N516AS
Service difficulty reports · 400
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 = 'N516AS' 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.
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 = 'N516AS' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2019030128433Power Supply · inoperativeR2 DOOR SLIDE EMERGENCY LIGHT INOP. GROUNDED - YES. CONFIRMED FAULT, TROUBLESHOT TO DEFECTIVE EMERGENCY LIGHT BALLAST LOCATED NEXT TO FDR. REMOVED BALLAST ASSY REF AMM 33-51-06, NIS @ LAX. REMOVED & REPLACED BATTERY PACK PER AMM 33-51-06, OPS TESTED AND FOUND SDR ASAA2019021728211Wire · chafedFLIGHT ATTENDANTS REPORT NONE OF THE TOILETS WILL FLUSH. ATTEMPTED MULTIPLE TIMES. GROUNDED - YES. DIVERSION TIME 62 MINUTES. FOUND WIRE W5230-0514-18 BURNT IN TWO DUE TO CHAFFING AGAINST METAL FRAME. THE BURN SPOT WAS CLOSE TO D40152 J/P WHICH IS JUST FORWARDSDR ASAA2019020628109Indication Sys · malfunctionedNR 2 AFT FUEL PUMP LOW PRESSURE LIGHT REMAINS OFF WHEN PUMP SWITCH OFF. GROUNDED - YES. PERFORMED OPS CHECK OF NO2 FUEL BOOST PUMP LOW PRESSURE LIGHT AFT POSITION AMM 28-42-11-700-024.SDR ASAA2019020528051Control Panel · intermittentFLIGHT DIRECTOR "MASTER" ILLUMINATED ON BOTH SIDES WITH NO CORRESPONDING AUTOPILOT ON. (ONLY ONE MASTER SHOULD BE ILLUMINATED) FLIGHT DIRECTOR DOES NOT CORRESPOND TO RAW DATA. GROUNDED - YES. PERFORMED MCP TESTS PER FIM 22-11 TASK 803. ALL TESTS PASSED. DUE TOSDR ASAA2019020328155Warning System · false activationDURING CRUISE "CONT CABIN" AMBER LIGHT ILLUMINATED BRIEFLY DOES NOT ILLUMINATE ON RECALL. RAN QRC FOR ZONE TEMP. LIGHT WENT OUT BEFORE CHECKLIST COMPLETED LOWERED THE TEMP IN CONT CAB PER QRC LIGHT STAYED OUT. GROUNDED - YES. PERFORMED MASTER CAUTION RECALL NOSDR ASAA2019020328014Filter · dirtyDURING CRUISE, CONT CAB ZONE TEMP ILLUMINATED. LIGHT RESET WITH MASTER CAUTION. GROUNDED - YES. PERFORMED BITE OF BOTH PACK TEMP CONTROLLERS PER FIM 21-62 TASK 801 AND NO FAULTS FOUND. REMOVED 3 EA CABIN TEMP SENSOR FILTERS PER AMM 21-61-06. FOUND FILTHY. PERFSDR ASAA2019020228033Warning System · false activation"FD" AMBER CAUTION ON CAPT PFD. GROUNDED - YES. PERFORMED BITE TEST PER B737-800 FIM 22-11 TASK 801, NO FAULTS NOTED. REBOOTED A/C POWER, FLAG EXTINGUISHED UPON RESET.SDR ASAA201902048013Warning Light · false activationTHE "CONT CAB" ZONE TEMP AMBER CAUTION LIGHT ILLUMINATED PERIODICALLY THROUGHOUT DURATION OF FLIGHT. DOES NOT ILLUMINATE ON RECALL. GROUNDED - YES. CYCLED C/B'S AS LISTED IN B737-800 FIM 21-61 TASK 861. PERFORMED BITE CHECK OF CONTROL TEMP CONTROL SYSTEM, WITHSDR ASAA2019013027985Frame · crackedNR 1 ENG REAR TURBINE FRAME FLANGE ASSY IS CRACKED AT APPROX 4 HOLES ON THE INTERMEDIATE FLANGE BOLT CIRCLE. GROUNDED - YES. REPLACED NR 1 ENG. FLANGE ASSY PER AMM 72-56-00-400 STEP 3 F (2) & (3). PLUG ASSY REMOVED FOR ACCESS, REINSTALLED PER MM 78-11-02-400.SDR ASAA2019012927971Switch · excess playSUPPLY DUCT AIR TEMP SELECTOR SWITCH HAS EXCESSIVE PLAY IN IT, FEELS LIKE IT IS CLOSE TO BREAKING. GROUNDED - YES. REPLACED CABIN TEMPERATURE SELECTOR PANEL REF AMM 21-61-07-000-803-802. OPS CHECK NORMAL.SDR ASAA2019012027875Oil Filter · leakingON PUSH RAMP PERSONNEL NOTIFIED PILOT OF OIL DRIPPING FROM APU. GROUNDED - YES. INSPECTED APU, FOUND APU LUBE FILTER HOUSING LEAKING. CLEANED AND RETORQUE APU OIL FILTER, RAN APU VERIFIED NO LEAKS-CHECKED APU OIL QTY. FOUND TO BE FULL REF AMM 49-91-12-4000-802SDR ASAA2019011527874Oil System · lowUPON LANDING IN HNL AND AFTER ONE START ATTEMPT ON THE APU THE APU "LOW OIL PRESSURE" LIGHT ILLUMINATED AND DID NOT EXTINGUISH. NO FURTHER START ATTEMPTS WERE CONDUCTED. GROUNDED - YES. REF AMM 12-13-31 VERIFIED APU OIL LEVEL USING SIGHT GLASS PROCEDURE, ADDEDSDR ASAA2018122177499Battery Pack · inoperativeOVER WING FWD EMERGENCY EXIT LIGHTS INOP LH & RH SIDE. GROUNDED - YES. OVERWING FWD EMERGENCY LIGHTS, OPS CHECK GOOD. M1694 BATTERY PACK REPLACED IAW B737-800 AMM 33-51-06-960-806. M1670 BATTERY PACK REPLACED IAW AMM 33-51-06-960-806. OPS CHECK GOOD.SDR ASAA2018120527391Pressure Deck · crackedRIGHT WING REAR SPAR VERTICAL PRESSURE DECK WEB IS CRACKED AT STA 663.75 APPROX RBL 35. GROUNDED - YES. CUT OUT DAMAGE IN WEB AND REPAIRED IAW SRM 57-10-10-2R-3 REPAIR 3.SDR ASAA2018120327338Plate · crackedPANEL BRAKE LOWER SURFACE HAS A CRACKED END AT STA 540 RBL 0. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK AND PLATE IAW BAC DWG 143A5240.SDR ASAA2018120327220Angle · crackedMAIN CABIN STA 540 LBL 0 TO LBL 24 PANEL BREAK ANGLES CRACKED. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK ASSY IAW BAC DWG 143A5240 AND BAC DWG 143A0060 REV-.SDR ASAA2018113027197Intercostal · crackedFWD WET AREA INTERCOSTAL IS CRACKED AT STA 312-328 LBL49. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL REF BAC DWG 141A5400 REV-.SDR ASAA2018121197282Channel · corrodedAFT PIT R/H ZEE CHANNEL SEVERAL SPOTS OF CORROSION BETWEEN BS727H - BS727J. GROUNDED - YES. BLENDED CORROSION ON AFT PIT R/H ZEE CHANNEL BETWEEN BS727H-727J ORG MAT .040, REMOVED .040, .000 REMAINS FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-00-53 ACCOMPLISHSDR ASAA2018121197281Channel · corrodedAFT PIT R/H ZEE CHANNEL SEVERAL SPOTS OF CORROSION BETWEEN BS727F - BS727H. GROUNDED - YES. BLENDED CORROSION FROM AFT PIT R/H ZEE CHANNEL B5727F-727H ORG MAT .040 REMOVED .040, .000 REMAINS, FOUND TO BE OUT OF LIMITS PER B737-800 SRM 53-00-53 ACCOMPLISHED SRMSDR ASAA2018121197278Channel · corrodedAFT PIT R/H ZEE CHANNEL SEVERAL SPOTS OF CORROSION BETWEEN BS727C - BS727D. GROUNDED - YES. BLENDED CORROSION FROM AFT PIT L/H ZEE CHANNEL BETWEEN BS727C-727D, ORG MAT .040, REMOVED .001, .039 REMAINS. FOUND TO BE IN LIMITS PER B737-800 SRM 51-00-53. ALODINED SDR ASAA2018121197275Web · corrodedAFT CARGO COMPARTMENT SCUFF PLATE THRESHOLD WEB CORRODED. GROUNDED - YES. REMOVE CORROSION ON AFT CARGO COMPARTMENT SCUFF PLATE THRESHOLD WEB AND WAS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15. REMOVED DAMAGED WEB IAW B737-800 SRM 51-40-02. LOCATED, DSDR ASAA2018101926525Unknown · odorFLIGHT ATTENDANTS REPORT BURNING RUBBER SMELL DURING TAKEOFF AND CLIMB IN ROW 26. THE SMELL DISSIPATED IN CRUISE. GROUNDED - YES. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING REF FIM TASK 05-51 TASK 814 RAN APU BOTH ENGS AND PACKS NO DISCREPANCIES NOTED. NO HISTORYSDR ASAA2018082525916Anti-Ice Valve · failedAMBER TAI INDICATION AND BRIGHT BLUE COWL VALVE OPEN LIGHT WITH SWITCH IN ON POSITION. ACFT GROUNDED. REMOVED AND REPLACED NR 1 ANTI-ICE VALVE IAW AMM 30-21-11. OPS CHECKED NORMAL.SDR ASAA201808205818Blade · failedNR 2 ENGINE CONTINUES TO HAVE GREATER THAN EXPECTED VIBRATION LEVELS AFTER LAST FAN LUBE AND ON BOARD FAN TRIM BALANCE. ACFT GROUNDED. ACCOMPLISHED STEP 1 OF TSR. REPLACED 1 PLATFORM. PERFORMED NR 2 ENGINE VIBRATION SURVEY TEST 7 & ON-BOARD FAN TRIM BALANCESDR ASAA2018073125585Warning System · false activationAUTO FAIL LIGHT ILLUMINATED ON PRESSURIZATION CONTROL PANEL. ALTN GREEN LIGHT ILLUMINATED. GROUNDED - YES. RECYCLED SWITCH TO MANUAL AND BACK TO AUTO. GOOD FOR SERVICE.SDR ASAA2018072325485Circuit Breaker · trippedAFTER LEVEL OFF FA REPORTS ALL LAVS WILL NOT FLUSH. GROUNDED - YES. DIVERSION TIME 63 MINUTES - FOUND VAC WASTE CNTRL C/B ON P91 PNL OPEN, RESET C/B AS PER AMM 20-60-01. ACCOMPLISHED OPS CHK OF ALL LAVS OPS CHK GOOD OK FOR SERVICE REF FIM 38-30 TASK 811.SDR ASAA2018070925337Wire Harness · corrodedFOUND FAULT CODE 73-31071, FUEL FILTER SIGNALS DISAGREE, LONG TIME FAULT ON NR 1 ENG. GROUNDED - YES. CW EEC BITE NR 1 ENG SHOWS NO FAULTS. REMOVED AND REPLACED J8 HARNESS REF AMM 73-21-06 DUE TO CORROSION. OP CK GOOD.SDR ASAA2018070925327Blade · wornNR 2 ENG, NR 13 FAN BLADE HAS CU-NI-IN MISSING BEYOND LIMITS. GROUNDED - YES. ON NR 2 ENG REMOVED AND REPLACED NR 13 FAN BLADE IAW MX T/C 78472002.SDR ASAA2018070925326Blade · damagedNR 2 ENG, NR 1, 6, 8 FAN BLADE PLATFORMS HAS DAMAGE. GROUNDED - YES. ON NR 2 ENG REMOVED AND REPLACED NR 1, 6, 8 FAN BLADE PLATFORMS IAW MX T/C 78472002.SDR ASAA2018070225267Blade · crackedPER TSR 701960 STEP 2 NGV INSPECTION AT 1 O'CLOCK POSITION FOUND AXIAL CRACK LE TO TE 1 AIRFOIL AT NR 1 ENGINE. GROUNDED - YES. ON DEFERRAL.SDR ASAA2018070125325Valve · leakingWHILE PERFORMING TSR701958 FOUND NR 1 ENG EGT EXCEEDANCE. GROUNDED - YES. ACCOMPLISHED EEC TEST REF FIM 71-06-805 NO FAULTS FOUND PERFORMED STEP 2. ACCOMPLISHED NR 1 ENGINE HPT BLADES BORESCOPE INSPECTION REF AMM 72-00-00-200-807-F00 NO DAMAGE NOTED. ACCOMPLISSDR ASAA2018062525195Seal · damagedWHILE ACCOMPLISHING TASKCARD 78472000, FOUND OUTLET GUIDE VANE AT AROUND THE 4 O CLOCK POSITION ( FORWARD LOOKING AFT) WITH A DAMAGED BASE SEAL. GROUNDED - YES. REMOVED AND REPLACED OUTLET GUIDE VANE SEAL AT AROUND THE 4 O CLOCK POSITION REF AMM 72-23-01.SDR ASAA2018062525193Blade · wornENG NR 1 FAN BLADE 1, 5, 6, 7, 8, 11, 20 HAS FAN BLADE ROOT CU-NI-IN COATING OUT OF LIMITS. NO BASE METAL WEAR NOTED. GROUNDED - YES. REPLACED 1, 5, 6, 7, 8, 11, AND 20 BLADES. REF TC 78472002. SEE TC 78472002, FIGURE 400 TABLE 2 FOR NEW BLADE P/N, S/N AND PLASDR ASAA2018061325045Probe · defectiveNR 1 ENGINE TREND DATA SHOWS AN INCREASE IN DELTA EGT AND DECREASE IN EGT HOT DAY. FUEL FLOW AND CORE SPEED REMAIN STABLE. GROUNDED - YES. PRIOR TO RUNNING THE NR 1 ENGINE, TOOK A LOOK AT THE EGT PROBE READINGS AND OBSERVED THE S4 ALTERNATING FROM DASHES TO RESDR ASAA2018060624887Valve · failedON RECALL, THE CONTROL CABIN ZONE TEMP ILLUMINATED, EXTINGUISHED ON RESET. ACFT GROUNDED. REMOVED & REPLACED THE ZONE TRIM MODULATION VALVE IAW AMM 21-61-21-000/400. CHECKED GOOD IAW AMM 21-51-00-700-803, PACK ZONE TEMP CONTROLLER BITE TEST. OPS NORMAL.SDR ASAA2018053024903Probe · defectiveWHILE ACCOMPLISHING T/C 78273000, FOUND ECONOMIC FAULT MSG 77-20871 THE TOP LET EGT SIGNAL (T495S4) IS OUT OF RANGE ON NR 1 ENG. GROUNDED - YES. DEFERRED MAINTENANCE FOR 500 FLT HRS PER T/C 78273000. REF FIM 77-21 TASK 804, INITIAL EVALUATION COMPLETED STEPS 1SDR ASAA2018051324619Warning System · false activationCA FLT DIR FLAG CAME ON, 10 MIN PRIOR TO DEPARTURE. GROUNDED - YES. CYCLED A/C POWER REF AMM 22-60-99 CAP T/O RETURN TO NORMAL ACCOMPLISHED DFGS F/D TEST NORMAL REF AMM 22-11-00 A/C OK OPS CHECK NORMAL.SDR ASAA2018041724291Control Valve · faultedZONE TEMP LIGHT ON RECALL CONT CABIN. ACFT GROUNDED. PERFORMED A BITE TEST OF PACK ZONE TEMP CONTROLLER IAW AMM 21-61-00-700-806-002, THE TEST INDICATES FLIGHT DECK TRIM VALVE FAULT. REMOVED AND REPLACED ZONE TRIM AIR MODULATING VALVE IAW AMM 21-61-21, OPSSDR ASAA2018041424242Coupler · failedNR 1 AND 2 HF RADIO NO COMM APPROACHING GATEWAY FIX. SEEMED TO BE TUNING, HAD SIDETONE. COULDNT HEAR MUCH STATIC IN AUDIO, SEEMED ABNORMAL. ACFT GROUNDED. PERFORMED FIM 23-11 TASK 801, NR 1 AND 2 HF BITE PASSED. PERFORMED HF COMM SYSTEM TEST IAW FIM 23-11 SDR ASAA2018041324244Fire Detector · inoperativeAPU DETECTOR INOPERATIVE LIGHT ILLUMINATED ON THE GROUND, ALONG WITH MASTER CAUTION OVERHEAT DETECTOR. ACFT GROUNDED. TROUBLESHOT TO THE APU LOWER LOOP. REMOVED AND REPLACED THE APU LOWER FIRE DETECTION LOOP, OPS CHECKED NORMAL IAW AMM 26-10-01 AND 26-15-SDR ASAA2018033124091Valve · malfunctionedDURING CLIMBOUT, FA STATED WATER PRESSURE IN LAVS AND WATER DISPENSED WITH COFFEE MAKERS LOW PRESSURE, THROUGHOUT AIRCRAFT. ACFT GROUNDED. AIR TURNBACK. OPENED THE WATER SERVICE PANEL, CYCLED WATER DRAIN VALVE OPEN THEN CLOSED. WATER PRESSURE & FLOW NORMSDR ASAA2018032024003Starter · failedNR 2 ENGINE WILL NOT START, APU DUCT PRESSURE 45 PSI. START SWITCH IN GROUND MODE, START VALVE OPEN INDICATION N2 0 PERCENT. FAN BLADES TURNED BY HAND. EXTERNAL HEAT SOURCE APPLIED WITH COWL COVERS. NO CHANGE ON RESTART ATTEMP, NR 1 ENGINE TURNS NORMALLY SDR ASAA2018030723786Control Panel · failedAUTOPILOT CMD A BACK LIGHT INOPERATIVE. AUTO PILOT A OPERATED NORMALLY. ACFT GROUNDED. VERIFIED THE FAULT. REPLACED THE MCP IAW AMM 22-11-34/401. THE NEW MCP OPS CHECKED GOOD.SDR ASAA2018010923123Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. RESET WITH THE MASTER CAUTION. ACFT GROUNDED. BITE CHECKED THE RT ZONE TEMP CONTROLLER IAW FIM 21-62 TASK 801. FAULTED FLT DECK TRIM VALVE. RAN VERIFY TEST THREE TIMES IAW FIM 21-62 TASK 832, FAULT CLEASDR ASAA2017120522803Display · faultyCAPTAINS CDU FLICKERING ON DESCENT. GROUNDED - YES. PERFORMED CAPT FMC L CDU BIT FLT FAULT. FOUND CDU LIGHT SENSOR AND SEVERAL CDU POWER FAULTS LOGGED. REMOVED AND INSTALLED NEW MCDU ON CAPT SIDE REF AMM 34-61-01-000-802. PERFORMED SW CONFIG CDU SOFTWARE CONFISDR ASAA2017120422781Display · malfunctionedCAPT MCDU SCREEN FLICKERING INTERMITANTLY. GROUNDED - YES. OPS NORMAL REF B737-800 FIM 34-61 TASK 803.SDR ASAA2017112022657Window · failedRIGHT FWD WINDSHIELD OVERHEAT LIGHT IS ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED WINDOW HEAT CONTROL UNIT BITE PROCEDURE ON THE RIGHT FWD CONTROLLER. FOUND WINDOW SENSOR FAULT LIGHT ILLUMINATED, IAW FIM 30-41 TASK 801. MEASURED THE RESISTANCE OF THE WINDOW TSDR ASAA2017111522616Pump · failedDURING FLIGHT RIGHT CENTER TANK FUEL PUMP LIGHT ILLUMINATED. W/3100LBS OF FUEL IN CTR TANK. PILOT RAN QRH FOR CONDITION. STOPPING THE INCREASING FUEL IMBALANCE. ALL C/B'S REMAINED STOWED. GROUNDED - YES. REPLACED THE RT CENTER TANK BOOST PUMP MOTOR IMPELLER PESDR ASAA2017111322654Idg · failedNR 1 IDG HAD A THIRD DPI TRIP. ACFT GROUNDED. FLUSHED IDG OIL SYSTEM IAW AMM 12-13-21. REMOVED & REPLACED THE NR 1 ENGINE IDG IAW AMM 24-11-11. OPS CHECKED GOOD.SDR ASAA2017111322548Filter · cloggedDURING PDC, FOUND THE NR 1 IDG DIFFERENTAL PRESSURE INDICATOR POPPED. ACFT GROUNDED. ACCOMPLISHED AMM 12-13-21-200-802, CHANGED SCAVENGE CHARGE FILTERS AND IDG OIL NO METAL PARTICLES NOTED, LEAK CHECKED GOOD, DPI RESET.
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