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 ASAA2013062995357Autothrottle Sys · disconnectedON TAXI OUT AUTOTHROTTLE DISCONNECTED AND WOULD NOT RECONNECT. ACFT GROUNDED. ACCOMPLISHED FIMS 22-31T801 & 22-31T802 AND A/T SYS OPS REF MM 22-31-00. NO DEFECTS NOTED.Jun 29, 2013 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013062695342Indicator · inoperativeFUELER REPORT REFUEL CENTER QTY IND INOPERATIVE. ACFT GROUNDED. REPLACED CENTER REFUEL QTY IND IAW AMM 28-41-61/401. PART VERIFIED SEAMC PAT. REFUEL QTY IND OPS TEST NORMAL.Jun 26, 2013 · N518AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2013062295241Flight Dir · malfunctionedON TAXI OUT, LEFT NAV WOULD NOT ARM. ACFT GROUNDED. ACCOMPLISHED FLT FAULT REVIEW, GRP BITE 10, NO FAULTS LOGGED. ACCOMPLISHED FLT DIRECTOR TEST, GRP BITE 12, ALL TEST PASSED. ACCOMPLISHED LAND VERIFY TEST, GRP BITE 49, ALL TEST PASSED REF MM 22-00-01. ACFJun 22, 2013 · N518AS · Boeing 737890 · Autopilot SystemSDR ASAA2013052994932Unknown · unknownLIGHT ILLUMINATED ON ELECTRICAL PANEL AFTER GROUND POWER KICKED OFF. ACFT GROUNDED. ACCOMPLISHED FIM 24-31-801 ELEC LIGHT ILLUMINATED FAULT ISOLATION PROCEEDURE - SPCU FAULT DISPLAYED.ACCOMPLISHED FIM 24-34-802 , FAULT CLEARED WITH NO FURTHER DISCREPANCIES. May 29, 2013 · N518AS · Boeing 737890 · Central WarningSDR ASAA2013052594891Servo · failedAUTOTHROTTLE DISENGAGED ON CLIMB OUT WITH ACCOMPANING RED AUTOTHROTTLE LIGHT. QRH ACCOMPLISHED. AUTOTHROTTLE WOULD NOT STAY ENGAGED. ACFT GROUNDED. CONFIRMED FAULT, AUTOTHROTTLE BITE FAILS ASM NR 1. REPLACED NR 1 AUTOTHROTTLE ASM REF AMM TASK 22-31-91, OPS CMay 25, 2013 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013052594890Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. QRH PROCEDURE RUN, LIGHT WENT OUT.May 25, 2013 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013042494632Switch · inoperativeAUTO THROTTLE SWITCH WILL NOT ENGAGE. ACFT GROUNDED. PERFORMED AUTOTHROTTLE SERVO TEST NUMEROUS TIME IAW AMM REF 22-31-00-710-802, PASSES EVERY TIME. CURRENT STATUS SHOWS NO FAULTS. THE LEG SHOWING 75 FAULTS INDICATES ALL FAULTS WERE ON GROUND, PILOT DEFECApr 24, 2013 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013040194318Shim · wornNR 1 ENGINE FAN BLADE SHIMS WORN. ACFT GROUNDED. R & R TWENTY FOUR FAN BLADE SHIMS REF T/C 78472002.Apr 1, 2013 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2013032094217Pin · failedCREW REPORT EMERGENCY LIGHT LENS COVER AT L1 DOOR FELL OFF. FOUND PIN BAD ON LENS COVER REPLACED WITH SERVICABLE LENS COVER.Mar 20, 2013 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2013022794017Fmc · failedFMC NR2, INOPERATIVE FFR SHOWED NUMEROUS OCCURRENCES OF FMC DATA FAIL. ACFT GROUNDED. PERFORMED FMCS SYS BITE PROCEDURE REF FIM 34-61, TASK 801. INFLIGHT FAULTS SHOWED FMC FAULTS ONLY ON FLIGHT, LEG 5. PERFORMED FMCS OPS TEST REF MM34-61-00. TEST PASSED. Feb 27, 2013 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013021493917Shutoff Valve · inoperativeDURING CLIMBOUT DUCT PRESS LT 25, RT 45. AFTER LEVEL OFF LT DUCT PRESSURE STABILIZED TO 33 PSI. TOP OF DESCENT LT & RT DUCT EVEN AT 48. ACCOMPLISHED T/C NG-36WC-00001, BLEED SYS HEALTH CHECK. PRECOOLER VALVE FAILED, AND PRSOV FAILED TEST, NO OTHER DISCREPAFeb 14, 2013 · N518AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013020493823Actuator · malfunctionedLEFT PACK LIGHT ON RECALL. ACCOMP PACK/ZONE TEMP CONT BITE CK ON NR 1 CONTROLLER. RECORDED RAM AIR ACTUATOR FAULT AS AN ACTIVE FAULT REF MM 21-61-00. REPLACED LT RAM AIR ACTUATOR OPS NORMAL REF MM 21-51-21. RE-ACCOMP PACK/ZONE TEMP CONT BITE CK ON NR 1 CONTFeb 4, 2013 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013020293821Autothrottle Sys · inoperativeDURING T/O AUTOTHROTTLES DISENGAGED AND WOULD NOT STAY ENGAGED FOR MORE THAN 5 SEC QRH RUN. INFLIGHT FAULTS LOGGED ASM1 LEG 9, ACCOMPLISHED CURRENT STATUS TEST REF MM 22-31-00, TEST PASSED. SERVO MOTOR TEST PASSED REF SAME. NO HISTORY PAST 30 DAYS.Feb 2, 2013 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2013013193800Warning Light · false activationDURING CRUISE RT SIDE WINDOW HEAT OVERHEAT LIGHT LIGHT ILLUMINATED, PERFORMED QHR AND TURNED SWITCH OFF FOR 4 MINUTES. TURNED SWITCH ON , OVERHEAT LIGHT ILLUMINATED, TURNED SWITCH OFF. RESET C/B C 393 WINDOW HEAT POWER RT SIDE IAW MM 20-60-01, RT FLT DECK SLIJan 31, 2013 · N518AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2013012793766Door · faultedLEFT PACK LIGHT ILLUMINATED ON LANDING RECALL. ACCOMPLISHED TEMP CONTROLLER BITE REF FIM 21-62 TASK 801. FOUND RAM DOOR FAULT STORED IN MEMORY. PASSED VERIFY TEST & RESET FAULT. OPS NORMAL REF SAME.Jan 27, 2013 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013011493676Warning Light · false activationCONT CAB ZONE TEMP ILLUMINATES ON RECALL & EXTINGUISHED ON RESET. VERIFIED FAULT FOR CABIN RECALL. ACCOMPLISHED PACK/ ZONE TEMP CONT BITE NR 1 CONT NO FAULTS. NR 2 CONT FAULTED FLT DECK TRIM VALVE (V143). CLEARED FAULT, ACCOMPLISHED CABIN TEMP CONT & IND OJan 14, 2013 · N518AS · Boeing 737890 · Air Conditioning SystemSDR ASAA2013010593614Smoke Detector · failedCARGO FIRE/ SMOKE DETECT TEST FAILED. A LOOP FAILED. B LOOP TESTED GOOD. TESTED THE SYS FOUND AFT CARGO BAY A3 SMOKE DETECTOR INOPERATIVE. REPLACED A3 SMOKE DETECTOR, OPS CHECKED NORMAL, NO FAULT AT THIS TIME, REF MM 26-16-01.Jan 5, 2013 · N518AS · Boeing 737890 · Smoke DetectionSDR ASAA2013010293597Fire Loop · no testCARGO FIRE AFT LOOP A WILL NOT TEST. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, ACCOMPLISHED CARGO FIRE TEST REF MM 26-16-00, TEST PASSED. ACCOMPLISHED TEST SEVERAL TIMES. CEU DOES NOT LOG ANY DETECTOR FAULTS DURING TEST. NO HISTORY PAST 30 DAYS.Jan 2, 2013 · N518AS · Boeing 737890 · Smoke DetectionSDR ASAA2012123093584Panel · damagedNR 2 ENGINE, NR 1 FAN DUCT PANEL HAS CAPTIVE BOLT LOOSE AND PULLED THRU PANEL. REMOVED PANEL IAW AMM 72-23-07-000-801-F00. INSTALLED NEW PANEL IAW AMM 72-23-07-400-801-F00.Dec 30, 2012 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2012122693559Fire Loop · inoperativeAFT CARGO FIRE TEST LOOP A INOPERATIVE. REPLACED A1 SMOKE DETECTOR. OPS CHECKED GOOD. REF AMM 26-26-02.Dec 26, 2012 · N518AS · Boeing 737890 · Fire DetectionSDR ASAA2012121993503Control Valve · failedDURING CRUISE AT FL250, ENCOUNTERED ICING CONDITIONS. SELECTED WING AND ENGINE ANTI ICE ON. RT BLEED TRIP OFF LIGHT ILLUMINATED. USED QRH PROCEDURE, BLEED TRIP RESET, WITH WING ANTI ICE SWITCH OFF. ACCOMPLISHED T/C NG-36WC-00001 ENGINE BLEED AIR SYS HEALTDec 19, 2012 · N518AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2012120393402Smoke Detector · dirtyAFT CARGO FIRE DET LOOP A INOPERATIVE. CLEANED AFT PIT CARGO SMOKE DETECTORS IAW AMM 26-16-01. OPS NORMAL IAW AMM 26-16-00. GROUND VERIFICATION SUCCESSFUL.Dec 3, 2012 · N518AS · Boeing 737890 · Smoke DetectionSDR ASAA2012112693372Bulb · inoperativeFWD ENTRY EMERGENCY LIGHT INOP. COVER MISSING. ACFT GROUNDED. R & R BULB INSTALLED NEW COVER, OPS CHECK GOOD.Nov 26, 2012 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2012110293227Unknown · unknownLEFT FORWARD WINDSCREEN HEAT INOPERATIVE. CIRCUIT BREAKER TRIPPED. VISUAL INSPECTION OF WINDOW, & AT L1 CONTROLLER RACK, CHECKED GOOD. TRANSFORMER TAP TO WINDOW RES MATCH. L1 WINDOW HEAT POWER CIRCUIT BREAKER RESET NORMALLY & STAYS IN. OPS CHECKED SAME WNov 2, 2012 · N518AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012103193218Circuit Breaker · trippedRIGHT WINDOW HEAT, OVERHEAT LIGHT ILLUMINATED. QRH PROCEDURES COMPLIED WITH. FAULT CODE 30402042. FOUND RT SIDE WINDOW HEAT POWER CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER IAW AMM 20-60-01. WINDOW HEAT SYS OPS CHECKED GOOD IAW MM 30-41-00. GROUND VEROct 31, 2012 · N518AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2012100393010Indicator · trippedNR 1 IDG DPI IS POPPED SECOND NUISANCE FAULT. FMC CDU TC 78273000 C/W NO FAULTS FOUND. C/W FIM TASK 24-11-00-810-803, T/C 78424000 C/W RESET DPI RAN ENGINE OPS & LEAK CHECKED GOOD. REMOVED NR 2 ON DECAL COUNTER OK FOR SERVICE.Oct 3, 2012 · N518AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2012100293005Autothrottle Sys · inoperativeAUTO THROTTLE INOPERATIVE. COULD NOT DUPLICATE. AUTOTHROTTLE FAULT LOGGED RATE MONITOR FAULT NR 22-31687 LAST FLT. ACCOMPLISHED FIM 22-32/819, AUTO THROTTLE CURRENT STATUS CHECKED NORMAL. ALSO ACCOMPLISHED SEVERAL TIMES SERVO MOTOR TEST REF MM22-31-00 STEPOct 2, 2012 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012090992854Autothrottle Sys · malfunctionedAUTOTHROTTLES WILL NOT STAY ENGAGED. CONSTANTLY CLICKED OFF, T/O CLIMB & CRUISE. UNABLE TO DUPLICATE. AUTOTHROTTLES OPS TESTED GOOD REF MM 22-31-00. SERVO MOTOR TEST OPS NORMAL REF SYS TEST 22-31-00, STEP I. NO FAULTS.Sep 9, 2012 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012092092923Lens · missingEMERGENCY LIGHTING SYSTEM, LENS COVER AT OVERWING EXIT RT AFT MISSING. REPLACED EMERGENCY LIGHTING LENS COVER AR OVERWING EXIT RIGHT AFT REF AMM 33-51-01.Sep 2, 2012 · N518AS · Boeing 737890 · Emergency LightingSDR ASAA2012091392887Servo · failedAUTOTHROTTLE WILL NOT STAY ENGAGED. IT ENGAGES FOR 3-4 SECONDS, THEN DISENGAGES. NUMEROUS ASM NR 1 FAULTS LOGGED. SERVO MOTOR TEST FAILED NR 1, ASM MSG 22-31794. R & R NR 1 ASM REF MM 22-31-91, OPS CHECKED NORMAL. ACFT REMAINS CATIIIA AUTOLAND & HGS, VERIFSep 1, 2012 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012091092862Screw · looseNR 2 ENG FAN DUCT PANELS AT 500 AND 700 POSITIONS HAVE 1 EA LOOSE BOLT IAW PANEL. ACFT GROUNDED. SECURED LOOSE FASTENERS AS REQUIRED REF MM 72-23-07. NO DISCREPENCIES NOTED.Sep 1, 2012 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2012081892753Terminal · brokenNR 2 ENGINE FIRE LIGHT AND ENGINE OVERHEAT LIGHT FAILED TEST. PERFORMED BITE PROCEDURE ON ENGINE & APU FIRE DETECTION CONTROL MODULE.0 NR 2 LOOP B AMBER LIGHT DID NOT COME ON DURING BITE TEST, ALSO NOTE NO FAULTS LIGHTS DURING TEST. ACCOMPLISHED DVI OF NR Aug 1, 2012 · N518AS · Boeing 737890 · Fire Protection System WiringSDR ASAA2012073192640Warning Message · false activationON TAXIOUT OGG FMC DISAGREE LT ILLUMINATED. PERFORMED QRH AND ALL OPS NORMAL.Jul 3, 2012 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012072992629Idg · malfunctionedDURING WALKAROUND FOUND NR 2 IDG DRIVE NOT ILLUMINATED AT SHUTDOWN. ACCOMPLISHED GCU BITE CHECK REF MM 24-21-00 NO FAULTS FOUND. R & R NR 2 ENGINE IDG ASSY REF M/M 24-11-11-400-801. OPS AND LEAK CHECKED GOOD.Jul 2, 2012 · N518AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA12511676Servo · failedAUTOTHROTTLES WILL NOT STAY ENGAGED FOR MORE THAN 5 SECONDS AND THE THEY DISENGAGE. FOR THE 5 SECS THEY ARE ENGAGED THE THROTTLES ARE SPLIT. NO OTHER ABNORMALITIES WERE NOTED ON ANY FMC OR OTHER ACFT INSTRUMENTS. ALL CIRCUIT BREAKERS WERE CHECKED ALSO. ACFT Jun 10, 2012 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012062792435Warning Light · false activationON GROUND, FMC DISAGREE LIGHT. ACCOMPLISHED QRH PROCEDURE. NORMAL OPS.Jun 2, 2012 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511592Autothrottle Sys · failedAUTO THROTTLE FAILED DURING TAKEOFF. COULD NOT RE-ENGAGE. ACFT GROUNDED. NO HISTORY. NR 1 SERVO MOTOR FAILED TEST. PULLED AND RESET THE AUTOTHROTTLE DC CIRCUIT BREAKER. AUTOTHROTTLE SYS OPS CKS NORMAL IAW 22-31-00-710-801. AUTOTHROTTLE SERVO MOTOR TEST, May 26, 2012 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA12511419Autothrottle Sys · malfunctionedAUTO THROTTLE DOES NOT FUNCTION. AUTO THROTTLE WILL ENGAGE ON BUT WHEN AUTO THROTTLE MOVEMENT IS COMMANDED, IT APPEARS AS THOUGH THE RT THROTTLE MOVES AND THE LT THROTTLE DOES NOT, CAUSING THE AUTO THROTTLE SWITCH TO TRIP OFF AND DISENGAGE (NON ETOPS AIRSPACE)Apr 15, 2012 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA12511395Control Valve · malfunctionedLEFT PACK LIGHT ILLUMINATED ON RECALL EXTINGUISHED AFTER PUSHING MASTER CAUTION RESET. FOUND TCV FAULT IN NR 1 PACK/ZONE TEMP CONTROLLER. REMOVED & REPLACED LT TCV REF AMM 21 51 10. OPS & LEAK CHECKED GOOD.Apr 13, 2012 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511351Bypass Switch · failedNR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED DURING CLIMBOUT AND REMAINED ON. PERFORMED FIM TASK 73-05-00-810-801-F00 TO SLUPS 4 CONF FILTER BYPASS SWITCH DEFECTIVE. REPLACED FUEL FLTR NR 2 ENG PER AMM 73-11-02-400-801. NO DEBRIS. REPLACED SWITCH PER AMM 73-Apr 4, 2012 · N518AS · Boeing 737890 · Engine Fuel Indicating SystemSDR ASAA12511305Unknown · malfunctionedTHE AUTOTHROTTLE DISENGAGED IN FLIGHT AND WOULD NOT RE-ENGAGE. ACCOMPLISHED AUTOTHROTTLE BIT PER FIM TASK 22 31 00 810 801. LEG 03 LOGGED FOUR INSTANCES OF MSG 22 31687. ACCOMPLISHED FIM TASK 22 32 00 810 819 FOR MSG 22 31687 ASM 1. TORQUE AND SERVO MOTOR Mar 28, 2012 · N518AS · Boeing 737890 · Auto Throttle SystemSDR ASAA12511268Lug · brokenUPON PREFLIGHT FOUND FIRE DETECTION LOOP B INOP ON NR 2 ENGINE. DUPLICATED FAULT HARD FAIL NR 2 ENG B LOOP FIRE LOOP. M279 ENG/APU FIRE OVHT DET CONTROL MODULE BITE SHOWS OPEN CKT/BAD DETECTOR (3 RED LIGHTS). CHECKED ALL 4 DETECTORS RESISTANCES ALL CHECKED Mar 18, 2012 · N518AS · Boeing 737890 · Fire DetectionSDR ASAA12511267Screw · looseNR 1 ENG SEVERAL FASTENERS LOOSE ON FAN FRAME ACOUSTICAL PNLS LEFT SIDE. SECURED FASTENERS NR 1 ENG ON FAN FRAME ACOUSTICAL PNL LEFT SIDE REF AMM 72 23 07.Mar 16, 2012 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA12511259Fastener · looseNR 1 ENG FAN DUCT PNL LOOSE FASTENERS AT 7 O'CLOCK POSITION VEIW AFT LOOKING FWD. SECURED FASTENERS NR 1 ENG FAN DUCT PNL AT 7 O'CLOCK POS VEIW AFT LOOKING FWD REF AMM 72 23 07.Mar 16, 2012 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA12511257Fastener · looseNR 1 ENG INLET COWL HAS FASTENER LOOSE AT 6 O'CLOCK POSITION LOOKING INTO FAN. ON DEFERRAL.Mar 16, 2012 · N518AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA12511186Duct · damagedWHILE PERFORMING T/C N2471001 FOUND LOUVER MISSING ON RT COWL THERMAL ANTI ICE DUCT. ON DEFERRAL. REMOVED AND REPLACED COWL THERMAL ANTI ICE DUCT PER CMM 71 11 22.Mar 4, 2012 · N518AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA12511150Unknown · malfunctionedFMC DISAGREE ON GROUND. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.Feb 23, 2012 · N518AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511118Control Valve · malfunctionedCABIN ZONE LIGHT ILLUMINATED ON RECALL. EXTINGUISHES WHEN MASTER CAUTION PRESSED. REPLACED ZONE TRIM MODULATING VALVE (FLT DECK) REF AMM 21-61-21-400-801.Feb 16, 2012 · N518AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511095Engine · vibrationAT 15 000 FT 71% N ENG VIB INDICATES .4 ON NR 1 .2 ON NR 2. TACTILE VIBRATION FELT IN RUDDER PEDALS PILOT SEATS FLOOR AND THROTTLES. ENG NR 1 THROTTLE VIBRATES THE MOST. VIBRATION FELT FROM 71.7 TO 69.3 NI. WITH ENG NR 1 SET AT 73 PERECENT AND ENG NR 1 THROTFeb 12, 2012 · N518AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA12511078Warning System · false activationCONTROL CABIN ZONE TEMP ILLUMINATED ON MASTER CAUTION RECALL. EXTINGUISHES WHEN RESET. PERFORMED PACK/ZONE TEMP CONTROLLED BIT TEST & OPS CHECK GOOD IAW B737NG AMM 21 51 00 700 803. RAN ENGINES AND OPERATED PACKS SHUT DOWN ENGINES AND PERFORMED PACK/ZONE TEFeb 11, 2012 · N518AS · Boeing 737890 · Cabin Temperature Control System
Back to N518AS