AMM 22-11-00, CURRENT STATUS SHOWS NO FAULTS ON CH B. ADDITIONALSep 17, 2013 · N517AS · Boeing 737890 · Autopilot SystemSDR ASAA2013081295784Fmc · false indicationFMC DISAGREE ON THE GROUND. ACFT GROUNDED. COMPLIED WITH QRH OPS NORMAL.Aug 12, 2013 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013071695626Control Valve · inoperativeLEFT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. R & R LT PACK TCV IAW MM 21-51-10. BITE CHECKED GOOD.Jul 16, 2013 · N517AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013071495601Fmc · false indicationFMC DISAGREE ON TAXI OUT. ACFT GROUNDED. COMPLETED QRH, OPS NORMAL THEREAFTER.Jul 14, 2013 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013062495292Coupler · failedNR 1 HF WAS UNREADABLE ON ALL ASSIGNED FREQUENCIES THROUGHOUT THE FLIGHT. NR 2 HF WORKED 5X5 GOOD ON ALL FREQUENCIES. ACFT GROUNDED. CONFIRMED FAULT WITH NR 1 HF, REF FIM 23-11-806. SWAPPED 1 HF AND NR 2 HF COUPLERS FOR TROUBLESHOOTING, REF MM 23-11-61. FAJun 24, 2013 · N517AS · Boeing 737890 · Communications System WiringSDR ASAA2013061695116Fmc · warning lightDURING TAXI FMC DISAGREE CAME ON. ACFT GROUNDED. DID STEPS IN QRH & FMCS RETURNED TO NORMAL OPS.Jun 16, 2013 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013061595106Display · malfunctionedTWO HOURS INTO ETOPS FLIGHT, CAPTAIN`S FMC/CDU SCREEN WENT BLANK FOR 10 TO 15 SECONDS FOLLOWED BY A BITE TEST MESSAGE ON THE SCREEN. OTHER INDICATIONS WERE ILLUMINATION OF ALL CAPTAINS FMC/CDU ALERT LIGHTS (CALL ECT). NO OTHER ANOMALIES NOTED. NO MAP OR VTKJun 15, 2013 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013052294878Warning Light · false activationNR 1 ENG COWL VALVE OPEN LIGHT REMAINED ILLUMINATED WITH NR 1 ENG ANTI ICE OFF SELECTED. ACFT GROUNDED. ACCOMPLISHED ENG NR 1 REF FLT HANDBOOK 5.030, PG 20. CYCLED NR 1 ENG ANTI-ICE VALVE, NUMEROUS TIMES, OPS NORMAL.May 22, 2013 · N517AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2013050494689Battery · dischargedBATTERY INDICATES 14 VOLTS -11 VOLTS. AUX BATTERY INDICATES 14 VOLTS - 12 VOLTS. ACFT GROUNDED. REPLACED MAIN BATTERY REF MM 24-31-11, OPS CK OK. R & R AUX BATTERY REF MM 24-31-11. OPS NORMAL IAW SAME. ETOPS GROUND VERIFICATION TEST SUCCESSFUL.May 4, 2013 · N517AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2013042994649Warning Light · false activationFMC DISAGREE DISPLAYED. ACFT GROUNDED. RAN QRH. NO FURTHER PROBLEMS.Apr 29, 2013 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013042794622Warning Light · illuminatedNR 1 ENGINE COWL VALVE OPEN LIGHT ILLUMINATED WITH NR 1 ENGINE ANTI ICE OFF SELECTED. ACFT GROUNDED. ACCOMPLISHED ENG RUN (NR 1) REF FLT HANDBOOK 5.030 PG 20. CYCLED NR 1 ENG ANTI-ICE OPS NORMAL. OK FOR SERVICE.Apr 27, 2013 · N517AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2013042194558Fmc · malfunctionedFMC DISAGREE LIGHT ON TAXI. EXECUTED QRH CHECKLIST. SYS RETURNED TO NORMAL OPS.Apr 21, 2013 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013031594176Control Unit · faultedLIGHT ON OVERHEAD PANEL OBSERVED ON PREFLIGHT. SPCU FAULT LOGGED WILL NOT RESET. REPLACED SPCU IAW AMM 24-34-11, OPS CKD NORMAL. ALL GROUND FUNCTIONAL TESTS GOOD.Mar 15, 2013 · N517AS · Boeing 737890 · DC Generating SystemSDR ASAA2013010293595Sensor · looseTHERE IS A SOUND COMING FROM THE OVERHEAD PANEL OVER SEAT 1D AND BELOW THE CABIN BIN. FOUND VIBRATING FWD CABIN TEMP SENSOR. SECURED SENSOR AND VIBRATION GONE REF AMM 21-61-10.Jan 2, 2013 · N517AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2012123093581Charger · malfunctionedDURING PREFLIGHT OVERHEAD ELEC LIGHT WAS ILLUMINATED. ACCOMPLISHED P5-13 BITE PROCEDURE IAW FIM TASK 24-31, TASK 801. FOUND FAULT MESSAGE FOR BATTERY CHARGER INOPERATIVE. CLEARED FAULT. ACCOMPLISHED BATTERY CHARGER OPERATIONAL TEST IAW AMM 24-31-21-710-80Dec 30, 2012 · N517AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2012122593537Warning Light · false activationELECRICAL LIGHT DISPLAYED ON OVERHEAD PANEL. PERFORMED P5-13 BITE PROCEDURE IAW FIM 24-31, TASK 801 BATTERY CHARGER INOPERATIVE, ONE MX MESSAGE. CLEARED MESSAGE, ALL SYS CHECKED NORMAL. ACFT OK FOR SERVICE.Dec 25, 2012 · N517AS · Boeing 737890 · Central WarningSDR ASAA2012122393531Battery Pack · failedEMERGENCY LIGHT POWER SUPPLY M1873 BATTERY PACK FAILS DEEP CYCLE CHECK. REF SSM 33-51-14 R & R AND TESTED BATTERY PACK FOR EMERGENCY LIGHT POWER SUPPLY M1873 IAW MM 33-51-06-960-805. OPS NORMAL.Dec 23, 2012 · N517AS · Boeing 737890 · Emergency LightingSDR ASAA2012121993510Window · malfunctionedDURING CLIMBOUT, THE LT SIDE WINDOW OVERHEAT AMBER LIGHT ILLUMINATED. THE QRC PROCEDURE WAS ACCOMPLISHED. THE WINDOW HEAT SWITCH WAS OFF FOR 5 MINUTES & AT THAT POINT TURNED BACK ON ( FL220) 710 LATER AT FL 320,THE AMBER LIGHT ILLUMINATED AGAIN. UNABLE TO DUDec 19, 2012 · N517AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012121893485Sensing Element · failedAFTER TAKEOFF, THE LT SIDE WINDOW OVERHEAT AMBER LIGHT ILLUMINATED. QRH PROCEDURE WAS ACCOMPLISHED. AFTER THE POWER TO THE WINDOW WAS OFF FOR 3 MINUTES - IT WAS TURNED BACK ON. THE AMBER LIGHT RE-ILLUMINATED AFTER 35 SECONDS. ACFT GROUNDED. VERIFIED FAULDec 18, 2012 · N517AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012121893484Controller · faultyWINDOW HEAT LT-SIDE AMBER LIGHT CAME ON IN FLIGHT. QRH ACCOMPLISHED OFF 5 MINS THEN ON AFTER 2 MINS AMBER LIGHT CAME ON. MOVED TO OFF REMAINDER OF FLIGHT. PERFORMED FIM 30-41-801. BITE TEST OK. FAULT HISTORY HAS WINDOW SENSOR FAULT. PERFORMED TASK 30-41-811 Dec 18, 2012 · N517AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012121893483Warning Light · false activationL2 WINDOW OVERHEAT LIGHT ILLUMINATED, TURNED OFF L2 WINDOW HEAT FOR 5 MINUTES IAW QRH PROCEDURE 3.3. TURNED ON L2 WINDOW HEAT, L2 WINDOW OVERHEAT LIGHT ILLUMINATED AGAIN AFTER 45 MINUTES. L2 WINDOW HEAT SWITCH PLACED OFF. TURNED WINDOW HEAT ON FOR 90 MINDec 18, 2012 · N517AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012120993427Circuit Breaker · trippedAFTER START RECALL MACH TRIM FAIL LIGHT ILLUMINATED. FOUND P18-1 D4 CIRCUIT BREAKER TRIPPED, AFCS SYS A, MACH TRIM DC. RESET CIRCUIT BREAKER IAW PROCEDURES REF MM 20-60-01. PERFORMED CURRENT STATUS QUICK TEST (GROUP 10) AND MACH TRIM SYS (GROUP 13) BITES REFDec 9, 2012 · N517AS · Boeing 737890 · Speed-Attitude Correction SystemSDR ASAA2012120793420Warning Light · false activationFMC DISAGREE CAUTION LT ON BOTH NAV DISPLAYS DURING TAXI OUT. PERFORMED QRH AND SYS RESET PROPERLY. CONTINUED WITH FLIGHT.Dec 7, 2012 · N517AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012112593369Circuit Breaker · unknownSTANDBY BATTERY CIRCUIT BREAKER OPEN. RESET M1720 CIRCUIT BREAKER. PERFORMED OPS IAW MM 24-34-11-400-801. OPS NORMAL. GROUND VERIFICATION GOOD.Nov 25, 2012 · N517AS · Boeing 737890 · Electrical Power SystemSDR ASAA2012111493299Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. LIGHT RESETS NORMALLY. ZONE TEMP CONTROLLER NR 2 WITH FLT DECK TRIM VALVE FAULT. RESET AND BOTH ZONE TEMP CONTROLLERS BITE TEST NORMAL IAW FIM 21-61, TASK 801.Nov 14, 2012 · N517AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2012103093213Warning Light · false activationCABIN ZONE TEMP ILLUMINATED DURING RECALL ON APPROACH. RESET TO SATISFACTION. RESET SYS, RAN PACKS AND THEN TESTED CONTROLLERS. OPS CHECKED GOOD AMM REF 21-61-20-400-801. GROUND VERIFICATION GOOD IAW AMM 21-61-20-400-801.Oct 30, 2012 · N517AS · Boeing 737890 · Central WarningSDR ASAA2012102093155Sensor · failedAT FL 400, DURING SLIGHT POWER REDUCTION FOR SPEED CHANGE, LT BLEED TRIP OFF LIGHT ILLUMINATED. PRESSURIZATION NORMAL. RESET OK. NR 1 N1 86.6, NR 1 N2 90.9. LEFT BLEED TRIP OFF, OCCURED AGAIN DURING INITIAL DESCENT, FL400. RESET OK AGAIN. ACCOMPLISHED NOct 20, 2012 · N517AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2012100493019Warning Message · false activationRECEIVED SINGLE FMC OPERATION WITH MAP INDICATED ON RT NAV DISPLAY. ACCOMPLISHED QRH PROCEDURES BUT NEVER GOT DUAL FMC OP RESTORED MSG. SUSPECT RT FMC FAILURE. ACFT GROUNDED. CHECKED FMC COMPUTER, NO CURRENT FAULTS STORED, NO FAULT LIGHT ON FRONT OF COMPUTEROct 4, 2012 · N517AS · Boeing 737890 · Flight Management Computing Hardware System
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