N514AS

Service difficulty reports · 370

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 = 'N514AS' 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 ASAA2021011533886Controller · inoperativeLT SIDE WINDOW HEAT INOPERABLE. GROUNDED-YES. REF B737-800 FIM 30-41 TASK 801, REMOVED AND REPLACED WHCU M322, IAW B737-800 AMM 30-41-11/401. WHCU BITE TESTED GOOD AND LEFT SIDE WINDOW HEAT OPERATIONS CHECKED GOOD.Jan 15, 2021 · N514AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2020121633706Fmc · intermittentON TAXI IN FMC NR 1 FAIL (VTK CA SIDE, FMC MESSAGE LIGHT, FMC ON MEANS SCRATCH PAD GONE). GROUNDED-YES. PERFORMED B737-800 FIM 34-61 TASK 836 AND FAULT FOUND TO BE INTERMITTENT, NO FURTHER DEFECTS NOTED. OPERATIONS CHECK GOOD.Dec 16, 2020 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2020121233669Modulating Valve · faultedCONT CAB ZONE TEMP LIGHT ILLUMINATED UPON MASTER CAUTION RECALL. GROUNDED-YES. PERFORMED PACK/ZONE TEMPERATURE CONTROL BITE TEST, REF B737-800 AMM 21-61-00-70-806-002. VERIFIED FLIGHT DECK TRIM VALVE FAULT, PER B737-800 FIM 21-62 TASK 834. REPLACED FWD CABDec 12, 2020 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2020120633644Annunciator · faultedF/O SIDE AMBER FMC ANNUNCIATION ILLUMINATED FOR UNDETERMINED REASON. GROUNDED-YES. ANNUNCIATOR AND FMC PREVIOUSLY REPLACED. UNABLE TO INDUCE FAULT THAT WOULD NOT CLEAR PREVIOUSLY. REMOVED & REPLACED F/O'S AUTO FLIGHT STATUS ANNUNCIATOR. OPERATIONS CHECK NDec 6, 2020 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2020120533649Warning Light · false activationZONE TEMP LIGHT ON AFTER ENGINE START ON RECALL-LIGHT RESETS. GROUNDED-YES. PERFORMED BITE CHECK, PER B737-800 AMM 21-61-00. FOUND FLIGHT DECK TCV FAULT, AND RESET. PERFORMED BITE ALL PASS GO. A/C GOOD FOR SERVICE.Dec 5, 2020 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2020112033577Fmc · malfunctionedF/O FMC P/RST ANNUNCIATOR LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED DFCS, A/T FAULT HISTORY, NO FAULTS NOTED. THERE WERE NUMEROUS FMC DATA INV (CHB) MESSAGE NR 22-11822. FOUND WHEN F/O AUTOFLIGHT STATUS ANNUNCIATOR TEST SWITCH SELECTED TO POSITION 2 Nov 20, 2020 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2020110833521Fmc · abnormalIN DESCENT, VNAV DISENGAGED AND AUTOTHROTTLES CLICKED OFF AT 15,000'. FMA REVERTED INTO CWP. ABLE TO ENGAGE LEVEL CHANGE BUT NO VNAV. AUTOTHROTTLES SWITCH RE-ENGAGED BUT WAS NOT RESPONSIVE TO THRUST REQUIREMENTS. REFERENCE PREVIOUS SIMILAR WRITE UP PAGE 60Nov 8, 2020 · N514AS · Boeing 737890 · Autopilot SystemSDR ASAA2020110633509Computer · faultedCLIMBING FROM FL400 TO FL410 VNAV DISCONNECTED AND FMA DISPLAYS ARM, LNAV. ALT HOLD. A/T REMAINS ENGAGED (ARM LT ON), BUT AUTO THROTTLES ARE NON RESPONSIVE TO CLIMB AND/OR SPEED CHANGES. VNAV WILL NOT RE-ENGAGE. CRUISE ALTITUDE IN FMC SET FL410, BUT HAD TONov 6, 2020 · N514AS · Boeing 737890 · Autopilot SystemSDR ASAA2020102933449Computer · malfunctionedJUST AFTER LEVEL OFF AT FL410, VNAV DISENGAGED AND A/T THRUST MODE SHOWED IN CLB MOVE. VNAV WOULD NOT REENGAGE AT ANY POINT IN FLIGHT. FMC SEEMED TO BE STUCK IN CLB MODE. GROUNDED-YES. INITIALLY COULD NOT GET INTO DFCS BITE AND THROTTLE TEST WAS FAILING. Oct 29, 2020 · N514AS · Boeing 737890 · Autopilot SystemSDR ASAA2020101733363Transceiver · failedIN CRUISE HF2 SHOWING FAIL IN ACTIVE AND STANDBY WINDOWS OF RADIO TUNING PANEL. GROUNDED-YES. REMOVED AND REPLACED NR 2 HF TRANSCEIVER, IAW W/B737-800 AMM 23-11-21. SYSTEM OPERATIONS CHECK OK.Oct 17, 2020 · N514AS · Boeing 737890 · HF Communications SystemSDR ASAA2020101233339Control Panel · defectiveCAPTAIN'S MCP COURSE DIGITAL DISPLAY HARD TO READ (SECOND DIGIT "ZERO" DISPLAYED AS EIGHT). GROUNDED-YES. REPLACED THE MCP, ALL TESTS PASSED, REF B737-800 AMM 22-11-34-400-801.Oct 12, 2020 · N514AS · Boeing 737890 · Autopilot SystemSDR ASAA2020091833209Actuator · faultedDURING ACCOMPLISHMENT OF T/C 78273000 NR 1 ENGINE HAS SHORT TIME FAULT MESSAGE 75-30401 THE VSV POSITION SIGNALS DISAGREE. GROUNDED-YES. REMOVED AND REPLACED NR 1 ENGINE LT VSV ACTUATOR, REF B737-800 AMM 75-31-01-400-801-F00/AMM 72-23-03-400-802-F00. LEAK &Sep 18, 2020 · N514AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2020090933159Bleed Valve · out of limitsENGINE NR 2 STAGE 5TH CHECK VALVE FAILED AD20201651-NG-36-2. INSPECTION STEP 3H(1)(II)- VALVE BUSHING CLEARANCE. GROUNDED - YES. REMOVED AND REPLACED 5TH STAGE CHECK VALVE, REF B737-800 AMM 36-11-02.Sep 9, 2020 · N514AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2020090213128Battery Pack · inoperativeEMERGENCY LIGHTS AT L1 DOOR AND L ROWS 17-24 INOPERABLE. GROUNDED - YES. REPLACED BATTERY PACKS M1675 AND M1671, PER TASK 33-51-06-960-805. OPS GOOD.Sep 1, 2020 · N514AS · Boeing 737890 · Emergency LightingSDR ASAA2020052632504Bleed Valve · leakingLEAK CK, FOUND NR 1 ENGINE LEAKING FUEL FROM DRAIN. GROUNDED - YES. REMOVED AND REPLACED TRANSIENT BLEED VALVE IAW AMM 75-23-01/401. PERFORMED ACTUATOR TEST IAW AMM 71-00-00-700-807-F00. TEST PASSED, NO ACTUATOR TEST FAULTS. PERFORMED IDLE POWER LEAK CHECKMar 22, 2020 · N514AS · Boeing 737890 · Compressor Bleed ValveSDR ASAA2020052632503Actuator · leakingLEAK CHECK, FOUND NR 1 ENGINE LEAKING FUEL FROM DRAIN. GROUNDED - YES. REMOVED AND REPLACED RT VSV ACTUATOR IAW AMM 75-31-01-000-802-F00/75-31-01-400-802-F00. ACCOMPLISHED VSV ACTUATOR LEAK TEST IAW AMM 75-31-01-790-801-F00 AND OPERATIONAL CHECK REF AMM 71-Mar 22, 2020 · N514AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2020032632504Fuel · leakingREF LP 12103257 LEAK CK, FOUND #1 ENGINE LEAKING FUEL FROM DRAIN. GROUNDED - YES. ON DEFERRAL.Mar 22, 2020 · N514AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2020032632503Fuel · leakingREF LP 12103257 LEAK CHECK, FOUND #1 ENGINE LEAKING FUEL FROM DRAIN. GROUNDED - YES. ON DEFERRAL.Mar 22, 2020 · N514AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2020022932333Regulator · inoperativeCLIMBING THROUGH 8000 DUCT PRESSURE INDICATED R-4 AND LEFT 44. AT CRUSE 31000 DUCT INDICATED R 9 AND LEFT 34 NO OTHER ABNORMALITIES NOTED CABIN PRESSURE DIFFERENTIAL 7.8 PSI. GROUNDED - YES. DIVERSION TIME 83 MINUTES - ACCOMPLISHED TASK CARD NG-36-WC-0001 BLEEFeb 29, 2020 · N514AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2020021203149Fmc · malfunctionedFMC DISAGREE ILLUMINATED AT THE GATE. GROUNDED - YES. ACCOMPLISHED QRC OPS NORMAL.Feb 10, 2020 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA202002032061Battery Pack · no testEMERGENCY LIGHTS AT L2 DOOR FAILED BATTERY CAPACITANCE CHECK PER TASK CARD# 78233001. PACK FAILED AFTER DEEP CYCLE. GROUNDED - YES. REMOVED AND REPLACED L2 DOOR BATTERY PACK PER B737-800 AMM TASK 33-51-06-960-805, LIGHTS TEST GOOD.Feb 2, 2020 · N514AS · Boeing 737890 · Emergency LightingSDR ASAA2020010731799Nozzle · crackedREF S/O 1010104 N/R-00001, DURING RE-INSPECT OF #2 ENGINE ESN 896776 LPT NOZZLES FOUND PROGRESSION IN CRACKS, 5 EACH FULL CRACKS RADIAL CRACKS ON 2 INTERSECTING, CRACK ON 3, AND 1 AIRFOIL WITH 2 HOLES. REQUIRES REPLACEMENT OF ENGINE REF B737-800 AMM 72-00-00-2Jan 6, 2020 · N514AS · Boeing 737890 · Turbine SectionSDR ASAA201912031489Fire Detector · inoperative#2 ENGINE FIRE DETECTOR B LOOP DOES NOT TEST. GROUNDED - YES. FIRE DETECTION CONTROL MODULE FAULTS #2 ENGINE LEFT CORE LOOP. #2 ENGINE LEFT CORE LOOP REMOVED AND REPLACED REF B737-800 AMM 26-11-00. OPERATIONAL CHECK GOOD AND NO FAULTS ON CONTROL MODULE. GROUNDDec 2, 2019 · N514AS · Boeing 737890 · Fire DetectionSDR ASAA2019110931301Wire Harness · failed#2 ENGINE TREND DATA SHOWS EGT INDICATION TO HAVE GREATER THAN EXPECTED SCATTER. INDICATION ERRORS ARE SUSPECT. GROUNDED - YES. ACCOMPLISHED ALTERNATED DEACTIVATION PER CHAPTER 5 TABLE 3, ITEMS 8 & 9. REMOVED AND REPLACED CJ10 WIRING HARNESS PER B737-800 AMM TNov 9, 2019 · N514AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2019102161034Indicator · failedFUELER REPORTS THAT THE GAGE FOR TANK #1 AT THE FUEL PANEL IS INOP. FUEL QUANTITY FOR TANK #1 IN COCKPIT WORKS. GROUNDED - YES. REMOVED AND REPLACED REFUEL QUANTITY INDICATOR #1 IAW B737-800 AMM 28-41-61/401 OPC GOOD.Oct 16, 2019 · N514AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2019101431015Anti-Ice Valve · intermittentENGINE #2 AMBER TAI LIGHT ILLUMINATES INTERMITTENTLY DURING CRUISE WITH THE #2 ENGINE ANTI ICE SWITCH OFF. GROUNDED - YES. REMOVED AND REPLACED #2 ENG TAI VALVE PER B737-800 AMM 30-21-11. OPS AND LEAK CHECKS GOOD.Oct 14, 2019 · N514AS · Boeing 737890 · Engine Anti-Icing SystemSDR ASAA2019100753937Fmc · malfunctionedR FMC FAIL ON ARRIVAL TO PHX. GROUNDED - YES. ACCOMPLISHED FMC BITE, NO FAULTS, & FMC OPS TEST REF B737-800 AMM 34-61-00-710-801. OPS NORMAL.Oct 5, 2019 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2019100230892Acoustic Panel · damagedNR 2 ENG ACOUSTICAL PANEL AT 2-3 OCLOCK A.L.F, THE FWD LWR FASTENER IS PULLED THROUGH THE PANEL. MARKED. GROUNDED - YES. REPLACED THE NR 2 ENG ACOUSTICAL PANEL IAW AMM 72-23-02.Oct 2, 2019 · N514AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2019092030792Sensor · faultyWHILE PERFORMING T/C 78273000 HAD SHORT TIME FAULT ON #2 ENGINE, 73-30902 - T12 SIGNALS DISAGREE. GROUNDED - YES. VERIFIED MAINT MSG/FAULT 73-30902 STILL ACTIVE ON ALL LEGS #2 ENGINE. PERFORMED EEC TEST AND SHOWS FAULT STILL ACTIVE. REMOVED AND REPLACED #2 ENGSep 20, 2019 · N514AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2019092030791Heat Exchanger · leakingDURING PDC INSPECTION FOUND #2 ENGINE DRIPPING FUEL FROM MAIN OIL/FUEL HEAT EXCHANGER PAD DRAIN. GROUNDED - YES. REFERENCING AMM 71-71-00-200-801-F00 - ENGINE VENTS AND DRAINS INSPECTION - THE LEAK RATE IS WITHIN LIMITS FOR DISPATCH (4 DRIPS/MIN, LIMIT IS 90).Sep 20, 2019 · N514AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2019090730633Tube · damagedWHILE WORKING ON T/C N8420001, FOUND HPTACC STAGE 9 INLET TUBE DAMAGED BY J9 BRAIDED SHIELD AT CJ9 DISCONNECT. GROUNDED - YES. REPLACED #2 ENG HPTACC INLET TUBE REF AMM 75-21-01-400-801-F00 STEPS 3G (5)-3G (6).Sep 7, 2019 · N514AS · Boeing 737890 · Engine Cooling SystemSDR ASAA2019090730632Wire Harness · damagedWHILE WORKING ON T/C N8420001, FOUND J9 HARNESS METAL BRANDED SHIELD DAMAGED AT CJ9 DISCONNECT. GROUNDED - YES. DAMAGE IS ON THE #2 ENGINE J10 HARNESS, REPLACED J10 REF AMM 73-21-06-400-802. PERFORMED FADEC SYSTEM TEST IAW AMM 73-21-00-700-802-F00, ALL TESTS PSep 7, 2019 · N514AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2019082830528Idg · malfunctioned#1 GEN DRIVE LIGHT DOES NOT ILLUMINATE WITH APU POWERING THE BUS-INTERMITTENT. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE IDG REF AMM 24-11-11. OPS AND LEAK CHECK GOOD.Aug 28, 2019 · N514AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2019082983529Smoke Detector · intermittentAFT CARGO FIRE DETECTION TEST DOES NOT WORK INTERMITTENTLY. GROUNDED - YES. PERFORMED CEU BITE PER B737-800 FIM 26-16 TASK 801. CEU FAULTED AFT CARGO PIT DETECTOR A3. REMOVED AND REPLACED DETECTOR A3 PER B737-800 AMM 26-16-01. PERFORMED CARGO BAY SMOKE DETECTIAug 28, 2019 · N514AS · Boeing 737890 · Smoke DetectionSDR ASAA2019072330165Blade · wornESN 896776 FAN BLADE CUNI COATING BEYOND LIMITS, BLADE #1, S/N DE187595-D, BLADE #2 S/N DE187397-D BLADE #6 S/N DE184833-G, BLADE #8 S/N DE187677-B, BLADE #10 S/N DE190203-A, BLADE #13 S/N DE187748-T, BLADE #21 S/N DE186783-E, BLADE #22 S/N DE188483-1, AND BLAJul 23, 2019 · N514AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2019071630096Fmc · malfunctionedF/O'S FMC FAILED PRIOR TO DESCENT RAN CHECKLIST COULD NOT RESTORE F/O'S FMC TO NORMAL OPS. CONT FLIGHT WITH SINGLE FMC OPERATION. GROUNDED - YES. FOUND RT FMC BITE INOP. COMPLETED FIM TASK 34-61-00-810-836 FMC DOES NOT OPERATE. RT FMC REBOOTED LT & RT FMC OPS Jul 16, 2019 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2019070829962Warning System · false activationCONT CAB ZONE TEMP LT ON RECALL. EXT WITH MASTER CAUTION RESET. GROUNDED - YES. RIGHT CONTROLLER LOGGED FLT DECK TRIM VALVE FAULT. RESET FAULT. VALVE OPERATION WAS NORMAL & SMOOTH DURING BITE. COULD NOT RE-DUPLICATE FAULT. OP CK NORMAL. REF FIM 21-62 TASK 832.Jul 8, 2019 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2019070329950Relay · defectiveAPU BITE INOP MSG WHEN ATTEMPTING APU BITE TEST. GROUNDED - YES. 1ST ATTEMPT ABLE TO ACCESS APU BITE PAGE AND ABLE TO DUPLICATE FAULT BY DATA LOAD KNOB TO APU THEN APU BITE PAGE AUTO EXIT THEN UNABLE TO ACCESS BACK TO THE APU BITE PAGE AND APU BITE INOP MSG APJul 3, 2019 · N514AS · Boeing 737890 · APU ControlsSDR ASAA2019070229912Unknown · malfunctionedAPU BITE INOP MSG WHEN ATTEMPTING APU BITE TEST. GROUNDED - YES. APU START, RUNS & LOADS NORMALLY REF AMM 49-11-00-710-801 BUT WILL NOT ENTER APU BITE TEST ON FMC CDU. ACCOMP FIM 49-65 TASK 801, APU ECU WAS RMVD & RE-INSTALLED PER THIS FIM TASK. APU NOW BITE TJul 2, 2019 · N514AS · Boeing 737890 · APU ControlsSDR ASAA2019052529491Seal · missingWHILE ACCOMPLISHING TC 78472010 ON ENGINE #1 FOUND TWO PLATFORMS #14 AND #21 MISSING PLATFORM SEAL ON ONE SIDE. GROUNDED - YES. REMOVED AND REPLACED #14 AND #21 PLATFORMS ON #1 ENG PER T/C 78472010. REF T/C FOR WORK ACCOMPLISHED.May 25, 2019 · N514AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2019052529489Spacer · debondedWHILE ACCOMPLISHING TC 78472010 FAN BLADE LUBE, FOUND OVER NINE SPACERS DISBONDED ON ENGINE #1. GROUNDED - YES. REMOVED AND REPLACED ALL 24 SPACERS ON #1 ENG. PER T/C 78472010. REF T/C FOR WORK ACCOMPLISHED.May 25, 2019 · N514AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2019050129221Roller · out of positionFO WINDOW WILL NOT LATCH. GROUNDED - YES. FOUND FWD LOWER ROLLER OUT OF WINDOW, REINSTALLED ROLLER , NO ADJUSTMENT REQUIRED. REF TASK SUB TASK 56-12-11-410-004 9 A,B,C,D ACCOMPLISHED HEAT TEST 30-41-00-710-801.May 1, 2019 · N514AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA2019041829055Filter · clogged#2 ENGINE OIL FILTER POP OUT INDICATOR IS EXTENDED REF T/C N2479001. GROUNDED - YES. OIL FILTER BYPASS WARNING LIGHT WAS NOT ILLUMINATED. RESET AND REPLACED OIL SUPPLY FILTER PER B737-800 AMM 79-21-03. RESET POP OUT INDICATOR PERFORMED IDLE LEAK CHECK. NO LEAKApr 18, 2019 · N514AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA2019040428879Warning Light · false activation"ELEC" LIGHT ILLUMINATED PRIOR TO TAKEOFF. GROUNDED - YES. P5-13 SHOWS AUX BATT CHGR - FAULT RESET - BOTH CHGR'S & BATT'S INDICATE GOOD.Apr 2, 2019 · N514AS · Boeing 737890 · Battery/Charger SystemSDR ASAA201904028824Idg · failed#2 DRIVE LIGHT ILLUMINATED IN FLIGHT. DISCONNECTED PER QRH. GROUNDED - YES. PERFORMED IDG UNSCHEDULED REMOVAL FOR CAUSE, REF AMM 24-11-11. COMPLETED STEPS A.(1)(C)1-3 FOR CONTAMINATED OIL FILTER. ACCOMPLISHED OPERATION TEST IAW AMM 24-11-11. OPS CKS GOOD.Mar 30, 2019 · N514AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2019031728631Warning System · false activationCONT CABIN ZONE TEMP LIGHT ILLUMINATED. EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. PERFORMED BITE CHECK PER AMM 21-61-00. VERIFIED PRIOR FAULT IN FLT DK. FAULT NOT CURRENT IN GROUND VERIFICATION TEST. THIS CLEARS MEL 21-21G.Mar 17, 2019 · N514AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2019031328593Warning System · false activationRECEIVED PACK LIGHT ON CLIMB OUT. GROUNDED - YES. RAN CHECKLIST AND PACK LIGHT CLEARED.Mar 13, 2019 · N514AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2019031228586Unknown · malfunctionedAT CRUISE WITH FO FLT DIRECTOR AS MASTER L NAV DISCONNECTED V NAV WENT TO SPEED MODE. SINGLE FMC OPERATION SCRATCH PAD MESSAGE DISPLAYED. FO PFD HAD MAP FLAG. COMPLETED QRD FOR SINGLE FMC OPS AFTER I MIN OF BOTH ON LEFT RETURNED FMC SELECT SWITCH TO NORMAL, NOMar 12, 2019 · N514AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2019030328436Panel · damagedWHILE ACCOMPLISHING TC 78472000 NR 2 ENGINE FOUND FAN FRAME STRUT PANEL 3 LOOKING FORWARD HAS ELONGATED SCREW HOLE. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE FAN FRAME STRUT PANEL SHOUD SEGMENT FAIRING REF AMM 72-23-03.Mar 3, 2019 · N514AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2019021928234Fan · inoperativeRADAR MOUNT FAN IS INOP. GROUNDED - YES. REPLACED BLOWER PER B737-800 AMM TASK 34-43-51-000-801. OPS GOOD. WXR OPS GOOD PER TASK 34-43-00-710-802-001.Feb 19, 2019 · N514AS · Boeing 737890 · Independent Position Determining System
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