N560AS
Service difficulty reports · 562
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 = 'N560AS' 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 = 'N560AS' 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 ASAA2020091403171Drive Unit · failedWXR FAIL LIGHT ON WHEN WXR RADAR SELECTED. GROUNDED - YES. REMOVED AND REPLACED WXR ANTENNA DRIVE UNIT, REF B737-800 AMM 34-43-11. OPS CHECKS GOOD, REF AMM 34-43-00-710-802-001. GROUND VERIFICATION GOOD FOR ETOPS.SDR ASAA2020090833152Heater · inoperativeAFTER ENGINE START, LT ELEV PITOT AMBER LIGHT ILLUMINATED. GROUNDED - YES. HEATING ELEMENT ON PITOT TUBE OPEN. REMOVED AND REPLACED LEFT ELEVATOR FEEL PITOT PROBE, IAW B737-800 AMM 27-31-94.SDR ASAA2020081033008Valve · inoperativeFWD CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. GROUNDED - YES. PERFORMED BITE FOUND FWD CABIN PASSENGER TRIM AIR VALVE HARD FAULT. REPLACED FWD TRIM AIR VALE REF B737-800 AMM 21-15-10 BIT CK GOOD LK CK GOOD.SDR ASAA2020071082881Fmc · unknownIN CRUISE, CAPTAINS ND DISPLAYED VTK THEN MAP THE PROBLEM RESOLVED ITSELF. ND RETURNED TO NORMAL IN ABOUT 1 MINUTE. GROUNDED - YES. ACCOMP FMC BITE L/H FMC SHOWS LAST FLT FAULT FOR R FMC MSG IN R FMC REF B737-800 FIM 34-61 TASK 801. ACCOMP ADIRS BITE L & R ADISDR ASAA2020062932851Sensor · faultedDURING CRUISE, THE NR 1 ENGINE TREND DATA SHOWS OIL PRESSURE TO BE LOWER THAN EXPECTED, INDICATION ERRORS ARE SUSPECT. GROUNDED - YES. REMOVED AND REPLACED THE OIL PRESSURE SENSOR FROM THE NR 1 ENGINE IAW AMM 79-32-01, OPS AND OIL CHECKED GOOD.SDR ASAA2020062963846Warning Light · false activationCONT CAB ZONE TEMP ON RECALL. GROUNDED - YES. BITE CHECK OF NR 2 ZONE TEMP CONTROLLER SHOWS FAULT ON FLT DECK TRIM VALVE, VERIFY STEP PASSES. PERFORMED FIM 21-62 TASK 842 AND PERFORMED PACK TEMP CONTROLLER BITE PROCEDURE 1 & 2 IAW FIM 21-62 TASK 801. UNABLE TOSDR ASAA2020062652841Circuit Breaker · trippedWX RADAR CB POPPED. GROUNDED - YES. CHK'D & RESET C/B, RAN RADAR TEST, OPS NORMAL.SDR ASAA2020061872806Antenna · failedPWS FAIL ANNUNCIATED AFTER TAKEOFF. TURNED OFF WXR AND THEN HEARD & FELT GRINDING CYCLIC NOISE. TURNED OFF WXR, MOMENTARILY WXR FAIL ANNUNCIATED. GROUNDED - YES. DIVERSION TIME 35 MINUTES - REMOVED AND REPLACED WXR ANTENNA DRIVE UNIT, WXR OPS TEST OK REF B737-SDR ASAA2020041332633Valve · faultedCONT CAB ZONE TEMP LIGHT EXTINGUISHES WITH MC RESET. GROUNDED - YES. BITE CHECK OF ZONE TEMP CONTROL #2 (M1443) FAULTED FLIGHT DECK TRIM VALVE. REPLACED TRIM VALVE(V143). BITE TEST PASSES NO LEAKS NOTED. REF B737-800 FIM 21-62 TASK 832 AND B737-800 AMM 21-61-2SDR ASAA2020040132583Warning System · false activationUPON ANNUNCIATOR RECALL, CONT CAB ZONE TEMP ILLUMINATED. LIGHT EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. GROUNDED - YES. PERFORMED PACK TEMP CONTROLLLER 1&2 BITE IAW B737-800 FIM 21-62 TASK 801. FOUND CONTROLLER 2 BIT, AND PREV "FLIGHT DECK TRIM VALVE"SDR ASAA2020030932383Drive Unit · failedDURING CRUISE IN "AUTO" RADAR DISPLAY ALL RED IN FRONT OF A/C IN CLEAR CONDITIONS. LOUD MOTOR SOUND AND VIBRATIONS FELT AT THE SAME TIME. SHORTLY AFTER WXR FAIL FLAG ILLUMINATED. AFTER ABOUT 20 SECONDS - EVERYTHING RETURNED TO NORMAL. GROUNDED - YES. REMOVED ASDR ASAA2020030932384Drive Unit · faultyRADAR IS COMPLETELY UNRELIABLE - PAINTS RED WHERE THERE IS NO WEATHER. GROUNDED - YES. REMOVED ANTENNA DRIVE UNIT AND ANTENNA PLATE PER B737-800 AMM 34-43-11-00-802. INSTALLED ANTENNA PLATE AND DRIVE UNIT PER AMM 34-43-11-400-802. REMOVED WXR R/T PER AMM 34-43SDR ASAA2020030932382Transceiver · failedCAPT WEATHER RADAR FAILED. GROUNDED - YES. REMOVED ANTENNA DRIVE UNIT AND ANTENNA PLATE PER B737-800 AMM 34-43-11-00-802. INSTALLED ANTENNA PLATE AND DRIVE UNIT PER AMM 34-43-11-400-802. REMOVED WXR R/T PER AMM 34-43-41-000-802. INSTALLED WXR R/T PER AMM 34-43SDR ASAA2020030632366Control Panel · malfunctionedWX RADAR FAILED 2 HOURS INTO FLIGHT IN MANUAL MODE. WX RADAR APPEARS TO BE WORKING ON F/O SIDE WHILE WX FAIL FLAG IS DISPLAYED ON THE CAPT SIDE. GROUNDED - YES. NOTED FAIL OF WX RADAR FAIL CAPT SIDE ONLY. REF L/P 12167831 FOR WX RADAR CONTROL PANEL CHANGE. PERSDR ASAA2020030632365Control Panel · faultyAPPROX 15 MIN AFTER T/O THE WEATHER RADAR FAIL 9WXR FAIL ANNUNCIATED ON THE CAPT'S SIDE. ANNUNCIATION EXTINGUISHED APPROX 5 MIN LATER. WITH RADAR IN "AUTO" MODE, DISPLAYS (BOTH) SHOWED ABOUT 80% RED WHILE VISUALLY IN CLR CONDITIONS. RADAR SEEMS TO OPERATE NORMSDR ASAA2020022932330Transceiver · malfunctionedWEATHER RADAR FAILED IN FLIGHT. GROUNDED - YES. PER B737-800 FIM 34-43 TASK 801 WXR BITE TEST NORMAL NO FAULT NOTED. DUE PAST MX HISTORY, REMOVED & REPLACED WXR TRANSCEIVER PER B737-800 AMM 34-43-41. PERFORMED SYSTEM OPS TEST NORMAL REF AMM 34-43-00SDR ASAA2020022753287Radar · malfunctioned3 HOURS INTO FLIGHT WXR FAIL ON BOTH CAPTAIN AND FO DISPLAY UNITS ILLUMINATED. IN TEST MODE PWS FAIL, WXR FAIL AND ANT ANNUNCIATED IN BOTH CAPTAIN AND FO DU'S. GROUNDED - YES. PERFORMED BITE PER B737-800 FIM 34-43-00 TASK 810-801. NO FAULT DISPLAYED.SDR ASAA2020021032097Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL TRANSITION BETWEEN STA 727D - 727J HASCORROSION IN NUMEROUS AREAS. GROUNDED - YES. REPAIRED AFT PIT L/H TRANSITION PANEL TRANSITION BETWEEN STA 727D-727J IAWB737-800 SRM 53-00-53. CORROSION OUT OF LIMITS ORIGINAL THICKNESS .040 REMSDR ASAA2020021032100Skin · crackedCRACK FOUND R/H HORIZ. STAB LOWER SKIN: STAB STA. 129.50 I/B OF FASTENER ROW AT 17" AFT OF L/E. MARKED 1.020"L. GROUNDED - YES. DAMAGE CUTOUT AND REPAIRED ON R/H HOIRZ STAB LOWER SKIN AT APPROX STAB STA 129.50 AT 17" AFT OF LEADING EDGE IAW B737-800 SRM 51-40-SDR ASAA2020020782077Bulb · failedEMERGENCY LIGHT AT SEAT 12DEF INOP. GROUNDED - YES. RELAMPED SEAT 12 DEF EMERGENCY LIGHT TEST GOOD PER B737-800 AMM33-51-03-960-801.NOTE: DUPLICATED. SDR ALREADY SUBMITTED TO FAA ON 2/03/2020. MIG-23A EMAILED TO RELIABILITY DEPT BY ANDREW SCHOMPERT (HAECO)SDR ASAA202002032063Bulb · inoperativeEMERGENCY LIGHT AT SEAT 12DEF INOP. GROUNDED - YES. RELAMPED SEAT 12DEF EMERGENCY LIGHT, TEST GOOD IAW B737-800 AMM 33-51-03-960-801SDR ASAA2020021827199Wire Harness · failedAPU CT5ATP EGT HAS SHIFTED ABOVE THE 593 DEGREE THRESHOLD AND REMAINS ABOVE THE 605 THRESHOLD. GROUNDED - YES. REPLACED BRANCHED APU HARNESS AND PERFORMED OPS CHECKS; CHECKS GOOD ON CARD #G1350537. PERFORMED WIRING RESISTANCE CHECKS IAW B737-800 FIM 49-70 TASSDR ASAA2019121091557Blade · damagedDURING ACCOMPLISHMENT OF NR 1 ENG HPT BLADES FOR EGT EXCEEDANCE BOROSCOPE, FOUND EVIDENCE OF MELTING TO THE TRAILING EDGE ON 1 HPT BLADE IN AREA B. GROUNDED - YES. REMOVED & REPLACED NR 1 ENGINE IAW TASK CARDS 78471000, 78471001 UNDER W/O 1014088. PERFORMED NSDR ASAA2019112643444Smoke Detector · false activationAT FL280 AFT LAV SMOKE DETECTOR SOUNDED WITH NO OTHER INDICATIONS OF FIRE. A/C AFT LEFT FORWARD LAV. GROUNDED - YES. DIVERSION TIME 25 MINUTES - REMOVED AND REPLACED LEFT AFT FWD LAV SMOKE DETECTOR IAW B737-800 AMM 26-14-01/401. SMOKE DETECTOR INSTALLATION TESSDR ASAA201911251429Fmc · malfunctionedPILOT REPORTS LEFT FMC WOULD NOT LOAD PERFORMANCE FIGURES. GROUNDED - YES. ACCOMPLISHED BITE OF BOTH FMC'S REF B737-800 FIM 34-61 TASK 801 ON GND & FLT 1 L FMC HAD FAULT, ACCOMPLISHED SENSOR TEST ALL FMC SENSORS STATUS GOOD. ACCOMPLISHED RESET OPENED RESET P18SDR ASAA2019112531426Transceiver · failedHF1 ABLE TO RECEIVE SELCAL AND VOICE BUT APPEARS UNABLE TO TRANSMIT. WE DID HEAR TONE WHEN TUNING, HF 2 WORKS FINE,. GROUNDED - YES. REMOVED & REPLACED #1 HF TRANSCEIVER B737-800 AMM 23-11-21 PULLED & RESET 1 ASSOCIATED C.B. OPS CHECK NORMAL.SDR ASAA2019100863956Switch · intermittentV/S MODE ON MCP THUMBWHEEL SWITCH OCCASIONALLY UNRESPONSIVE. GROUNDED - YES. VERIFIED, REMOVED & REPLACED MCP REF B737-800 AMM 22-11-34. INSTALLATION & LLM TEST PASSED.SDR ASAA2019100293869Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL ENGAGE, BUT DISENGAGES AFTER ABOUT 3 SECS, ANY MODE, EITHER AUTOPILOT ENGAGED OR NO A/P ENGAGED. GROUNDED - YES. REF B737-800 FIM 22-31 TASK 801 A/T BITE PROC., FOUND ASM-1 FAIL ON DISCREPANCY FLIGHT IN FAULT REVIEW. #1 THROTTLE WON'T MOVE DUSDR ASAA2019092530821Unknown · malfunctionedHF#1 RADIO DOES NOT TRANSMIT. GROUNDED - YES. PERFORMED FIM 23-11 TASK 806, USED HF FREQ 50547. NO FAULTS NOTED.SDR ASAA2019091430693Unknown · malfunctionedCONT CAB ZONE TEMP LIGHT ILLUMINATES-RESETS WITH MASTER CAUTION. GROUNDED - YES. INTERROGATED LEFT AND RIGHT PACK ZONE TEMP CONTROLLERS. RIGHT PZTC "FLIGHT DECK TRIM VALVE" FAULT. BITE TEST PASSED. UNABLE TO DUPLICATE WITH APU. 115V AT PLUG D3886 ON THE CONTROSDR ASAA2019090430616Skin · corrodedCORROSION AROUND LAV VENT OPENING. GROUNDED - YES. REPAIRED SKIN IAW SRM 53-70-01-2R-3. THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 50,000 CYCLES, A/C CYCLES AT TIME OF REPAIR 14,913W-1"O-.125"R-0.0L-1"D-.125".SDR ASAA2019082930581Unknown · malfunctionedA/P DISCONNECT WARNING INOP. GROUNDED - YES. REF FIM 22-12 TASK 817, AMM 20-60-01. FOUND (1) C/B. OPEN (AURAL WARNING). RESET C/B AND ACCOMPLISHED INSPECTIONS FOR C/B RESET. NO DEFECTS. ACCOMPLISHED LIBRARY # 62 DISENG WARN TEST AND LAND VERIFY TEST REF 22-11-SDR ASAA2019082030431Warning Message · false activationAT TOP OF DESCENT PRESSING MASTER RECALL, GOT CONT CABIN "ZONE TEMP": LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. TEMP LINE CONTROLLABLE. GROUNDED - YES. PERFORMED B737-800 FIM 21-62 TASK 801. L/H ZONE TEMP CONTROLLER TESTED GOOD. R/H ZONE TEMP CONTROLLER GOSDR ASAA2019080643318Fmc · malfunctionedENROUTE AT FL 330. FMC MESSAGE & VTK DISPLAYED ON CAPTAINS MAP. CAPTAINS MCDU MENU PAGE MISSING FMC. AUTOPILOT A WAS SELECTED AT THE TIME. LNAV/VNAV DISENGAGED. APPROXIMATELY 2 MINUTES LATER LEFT FMC RESTORED. LNAV/VNAV RE-ENGAGED. OPERATIONS NORMAL. GROUNDSDR ASAA2019080133258Hf Comm · malfunctionedNR 1 HF TRANSMIT IS INOPERATIVE. CAN HEAR SIDETONE WHEN TRYING TO TRANSMIT BUT SFO RADIO CAN'T HEAR YOU. GROUNDED - YES. ACCOMPLISHED HF-1 COMMUNICATION OPERATIONAL TEST REF B737-800 AMM 23-11-00 TEST PASSED. COMMUNICATIONS WITH SFO WITH AC ON GROUND REPORTED SDR ASAA2019072230142Ignition Lead · wornAPU IGNITOR PLUG LEAD WORN. GROUNDED - YES. REMOVED AND REPLACED APU IGNITOR PLUG LEAD IAW AMM TASK 49-41-52/401. APU START AND RUN OPS CHECK GOOD.SDR ASAA2019053029541Exciter · failedDURING #1 ENG START, AFTER START LEVER TO IDLE, NO LIGHT OFF NO INCREASE IN EGT, ABORTED START. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE L/H EXCITER BOX REF B737-800 AMM 74-11-01. PERFORMED SNAP CHECK, SNAP CHECK SUCCESSFUL REF AMM 74-00-00. ATTEMPTED TOSDR ASAA2019052129437Control Valve · faultedLEFT PACK ILLUMINATES WITH MASTER CAUTION RECALL AND EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. PERFORMED PACK ZONE TEMP CONTROLLER BITE PER AMM 21-61-00 #1 CONTROLLER FAULTED LT PACK TEMP CONTROL VALVE (TCV). REMOVED LT PACK TCV PER AMM 21-51-10-00SDR ASAA2019022228330Nut Plate · corrodedNR 1 ENGINE HAS ONE CORRODED NUTPLATE ON FAN FRAME, LOCATED AT 6:00 POSITION. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019022228332Grommet · migratedWHILE ACCOMPLISHING TASK CARD NR 1 ENGINE FOUND GROMMET MIGRATING CAUSING CUT INSULATION ON WIRE AT THE THEMO ANTI ICE VALVE SOLENOID. GROUNDED - YES. THE DAMAGE REFERENCED ABOVE IS CONTAINED WITHIN THE ENGINE COWL TAI VALVE. LRU REQUIRES REPLACEMENT. REMOVED SDR ASAA201902258323Link · looseWHILE ACCOMPLISHING TASK CARD #1 ENGINE FOUND FWD SUPPORT LINK ON INTERSECTION MANIFOLD DUCT LOOSE. GROUNDED - YES. REMOVED AND REPLACED #1 ENG INTERSECTION MANIFOLD DUCT PER B737-800 AMM 36-11-01/401. PERFORMED LEAK CHECK ON #1 ENG INTERSECTION MANIFOLD DUCT SDR ASAA2019013028023Turbine Blades · burnedWHILE ACCOMPLISHED TASK CARD ON NR 2 ENG. FOUND TRAILING EDGE OF THE HPT BLADES BURNING ( 8 BLADES). GROUNDED - YES. REMOVE AND REPLACE ENGINE NR 2.SDR ASAA2019012127892Unknown · malfunctionedON PERFORMING AUTO LAND HGS, AUTO LAND PORTION UNSUCCESSFUL. AIRPLANE DRIFTED WELL OUTSIDE OF TOLERANCES TO THE LEFT APPROX 50 FEET, DISCONNECTED AUTO PILOT AND LANDED HGS PORTION APPEARED SUCCESSFUL. GROUNDED - YES. ACCOMPLISHED MAINT PRACTICE FOR LLM SPECIALSDR ASAA2018122617533Exciter · inoperativeON ENGINE START #1 ENGINE WOULD NOT START WITH IGN SWITCH IN IGN R. ENGINE STARTED NORMALLY IN IGN L POSITION. GROUNDED - YES. FOUND R IGNITION EXCITER INOP ON #1 ENGINE. REMOVED AND REPLACED R IGNITION EXCITER PER B737-800 AMM 74-11-01 IGNITION SYSTEM AUDIBLESDR ASAA2018121427380Compensator · out of limitsTECH SERVICE REQUEST. CHECK FQIS SYSTEM IN THE LEFT TANK TO PREVENT POTENTIAL INCORRECT FUEL QTY READINGS. GROUNDED - YES. PERFORMED TANK AND COMPENSATOR UNITS TEST REF B737-800 AMM 28-41-21-710-801. FOUND COMPENSATOR PROBE F15L, TANK PROBES F6L AND F10L OUT OSDR ASAA2018121427379Valve · out of adjustTECH SERVICE REQUEST. FOLLOW-UP TO REPORTS OF FUEL IMBALANCE. GROUNDED - YES. ACCOMPLISHED CROSSFEED VALVE FUNCTIONAL CHECK, FOUND FUEL TRANSFERRING. ACCOMPLISHED CROSSFEED VALVE ALIGNMENT, REF B737-800 AMM TASK 28-22-21-820-801. REPEATED FUNCTIONAL CHECK NO FSDR ASAA2018111636865Satcom · malfunctionedSATCOM CALLS UNSUCCESSFUL- CALLS DIAL AND ARE ANSWERED BUT NOTHING IS HEARD ON THE AIRCRAFT END ON SAT 1 OR SAT 2. GROUNDED - YES. T/S SATCOM SYSTEM B737-800 AMM 23-15-00/601 AND 23-27-00-730, B737-800 FIM 23-15 TASK 801. NO HISTORY 30 DAYS. OK FOR SERVICE.SDR ASAA2018110966752Warning Message · illuminatedL-2 WINDOW OVERHEAT IN CRUISE, RAN QRH. NO SUCCESS. GROUNDED - YES. REMOVED AND REPLACED L2 SLIDING WINDOW REF B737-800 AMM 56-12-11. OPS AND LEAK CHECK GOOD. THIS CLEARS MEL 30-11E. REMOVED CN 06043560. RETAPPED NEW WINDOW CODE H15 TO TERMINAL #2 REF. WDM 30-SDR ASAA2018110226716Wire · damagedL SIDE WINDOW OVERHEAT LIGHT ILLUMINATED DURING CRUISE. FOLLOWED QRH PROCEDURE, ALLOWING COOL DOWN TIME. FAILURE MODE REPEATED. GROUNDED - YES. ON THE LEFT SIDE WINDOW HEAT HARNESS FOUND DAMAGED WIRE. INSTALLED 2 EA SENSOR WIRING APS ON CAPT'S SLIDER WINDOW PESDR ASAA2018102126557Start Valve · stuckON ENGINE NR 2 START. START VALVE OPEN LIGHT DOES NOT ILLUMINATE. GROUNDED - YES. MANUALLY OPENED START VALVE, ENGINE NR 2 STARTED NR 2. REMOVED & REPLACED NR 2 ENG START VALVE ASSY REF AMM 80-11-03. OPS CK NR 2 ENG REF AMM 71-00-00. OPS CK'S NORMAL. SUCCESSFU
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