N590AS
Service difficulty reports · 440
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 = 'N590AS' 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 = 'N590AS' 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 ASAA2018012323278Computer · failedCREW REPORTS CAPTS FLT DIR FLAG IN VIEW. GROUNDED - YES. REMOVED AND REPLACED FCCA PER AMM 22-11-33. PERFORMED DFCS TEST GROUP 35 PER AMM 22-11-33 AND DFCS GROUP 49 PER AMM 22-11-00. ALL TESTS PASS, PERFORMED HGS OPS TEST PER HGS 4000 SMM 34-36-00 ALL TESTS PASDR ASAA2018011323177Transceiver · failedBOTH HF RADIOS WOULD TUNE BUT TRANSMISSION AND RECEPTION GARBLED AND UNREADABLE. ACFT GROUNDED. VERIFIED REU AUDIO PATH USING SATCOM IAW AMM 23-15-00-730-801, NO DEFECTS NOTED. REMOVED AND REPLACED THE NR 1 AND 2 HF TRANSCEIVERS IAW AMM 23-11-21/401. TRANSMSDR ASAA2018010523091Hf Comm · malfunctionedHF RADIO NR 1 AND 2 TRANSMITTING OFF FREQUENCY, BOTH HF RADIOS ARE READABLE BUT SLIGHTLY GARBLED. ACFT GROUNDED. ACCOMPLISHED HF OPS TEST IAW AMM 23-11-00, NO DEFECTS NOTED ON BITE CHECK, COMMUNICATIONS CHECKED NORMAL. OK FOR SERVICE.SDR ASAA2018010523089Door · unsecureACCELERATING OUT OF 10,000 FT AND 250KTS, STARTED TO FEEL A SLIGHT VIBRATION. ALL ENGINE PARAMETERS WERE NORMAL, NO DOOR LIGHTS ON. SOUND AND VIBRATION DECREASED AT LOWER SPEEDS. ACFT GROUNDED. DURING TAXI OBSERVED EXTERNAL POWER DOOR OPEN. GVI OF NOSE ARSDR ASAA2018010223068Warning Light · false activationLIGHT ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. SPCU INOPERATIVE LOGGED. CYCLED POWER & CLEARED FAULT. OP CHECKED NORMAL IAW FIM 24-34 TASK 802.SDR ASAA2018010123069Antenna · vibrationON APPROACH, WITH THE GEAR UP AND THE FLAPS AT 5, OBSERVED PWS FAIL ON BOTH NAV DISPLAYS ACCOMPANIED BY A LOUD LOW FREQUENCY RUMBLING VIBRATION IN THE RADOME/NOSE GEAR AREA. THIS CONTINUED THROUGH GEAR EXTENSION, LANDING AND TAXI. AND CONTINUED WHILE PARKED WSDR ASAA2017123023029Control Panel · faultedAIRCRAFT CONFIGURED FOR LANDING, SPEED 150 KTS, A RUMBLE AND VIBRATION FELT BY BOTH PILOTS FOLLOWED BY PWS FAIL ON BOTH DISPLAYS. ACFT GROUNDED. PERFORMED A WEATHER RADAR SYSTEM BITEIAW FIM 34-43 TASK 801. WEATHER RADAR SYSTEM OPS TESTED IAW AMM 34-43-00-7SDR ASAA2017122823060Probe · failedWHILE PERFORMING T/C 78273000 FOUND ECONOMIC FAULT MSG 77-10842 THE TOP RIGHT EGT SIGNAL (T49.5S1) IS OUT OF RANGE ON THE NR 2 ENGINE. GROUNDED - YES. PERFORMED FIM 77-21 TASK 801. COMPLETED EGT INDICATION SYSTEM TROUBLESHOOTING AND CONNECTOR CLEANING REF AMM SDR ASAA2017122723025Transceiver · faultedWHEN WEATHER RADAR WAS SELECTED ON CAPTAIN`S OR FIRST OFFICER`S SIDE, A LOUD RUMBLING NOISE AND VIBRATION FELT IN THE FLIGHT DECK. AMBER WEATHER CODE & PREDICTIVE W/S FAIL ON DU. ACFT GROUNDED. COULD NOT DUPLICATE. DUE TO HISTORY, REMOVED, REPLACED, AND TSDR ASAA2017122523010Radar · malfunctionedRADAR AUTO MODE, FALSE RETURNS FM 80-200 NM. MANUAL MODE ONE DEGREE UP FOR ACCURATE WEATHER RETURNS. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, WEATHER RADAR GROUND VERIFICATION TEST PASSED IAW AMM 34-43-00. LONG RANGE DISPLAY AND FUNCTIONS WHEN COMPARED WISDR ASAA2017122222993Antenna · failedPWS FAIL LIGHT ILLUMINATED ON MFD, COINCIDED WITH STRONG VIBRATION FROM BELOW BOTH PILOTS FEET. ACFT GROUNDED. CONFIRMED FLOOR VIBRATION WHEN WX RADAR TURNED ON OR THROTTLES MOVED FORWARD. ACFT CHECKED. COMPLIED WITH SP-2, PULLED AND COLLARED WX RADAR R/T ISDR ASAA2017121522937Probe · failedWHILE PERFORMING T/C 78273000 FOUND F/C 73-31372 NR 2 ENGINE. ACFT GROUNDED. PERFORMED FIM 77-21 TASK 801. COMPLETED EGT INDICATION SYSTEM TROUBLESHOOTING AND CONNECTOR CLEANING IAW AMM 77-21-00-140-801. PERFORMED T49.5 AND EGT SYSTEM INSPECTION IAW AMM 77SDR ASAA2017121322901Unknown · unknownHF RADIO #1 & #2 TRANSITION AND RECEIVES SLIGHTLY OFF OF FREQUENCY, FOR BOTH CAPTAIN AND FIRST OFFICER, TRANSMITTING AND RECEIVING IS ACCEPTABLE/SERVICABLE/USABLE. GROUNDED - YES. REF B737-800 FIM TASK 23-11 TASK 801 PERFORMED BIT CHECK OF HF SYSTEM, NO FAULTSSDR ASAA2017120822841Screw · worn#2 ENGINE FAN DUCT PANEL AT 3 O'CLOCK POSITION AFT UPPER SCREW WORN THRU PANEL. GROUNDED - YES. REPLACED FAN DUCT PANEL AT 3 O'CLOCK POSITION ON #2 ENGINE REF B737-800 AMM 72-23-07.SDR ASAA2017120522842Probe · failedECONOMIC FAULT WHILE PERFORMING TASK CARD 78273000 #2 ENGINE S/N 869-209 FAULT # MS 73-313272 UPPER EGT SECTORS READING HIGH FAULT LEG #4. GROUNDED - YES. PERFORMED B737-800 FIM 77-21 TASK 801. COMPLETED EGT INDICATION SYSTEM TROUBLESHOOTING AND CONNECTOR CLESDR ASAA2017111122529Seal · missingWHILE ACCOMP T/C 78472002 (FAN LUBE) NR 2 ENG FOUND PLATFORMS ELASTOMER SEAL MISSING MORE THAN 39.7 INCHES. GROUNDED - YES. INSTALLED NEW PLATFORMS AS PER TASK CARD 78472002, REF AMM 72-21-02. REF TASK CARD 78472002 FOR VIBE SURVEY ACCOMPLISHMENT.SDR ASAA2017101922269Switch · failedAUTOPILOT B AND CWS B INOPERATIVE. ACFT GROUNDED. LAST LEG FCC B FAULTS, FO AUTOPILOT DISC SWITCH FCCB J1B K07. IAW WDM 22-11-12, PG 3, SH 2, GOOD 28 VOLTS AT TB806 X A14 - 0 VOLTS AT XA13. REMOVED & REPLACED THE CAPTAIN'S AUTOPILOT DISCONNECT SWITCH S231 ISDR ASAA2017073021496Seal · missingWHILE PERFORMING FAN BLADE LUBRICATION ON THE NR 1 ENGINE, STEP 33 FOUND PLATFORM ELASTOMER SEAL MISSING. TOTAL LENGTH 41.00 INCHES. ACFT GROUNDED. REMOVED AND REPLACED IAW AMM 72-21-02-00-000-801-F00. ACCOMPLISHED TEST 7 VIBRATION SURVEY IAW AMM 71-00-00-7SDR ASAA2017071721404Valve · failedNR 2 BLEED TRIP OFF LIGHT ILLUMINATED AT FL 380, RESET IAW QRH. LIGHT REMAINED EXTINGUISHED. WHEN LIGHT CAME ON, LEFT DUCT PRESSURE 35 PSI, RIGHT 10 PSI. BOTH AT 35 PSI AFTER RESET. ACFT GROUNDED. ACCOMPLISHED ENGINE BLEED AIR SYS HEALTH CHECK IAW T/C NG-NGSDR ASAA2017071521393Fuel Heater · leakingNR 2 ENGINE, FUEL HEATER SERVO LEAKING FUEL FROM UPPER GASKET. FOUND DURING IDLE LEAK CHECK. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 ENG FUEL SERVO HEATER IAW AMM 73-11-07-000-801-F00 AND 73-11-07-400-801-F00. FUEL SERVO HEATER LEAK CHECKED GOOD.SDR ASAA2017062121146Fmc · faultedDURING TAXI IN, THE LEFT FMC FAILED. DUAL OPS RESTORED AFTER 2 MINUTES. ACFT GROUNDED. PERFORMED FMC BITE PROCEDURE IAW FIM 34-61 TASK 801. FOUND THE LEFT FMC PROGRAM FAULT, INFLIGHT FAULTS. ACCOMPLISHED FAULT PROCEDURE FIM 34-61, TASK 807. NO FURTHER SDR ASAA2017061421079Warning Light · false indicationDURING THE AFTER START RECALL CHECK THE CONT CAB ZONE TEMP LIGHT ILLUMINATED AFTER QRH PROCEEDURES THE ZONE TEMP LIGHT EXTINGUISHED BUT WOULD REILLUMINATE ON RECALL. ACFT GROUNDED. PERFORMED FIM 21-62 TASK 845. WHILE OPERATING PACKS, ZONE TEMP LIGHT DID NOT ISDR ASAA2017051620790Lens · brokenFLOOR LIGHT BY L1 DOOR BROKEN. ACFT GROUNDED. REMOVED AND REPLACED THE LIGHT COVER.SDR ASAA2017050720672Trim Motor · failedAFTER TAKEOFF (THEN 1500 FT) ELECTRIC TRIM FAILED. UNABLE TO OPERATE ELECTRIC TRIM WITH EITHER YOKE SWITCH. GROUNDED - YES. REMOVED AND REPLACED STAB TRIM MOTOR. OPS CHECK GOOD, REF AMM 27-41-71, 27-40-71-700-801, AND 22-11-81-710-801. OPS CHECK GOOD.SDR ASAA2017041220439Unknown · unknownWHEN PRESSING TOGA, ONLY ONE POWER LEVER ENGAGES THEN AUTOTHROTTLES DISENGAGE. ACFT GROUNDED. RESET SYSTEM, OPS CHECKED GOOD IAW AMM 22-31-00-710-801, AND 22-31-00-710-802.SDR ASAA2017022719956Control Valve · failedDURING MASTER CAUTION RECALL, CONTROL CABIN ZONE TEMP LIGHT ILLUMINATED, EXTINGUISHED ON MASTER CAUTION RECALL. ACFT GROUNDED. CONFIRMED DEFECT. BITE OF LEFT AND RIGHT PACK/ZONE TEMP CONTROLLERS IAW FIM 21-62 TASK 801. SHOWED FAULT FOR CONTROL CABIN TRIM ASDR ASAA2017022619943Control Valve · failedCONTROL CABIN ZONE TEMP ILLUMINATED ON RECALL. CLEARS ON MASTER CAUTION RESET. ACFT GROUNDED. CONFIRMED DEFECT - BITE OF LEFT AND RIGHT PACK/ZONE TEMP CONTROLLERS IAW FIM 21-62 TASK 801. SHOWED FAULT FOR CONTROL CABIN TRIM AIR VALVE LOGGED ON BOTH RIGHT (PRISDR ASAA2017022619946Warning Flag · false activationYELLOW FD FLAG ON CAPTAIN'S HSI. ACFT GROUNDED. PERFORMED DFCS CURRENT STATUS ON "A" CHANNEL & NO FAULTS FOUND. FD FLAG EXTINGUISHED AFTER BITE CHECK, IAW AMM 22-11-00-740-801.SDR ASAA2017022519926Compensator · out of toleranceREF ASA TASK CARD NG-28FCD-18090-1 FOUND 11 PROBES OUT OF TOLERANCE, F15,F1,,F2,F3,F4,F5,F6,F7,F8,F9 AND F10 IN TANK 2. ACFT GROUNDED. R & R COMPENSATOR AND TANK UNITS IAW AMM 28-41-21. SYSTEM TEST FUEL QTY INDICATION SYSTEM TESTED NORMAL IAW AMM 28-41-00-730SDR ASAA2017022519925Compensator · out of toleranceFOUND EIGHT PROBES OUT OF TOLERANCE IN TANK 1. ACFT GROUNDED. R & R THE PROBES IAW AMM 28-41-21. SYSTEM OPS TESTED NORMAL IAW AMM 28-41-00.SDR ASAA2017021319798Cdu · failedFIRST OFFICER`S CDU WENT BLANK IN FLT. ACFT GROUNDED. POWER CYCLE & MCDU REMAINED BLANK. REMOVED & REPLACED THE MCDU. OP CHECKED NORMAL. IAW AMM 34-61-01-00-802, & 34-61-01-400-802.SDR ASAA2016122719171Autothrottle Sys · malfunctionedAUTO THROTTLES DISENGAGED ON IT`S OWN AND WOULD NOT REENGAGE. ACFT GROUNDED. DFGS FAULT REVIEW SHOWS THE FOLLOWING FAULT FOR THAT FLIGHT. FGN FAILS TO ENT TO TO GA, FCC-A. MSG 22-11209. ACCOMPLISHED FIM 22-11 TASK 801, NO FAULTS. NO FAULTS IN A/T HISTORY.SDR ASAA2016121018985Sensor · failedLEFT FWD WINDOW OVHT LIGHT ILLUMINATED WHEN POWER APPLIED. ACFT GROUNDED. L1 WHCU SHOWS SENSOR FAULT. SWITCHED SENSOR SND FROM AUX TO PRO. STILL SHOWS SENSOR FAULT. BOTH PRO & AUX TEMP SENSOR RING OPEN FROM L1 WHCU. MANY FINE CRACKS ACROSS TEMP SENSORS IN L1SDR ASAA2016111118621Charger · failedBATTERY DISCHARGE LIGHT ILLUMINATED FOR GREATER THAN ONE MINUTE. DID NOT EXTINGUISH WITH GROUND POWER APPLIED. ACFT GROUNDED. REMOVED AND REPLACED THE MAIN BATTERY CHARGER IAW AMM 24-31-21 OPS CHECKED NORMAL.SDR ASAA2016092918157Autothrottle Sys · malfunctionedAUTOTHROTTLES DISENGAGED INFLIGHT WOULD RE-ENGAGE. ACFT GROUNDED. VERIFIED FAULT 22-31687 FOUND IN INFLIGHT FAULTS DURING AUTO THROTTLE FAULT REVIEW. PERFORMED FIM 22-32 TASK 819 INITIAL EVALUATION AND FAULT DID NOT RE-OCCUR IN CURRENT STATUS AFTER AUTOTHROSDR ASAA2016091918080Starter · failedNR 2 ENGINE WOULD NOT START. START PRESSURE DUCT 40 PSI, N2 REACHED 3% AND THEN 0%. ABORTED ENGINE START. GROUNDED - YES. REMOVED AND REPLACED NR 2 ENGINE STARTER, IAW AMM 80-11-01. OPS AND LEAK CHECK GOOD. SERVICED STARTER, IAW AMM 80-11-01.SDR ASAA2016082817833Circuit Breaker · trippedPWS FAIL ILLUMINATED ON NAV DISPLAY WHEN WEATHER RADAR SELECTED, BOTH POSITIONS FAIL AND WEATHER RADAR FAIL ARE DISPLAYED ON NAV DISPLAY, WEATHER RADAR WILL NOT TEST. ACFT GROUNDED. FOUND WEATHER RADAR CIRCUIT BREAKER OUT. RESET CIRCUIT BREAKER, GROUND FUNCSDR ASAA2016082217783Idg · defectiveFOLLOW-UP TO NR 2 IDG CONTINUED FREQUENT SERVICING. ACFT GROUNDED. NR 2 ENGINE IDG OIL WAS AT ADD. CLEANED CONNECTORS, ACCOMPLISHED IDG OIL SYSTEM STATIC LEAK CHECK, NO LEAKS FOUND, REF AMM 24-11-00 IAW TSR REPLACED NR 2 ENGINE IDG. NO LEAKS, OPS CHECK GOOSDR ASAA2016081917753Unknown · malfunctionedSATCOM LOCK-UP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL, REF AMM 23-15-00.SDR ASAA2016072117459Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE PER QRH. SATCOM RESTORED NORMAL.SDR ASAA2016071417389Fire Detector · failedAPU DETECTOR INOPERATIVE LIGHT ILLUMINATED. ACFT GROUNDED. REMOVED AND INSTALLED NEW TAIL APU FIRE DETECTOR. PERFORMED APU FIRE DETECTION TEST IAW AMM 26-15-00-710-801. SYSTEM CHECKED NORMAL.SDR ASAA2016061617058Circuit Breaker · poppedTR UNIT LIGHT ILLUMINATED. ACFT GROUNDED. BITE CHECK OF P5-13 MODULE FAULTS TR1. FOUND TRU 1 C/B OUT ON P91, A6. RESET C/B, REF AMM 20-60-01. TR UNIT LIGHT NOW EXTINGUISHED. PERFORMED FIM 24-31, TASK 826 WITH NO DEFECTS NOTED.SDR ASAA2016060516951Pump · failedRT CENTER TANK FWD PUMP LOW PRESSURE LIGHT STAY ILLUMINATED WITH THE PUMP ON AN 1500 LBS AT THE CENTER FUEL. ACFT GROUNDED. REMOVED CONNECTOR D804 AT RT CENTER PUMP, CLOSED C/B AND TURNED PUMP ON, C/B STAYED CLOSED. ACCOMPLISHED A/C VOLT CHECKS AT D804, NO SDR ASAA2016051616856Channel · crackedAFT CARGO COMPARTMENT, RT ZEE CHANNEL SECTION BS 727F TO BS 767 IS CRACKED. ACFT GROUNDED. R & R DAMAGED ZEE CHANNEL SECTION 727E +10 TO 7 IAW SRM 53-00-553-2R-5 AND DWG 146A7500, REV.SDR ASAA2016051616838Channel · corrodedAFT CARGO COMPARTMENT, LT ZEE CHANNEL HAS CORROSION BS 727A TO 847. ACFT GROUNDED. BLENDED CORROSION ON LT SIDE 727A-847 TO BE WITHIN LIMITS, ORIGINAL MATERIAL .040". REMOVED .002, REMAINING .038, EXCEPT 727D-BS 727, BEYOND LIMITS ORIGINAL MATERIAL .040". REMSDR ASAA2016051616828Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN, .5" CRACK FOUND AT STABILIZER BS 129, 9.5" AFT OF FORWARD SPAR. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER LOWER SKIN AT STABILIZER BS 129. 9.5, AFT OF FWD SPAR IAW SRM 55-10-01-2R-11.SDR ASAA2016051516855Web · corrodedAFT CARGO DOOR SURROUND LOWER MAIN SILL WEB IS CORRODED. ACFT GROUNDED. BLEND AFT CARGO LOWER MAIN SILL WEB ORIGINAL THICKNESS .045 IAW DWG 146A-8123, REV A. MATERIAL LOSS .009" REMAINING THICKNESS .036" FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. R & R LWSDR ASAA2016031215865Autothrottle Sys · malfunctionedAUTO THROTTLE WOULD NOT STAY ENGAGED. ACFT GROUNDED. NR 1 THROTTLE LEVER DOES NOT RESPOND TO SERVO MOTOR TEST. MULTIPLE ASM 1 FAULTS. CYCLED AUTOTHROTTLE DC1 C/B. SYS RESTORED. SERVO MOTOR TEST PASS, A/T OPS CHECK IAW AMM 22-31-00 PASS AND DFCS BITE GRP SDR ASAA2016030315746Autoland Sys · malfunctionedAUTOLAND UNSUCCESSFUL: AT 100' AGL ACFT DRIFTED WELL LT OF CENTERLINE AND LANDED OUTSIDE THE TOUCHDOWN ZONE LT. THERE WAS A LT CROSSWIND OF 8 KTS. ACFT GROUNDED. PERFORMED FIM 22-11, TASK 825 - NR 49 BITE LAND VERIFY TEST WITH NO FAULTS. HOUSING SYSTEM, OPSSDR ASAA2016022115609Exciter · failedON GROUND TRIED TO START APU, WOULD NOT START W/ FAULT LIGHT ILLUMINATED. AFTER 5 MINUTES FAULT LIGHT EXTINGUISHED. ACFT GROUNDED. R & R APU IGNITION UNIT REF AMM 49-41-31, R & R APU IGNITION LEAD REF AMM 49-41-52. OPS CHECK NORMAL, APU STARTS NO CURRENT
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