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 ASAA2023012541625Floorboard · damagedFWD WET AREA FLOORBOARD PNL PN:141A5810-236 DAMAGED HAS CORRODED INSERTS AND DAMAGED SURFACE FIBERS. GROUNDED - YES. REPAIRED FWD WET AREA FLOOROARD P/N 141A5810-236 BY REMOVING 19EA DAMAGED INSERTS AND DAMAGED UPPER SKIN PLIES AND PERFORMING WET LAY UP REPAIRSDR ASAA2023012514624Floorboard · damagedFWD WET AREA FLOORBOARD PNL PN:141A5810-155 DAMAGED CORRODED INSERTS, DAMAGED SURFACE FIBERS. GROUNDED - YES. REPAIRED DAMAGES ON FWD WET AREA FLOORBOARDS PNL PN: 141A5810-155, REPAIRED DAMAGED SURFACE FIBERS AND REPLACED CORRODED INSERTSIAW B737-800 SRM 53-00SDR ASAA2023012514623Floorboard · damagedFWD WET AREA FLOORBOARD PNL PN: 141A5810-175 DAMAGED HAS CORRODED INSERTS AND BROKEN OFF TAB. GROUNDED - YES. REPAIRED FWD WET AREA FLOORBOARD PANEL PN: 141A5810-175 HAS CORRODED INSERTS AND BROKEN OFF TAB IAW ASA B7737 SRM 50-00-2R-0 & 53-00-50-2R-6.SDR ASAA2023011041622Pan · gougedR1 DOOR OUTER HANDLE PAN GOUGED AT EDGE OF BORE. GROUNDED - YES. REMOVE & REPLACED HANDLE PAN REF B737-800 SRM 51-40-02 & BAC DWG 141A6516 REF - & B737-800 SRM 52-10-02-1A-2 PARA 4.D.(3).SDR ASAA2023011801544Shield · crackedFWD CARGO DOOR CUTOUT APPRX. STA.494 AT S-26R, TRANSITION PANEL CRACKED AS MARKED. GROUNDED - YES. EVALUATED SHEILD AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVENREMOVED OLD SHEILD, LOCATED AND DRILLED NEW SHEILD P/N 143A8126Y29PO 1047115.3 AND INSTALLEDSDR ASAA2022123041860Compensator · out of rangeFUEL IMBALANCE OF 800 LBS GREATER ON RIGHT SIDE DURING CRUISE. FLIGHT FOLLOWED QRH PROCEDURES REBALANCED FUEL. FUEL STAYED BALANCED WITHIN LIMITS FOR REMAINDER OF FLIGHT. GROUNDED - YES. PERFORMED TANK COMPENSATOR UNITS RESISTANCE AND CAPACITANCE TEST IAW ASA SDR ASAA2022122941305Warning Message · false activationCONT CAB ZONE TEMP LIGHT ILLUMINATES ON MASTER RECALL. LIGHT EXTINGUISHES ON MASTER CAUTION RESET. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE PROCEDURE ON #1 & 2 PACK /ZONE TEMP CONTROLLER. PER B737-800 FIM 21-62. FOUND FAULT ON ZONE TEMP CONTROLLER 2 "FSDR ASAA2022122041229Transceiver · faultedHF 1 ACTIVE AND STBY SHOW FAIL ON BOTH COMM HEADS. GROUNDED - YES. REMOVED AND INSTALLED NEW #1 HF TRANSCEIVER PER B737-800 AMM 23-11-21/401, OPS NORMAL. NFF. GROUND VERIFICATION SUCCESSFUL. ORIG SUBMISSION DATE: 12/27/2022SDR ASAA2022122091189Radio · failedHF #1 RADIO FAILED HF #2 OPS NORMAL. GROUNDED - YES. CONTROL PANEL SHOWS FAIL MSG FOR #1 HF. PERFORMED B737-800 FIM 23-11 TASK 801 AND BITE CK PASSED. FAIL MSG EXTINGUISHED, PERFORMED OPERATIONAL CK OF BOTH #1 AND #2 HF SYSTEMS AND OPS TEST PASSED GROUND FUNCTSDR ASAA2022112940962Sign · brokenEMERGENCY LIGHT EXIT SIGN ABOVE RIGHT AFT OVERWING EXIT HAS BROKEN LENS RETAINER. GROUNDED - YES. REF B737-800 WDM 33-51-13-106 - REMOVED, REPLACED, AND TESTED EXIT SIGN L1365 PER B737-800 AMM 33-51-01-960-802 - OPS NORMAL.SDR ASAA2022110840760Sensor · faultedENG #2 FAULT CODE 75-20802 T25 SIGNALS DISAGREE SHORT TIME FAULT. GROUNDED - YES. REMOVED & REPLACED PT25 SENSOR REFB737-800 AMM 73-21-02 OPS CHECK GOOD.SDR ASAA2022110740682Warning Light · illuminatedCONT CAB ZONE TEMP LIGHT ILLUMINATED AFTER PUSHBACK. GROUNDED - YES. PERFORMED PZTC BITE FLIGHT DECK TRIM FAULT FOR #1 CONTROLLER. ACCOMPLISHED B737-800 FIM 21-62. RESET AND PERFORMED BITE TEST, NO FAULTS FOUND. #1 AND #2 CONTROLLER PZTC BITE TEST PASSED.SDR ASAA2022110540633Modulating Valve · faultedZONE TEMP ILLUMINATES ON RECALL EXTINGUISHES W/ MASTER RESET. GROUNDED - YES. ACCOMPLISHED PZTC BITE AND HAD FLIGHT DECK TRIM VALVE FAULT. ACCOMPLISHED B737-800 FIM 21-62 TASK 832 AND FOUND TCV "V00143" INOP. REMOVED AND REPLACED TCV "V00143" REF B737-800 AMM SDR ASAA2022102440458Coupler · damagedHF #2 DOES NOT TRANSMIT BUT RECEIVES OK. GROUNDED - YES. REPLACED #2 HF COUPLER, REF B737-800 AMM 23-11-61. NR 2 HF RADIO OPS CHECK GOOD IAW AMM 23-11-61.SDR ASAA2022102440461Dfgs · inoperativeSECTION OF CAPT SIDE GLARESHIELD BACK LIGHTING, INCLUDING F/O SWITCH & C/O, SPO INTV BUTTONS, INOPERATIVE. GROUNDED - YES. REMOVED AND REPLACED DFCS MCP PER B737-800 AMM 22-11-34/401.SDR ASAA2022102440441Transceiver · faultyHF #2 NO TRANSMIT. RECEIVES OKAY. GROUNDED - YES. PERFFORMED HF SYSTEM FAULT ISOLATION PER B737-800 FIM 23-11 TASK 806. #2 TRANSCEIVER PASSED BITE TEST SO SWAPPED #1 & 2 TRANSCEIVERS. PROBLEM FOLLOWED #2 TRANSCEIVER SWAPPED TRANSCEIVERS BACK TO ORIGINAL POSITISDR ASAA2022102040412Transceiver · faultyNO. 2 HF RADIO FAILED. LOUD TONE LIKE TUNING TONE. UNABLE TO TRANSMIT OVER. GROUNDED - YES. R&R HF 2 R/T. HF 2 CHECKS OK REF B737-800 AMM 23-11-21.SDR ASAA2022101140249A/C Pack · warning lightAFTER ENG START CONT CAB ZONE TEMP ON AFTER RECALL. RESETS WITH MASTER CAUTION. GROUNDED - YES. PERFORMED PACK/ZONE BITE TEST. FLIGHT DECK TRIM VALVE LOGGED FAULT ON ZONE TEMP CONT #2. RESET FAULT , RAN BITE TEST A SECOND TIME OPS CHECK NORMAL PER B737-800 AMMSDR ASAA2022100340776Actuator · out of toleranceENG #1 LONG TERM FAULT. 75-10391 - THE VSV POSITION SIGNAL IS OUT OF RANGE. DEFER PER ASA TC 78273000. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE R/H VSV ACTUATOR REF B737-800 AMM 75-31-01.SDR ASAA2022081839564Hf Comm · failedHF # 2 FAILED INFLIGHT. GROUNDED - YES. PERFORMED HF #2 BITE REF. B737-800 FIM 23-11 TASK 801, NO FAULTS NOTED. PERFORMED HF 2 OPS CHECK REF. FIM 43-11 TASK 806 OPS CHECK GOOD. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2022071739082Sign · intermittentR2 DOOR EMERGENCY EXIT SIGNS ILLUMINATING INTERMITTENTLY. GROUNDED - YES. REMOVED & REPLACED R2 DOOR EMERGANCY EXIT SIGN POWER SUPPLY REF B737-800 AMM 33-51-06.SDR ASAA2022071539080Battery Pack · inoperativeON TAXI OUT, R2 DOOR LIGHT CAME ON IN AFT GALLEY. NO COCKPIT INDICATIONS. GROUNDED - YES. REMOVED AND REPLACED R2 DOOR EMERGENCY LIGHT BATTERY PACK. OPS CHECKS GOOD. REF B737-800 AMM 33-51-06-960-825.SDR ASAA2022062538798Labyrinth Seal · out of limitsWHILE PERFORMING TSR71285 FOUND LABYRINTH SEAL TEETH ON CENTER VENT TUBE REAR OF EXTENSION DUCT DIAMETER TO BE OUT OF LIMITS AT MEASUREMENTS OF 2.061", 2.050 AND 2.073" AND AFT OIL SEPARATOR HOLE ELONGATED ON #2 ENGINE. GROUNDED - YES. ENGINE REPLACED PER W/O SDR ASAA2022062438940Oil System · coked#2 ENGINE OIL TREND DATA SHOWS OIL CONSUMPTION TO GREATER THAN EXPECTED. MXCTL REQUEST. ENGINE POWER RUN REQUIRED. GROUNDED - YES. COMPLETED STEPS 1 THRU 5 OF TSR. WHILE PERFORMING GVI FOUND LARGE AMOUNT OF OIL PUDDLING AT ENG TAILCONE TURBINE REAR FRAME AND SSDR ASAA2022062438792Seal · leakingFOLLOWUP TO REPORT OF #2 ENGINE WITH OIL POOLING IN EXHAUST AND LEAKING FROM EXHAUST PLUG DRAIN. GROUNDED - YES. ACCOMPLISHED AFT SUMP INSPECTION PER B737-800 AMM 79-00-00-200-806-F01 UP TO STEP E(2)(E). FOUND OIL LEAKING AT BOTTOM OF SUMP. PERFORMED TURBINE SDR ASAA2022051938408Lamp · inoperativeEMERGENCY CEILING LIGHT @ 12DEF INOP. GROUNDED - YES. RELAMPED EMERGENCY AREA LIGHT AT ROW 12 DEF. OPS CHECK GOOD. REF B737-800 AMM 33-51-03.SDR ASAA2022032237791Valve · inoperativeON TAKE OFF WHEN POWER BEING SET AT AROUND 60% N1 RIGHT AMBER COWL ANTI ICE LIGHT AND MASTER CAUTION CAME ON. INITIATED A LOW SPEED ABORT. COWL ANTI ICE LIGHT WAS NOT TO COME ON PER THE MEL. GROUNDED - YES. PERFORMED TROUBLE SHOOT PER B737-800 FIM 30-21-00 TASSDR ASAA2022032237751Valve · inoperativeON TAKE OFF AND INITIAL CLIMB, TAI INDICATION ENG #2 INTERMITTANTLY WENT BLANK, TO AMBER, TO GREEN, SEVERAL TIMES. ENG ANTI-ICE SWITCH VALVE POSITION WAS DIM AT ALL TIMES. GROUNDED - YES. #2 ENG TAI COWL VALVE R&R PER B737-800 AMM 30-21-00. OPS CHK GOOD.SDR ASAA2022020637374Pressure Switch · inoperativeLEFT FUEL FILTER BYPASS LIGHT ILLUMINATED AFTER ENGINE START. GROUNDED - YES. REF B737-800 AMM 73-34-01-000-801-F00 / 73-34-01-400-801-F00. REMOVED AND REPLACED #1 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. IDLE LEAK CHECK AND EEC TEST PASSED. PERFORMED SDR ASAA2022020537352Valve · faulty#1 ENGINE ANTI-ICE BLUE DISAGREEMENT LIGHT DOES NOT ILLUMINATE AND ENGINE #1 ENGINE AND WING CONTROL BREAKER POPPED. GROUNDED - YES. REMOVED AND REPLACED ENGINE COWL TAI VALVE, REF B737-800 AMM 30-21-11. OP CHECK/LEAK CHECK GOOD.SDR ASAA2022012537259Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #23 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #23 PER T/C 78472010 (OPPOSITE BLADE #11 ALSO REPLACED FOR PAIRING).SDR ASAA2022012537258Platform · tornPER T/C 78472010 #2 FAN BLADE LUBE PLATFORMS #1,2,3,5,6,7,,9,10,10,20,23 AND 24 SEALS ARE TORN. GROUNDED - YES. REPLACED FAN BLADE PLATFORMS AT POSITIONS 1,2,3,5,6,7,9,10,19,20,23 AND 24, REF ASA T/C 78472010.SDR ASAA2022012537257Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #6 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #6, REF T/C 78472010 (OPPOSITE BLADE #18 ALSO REPLACED FOR WEIGHT PAIRING).SDR ASAA2022012537256Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #10 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #10 REF T/C 78472010 (OPPOSITE BLADE #22 REPLACE FOR WEIGHT PAIRING).SDR ASAA2022012537255Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #13 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #13 REF T/C 78472010 (OPPOSITE BLADE #1 REPLACED, ALSO FOR WEIGHT PAIRING).SDR ASAA2022012537254Blade · damagedPER T/C 78472010 #2 ENGINE FAN BLADE LUBE #19 FAN BLADE CU NI IN COATING MISSING BEYOND LIMITS CONCAVE SIDE. GROUNDED - YES. REPLACED #2 ENGINE FAN BLADE #19, REF T/C 78472010 (OPPOSITE BLADE # 7 ALSO REPLACED FOR WEIGHT PAIRING).SDR ASAA2022012337228Unknown · unknownVERTICAL SPEED SELECTOR JUMPS BETWEEN VALUES INSTEAD OF HAVING LINEAR SCALING WHEN SELECTED. GROUNDED - YES. ACCOMPLISHED DFCS OPERATION TEST REF B737-800 AMM 22-11-00-740-801 MCP VERTICAL SPEED KNOB CK 12.56 TEST PASS. WIITH VERTICAL SPEED SELECTOR CYCLED THRSDR ASAA2021121336893Heater · inoperativeAUX PITOT LIGHT ON. GROUNDED - YES. RESISTANCE CKS RANG OPEN FOR AUX PITOT PROBE. REMOVED & REPLACED PROBE REF B737-800 AMM 34-11-01. ALTERNATE PITOT SYSTEM LEAK TEST PASS REF AMM 34-11-00 & PITOT HEAT OPS NORMAL. APPLIED AERODYNAMICS SEALANT.SDR ASAA2021120336798Unknown · unknownLEFT FORWARD WINDOW OVERHEAT ILLUMINATED ON GROUND GROUNDED - YES. CONDUCTED QRH CHECKLIST AND WINDOW OVERHEAT EXTINGUISHED.SDR ASAA2021112636733Unknown · unknownLEFT CDU IS BLINKING/FLICKERING. GROUNDED - YES. OPEN MCDU 1 C/B, REMOVED LEFT MCDU, VERIFIED GOOD AIR FLOW FOR COOLING, REINSTALLED MCDU, OPS CK PASS REF B737-800 AMM 34-61-01. MCDU 1 C/B WAS RESET.SDR ASAA2021110736547Light · brokenEXIT SIGN PLACARD IS NOT FIXED. IT HAS BECOME LOOSENED AND FALLEN OFF. GROUNDED - YES. FLOOR LEVEL EXIT SIGN LIGHT ASSEMBLY AT AFT LEFT OVERWING EXIT IS BROKEN & MISSING A PIECE. REMOVED & REPLACED EXIT SIGN LIGHT ASSEMBLY REF B737-800 AMM 33-51-00. OPS CHECK SDR ASAA2021110436539Pressure Switch · faultedON TAXI OUT NUMBER ONE FUEL FILTER BYPASS LIGHT ILLUMINATED AND REMAIND ILLUMINATED APROXIMATELY 15 SECONDS, AND THEN EXTINGUISHED. POWER WAS AT IDEL. GROUNDED - YES. REF TSR711282 REMOVED AND REPLACED #1 FUEL DIFFERENTIAL PRESSURE SWITCH REF B737-800 AMM 73-3SDR ASAA2021110136479Unknown · unknownF/A REPORTS AFT GALLEY EMERGENCY LIGHTS ILLUMINATED FOR APPROX 2 MINUTES DURING FLIGHT.. SWITCH IN GUARD POSITION. GROUNDED - YES. GROUND VERIFICATION CHECK OF AFT AFT GALLEY EMERGENCY LIGHTS REF B737-800 AMM 33-51-00. NO FAULTS FOUND.SDR ASAA2021103136470Unknown · unknownFA REPORTS EXIT SIGNS ABOVE AFT GALLEY AND AFT LEFT EXIT DOORS GOING ON AND OFF INTERMITTANTLY. GROUNDED - YES. GROUND VERIFIED AFT GALLEY EMERGENCY EXIT SIGNS AND AFT DOORS EXIT SIGNS REF B737-800 FIM 33-50 TASK 801. OPS CHECK GOOD. NO DEFECTS NOTED.SDR ASAA2021103036454Unknown · unknownFA IN AFT GALLEY REPORT EMERGENCY LIGHTS IN GALLEY COME ON INTERMITANTLY. GROUNDED - YES. PERFORMED EMERGENCY LIGHTS - OPERATIONAL CHECK PER B737-800 MM 33-51-00-720-801. CHECKS GOOD NO HISTORY 30 DAYS.SDR ASAA2021102936464Filter · inoperativeLEFT FUEL FILTER BYPASS LIGHT ILLUMINATED AFTER START, AND STAYED LIT FOR APROX. 30 SECONDS,TO 1 MINUTE. GROUNDED - YES. REMOVED AND REPLACED NO. 1 ENG. FUEL FILTER, LK. AND OPS. CK. GOOD. REF. B737-800 AMM 73-11-02-000-801-F00. AND 73-11-02-400-801-F00. SEAMCSDR ASAA2021101436289Light · detached17A EMERGENCY EXIT LIGHT LENS MISSING. GROUNDED - YES. INSTALLED 17A EMERGENCY EXIT LIGHT LENS COVER.REF IPC 33-51-05-02A.GRD CHECK OK PER AMM 33-51-01-201.SDR ASAA2021100936234Harness · damagedWHILE REPLACING RH ENG HPTACC, FOUND CHAFING ON RH ENG HARNESS MW0311 OUTER SHEATH. DAMAGE PENETRATED THROUGH SHIELDING. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE MW0311 HARNESS REF B737-800 AMM 73-21-06. ALL TEST PASS EXCEPT BLEED AIR REGULATOR OPERATIONSDR ASAA2021090235855Indicator · malfunctionedFUEL QUANTITY INCREASED 800 LBS FOR NO APPARENT REASON. GROUNDED - YES. ACCOMP FUEL QUANTITY BITE NO PRESENT FAULTS & GROUND TEST PASS REF B737 FIM 28-41 TASK 801 ALSO ACCOMP REFUEL QUANTITY IND TEST, TEST PASS REF B737-800 28-41-61-710-001.SDR ASAA2021080435657Actuator · faultedWHILE ACCOMPLISHING T/C 78273000, FOUND #2 ENGINE 75-20452 AND 75-10452, THE VBV POSITION SIGNALS DISAGREE, SHORT TERM FAULTS. GROUNDED - YES. REMOVED AND REPLACED THE #2 ENGINE LH VBV ACTUATOR REF B737-800 AMM 75-32-02-400-801-F00. OPS CHECK GOOD. LEAK CHECK
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