N564AS

Service difficulty reports · 539

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 = 'N564AS' 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 ASAA2022050338371Sidewall Support · corrodedAFT PIT STA 727D L/H SIDEWALL SUPPORT HAS CORROSION AT TRANSITION. GROUNDED - YES. REMOVED AND REPLACED SIDEWALL SUPPORT IAW B737-800 SRM 51-40-02-0G-0.W= 2.0" O= .071" R= .061" L= 1.010" D= .010".May 3, 2022 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2022050338370Sidewall Support · corrodedAFT PIT STA 727D R/H SIDEWALL SUPPORT HAS CORROSION AT TRANSITION. GROUNDED - YES. REMOVED AND REPLACED SIDEWALL SUPPORT IAW B737-800 SMR 51-40-02-0G-0.W= 1.3" O= .063" R= .051" L= 1.012" D= .012".May 3, 2022 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2022050338369Transition Panel · corrodedAFT PIT L/H TRANSITION HAS AREAS OF CORROSION STA 727 TO 847. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSTIION PANEL PANEL WAS FOUND TO BE OUT OF LIMITS FROM STA 727Z-10 TO STA 847 IAW B737-800 SRM 53-00-53-1A-2. FABRICATED AND INSTALLED NEW L/H TMay 3, 2022 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2022050338368Transition Panel · corrodedAFT PIT R/H TRANSITION HAS AREAS OFF CORROSION STA 727 TO 787. GROUNDED - YES. REPAIRED TRANSTIION PANEL R/H FROM STA 727- STA 787 IAW B737-800 SRM 51-40-02-0G-0.W= 4 O= .040 R= .010 L= 1.0 D= .030.May 3, 2022 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2022040437888Unknown · faultyDURING CLIMB OUT OF SEA @1000' COMMAND BARS ON BOTH CA & FO ALTITUDE DISPLAYS DISAPPEARED & LNAV AND VNAV ON MCP WERE UNABLE TO RESELECT. NO MCP MODES WERE SELECTABLE. UPON RESETTING MCP ALTITUDE SELECTOR TO HIGHER ALTITUDE, THE ALTITUDE WINDOW TWICE INDICATEDApr 4, 2022 · N564AS · Boeing 737890 · Autopilot SystemSDR ASAA2022040237867None · noneAUTOPILOT B DISENGAGED DURING DESCENT. WOULD NOT RE ENGAGE NO OTHER LIGHTS OR WARNINGS ENGAGES AUTOPILOT A NO ISSUES. GROUNDED - YES. PERFORMED DFCS BITE REF B737-800 FIM 22-11 TASK 801 FOUND FAULTS FOR MCP CHAN A+B 22-11607. DUE TO INSTALLED MCP S/N 01687669 Apr 2, 2022 · N564AS · Boeing 737890 · Autopilot SystemSDR ASAA2022032737805Control Panel · inoperativeVERTICAL SPEED RATE WHEEL INOP. GROUNDED - YES. REPLACED MODE CONTROL PANEL, OPS CHECKS GOOD. REF B737-800 AMM 22-11-34.Mar 27, 2022 · N564AS · Boeing 737890 · Autopilot SystemSDR ASAA2022031137674Unknown · unknownUPON LANDING BOTH FMC PAGES STOPPED DISPLAYING ON BOTH MCDUS. SHORTLY AFTER THE MENU PAGE SHOWED BOTH MCDUS WITHOUT SHOWING THE FMC SELECTION AT SELECTION KEY 1L. SHORTLY AFTER THAT THE FMC SELECTION CUE APPEARED AT 1L ON MENU PAGE UPON SELECTION OF FMC ALL DAMar 11, 2022 · N564AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2022030837652Unknown · unknownHF #1 FAIL/FAIL ON RTP. GROUNDED - YES. PERFORMED HF BITE PROCEDURE IAW B737-800 FIM 23-11 TASK 801 NO FAULTS. PERFORMED HF1 OPS CHECK IAW B737-800 AMM 23-11-00-710-801 OPS CHECK GOOD ON GROUND.Mar 8, 2022 · N564AS · Boeing 737890 · HF Communications SystemSDR ASAA2022030837651Unknown · unknownVERT SPEED WHEEL ON MCP NOT CONTROLLING/ INOP. GROUNDED - YES. PERFORMED DFCS BITE LIBRARY TEST REF B737-800 AMM 22-11-00-740-806 GROUP # 60.56 MCP VERTICAL SPEED KNOB TEST PASS. NO DEFECTS NOTED.Mar 8, 2022 · N564AS · Boeing 737890 · Autopilot SystemSDR ASAA2022013137317Unknown · unknownZONE TEMP LIGHT ON. GROUNDED - YES. #2 TEMP CONTROLLER LOGGED " FLT DECK" TRIM AIR VALVE FAULT LAST FLT. PERFORMED B737-800 FIM 21-62 TASK 842 AND FAULT CLEARED. OPS CKS NORMAL.Jan 31, 2022 · N564AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2022011337137Unknown · unknownELEC LIGHT ILLUMINATED ON TAXI. GROUNDED - YES. FAULT OCCURRED AFTER POWER TRANSFER ACCOMPLISHED B737-800 FIM 24-31 TASK 801 AUX BATT CHARGER AND STAT INV FAULTED. SYSTEM RESET, NORMAL INDICATOR RESTORED. A/C OK FOR SERVICE.Jan 13, 2022 · N564AS · Boeing 737890 · DC Generating SystemSDR ASAA2022011037114Lamp · inoperativeEMERGENCY LIGHT AREA LIGHT (AISLE LIGHT) INOP AT ROW 16 LEFT. GROUNDED - YES. RELAMPED AND TESTED PER B737-800 AMM 33-51-03-960-801 - OPS NORMAL.Jan 10, 2022 · N564AS · Boeing 737890 · Emergency LightingSDR ASAA2021102736416Platform · damagedPER T/C 78472010 #1 ENG. FAN BLADE LUBE PLATFORMS #2, 13, 18,19,21, AND 23 ELASTOMER SEALS ARE TORN. GROUNDED - YES. REMOVED AND REPLACED #1 ENG FAN BLADE PLATFORMS #2, 13, 18, 19, 21 AND 23. REF T/C 78472010.Oct 27, 2021 · N564AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2021101536312Unknown · unknownCONT CAB ZONE TEMP LIGHT COMES ON AFTER PRESSING RECALL. RESETS AFTER PRESSING MASTER CAUTION. GROUNDED - YES. FOUND CONTROL CABIN TRIM AIR VALVE FAULT ON RIGHT PACK TEMP CONTROLLER. WAS ABLE TO RESET FAULT. OPS CHECK GOOD I/A/W FIM 21-62 TASK 832.Oct 15, 2021 · N564AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2021082635818Bleed Valve · leakingAFTER ENG START, DUCT PRESSURE #2 DUCT INDICATED NORMAL POST. ENG START PRESSURE DURING CLIMB AFTER T/O, DUCT PRESSURE #2 INDICATED 5-10 PSI. (#1 WAS APPROX 40 PSI) A/C WAS PRESSURIZING NORMALLY. CLIMBING THROUGH 10,000 OR SO DUCT PRESSURE #2 POPPED UP TO APPRAug 26, 2021 · N564AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2021080655631Warning Light · false activationELEC LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED BITE TEST PER B737-800 FIM 24-31 TASK 801. STAT INV 1 FAULT CLEARED. NO FAULTS EXIST NOW.Aug 5, 2021 · N564AS · Boeing 737890 · Central WarningSDR ASAA2021060835057Lens · missingF/A REPORTED 16A EMERGENCY EXIT SIGN LENS MISSING. GROUNDED - YES. REPLACED W/NEW EMERGENCY EXIT SIGN LENS AND OK FOR SVC.Jun 8, 2021 · N564AS · Boeing 737890 · Emergency LightingSDR ASAA2021052534906Display · failedFAIL DISPLAYED ON HF2 RECEIVER. GROUNDED - YES. PERFORMED BITE TEST OF HF2 RECEIVER LRU PER SUBTASK B737-800 FIM 23-11-00-860-007. TEST GOOD. PERFORMED OPERATIONAL TEST B737-800 AMM 23-11-00. TEST OK. FAIL LIGHT WENT OUT. ACFT OK FOR SERVICE.May 25, 2021 · N564AS · Boeing 737890 · HF Communications SystemSDR ASAA2021041134587Control Valve · failedON MASTER CAUTION RECALL CONT CAB ZONE TEMP LIGHT ILLUMINATES EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. CONFIRMED FAULT, #2 PACK/ZONE TEMP CONTROLLER SHOWS HARD FAIL "FLIGHT DECK TCV". REMOVED & REPLACED FLIGHT DECK TCV (V143) REF B737-800 AMM 21-6Apr 11, 2021 · N564AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2021030134234Harness · shortedDESCENDING THROUGH 9000' LEFT VIB WENT UP TO AT LEAST 4.9 WITH FLASHING BOX. A/T DISCONNECTED. ENGINES AT OR CLOSE TO IDLE. VIB DROPPED TO 3.9 THEN POWER WAS BROUGHT UP AND NORMAL FOR REMAINDER OF FLIGHT. GROUNDED - YES. FLIGHT LEG 6 OF FLIGHT HISTORY RECORDEDMar 1, 2021 · N564AS · Boeing 737890 · Engine Vibration AnalyzerSDR ASAA2021022034146Pump · failedAFTER ENGINE START AT THE GATE, NUMBER 2 ENG HYDRAULIC PRESS LOW ILLUMINATED, AND STAYED ILLUMINATED. GROUNDED - YES. CHECKED PUMP DEPRESSURIZING C/B FOUND IN, CHECKED CANNON PLUG ON PUMP OR DRY MOTORED NR 2 ENG. VERIFIED NO PRESSURE AND LOW PRESS LT STAYEDFeb 20, 2021 · N564AS · Boeing 737890 · Hydraulic Pump (Electric/Engine), MainSDR ASAA2021020634050Warning Message · illuminatedDURING CLIMBOUT, TURNED ON THE ENGINE A/I ( HIGH POWER SETTING) AND GOT AN AMBER TAI ON THE #2 ENGINE AS WELL AS THE "COWL VALVE OPEN" BLUE LIGHT REMAINED BRIGHT BLUE. CYCLED SEVERAL TIMES AT DIFFERENT ALTITUDES BUT INDICATIONS REMAINED. AT LEVEL OFF W/ REDUCEFeb 6, 2021 · N564AS · Boeing 737890 · Engine Anti-Icing SystemSDR ASAA2020122833779Warning Message · false activationZONE TEMP ILLUMINATED FOR CONT CAB, IT WENT OUT DURING MASTER CAUTION RESET. GROUNDED-YES. INSPECTED AND FOUND NR 2 PZTC WITH "FLT DECK TRIM VLV " FAULT LOGGED 1 TIME. ACCOMPLISHED PZTC BITE, REF B737-800 AMM 21-61-00. FAULT ABLE TO RESET. GROUND RAN PACKDec 28, 2020 · N564AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2020122533747Transceiver · inoperativeHF NR 2 INOPERABLE ON TRANSMIT & RECEIVE. GROUNDED-YES. FOUND BITE ON NR 2 HF TRANSCEIVER INOPERABLE. REMOVED AND REPLACED NR 2 HF TRANSCEIVER, IAW B737-800 AMM 23-11-21. OPERATIONS CHECKS GOOD. GROUND VERIFICATION GOOD.Dec 25, 2020 · N564AS · Boeing 737890 · HF Communications SystemSDR ASAA2020122033727Acoustic Panel · looseREF T/C 78472000, NR 2 ENGINE INLET AND FAN BLADES DETAILED INSPECTION FOUND AFT LOWER ACOUSTICAL PANEL LOOSE, RT SIDE ALF. GROUNDED-YES. REMOVED AND REPLACED 1 BROKEN NUTPLATE AT 4 O'CLOCK POSITION, REF B737-800 SRM 51-40-02. PANEL PREVIOUSLY INSTALLED, SEDec 20, 2020 · N564AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2020121833724Drive Unit · failedWHEN ATTEMPTING TO USE WX RADAR THE "WXR FAIL" MESSAGE COMES ON ON ND SCREEN. GROUNDED-YES. ACCOMPLISHED "WEATHER RADAR ANTENNA PROBLEM" FAULT ISOLATION, SHOWS "WXR FAIL ANT" MESSAGE. REMOVED & REPLACED WXR ANTENNA DRIVE UNIT, REF B737-800 AMM 34-43-11, "WXDec 18, 2020 · N564AS · Boeing 737890 · Weather Radar SystemSDR ASAA2020100133269Hmu · faultedON LINE-UP FOR TAKE-OFF, BEFORE POWER APPLIED, MASTER CAUTION-ENGINE CONTROL LIGHT NR 2 IN ALT AND LIGHT DID NOT EXTINGUISH. GROUNDED-YES. RAN B737-800 FIM TASK 73-00 TASK 801 EEC BITE SHOWS FAULTS 75-10582 AND 75-30532. RAN AFT TEST B737-800 AMM TASK 71-00Oct 1, 2020 · N564AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2020092933239Warning Light · false activationNR 2 ENGINE CONTROL LIGHT ILLUMINATED ON LANDING. GROUNDED-YES. FOUND FAULT CODE 75-10582 ACCOMPLISHED ACTUATORS TEST, PER B737-800 FIM 71-00-00-700-807-F00. TEST PASSED NO ACTUATORS, TEST FAULTS, OK FOR SERVICE.Sep 29, 2020 · N564AS · Boeing 737890 · Central WarningSDR ASAA2020091423180Warning Light · false activationENG NR 2 ENGINE CONTROL LIGHT ILLUMINATED ON TOUCHDOWN. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 75-23 TASK 801 FOR ENGINE CONTROL CDU MESSAGE 75-20582. ACTUATORS TEST PASSED, LIGHT EXTINGUISHED. COULD NOT DUPLICATE FAULT WITH ENGINE RUN. FAULT INTERMITTSep 12, 2020 · N564AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2020090843138Modulating Valve · failedZONE TEMP LIGHT CAME ON DURING AFTER START. LIGHT WENT OUT AFTER RESETTING. GROUNDED - YES. HAD FLIGHT DECK TRIM VALVE FAULT. REMOVED AND REPLACED FLIGHT DECK TRIM VALVE MODULATING VALVE, IAW B737-800 AMM 21-61-21-000-801 AND AMM 21-61-21-400-801. ETOPS GSep 4, 2020 · N564AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2020090843137Actuator · failedON MASTER CAUTION RECALL, LEFT PACK LIGHT ILLUMINATED. EXTINGUISHED ON MC RESET. GROUNDED - YES. LEFT RAM AIR ACTUATOR FAULT SHOWN. R & R LEFT RAM ACTUATOR, REF B737-800 AMM 21-51-21. TEMP CONTROLLER BITE CHK GOOD. MASTER CAUTION RESET NORMAL.Sep 4, 2020 · N564AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2020081633038Warning Light · false activationMASTER CAUTION AIR COND LIGHT ILLUMINATED AFTER RUNNING DESCENT CHECKLIST. LEFT PACK LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER PRESSING MASTER CAUTION - PRESS TO RESET, RAN QRH 12.2. GROUNDED - YES. NR 1 ZONE CONT LOGGED RAM AIR ACT FAULT. FAULT CLEAREDAug 16, 2020 · N564AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2020080332972Blade · failed#2 ENGINE TREND DATA STILL SHOWS A RISE IN LOW PRESSURE ROTOR VIBRATION LEVELS WITH EXCESSIVE FAN SCATTER. GROUNDED - YES. FAN LUBE PREFORMED REF TC 7842010, REPLACED 1 PLATFORM & 1 SPACER. TEST 7 ACCOMPLISHED AL VIBS WITH NORMAL LIMIT.Aug 3, 2020 · N564AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2020072732935Check Valve · corrodedWHILE ACCOMPLISHING NG-36EO-22817-1, FOUND BOTH 5TH STG BLEED AIR CHECK VALVES CORRODED OUT OF LIMITS. GROUNDED - YES. REMOVED AND REPLACED #1 AND #2 ENGINE 5TH STG BLEED AIR CHECK VALVES. REF B737-800 AMM 36-11-02.Jul 23, 2020 · N564AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2020062232814Transition Panel · corrodedAFTER REMOVAL OF SIDEWALL PANEL FOUND TRANSITION PANEL ON LEFT SIDE AT STA 727D+10 TO BE EXFOLIATED. GROUNDED - YES. REPAIRED TRANSITION SECTION IAW SRM 53 00 53 2R 5 W 2" O .040" R 0 L 2" D .040".Jun 4, 2020 · N564AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2020062232815Battery Pack · dischargedEMERGENCY LIGHTS AT R2 DOOR OUTSIDE LIGHT, ABOVE L2 DOOR, RT OF G4 GALLEY AND TWO AFT BULL NOSE LIGHTS ON RT SIDE FAILED TO COME ON DURING TEST. GROUNDED - YES. REMOVED AND REPLACED AFT RT EMERGENCY EXIT LIGHT BATTERY (M1672) S/N 47319 AND PERFORMED SATISFACJun 1, 2020 · N564AS · Boeing 737890 · Emergency LightingSDR ASAA2020032332490Warning System · false activationLEFT PACK ILLUMINATED DURING "MASTER CAUTION RECALL" DURING DESCENT CHECK. GROUNDED - YES. REF B737-800 FIM 21-53 TASK 807, #1 PZTC PREV FLT BITE LOGGED "RAM ACT" FAULT. BITE VERIFY TESTED GOOD W/O FAULT. GVI, NO OBSTRUCTIONS IN RAM AIR INLET DUCT. VERIFIED LEMar 18, 2020 · N564AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2020031332409Unknown · malfunctionedA/C APPROACH SURVEY COMPLETED UNSATISFACTORY. IN THE FLARE WITH A 5 KT CROSSWIND THE A/C BANKED LEFT AND WAS 30 FEET LEFT OF CENTERLINE WITHOUT SHOWING ANY SIGN OF RETURNING TO COURSE. GROUNDED - YES. PERFORMED B737-800 FIM 22-11 TASK 899. NO FAULTS, ALL TESTSMar 11, 2020 · N564AS · Boeing 737890 · Autopilot SystemSDR ASAA2020022652274Lens · brokenEMERG SIGN AT FWD LH OVERWING EXIT HAS BULB OUT & SIGN IS BROKEN. GROUNDED - YES. RELAMPED & INSTALLED NEW LENS (EXIT COVER SIGN) REF AMM 33-51-01-960-801. OPS CHECK GOOD.Feb 25, 2020 · N564AS · Boeing 737890 · Emergency LightingSDR ASAA202002032052Warning Light · false activationRIGHT SIDE PACK LT ILLUM ON RECALL. GROUNDED - YES. REF FIM TASK 21-53 TASK 821, #2 PZTC BITE PREV FLT LOGGED RAM AIR ACT FAULT, FAULT RESETTABLE. PZTC BITE VERIFY TESTED GOOD W/O FAULTS. VERIFIED RIGHT PACK OPS CHECKED NORMAL ON GND W/O FAULTS.Jan 29, 2020 · N564AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2020012743959Warning Light · false activationCONT CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL AND RESETS. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE PROCEDURE IAW FIM 21-62, TASK 801. RESET PACK TEMP CONTROLLER AND RAN PACKS, CONT CABIN ZONE TEMP LIGHT REMAINS EXTINGUISHED ON RECALL.Jan 24, 2020 · N564AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA202001281990Nut Plate · corrodedNR 1 ENG INLET AND FAN BLADES-DETAILED INSP FOUND 17 EACH NUTPLATES HAVE CORROSION UNDER THEM ON O/B FAN FRAME CASE AT AFT ACOUSTICAL PANEL LOCATION. GROUNDED - YES. CONTINUE IN-SERVICE OF 50 CYCLES, NO CRACKS IN ALL NUTPLATES FOUND IAW AMM 72-23-05-700-80Jan 8, 2020 · N564AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2019120431503Actuator · leakingFLUID LEAK FOUND UNDER NR 2 ENGINE. GROUNDED - YES. IAW AMM 71-71-00-200-801-F00 PERFORMED ENG DRAIN AND VENT INSPECTION, FOUND NR 7 ENG LEFT VSV DRAIN LEAKING, LEAK RATE LIMIT WITH SERVICEABLE LIMITS. REMOVED AND REPLACED THE NR 2 ENG VSV ACTUATOR IAW AMM Nov 30, 2019 · N564AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2019112623425Coupler · failedHF1 XMIT WAS NOT RECEIVED BY ATC. RECEIVED TRANSMISSIONS FROM ATC ON HF2. GROUNDED - YES. REMOVED AND REPLACED #1 HF ANTENNA COUPLER IAW B737-800 AMM 23-11-61/401. INSTALLATION TESTED NORMAL. VERIFIED #1 HF TRANSMIT AND RECEIVED NORMAL. REMOVED MEL 23-11A.Nov 22, 2019 · N564AS · Boeing 737890 · Communications System WiringSDR ASAA2019100320887Panel · failedNR 1 HF RADIO UNABLE TO TRANSMIT. ATTEMPTED SEVERAL TIMES ON FREQ 5547 AND 6673. RECEIVE FUNCTION WORKS NORMALLY. GROUNDED - YES. ACCOMPLISHED HF COMMUNICATION SYSTEM BITE IAW FIM 23-11 TASK 801. OPS CHECKED GOOD WITH NO FAULTS. ACCOMPLISHED FIM 23-11 TASK 806Oct 2, 2019 · N564AS · Boeing 737890 · HF Communications SystemSDR ASAA2019091830723Spinner · worn#1 ENG FRONT SPINNER CONE BLACK COATING WORN. GROUNDED - YES. REPLACED #1 ENG FRONT SPINNER CONE PER AMM 72-21-01 STEP F (5).Sep 18, 2019 · N564AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2019081930430Spacer · debondedDURING ACCOMPLISHMENT FO TC 78472010, FOUND NR 2 ENG FAN BLADE SPACERS #3 AND #21 DISBONDED BOTH SIDES TO ELASTOMERS. GROUNDED - YES. REPLACED SPACERS 3 AND 21 ON T/C 78472010.Aug 19, 2019 · N564AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2019081130376Display · malfunctionedF/O FD FLAG PRESENT ON PFD. GROUNDED - YES. PERFORMED DFCS BITE PROC PER B737-800 FIM TASK 22-11 TASK 801. CHECKED FAULT HISTORY AND FOUND NO FAULTS. PERFORMED CURRENT STATUS QUICK TEST FOR FLIGHT DIRECTOR (GROUP 12), VERIFIED ALL C/B'S FOR FCCB SET, TEST PASSAug 11, 2019 · N564AS · Boeing 737890 · Central DisplaySDR ASAA2019071630110Fire Detector · failedDURING OVHT/FIRE TEST, ENGINE #2 DOES NOT TEST PROPERLY WITH DETECTOR SWITCH IN BOTH. GROUNDED - YES. REPLACED ENG 2 M1757 AND M1758 ENG FAN FIRE DETECTORS ASSY. REF AMM 26-11-01-400-802, OPS NML REF AMM 26-10-00-710-801. ACCOMPLISHED VISUAL INSP ON THE # 2 ENJul 16, 2019 · N564AS · Boeing 737890 · Fire Detection
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