N512AS

Service difficulty reports · 394

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 = 'N512AS' 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 ASAA2018122677567Skin · crackedL/H HORIZ LOWER SKIN HAS A CRACK BETWEEN STA 147 AND 167 9 IN. FWD OF REAR SPAR. GROUNDED - YES. REPAIRED DAMAGE TO SKIN IAW B737 800 SRM 55 10 01 2R 11 REP 11 THIS IS A CAT. B REPAIR WITH AN INSPECTION THRESHOLD OF 56000 TOTAL FLT. CYCLES AND 9,000 FLT. CYCLENov 27, 2018 · N512AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2018122677566Skin · crackedL/H HORIZ LOWER SKIN HAS A CRACK BETWEEN STA 120 AND 129. 9 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED DMGE TO SKIN IAW B737 800 SRM 55 10 01 2R 11 REP 11. THIS IS A CAT. B REPAIR IWTH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLT. CYCLES AND 9,000 FLT. CNov 27, 2018 · N512AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2018122627541Skin · crackedRH HORIZ STAB LOWER SKIN IS CRACKED BETWEEN STA 92 AND 101 APPROX 11 IN. FWD OF REAR SPAR. GROUNDED - YES. REPAIRED DAMAGE TO SKIN IAW B737 800 SRM 55 10 01 2R 11 REPAIR 11 THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 TOTAL FLT. CYCLES ANNov 27, 2018 · N512AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2018112627050Warning Light · false activationON CLIMBOUT, GOT RIGHT "PACK" LIGHT, FOLLOWED QRH. LIGHT WENT OUT, COMES BACK ON RECALL. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE PROCEDURE FOR BOTH ZONE TEMP CONTROLLERS PER B737-800 FIM 21-62 TASK 801. PERFORMED NUMEROUS FIM 21-53 TASKS 806. LIGHT STNov 22, 2018 · N512AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018110826786Idg · inoperativeGENERATOR NR 2 WILL NOT COME ON LINE. NO VOLTS/ FREQS AND DRIVE LIGHT IS ILLUMINATED. GROUNDED - YES. REMOVED AND REPLACED IDG REF AMM 24-11-11. OPS CHECK GOOD.Nov 8, 2018 · N512AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2018103126677Modulating Valve · inoperativeRIGHT PACK LIGHT ILLUMINATES ON RECALL DURING AFTER START. GROUNDED - YES. HARD RT TEMPERATURE CONTROL VALVE FAULT. I RESET THE CONTROL BOX BUT AFTER RUNNING THE PACKS THE TCV FAULT CAME UP RIGHT AWAY. REMOVED AND REPLACED RT TEMPERATURE CONTROL VALVE IAW AMM Oct 31, 2018 · N512AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2018102926647Actuator · inoperativeAFTER START, ENG NR 2 SPAR VALVE CLOSED LIGHT STAYED ILLUMINATED. GROUNDED - YES. REMOVED AND REPLACED ENG NR 2 SPAR VALVE ACTUATOR. PERFORMED ELECTRICAL CONTROL AND INDICATION TEST. TEST PASSED. REF AMM 28-22-11.Oct 28, 2018 · N512AS · Boeing 737890 · Aircraft Fuel Distribution SystemSDR ASAA2018100826396Transceiver · failedFAIL LIGHT ON HF PANEL 2. GROUNDED - YES. PERFORMED HF COMMUNICATION BITE ON HF2. FOUND LRU FAULT. REF FIM 23-11 TASK 801. REMOVED & REPLACED HF2 TRANSCEIVER REF AMM 23-11-21. OPS CHECK GOOD.Oct 5, 2018 · N512AS · Boeing 737890 · HF Communications SystemSDR ASAA2018090826070Starter Gen · faultyAPU FAILED TO START, FAULT LIGHT ILLUMINATED. NO ROTATION SHUTDOWN MAINT MESSAGE 49-41012. GROUNDED - YES. REMOVED AND REPLACED APU STARTER-GENERATOR UNIT PER AMM 49-41-21. REPLACEMENT AND GROUND VERIFICATION INSTALLATION ACCOMPLISHED, OPS CK GOOD. APU CURRENTSep 8, 2018 · N512AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2018091026059Indicator · failedCENTER TANK FUEL QTY INDICATOR AT THE WING PANEL IS BLANKING INOP. GROUNDED - YES. REPLACED CENTER TANK FUEL QUANTITY IND ON WING REFUELING PANEL PER AMM 28-41-. OPS CHECK GOOD.Sep 7, 2018 · N512AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2018090425994Warning System · false activationON INITIAL START UP APU FAULT LIGHT ILLUMINATED. GROUNDED - YES. OPERATED APU 4X. NO FAULTS NOTED AND NO HISTORY PAST 30 DAYS. COMPLETED APU BITE CHECK REF AMM 49-60-801. REF FIM 49-40 TASK 803.Sep 2, 2018 · N512AS · Boeing 737890 · APU Indicating SystemSDR ASAA2018090425993Door · out of positionON INITIAL START - APU FAILED TO START AND "FAULT" LIGHT ILLUMINATED. GROUNDED - YES. RESET INLET DOOR POSITION FOR APU, RESET SUCCESSFUL, APU TESTS GOOD IAW AMM 49-11-00-710-801.Aug 31, 2018 · N512AS · Boeing 737890 · APU Cowling/ContainmentSDR ASAA2018082982945Sign · detachedEMERGENCY EXIT SIGN ON THE CABIN CEILING, BETWEEN THE OVERWING EXITS WAS DETACHED. ACFT GROUNDED. REINSTALLED AND TESTED THE SIGN IAW AMM 33-51-01-960-801, OPS NORMAL.Aug 28, 2018 · N512AS · Boeing 737890 · Emergency LightingSDR ASAA2018082725914Warning Light · false activationPRIOR TO TAKEOFF, AUTO FAIL LIGHT ILLUMINATED, AFTER CYCLING SYSTEM TO MANUAL AND BACK TO AUTO THE LIGHT WENT OUT. ACFT GROUNDED. ACCOMPLISHED FIM 21-31, TASK 827, AND FIM 21-31, TASK 801. NO FAULTS ON CABIN PRESSURE CONTROLLERS AND AUTO FAIL LIGHT OUT.Aug 26, 2018 · N512AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2018070225241Idg · failedNR 1 DRIVE LIGHT NOT ILLUMINATED WITH ENGINE SHUT DOWN. GROUNDED - YES. PERFORMED FIM 24-11 TASK 804, CHANGE PRESSURE SWITCH RESISTANCE OUT OF LIMITS, REQUIRES IDG CHANGE. REMOVED AND REPLACED IDG REF AMM 24-11-11. OPS CHECK GOOD.Jun 30, 2018 · N512AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2018062725234Sensor · intermittentLT SIDE WINDOW HEAT CAUTION OVERHEAT ILLUMINATED IN FLIGHT. TURNED SWITCH OFF. GROUNDED - YES. REMOVED AND REPLACED L2 SLIDER WINDOW REF AMM 56-12-11. OPENABLE WINDOW ADJUSTMENT GOOD AT THIS TIME REF AMM 56-12-11-820-801. WINDOW HEAT SYSTEM OPERATION TEST GOODJun 27, 2018 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2018062725223Control Panel · malfunctionedCAPT WX RADAR IN AUTO MODE SHOWING GROUND CLUTTER IN ALL MODES FO'S SIDE SHOWS ACCURATE RETURNS. GROUNDED - YES. REPLACED WEATHER RADAR CONTROL PANEL PER AMM 34-43-91. PERFORMED GOOD INSTALLATION TEST PER AMM 34-43-91-400-801. PERFORMED GOOD SYSTEM TEST PER AMJun 27, 2018 · N512AS · Boeing 737890 · Weather Radar SystemSDR ASAA2018062725222Sensor · failedLEFT FWD WINDOW OVERHEAT LIGHT CAME ON. GROUNDED - YES. PERFORMED FIM 30-41 TASK 801. FOUND LEFT FWD SENSOR FAULT. SWITCHED TO OTHER SENSOR, REF FIM 30-41-TASK 812. OPS CHK-GOOD. LIGHT EXTINGUISHED.Jun 27, 2018 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2018062625214Warning System · false activationL SIDE WINDOW HEAT OVERHEAT LIGHT CAME ON IN FLIGHT. GROUNDED - YES. CYCLED SWITCH OFF FOR 3 MINUTES IN ACCORDANCE WITH QRH. LIGHT DID NOT COME BACK ON WHEN SWITCH WAS RETURNED TO ON.Jun 26, 2018 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2018061985117Ecu · faultedAPU ECU FAULT CODE 49-61145 FOUND DURING TSR701868. ACFT GROUNDED. PERFORMED FIM 49-60, TASK 802, REQUIRES REPLACEMENT OF APU ECU. REMOVED APU ECU IAW AMM 49-61-12-000-801 AND REPLACED APU ECU IAW AMM 49-61-12-400-801 STEPS 3A -E(2) . ACCOMPLISHED AMM 49-61-Jun 18, 2018 · N512AS · Boeing 737890 · APU ControlsSDR ASAA2018061625077Transceiver · malfunctionedCAPTAIN'S SIDE RADAR RETURNS INACCURATE. FIRST OFFICERS SIDE ACCURATE. TESTED OKAY, BOTH SIDES. ACFT GROUNDED. REMOVED & REPLACED THE RADAR TRANSCEIVER IAW AMM 34-43-41, OPS CHECKED NORMAL IAW AMM 34-43-00-710-802-001.Jun 16, 2018 · N512AS · Boeing 737890 · Weather Radar SystemSDR ASAA2018060924999Button · faultyWEATHER RADAR STAYS IN NORMAL EVEN WHEN AUTO IS SELECTED. AUTO MODE CAN BE OBTAINED BY DEPRESSING AND HOLDING DOWN THE AUTO BUTTON, WHEN YOU LIFT OFF THE BUTTON IT WILL GO BACK TO MANUAL MODE. ACFT GROUNDED. REPLACED THE WEATHER RADAR CONTROL PANEL IAW AMMJun 9, 2018 · N512AS · Boeing 737890 · Weather Radar SystemSDR ASAA2018060724972Shim · wornREF T/C 78472002, NR 1 ENG S/N 897424 FAN BLADE SHIMS MOLYDAG COATING WORN THRU (100%). GROUNDED - YES. REPLACED THE NR 1 ENG FAN BLADE SHIMS (ALL 24) REF T/C 78472002.Jun 7, 2018 · N512AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2018060724971Seal · tornREF T/C 78472002, NR 1 ENG S/N 897424 FAN BLADE PLATFORM SEALS TORN, CUMULATIVE LENGTH IN EXCESS OF 40". GROUNDED - YES. REPLACED THE NR 1 ENG FAN BLADE PLATFORMS (ALL 24) REF T/C 78472002.Jun 7, 2018 · N512AS · Boeing 737890 · Turbine Engine Compressor SectionSDR ASAA2018060874963Probe · no testNR 1 MAIN TANK FQIS FAILED A SYSTEM TEST IAW AMM 28-41-00-730-801, & NG-28FCD-18088-1. ACFT GROUNDED. THE NR 2 TANK UNIT AND NR 9 TANK UNIT WERE OUT OF LIMITS. REPLACED IAW AMM 28-41-21/401. TANK AND COMPENSATOR UNITS TESTED FOR THE NR 1 TANK PASSED IAW AMM Jun 7, 2018 · N512AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2018061164968Apu · malfunctionedAPU FAULT LIGHT WHEN START ATTEMPTED DURING TAXI IN. ACCOMPLISHED QRH PROCEEDING ATTEMPTED ANOTHER START WHEN THE FAULT LIGHT WHEN OUT APU FAULT LIGHT ILLUMINATED AGAIN, OBSERVED NO EGT RISE PRIOR TO FAULT LIGHT ILLUMINATING. GROUNDED - YES. ACCOMPLISHED APJun 6, 2018 · N512AS · Boeing 737890 · Airborne Auxiliary Power Unit (APU) SystemSDR ASAA2018060864962Probe · no testNR 2 MAIN TANK FUEL QUANTITY INDICATING SYSTEM FAILED A SYSTEM TEST IAW AMM 28-41-00-730-801. ACFT GROUNDED. REMOVED AND REPLACED THE FUEL QUANTITY PROBES NR F8 & F9 IAW AMM 28-41-21-400-801. ACCOMPLISHED FQIS SYSTEM TEST IAW AMM 28-41-00-730-801. OPS CHECKJun 6, 2018 · N512AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2018051424623Seal · debondedWHILE ACCOMP FAN LUBE ESN 895170 FOUND ONE PLATFORM @ POS 12 WITH DISBONDED SEAL. GROUNDED - YES. REMOVED AND REPLACED 1 EA PLATFORM AT POSITION 12 IAW TASK CARD 78472002, SUB TASK 839-045.May 14, 2018 · N512AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018051424622Blade · damagedWHILE ACCOMPLISHING FAN LUBE ESN 895170 FOUND CU-N1 COATING ON NR 17 BLADE. GROUNDED - YES. REMOVED AND REPLACED BLADES NR 17 AND NR 5 IAW AMM 72-21-02-000-802-F00. ACCOMP ULTRASONIC INSPECTION OF NEW FAN BLADE ROOTS PER SUPPLEMENT 72-21-02 NO DISCONTINUITIES May 14, 2018 · N512AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018051424621Blade · damagedWHILE ACC FAN LUBE ESN-895170 CUNI COATING BEYOND AREA X LIMITS BLADE NR 11. GROUNDED - YES. REMOVED AND REPLACED BLADES NR 11 AND NR 23 IAW AMM 72-21-02-000-802-F00. ACCOMP ULTRASONIC INSP OF NEW FAN BLADE DOVETAILS PER SUPPLEMENT NO DISCONTINUITIES NOTED. ACMay 14, 2018 · N512AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2018050124449Eec · faultedWHILE PERFORMING TC 78273000, TO INTERROGATE THE FMC CDU FOR ENGINE FAULTS, FOUND TWO SHORT TERM FAULTS FOR THE INTERNAL EEC FAULT (FC 73-10011, 73-10021) NR 1 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE EEC IAW AMM 73-21-60. PERFORMED TESApr 30, 2018 · N512AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2018042324379Compensator · failedPERFORMED A TANK AND COMPENSATOR UNITS TEST OF THE NR 2 TANK IAW AMM 28-41-21-710-801. FOUND THE TU NR 3 TO BE OUT OF LIMITS. REPLACED TU IAW AMM 28-41-21/401. LEAK CHECKED GOOD. NR 2 FQIS CHECKED GOOD IAW AMM 28-41-00-710-801. NR 2 FQIS SYSTEM TEST PASSED IApr 23, 2018 · N512AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2018032524026Warning Message · false activationAPU FIRE DETECTOR FAILED AN OPS CHECK. APU DETECTOR INOPERATIVE ILLUMINATED. ACFT GROUNDED. PERFORMED AN OPS CHECK OF APU FIRE DETECTION SYSTEM IAW AMM 26-15-00-710-801. OPS CHECKED GOOD.Mar 25, 2018 · N512AS · Boeing 737890 · Fire DetectionSDR ASAA2018012123234Indicator · failedDURING REFUELING, REFUEL PANEL CENTER TANK INDICATOR WENT BLANK DURING REFUELING. GROUNDED - YES. REMOVED & REPLACED CENTER TANK INDICATOR AT REFUEL PANEL REF AMM 28-41-61-000-801 & 28-41-61-400-801. OPS CKD GOOD.Jan 21, 2018 · N512AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2017121522932Controller · faultedUPON LANDING L2 WINDOW HEAT ON LIGHT WENT OFF. WINDOW FEELS COLD. ACFT GROUNDED. PERFORMED TROUBLESHOOTING IAW FIM 30-41 TASK 809. WHCU BITE FOR M0322 WAS GOOD WITH NO FAULTS. HEATER ELEMENT AT WINDOW WAS 60.3 OHMS. WINDOW HEAT SENSOR RESISTANCE FOR PRIMARYDec 15, 2017 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017121522931Warning Light · false activationL2 WINDOW OVERHEAT. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE, OVERHEAT LIGHT EXTINGUSHED AND REMAINED EXTINGUISHED.Dec 15, 2017 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017121422930Warning Light · false activationL2 COCKPIT WINDOW OVERHEAT. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE, OVERHEAT LIGHT EXTINGUISHED AND REMAINED EXTINGUISHED.Dec 14, 2017 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017121322904Warning Light · false activationLEFT SIDE WINDOW OVERHEAT ILLUMINATED. QRH FOLLOWED, STAYED EXTINGUISHED. GROUNDED - YES. ACCOMPLISHED QRH PROCEDURE. WINDOW OVERHEAT LIGHT EXTINGUISHED AND STAYED EXTINGUISHED.Dec 13, 2017 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017121222886Warning Light · false activationLEFT SIDE WINDOW HEAT LIGHT ILLUMINATED IN FLIGHT. GROUNDED - YES. ACCOMPLISHED QRH PROCEDURE. WINDOW HEAT LIGHT EXTINGUISHED.Dec 12, 2017 · N512AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2017120522806Pump · leakingWHILE ACCOMPLISHING TSR 701083 FOUND FUEL LEAKING FROM NR 2 ENGINE FUEL PUMP DRAIN PAD. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG FUEL PUMP REF AMM 73-11-11-000-801-F00 & AMM 73-11-11-400-801-F00. REMOVED AND REPLACED NR 2 ENG FUEL PUMP SEAL REF AMM 72-60-Dec 5, 2017 · N512AS · Boeing 737890 · Engine Fuel PumpSDR ASAA2017120522799Seal · leakingWHILE ACCOMPLISHING TSR701083 FOUND IDG PAD DRAIN LEAKING OIL ON #2 ENG. GROUNDED - YES. REMOVED IDG #2 ENG, REMOVED AND REINSTALLED SEALOL SEAL PER SUBTASK 72-60-00-410-004-F00. REINSTALLED #2 ENG IDG PER MM 24-11-11-400-801. LEAK & OPS CHECKS REQ. 13072 12/0Dec 5, 2017 · N512AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA2017120122754Seal · leakingFOUND OIL LEAKING FROM #2 ENGINE. GROUNDED - YES. REMOVED THE FUEL PUMP PACKAGE AND REPLACED SEALOL SEAL PER B737-800 MM 72-60-00. REINSTALLED THE FUEL PUMP PACKAGE PER AMM 73-11-01. IDLE LEAK LK CK GOOD, EEC AND ACTUATORS TEST GOOD. ALTERNATE DEACTIVATION PRODec 1, 2017 · N512AS · Boeing 737890 · Engine Fuel PumpSDR ASAA2017112222666Controller · malfunctionedON MASTER RECALL, ZONE TEMP CONTROL CABIN ILLUMINATED. ACFT GROUNDED. INITIAL INSPECTION SHOWED THE NR 2 TEMP CONTROLLER WITH FLT DECK TRIM VALVE FAULT. PERFORMED AMM 21-61-20-860-005. RESET FAULT, RAN TEST 3 MORE TIMES, NO DEFECTS NOTED.Nov 22, 2017 · N512AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017110722474Autothrottle Sys · malfunctionedAUTOTHROTTLE ARMED FOR TAKEOFF AND DISCONNECTED AT TOGA ON TAKEOFF. ADVANCED THROTTLES MANUALLY. ATTEMPTED TO REENGAGE BUT THE AUTOTHROTTLE DISENGAGED AGAIN. ACFT GROUNDED. FAULT HISTORY SHOWED NR 2 AUTOTHROTTLE SERVO MOTOR FAILURE, FOR 7 LEGS. NO OTHER FNov 7, 2017 · N512AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2017102322297Wire Harness · damagedWHILE ACCOMPLISHING DVI OF WIRE HARNESSES FOR THE NR 2 ENGINE, FOUND FABRIC SHEATH OF J10 HARNESS TORN AND RUBBED AWAY NEAR CJ10 CONNECTION POINT. ACFT GROUNDED. PERFORMED ENGINE WIRING HARNESS REPAIR IAW AMM 70-70-01-350-801-F00.Oct 23, 2017 · N512AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2017102322293Terminal · damagedWHILE ACCOMPLISHING DVI FOR THE NR 2 ENGINE FIRE DETECTOR HARNESS MW0326, FOUND MW0326 TERMINAL LUGS DAMAGED. ACFT GROUNDED. INSTALLED NEW TERMINAL ENDS IAW AMM 26-11-02 P801. PERFORMED ENGINE FIRE DETECTION - OPERATIONAL TEST IAW AMM 26-11-00-701-801, TEOct 23, 2017 · N512AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2017101022156Indicator · failedCENTER TANK REFUELING CONTROL PANEL QUANTITY INDICATOR BLANK. ACFT GROUNDED. CHECKED VOLTAGE AT PIN 24, NO DEFECTS NOTED. REMOVED AND REPLACED CENTER REFUELING QUANTITY INDICATOR. OPS CHECKED GOOD IAW IAW AMM 28-41-61.Oct 10, 2017 · N512AS · Boeing 737890 · Fuel Quantity IndicatorSDR ASAA2017092622060Lens · detachedF/A REPORTED THE EXIT SIGN LENS CAME OFF. ACFT GROUNDED. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECKED GOOD IAW AMM 33-51-14.Sep 26, 2017 · N512AS · Boeing 737890 · Emergency LightingSDR ASAA2017092222023Fastener · brokenWHILE ACCOMPLISHING TC #78472022 NO 2 ENGINE, ACCOMPLISHED ENGINE FOD CHECK FOR ENGINE DRY PAD FOUND STARTER ASSY FASTENER BROKE OFF. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE STARTER IAW AMM 80-11-01-000-801-F00, & 80-11-01-400-801-F00. OPS AND LEASep 22, 2017 · N512AS · Boeing 737890 · Engine CrankingSDR ASAA2017092222016Panel · dentedWHILE ACCOMPLISHING TC PWRPL-72EO-08477-1 FOR THE NR 2 ENGINE, FOUND AT THE 3 O'CLOCK, FAN STRUT PANEL COVER DENTED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENGINE FAN DUCT PANEL IAW AMM 72-23-07-000-801-F00, AND AMM 72-23-07-400-801-F00.Sep 22, 2017 · N512AS · Boeing 737890 · Engine (Turbine/Turboprop)
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