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 ASAA2015122414458Valve · failedAFTER LANDING ENGINE TAI SELECTED OFF NR 2 ENGINE TAI REMAINED ON WITH BRIGHT BLUE COWL VALVE OPEN LIGHT AND TAI ANNUNCIATED ON ENGINE INSTRUMENTS. AFTER ENGINE SHUT DOWN COWL LIGHT WENT OUT. ACFT GROUNDED. REPLACED NR 2 ENGINE COWL THERMAL A/I CONTROL VALVEDec 24, 2015 · N518AS · Boeing 737890 · Engine Anti-Icing SystemSDR ASAA2015121114213Battery Pack · failedEMERGENCY LIGHTING SWITCH, OPS CHECK AND BATTERY PACKS, FUNCTIONAL CHECK, BATTERY PACKS AT M1673 AND M1675 FAILED CAPACITY CHECK. ACFT GROUNDED. REPLACED BATTERY PACKS AT M1673 AND M1675. INSTALLATION TEST PASSES. REF AMM 33-51-06/201.Dec 11, 2015 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2015110913713Warning Light · false activationELECTRONIC CAUTION LIGHT ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. PERFORMED FIM TASK 24-31-801, SPCU INOPERATIVE "I" INDICATED, FAULT RESET, ELECTRONIC LIGHT EXTINGUISHED INTERMITTENT FAULT. ACFT OK FOR SERVICE.Nov 9, 2015 · N518AS · Boeing 737890 · Central WarningSDR ASAA2015110313617Control Valve · failedLEFT PACK LIGHT ILLUMINATES AFTER MASTER CAUTION RECALL. EXTINGUSHES WITH MASTER CAUTION RESET, ACFT GROUNDED. BITE CHECK OF NR 1 PACK/ZONE TEMP CONTROLLER, M 1442, FAULTS TCV THIS PACK. REPLACED LT PACK TCV, V 139. INSTALLATION TEST PASSES. NO LEAKS NOTED,Nov 3, 2015 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015101013421Computer · malfunctionedWHEN LOWER CRUISE ALTITUDE IS SET IN ALTITUDE ALERTER WHILE ON VNAV & ALTITUDE INTERVENTION BUTTON PRESSED, NEW MCP ALTITUDE DOES NOT DISPLAY IN FMC CRUISE PAGE AND FMA ANNUNCIATION ON LEVEL OFF AT NEW CRUISE ALTITUDE CHANGES TO ALT HOLD. ACFT GROUNDED. DFCSOct 10, 2015 · N518AS · Boeing 737890 · Autopilot SystemSDR ASAA2015092713233Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. QRH PROCEDURE FOLLOWED FOR RESET. SYSTEM SUCCESFULLY RESET.Sep 27, 2015 · N518AS · Boeing 737890 · Communications SystemSDR ASAA2015090712970Lens · missingROW 16ABC, EMERGENCY EXIT LIGHT LENS MISSING. ACFT GROUNDED. INSTALLED NEW LENS COVER.Sep 7, 2015 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2015090412913Valve · unknownTECH SERVICES REQUESTS FOLLOW-UP TO NR 2 ENGINE IDG FREQUENT SERVICING. ACFT GROUNDED. PERFORMED STATIC LEAK CHECK ON NR 2 IDG NO LEAKS AMM REF 24-11-00-700-801. R & R IDG VENT VALVE AND IDG SERVICE FITTING ON NR 2 IDG AMM REF 24-11-00-700-804, NO LEAKS NOTESep 4, 2015 · N518AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2015090212912Control Valve · faultedLEFT PACK LIGHT ILLUMINATED AFTER TAKEOFF. AFTER RESET, IT EXTINGUISHED. UPON RECALL IT ILLUMINATES, BUT CLEARS ON RESET. ACFT GROUNDED. ACCOMPLISHED CABIN TEMP CONTROLLER BITE. FOUND LT PACK TCV VALVE FAULT. RESET, OPS CHECK NORMAL. NO HISTORY, REF FIM TSep 2, 2015 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015080112668Fastener · looseNR 1 ENGINE AFT ACCOUSTICAL PANELS AT 4-6 O`CLOCK, FASTENERS ARE LOOSE AND WORN 6 TOTAL. ACFT GROUNDED. REPLACED THE FASTENERS IAW AMM 72-23-02-400-801-F00.Aug 1, 2015 · N518AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2015062512289Strip · corrodedAFT CARGO COMPARTMENT, RT NR 5 CAP STRIP HAS SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL THICKNESS IS 0.063", REMAINING THICKNESS IS 0.050", REMOVED 0.013". REPLACED CAPSTRIP Jun 25, 2015 · N518AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015062012360Channel · corrodedAFT CARGO BAY TRANSITION PANEL BS 727F - 767 LT SIDE HAS NUMEROUS AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-00-53-01, ORIGINAL MATERIAL THICKNESS .040 IAW SRM 53-00-53 AND DWG 1496-377 MATERIAL REMOVED .003, MAT REMAINING AFTER BLENDOUT .Jun 20, 2015 · N518AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015062012157Channel · corrodedAFT CARGO BAY TRANSITION PANEL BS 727F-767, LT SIDE HAS NUMEROUS AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-00-53-01, SRM 53-00-53 AND DWG 1496-377. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53.Jun 20, 2015 · N518AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015062012282Channel · corrodedAFT PIT, TRANSITION PANEL FROM FWD BULKHEAD TO BS 727D RT SIDE HAS NUMEROUS AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-00-53 FROM BS 727+4 TO 727C+8 AND 727C+13 TO 727D FOUND TO BE WITHIN LIMITS ORIG THICKNESS .040 REMOVED .002 REMAINIJun 20, 2015 · N518AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015062012180Floorbeam · corrodedAFT CARGO BAY FLOORBOARD ATTACH STRAP IS CORRODED AT BS 767. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. ORIGINAL THICKNESS IS .070", REMAINING THICKNESS IS 0.037", REMOVED 0.033". R & R STRAP IAW SRM 51-40-02 AJun 20, 2015 · N518AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015061912176Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED BS 540, BL 0, LBL 5. ACFT GROUNDED. REMOVED THE CRACKED FLOORBEAM IAW SRM 51-40-02, PARA NR 7. DRILLED TO FIT THE NEW FLOORBEAM IAW SRM 51-40-05. INSTALLED THE NEW FLOORBEAM IAW SRM 51-40-02, PARA NR 7.Jun 19, 2015 · N518AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015061912175Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED BS 540, BL 0 - RBL 5. ACFT GROUNDED. REMOVED THE CRACKED FLOORBEAM IAW SRM 51-40-02, PARA NR 7. DRILLED TO FIT NEW FLOORBEAM IAW SRM 51-40-05. INSTALLED THE NEW FLOORBEAM IAW SRM 51-40-02, PARA NR 7.Jun 19, 2015 · N518AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015061712281Floor Panel · gougedFWD CARGO COMPARTMENT, FLOOR PANEL 120CF IS GOUGED, ACFT GROUNDED. FABRICATED NEW FLOOR PANEL 120CF IAW DWG 453A0610, TREATED IAW SRM 51-20-01. ALODINED AND PRIMED.Jun 17, 2015 · N518AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2015061512099Indicator · inoperativeNR 1 REFUEL GAUGE INOPERATIVE. ACFT GROUNDED.Jun 15, 2015 · N518AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2015061012060Warning Message · false activationFMC DISAGREE ON TAXI OUT. ACFT GROUNDED. RESOLVED IAW QRH.Jun 10, 2015 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015060611993Window · failedON FINAL THE RT SIDE WINDOW HEAT OVERHEAT ILLUMINATED. COMPLETED THE QRH CHECKLIST AND OVERHEAT LIGHT EXTINGUISHED. LINE MAINTENANCE ADVISED. ACFT GROUNDED. BITE TESTED RT SIDE WHCU REF FIM 30-41, TASK 801. TEST OK. LAST FLIGHT LEG HAS FAULT FOR SENSOR. Jun 6, 2015 · N518AS · Boeing 737890 · Flight Compartment WindowsSDR ASAA2015060411996Keyboard · wornF/O MCDU, CONTROL DISPLAY UNIT, BUTTON 6L COMING OFF. ACFT GROUNDED. REPLACED F/O MCDU KEYPAD. INSTALLATION TEST PASSES. REF AMM 34-61-01-400-801.Jun 4, 2015 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015060411991Sensor · failedWINDOW HEAT, RIGHT SIDE OVERHEAT LIGHT ON. ACFT GROUNDED. RIGHT SIDE WINDOW PRIMARY SENSOR OPEN. MOVED "D" TERMINAL TO SPARE TERMINAL. WHCU UNIT BITE VERIFY CHECK PASSES. REF FIM 30-41, TASK 811.Jun 4, 2015 · N518AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2015052111827Control Unit · failedRT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED AT 15,000 FT. SWITCH TURNED OFF BY DIRECTION OF QRH. SWITCH TURNED BACK TO ON. WINDOW HEAT THEN FUNCTIONED NORMALLY. ACFT GROUNDED. REF AMM 30-41, TASK 801, PERFORMED BITE CHECK ON WINDOW HEAT SYS NO FAULTS FOMay 21, 2015 · N518AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2015051411744Warning Light · false activationRIGHT SIDE WINDOW HEAT OVERHEAT. ACFT GROUNDED. PERFORMED AMM TASK 30-41, TASK 801. OPS NORMAL. NO HISTORY IN 30 DAYS. NO FAULT NOTED.May 14, 2015 · N518AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2015051011678Satcom · lockedSATCOM LOCKUP DURING PREFLIGHT. ACFT GROUNDED. RESET SATCOM IAW QRH PROCEDURE OPS NORMAL.May 10, 2015 · N518AS · Boeing 737890 · Communications SystemSDR ASAA2015050211591Autothrottle Sys · malfunctionedAUTOTHROTTLE INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED AT BITE, NO FAULTS REF AMM 22-31-00-710-801 AND DFCS BITE LRU REPLACEMENT TEST, NO FAULTS REF AMM 22-00-01-730-801. NO HISTORY.May 2, 2015 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2015042811573Stator Vane · leakingFUEL DRIP ON NR 2 ENGINE. ACFT GROUNDED. ACCOMPLISHED VENT AND DRAIN INSP REF AMM 71-71-00-200-801. IDENTIFIED LEAK FROM NR 2 ENG LEFT VSV AT 4 DROPS PER MINUTE. LESS THAN THRESHOLD LIMIT OF 60 DROPS IAW MINUTE. PLACED ON 75 CYCLES PLT, FOR COMPONENT TO BEApr 28, 2015 · N518AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2015042511516Actuator · malfunctionedPACK LT OBSERVED ON DURING CLIMBOUT, =18,000, RAN QRH. WARMED TEMP, TRIP RESET, PACK LIGHT CLEARED ON MASTER CAUTION RESET. ACFT GROUNDED. WHILE ON DEFERRAL, AT CRUISE, RT PACK LIGHT ILLUMINATED. FOLLOWED CHECKLIST. LIGHT EXTINGUISHED WHEN MASTER CAUTION SApr 25, 2015 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015042311476Warning Light · false activationON RECALL RT PACK LIGHT ILLUMINATED. PERFORMED QRH PROCEDURES PRESSING MASTER CAUTION - PUSH IT RESET LIGHT WENT OUT. GROUNDED - YES. OPERATED RT. PACK PER FIM TASK 21-53 TASK 804, PACK LIGHT DID NOT ILLUMINATE AGAIN. OK FOR SERVICE.Apr 23, 2015 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015032911161Warning Message · false activationFMC DISAGREE ON GROUND, ACFT GROUNDED. QRH CORRECTED THE ANOMALY.Mar 29, 2015 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015032811136Satcom · lockedSAT/COM LOCK UP. ACFT GROUNDED. ACCOMPLISHED QRH. OPS NORMAL.Mar 28, 2015 · N518AS · Boeing 737890 · Communications SystemSDR ASAA2015031710989Warning Message · false activation"FMC" DISAGREE", ACFT GROUNDED. ACCOMPLISHED "FMC" DISAGREE" QRH PROCEDURE.Mar 17, 2015 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015030910900Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. RESET IAW QRH.Mar 9, 2015 · N518AS · Boeing 737890 · Communications SystemSDR ASAA2015030910899Unknown · unknownDC 1 AUTOTHROTTLE CB OUT. ACFT GROUNDED. RESET C/B, A/T CURRENT STATUS BITE TEST, NO FAULTS. DFCS LRU REPLACEMENT TEST FOR A/T, BITE GROUP NR 43, REF FIM 22-11, TASK 802 - PASS.Mar 9, 2015 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2015030910897Valve · malfunctionedCONTROLLER CABIN ZONE TEMP LIGHT ILLUMINATED UPON RECALL, EXTINGUISHES UPON MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED TEMP CONTROLLER BITE, NR 1 AND NR 2 TEMP CONTROLLERS BOTH SHOW FLT DECK TRIM VALVE FAULTS ON BITE AND PREVIOUS FLTS. REPLACED CONTROLLMar 9, 2015 · N518AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015030810892Unknown · unknownEEC-ON -OTA 15'C-WIND CALM ENG ANTI-ICE-OFF-30.08 WING ANTI-ICE-OFF REDUCE POWER TAKEOFF 8 FMC COMPUTED DIFFERENT N1 TARGET VALUES OF 0.7 ENG 1 89.8 ENG NR 2, 89.1. ACFT GROUNDED. PREFORMED FIM TASK 34-61-839, AND SUB TASK MM 34-61-00-730-001. NO DEFECTS FOUMar 8, 2015 · N518AS · Boeing 737890 · Standard Practices/StructuresSDR ASAA2015022410767Unknown · unknownON GROUND, AFTER PUSHBACK GOT FMC DISAGREE ALERT. ACFT GROUNDED. FOLLOWED QRH PROCEDURES ALERT DISAPPEARED.Feb 24, 2015 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015022010710Warning Light · false activationUPON PUSH BACK STARTUP IN MCO MASTER CAUTION RECALL TEST REVEALED ZONE TEMP LIGHT ILLUMINATED EXTINGUISHED WHEN MASTER CAUTION RESET BUTTON PRESSED. ACFT GROUNDED. PERFORMED BITE CK OF NR 2 TEMP CONTROLLER. FOUND INTERMITTENT FAULT.Feb 20, 2015 · N518AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015020710571Warning Message · false activationDURING TAXI FMC DISAGREE ANNUNCIATED. ACFT GROUNDED. FOLLOWED QRH- SUCCESSFULLY RESET.Feb 7, 2015 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015012810463Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. QRH PROCEDURE FOLLOWED. SATCOM RESTORED.Jan 28, 2015 · N518AS · Boeing 737890 · Communications SystemSDR ASAA2015012410396Fmc · malfunctionedRT FMC FAILED. ACFT GROUNDED. PERFORMED FIM TASK 34-61-801, FMC GROUND VERIFICATION. TEST PASSED. NO FAULTS FOUND. NO FURTHER MAINTENANCE ACTION REQUIRED.Jan 24, 2015 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014122410054Warning Message · false activationAFTER PUSH BACK RECEIVED "FMC DISAGREE" MESSAGE, ACFT GROUNDED. PERFORMED QRH FMC RESET PROCEDURE, OPS NORMAL. VERIFIED FMC OPS NORMAL, IAW MM 34-61-01-800-801.Dec 24, 2014 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014121709994Valve · failedAFTER ENGINE START, PLACED BOTH ENGINE ANTI-ICE SWITCHES ON , THE ENGINE NR 2 COWL VALVE OPEN LIGHT REMAINED BRIGHT. CLOSED APU BLEED AIR SWITCH OFF & INCREASED THRUST TO 40 PERCENT N1 ON NR 2 ENGINE. COWL VALVE OPEN LIGHT REMAINED ILLUMINATED BRIGHT BLUE ADec 17, 2014 · N518AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2014120509877Acoustic Liner · wornNR 1 ENGINE, FOUND AT FIVE O-CLOCK ACOUSTICAL PANEL FWD CTR FASTENER WASHER MISSING & PULL THRU DAMAGE IN PANEL. ACFT GROUNDED. REPLACED NR 1 ENG 5' O CLOCK ACOUSTICAL PANEL WITH NEW REF: AMM 72-23-02.Dec 5, 2014 · N518AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2014111609685Warning Message · false activationNR 2 ENGINE, PERFORMED TC 78273000, HAD FAULT CODE 77-20872 - ECONOMIC FAULT, "THE TOP LEFT EGT SIGNAL IS OUT OF RANGE". ACFT GROUNDED. PERFORMED TC 78273000 NO FAULTS FOUND.Nov 16, 2014 · N518AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2014100409301Warning Light · activatedNR 2 START VALVE OPEN LIGHT REMAINED ILLUMINATED AFTER ENGINE START. ACFT GROUNDED. PERFORMED ENGINE NORMAL START PROCEDURE IAW 71-00-00. ALL OPS NORMAL, ACFT OK FOR SERVICE, IAW ENGINEERING REQUEST, REPLACED NR 2 START VALVE IAW AMM 80-11-03-000-801-F00. OOct 4, 2014 · N518AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2014091609139Circuit Breaker · broken"WINDOW HEAT LT SIDE ACFT" BREAKER APPEARS TO BE BROKEN- NOT POPPED, JUST BROKEN. ACFT GROUNDED. REPLACED CB C225, REF WDM 30-41-12, PG 2.1, SHEET 2 AND SWPM 20-30-00, TABLE 10. WINDOW HEAT OPS TEST GOOD IAW MM 30-41-00.Sep 16, 2014 · N518AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2014090709072Wire · misinstalledNR 2 ENGINE FIRE HANDLE DOES NOT ILLUMINATE DURING TEST IN NORMAL, BUT LIGHTS WHEN SELECTED TO A. ACFT GROUNDED. OPENED NR 2 ENGINE FAN AND DUCT COWLING. INSPECTED ALL B LOOP FIRE DETECTORS AND FOUND DETECTOR MW0326 AT LT SIDE ENGINE CORE WITH AN IMPROPER CSep 7, 2014 · N518AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2014090109028Satcom · lockedSATCOM LOCKED UP ON GROUND, ACFT GROUNDED. SATCOM CHECKLIST ACCOMPLISHED, NORMAL OPS RESTORED.Sep 1, 2014 · N518AS · Boeing 737890 · Communications System
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