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 ASAA2022082139598Starter · inoperativeNO. 1 ENGINE WILL NOT START AFTER 2 ATTEMPTS. START VALVE OPENS WITH NO N2 ROTATION. DUCT PRESSURE INDICATES 20 PSI. GROUNDED - YES. REMOVED AND REPLACED ENG. #1 PNEU. STARTER IAW B737-800 AMM 80-11-01/401.SDR ASAA2022080239412Control Valve · faultyON CLIMB OUT LEFT DUCT PREESSURE WAS 18PSI AND RIGHT WAS 40PSI UNTIL ABOUT FL300. BY LEVEL OFF AT FL380 LEFT WAS 32PSI AND RIGHT WAS AT 40PSI. ON TAXI BOTH READ ABOUT 20PSI. PRESSURIZATION WAS NORMAL THOUGHOUT THE FLT. GROUNDED - YES. REMOVED AND REPLACED #1 ESDR ASAA2022070438921Satcom · intermittentSATCOM #2 SHOWS NOT READY/FAIL. GROUNDED - YES. CYCLED AIRCRAFT ELECTRICAL POWER, PERFORMED SATCOM COMMUNICATION TEST, OPS CHECK GOOD REF B737-800 AMM 23-15-00-730-801.SDR ASAA2022052238413Door · stickingL1 DOOR HARD TO CLOSE. TOOK MULTIPLE ATTEMPTS TO SECURE CLOSE. GROUNDED - YES. PERFORMED B737-800 AMM TASK 52-11-200-801 OPS CHECK OK, OK FOR SERVICE COULD NOT DUPLICATE.SDR ASAA2022051938428Modulating Valve · inoperativeFLIGHT DECK PRIMARY TEMP CONTROLLER INOP. GROUNDED - YES. REMOVE AND REPLACED TRIM MODULATING VALVE FOR CONT CABIN PER B737-800 AMM 21-61-21. OPS CHK GOOD.SDR ASAA2022051938406Window · false indicationL & R FWD WINDOW HEAT INOP. GROUNDED - YES. FWD FLT DECK WINDOWS IN DIRECT SUNLIGHT HIGH TEMP @ DEN WINDOW HEAT TEMP OVER 40 DEGREES C. CAUSING WHC NOT TO PWR FWD WINDOW HEAT THIS IS NORMAL OP'S REF B737-800 FIM 30-41-11-710-801 FLT CREW ALSO CONFIRM NORMAL OPSDR ASAA2022041338032Unknown · unknownCONT CABIN ZONE TEMP ANNUNCIATOR ILLUMINATES ON MASTER CAUTION RECALL. EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. VERIFIED DISCREP ON MASTER CAUTION RECALL. PERFORMED PACK TEMP CONTROL-BITE PROCEDURE REF B737-800 FIM 21-62 TASK 801 ON # 2 CONTROLLERSDR ASAA2022041337980Seal · degradedWHILE ACCOMPLISHING APU REPLACEMENT, FOUND AIR INLET SEAL MEASURES 1.25". REQUIRES REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED APU INLET SEAL PER B737-800 AMM 49-15-11-000-801 AND AMM 49-15-11-400-801.SDR ASAA2022040237878Apu · unknownAPU OIL CONSUMPTION INSPECTION DUE TO REPORT OF EXCESSIVE SERVICING. ETOPS SIGNIFICANT SYSTEM TASK AFFECTS APU ON DEMAND IN-FLIGHT START CAPABILITY. GROUNDED - YES. REF ITEM 1 OF TSR B737-800 FIM TASK 49-95-00-810-801. REMOVED AND REINSTALLED PORT 1 EGT PROBESDR ASAA2022040137883Oil Cap · damagedREF L/P 60343057 GVI OF #2 ENGINE FOR OIL LEAKS ACCOMPLISHED. FOUND ENGINE OIL POOLING INSIDE FAN COWL. GROUNDED - YES. OPENED #2 ENG FAN COWLS. FOUND OIL CAP AND OIL CAP O-RING DAMAGED. REMOVED AND REPLACED OIL CAP, OIL CAP O-RING AND LEAK CHECK NORMAL.SDR ASAA2022033037857Unknown · unknownWHILE ADDING OIL IN APU FOUND OIL FILTER INDICATOR EXTENDED [ RED DELTA P BUTTON }. GROUNDED - YES. CHECKED MAGNETIC DRAIN PLUG & FILTER REF B737-800 AMM 49-91-81-200-801 & 49-91-12-000-802 NO CONTAMINATION FOUND. GROUND CHECK VERIFICATION GOOD. NO LEAKS NOTEDSDR ASAA2022031837719Unknown · unknownLEFT FMC FAIL. GROUNDED - YES. PERFORMED POWER RESET OF AIRCRAFT. PERFORMED BITE OF FMC L PER B737-800 FIM 34-61 TASK 801. FOUND ALL SENSORS TO BE OPERATING NORMALLY. OPS TEST GOOD.SDR ASAA2022031437687Keyboard · inoperativeFIRST OFFICER FMC R-1 BUTTON IS INOP. GROUNDED - YES. VERIFIED DEFECT. R1 BUTTON INOP. REMOVED AND REPLACED FMCS CDU KEYBOARD IAW B737-800 AMM 34-61-01-000/400-801. PASSES INSTALL TEST. NO OTHER DEFECTS NOTED.SDR ASAA2022011937206Lens · brokenEMERGENCY EXIT SIGN LIGHT COVER BROKEN AT 16A. GROUNDED - YES. REPLACED LENSE COVER OPS CHK GOOD, REF B737-800 AMM 33-51-14.SDR ASAA2021123037036Valve · faultyAT FL 380 GOT ZONE TEMP LIGHT CONT CABIN IT RESET WHEN WE DECREASED THE CONT CABIN TEMPERATURE (1 CONTROLLER IS MEL'D). GROUNDED - YES. REF MEL 21-21G, CONFIRMED FAULT. REMOVED AND REPLACED DEFECTIVE FLIGHT DECK TCV (V143) PER AMM 21-61-21, OPS CK NML REF B737SDR ASAA2021122937037Valve · faultyZONE TEMP CONT CAB SINGLE CHANNEL FAILURE. GROUNDED - YES. CONFIRMED FAULT, CONTROL CABIN ZONE TEMP LIGHT ILLUMINATES WHEN RECALLED. #2 PACK/ZONE TEMP CONTROLLER SHOWS HARD FAIL "FLIGHT DECK TCV". REMOVED & REPLACED "FLIGHT DECK TCV (V143)" REF B737-800 AMM 21SDR ASAA2021102936450Unknown · unknownOVERHEAT B NOT WORKING ON ENG 1. GROUNDED - YES. (RESOLVED ON W/O: 1890094 TASKCARD: N/R-00001 ) PER B737-800 FIM 26-10 TASK 801 AND 805 BITE OF FIRE DET CTR MODULE SHOWS ENG 1, LOOP B OPEN OR DET FAULT. INSPECTED FIRE LOOPS. FOUND BROKEN LUG AT ENGINE FAN UPPSDR ASAA2021102136371Actuator · noneUPON MASTER CAUTION RECALL AT 28,000' THE LEFT PACK LIGHT CAME ON. RAN CHECKLIST AND LIGHT WENT OFF WITH MASTER CAUTION PUSH. SYSTEM ANNUNCIATOR PANEL FO SIDE DID NOT LIGHT UP WITH AIR COND HOWEVER. GROUNDED - YES. REMOVED PANELS 191GI, & 191FF. TROUBLESHOT PESDR ASAA2021101536314Control Valve · faultyAFTER ENGINE START ON RECALL, LEFT PACK LITE ILLUMINATED. RAN CHECKLIST. UPON MASTER CAUTION RESET, THE LITE WENT OUT. GROUNDED - YES. REMOVED AND REPLACED LH TEMPERATURE CONTROL VALVE IAW B737-800 AMM 21-51-10-000-801 AND AMM 21-51-10-400-801, ETOPS GROUND FUSDR ASAA2021101236287Indicator · inoperative#1 MAIN TANK FUEL INDICATOR INOP (FUELING PANEL). GROUNDED - YES. REMOVED #1 REFUELING QUANTITY INDICATOR PER B737-800 AMM 28-41-61-000-801 INSTALLED PER AMM 28-41-61-400-801 PERFORMED OPS TEST PER SAME OPS TEST IS GOOD.SDR ASAA2021100536205None · noneREFUELING TANK #1 FUEL QTY INOP. GROUNDED - YES. REPLACED #1 FUEL QTY IND AT REFUEL PNL REF B737-800 AMM 28-41-61-400-801. FQIS TEST & IND TEST OK.SDR ASAA2021091936003Idg · inoperative#2 DRIVE LIGHT EXTINGUISHED ON THE GROUND WITH ENGINE SHUTDOWN BULB PUSHED TO TEST NORMALLY. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 24-11 TASK 805. GCU BITE TEST PASSED. PER FIM 24-21 TASK 801. REMOVED #2 ENGINE IDG OIL FILTERS, NO CONTAMINATION OR METAL FOSDR ASAA2021091935975Unknown · unknownHF1 ILLUMINATES FAIL MESSAGE WHEN ENTERING HF FREQUENCIES. GROUNDED - YES. CYCLED AIRCRAFT POWER OPS CHECKED HF1 PER B737-800 AMM 23-11-00-730-801CHECKS GOOD.SDR ASAA2021072335497Fmc · faultedON TAXI WE HAD A FMC DISAGREE. GROUNDED - YES. AFTER CONSULTING MAINTENANCE CONTROL WE RAN QRH 11.2. AFTER COMPLETION OF CHECK LIST WE HAD NORMAL FMC OPERATION AND CONTINUED NORMAL OPERATION.SDR ASAA2021070735339Coupling · failedHF 1 SHOWS FAIL IN BOTH ACTIVE AND STANDBY. GROUNDED - YES. REMOVED & REPLACED HF 1 ANTENNA COUPLER PER B737-800 AMM 23-11-61. INSTALLATION TEST GOOD PER AMM 23-11-61. PERFORMED HF COMM STSTEM TEST PER AMM 23-11-00-730-801. BOTH HF 1 +2 TEST NORMAL.SDR ASAA2021061635119Fire Detector · brokenFAULT LIGHT #1 ENGINE B LOOP. GROUNDED - YES. VERIFIED DISCREP FIRE DETECTION CONTROL UNIT SHOWS #1 ENG B LOOP UPPER FAN DETECTOR FAULT. UPON INSPECTION OF UPPER FAN DETECTOR ASSY. FOUND BROKEN B LOOP ELEMENT REF B737-800 AMM 26-11-01, REMOVED/REPLACED UPPER FSDR ASAA2021051434816Knob · looseTHE LEFT HAND "TILT/GAIN" KNOB ON THE RADAR CONTROL PANEL IS LOOSE. GROUNDED - YES. RMVD & RPLCD WXR CNTL PANEL REF B737-800 AMM 34-43-91. OPS NML PER SAME. ETOPS GND VERIFICATION SUCCESSFUL.SDR ASAA2021042934727Control Cable · brokenON CLIMBOUT, FA REPORTED NO WATER PRESSURE IN ANY OF THE LAVATORY SINKS OR TOILETS. GROUNDED - YES. DIVERSION TIME 29 MINUTES - FOUND WATER TANK FILL VALVE LOOSE AND ALLOWING FILL VALVE TO LOOSE PRESSURE (SUSPECT BAD VALVE CONTROL CABLE). REMOVED AND REPLACED SDR ASAA2021042934712Actuator · failedRIGHT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL, GOES OUT WITH MASTER CAUTION RESET. GROUNDED - YES. PERFORMED RH PACK TEMP CONTROL BITE PROCEDURE PER B737-800 FIM 21-62 TASK 801. HARD FAULT FOUND FOR RAM AIR ACTR PER FIM 21-62 TASK 836. REPLACED RH RAM SDR ASAA2021041934622Eec · malfunctionedENG CONTROL NR 2 LIGHT ILLUMINATED ON LANDING. GROUNDED - YES. FOUND ENG 2 ALTN PWR CH-A C/B POPPED. RESET C/B AND WHEN NR 2 EEC BITE TEST C/B POPPED AGAIN, CH-A FAILED TEST CH-B OK. REF B737-800 WDM 73-27-11, SUSPECTS ENG 2 EEC INOP. REMOVED & REPLACED NR 2 ESDR ASAA2021041734623Valve · out of limitsACCOMPLISHING TC 78276000 FOUND #2 ENG FAULT CODE 75-10592. THE TBV POSITION SIGNAL IS OUT OF RANGE. LONG TIME FAULT. GROUNDED - YES. REMOVED AND REPLACED ENGINE #2 TBV REF B737-800 AMM 75-23-01-000-801-F00/75-23-01-400-801-F00, PERFORMED IDLE POWER LEAK CHECKSDR ASAA2021041734596Blade · wornWHILE ACCOMPLISHING FAN LUBE ON #2 ENG T/C #78472010 FOUND #13 BLADE WITH MISSING CUNI COATING BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED #13 FAN BLADE ON #2 ENG IAW ASA MTX TASKCARD #78472010.SDR ASAA2021040734525Fmc · malfunctionedCREW REPORT MOMENTARY FMC DROP. VTK ON NAV DISPLAY, LEFT SIDE. GROUNDED - YES. REF B737-800 FIM 34-61 TASK 836 RESET FMCS 1 & 2. NO FAULTS NOTED. VTK FLAGS NOT PRESENT. NO FURTHER ACTIONS REQUIRED AT THIS TIME. 2 MIG 51-A INSTALLED AND REMOVED.SDR ASAA2021040534516Autothrottle Sys · malfunctionedAUTO THROTTLE WILL NOT ARM ON TAXI OUT. FOUND C/B E1 POPPED. GROUNDED - YES. RESET C/B E1 (A/T DC1), PERFORMED A/T BITE PROCEDURE REF B737-800 FIM 22-31 801 FOUND FAULT MSG 22-31263 (A/T 28 VDC PWR INV) IN FLIGHT HISTORY, CURRENT STATUS SHOWS NO FAULTS, PER FISDR ASAA2021040434506Module · malfunctionedWHEN DISCONNECTING AUTOPILOT A CHANNEL NO HORN ANNUNCIATED. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 22-12 TASK 817 FOR CHECK OF AURAL WARNING MODULE DFCS BITE TEST AURAL WARNING ON DISCONNECT CHECKS GOOD.SDR ASAA2021010233795Wire Harness · brokenDURING PRE FLIGHT ENGINE FIRE TEST REVEALED FAULT LIGHT. GROUNDED-YES. CW B737-800 FIM 26-10 TASK 805 STEPS F(4)(D). MANIPULATED MW0325 HARNESS. RESISTANCE AT LT CORE LOOP (RIGHT SIDE OF ENGINE) RING TERMINAL ERRATIC WIRE EASILY BROKE OFF WHILE CHECKING. SDR ASAA2020123033791Actuator · inoperativeNR 2 PACK LIGHT ON MASTER CAUTION CHECK, EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED-YES. CHANGED RAM AIR INLET ACTUATOR DUE TO HISTORY, FOUND MODULATION PANEL OUT OF ITS TRACKS. RE-INSTALLED CORRECTLY OPERATIONS CHECK NORMAL, REF B737-800 AMM 21-51-21.SDR ASAA2020122733750Fire Loop · inoperativeNR 1 ENGINE A FIRE LOOP INOPERABLE. GROUNDED-YES. ON DEFERRAL.SDR ASAA2020122733782Control Valve · faultyWHEN RECALL IS PUSHED THE RIGHT PACK LIGHT ILLUMINATES. IT EXTINGUISHES WHEN RESET. GROUNDED-YES. TASK CARD COMPLIED WITH PERFORMED PACK TEMPERATURE CONTROL BITE PROCEDURE, REF B737-800 FIM 21-62 TASK 801. BITE TEST FAULTED AT ZONE TRIM VALVE. REMOVED ANDSDR ASAA2020122333742Actuator · inoperativeDURING DESCENT CHECK PACK LIGHT (RT) ILLUMINATED DURING RECALL. GROUNDED-YES. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST, ZONE TEMP CONT NR 2 FAULTED "RAM AIR DOOR ACTUATOR", REF B737-800 AMM 21-61-00. REMOVED RT RAM AIR DOOR ACTUATOR AND REPLACED WITH NSDR ASAA2020122033731Modulating Valve · failedRT PACK LIGHT ON MASTER CAUTION RECALL EXTINGUISHED ON RESET. GROUNDED-YES. PERFORMED BITE CHECK, REF B737-800 FIM 21-62 TASK 801/802, TRIM VALVE LIGHT ILLUMINATED. REMOVED & REPLACED ZONE TRIM VALVE OPERATIONS CHECK GOOD, REF B737-800 AMM 21-61-21.SDR ASAA2020121833712Actuator · failedRIGHT PACK LT ILLUM ON MASTER CAUTION RECALL. EXTINGUISHED WITH RESET. GROUNDED-YES. TROUBLESHOT BOTH CONTROLLER FAULT FOUND NR 2 RAM AIR ACTUATOR WON`T CLEAR. REMOVED AND REPLACED RT RAM AIR INLET ACTUATOR, REF B737-800 AMM 21-51-21/401. BITE TEST AND OPSDR ASAA2020121833710Control Valve · false indicationRIGHT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL, EXTINGUISHES DURING RESET. GROUNDED-YES. REMOVED AND REPLACED RIGHT PACK TEMPERATURE CONTROL VALVE, PER B737-800 AMM 21-51-10. OPERATIONAL CHECKED GOOD AT THIS TIME, NO FAULTS FOUND.SDR ASAA2020121733703Warning Light · false activationRIGHT PACK LIGHT ILLUMINATES ON RECALL. LIGHT EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED-YES. PERFORMED BITE ON NR 2 PACK CONTROLLER FOUND RAM AIR ACT FAULT, NO FAULTS PREV FLIGHT. PERFORMED VERIFY NO FAULTS FOUND, REF B737-800 AMM 21-61-00.SDR ASAA2020112333662Cargo Track · gougedFWD PIT FLOOR SUPPORT AT STATION 460 RBL 17 HAS LARGE GOUGE. GROUNDED-YES. MEASURED THE DEPTH OF THE GOUGE ON THE CARGO TRACK, DEPTH=0.060 X WIDTH= 0.400, ORIGINAL THICKNESS 0.170, FOUND TO BE OUT OF LIMITS, IAW B737-800 SRM53-00-53-1A-Z. REMOVED DAMAGED SESDR ASAA2020112333631Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN CRACK NOTED IN SECTION STAB STA 92.70 AND STAB STA 101.90 7 INCH FROM AFT SPAR RIVETS. CRACK APPROXIMATELY 1.1 INCH IN LENGTH AND END POINTS, MARKED IN RED. GROUNDED-YES. DAMAGE CUTOUT AND REPAIRED ON RT HORIZ STAB LOWSDR ASAA2020082413070Platform · damagedFOLLOW UP TO DAMAGE FOUND ON FAN BLADE PLATFORM NR 21 DURING FAN LUBE INSPECTION OF NR 1 ENGINE. GROUNDED - YES. REMOVED AND REPLACED FAN BLADE NR 21 P/N 340-001-038-0, S/N DC610218-C; BLADE NR 22 P/N 340-001-038-0, S/N DB632189-M AND ITS OPPOSITE SIDES, P/SDR ASAA2020082413069Platform · crackedFOUND NR 21 PLATFORM CRACKED, REF T/C 78472010 STEP 35. GROUNDED - YES. REMOVED AND REPLACED COMPLETE SET OF PLATFORMS (24 EA), REF T/C 78472010 STEP 35.SDR ASAA2020082413068Nut Plate · damagedFOUND BAD NUTPLATE ON REAR SPINNER CONE NR 1 ENGINE WHILE ACCOMPLISHING FAN BLADE LUBE, REF TC 78472010. GROUNDED - YES. REMOVED AND REPLACED ENG NR 1 REAR SPINNER CONE, REF TC 78472010 SUBTASK 839-051. ALL SPINNER WEIGHTS ARE PUT BACK TO NOMINAL, IN REFERESDR ASAA2020070632871Fastener · looseREF T/C 78472000 NR 1 ENG INLET AND FAN BLADES, DETAILED INSP FOUND 1 EACH LOOSE FASTENER ON NR 3 FAN CASE PANEL, AFT RT CORNER, MAY HAVE WORN FASTENER HOLE IN PANEL. GROUNDED - YES. FOUND FASTENER TO BE LOOSE. RE-TORQUED FASTENER REF AMM 72-23-07.
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