N568AS
Service difficulty reports · 479
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 = 'N568AS' 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 = 'N568AS' 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 ASAA2013122112187Warning Light · false activationCONT CABIN ZONE, TEMP LIGHT ILLUMINATED ON RECALL BUT RESETS SYSTEM APPEARS TO OPERATE NORMALLY. ACFT GROUNDED. PERFORMED FIM 21-62/832. NO FAULTS FOUND. INTERMITTENT FAULT. NO HISTORY 60 DAYS.SDR ASAA2013121096710Lens · detachedMID CABIN EXIT SIGN LENS DETACHED. ACFT GROUNDED. REATTACHED MID CABIN EXIT LIGHT LENS COVER TO FIXTURE.SDR ASAA2013110196276Warning Light · false activationFMC DISAGREE ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. ALL CHECKED GOOD.SDR ASAA2013100996147Probe · malfunctionedANTI-ICE LIGHT ON MASTER CAUTION KEEPS COMING ON. TAT WAS SHOWING 99C THEN BACK TO 12C GROUNDED. ACFT EQUIPED WITH AUTO FUNCTION ON ANTI-ICE PANEL, HEATER FOR TAT PROBE WAS ON AT GATE. AFTER PROBE COOLED. RAN TAT PROBE CHECK REF 34-21, TASK 813 & ADIRU BITSDR ASAA2013091695990Warning Message · false activationFMC DISAGREE MESSAGE CAME ON AFTER ENGINE START. ACFT GROUNDED. RAN QRH PROCEDURES AND FMC DISAGREE MESSAGE NO LONGER DISPLAYED.SDR ASAA2013091195950Warning Light · illuminatedAUTO FAIL AND ALTITUDE LIGHTS ILLUMINATED ON PRESSURE CONT PANEL. ACFT GROUNDED. NR 2 CABIN PRESSURE CONTROLLER WITH SELECTOR PANEL LRU FAIL CODE 101, IAW FIM 21-31, TASK 827. FAULT ISOLATION IAW FIM 21-31, TASK 803 RESULTS IN NO FAULT CODES, NO FURTHER MXSDR ASAA2013091195949Warning Light · illuminatedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATES ON RECALL, RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. VERIFIED CONTROL CABIN ZONE TEMP ANNUNCIATOR ILLUMINATOR ON RECALL. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST FOUND FLT DECK TRIM VALVE FAULT LT ON NR 2SDR ASAA2013090995940Valve · failedDURING CLIMB NR 2 ENGINE AMBER TAI LIGHT ILLUMINATED FOR APPROX 10 SECONDS. LIGHT WENT OFF FOR APPROX 5 SECONDS THEN ILLUMINATED FOR 5 SECONDS. ENGINE ANTI ICE WAS OFF ENTIRE TIME DURING CLIMB. ACFT GROUNDED. REPLACED NR 2 ENG COWL TAI VALVE IAW MM 30-21-1SDR ASAA2013090995939Valve · openNR 1 COWL ANTI-ICE VALVE & WING CTL FOUND OPEN. ENG NR 2 ANTI-ICE & RAIN CTL (C149) FOUND OPEN. ACFT GROUNDED. INSPECTED WIRING AT P18-3 & NR 1 ENG VALVE ANTI-ICE. NO DEFECTS NOTED. ALSO INSPECTED AT P5-11. NO DEFECTS NOTED. RESET C/BS ENG NR 1 COWL ANTI-SDR ASAA2013090495923Charger · inoperativeON ARRIVAL, FOUND ELEC LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED MAINT BITE TEST, FOUND AUX BATTERY CHARGER INOP FAULT. REPLACED AUX BATTERY CHARGER. REF MM 24-31-31. OPS CHECK NORMAL. REF MM 24-31-21-710-801.SDR ASAA2013083195907Warning Light · intermittentON LANDING, LIGHT ON OVERHEAD ILLUMINATED. ACFT GROUNDED. PERFORMED BITE FOUND AUX BATTERY CHARGER INOP MAINT MESSAGE AND LIGHT ON. CLEARED MAINT MESSAGE IAW FIM 24-31 TASK 801. IAW FIM 24-31, TASK 825. FAULT CLEARED AND TWO INDICATOR LIGHTS ON THE FRONSDR ASAA2013070995534Fmc · false indicationFMC DISAGREE ON TAXI. COMPLETED CHECK LIST ITEMS, VERIFIED INFO MESSAGE NO LONGER DISPLAYED. ACFT GROUNDED. COMPLETED CHECK LIST ITEMS, VERIFIED MESSAGE NO LONGER DISPLAYED.SDR ASAA2013070895500Radio · malfunctionedNR 1 HF RADIO AUDIO GARBLED, UNINTELLIGIBLE. SWITCHED TO HF 2 AND ON SAME FREQUENCIES THAT HAD BEEN IN USE ON HF 1, NORMAL COMMUNICATION QUALITY RESUMED. ACFT GROUNDED. ACCOMPLISHED HF COMMUNICATION SYS BITE PROCEDURE REF FIM 23-11/801, OPS CHECKED GOOD. GSDR ASAA2013061595099Warning Light · false activationDURING CRUISE FLIGHT, THE N1 LIMIT DISPLAY ON THE UPPER DU CHANGED TO A/T LIM. BOTH EECS REMAIN ON. ACFT GROUNDED. PERFORMED FIM 22-32, TASK 812 A/T BITE LEG 1 SHOWED EEC 2A/2B FAULT. PERFORMED EEC BITE IAW FIM 73-00, TASK 801, NO CURRENT FAULTS NO HISTORYSDR ASAA2013061095064Key Pad · damagedFOS CDU TYPE PAD LETTER G INOPERATIVE. ACFT GROUNDED. FIRST OFFICERS MCDU KEYPAD TESTED IAW TASK 34-61-01 AND ALL LETTERS AND NRS OPS/CHECK GOOD. TEST THE KEYPAD LETTER G SEVERAL TIMES AND OPS TEST GOOD.SDR ASAA2013053194940Acm · unsecurePASSING 17000 FT FLIGHT DECK AMBIENT TEMP BECAME VERY HOT. LEFT PACK SELECTED AND TEMPERATURE NOTED, PEGGED AT 100C PACK TEMP COULD NEVER BE CONTROLLED. AT 10,000 FEET, LT PACK WAS SHUTDOWN. NO LIGHT ANNUNCIATED, PACK DID NOT TRIP. ACFT GROUNDED. PERFORM FSDR ASAA2013053094939Actuator · failedRIGHT PACK LIGHT ILLUMINATES ON RECALL. ACFT GROUNDED. R & R RT AIR INLET RAM DOOR ACTUATOR IAW AMM 21-51-21-000-801 FOR REMOVAL AND AMM 21-51-21-400-801 FOR INSTALLATION. OPS TEST GOOD, NO FAULTS WAS NOTED ON RT ZONE TEMP CONTROLLER.SDR ASAA2013052994930Warning Light · false indicationAFTER LANDING, RT PACK LIGHT ILLUMINATED. ACFT GROUNDED. REFRORMED FIM 21-62, TASK 801- ZONE TEMP CONTROLLER BITE TEST. INTERROGATED BOTH NR 2 & NR 1 ZONE TEMP CONTOLLERS NO FAULTS FOUND. INSPECTED VALVES IN RT AC BAY- ALL CONNECTOR PLUGS SECURE & VALVES RSDR ASAA2013052894935Transceiver · malfunctionedNO SAT PROMT ON LINE 4L ON SAT COM NOT AVAILABLE FOR USE PROMT WAS RESENT DURING PREFLIGHT. ACFT GROUNDED. R & R SDU. OPS CHECKED GOOD.SDR ASAA2013052794912Warning Light · illuminatedRIGHT PACK LIGHT ILLUMINATED ON RECALL DURING LANDING CHECK. ACFT GROUNDED. ACCOMPLISHED PACK/ZONE TEMP CONTROLLER BITE TEST ON RT CONTROLLER REF MM 21-61-00. FOUND NO FAULT LOGGED. RT PACK OPS CK NORMAL REF MM 21-61-00. NO HISTORY PAST 60 DAYS.SDR ASAA2013052594899Pump · leakingNR 2 ENGINE DRIVEN HYD PUMP LEAKING. ACFT GROUNDED. R & R NR 2 EDP AND PRESSURE LINE IAW AMM 29-11-11. LEAK AND OPS CK GOOD IAW AMM 29-11-11.SDR ASAA2013052194866Control Panel · failedAUTOPILOT B WILL NOT ENGAGE. ACFT GROUNDED. REMOVED MODE CONTROL PANEL IAW AMM 22-11-34-000-801. INSTALLED MODE CONTROL PANEL IAW B737-800 AMM 22-11-34-400-801. ACCOMPLISHED OPS CHECK IAW AMM 22-11-34-740-801. OPS CHECK GOOD.SDR ASAA2013050794793Seat Track · crackedBS 727B, RBL 24 SEAT TRACK ATTACH HOLE CRACKED. ACFT GROUNDED. REAMED HOLE TO .247 IAW SB 757-53-1296-NG-1. ACCOMPLISHED NEC INSP IAW NDT M PT6 51-00-00, NO CRACKS FOUND.SDR ASAA2013050694882Skin · dentedFUSELAGE SKIN DENTED BS 807, BL0. ACFT GROUNDED. FABRICATED AND INSTALLED REPAIR IAW EA 800-53EA-10392, REV, REW 05-22-2013 REO-G16251, REV A.SDR ASAA2013050694847Seat Track · wornBS 520, LBL24, SEAT TRACK IS WORN ON UPPER SURFACE. ACFT GROUNDED. R & R DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-1A-1, SRM 53-00-52-2R-4, SRM 51-20-01, SRM 51-40-02, SOPM 20-43-01, REV 014 AND SOPM 20-41-04.SDR ASAA2013050694846Seat Track · wornBS 520, LBL45 SEAT TRACK IS WORN ON UPPER SURFACE. ACFT GROUNDED. R & R DAMAGED SEAT TRACK SECTION IAW SRM 53-00-53-1A-1, SRM 53-00-52-2R-4, SRM 51-20-01, SRM 51-40-02, SOPM 20-43-01, REV 014 SOPM 20-41-04 AND SRM 51-40-02.SDR ASAA2013050694845Seat Track · wornCABIN STA 520, RBL45 SEAT TRACK IS WORN ON UPPER SURFACE. ACFT GROUNDED. R & R DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-2R-4, SRM 51-20-01, SOPM 20-43-01, REV 014 SOPM 20-41-04.SDR ASAA2013050694834Seat Track · wornBS 520, RBL 24, SEAT TRACK IS WORN ON UPPER SURFACE. ACFT GROUNDED. R & R DAMAGED SEAT TRACK SECTION IAW SRM 53-00-52-1A-1, SRM 53-00-52-2R-4, SRM 51-20-01, SOPM 20-43-01, REV 014 AND SOPM 20-41-04.SDR ASAA2013050594791Web · corrodedMAIN CABIN FLOOR RT SIDE BS 986, BL 45 WEB HAS LIGHT CORROSION AROUND FASTENER HOLES. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-70-51-1A-1. ORIGINAL MATERIAL THICKNESS IS .1500, REMOVED .0030, .1470 MATERIAL REMAINING IS FOUND TO BE WITHIN LIMITS, APPLIED SDR ASAA2013041794525Selector Panel · malfunctionedLEFT MOST DIGIT ON MCP HEADING SELECT DISPLAY IS ALMOST INVISIBLE FROM F/O SEAT. REPLACED MCP REF MM 22-11-34. OPS CHECK NORMAL. ACCOMPLISHED MCP LWMP CHECKS REF CHECKLIST MM 22-00-01, ALL TEST PASSED. ACFT REMAINS CAT III A AUTOLAND & HGS. VERIFIED STATUSSDR ASAA2013040694355Switch · failedAFTER LANDING, ENGINE CAUTION & NR 2 REVERSER LIGHT ON OVERHEAD ILLUMINATED FOR 2 MINUTES, WENT OUT PROIR TO SHUTDOWN. VERIFIED S5 HAS HIGH RESISTANCE IN THE DEPLOYED POSITION. 2.5 OHMS. IAW W/D 78-34-21. REQS SWITCHPACK. REPLACED AUTO THROTTLE SWITCH PACK. OSDR ASAA2013033094296Fmc · malfunctionedAFTER ENGINE START HAD FMC DISAGREE. RAN QRH PROCEDURE, FMC CAME BACK ONLINE BUT WITH SINGLE FMC WARNING RETURNED TO GATE. AS WE PULLED INTO GATE SINGLE FMC WARNING EXTINGUISHED. INFO NOTED CREW RAN QRH SUCCESSFULLY. NO HISTORY 90 DAYS. NO MX REQ REF FIM SDR ASAA2013032894286Control Valve · inoperativeLT A/C PACK LIGHT ON WITH MASTER CAUTION RECALL. LIGHT GOES OUT WITH MASTER CAUTION RESET. VERIFIED TCV DOESNT MOVE DURING BITE. R & R LT PACK TCV. OPS CK NORMAL REF MM 21-51-10.SDR ASAA2013031394158Warning Light · false activationLEFT PACK LIGHT ON RECALL ON (UNREADABLE) EXTINGUISHES WITH MASTER CAUTION RESET. ACCOMPLISHED PACK/ZONE TEMPERATURE CONTROL BITE TEST, CLEARED FAULTS, OPS NORMAL REF MM 21-61-00-700-806-002. NO HISTORY LAST 60 DAYS.SDR ASAA2013030194038Warning Light · false activationRIGHT WINDOW OVERHEAT, RAN QRH PROCEDURE AND OVERHEAT LIGHT ILLUMINATED AGAIN. TURNED OFF SWITCH REMAINDER OF FLIGHT. PERFORMED BITE CHECK OF WINDOW HEAT CONTROL UNIT, NO FAULT FOUND. PERFORMED OPS TEST IAW AMM 30-41-TASK 801, GROUND VERIFICATION CHECK GOOD.SDR ASAA2013020593829Filter · cloggedCONT CABIN ZONE TEMP LIGHT ILLUMINATES ON MASTER CAUTION RECALL. REPLACED FLIGHT COMPARTMENT ZONE - CABIN TEMP SENSOR FILTER REF AMM 21-61-06-400-801. PERFORMED PACK/ZONE TEMP CONTROLLER BITE CHECK, CHECKS GOOD REF FIM 21-62, TASK 801.SDR ASAA2013013193802Valve · failedA/C DUCT PRESSURE DIFF AT CRUISE RT 15 PSI (STEADY) LT 35-40 PSI (FLUCTUATING) FL 360. RT ENGINE PRECOOLER CONTROL VALVE FAILED STEP F.(5) (C) OF FIM TASK 36-10, TASK 810. ACCOMPLISHED QUICK FIM TASK 36-10 TASK 810. R & R NR 2 ENG PRE COOLER CONTROL VALVE RSDR ASAA2013011393682Brake Assy · shortedLEFT ENGINE VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE. LT ENGINE INDICATIONS NORMAL TROUGHOUT, LIGHT WENT OUT. CAME BACK ON, REMAINED ON THROUGH DECENT, LANDING AND TAXI TO GATE. DISCONNECTED D626 AND HMU DP1207, READ PIN 12, D626 TO GROUND, OPEN CIRCUIT TSDR ASAA2013011393670Relay · inoperativeLOW PRESSURE LIGHT FOR THE CENTER TANK LT FUEL PUMP FAILS TO COME ON. REF T/C 78128006, PARA. D. (9)-(11). FOUND R936 RELAY BAD. REPLACED R936 REF WDM 28-23-11. NOW T/CS 78128006 AND 78128007, OPS NML.SDR ASAA2012123093579Autoland Sys · malfunctionedAUTOLAND FAILED - FLAIR WOULD NOT ARM. ACCOMPLISHED DFCS FAULT REVIEW BG 20 FOR 30DEC12. NO RELEVANT FLIGHT LEG FAULTS AND ALL FAULT LRU TESTS PASS 20.01, 20.18, 20.24. ALSO ACCOMPLISHED LAND VERIFY BG 49. ALL TESTS PASS.SDR ASAA2012122993564Control Valve · faultedLEFT PACK LIGHT ILLUMINATES ON RECALL. LT ZONE CONT, LOGGED TCV FAULT. ACCOMP FIM 21-62 801, FAULT CLEARED & TESTS NORMAL.SDR ASAA2012122993560Control Valve · faultedLEFT PACK LIGHT ILLUNIMATED ON RECALL. EXTINGUISHED WITH RESET. ACCOMPLISHED PACK/ ZONE TEMP CONTROLLER BITE M1442, FIM 21-62, 801. MESSAGE FAULT TCV. R & R LEFT TEMP CONTROL VALVE IAW MM 21-51-10-400-801. OPS AND LEAK CHECKED GOOD.SDR ASAA2012122893576Warning Light · malfunctionedDURING NR 1 ENGINE START SEQUENCE, BLUE ENGINE VALVE CLOSED LIGHT REMAINED ILLUMINATED LONGER THAN NORMALLY OBSERVED. FUEL FLOW AND EGT RISE OCCURRED WITH LIGHT. LIGHT EXTINGUISHED. ALL INDICATIONS NORMAL. OP AND LEAK CHECKED NR 1 ENGINE HPSOV VALVE REF SDR ASAA2012122193512Keyboard · inoperativeCAPTAINS CDU LIGHT RHEOSTAT DIMMER SWITCH IS NOT ADJUSTING THE LIGHT PROPERLY. R & R FMC CDU KEYBOARD, OPS NORMAL REF MM 34-61-01-400-801.SDR ASAA2012120393403Cdu · failedCOCKPIT CDU FAIL DURING BUS TRANSFER. ACFT GROUNDED. DUPLICATED. REPLACED LT FMCS MCDU REF MM34-61-01, OPS CK NORMAL & S/W CK OK.SDR ASAA2012120293394Control Valve · malfunctionedRIGHT PACK LIGHT CAME ON DURING FLIGHT WENT OUT ON MASTER CAUTION RECALL. NR 2 A/C PACK CONTROLLER LOGGED TCV FAULT. ACCOMPLISHED TEST AND RESET WITH NO CURRENT FAULTS REF CONTROLLER BITE 21-62-801.SDR ASAA2012112893382Panel · damagedWHILE ACCOMPLISHING ENGINE FAN BLADE INSPECTION ON NR 2 ENGINE, FOUND NR 6 FAN DUCT PANEL WITH A PULLED THRU FASTENER, REF AMM 72-23-07. ACFT GROUNDED. R & R NR 6 FAN DUCT PANEL REF AMM 72-23-07.SDR ASAA2012102693194Fmc · unknownCAPTAIN`S FMC FAIL LIGHT ILLUMINATED. THE SCREEN IS BLANK. UNABLE TO DUPLICATE, PERFORMED FMC CDU INSTALLATION TEST REF MM 34-61-400-802. OPS NORMAL. NO HISTORY PAST 90 DAYS.SDR ASAA2012101393108Computer · failedAFTER SOFTWARE LOAD FCC A SHOWS CH A UNAVAILABLE DURING DFCS BITE. R & R FCC A COMPUTER, REF MM 22-11-33-400-801-8, C/B OPEN & CLOSED OPS NORMAL. REF LOG 7061279 FOR LWMP TESTING & CAT STATUS. PART VERIFIED SEAM C.SDR ASAA2012100893080Indicator · activatedDURING PDC WALK AROUND, FOUND NR 2 ENGINE IDG DELTA P INDICATOR EXTENDED. ACFT GROUNDED. ON ENGINE NR 2 IDG DRAINED OIL, REMOVED SCAVENGE FILTER, INSPECTED, NO METAL PARTICLES OR CONTAMINATION FOUND. REPLACED FILTER AND SERVICED OIL IAW AMM 24-11-41-200-80
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