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 ASAA2014021006819Warning Message · false activationMACH TRIM FAIL LIGHT ILLUMINATED FOLLOWED QRH AND LIGHT RESET WITH MASTER CAUTION. CAPTAINS PITCH BAR ON F/O FAILED AND CB SENSOR EXC AC TRIPPED. RESET CIRCUIT BREAKER ON PANEL P-18-1 C-5 "SENSOR-EXC-AC" IAW AMM 20-60-01-860-801. PERFORMED BITE TEST OF INTSDR ASAA2014020106728Warning Light · false indicationRT PACK LIGHT ILLUMINATED DURING RECALL. ACFT GROUNDED. PERFORMED FIM BITE OF PACK-ZONE TEMP CONTROLLER 21-62, TASK 801. NO FAULTS, RAN PACKS 20 MINUTES THRU FULL TEMP COMMANDS, RAN FIM TASK 21-62, TASK 801, NO FAULTS AND NO RECENT HISTORY.SDR ASAA2014011812417Valve · no testON INITIAL DECENT, LEFT BLEED TRIP OFF LIGHT ILLUMINATED. RESET TRIP IAW QRH, LIGHT STAYED OUT, EXTINGUISHES. ACFT GROUNDED. PERFORMED FIM TASK 36-10-809, WRENCH CHECKED ALL VALVES. VALVES CHECK OK. AS PRECAUTIONARY MEASURE, REPLACED HIGH STAGE REGULATOR RESDR ASAA2014010112292Control Valve · failedLT PACK LIGHT ILLUMINATES ON M.C. EXTINGUISHES ON RESET. ACFT GROUNDED. REPLACED THE LEFT PACK TEMP CONTROL VALVE REF TO AMM 21-51-10. OPS AND LEAK CHECK GOOD.SDR ASAA2013111096329Lens · unsecureF/A REPORT MID CABIN EXIT SIGH COVER FELL OUT. ACFT GROUNDED. REINSTALL MID CABIN EXIT SIGN. OK FOR SERVICE.SDR ASAA2013110196273Computer · failedAUTOTHROTTLES CIRCUIT BREAKER TRIPPED OPEN, AUTOTHROTTLES INOPERATIVE. ACFT GROUNDED. DFCS FAULT CODE 22-31263, REPLACED FCC A IAW FIM 22-31, TASK 801, MM 22-11-33. DFCS BITE GROUP NR 35 LRU REPLACEMENT TEST FOR FCC A PASS, DFCS BITE GROUP NR 49 LAND VERIFYSDR ASAA2013101896198Control Valve · warning lightRT PACK TEMP OVERHEAT LIGHT COME ON DURING RECALL. ACFT GROUNDED. REPLACED RT TCV IAW MM 21-51-10, LEAK AND OPS CHECKED NORMAL.SDR ASAA2013100496109Warning Light · false activationAFTER ENGINE START, ON RECALL THE FLT CONTROL MASTER CAUTION LIGHT CAME ON WITH MACH TRIM FAIL AND AUTO SLAT FAIL LIGHTS ON THE OVERHEAD FLIGHT CONTROL PANEL. ALL LIGHTS GO OUT WHEN MC RESET IS PRESSED. ACFT GROUNDED. CYCLED POWER, C/W OPS TEST OF STALL WASDR ASAA2013092596061Shim · wornDURING FAN LUBE OF NR 1 ENG ALL FAN BLADE SHIMS WERE FOUND TO HAVE MOLYDAG COATING WORN BEYOND LIMITS. ACFT GROUNDED. ALL SHIMS, FAN BLADE, NR 1 ENG REPLACED REF T/C 78472002.SDR ASAA2013092096019Warning Light · false activationON RECALL, RT PACK LIGHT ILLUMINATES. ACFT GROUNDED. CONFIRMED RT PACK LIGHT ON OVERHEAD WING MASTER RECALL. IAW FD PACK/ZONE TEMP CONTROLR NR 2 BITE IAW AMM 21-61-00, FOUND PREV FLT- THIS PACK FAULT ANNUNC ON CONTROLLER FRONT PANEL. CONTINUED W/ BITE SUCCESSDR ASAA2013090995942Indicator · inoperativeNR 2 REFUEL QTY INDICATOR LOWER DATA LINE BLANK. ACFT GROUNDED. REMOVED NR 2 INDICATOR, INSTALLED SERVICEABLE INDICATOR, OPS CHECKS GOOD REF MM 28-41-61.SDR ASAA2013082995899Computer · failedLEFT FMC FAILED. ACFT GROUNDED. WHILE ON DEFERRAL DURING CRUISE FMC ALERT, MSG VNAV DISENGAGED, FMA SHOWED FMC SPEED/LNAV/ALT HOLD. SPEED MODE ILLUMINATED ON MCP. VNAV WOULD NOT REENGAGE UNTIL WE BEGAN TO DESCENT, THEN ALL VNAV FUNCTIONS RETURNED TO NORMAL.SDR ASAA2013080195717Warning Light · false activationWINDOW OVERHEAT RT SIDE ILLUMINATED IN CRUISE. FOLLOWED QRH, WHEN SWITCHED BACK ON OVERHEAT LIGHT DID NOT ILLUMINATE. ACFT GROUNDED. WHCU SHOWS FOR LAST FLT & WINDOW POWER FOR PREVIOUS 2 LEGS. RESISTANCE CHECK OF SENSORS SHOWS WITH IN LIMITS EVEN COMPARED SDR ASAA2013080195716Warning Light · false activationWINDOW OVERHEAT, RT SIDE ILLUMINATED. FOLLOWED QRH. WHEN SWITCHED, TURNED BACK ON, OVERHEAT LIGHT DID NOT ILLUMINATE. OPS NORMAL. ACFT GROUNDED. COMPLIED WITH WINDOW HEAT OPS TEST IAW AMM 30-41-00-710-801. GROUND VERIFICATION, OPS CHECKED GOOD. NO HISTORYSDR ASAA2013071595610Unknown · unknownSATCOM PROMPT IS MISSING FROM FMC CDU GROUNDED. FOUND R/T POWER LIGHT GREEN BUT MCDU SAT PROMPT NOT SHOWING. CYCLED SATCOM CIRCUIT BREAKER. OPS NORMAL IAW MM 23-15-00.SDR ASAA2013071295607Valve · leakingNR 2 ENGINE OIL LEVEL DROPS 3 QUARTS SHORTLY AFTER SERVICING TO FULL. OIL CONSUMPTION WITHIN LIMITS. ACFT GROUNDED. IAW TSR, REPLACED NR 2 ENGINE OIL ANTI-LEAK VALVE IAW AMM 79-21-09-000-801-F00, 79-21-09-400-801-F00, 71-00-00-800-811-F00. SERVICED ENGINE SDR ASAA2013062295246Probe · out of limitsDIAGNOSTICS REPORTS NR 1 ENGINE EGTHDM CONTINUES TO SHOW GREATER THAN EXPECTED DATA SCATTER WITH AN INCREASE IN DELTA EGT. ACFT GROUNDED. INSPECTED ALL EGT PROBES IAW 77-21-01, TABLE C. FOUND PROBE S4 OUT OF LIMITS. REMOVED AND INSTALLED NEW S4 PROBE REF 77SDR ASAA2013062195244Radar · malfunctionedCAPTAINS RADAR DISPLAY CONTINUOUSLY PAINTS WEATHER AT THE 10 O`CLOCK AND 2 O`CLOCK POSITIONS AT 5 MILES RANGE. THIS OCCURS IN AUTO, WX, AND WX T MODES. F/O S DISPLAY WORKS PROPERLY. ACFT GROUNDED. PERFORMED RADAR SYS TEST AND FOUND NO FAULTS. SYS IS WORKINSDR ASAA2013061095066Valve · failedLEFT BLEED TRIP OFF ILLUMINATED AFTER CLIMB TO FL 410, LT PACK PRESSURE DROPPED TO 0. RESET AND HAD NORMAL OPERATION FOR 5 MIN AND THEN CONDITION REASSERTED. DESCENDED TO FL 390 AND RESET, OPS NORMAL. ACFT GROUNDED. PERFORMED ENGINE BLEED AIR SYS HEALTH CHECSDR ASAA2013052494893Warning Message · no indicationNO SATCOM PROMPT ON FMC MENU PAGE. ACFT GROUNDED. CYCLED ACFT GROUND POWER, BOTH SATCOM PROMPTS APPEAR IN FMC CDUS. COMMUNICATION TEST WITH DISPATCH (VOICE TEST) GOOD REF SYS TEST 23-15-00, GROUND VERIFICATION SUCCESSFUL.SDR ASAA2013042794620Unknown · malfunctionedSATCOM PROMPT DOES NOT APPEAR ON MENU PAGE OF MCDU. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT SATCOM PROMPT PRESENT ON BOTH MCDUS. PERFORMED SATCOM COMMUNICATION SYS ADJUSTMENT/TEST IAW MM 23-15-00-730-801, STEPS A THROUGH E ALL TESTS PASS. GROUND VERIFICASDR ASAA2013040294366Transceiver · unknownSATCOM PROMPT DOES NOT APPEAR ON MCDU PAGE. ACFT GROUNDED. NOT ABLE TO GET SATCOM PROMPT TO DISAPPEAR. REMOVED AND REAPPLIED POWER AND TRANSFERRED POWER BETWEEN APU AND GROUND POWER. COULD NOT GET SATCOM TO FAIL REMOVED AND REPLACED SATCOM TRANSCEIVER. OPS NOSDR ASAA2013031994205A/C Pack · malfunctionedLEFT PACK BLEED TRIP AT FL 400, RESET ONCE, BLEED TRIP HAPPENED AGAIN, RESET A SECOND TIME, LIGHT STAYED OUT. PERFORMED BLEED TRIP OFF LIGHT ON, FAULT ISOLATION IAW FIM TASK 36-10 TASK 801. PREFORMED PRELIMINARY CHECKS, FAULT ISOLATION PROCEDURES AND REPAISDR ASAA2013031994200Idg · failedDURING CRUISE AT FL 340, NR 1 IDG DRIVE LIGHT ILLUMINATED AND VOLTS AND FREQ INDICATED 0. IDG DISCONNECTED VIA CHECKLIST. REPLACED NR 1 ENG IDG IAW NG-800 ASA MM 24-11-400-801 AND 24-11-00-700-802. INSTALLATION TEST AND LEAK CHECK. IS GOOD.SDR ASAA2013031894194Warning Light · malfunctionedDURING STANDBY POWER CHECKS, SPAR VALVE. ENGINE VALVE TEST WITH P6-3 C-6 PULLED START LEVERS 12 TO IDLE SPAR VALVE CLOSED LIGHTS DID NOT EXTINGUISH (STAYED BRIGHT). WHEN ENG FIRE CHARGED EMERGENCY FUEL SHUTOFF BATTERY FOR 1 HR IAW AMM 28-22-14-400-801. FUEL SSDR ASAA2013031694164Epsu · inoperativeBATTERY PACK M1694 WOULD NOT POWER THE FLOOR PROXIMITY LIGHTS AT THE RT & LT FWD OVER WING EMERGENCY EXIT DOORS REPLACED BATTERY PACK & OPS CHECKED GOOD.SDR ASAA2013031494180Transmitter · leakingNR 2 ENGINE OIL QUANTITY READS ZERO. R & R NR 2 ENGINE OIL QTY TRANSMITTER REF AMM 79-31-01. LEAK CHECKED TRANSMITTER REF AMM 71-00-00 TEST 3A, NO LEAKS NOTED. PERFORMED FUNCTIONAL TEST OF OIL QTY INDICATION REF AMM 79-31-01. INDICATION CHECK NORMAL.SDR ASAA2013022794157Seat Track · gougedMAIN CABIN SEAT TRACK, STA 520, LBL 45.57 UPPER SURFACE IS GOUGED. ACFT GROUNDED. BLENDED AREA SEAT TRACK BETWEEN SCALLOPS .480, FROM CENTER OF TRACK TO INBD IS 280 MAT REMAINING .240 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, CUT THE DAMAGED AREA IAW SRM 5SDR ASAA2013022794156Seat Track · gougedMAIN CABIN SEAT TRACK, BS 520, RBL 24.82 UPPER SURFACE IS GOUGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-00-52, REPAIR 4.SDR ASAA2013022794155Seat Track · gougedMAIN CABIN SEAT TRACK BS 520, RBL 45.57 UPPER SURFACE IS GOUGED. ACFT GROUNDED. BLENDED GOUGED AREA IAW SRM 53-00-52. ORIG MAT .146, REMAINING MAT .112, REMOVED MAT .034, FOUND OUT OF LIMITS IAW SRM 53-00-52. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-SDR ASAA2013022794154Seat Track · gougedMAIN CABIN SEAT TRACK BS 520, LBL 24.82 UPPER SURFACE IS GOUGED. BLENDED AREA, FOUND OUT OF LIMITS IAW SRM 53-00-52, CUT DAMAGE ARE IAW SRM 53-00-52. FABRICATED SEAT TRACK AND SPLICE IAW SRM 53-00-52. TREATED WITH ALODINED & PRIMED IAW SRM 51-20-01, INSTSDR ASAA2013012293723Engine · damagedNR 2 ENGINE TREND DATA SHOWS A SUDDEN SHIFT IN EGT (TAKEOFF AND CRUISE), FUEL FLOW AND DELTA CORE SPEED. CORE SPEED AND EGT ARE CURRENTLY WITH ETOPS LIMITS. NR 2 ENGINE VBV GUIDE PAD UNDER NR 9 FAN DUCT PANEL IS DISBONDED. (REF AMM 75-32-00-200-801-F00) ACFT SDR ASAA2013010993646Wire Harness · shortedDURING CLIMBOUT, TURNED ON ENGINE ANTI-ICE, NO BLUE LIGHT INDICATION. CHECKED CIRCUIT BREAKER PANEL AND CB A-6, ENG 1, ENG WING CONTROL WAS TRIPPED. R & R NR 2 ENG MW0311 STRUT HARNESS REF AMM TASK 73-21-06-000-802-F00 AND TASK 73-21-06-400-802-F00. PERFORMESDR ASAA2013010893637Solenoid Valve · failedBOTH WING ANTI-ICE LIGHTS FAILED TO TEST. NR 1 ENGINE COWL VALVE OPEN LIGHT OUT FAILS TO TEST. ENGINE NR 1 AND WING CONTROL ANTI-ICE & RAIN CIRCUIT BREAKER TRIPPED. ACCOMPLISHED FIM TASK 30-11, TASK 810 C/B C148 OPENS INTERMITTENTLY ON GND. NR1 ENG GROUND SDR ASAA2013010693635Unknown · unknownDURING FLIGHT, LAVATORY INOPERATIVE LIGHT ILLUMINATED ON AFT F/A PANEL, DEACTIVATING ALL TOILETS FROM FLUSHING OR DRAINING. ON ARRIVAL SERVICE PERSONNEL NOTED LARGE AMOUNT OF WASTE WAS DUMPED. PERFORMED TOILET FLUSH SYS. ALL TOILETS DO NOT FLUSH REF MM 38-3SDR ASAA2012122693554Screw · wornNR 2 ENGINE, NR 5 FAN DUCT PANEL WITH LPTACC SCOOP HAS 2 LOOSE FASTENERS AND MISSING 2 WASHERS. ON FURTHER INSPECTION, NOTED THAT THERE WERE NO MISSING WASHERS, THE SCREW HEADS HAD WORN LEAVING A GAP BETWEEN THE PANEL AND SCREW HEAD. REPLACED ALL SCREWS ONSDR ASAA2012122593539Circuit Breaker · trippedP18-3 A-6, CIRCUIT BREAKER FOUND TRIPPED. RESET CIRCUIT BREAKER AT P18-3 A-6 IAW AMM 20-60-01 AND WDM 30-21-11. CIRCUIT BREAKER REMAINS SET. ACCOMPLISHED NR 1 ENGINE COWL ANTI-ICE OPS TEST IAW AMM 30-21-00. OPS CHECKED GOOD. OK FOR SERVICE. SYS GROUND FUSDR ASAA2012122593538Indication Sys · malfunctionedAT PUSHBACK, THE NR 2 FUEL SYS DECREASED UNILATERALLY BY 400 POUNDS. DRAINED AND SUMPED NR 2 MAIN TANK. TANK UNIT AND COMPENSATOR VALUES WITHIN LIMITS. BITE TEST PASSES. NO CURRENT FAULTS, REF AMM 28-41-00-730-801.SDR ASAA2012121993501Circuit Breaker · trippedNR 1 ENGINE & WING CONTROL CIRCUIT BREAKER TRIPPED. CHECKED W2112-6049, NO SHORT OR GROUND, RESET CIRCUIT BREAKER C148 IAW SWPM 20-60-01. OPS CHECKED WING AND NR 1 ENGINE ANTI-ICE, OPS NORMAL REF MM 30-11-11/501.SDR ASAA2012120693416Eec · failedDURING CRUISE, FLT AUTOTHROTTLE LIM BOX APPEARED ABOVE NS ON COMPACT DISPLAY. NR 2 ENGINE ADVANCED BEYOND CLIMB LIM MARKING/CARAT DURING ALL CLIMBS - DISCONNECTED AUTOTHROTTLE DURING CLIMBS TO PREVENT NR 2 ENG FROM EXCEEDING CLB LIMIT. REPLACED NR 2 EEC IAW SDR ASAA2012112193343Drain Mast · crackedDURING SERVICE CHECK, FOUND APU FUEL SHROUD DRAIN MAST CRACKED. REMOVED NOTED DRAIN MAST IAW TASK 28-25-07-020-801. INSTALLED DRAIN MAST IAW MM TASK 28-25-07. REPLACED DRAIN MAST LINE.SDR ASAA2012111493300Fmc · inoperativeRT FMC INOPERATIVE. REPLACED FMC IAW MM 34-61-02.SDR ASAA2012110993273Transceiver · malfunctionedHF 2 CIRCUIT BREAKER TRIPPED. CONFIRMED FAULT, HF NR 2 CIRCUIT BREAKER TRIPPED. REPLACED NR 2 HF COMM TRANSCEIVER IAW MM 23-11-21, TRANSMITTED AND RECEIVED HF VOICE SIGNALS AND DATA, OPS CHECKED GOOD.SDR ASAA2012110693257Connector · dirtyDISCONNECTED AUTOTHROTTLE FOR ENGINE CONDITION MONITOR. AFTER ENGAGING AUTOTHROTTLE SWITCH, WHITE AUTOTHROTTLE LIMIT APPEARED ON UPPER DISPLAY UNIT. GREEN CARETS CORRESPOND TO THRUST LIMIT SELECTED ON N1 LIMIT PAGE OF FMC. ON DESCENT OUT OF FL 380, RETURNED SDR ASAA2012102793195Rheostat · brokenFMC DIMMER RHEOSTAT SPINS COMPLETELY AROUND. ACFT GROUNDED. REMOVED REPLACED F/OS MCDU KEYBOARD IAW AMM REF 34-61-01. OPS CKS GOOD.SDR ASAA2012102693191Warning Light · false activationDURING APU POWER TRANSFER THE LIGHT ILLUMINATED. FOUND FAULT SPCU INOP. COMPLIED WITH BITE IAW FIM 24-31 TASK 801 AND FIM 24-34 TASK 802. FAULT CLEARED AND DID NOT RETURN. ACFT OK FOR SERVICE.SDR ASAA2012101893158Valve · malfunctionedNR 1 BLEED TRIP LIGHT DESCENDING THRU 37000 THROTTLE AT 60 N1 LIGHT EXTINGUISHED ON RESET. ACCOMPLISHED QUICK FIM TASK 36-10 VISUAL INSPECTION FOUND NR 1 PRE-COOLER VALVE KISS SEAL SCREWS LOOSE AND HOLES ELONGATED. REPLACED NR 1 PRE-COOLER VALVE AND KISS SEASDR ASAA2012101793150Control Unit · malfunctionedFIRST OFFICER`S SLIDER WINDOW OVERHEAT LIGHT ILLUMINATED. CYCLED POWER WINDOW, HEATS NORMALLY, WINDSHIELD HEAT CONTROL UNIT SHOWS SENSOR FAULT. CONTROL UNIT BITE CHECKED OK. WINDOW SENSOR CHECKED RESISTANCE WAS WITHIN LIMITS REF AMM 30-41-21-760-801. REPLASDR ASAA2012101393110Antenna · malfunctionedWEATHER RADAR RETURNS DID NOT MATCH OUTSIDE VISUAL CONDITIONS. RADAR CALIBRATION SEEMED CALIBRATED 3 DEGREES TOO HIGH. MINUS 3 DEGREES SEEMED TO EQUAL ZERO DEGREES. ACFT GROUNDED. R & R WX RADAR ANTENNA DRIVE UNIT REF MM 34-43-11-000-802 & 34-43-11-400-802SDR ASAA2012100993091Circuit Breaker · trippedAFT CARGO FIRE DETECTION LOOP A, DID NOT TEST, FOUND CIRCUIT BREAKER OUT. INSPECTED WDM REF 26-16-22 FOR AFT CARGO FIRE DETECTION LOOP A, CIRCUIT NORMAL. RESET AFT CARGO FIRE DETECTION LOOP A CIRCUIT BREAKER ON P18-3. GROUND VERIFICATION SUCCESSFUL REF MM
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