N513AS

Service difficulty reports · 437

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 = 'N513AS' 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 ASAA2019072230157Warning System · false activationLEFT PACK LT ILLUMINATES ON RECALL. GROUNDED - YES. BITE AND VERIFY NO FAULTS.Jul 22, 2019 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2019071430054Wire Harness · damagedPER T/C N8420001 - RIGHT ENGINE HARNESS INSPECTION FOUND ENG J9 + J10 HARNESS DAMAGE AT T3 SENSOR CONN'S. GROUNDED - YES. REMOVED AND REPLACED J9 HARNESS ON #2 ENGINE REF AMM 73-21-06. FOR J10 HARNESS REPLACEMENT REF L/P 11973793. EEC DISCRETES TEST GOOD REF AJul 14, 2019 · N513AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2019071430053Wire Harness · tornPER T/C N8420001 RIGHT ENGINE HARNESS INSPECTION FOUND BLACK BRAID TORN AT CJ10 DISCONNECT. DAMAGED BRAID IS ON THE J10 HARNESS. GROUNDED - YES. REMOVED AND REPLACED J10 HARNESS IAW AMM 73-21-06. FOR ALL HARNESS TESTS REF L/P 11973794, ALL TESTS PASSED.Jul 14, 2019 · N513AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA201905319492Engine · crackedWHILE ACCOMPLISHING T/C 78472022 AT STAGE 1 LPT INSPECTION FOUND 1 FULL CRACK, 1 HOLE .0267 INCH SQUARE, 4 MULTI CRACKS (ON 1 AIRFOIL) AND 4 RADIAL CRACKS (ON 1 AIRFOIL) PER AMM 72-00-00-200-811-F00 FIG. 634. CONTINUE IN SERVICE LIMIT OF 25 CYCLES FOR #2 EMG. May 27, 2019 · N513AS · Boeing 737890 · Turbine SectionSDR ASAA2019052729487Wire Harness · intermittentAPU HAS HISTORY OF FAULT CODE 49-31171 WITH NO STARTS ON LANDING. GROUNDED - YES. ACCOMPLISHED FIM 49-31 TASK 808 STEP F.(4) CONTINUITY FROM CONNECTOR D3599B PIN A9 TO P23 PIN 1 IS GOOD REF WDM 49-62-12 P23 PIN 2 TO GROUND IS GOOD. P23 PIN 3 GROUND IS INTERMITMay 27, 2019 · N513AS · Boeing 737890 · APU System WiringSDR ASAA2019052529488Filter Element · cloggedWHILE PERFORMING INSPECTION ON THE APU FOUND OIL FILTER INDICATOR FOR THE LUBE FILTER HOUSING EXTENDED OUT. GROUNDED - YES. REMOVED AND REPLACED LUBE FILTER ELEMENT PER AMM 49-91-12 AND REMOVED AND REPLACED OIL FILTER INDICATOR PER AMM 49-91-13 OPS CHECK GOOD.May 25, 2019 · N513AS · Boeing 737890 · APU Oil SystemSDR ASAA2019052029426Warning System · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. BITE CK FOUND FLT. DECK TEMP SENSOR FAULT ON PREV FLT. BITE CK OF BOTH ACC CONTROLS TEST NML. NO PRESENT FAULT. OPS CK NML. OK FOR SVC..May 20, 2019 · N513AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2019051829386Seal · leaking#1 ENGINE OIL CONSUMPTION TREND DATA SHOWS CONSUMPTION RATES TO BE GREATER THAN EXPECTED. GROUNDED - YES. UPON INSPECTION AFTER ENGINE RUN LEAK CHECK FOUND OIL LEAKING ON #1 ENGINE FROM IDG/AGB DRAIN. FOUND TO BE OUT OF LIMITS (MORE THAN ONE DROP IN 3 MINUTES)May 18, 2019 · N513AS · Boeing 737890 · Turbine Engine Accessory DriveSDR ASAA2019051829376Idg · leakingDURING IDLE LEAK CHECK OF #1 ENGINE. FOUND OIL LEAKING FROM IDG VALVE CAP PLATE. GROUNDED - YES. REMOVED #1 ENGINE IDG IAW AMM 24-11-11-000-801. INSTALLED A SERVICEABLE IDG IAW AMM 24-11-11-400-801 PARA 3A THRU 3H. ACCOMPLISHED AMM 24-11-11-400-801 PARA 3.I. TMay 18, 2019 · N513AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2019051729384Warning System · false activationPER INBOUND FLT CREW APU FAULT LT ILLUMINATED ON APU RESTART. GROUNDED - YES. PERFORMED APU BITE TEST REF FIM 49-60 TASK 801. FOUND MX MESSAGE 49-31171. PERFORMED FIM 49-31 TASK 808 WAITED 30 MIN AND RESTARTED APU START WAS NORMAL. NO MESSAGE ON CURRENT STATUSMay 17, 2019 · N513AS · Boeing 737890 · APU Indicating SystemSDR ASAA2019051229317Warning System · false activationDURING TAXI IN TRIED STARTING APU RECEIVED APU FAULT LIGHT. GROUNDED - YES. APU WAS CONTINUOUS RUN IN FLIGHT. CREW TURNED OFF PRIOR TO TOP OF DESCENT. APU START ATTEMPTS WAS AFTER LANDING. NO SECOND ATTEMPT MADE. APU BITE ACCOMPLISHED. CODE 49-31171 DISPLAYED.May 12, 2019 · N513AS · Boeing 737890 · APU Indicating SystemSDR ASAA2019051129289Control Panel · defectiveDIGITS ARE DIFFICULT TO READ ON CAPTAINS COURSE DISPLAY ON THE MODE CONTROL PANEL. GROUNDED - YES. REMOVED AND REPLACED MCP PER AMM 22-11-34. PERFORMED INSTALLATION TEST OF MCP PER AMM 22-11-34-740-801. PERFORMED LRU REPLACEMENT TEST FOR MCP BITE TEST GROUP #3May 11, 2019 · N513AS · Boeing 737890 · Autopilot SystemSDR ASAA2019042629173Wire Harness · damagedWHILE INSTALLING RH VSV, (ENG #2) FOUND DAMAGED WIRES. GROUNDED - YES. REPLACED J9 AND J10 HARNESS. ALL OPS NML. ALL TEST PASS, REF B737-800 AMM 73-21-06, 71-00-00. GROUND VERIFICATION SAT.Apr 26, 2019 · N513AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA201904295171Switch · inoperativeWHEN INTERROGATING THE FMC CDU FOR ENGINE FAULTS FOUND ENGINE NBR 2 MSG NBR 73-31072 THE FUEL FILTER SIGNALS DISAGREE. GROUNDED - YES. REMOVED AND REPLACED FUEL FILTER DIFF PRESSURE SWITCH REF B737-800 AMM 73-34-01. OPS CHECKS AND LEAK CHECK GOOD.Apr 25, 2019 · N513AS · Boeing 737890 · Fuel Selector/Shut-Off ValveSDR ASAA2019042639142Filter · abnormal#2 FUEL FILTER BYPASS LIGHT ILLUMINATED AFTER ENGINE START. GROUNDED - YES. REMOVED AND REPLACED #2 ENG FUEL FILTER, DRAIN PLUG O-RING, AND RE-SAFETIED DRAIN PLUG IAW B737-800 AMM 73-11-02. ACCOMPLISHED GROUND VERIFICATION, PERFORMED IDLE ENG RUN OF #2 ENG, NOApr 23, 2019 · N513AS · Boeing 737890 · Engine Fuel DistributionSDR ASAA2019042639139Control Valve · stuckRT PACK LIGHT ON UPON MASTER CAUTION RECALL LIGHT EXTINGUISHES UPON MASTER CAUTION RESET. GROUNDED - YES. REF L/P 11972111, TCV 2 (V141) FAILED BITE TEST. REMOVED & REPLACED TCV 2 REF B737-800 AMM 21-51-10. ACCOMPLISHED PACK-ZONE TEMP CONTROLLER BITE TEST REF Apr 23, 2019 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2019042639136Control Valve · stuckWITH MASTER CAUTION RECALL: # 2 PACK LIGHT REMAIN ON AFTER MASTER CAUTION RESET BUTTON PUSHED. GROUNDED - YES. CONFIRMED FAULT, BOTH #1 & #2 PACK-ZONE TEMP CONTROLLER BITE TEST FAILS TCV 2 (V141), WILL NOT RESET FAULT. FOUND TCV 2 FROZEN. REMOVED & REPLACED TCApr 23, 2019 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2019042029085Actuator · leakingWHILE PERFORMING IDLE RUN CHECK ON ENG #2, FOUND LEFT VSV LEAKING. GROUNDED - YES. REMOVED AND REPLACED VSV ACTUATOR IAW B737-800 AMM TASK 75-31-01. LEAK AND OPS CHECKS GOOD. THIS CLEARS PLT.Apr 20, 2019 · N513AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2019042392986Actuator · leakingWHILE PERFORMING IDLE RUN CHECK ON ENG # 2 FOUND RIGHT VSV LEAKING. GROUNDED - YES. REMOVED AND REPLACED #2 ENG RIGHT VSV ACT IAW AMM 75-31-01. LEAK AND OPS CHECKS GOOD. THIS CLEARS PLT.Apr 19, 2019 · N513AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2019041879025A/C Pack · faultedR/H PACK LT W/ MC RECALL, GOES OUT W/ RESET. GROUNDED - YES. BITE CHECKED #2 ZTC - FAULTED TCV. PERF B737-800 FIM 21-62 TASK 831. VERIFY TEST PASSED. FAULT RESETS. RAN L/H & R/H PACKS W/ NO DEFECTS NOTED. ETOPS GND VERIFICATION TEST SUCCESSFUL.Apr 17, 2019 · N513AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA201904158975Fmc · warning lightFMC DISAGREE LIGHT CAME ON DURING TAXI OUT. GROUNDED - YES. ACCOMPLISHED RESET PROCEDURE PER QRH. FMCS RESTORED NORMAL.Apr 12, 2019 · N513AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2019041088948Lens · brokenFA REPORTS EXIT SIGN BROKEN OFF BY R2 DOOR. GROUNDED - YES. INSTALLED NEW EXIT SIGN COVER.Apr 8, 2019 · N513AS · Boeing 737890 · Emergency LightingSDR ASAA201904028852Anti-Ice Valve · failedR/H ENG ANTI-ICE WILL NOT TURN OFF, LIGHT IS BRIGHT BLUE WITH SWITCH IN OFF POSITION. GROUNDED - YES. REMOVED AND REPLACED #2 ENG TAI VALVE, LEAK CHECK AND ENGINE RUN OPS CHECK GOOD REF B737-800 AMM 30-21-11-400-801.Mar 31, 2019 · N513AS · Boeing 737890 · Engine Anti-Icing SystemSDR ASAA2019032428774Warning System · false activationHF 1 SHOW FAIL IN BOTH THE ACTIVE & STANDBY WINDOWS, HOWEVER WE WERE ABLE TO TRANSMIT & RECEIVE. GROUNDED - YES. REF FIM 23-11 TASK 801. PERFORMED NR 1 HF BITE TEST NO FAULTS FOUND. TEST PASSED. AS PRECAUTIONARY R&R NR 1 HF TRANSCEIVER. REF AMM 23-11-21-000-80Mar 24, 2019 · N513AS · Boeing 737890 · HF Communications SystemSDR ASAA2019030528479Unknown · malfunctionedHF NR 1 FAIL, CYCLED POWER OP CHECK NORMAL. GROUNDED - YES. UNABLE TO DUPLICATE HF NR 1 ISSUES. OPS CHECK GOOD.Mar 5, 2019 · N513AS · Boeing 737890 · HF Communications SystemSDR ASAA2019030328432Sign · unsecureMID CABIN OVERWING EMERGENCY EXIT SIGN FELL OFF CEILING. GROUNDED - YES. REPLACED MISSING HARDWARE AND MOUNTED EMERGENCY EXIT SIGN.Mar 3, 2019 · N513AS · Boeing 737890 · Emergency LightingSDR ASAA2019022728395Unknown · abnormalAUTO THROTTLE WILL NOT ARM. GROUNDED - YES. ACCOMPLISHED AUTOTHROTTLE SYSTEM TEST AMM TASK 22-31-00-710-802. ALL TESTS PASS. ACCOMPLISHED LRU REPLACEMENT TEST FOR FCC A & FCC B. ALL TESTS PASS. REF AMM 22-11-00-740-815. ACCOMPLISHED LAND VERIFY TEST. ALL TESTSFeb 27, 2019 · N513AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2019021928263Warning System · false activationNR 2 ENG BLUE COWL VALVE OPEN LITE AND NR 2 ENG AMBER TAI LITE REMAIN ILLUMINATED WITH ENG A/I SWITCH IN OFF POSITION. DURING DESCENT BOTH LIGHTS EXTINGUISHED AND OPS NORMAL TO SHUTDOWN. GROUNDED - YES. VERIFIED NR 2 ENG COWL ANTI-ICE & COWL VALVE OPEN LIGHTS Feb 19, 2019 · N513AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2019021728206Sign · unsecureTHE EXIT SIGN NEAR R-2 DOOR NEEDS TO BE REPLACED. IT WILL NOT STAY ATTACHED TO THE WALL. GROUNDED - YES. REMOVED AND REPLACED EMER LIGHT BASE ASSY ON R-2 DOOR (LOWER LIGHT ASSY) IAW AMM 33-51-01. OPS CHECK GOOD. OK FOR SERVICE.Feb 17, 2019 · N513AS · Boeing 737890 · Emergency LightingSDR ASAA2019012127894Unknown · malfunctionedHF NR 1 PANEL 'FAIL' SHOWN ON BOTH FREQUENCY INDICATORS. SYSTEMS HANDBOOK NOTES POSSIBLE TRANSCEIVER FAILURE. NOTE BOTH HF RADIOS VOICE AND SELCAL CHECK GOOD. NA ACTUAL PROBLEMS NOTED DURING USE. GROUNDED - YES. RESET POWER TO HF SYSTEM. PERFORMED BITE PROCEDUJan 21, 2019 · N513AS · Boeing 737890 · HF Communications SystemSDR ASAA2019011227800Not Reported · malfunctionedWHILE PERFORMING TASK CARD, FOUND FAULT MSG NR: 73-31072 THE FUEL FILTER SIGNALS DISAGREE NR 2 ENG LONGTIME. GROUNDED - YES. FAULT DEFERRED PER T/C 78273000 FOR 450 FLT HRS. WHILE PERFORMING CDU FAULT CHECK. NO FAULTS NOTED ON NR 2 ENG. THIS CLEARS "PLT".Jan 12, 2019 · N513AS · Boeing 737890 · Engine Fuel Indicating SystemSDR ASAA2018111327094Fitting · crackedFWD CARGO AFT BAFFLE CLIP STA 500H RT IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE CLIP IAW SRM 51 40 05 0G 0.Nov 13, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018110827097Baffle · crackedFWD PIT BAFFLE RT SIDE STA 500D - 500E IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO BAFFLE RT STA 500D - 500E IAW SRM 51 40 05 0G 0 AND SRM 51 40 02 0G 0.Nov 8, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018110727096Fitting · crackedFWD CARGO COMP BAFFLE CLIP AT STA 500H IS CRACKED RT SIDE. GROUNDED - YES. REMOVED/REPLACED FWD BAFFLE CARGO CLIP AT STA 500H RT SIDE IAW SRM 51 40 50 0G 0 AND SRM 51 40 02 0G 0.Nov 7, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018110727093Fitting · crackedFWD CARGO COMP BAFFLE CLIP AT STA 500H IS CRACKED, LT SIDE. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO BAFFLE CLIP AT STA 500H LT SIDE IAW SRM 51 40 05 0G 0 AND SRM 51 40 02 0G 0.Nov 7, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018113067149Skin · crackedLEFT HORIZ LOWER SKIN IS CRACKED AT RIB STA 184.70 APPROX 10" FROM REAR SPAR. GROUNDED - YES. REPAIRED L/H HORIZ STAB SKIN IAW 737 800 SRM 55 10 01 2R 11 REPAIR IS A CATEGORY B WITH AN INSP. THRESHOLD OF 56,000 CYCLES AND REINSPECT EVERY 9,000 CYCLES.Nov 6, 2018 · N513AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2018110627095Floorbeam · corrodedFLOORBEAM AT STA 986 HAS CORR ON SCREW HOLE AT RBL 64. GROUNDED - YES. REPAIRED FLOORBEAM AT STA 986, RBL 24, IAW SRM 53 70 57 2R 6, STEP 4 W 1 O .150 R .120 L 1" D .030.Nov 6, 2018 · N513AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2018113057148Skin · crackedRIGHT HORIZ STAB LOWER SKIN IS CRACKED AT STA 167.10 APPROX 8" FWD OF AFT SPAR. GROUNDED - YES. REPAIRED R/H HORIZ. STAB SKIN IAW 737 800 SRM 55 10 01 2R 11 REPAIR IS A CATEGORY B WITH INSP. THRESHOLD OF 56,000 CYCLES AND REINSPECT EVERY 9,000 CYCLES.Nov 5, 2018 · N513AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2018110527092Support Angle · corrodedAFT CARGO COMP RT FLOOR SUPPORT ANGLE FROM STA 767 TO 787 HAS CORR. GROUNDED - YES. REMOVED CORR FROM AFT CARGO COMPT. RT FLOOR SUPPORT ANGLE FROM STA 767 TO 787, FOUND TO BE OUT OF LIMITS IAW SRM 53 60 15 1A 1 FIG 103 DETAIL D, REMOVED AND REPLACED AFT CARGO Nov 5, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018110527047Channel · corrodedAFT CARGO COMP LT Z CHANNEL FROM STA 727A TO 787 HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. REMOVED AND REPLACED LT Z CHANNEL FROM STA 727 TO 847 IAW SRM 53 00 53 2R 6 W .5 O .040 R 0 L 1.1 D .040.Nov 5, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018110527039Channel · corrodedAFT CARGO COMP RT Z CHANNEL FROM STA 727A TO 767 HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. REMOVED AND REPLACED RT Z CHANNEL FROM STA 727 TO 767 IAW SRM 53 00 53 2R 6 W 0.5 O .040 R .020 L 1.2 D .020.Nov 5, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018110527038Channel · corrodedAFT CARGO COMP FLOOR SUPPORT CHANNEL ON FRAME 767 HAS CORROSION. GROUNDED - YES. REMOVED CORR AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53 60 15 A 1. REMOVED AND REPLACED CHANNEL (WEB) IAW SRM 51 40 02 0G 0 W 0.5 O .050 R .040 L 1 D .010.Nov 5, 2018 · N513AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018091426088Unknown · malfunctionedA/T DISENGAGED INFLIGHT WOULD NOT REENGAGE. GROUNDED - YES. CHECKED THE A/T FAULT HISTORY AND FOUND FAULT 22-31687 (ASM1) RECORDED ON TWO LEGS ON 9/10/18. PERFORMED FIM 22-31 TASK 805 WITH NO ACTIVE FAULTS NOTED. PERFORMED AN A/T OP-TEST PER AMM 22-31-00-710-8Sep 10, 2018 · N513AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2018080225645Anti-Ice Valve · stuckNR 2 ENGINE ANTI-ICE COWL VALVE WAS STUCK IN THE OPEN POSITION. ACFT GROUNDED. INSPECTED THE NR 2 ENG ANTI-ICE VALVE. ACCOMPLISHED INITAL OPS CHECKS IAW AMM 30-21-00. BOTH APU AND ENG SOURCE NORMAL. INDICATION VALVE OPS CHECKED OKAY.Aug 2, 2018 · N513AS · Boeing 737890 · Engine Anti-Icing SystemSDR ASAA2018080025625Fault Message · false indicationAFTER LANDING CAPTAIN'S INBOARD DU WAS GETTING INTERMITTEN VTK FLAG. GROUNDED - YES. PERFORMED FIM 34-61 TASK 801. NO FAULTS NOTED FIM TASK 34-61 TASK 836 LIST VTK FLAG AS NUISANCE FAULT AND A/C REBOOTED AND CLEARED W/ NO FAULTS NOTED.Jul 31, 2018 · N513AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2018072125525Engine · dirtyON TAKEOFF FROM LAS AT GEAR RETRACTION NOTICED NR 1 ENG EGT GAUGE RED INDICATING 917 DEG C. REDUCED POWER ON ENGINE TO APPROX 97% N1 AND EGT RETURNED TO NORMAL. 27K BUMP TO, 32 DEG C AT KLAS. GROUNDED - YES. ACCOMPLISHED NR 1 ENGINE GAS PATH WASH WITH WATER REJul 21, 2018 · N513AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2018062195141Autopilot Sys · malfunctionedAUTOPILOT A DISCONNECTED DURING CRUISE, WITH ALL OTHER INDICATIONS NORMAL. AUTOPILOT A WAS ENGAGED BUT DISCONNECTED EARLY DURING DESCENT, AUTOPILOT B USED FOR REMAINDER OF FLIGHT. ACFT GROUNDED. FLIGHT FAULT REVIEW LOGGED MCP DATA INV, MESSAGE 22-11607, AJun 19, 2018 · N513AS · Boeing 737890 · Autopilot SystemSDR ASAA2018061225065Paint · missingWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENG T/C 78472002, FOUND FRONT SPINNER WITH MISSING PAINT. GROUNDED - YES. ON DEFERRAL.Jun 12, 2018 · N513AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018061225044Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE T/C 78472002, ON NR 1 ENGINE FOUND ALL SHIMS WORN INTO PARENT MATERIAL. GROUNDED - YES. REMOVED AND REPLACED ALL FAN BLADE SHIMS ON NR 1 ENGINE, REF AMM 72-21-02/401.Jun 12, 2018 · N513AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018061225043Blade · wornWHILE ACCOMPLISHING FAN BLADE LUBE, T/C 78472002 ON NR 1 ENG FOUND 4 EA BLADES 6, 7,13,14 WITH CU-NI-IN COATING WORN BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED FAN BLADES 1 2 6 7 13 14, AND 18 REF AMM 72-12-02-401 AND T/C 78472002.Jun 12, 2018 · N513AS · Boeing 737890 · Turbine Engine Compressor Section
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