N565AS
Service difficulty reports · 509
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 = 'N565AS' 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 = 'N565AS' 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 ASAA2020010931815Light · inoperativeEXTERIOR FWD MOST EMERGENCY LIGHT INOP ON A/C L/H SIDE (BY L2 DOOR). GROUNDED - YES. RELAMPED EMERGENCY EXIT EXIT EXTERIOR SLIDE/OVERWING LIGHT BY L2 DOOR PER B737-800 AMM 33-51-04.SDR ASAA2019121783554Compensator · out of limitsAPPROXIMATELY ONE HOUR INTO FLIGHT WHEN CENTER FUEL TANK BECAME EMPTY FUEL SPLIT BETWEEN LEFT AND RIGHT TANK INCREASED TO 500 LBS WITH LEFT TANK INDICATING LOWER QUANTITY. FUEL BURN INCREASING TO 900 LBS BELOW PROJECTED FUEL QUANTITY. SPLIT DECREASED TO 350LBSSDR ASAA2019120971535Fmc · malfunctionedAFTER LANDING LEFT FMC FAILURE, VTK FLAG ON CAPTS ND. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 34-61 TASK 836. L/H FMC RESET. NO FAULTS NOTED.SDR ASAA2019112531428Warning Message · false activationON PREFLIGHT - LEFT FORWARD WINDSHIELD OVERHEAT ON. GROUNDED - YES. FOUND LEFT FRONT C/B OUT P6-11, ACCOMPLISHED C/B RESET REF B737-800 AMM 20-60-11 & WINDOW HEAT CONTROL TEST REF AMM 30-60-11 OPS NORMAL. NO HISTORY PAST 90 DAYS.SDR ASAA2019112203410Fan · dirtyON TAXI OUT @ SEA DURING AFTER START CHECKLIST- RECALL WE GOT AN AIR CON. M.C. W/CONT CAB ZONE TEMP LIGHT. EXTINGUISHES DURING M.C. RESET. GROUNDED - YES. REF B737-800 FIM 21-62 TASK 801. NO ZONE TEMP LT ON RECALL. PACK TEMP CONTROLLER BITE FOR #1 & #2 SHOWS NSDR ASAA2019111931393Shutoff Valve · failedNO DUCT PRESSURE ON RIGHT SIDE. GROUNDED - YES. MANUALLY CYCLED THE PRSOV AND PCCV W/ NO DEFECT. VERIFIED ALL LINES TO BAR AND PRSOV ARE TIGHT. NO CIRCUIT BREAKERS TRIPPED. W/ APU AS BLEED SOURCE, BOTH DUCT PRESSURE NEEDLES ARE MARRIED. WHEN CYCLING #2 BLEED SSDR ASAA2019092330805Control Panel · lockedMCP ALTITUDE WINDOW LOCKED UP READING 50000' OUR ALTITUDE WAS FL350 AND WE HAD BEEN CLEARED TO 10000' IT HAPPENED AFTER WE SPUN THE KNOB. ALTITUDE AURAL WARNING WAS HAPPENING. FOLLOWED QRH AND THE PROBLEM WAS FIXED. GROUNDED - YES. ACCOMPLISHED FIM 31-62 TASK SDR ASAA2019092230771Fmc · malfunctionedON LND CA SIDE "VTK" CYCLES ON/OFF 30" SEC CYCLE. GROUNDED - YES. ACCOMPLISHED FMC RESET PER FIM 34-61 TASK 836. FMC RESET NORMAL.SDR ASAA2019092230770Fmc · malfunctionedMCP LOCKUP ABOUT 30" DURING DESCENT THEN RETURNED TO NORMAL OPERATION. NOTE: DID NOT HAVE TO DO QRH PROCEDURE. GROUNDED - YES. ACCOMPLISHED FMC RESET PER FIM 34-61 TASK 836, FMC RESET NORMAL.SDR ASAA2019091930732Control Panel · failedF/O'S COURSE SELECT WINDOW IS BLANK. GROUNDED - YES. REMOVED ANDD REPLACED DFCS MCP REF AMM 22-11-34 OP CK GOOD 9 CBS PULLED.SDR ASAA2019082213444Battery Pack · failedREF T/C 78233001 EMERGENCY LIGHT BATTERY PACKS M1671 AND M1673 FAIL CAPACITY CHECK. GROUNDED - YES. REPLACED EMERGENCY LIGHT BATTERY PACK M1671 AND M1673 REF B737-800 AMM 33-51-06-960-805. OPS CHECK GOOD.SDR ASAA2019072730211Ecu · failedREF DEFECT # TSR703265 DURING INSTALLATION TEST OF APU P/N 3800702-1 S/N P-8133APU CURRENT STATUS SHOWS MAINT MSG 49-72104 "DATA MEMORY MODULE SHOWS CIRCUIT FAILURE". GROUNDED - YES. REMOVED AND REPLACED THE APU ECU, OPS CHECK GOOD AND NO FAULTS ON APU BITE CUSDR ASAA2019072730210Apu · overtempAPU REPORTS SHOW A RAPID SPIKE IN CT5ATP TEMP. CT5ATP TEMP IS AT OR ABOVE THE THRESHOLD 605 DEGREES. INSTALLATION TASKS MAY AFFECT APU ON DEMAND IN-FLIGHT START CAPABILITY. UPON COMPLETION CONTACT MAINTENANCE CONTROL AND REPORT THAT THIS TASK HAS AFFECTED APU SDR ASAA2019070129889Unknown · malfunctionedL-1 WINDOW OVERHEAT LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED FIM 30-41 TASK 812. MOVED L-1 WINDOW SENSOR SELECT SWITCH TO OTHER POSITION. TESTED GOOD.SDR ASAA2019060329549Coupler · failedUNABLE TO TRANSMIT ON HF 1, RECEIVE ONLY. GROUNDED - YES. REMOVED AND REPLACED #1 HF COUPLER PER B737-800 AMM 23-11-61. OPS CHECK GOOD.SDR ASAA2019060329550Transceiver · failedCANNOT TRANSMIT ON HF1. RECEIVER PORTION OPERATES NORMALLY. GROUNDED - YES. REMOVED AND REPLACED HF1 TRANSCEIVER PER B737-800 AMM 23-11-21. OPS CHECK WAS GOOD.SDR ASAA2019040438887Detector · faultedRIGHT WING BODY OVERHEAT LIGHT ANNUNCIATED AFTER TAKEOFF. RAN QRH ISOLATED RT PACK & RT BLEED OFF. GROUNDED - YES. INTERROGATED THE CODCU UPON ARRIVAL FOUND FAULT FAULT CODE 64, RAN RIGHT PACK INSPECTED FOR LEAKS, NO LEAKS NOTED IN THE A/C BAY OR ENG PYLON. STSDR ASAA2019040128825Sensor · corrodedCLIMB OUT, 25,000 FT #2 WING BODY OVERHEAT LIGHT DID QRH LIGHT REMAINED ILLUMINATED. GROUNDED - YES. DIVERSION TIME 42 MINUTES - FOUND NO ACTIVE FAULTS RECORDED ON THE CODCU. VISUALLY INSPECTED THE ELEMENTS ASSOCIATED WITH FAULT 64 (FROM T/S ENTRY), AND FOUND SDR ASAA2019032228748Fmc · malfunctionedON DESCENT F/O FMC FAIL, VTK, PERFORMED QRH AND DID NOT RESET. STAYED ON FMC BOTH ON LEFT. GROUNDED - YES. RESET FMC NR 2 BY CYCLING SYSTEM POWER. AFTER SYSTEM RESET NR 2 FMC CHECKS GOOD IAW AMM 34-61-00-710-801.SDR ASAA2019031428610Hf Comm · malfunctionedHF SHOWS FAIL ON NR 1. GROUNDED - YES. CYCLED NR 1 HF RADIO C/B ON P18 PANEL. ESTABLISHED COMMUNICATION WITH SFO RADIO. NR 1 HF OPS CHECK GOOD.SDR ASAA2019030128438Platform · wornNR 1 ENG HAS 24 WORN PLATFORMS. GROUNDED - YES. REMOVED AND REPLACED ALL 24 PLATFORMS ON NR 1 ENG. REF T/C 78472010.SDR ASAA2019030128437Spacer · wornNR 1 ENG HAS 5 WORN SPACERS. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG 5 WORN SPACERS REF T/C 78472010.SDR ASAA2019012927979Blade · damagedWHILE ACCOMPLISHING TC 78472002, FOUND NR 12 BLADE ON NR 2 ENGINE MISSING CU-NI OUTSIDE OF AREA "X" ON FWD CONVEX SIDE PRESSURE FACE. GROUNDED - YES. REPLACED NR 12 BLADE AND NR 24 BLADE ON NR 2 ENG.SDR ASAA2019012927978Elastomer · missingWHILE ACCOMPLISHING TC 78472002, NR 2 ENG PLATFORMS ARE MISSING ELASTOMER SEALS WITH OVER CUMULATED LENGTH OF 41 INCHES. GROUNDED - YES. INSTALLED SERVICEABLE PLATFORMS 24 EA.SDR ASAA2019012927977A/C Pack · defectiveWHILE ACCOMPLISHING TASK CARD, FOUND NR 2 ENG REAR SPINNER CONE WITH BAD NUT PLATE. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENG REAR SPINNER CONE.SDR ASAA2019011827876Door Seal · defectiveFA'S REPORTED AFTER TAKEOFF LOUD AIR NOISE FROM L-1 DOOR. PILOTS CONFIRMED L-1 ENTRY DOOR LT WAS EXTINGUISHED. ALSO CONFIRMED A/C WAS NOT PRESSURIZING. GROUNDED - YES. AIR TURNBACK - DIVERSION TIME 16 MINUTES. FOUND LOWER INTERIOR HINGE COVER SNUBBER CREATES ASDR ASAA2019011727966Fan · out of balance2 ENGINE TREND DATA SHOWS AN INCREASE IN LOW PRESSURE ROTOR VIBRATION LEVELS. DATA SCATTER INDICATES FAN LUBE REQUIRED. GROUNDED - YES. ACCOMPLISHED T/C 78472002 ON NR 2 ENG. REPLACED ALL PLATFORMS, SHIMS AND NR 12 AND 24 BLADES. REMAPPED BLADES PER BLAMAP VERSDR ASAA2018121627451Fmc · malfunctionedRIGHT FMC FAILED AT CRUISE FOR 20-30 SECONDS. VTK DISPLAYED ON NAV DISPLAY. NO FMC ALERT MESSAGES. GROUNDED - YES. ACCOMPLISHED FIM 34-61 TASK 836, FMC OPERATIONS RESTORED.SDR ASAA2018110426729Spacer · migratedNR 2 ENGINE NR 6 BLADE SPACER HAS MIGRATED OUT. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE, NR 6 FAN BLADE PLATFORM REF AMM 72-21-02/401. REMOVED AND REINSTALLED REAR AND FRONT SPINNER CONE REF AMM 72-21-01/401.SDR ASAA2018092526275Seal · damagedF/A'S REPORT L1 DOOR SQUEAL INTERFERING WITH COMMUNICATION. GROUNDED - YES. AIR TURNBACK - DIVERSION TIME 43 MINUTES. REMOVED AND REPLACED L-1 LWR FLAPPER SEAL REF AMM 52-11-00-420-801, PRESSURIZED AIRCRAFT UP TO 6 PSI NO LEAK OR NOISE NOTED.SDR ASAA2018092546242Cover · deformedAFTER TAKE OFF A-F/A INFORMED US L-1 DOOR WAS MAKING EXCESSIVE AIR NOISE LEVELED OFF AT 15000 AND DECIDED TO RETURN TO DEP AIRPORT LOWER DOOR HINGE COVER NOT IN CORRECT POSITION. GROUNDED - YES. DIVERSION TIME 16 MINUTES - COMPLIED WITH ASA 800-52EA-20774, REFSDR ASAA2018091726320Compressor · out of balanceNR 2 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS ARE RISING. GROUNDED - YES. INSPECTED NR 2 ENGINE FAN, NO IRREGULARITIES NOTED. ORIGINAL WEIGHT CONFIG. AS FOLLOWS: LOC 1 - P06, LOC 5 - P05, LOC 33 - P05, MATCHED AAVM. ACCOMPLISHED 71-00-00 TESSDR ASAA2018082925954Smoke Detector · failedAFT CARGO DETECTION LOOP A INOP. GROUNDED - YES. CONFIRMED FAULT, CARGO ELECTRONIC UNIT (CEU) BITE SHOWS AFT CARGO A2244 (A3) AFT SMOKE DETECTOR FAILS TEST. REMOVED & REPLACED CARGO BAY SMOKE DETECTOR REF AMM 26-16-01, OPS CK NML REF AMM 26-16-00-730-801. PULLSDR ASAA2018082755913Fire Loop · malfunctionedAFT CARGO FIRE TEST FAILED FOR THE A LOOP. ACFT GROUNDED. PLACED AFT PIT LOOP SELECTOR TO NORMAL POSITION. ACCOMPLISHED AFT CARGO BAY SMOKE DETECTION, SMOKE TEST IAW AMM 26-16-00-730-801. ON ALL POSITIONS A & B NORMAL, LOOP SELECTOR. ALL TESTS PASSED. PERSDR ASAA2018082105862Battery Pack · inoperativeINTERIOR EMERGENCY EXIT LIGHTS, ROWS 6, 9, AND 11 WILL NOT ILLUMINATE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805-4D, AND OPS CHECKED GOOD IAW AMM 33-51-00-960-805.SDR ASAA2018082155861Gusset · crackedWHILE REMOVING THE LEFT AFT CARGO TRANSITION PANEL, FOUND THE GUSSET CRACKED ON THE WASTE TANK STRUCTURE. ACFT GROUNDED. REMOVED GUSSET ON WASTE TANK ENCLOSURE STRUCTURE IAW SRM 57-40-02-0G-0, PARA 7D.6. LOCATED AND DRILLED A NEW GUSSET IAW SRM 51-40-05-0GSDR ASAA2018081525777Bulkhead Web · crackedPRESSURE BULKHEAD WEB WAS CRACKED BS 663, LBL 25-45. ACFT GROUNDED. REPAIRED THE PRESSURE BULKHEAD WEB IAW SRM 57-10-10-2R.SDR ASAA2018081525773Floor Support · corrodedFLOOR SUPPORT BS 950, LBL 24 WAS CORRODED AT MULTIPLE AREAS. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR ASAA2018081525769Bulkhead Web · crackedRIGHT AFT PRESSURE BULKHEAD WEB AT BS 663 WAS CRACKED ON THE OTBD SIDE. ACFT GROUNDED. THE PRESSURE WEB WAS REPAIRED IAW SRM 57 10 10 2R 3.SDR ASAA2018082165867Floorbeam · corrodedFWD WET AREA BS 312 FLOORBEAM LBL 10 TO 20 HAD CORROSION ON THE UPPER HORIZONTAL FLANGE. ACFT GROUNDED. REPAIRED THE FLOORBEAM IAW EA 800-53EA-20655, AND SRM 53-10-51-2R-12, REPAIR 12.SDR ASAA2018082044444Floor Support · corrodedFWD WET AREA FLOOR SUPPORT AT LBL 10, BETWEEN BS 294 - 312 HAD AREAS OF CORROSION. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G.SDR ASAA2018082065827Floorbeam · corrodedFWD WET AREA BS 294, FLOORBEAM, LBL 12 HAS AREA OF CORR ON UPPER FLANGE. ACFT GROUNDED. THE FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. REPAIRED THE FLOORBEAM IAW EA 800 53EA 20611.SDR ASAA2018082065794Angle · corrodedL2 INNER ANGLE UPPER SURFACE HAD AN AREA OF CORROSION. ACFT GROUNDED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, PG 2, STEP B AND E. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1.SDR ASAA2018082065775Floor Support · corrodedFWD WET AREA FLOOR SUPPORT, LBL 12, BETWEEN BS 312 TO 328 WAS CORRODED ON THE UPPER FLANGE. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G.SDR ASAA2018081625793Support Angle · corrodedLT SHEAR WEB SUPPORT ANGLE AT AFT END LBL 32 HAS AREA OF CORROSION. ACFT GROUNDED. REMOVED AND REPLACED THE SHEAR WEB SUPPORT ANGLE IAW SRM 51-40-02-0G-0.SDR ASAA201801525776Floor Support · corrodedFLOOR SUPPORT AT LBL12 BETWEEN BS 312 - 328, WAS CORRODED. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR ASAA2018081525774Floorbeam · corrodedBS 986 FLOORBEAM HAD AREAS OF CORROSION ON THE UPPER FLANGE. ACFT GROUNDED. THE FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51.SDR ASAA201808155772Floorbeam · corrodedAFT WET AREA, BS 947 FLOORBEAM UPPER FLANGE, LBL 47-50 HAD AREAS OF CORROSION. ACFT GROUNDED. REPAIRED AND REPLACED THE FLOORBEAM TEE IAW SRM 53-70-51-2R-5.SDR ASAA20180815771Floorbeam · corrodedAFT WET AREA FLOORBEAM, BS 952, LBL 16 TO LBL 24, HAD AN AREA OF CORROSION. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, FIG 104, DETAIL C. REMOVED THE FLOORBEAM IAW SRM 51-40-02-0G-0, PARA 7D.6, FABRICATSDR ASAA201808205820Transition Panel · corrodedAFT CARGO BAY, RBL 25 TRANSITION PANEL BETWEEN BS 727 AND 767 CORRODED. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED TRANSITION PANEL IAW SRM 51-40-02-0G-0, 51-40-05-0G-0.
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