N568AS

Service difficulty reports · 479

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 = 'N568AS' 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 ASAA2018033124085Warning Message · false activationLEFT FWD WINDOW OVERHEAT LIGHT ON GROUND. FOLLOWED QRH, TURNED OFF FOR 5 MINUTES, LIGHT CAME BACK ON. ACFT GROUNDED. LEFT WHCU LOGGED P5-9 CONTROL POWER FAULT. COULD NOT DUPLICATE MALFUNCTION. LEFT WINDOW HEAT OPS CHECKED NORMAL IAW FIM 30-41 TASKS 802, 8Mar 31, 2018 · N568AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2018031223879Wire · shortedNR 1 FUEL TANK AFT PUMP LOW PRESSURE LIGHT ILLUMINATED WITH 5900 LBS INDICATED. ACFT GROUNDED. R18 GFI RELAY TRIPPED. ACCOMPLISHED FIM 28-22 / 803. FOUND WIRE W1136-3601B-16 SHORTED AT CONNECTOR D70 BACKSHELL. REMOVED THE DAMAGE, PINNED WIRING AND REPLACEMar 12, 2018 · N568AS · Boeing 737890 · Fuel System WiringSDR ASAA2018031123808Overheat Loop · malfunctionedNR 1 ENGINE OVERHEATT B SIDE, HAS A FAULT ON FIRE - OVERHEATT TEST. ACFT GROUNDED. COULD NOT DUPLICATE, NO FAULTS ON FIRE CONTROL PANEL OR MODULE BITE. OPS GOOD IAW AMM 26-11-02. NO HISTORY 30 DAYS.Mar 11, 2018 · N568AS · Boeing 737890 · Overheat DetectionSDR ASAA2018031023799Switch · malfunctionedAUTO FAIL CAUTION LIGHT ILLUMINATED ON PRESSURIZATION CONTROL PANEL. ACFT GROUNDED. CYCLED CABIN PRESSURE CONTROL SWITCH FROM AUTO TO MANUAL AND BACK. OPS CHECKED GOOD. LIGHT WENT OUT, GROUND VERIFICATION SUCESSFUL.Mar 10, 2018 · N568AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2018022723740Pressure Switch · faultedLEFT AFT FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. ACFT GROUNDED. REMOVED AND REPLACED GFI RELAY R18 IAW AMM 28-22-18-000-801, AND AMM 28-22-18-400-801. REMOVED NR 1 AFT BOOST PUMP & INSTALLED SERVICEABLE BOOST PUMP IAW AMM 28-22-41-000-801, & AMM 28-22-41-Feb 27, 2018 · N568AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2018022323680Wire Harness · failedDURING ENGINE OVERHEAT TEST, NR 2 ENGINE DID NOT LIGHT UP. ACFT GROUNDED. CONFIRMED NR 2 ENGINE B FIRE LOOP TEST INOPERATIVE. TESTED OK, AURAL & NR 2 FIRE HANDLE LIGHT WITH A LOOP ONLY SELECTED . REPLACED MW0326 CORE DETECTOR HARNESS. ALL OPS NORMAL IAW AFeb 23, 2018 · N568AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2018022723680Not Reported · malfunctionedDURING ENG OVERHEAT TEST, NR 2 ENG DID NOT LIGHT UP. GROUNDED - YES. ON DEFERRAL.Feb 23, 2018 · N568AS · Boeing 737890 · Overheat DetectionSDR ASAA2018021823657Pump · failedNR 1 AFT FUEL BOOST PUMP LOW PRESSURE LIGHT IS ILLUMINATED. ACFT GROUNDED. GVI NR 1 AFT B/P C/B & GFI RELAY R18 NO DEFECT NOTED GFI OPS TEST COMPLETED IAW AMM 28-22-41-720-802. NO DEFECT NOTED. COMPLETED FIM 28-22, 803. OPS NORMAL. REMOVED & REPLACED THE NRFeb 18, 2018 · N568AS · Boeing 737890 · Fuel Boost PumpSDR ASAA2018020623435Lamp · failedEMERGENCY LIGHT OUT, AFT OF THE L2 DOOR. ACFT GROUNDED. REPLACED THE LAMPS. OPS GOOD IAW AMM 33-51-04/201.Feb 6, 2018 · N568AS · Boeing 737890 · Emergency LightingSDR ASAA2018020323377Control Valve · failedBOTH ENGINES SLOW TO START DUE LOW PRESSURE. APU DUCT PRESSURE 20 PSIG MAX DURING ENGINE START. AIRFLOW AUDIBLE IN FLIGHT DECK WITH PACKS OFF & NR 1 ENGINE BLEED ON. ACFT GROUNDED. LEFT PACK FLOW CONTROL & SHUTOFF VALVE BYPASSING AIR. REMOVED & REPLACED THFeb 3, 2018 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018012723305Warning Light · false activationFOUND AIRCRAFT WITH THE BATTERY SWITCH ON, AND GROUND POWER OFF, ELEC CAUTION LIGHT ILLUMINATED WHEN GROUND POWER ESTABLISHED. ACFT GROUNDED. BITE SHOWED AUX BATTERY CHARGER INOPERATIVE, STATIC INVERTER INOPERATIVE. CLEARED FAULTS IAW AMM 24-21-53. BATTERIEJan 27, 2018 · N568AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2018012323273Spinner · damagedNR 1 ENGINE FWD SPINNER MISSING 50% COATING. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENGINE FWD SPINNER. REF T/C 78472002.Jan 23, 2018 · N568AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017122122973Control Valve · faultedRIGHT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL, EXTINGUSHED WHEN MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED PACK ZONE TEMPERATURE BITE IAW AMM 21-61-00-700-806-002. NR 2 CONTROLLER FAULTED TCV. REMOVED & REPLACED TEMPERATURE CONTROL VALVE IDec 21, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017122022962Switch · defectiveAIR CONDITIONING PANEL, ISOLATION VALVE APPEARS INOPERATIVE. ACFT GROUNDED. ON ARRIVAL, PACKS INOPERATION, ISOLATION VALVE INOPERATIVE. WOULD NOT CLOSE. NORMAL OPS WITH SWITCH. FORCEFULLY JIGGLED SWITCH TO OFF POSITION, THE ISOLATION VALVE OPS NORMAL OPENDec 20, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017122022961Actuator · no testDURING A BITE TEST, THE NR 1 TEMP CONTROLLER LT RAM AIR ACTUATOR FAILED, UNABLE TO CLEAR FAULTS. ACFT GROUNDED. REMOVED AND REPLACED THE LT RAM AIR ACTUATOR IAW MM 21-51-21. PERFORMED A BITE CHECK, NO FAULTS, CHECKED GOOD.Dec 20, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017121022838Screw · looseREF T/C # 78472000 #2 ENG INLET AND FAN BLADES - DETAILED INSPECTION FOUND 1 LOOSE SCREW ON LWR FWD SIDE OF 3 O'CLOCK STRUT PANEL. GROUNDED - YES. RESECURED/TIGHTENED LOOSE FASTENER/SCREW LWR SIDE OF 3 O'CLOCK STRUT PANEL AS NEEDED.Dec 10, 2017 · N568AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017112722700Warning Light · false activationRIGHT PACK LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. ACCOMPLISHED FIM 21-53 ,TASK 810. ZONE TEMP CONTROLLER BITE SHOWS TCV FAULT PREVIOUS FLIGHT. FAULT RESETS AND BITE TESTED GOOD IAW AMM 21-61-00, AND PACK FLOW TEMP CONTROL BITE, IAW AMM 21-61-00-740, NONov 27, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017112122653Warning Light · false activationFLIGHT CREW REPORTED A HF TUNING PANEL WINDOW FAILED. ACFT GROUNDED. CYCLED POWER, PERFORMED HF BITE CHECK IAW FIM 23-11, TASK 801. OPS CHECKED GOOD, FAIL LIGHT EXTINGUISHED.Nov 21, 2017 · N568AS · Boeing 737890 · HF Communications SystemSDR ASAA2017102422317Warning Light · false activationRED BOXES ILLUMINATED ON BOTH EGT DISPLAYS AFTER ENGINE SHUTDOWN ON THE GROUND. ACFT GROUNDED. ACCOMPLISHED HPT BLADE BSI IAW AMM 72-00-00-200-807-F00, NO DEFECTS NOTED. PERFORMED STEPS F (3)A PNEUMATIC LEAK CHECK. LEAK CHECKED GOOD. PERFORMED STEPS FOct 24, 2017 · N568AS · Boeing 737890 · Central WarningSDR ASAA2017092622054Controller · malfunctionedRIGHT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL. EXTINGUISH ON MASTER CAUTION RESET. GROUNDED - YES. RESET PACK CONTROLLER, REF AMM 21-61-00. OPS CHECK GOOD.Sep 26, 2017 · N568AS · Boeing 737890 · Cabin Temperature ControllerSDR ASAA2017083121768Lens · missingFLIGHT ATTENDANTS REPORTED AN EMERGENCY EXIT LIGHT LENS MISSING. ACFT GROUNDED. REMOVED AND REPLACED EMERGENCY EXIT ROW LIGHT ASSY. OPS NORMAL IAW AMM 33-51-01-960-802.Aug 31, 2017 · N568AS · Boeing 737890 · Emergency LightingSDR ASAA2017071421398Bulkhead Web · crackedLEFT MLG WW FWD BULKHEAD WEB CRACKED, BS 663.75, WL 203.5, LBL 33.5. ACFT GROUNDED. ACCOMPLISHED A CATEGORY B REPAIR IAW SRM 57-10-10-2R-3, REPAIR 3, ALTERNATE I.Jul 14, 2017 · N568AS · Boeing 737890 · Fuselage Main, BulkheadSDR ASAA2017052320857Circuit Breaker · trippedNR 2 COWL ANTI-ICE VALVE CIRCUIT BREAKER TRIPPED. ACFT GROUNDED. INSPECTED THE CIRCUIT BREAKER ON P18-3 PANEL WITH NO DEFECTS NOTED. RESET THE CIRCUIT BREAKER AS ALLOWED BY AMM 20-60-01. RAN THE NR 2 ENGINE AND OPERATED COWL ANTI-ICE VALVE SEVERAL TIMES, CMay 23, 2017 · N568AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2017032220244Cdu · faultedWHILE PERFORMING CDU FAULT INTERROGATION ON THE NR 1 ENGINE, FOUND MESSAGES 73-10791 AND 73-10791, PS3 SIGNALS DISAGREE SHORT TIME FAULT. ACFT GROUNDED. THIS FAULT DID NOT SHOW UP AGAIN. SHORT TIME CODE 73-10791 IS CLEARED IAW TASK CARD 78273000.Mar 22, 2017 · N568AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2017030920113Warning Light · false activationRIGHT PACK LIGHT ON MASTER RECALL. EXTINGUISHES WITH RESET. ACFT GROUNDED. RIGHT ZONE TEMP CONTROLLER SHOWS TCV FAULT. FAULT CLEARED IAW AMM 21-61-20-400-201. OPS CHECKED NORMAL.Mar 9, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017030720101Warning Message · false activationFOUND NR 1 ENGINE SHORT TIME FAULT MESSAGE 73-10791. PS3 SIGNALS DISAGREE. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE INTERROGATION OF FMC FOR ENGINE FAULTS T/C 78273000, CURRENT STATUS & FLIGHT FAULT HISTORY SHOW NO FAULTS.Mar 7, 2017 · N568AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2017030720100Warning Message · false activationFOUND NR 1 ENGINE SHORT TIME FAULT MESSAGE 73-20791. PS3 SIGNALS DISAGREE. ACFT GROUNDED. ACCOMPLISHED NR 1 ENGINE INTERROGATION OF FMC FOR ENGINE FAULTS T/C 78273000, CURRENT STATUS & FLIGHT FAULT HISTORY SHOW NO FAULTS.Mar 7, 2017 · N568AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2017022619950Warning Light · false activationAPU FAULT LIGHT DURING START. ACFT GROUNDED. STARTED AND OPERATED APU. APU STARTS AND OPERATES NORMALLY. PERFORMED FIM 49-55 TASK 801 E(1) THRU (6). NO FAULTS FOUND. IAW FIM, SOME FLAME IN EXHAUST DURING START IS NORMAL DURING CONSECUTIVE STARTS. NO CURRFeb 26, 2017 · N568AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2017021919849Sensor · failedON RECALL, LEFT PACK LIGHT ILLUMINATES. GOES OUT WHEN RESET MASTER CAUTION. ACFT GROUNDED. REMOVED AND REPLACED LT RAM AIR SENSOR, IAW AMM 21-51-50, BITE CHECKED GOOD IAW AMM TASK 21-61-00-700-806-002.Feb 19, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017021819848Acm · failedLEFT PACK LIGHT ILLUMINATED. ACFT GROUNDED. AFTER 3 RESETS, ZONE TEMP CONTROLLER NR 1 SHOWS PACK TEMP CONTROL VALVE IAW FIM 21-61 TASK 801. REPLACED THE LEFT PACK TEMP CONTROL VALVE IAW AMM TASK 21-51-10-000-801, & 21-51-10-400-801. ACCOMPLISHED BITE- PASSED.Feb 18, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017021819845Warning Message · illuminatedAUTO FAIL LIGHT ILLUMINATED ON PRESSURIZATION PANEL. AFTER CYCLING SELECTOR SWITCH, AUTO FAIL LIGHT EXTINGUISHED. ACFT GROUNDED. NR 2 CPC SHOWED MESSAGE 006 FOR PREVIOUS FLT, SYSTEM TESTED NORMAL & FAULT HISTORY RESET. CPC PASSED GROUND VERIFICATION TEST IAFeb 18, 2017 · N568AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2017021219782Control Valve · failedDURING TAXI, ACFT IN NORMAL BLEED CONFIGURATION, THE NR 1 ENGINE TAKEOFF N1 WAS 90.5, NR 2 ENGINE TAKEOFF N1 WAS 89.9 ON FMC. ACFT GROUNDED. STARTED BOTH ENGINES AND FOUND NUMBERS ON FMCS TO BE THE SAME ON DEFECT. DISCRETES WOULD NOT CHANGE ON LT PACK FMC CDFeb 12, 2017 · N568AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017020619726Sensor · contaminatedON APU SHUT DOWN, APU FAULT LIGHT ILLUMINATED. WAITED 5 MINUTES AND FAULT LIGHT EXTINGUISHED. TRIED TO START APU TWICE AND BOTH TIMES APU FAILED TO START AND FAULT LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED FIM 49-60 TASK 801 & 49-60 TASK 812. REMOVED INLFeb 6, 2017 · N568AS · Boeing 737890 · APU ControlsSDR ASAA2017011219417Baffle · crackedFWD CARGO BAY RT TRANSITION PANEL BAFFLE AND ANGLE BETWEEN BS 500G AND 500H ARE CRACKED. ACFT GROUNDED. REMOVED AND REPLACED BAFFLE AND ANGLE IAW SRM 51-40-02.Jan 12, 2017 · N568AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017010719400Web · corrodedAFT CARGO BAY FLOOR WEB HAS CORROSION BETWEEN BS 787 AND 847, RBL 21-28. ACFT GROUNDED. REMOVED AND REPLACED THE WEB IAW DWG 146A8123 REV C AND SRM 51-40-02,Jan 7, 2017 · N568AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017010619451Floor Support · corrodedCOCKPIT FLOOR PANEL FLANGE HAS CORROSION AT ENTERYWAY. ACFT GROUNDED. REPAIRED IAW EA 800-53EA-18322 REV 00.Jan 6, 2017 · N568AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017010619420Channel · corrodedFWD PIT - RT TRANSITION PANEL HAS AREAS OF CORROSION FROM STA 500C TO STA 500I ( MARKED IN RED ). GROUNDED - YES. REMOVED CORROSION FROM STA 500L TO STA 500I IAW SRM 53-30-53-01. ORIG MAT .090 IAW SRM 53-00-53. MAT REMOVED .004, MATERIAL REMAINING .036. FOUNDJan 6, 2017 · N568AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017010619404Transition Panel · crackedAFT CARGO BAY RIGHT TRANSITION PANEL CRACKED BS 727G - 767, STRINGERS 25 - 26R. ACFT GROUNDED. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R-5, DWG 146A7502 REV- ND, AND 140N4500 REV G.Jan 6, 2017 · N568AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017010619399Transition Panel · corrodedAFT CARGO BAY LEFT TRANSITION PANEL UPPER SURFACE CORRODED BS 727 - 727G. ACFT GROUNDED. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-2R-5 AND DWG 146A7502 REV-, AND 140N4500 REV G.Jan 6, 2017 · N568AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016122819187Battery Pack · inoperativeR1 DOOR EMERGENCY LIGHTS INOPERATIVE. ACFT GROUNDED. REMOVED & REPLACED THE BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-06-960-805.Dec 28, 2016 · N568AS · Boeing 737890 · Emergency LightingSDR ASAA2016121619064Probe · failedNR 2 TANK FUEL PROBES F2, F7, F8, F9 &F10 OUT OF LIMITS IAW AMM 28-41-21. ACFT GROUNDED. REPLACED THE FUEL PROBES IAW AMM 28-41-21. FQIS SYSTEM TEST NORMAL IAW AMM 28-41-00-730-801.Dec 16, 2016 · N568AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016121619063Probe · failedNR 1 TANK FUEL PROBES F6, F7, & F8 OUT OF LIMITS IAW AMM 28-41-21. ACFT GROUNDED. REPLACED THE FUEL PROBES IAW AMM 28-41-21 . FQIS SYSTEM TEST NORMAL,Dec 16, 2016 · N568AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016121519061Warning Light · illuminatedAFTER TAKE OFF, RECEIVED A FUEL IMBALANCE ALERT. CENTER PUMPS WERE ON AND MAIN TANKS WERE BALANCED PRIOR TO TAKEOFF. QUANITY CONTINUED TO DECREASE THEN STABILIZED. ACFT GROUNDED. ACCOMPLISHED OPERATIONAL AND FUNCTIONAL TEST OF CROSSFEED VALVE. OPS CHECKED ODec 15, 2016 · N568AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016112518828Engine · faultedDURING CDU ENGINE BITE TEST FOUND SHORT TERM FAULT MESSAGE 73-20791. (PS3 SIGNALS DISAGREE) ON NR 1 ENGINE. ACFT GROUNDED. PERFORMED FIM 73-26 TASK 806, NO FAULTS DETECTED WITH EEC BITE TEST. PERFORMED WORK TASK CARD 78273000, NO FAULTS RECORDED IN RECENT OR FNov 25, 2016 · N568AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016112418803Control Panel · failedVERTICAL SPEED DISPLAY HAS ILLUMINATION THAT SHOULD NOT BE THERE. ACFT GROUNDED. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34. INSTALLATION TEST PASSED IAW AMM 22-11-34-740-801. ACCOMPLISHED DFCS MCP LRU INTERFACE TEST GRP BITE 32 AND LAND VERIFY TNov 24, 2016 · N568AS · Boeing 737890 · Autopilot SystemSDR ASAA2016112118790Transmitter · leakingNR 1 ENGINE FUEL FLOW TRANSMITTER LEAKING. ACFT GROUNDED. REPLACED THE FUEL FLOW TRANSMITTER IAW AMM 73-31-01-400-801-F00, LEAK AND OPS CHECKED GOOD.Nov 21, 2016 · N568AS · Boeing 737890 · Engine Fuel Indicating SystemSDR ASAA2016112118788Fairing · crackedWHILE PERFORMING A BORESCOPE INSPECTION, FOUND 3 O'CLOCK STRUT FAIRING ON NR 1 ENGINE TO BE CRACKED ON LOWER SECTION. ACFT GROUNDED. REMOVED & REPLACED THE STRUT FAIRING.Nov 21, 2016 · N568AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016110618584Transmitter · failedDURING TAKEOFF ROLL, LOST FUEL FLOW INDICATION FOR NR 2 ENGINE ALL OTHER INDICATIONS NORMAL. ACFT GROUNDED. FMC CDU BITE SHOWED 2 FAULTS -73-31052 ON FLT LEG 5 AND 6 FOR F/F TRANSMITTER. ACCOMPLISHED FIM 73-31 TASK 801. REPLACED THE F/F TRANSMITTER IAW AMM 7Nov 6, 2016 · N568AS · Boeing 737890 · Engine Fuel Indicating SystemSDR ASAA2016110318572Panel · damagedNR 1 ENGINE FAN DUCT PANEL AT 200 POSITION HAS LOOSE BOLT. GROUNDED - YES. FOUND ELONGATED HOLE AT PANEL 2.00 POSITION ON NR 1 ENGINE FAN DUCT. REMOVED AND REPLACED NR 1 ENGINE FAN DUCT PANEL AT 2.00 POSITION, IAW AMM 72-23-07.Nov 3, 2016 · N568AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2016101418345Blades · damagedNR 2 ENGINE, NR 4 COMPRESSOR STAGE BLADE 6 HAS DAMAGE .113" IN DIMENSION B AND NR 8 COMPRESSOR STAGE NR 36 BLADE HAS .052 DAMAGE IN DIMENSION B. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE IAW T/C 78471000.Oct 14, 2016 · N568AS · Boeing 737890 · Turbine Engine Compressor Section
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