N462AS
Service difficulty reports · 235
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 = 'N462AS' 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 = 'N462AS' 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 ASAA2018071625343Unknown · malfunctionedZONE TEMP CONT CAB ON RECALL. CLEARS WITH M/C RESET. GROUNDED - YES. PERFORMED PACK TEMP CONTROL BITE REF FI 21-62 TASK 801. NO FAULTS FOUND ZONE TEMP REMAINS EXTINGUISHED WITH RECALL.SDR ASAA2018060424896Shim · damagedWHILE ACCOMPLISHING FAN BLADE LUBE ON THE NR 2 ENGINE. FOUND THE COATING MISSING ON ALL SHIMS. NO WEAR TO BASE MATERIAL. ACFT GROUNDED.SDR ASAA2018032424133Transceiver · malfunctionedHF 2 RADIO COMMUNICATION PANEL HAS FAIL IN BOTH FREQUENCY INDICATORS. ACFT GROUNDED. ACCOMPLISHED HF SYSTEM BITE PROCEDURE IAW FIM 23-11, TASK 801, HF TRANSCEIVER 2 SHOWED NO FAULTS. AFTER BITE FAULT INDICATIONS REMOVED UNABLE TO DUPLICATE PROBLEM AFTER THATSDR ASAA2018031823936Control Unit · false indicationRIGHT FWD WINDOW, OVERHEAT LIGHT ILLUMINATED DURING TAKEOFF + 2:45. FOLLOWED QRH. LIGHT REMAINED ON. TURNED WINDOW HEAT SWITCH OFF. ACFT GROUNDED. REMOVED & REPLACED THE RIGHT FWD WHCU IAW AMM 30-41-11. OPS TESTED NORMAL AND FIM 30-41 / 801, BITE TESTED SDR ASAA2018021423543Warning System · false activationL SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED AT FL 280. GROUNDED - YES. FOLLOWED QRH PROCEDURE. LIGHT EXTINGUISHED.SDR ASAA2018012024068Lamp · inoperativeL1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS, OP CHECKED GOOD IAW AMM 33-51-04.SDR ASAA2017121822952Warning System · false activationZONE TEMP FOR CONTROL CABIN ILLUMINATED ON RECALL EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. INITIAL EVALUATION FOUND NR 2 TEMP CONTROLLER WITH FLT DECK TCV FAIL. PERFORMED BITE TEST REF AMM TASK 21-61-00-700-806-002. NO FAULT FOUND. RESET CONTROLSDR ASAA2017121322905Fmc · malfunctionedTHE FMC'S SEEM TO DROP WAYPOINTS ON THE RNAV ARRIVALS WHEN THE RUNWAY/APPROACH IS CHOSEN OR CHANGED. NO DISCO APPEARS, THEY JUST RANDOMLY CONNECT TWO POINTS OMITTING SOME BUT NOT ALL OF THE WAYPOINTS. GROUNDED - YES. COULD NOT DUPLICATE DISCREPANCY. #1 AND #2 SDR ASAA2017120522807Warning Light · false activationON NR 2 ENGINE START, START SWITCH CUT OUT CORRECTLY, ENGINE COMPLETED START, START VALVE LIGHT REMAINED ILLUMINATED. RAN QRH AND IT WANTED SHUT DOWN, SHUT DOWN, LIGHT EXTINGUISHED. GROUNDED - YES. OPEN NR 2 ENGINE I/B COWL ACCOMPLISHED GVI OF ENG STARTER NO DSDR ASAA2017112022642Hf Comm · malfunctionedHF 2 DISPLAYS FAIL ON RADIO CONTROL PANEL. ACFT GROUNDED. PERFORMED FIM 23-11, TASK 801 BITE CHECK, PASSED. PERFORMED AN OPS CHECK OF THE HF 2 SYSTEM, OPS CHECK PASSED IAW AMM 23-11-00. PERFORMED FIM 23-11, TASK 802, NO DEFECTS NOTED.SDR ASAA2017103122373Link · wornWHILE ACCOMPLISHING AN ENGINE INLET INSPECTION, NR 1 ENGINE, FOUND 1ST AND 2ND DUCT ATTACH LINKS WORN ABOVE THE HIGH STAGE VALVE. ACFT GROUNDED. REPLACED INTERSECTION MANIFOLD DUCT ASSY AND BOTH ATTACH LINKS, IAW AMM 36-11-01. LEAK CHECKED GOOD.SDR ASAA2017102122272Window · failedDURING DESCENT, THE R2 WINDOW HAD OVERHEAT. FOLLOWED QRH LIGHT REMAINED, EXTINGUISHED WHEN SWITCH TURNED BACK ON. ACFT GROUNDED. REMOVED AND REPLACED THE R2 WINDOW IAW AMM 56-12-11-400-801. CHANGED R2 TO WINDOW TAP TO MATCH H14 WINDOW INSTALLED IAW WDM 30SDR ASAA2017101722240Heater · malfunctionedRIGHT SIDE WINDOW OVERHEAT, RESET TWICE, FOLLOWED QRH. SWITCH REMAINED OFF FOR REMAINDER OF THE FLT. ACFT GROUNDED. TROUBLESHOOT IAW WDM 30-41-11, AND AMM 30-41-21-000-801. RT WINDOW TERMINAL TAB READING 59 OHMS. SWITCHED TAB TO POSITION -1 TO MATCH RESISSDR ASAA2017101622228Control Unit · malfunctionedRIGHT SIDE WINDOW GOES TO OVERHEAT ON GROUND. ACFT GROUNDED. RIGHT SIDE WINDOW HEAT CONTROL UNIT BITE COMPLETED IAW FIM 30-41, TASK 801, BITE TESTED OK. OPS CHECK OF THE RT SIDE WINDOW IAW AMM 30-41-00-710-801. CHECKED GOOD.SDR ASAA2017082621716Control Panel · failedDURING LLM TESTS FOR NOTED L/P, MODE CONTROL PANEL VERTICAL SPEED ANNUCIATOR READOUT WINDOW HAS BACK LIGHTING BLEED THRU. ACFT GROUNDED. REMOVED & REPLACED THE MODE CONTROL PANEL. OPS GOOD. GROUND VERIFICATION SUCCESSFUL IAW AMM 22-11-34/401.SDR ASAA2017082321709Trim System · malfunctionedMACH TRIM FAILURE ANNUNCIATOR ON RECALL AFTER ENGINE START. CANCELS ON MASTER CAUTION RESET. ACFT GROUNDED. FOUND AFCS SYSTEM A CANCEL EXC AC BRAKE OPEN ON PA18-1 PANEL. RESET THE CIRCUIT BREAKER IAW AMM 20-60-1. PERFORMED BITE CHECK MACH TRIM SYSTEM IAW AMM SDR ASAA2017082321706Computer · malfunctionedAUTOPILOT WOULD NOT ENGAGE AFTER TAKEOFF. NOT WORKING ENTIRE FLIGHT. ACFT GROUNDED. ACCOMPLISHED LAND VERIFY TEST. NO FAULTS FOUND. REMOVED AND REPLACED FCC A, IAW AMM 22-11-33.SDR ASAA2017071021341Static Inverter · failedELEC LIGHT ILLUMINATED ON RECALL AFTER PUSHBACK. ACFT GROUNDED. BITE CHECKED ELECT LIGHT SHOWS STATIC INVERTER FAILED. REMOVED AND REPLACED THE STATIC INVERTER IAW AMM 24-34-21-401. P5-13 PANEL FAULTS CLEARED AND BITE TESTED GOOD.SDR ASAA2017071021340Control Panel · malfunctionedELEC LIGHT ILLUMINATED ON THE GROUND. ACFT GROUNDED. P5-13 PANEL SHOWS STATIC INVERTER INOPERATIVE. INVERTER VOLTS ARE AT ZERO. CYCLED STANDBY POWER SWITCH. INVERTER VOLTS NOW 115V. CLEARED FAULT. MAINTENANCE TEST OF THE P5-13 PANEL IS NOW GOOD. NO FAULTSSDR ASAA2017071021339Warning Light · false activationELEC LIGHT ILLUMINATED ON LANDING. ACFT GROUNDED. ACCOMPLISHED ELECTRICAL METER POWER MODULE RESET IAW MM 24-21-53. NO FAULTS FOUND. OPS CHECKED NORMAL.SDR ASAA2017060120928Warning Message · false activationLEFT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL. THE PACK LIGHT EXTINGUISHES WHEN THE MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. ACCOMPLISHED FIM TASKS 21-62/848 AND 21-62/801. BITE CHECK OF 1 AND 2 CONTS NORMAL, BOTH GREEN GO. SUSPECT INTERMITTENT SDR ASAA2017052920916Battery · dischargedBATTERY SWITCH FOUND ON AND BATTERIES DRAINED UPON ARRIVAL AT AIRCRAFT. ACFT GROUNDED. REMOVED AND REPLACED AUX BATTERY IAW AMM 24-31-11, OPS CHECKED NORMAL. REMOVED AND REPLACED MAIN BATTERY IAW AMM 24-31-11, OPS CHECKED NORMAL.SDR ASAA2017051220721Warning Light · false activation"AUTO FAIL" LIGHT ILLUMINATED ON PRESSURIZATION CONTROLLER AFTER LANDING. ACFT GROUNDED. ACCOMPLISHED FIM TASK 21-31-801. NO CURRENT FAULTS SHOWING. AUTO FAIL LIGHT LIGHT EXTINGUISHED. ALL OTHER INDICATION ON PANEL CLEARED. ACFT GOOD FOR CONTINUED SERSDR ASAA2017042220503Unknown · malfunctionedHF NR 2 IS INDICATING "FAIL" ON CONTROL HEAD. GROUNDED - YES. ACCOMPLISHED HF NR 2 COMMUNICATION SYSTEM OPERATIONAL TEST, OPS NML REF AMM 23-11-00-710-801. ACCOMPLISHED HF NR 2 COMMUNICATION SYSTEM TEST, OPS NML REF AMM 23-11-00-730-801. NO HISTORY LAST 60 DAYSDR ASAA2017021819851Control Valve · failedON MASTER CAUTION RECAL CONT CAB ZONE TEMP LIGHT ILLUMINATED. EXTINGUISHED ON M.C. RESET. ACFT GROUNDED. CONFIRMED FAULT, RT PACK/ZONE TEMP CONTROLLER BITE SHOWS HARD FAIL FLIGHT DECK TCV. REMOVED & REPLACED THE FLIGHT DECK TCV IAW AMM 21-61-21, GROUND FUNCTSDR ASAA2017020419668Probe · failedPROBE HEAT,TEMP PROBE LIGHT STAYS ON AFTER ENGINE START AND WITH SWITCH ON, C/B IN. (TAT SHOWS ACTUAL OAT) ACFT GROUNDED. VERIFIED FAULT, TROUBLE TO TAT PROBE, REMOVED & REPLACED THE PROBE WITH SERVICEABLE UNIT. AFFECTED SYSTEM OPS CHECK IAW AMM 30-30-00-730-SDR ASAA2017012719571Warning Flag · false activationLEFT MAP DISPLAY SHOWED VTK, LEFT CDU WENT TO MENU PAGE. AFTER 10 SECONDS (APPROX) VTK FLAG WENT AWAY, RE-ENGAGED LNAV VNAV. NO PROBLEMS AFTER. OCCURED JUST PRIOR TO DESCENT. ACFT GROUNDED. NO CURRENT FAULTS, IAW AMM 34-61-00.SDR ASAA2016123019193Warning System · false activationON RECALL RIGHT PACK LIGHT ILLUMINATES IN FLIGHT. GROUNDED - YES. ACCOMPLISHED FIM 21-62 TASK 801. LAST FLIGHT SHOWED AN EXIT FAULT ON SRDA. FAULT RESETS AND BITE OPS NORMAL, REF AMM 21-51 TASK 803.SDR ASAA2016121419032Fmc · malfunctionedBOTH FMC FAILED DURING CRUISE. STARTED QRH AND BOTH FMC RESTORED THEMSELVES AFTER 5-10 MINUTES. ACFT GROUNDED. PERFORMED FMC BITE IAW FIM 34-61 TASK 801. NO SENSOR FAULT, NO INFLIGHT FAULT. FMC SYSTEMS OK TO CONTINUE.SDR ASAA2016111918736Filter · cloggedUNABLE TO CONTROL CABIN TEMP. STARTED OUT HOT, ADJUSTED TEMP VERY SMALL AMOUNT ON AFT CABIN CONTROL. CABIN WENT TOO COLD. READJUSTED TOWARD WARM, GOT REALLY HOT. RAN CABIN HOT QRH, TURNED OFF TRIM AIR SWITCH. CABIN TEMP CONTROL WENT BACK TO NORMAL. GROUNDED, YSDR ASAA2016093018151Warning Light · false activationLEFT PACK LIGHT ON MASTER CAUTION RECALL. ACFT GROUNDED. ACCOMPLISHED BITE OF BOTH PTC NR 1 FAULTED TCV ON BIT AND PREV FLT WITH A GREEN ON VERIFY, RESET AND RE-ACCOMPLISHED BITE WITH NO FURTHER FAULTS. ALL TESTS PASS IAW AMM 21-61-00 AND 0 FIM 21-62 TASK 801.SDR ASAA2016070817309Bulb · inoperativeOUTSIDE RIGHT AFT EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BULB IAW AMM 33-51-04. OPS CHECKED GOOD.SDR ASAA2016070617288Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE PER QRH. SATCOM OPS RESTORED NORMAL.SDR ASAA2016061217015Warning Light · false activationCABIN ZONE TEMP LIGHT ON RECALL AFTER STARTING ENGINES. ACFT GROUNDED. PERFORMED PACK ZONE TEMP BITE CHECK IAW AMM 21-60-00 ON BOTH CONTROLLERS, FOUND NR 2 CONTROLLER FLIGHT DECK RED LIGHT ON. BITE CHECK CLEARED ALL FAULTS AND PERFORMED BITE. NO DEFECTS NOTSDR ASAA2016051216720Fmc · failedRIGHT FMC FAILURE AT CRUISE 30 MINUTES AFTER DEPARTURE. GOT "SINGLE FMC OPERATION" ON SCRATCHPAD OF FMC, NO BEARING, DISTANCE ON POS SHIFT 3/3 FMC-R. ACFT GROUNDED. PERFORMED FMC BITE TEST, BITE CHECK GOOD REF FIM 34-61, TASK 801. PERFORMED FMC OPS TEST, OPSSDR ASAA2016041916469Radar · false indicationWEATHER FAIL ILLUMINATED ENROUTE. ACFT GROUNDED. PERFORMED FIM 34-43, TASK 814 - WEATHER RADAR FAULT ISOLATION. ALL TESTS PASSED AND GROUND FUNCTIONAL CHECK GOOD.SDR ASAA2016041716439Fmc · malfunctionedPWS CAUTION ON PILOT & CO-PILOT MAPS AT 500' ON APPROACH. AT TOUCHDOWN, PWS DISAPPEARED AND VTK ON CAPTAIN'S SIDE APPEARED WITH LOSS OF MAP INFO FOR APPROXIMATELY 30 SECONDS. ACFT GROUNDED. PERFORMED WEATHER RADAR SYS OPS TEST IAW AMM 34-43-00-710-802-001.SDR ASAA2016041416420Eec · malfunctionedAFTER COMPLETING CROSS BLEED START NOTICED BOTH OVERHEAD "ALTN" LIGHTS ILLUMINATED. ACFT GROUNDED. FOUND ELECTRONIC ENGINE CONTROL SWITCHES OUT, RETURNED ELECTRONIC ENGINE CONTROL SWITCHES BACK TO ON. RAN ENGINES, WORK NORMAL. NO OVERHEAD "ALTN " LIGHTS ILLSDR ASAA2016041216369Warning Light · false activationF/O VTK/FMC P/RST BOTH ILLUMINATED AT CRUISE. MOMENTARY THEN EXTINGUISHED. FMC-L/FMCR BOTH INDICATE NORMAL FUNCTION AFTER VTK INDICATED AND SELF RESOLVED. ACFT GROUNDED. ACCOMPLISHED FMCS BITE IAW FIM 34-61-801. SENSOR STATUS AND INFLIGHT FAULT SHOW NO FAUSDR ASAA2016041116351Fuel Control · failedAFTER LANDING APU FAULT LIGHT CAME ON DURING START CYCLE. ACFT GROUNDED. R & R FUEL CONTROL UNIT, REF AMM 49-31-11, OPS CHECK NORMAL.SDR ASAA2016040116194Knob · intermittentF/O'S COURSE SELECT KNOB INTERMITTANTLY INOPERATIVE. ACFT GROUNDED. COULD NOT DUPLICATE, SYS TESTS GOOD IAW AMM 22-00-01-730-801. ACFT REMAINS CAT III A A/L & HGS QUALIFIED. STATUS IND REFLECTS SAME.SDR ASAA2016012414976Warning Message · false activationON RECALL, MASTER CAUTION ILLUMINATED AND CONTROL CABIN ZONE TEMP ILLUMINATES. LIGHTS EXTINGUISHED WITH RESET. ACFT GROUNDED. PERFORMED BITE REF FIM 21-62, TASK 801. NR 2 FAULTED FLIGHT DECK TRIM VALVE, PERFORMED FIM 21-62, TASK 832, FAULT CLEARED.SDR ASAA2016012314969Arm · damagedCATERING REPORTS L2 DOOR HARD TO OPEN, FOUND LOWER DOOR ARM MISSING RUBBER BLOCK, APPEARS TO BE GLUED ON, PREVENTS ACTUATOR FROM OVER EXTENDING. ACFT GROUNDED. REPLACED THE FILLER IN THE L2 LOWER HINGE ARM, PN 65-73978-23, REF DWG. 65-73978, REV E, FRAME 3 OFSDR ASAA2016010814710Terminal · looseREF T/C 78128007, AD 08-10-10 CENTER TANK FUEL PUMP UNCOMMANDED ON TASK CARD. STEP C6, TERMINAL C2 HAS ERRATIC VOLTAGE ON RELAY R962. ACFT GROUNDED. FOUND ON RELAY R962 TERMINAL C2 , A LOOSE TERMINAL, TIGHTENED SAME. T/C 78128007 COMPLETED AND OPS NORMAL.SDR ASAA2016010214604Fmc · failedAT CRUISE, CAPTAIN'S ND DISPLAY HAD A "VTK", BOTH MCDU'S LOST FMC INFO. ACCOMPLISHED FMC FAIL QRH FOR LT FMC FAIL. RT FMC OPERATING NORMAL. ACFT GROUNDED. ACCOMPLISHED LT AND RT FMC BITE REF FIM 34-61, TASK 801. RT FMC NO CURRENT FAULTS. LT FMC NO CURRENSDR ASAA2015110213599A/C Pack · malfunctionedRIGHT PACK ON RECALL. ACFT GROUNDED. ACCOMPLISHED PACK TEMP CONTROLLER BITE ON BOTH CONTROLLERS, FIM 21-62, TASK 801, NR 2 HAD EXIT SRADA FAULT. NR 1, NO FAULTS. ON RECALL, NO PACK LT ILLUMINATED. OBSERVED GREEN LT ON RT AFT SRADA EXIT. OPS CKD NORMAL. RESDR ASAA2015100913432Warning Message · false activationCAPTAIN`S INBD DISPLAY UNIT DISPLAYED VTK & MAP. BOTH FMC'S WENT BLANK. INAV & LNAV DISENGAGED. AFTER 15 SECS EVERYTHING RETURNED TO NORMAL. ACFT GROUNDED. ACCOMPLISHED FMCS BITE IAW FIM 34-61, TASK 801. NO SENSOR FAULTS LOGGED. INFLIGHT FAULT FOR LEG 1 SSDR ASAA2015100913425Satcom · malfunctionedSATCOM UP, ACFT GROUNDED. QRH CHECKLIST RAN. OPS NORMAL.SDR ASAA2015100413317Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. QRH PERFORMED SUCCESSFULLY.SDR ASAA2015091213010Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. SATCOM LOCKUP PROCEDURE IAW QRH ACCOMPLISHED OPS NORMAL.
Back to N462AS