N518AS

Service difficulty reports · 480

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 = 'N518AS' 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 ASAA2017110722515Fire Loop · faultedNR 2 ENGINE A & B LOOP FAULTED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE A FIRE LOOP IAW AMM 26-11-02-400-802, AND 26-11-02-000-802. PERFORMED GOOD OPS TEST PER AMM 26-11-00-710-801.Nov 7, 2017 · N518AS · Boeing 737890 · Fire DetectionSDR ASAA2017110522431Power Supply · failedEMERGENCY LIGHTS LT AFT AREA & GALLEY INOP DURING LIGHT TEST (T/C 78233008). GROUNDED - YES. REMOVED AND REPLACED AFT GALLEY LT EMERGENCY LIGHT POWER SUPPLY REF AMM 33-51-06. LIGHTS OPS CK GOOD.Nov 5, 2017 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2017102922350Terminal · dirtyDURING OVERHEAT, & FIRE TEST, NR 2 ENGINE FIRE WARNING SWITCH AND THE NR 2 OVERHEAT LIGHT DO NOT ILLUMINATE. ACFT GROUNDED. PERFORMED ENGINE FIRE DETECTION SYSTEM OPS TEST IAW AMM 26-11-00-710-801. NO FAULTS FOUND. ACCESSED NR 2 ENGINE FIRE DETECTOR LOOPS. Oct 29, 2017 · N518AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2017102922364Anti-Ice Valve · failedON ARRIVAL, BOTH WING ANTI-ICE LIGHTS WENT OUT AND THE NR 1 TAI LIGHT WENT OUT. ALL THREE LIGHTS WOULD NOT TEST. NOTICED THE NR 1 ENGINE, ENGINE & WING CONTROL CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. TROUBLESHOT THE SYSTEM IAW FIM 30-11, TASK 810. DISCOct 29, 2017 · N518AS · Boeing 737890 · Airfoil Anti/De-ice SystemSDR ASAA2017092422008Wire · brokenFOUND TERMINAL BROKEN AT MW0325 LOOP A ON THE NR 2 ENGINE. ACFT GROUNDED. TERMINATED THE STUD, AND OPS CHECKED GOOD IAW AMM 26-11-00, AND SWPM 20-30-11.Sep 24, 2017 · N518AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2017091521926Idg · failedCREW REPORTED THE NR 2 ENG GENERATOR DRIVE LIGHT ANNUNCIATOR REMAINS EXTINGUISHED WITH ENGINE SHUTDOWN. LAMPS & PRESS TO TEST FUNCTION OKAY. ACFT GROUNDED. REPLACED THE NR 2 IDG IAW AMM 24-11-11-000-801, AND AMM 24-11-11-400-801. IDLE POWER LEAK CHECKED IAWSep 15, 2017 · N518AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2017080821586Fire Detector · failedNR 2 ENGINE FIRE DETECTION LOOP A INOPERATIVE. ACFT GROUNDED. RETURNED NR 2 ENGINE OVERHEAT DETECTOR SWITCH ON ENGINE AND APU FIRE CONTROL PANEL BACK TO THE NORMAL POSITION. PERFORMED BITE OF ENGINE AND APU FIRE DETECTION MODULE IAW FIM 26-10-801. FOUND AN ENGAug 8, 2017 · N518AS · Boeing 737890 · Fire DetectionSDR ASAA2017072521467Warning Light · false activationWINDOW HEAT R SIDE OVERHEAT LIGHT ILLUMINATED ON DESCENT THROUGH 6000. ACFT GROUNDED. ACCOMPLISHED WINDOW OVERHEAT QRH PROCEDURES. OVERHEAT LIGHT EXTINGUISHED.Jul 25, 2017 · N518AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017062721212Shim · wornWHILE ACCOMPLISHING T/C 78472002, FOUND ALL 24 SHIMS MISSING 100% OF MOLYDAM COATING ON THE NR 1 ENGINE. ACFT GROUNDED.Jun 27, 2017 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017061721116Shim · wornWHILE ACCOMPLISHING MAINTENANCE TASK CARD 78472002 FOR FAN BLADE LUBRICATION, FOUND 24 OF THE FAN BLADE SHIMS ON THE NR 2 ENGINE WORN. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADE SHIMS IAW TASK CARD 78472002.Jun 17, 2017 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017052020863Battery Pack · inoperativeR1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REMOVED & REPLACED THE BATTERY PACK & OPS CHECKED GOOD IAW AMM 33-51-06-960-005.May 20, 2017 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2017050720755Skin · crackedFOUND CRACK INDICATION LOWER RT STABILIZER STAB STA 101.90 AFT SECTION MARKED AND CIRCLE IN RED. GROUNDED - YES. REPAIRED HORZ STAB LOWER SKIN IAW SRM 55 10 01 2R 11.May 7, 2017 · N518AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2017041020416Unknown · malfunctionedDURING LANDING, THE PRESSURIZATION "AUTO" DRIVES THE OUTFLOW TO FULL CLOSED DURING, AFTER TOUCHDOWN. IT CONTINUES TO TRY TO PRESSURIZE THE AIRCRAFT ON THE GROUND THE SYSTEM WORKS NORMALLY IN ALTERNATE MODE. ACFT GROUNDED. COMPLIED WITH PRESSURE SYSTEM GROUNDApr 10, 2017 · N518AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2017040220332Transceiver · failedNR 1 HF UNABLE TO TRANSMIT/RECEIVE. REPORTS 4/5 SIGNAL BUT VOICE TOTALLY GARBLED. WE COULD NOT RECEIVE EITHER ON NR 1HF. NR 2 HF TESTED IN COMPARISON WAS 5/5, OPS NORMAL. TRANSMIT AND RECEIVE SAME GEOGRAPHIC LOCALE. GROUNDED - YES. REF HF SYSTEM/OPS TEST AMM 2Apr 2, 2017 · N518AS · Boeing 737890 · HF Communications SystemSDR ASAA2017031520183Cdu · failedF/O MCDU DOES NOT RESPOND TO KEY INPUTS. ACFT GROUNDED. REMOVED & REPLACED THE FO'S MCDU IAW AMM 34-36-01. OPS NORMAL.Mar 15, 2017 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017022219907Fire Loop · failedWITH NR 2 ENGINE OVER HEAT DETECTOR SWITCH IN A LOOP POSITION FAULT LIGHT ILLUMINATES INTERMITTENTLY. ACFT GROUNDED. REPLACED THE NR 2 ENGINE FAN FIRE DETECTION HARNESS IAW AMM 26-11-02-000-801, AND REPLACED THE UPPER FAN FIRE DETECTOR IAW AMM 26-11-01-400-Feb 22, 2017 · N518AS · Boeing 737890 · Fire DetectionSDR ASAA2017022219904Warning Light · false activationCONTROL CABIN ZONE TEMP ILLUMINATED DURING DESCENT. ACFT GROUNDED. THE NR 2 ZONE TEMP LOGGED FLT DECK TRIM VALVE, BITE TESTED GOOD, FAULT RESET IAW FIM 21-61 TASK 801.Feb 22, 2017 · N518AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017022019881Wire Harness · failedINTERMITTENT FAULT LIGHT ILLUMINATED DURING CLIMB, ON THE FIRE PANEL FOR ABOUT 2 MINUTES, THEN EXTINGUISHED. ACFT GROUNDED. REPLACED THE NR 2 ENGINE FAN FIRE DETECTION HARNESS, IAW AMM 26-11-02-000-801, AND REPLACED THE 2 ENGINE UPPER FAN FIRE DETECTOR IAWFeb 20, 2017 · N518AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2017021419816Unknown · malfunctionedAUTOTHROTTLES WILL NOT STAY ENGAGED. GROUNDED - YES. LAST FLT, A/T FLT FAULT SHOWS A/T ENG 28V DC INV 22-31543. PERFORMED FIM 22-31 TASK 802 / 22-31 TASK 801, A/T CURRENT STATUS AND A/T INTERACTIVE SERVO MOTOR TESTS NUMEROUS TIMES WITH NO FAULTS. NO HISTORY LAFeb 14, 2017 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2017012919585Fire Detector · failedCREW REPORTS NR 2 ENGINE B FIRE LOOP WILL NOT TEST (NO HANDLE LIGHT). ACFT GROUNDED. REPLACED BOTH ENGINE CORE FIRE DETECTOR ASSEMBLY, IAW AMM 26-11-01. INSPECTED AND FOUND UPPER FAN ENGINE FIRE DETECTOR LOOP GROMMETS WORN BEYOND LIMITS. REMOVED AND REPLACEDJan 29, 2017 · N518AS · Boeing 737890 · Smoke DetectionSDR ASAA2017012919586Anti-Ice Valve · failedC/B ENGINE NR 1 ENGINE & WING CONTROL POPPED. GROUNDED - YES. REF FIM 30-11 TASK, GROUND WING THERMAL ANTI-ICE VALVE FOR NR 1 ENGINE REPLACED ON 1/25/2017, REF LOG PAGE 11626191. CHECKED WIRING BETWEEN GROUND WING TAI TEMPERATURE SOLENOID VALVE M1236 AND FIREWJan 29, 2017 · N518AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2017012719565Module · failedNR 2 ENGINE FIRE TEST FAIL, A LOOP TESTS PASS. B LOOP TEST ENGINE 2 OVERHEAT LIGHT STAYS ILLUMINATED ALL OTHER FUNCTIONS TESTED NORMAL. GROUNDED - YES. REMOVED AND REPLACED ENG/APU FIRE DETECTION MODULE IAW AMM 26-10-01-000-801 AND 26-10-01-400-801. OPERATIONAJan 27, 2017 · N518AS · Boeing 737890 · Fire DetectionSDR ASAA2017012519548Solenoid · failedNR 1 ENGINE AND WING CONTROL CIRCUIT BREAKER TRIPPED ON P-18-3 PANEL. WING ANTI-ICE SWITCH FOUND IN ON POSITION. ACFT GROUNDED. REMOVED AND REPLACED THE WING GROUND THERMAL ANTI-ICE SOLENOID VALVE NR 1 ENGINE IAW AMM 30-11-12. OPS TEST PASSED.Jan 25, 2017 · N518AS · Boeing 737890 · Airfoil Anti/De-ice SystemSDR ASAA2017012121277Cover · missingEMERGENCY LIGHT COVER AT 23C IS MISSING. ACFT GROUNDED. INSTALLED A NEW COVER.Jan 21, 2017 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2017011719428Terminal · defectiveTHE NR ENGINE B FIRE LOOP FAILED A TEST. ACFT GROUNDED. REMOVED AND REPLACED BOTH TOP LUG TERMINALS (FOUND ONE BAD AND THE OTHER ONE QUESTIONABLE) FOR THE RIGHT CORE FIRE DETECTOR IAW AMM 26-11-02. REMOVED AND REPLACED RIGHT CORE FIRE DETECTOR AS PRECAUTIONJan 17, 2017 · N518AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2017011219373Anti-Ice Valve · failedAFTER LANDING SWITCHING TO APU PWR THE NR 1 COWL VALVE / WING ANTI ICE VALVE CIRCUIT BREAKER POPPED. GROUNDED - YES. NO HISTORY PAST 90 DAYS, OPENED & GVI P18-3A6 C/B NO DEFECTS NOTED. GND IDLE NR 1 ENG OPS CHECKED NR 1 ENG ANTI-ICE ON GENERATOR & APU PWR, P18Jan 12, 2017 · N518AS · Boeing 737890 · Airfoil Anti/De-ice SystemSDR ASAA2017011019300Warning Message · false activationF/O MCDU LOCKED UP WITH FLASHING "BUTTON PUSH IGNORED" MESSAGE IN SCRATCH PAD. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, F/O'S GROUND VERIFICATION TEST PASSED, IAW AMM 34-61-01.Jan 10, 2017 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017010619256Fire Loop · malfunctionedWITH LOOP SELECTORS IN, NR 2 ENGINE DOES NOT TEST ON FIRE SYSTEM CHECK. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT. IAW AMM 26-11-00, ACCOMPLISHED ENGINE FIRE DETECTION LOOP RESISTANCE SYSTEM TEST, ALL VALUES ARE WITHIN LIMITS. REINSTALLED ENGINE, AND APU FIJan 6, 2017 · N518AS · Boeing 737890 · Smoke DetectionSDR ASAA2016121519059Drain · crackedAPU DRAIN MAST CRACKED ON AFT EDGE. ACFT GROUNDED. VERIFIED 0.80 INCH CRACK W/ HFEC MM NDT- PART 6 51-0-0 NR 23. REMOVED APU DRAIN MAST IAW AMM 28-25-07-020-801. INSTALLED APU DRAIN MAST IAW AMM 28-25-07-420-801.Dec 15, 2016 · N518AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2016120118907Warning Light · false activationON MASTER CAUTION RECALL, CONTROL CAB ZONE TEMP LIGHT ILLUMINATED. ACFT GROUNDED. NO FAULT ON RECALL. ACCOMPLISHED FIM 21-61 TASK 801 CABIN TEMPERATURE CONTROLLER BITE PROCEDURE. NO FAULTS RECORDED. OPS TESTED NORMAL.Dec 1, 2016 · N518AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016112918881Control Valve · failedDURING MASTER CAUTION RECALL, RIGHT PACK LIGHT ILLUMINATED, RESET WITH MASTER CAUTION RESET. ACFT GROUNDED. FOUND THE RT TCV FAULTING, REMOVED & REPLACED THE TCV, IAW AMM 21-51-10. OPS & LEAK CHECKED GOOD.Nov 29, 2016 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016112218811Circuit Breaker · failedDURING PDC FOUND NR 1 TRANSFER BUS OFF LIGHT ON. NO POWER TO NR 1 BUSS. ACFT GROUNDED. PERFORMED TRANSFER BUSS OFF LIGHT ILLUMINATES FAULT ISOLATION IAW FIM 24-21 TASK 822. FOUND BTB FAULT ON NR 1 GEN CONTROL UNIT. PERFORMED BTB FAULT ISOLATION IAW FIM 24-21Nov 22, 2016 · N518AS · Boeing 737890 · AC Generation SystemSDR ASAA2016102318466Module · faultedWHILE ACCOMPLISHING TSR908214, FOUND APU BITE CURRENT STATUS WITH FAULT MESSAGES 49-72101 DATA MEMORY MODULE POWER SHOWS HIGH CURRENT AND 49-72103 DATA MEMORY MODULE SHOWS CIRCUIT FAILURE. GROUNDED - YES. REMOVED AND REPLACED APU DMM PER B737-800 AMM 49-72-11.Oct 23, 2016 · N518AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2016092518126Fmc · malfunctionedVTK ON CAPTAIN'S ND FOR ABOUT 10 SECONDS ON TAXI IN. LIGHT WENT OUT WITHOUT ANY CORRECTIVE ACTION. ACFT GROUNDED. PERFORMED LEFT FMC BITE FIM 34-61 TASK 801. FOUND PROGRAM FAULT LOGGED ONE TIME. CURRENT STATUS SHOWS NO FAULTS. ACCOMPLISHED FIM 34 -61 TASK 80Sep 25, 2016 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016092518125Fmc · malfunctionedVTK FLAG ON F/O ND AT CRUISE. SINGLE FMC OPS IN MCDU SCRATCH PAD. FAULT CLEARED IN APPROXIMATELY 10 SECONDS WITH NO CREW INTERVENTION. ACFT GROUNDED. PERFORMED RIGHT FMC BITE FIM 34-61 TASK 801. FOUND PROGRAM FAULT LOGGED ONE TIME. CURRENT STATUS SHOWS NO FAUSep 25, 2016 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016082617811Slide · out of adjustFA REPORTS HARD TO ARM R1 DOOR. ACFT GROUNDED. REMOVED SLIDEPACK, ADJUSTED SLIDE E-FOLD FOR PROPER EXPOSURE. REINSTALLED SLIDE PACK, IAW AMM 25-66-01-400-803.Aug 26, 2016 · N518AS · Boeing 737890 · Escape SlideSDR ASAA2016072017440Warning Light · false activationAUTO FAIL AMBER LIGHT ON OVERHEAD PRESSURIZATION PANEL ILLUMINATED AND REMAINED DURING PRE FLIGHT. ACFT GROUNDED. PERFORMED BITE PROCEDURE ON NR 1 & 2 DIGITAL CABIN PRESSURE CONTROLLERS IAW FIM 21-31 TASK 801, CHECKED GOOD, NO FAULTS NOTED. AUTOFAIL AMBER Jul 20, 2016 · N518AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2016070217232Regulator · faultyDURING CLIMB, PASSING FL 340, DUCT PRESSURE SPLIT EXCEEDING 20. RIGHT DUCT PRESSURE 25, LEFT 49. BOTH ENGINES AT 100 PERCENT N1. ACFT GROUNDED. R & R NR 2 ENG BLEED AIR REGULATOR IAW AMM 36-11-03-000-801 AND 36-11-03-400-801. OPS CHECK NORMAL.Jul 2, 2016 · N518AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2016061917084Oil Cooler · leakingDURING PDC WALK AROUND, FOUND FUEL LEAK ON NR 2 ENGINE. ACFT GROUNDED. R & R NR 2 ENGINE MAIN OIL/FUEL HEAT EXCHANGER REF AMM 79-21-02 AND 73-11-07. ACCOMPLISHED AMM 71-00-00-700-801-F00, TEST 3A. LEAK CHECK OK. ACCOMPLISHED TEST 12 ACTUATORS TEST REF AMMJun 19, 2016 · N518AS · Boeing 737890 · Engine Oil CoolerSDR ASAA2016060116919Girt Bar · out of positionF/A'S REPORT R1 EMERGENCY SLIDE PACK HANGS LOW AND MAKES IT HARD TO ARM AND DISARM. ACFT GROUNDED. REPOSITIONED R1 SLIDE AND GIRT INTO SLIDE COVER ASSY, REF AMM 25-66-01. GIRT BAR LATCHES AND UNLATCHES NORMAL.Jun 1, 2016 · N518AS · Boeing 737890 · Emergency EquipmentSDR ASAA2016051716765Warning Light · false activationCONTROLLER CAB ZONE TEMP ILLUMINATES ON RECALL. ACFT GROUNDED. BITE OF BOTH CONTROLLERS SHOWS CABIN SENSOR FAULT FOR PREVIOUS FLIGHT. FOUND CABIN SENSOR FILTER CLOGGED. CLEANED FILTER, REF AMM 21-61-06-100-801. BITE TEST BOTH CONTROLLERS CHECKS GOOD, REF AMay 17, 2016 · N518AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016040716313Fmc · malfunctionedFMC LT FAILED. QRH FOLLOWED WHICH RESTORED NORMAL OPS. ACFT GROUNDED. CYCLED POWER TO LT FMC, OPS RESTORED. CHECK OK, REF FIM TASK 34-61 NR 836.Apr 7, 2016 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016040416238Lens · detachedPLASTIC COVER OVER EXIT LIGHT AT 17A HAS COME UNATTACHED. ACFT GROUNDED. REINSTALLED LENS COVER AT 17A, OPS NORMAL.Apr 4, 2016 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2016032316077Sliding Window · out of positionF/O WINDOW WILL NOT SLIDE SHUT. ACFT GROUNDED. REPOSITION F/O SLIDING WINDOW BACK INTO TRACK. NO DAMAGE. OPS CHECK NORMAL. REF AMM 56-12-11-710-803.Mar 23, 2016 · N518AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA2016022615716Skin · crackedLEFT HORIZONTAL LOWER SKIN IS CRACKED-INBD OF THE 6TH DRAIN HOLE. ACFT GROUNDED. ACCOMPLISHED HFEC TO VERIFY CRACK LOCATION REF NDT MANUAL 51-00-00, PART 6 PROCEDURE 23, LOCATED END OF CRACK LOCATION MEASURED APPROXIMATELY 1.5" IN LENGTH, CRACK IS CONFIRMED. Feb 26, 2016 · N518AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2016022315640Lens · missingEXIT ROW LIGHT COVER IS MISSING NEAR FLOOR ROW 17A. ACFT GROUNDED. INSTALLED NEW EXIT LENS COVER.Feb 23, 2016 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2016011314770Shim · wornWHILE ACCOMPLISHING FAN BLADE LUBE ON NR 1 ENGINE FOUND SHIMS WORN AND SEVERAL RUBBER AXIAL BUMPERS WORN ON AFT SPINNER REF T/C 78472002. ACFT GROUNDED. R & R SHIMS AND RUBBER AXIAL BUMPERS FOR NR 1 ENGINE IAW FAN BLADE LUBE T/C 78472002.Jan 13, 2016 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016010614663Valve · malfunctionedON RECAL THE ZONE TEMP LIGHT FOR THE CONTROLLER CABIN ILLUMINATED. PERFORMED QRH PROCEDURE AND LIGHT WENT OUT WITH MASTER CAUTION PUSH TO RESET. ACFT GROUNDED. REPLACED THE CONTROLLER CABIN TRIM AIR MODEL VALVE ASSY REF MM 21-61-21. OPS BITES CHECK GOOD, NO Jan 6, 2016 · N518AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016010114618Shim · wornWHILE PERFORMING T/C 78472002 FAN BLADE LUBE ON NR 2 ENGINE FOUND FAN BLADE SHIMS WORN. ACFT GROUNDED. REPLACED, 24EA, FAN BLADE SHIMS, PN 340-252-307-0 ON NR 2 ENGINE IAW T/C 78472002, STEP 42.Jan 1, 2016 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016010114613Insert · missingNR 2 ENGINE FRONT SPINNER CONE HAS ONE JACKSCREW THREADED INSERT MISSING. ACFT GROUNDED. REPLACED NR 2 ENGINE FRONT SPINNER CONE IAW AMM 72-21-01.Jan 1, 2016 · N518AS · Boeing 737890 · Turbine Engine Air Inlet Section
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