N587AS
Service difficulty reports · 482
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 = 'N587AS' 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 = 'N587AS' 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 ASAA2017122823023Anti-Ice Valve · failedNR 2 TAI INDICATION AMBER AFTER ENGINE START AND ANTI-ICE SELECTED ON. ACFT GROUNDED. REMOVED AND REPLACED THE NR 2 TAI VALVE IAW AMM 30-21-11/401. OPS TESTED GOOD. LEAK CHECKED GOOD. ALL INDICATIONS NORMAL. PERFORMED BONDING TEST. BONDING TESTED GOOD IAW AMSDR ASAA2017121622928Warning Light · false activationAFTER ENGINE START "ELEC" LIGHT ON OVERHEAD PANEL ILLUMINATED. ACFT GROUNDED. PERFORMED FIM 24-31 TASK 801 & LOGGED SPCU INOPERATIVE FAULT. PERFORMED FIM 24-34 TASK 804 & FAULT CLEARED. BITE CHECK PASSED & GROUND FUNCTIONAL CHECKED GOOD.SDR ASAA2017121522941Pin · out of positionDURING ACCOMPLISHMENT OF E/C SBCFM56-7B-72-0986 ENG S/N #2 ENG FOUND STAGE NR 2 ANTI-ROTATION PIN AT 9 O'CLOCK ROTATED ABOUT 80 DEG. ACFT GROUNDED. REPLACED THE NR 2 ENGINE IAW T/C 7847100, & 78471001.SDR ASAA2017113022734Oil Cooler · leaking#2 ENGINE IDG AIR/OIL COOLER LEAKING. GROUNDED - YES. REMOVED AND REPLACED THE #2 ENGINE IDG AIR/OIL COOLER, LEAK CHECK GOOD, REF B737-800 AMM 24-11-21/401.SDR ASAA2017112222679Warning Light · false activationR1 WINDOW OVERHEAT LIGHT ON. ACFT GROUNDED. RESET THE SYSTEM AND PERFORMED WINDOW HEAT SYSTEM OPERATIONAL TEST IAW AMM 30-41-00-710-801. R1 WINDOW OVERHEAT LIGHT EXTENGUISHED. TESTED MULTIPLE TIMES, LIGHT REMAINED OUT. NO OTHER DEFECTS WITH SYSTEM NOTED.SDR ASAA2017111922647Fmc · failedEXPERIENCED 4 DUAL FMC FAILURES WITHIN AN HOUR. EACH TIME THE FMCS RECOVER BUT DUMPED ALL FMC DATA. NO FAILURES EXPERIENCED WITHIN LAST 3 HOURS OF FLIGHT. ACFT GROUNDED. REPLACED THE LT AND RT FMC COMPUTERS IAW AMM 34-61-02-400-801. LOADED ALL SOFTWARE IAW ASDR ASAA2017110622462Unknown · unknownAPU FAULT LIGHT ILLUMINATED DURING ATTEMPTED TO START AT THE GATE. QRH PROCEDURE ACCOMPLISHED. LIGHT WENT OUT. SECOND START ATTEMPT WAS SUCCESSFUL. GROUNDED. OPS CHECKED APU, APU STARTED 1ST TRY, OPS NORMAL, NO HISTORY.SDR ASAA2017100822131Pitot Tube · shortedAFTER ENGINES STARTED THE LT ELEVATOR PITOT LIGHT ILLUMINATED. ACFT GROUNDED. IAW WDM 30-31-11 FOUND THE LT ELEVATOR PITOT HEATER OPEN D644 PIN 40 TO GND OPEN. REPLACED LT ELEVATOR PITOT TUBE IAW AMM 27-31-94-000-801 & -400-801. OPS NORMAL. LEAK CHECKED GOODSDR ASAA2017091622028Transition Panel · corrodedAFT CARGO BAY, LT TRANSITION PANEL UPPER AND LOWER SURFACES, SEVERAL AREAS CORROSION, BS 727 - 790, LBL 20 - 20.5. ACFT GROUNDED. REMOVED THE CORROSION IAW SRM 53-00-53. FOUND TO BE OUT OF LIMITS. REMOVED THE TRANSISTION PANEL AND FABRICATED A NEW TRANSDR ASAA2017091621992Transition Panel · crackedAFT CARGO BAY RT TRANSITION PANEL CRACKED BS 727J, RBL 22. ACFT GROUNDED. REMOVED THE TRANSITION PANEL, FABRICATED A NEW TRANSITION PANEL IAW SRM 53-00-53-2R-5, REPAIR 5. ALODINED AND PRIMED IAW SRM 51-20-01, AND INSTALLED IAW SRM 53-00-53-2R-5, REPAIR 5.SDR ASAA2017091521991Floor Skin · dentedCOCKPIT FLOOR DENTED BS 263 - 264, BL 0. ACFT GROUNDED. REPAIRED THE FLOOR WEB IAW SRM 53-10-51-2R-2.SDR ASAA2017091521976Support Bracket · crackedFORWARD CARGO COMPARTMENT, LT INTERCOSTAL AT STRINGER 25L STA 500H HAS CRACKED SUPPORT ANGLES ON FWD AND AFT SIDE. GROUNDED - YES. REMOVED AND REPLACED SUPPORT BRACKETS AT STA 500H LT FWD AND AFT SIDES IAW BAC DWG 143A7505 REV A.SDR ASAA2017091521974Support Bracket · crackedFORWARD CARGO COMPARTMENT, LT INTERCOSTAL AT STRINGER 25L STA 500G HAS CRACKED SUPPORT ANGLES ON FWD SIDE. GROUNDED - YES. REMOVED AND REPLACED SUPPORT BRACKET STA 500G LT FWD SIDE IAW BAC DWG 143A7505 REV A.SDR ASAA2017083121771Warning Light · illuminatedDURING THE NR 1 ENGINE SHUTDOWN , AN EGT RED BOX APPEARED. THIS WAS A TAKEOFF EXCEEDANCE. ACFT GROUNDED.SDR ASAA2017072921484Control Valve · failedAFTER TAKE OFF. LEFT PACK LIGHT ILLUMINATED. ACCOMPLISHED QRH. PACK LIGHT DID NOT RESET. TURNED OFF THE LEFT PACK AND CLOSED ISOLATION VALVE. LEVELED OFF AT FL 250. ACFT PRESSURIZED NORMALLY. ACFT GROUNDED. PACK ZONE TEMP CONTROLLER 1 SHOWS TCV FAULT LASSDR ASAA2017072921483Warning Light · false activationON APPROACH, AUTO FAIL LIGHT ILLUMINATED. SWITCHED TO ALTERNATE MODE. CONTINUED NORMALLY. ACFT GROUNDED. CABIN PRESSURE CONTROLLER NR 1 AND 2 FAULT LOW INFL/HIGH LEAKAGE. ACCOMPLISHED PRESSURIZATION CONFIDENCE CHECK.IAW AMM 21-00-05-780-801. OPS CHECKED GOODSDR ASAA2017071521385Sensor · failedFORWARD RIGHT OVERHEAT LIGHT ILLUMINATED ON GROUND. GROUNDED - YES. SWITCHED RIGHT FORWARD WINDOW SENSOR TO THE SPARE SENSOR IAW FIM 30-41, TASK 812. RIGHT FORWARD WINDOW HEAT DETECTION OPS CHECKED GOOD.SDR ASAA2017052120847Warning System · false activationFAULT LIGHT ILLUMINATED DURING APU START. FOLLOWED QRH. AFTER 5 MIN RE-ATTEMPTED START AND LIGHT ILLUMINATED AGAIN. GROUNDED - YES. APU LAST FLIGHT LEG FAULT HISTORY SHOWS FAULT LIGHT MAINTENANCE MESSAGE 49-61157, ECU INTERNAL FAILURE. PERFORMED APU BITE PER FSDR ASAA2017051720815Shim · wornALL 24 BLADE SHIMS FOUND TO BE WORN ON THE NR 1 ENGINE. ACFT GROUNDED. REMOVED AND REPLACED THE BLADE SHIMS IAW T/C 78472002.SDR ASAA2017051720814Cone · wornNR 1 ENGINE FRONT SPINNER CONE PAINT WORN BELOW LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE FRONT SPINNER CONE IAW T/C 78072002.SDR ASAA2017051320722Control Panel · malfunctionedMCP N1 BUTTON DOES NOT ILLUMINATE. ACFT GROUNDED. CONFIRMED N1 BUTTON LIGHT DOES NOT ILLUMINATE WHEN PRESSED. ACCOMPLISHED ALT DEACTIVATION IAW CHAPTER 5, TABLE 3, ITEM 1. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34-401. ACCOMPLISHED OPS TESTSDR ASAA2017050820690Pcu · failedTRU UNIT LIGHT ILLUMINATED ON PREFLIGHT. GROUNDED - YES. VERIFIED DISCREPANCY T3 LIGHT ON. REMOVED AND INSTALLED NEW TR3 UNIT, REF FIM 24-31 TASK 826. PERFORMED TR3 OPS TEST - NO HELP, REF AMM 24-32-11. REMOVED AND INSTALLED NEW SPCU, REF AMM 24-34-11. PERFORMSDR ASAA2017050320627Controller · malfunctionedREF MEL 21-32B RH PACK LIGHT FAILS TO EXTINGUISH AFTER RECALL AND MASTER CAUTION RESET. GROUNDED - YES. REF AMM FIM TASK 21-61-801 RESET BOTH ZONE TEMP CONTROLLERS ALL FAULTS CLEARED MASTER CAUTION LT NOW DOES NOT ILLUMINATE AND EXTINGUISHED OK FOR CONTINUED SSDR ASAA2017050220612Unknown · malfunctionedRT PACK LIGHT FAILED TO EXTINGUISH AFTER RECALL AND MASTER CAUTION RESET. GROUNDED - YES. REF AMM TASK 21-61-801. PERFORMED TEMP CONTROLLER BITE, CLEARED FAULTS, RESET SYSTEM. PACK TEMP CONTROL IN CABIN NOW RESETS WITH MASTER CAUTION. OK FOR SERVICE.SDR ASAA2017050120591Control Valve · failedRIGHT PACK LIGHT WAS ILLUMINATED AFTER TAKEOFF. PACK LIGHT EXTINGUISHES WHEN MASTER CAUTION RESET IS PUSHED. GROUNDED - YES. PERFORMED RT PACK ZONE TEMP CONTROLLER BITE AND FOUND TCV FAULT IN VERIFY ONLY, REF AMM 21-51-00. REMOVED AND REPLACED RT PACK TEMP CONSDR ASAA2017042020501Unknown · malfunctionedSATCOM INOPERATIVE. GROUNDED - YES. ACCOMPLISHED SATCOM TST REF AMM 23-15-00-780-801. OPS TST NRML PER SAME. NO HISTORY LAST 30 DAYS. CLEARED MEL 23-18.SDR ASAA2017032620273Module · failedSUPPLY DUCT IN FWD AND CONTROL CABIN INDICATED 100+ DEGREES. INDICATION FLUCTUATED, NO ZONE TEMP LIGHTS. ACFT GROUNDED. REMOVED & REPLACED TEMP CONTROL MODULE P5-17 IAW AMM 21-61-15 & 401. CHECKED GOOD IAW AMM TASK 21-61-00-700-807-002. OPS NORMAL.SDR ASAA2017032620270Filter · contaminatedAIR TEMP CONT CAB IN "FWD" POSITION INDICATES 100+ AT CRUISE. FLIGHT ATTENDANT REPORTS HOT AIR IN CABIN ROWS 6-10. GAUGE FLUCTUATES AT TIMES WHEN IN FWD AND CONT CAB POSITION. GROUNDED - YES. INITIAL EVALUATION SHOWED ALL GAUGE READINGS NORMAL. SUSPECT INTERMISDR ASAA2017031420173Selector Switch · looseAIR TEMPERATURE SOURCE SELECTOR SWITCH INDICATES ERRATIC TEMP IS WHEN MOVED. ACFT GROUNDED. FOUND AIR TEMP SELECTOR SWITCH EXTREMELY LOOSE IN PANEL. REMOVED CONTROL PANEL LIGHT PLATE, NUT SECURING SWITCH TO PANEL WAS 5 FULL TURNS FROM TIGHT. TIGHTENED THE NUSDR ASAA2017021619867Shim · wornNR 2 ENGINE FAN BLADE SHIMS 24 EA REQUIRE REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED ALL 24 SHIMS ON NR 2 FAN BLADES REF TASK 78472002.SDR ASAA2017021419819Probe · faultyENGINE 1 SHOW ECONOMIC FAULT. EGT SIGNAL IS OUT OF RANGE. BOTTOM LEFT. GROUNDED - YES. NR 1 ENGINE FAULT 77-20861 WAS LOGGED ON ALL TEN STARTS IN EEC MEMORY AND INPUT MONITORING SHOWED BOTTOM LEFT PROBE (T495S3) TO BE ALL DASHES. REMOVED AND REPLACED BOTTOM LESDR ASAA2017012419541Bushing · wornNR 1 ENGINE BLEED DUCT INTERSECTION HAS WORN BUSHING AT SUPPORT ROD. ACFT GROUNDED. REMOVED THE INTERSECTION DUCT AT NR 1 ENGINE IAW AMM 36-11-01-000-802 STEP E. INSTALLED NEW INTERSECTION MANIFOLD DUCT ON NR 1 ENGINE IAW AMM 36-11-01-400-802.SDR ASAA2017011119319Control Valve · failedLEFT PACK LIGHT ILLUMINATES ON RECALL, WILL RESET WITH MASTER. GROUNDED - YES. REMOVED AND REPLACED LEFT PACK PRIMARY TEMP CONTROL VALVE REF AMM 21-51-10. PACK/ZONE TEMP CONTROLLER BITE TEST SATISFACTORY. REF AMM 12-61-00. LEAK CK. GOOD. CLEARS MEL 21-32B.SDR ASAA2017010219233Lens · brokenEMERGENCY LIGHT LENS ON INSIDE OF L1 DOOR BROKEN. ACFT GROUNDED. REMOVED AND REPLACED THE LENS.SDR ASAA2016122019108Filter · contaminatedNR 2 IDG DPI TRIPPED. ACFT GROUNDED. COMPLETED NR 2 IDG DPI INSPECTION IAW AMM 12-13-21. REMOVED AND REPLACED THE NR 2 IDG FILTERS IAW AMM 12-22-41. LEAK CHECKED OK.SDR ASAA2016120219327Fuel Nozzle · wornMESSAGE 73-31371 FOR UPPER EGT SECTORS READING HIGH ILLUMINATED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 ENGINE FUEL NOZZLES, IAW TC 73CMPT-07267-2 AND EA 800-36EA-18334.SDR ASAA2016112218810Idg · malfunctionedDURING PDC, FOUND THE NR 2 IDG DPI TRIPPED. ACFT GROUNDED. PERFORMED FIM 24-11 TASK 803 ALONG WITH AMM 24-11-41-200-801 & AMM 24-11-41 IDG SCAVENGE FILTER INSP & CHANGE. NO DEFECTS NOTED. LEAK CHECKED GOOD. FIRST DPI RESET ON NR 2 IDG.SDR ASAA2016111818745Bracket · brokenNR 1 ENGINE RIGHT FAN COWL ALIGNMENT BRACKET AT THE 6 O'CLOCK POSITION FOUND BROKEN. ACFT GROUNDED. REMOVED THE BRACKET, POSITIONED NEW BRACKET IAW AMM 20-50-11.SDR ASAA2016110918616Display · defectiveCAPTAIN`S MCP CRS SELECTOR WINDOW HAS DAMAGED SEGMENTS. ACFT GROUNDED. REMOVED & REPLACED THE MODE CONTROL PANEL IAW AMM 22-11-34, INSTALLATION TEST PASSED. ACCOMPLISHED DFCS LRU INTERFACE TEST FOR MCP 32, LAND VERIFY TEST 49 & HGS SENSOR TEST FOR FCC/AT IAWSDR ASAA2016100318203Compensator · failedDURING 800-28EA-16443, FOUND THE NR 1 FUEL QUANTITY FAILS SYSTEM TEST IAW AMM TASK 28-41-00-730-801. ACFT GROUNDED. REPLACED THE TANK UNIT NR 1 AND COMPENSATOR PROBE. FQIS READS NORMAL IAW AMM 28-41-21, AND 28-41-00.SDR ASAA2016100318202Compensator · failedDURING 800-28EA-16443, FOUND THE NR 2 FUEL QUANTITY FAILS SYSTEM TEST IAW AMM 28-41-730-801. ACFT GROUNDED. ACCOMPLISHED TANK AND COMPENSATOR TEST IAW AMM 28-41-21. FOUND F15R COMPENSATOR AND F1R, F8R, F9R, AND F10R BAD. REMOVED AND REPLACED TANK AND COMPENSDR ASAA2016092018088Window · malfunctionedOVERHEAT LIGHT ON FOR LH FWD WINDOW. ACFT GROUNDED. REPLACED LT NR 1 WINDOW IAW AMM 56-11-11-000-801 AND 56-11-11-400-801. GROUND VERIFICATION OF WINDOW HEAT IS GOOD.SDR ASAA2016083117876Anti-Ice Valve · failedDURING DESCENT, ENGINE ANTI-ICE TURNED ON. COWL VALVE OPEN LIGHT REMAINED ON. AMBER TAI ON ENGINE DISPLAY INDICATING ANTI-ICE VALVE FAILED CLOSED. CONFIRMED WITH FLIGHT CREW NR 2 ENGINE WAS THE ISSUE. ACFT GROUNDED. REPLACED NR 2 ENGINE INLET COWL ANTI-ICSDR ASAA2016083017867Connector · broken28 VOLT DC CHARGER HAD BRIEF ELECTRICAL ODOR WHEN PLUGGED INTO SERVICE OUTLET. REMOVED AND NO LONGER HAD ODOR THOUGH OUTLET PLUG NO LONGER HAS GROUND ATTACHED. ACFT GROUNDED. 28 VOLT DC CHARGER IS INOPERATIVE, GROUND CONNECTOR BROKEN. IAW WDM 25-29-11, CONFSDR ASAA2016082917841Controller · malfunctionedFLIGHT DECK ZONE TEMP LIGHT ILLUMINATES ON RECALL, EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. NR 2 ZONE TEMP CONTROLLER LOGGED FLIGHT DECK TRIM VALVE FAULT. RESET FAULT. ACCOMPLISHED ZONE TEMP CONTROLLER BITE IAW AMM 21-61-00,TEST PASSED.SDR ASAA2016082817832Actuator · leakingDURING POST RUN LEAK CHECK FOR NR 2 HPTACC VALVE CHANGE, FOUND RT VSV LEAKING AT A RATE OF 4 DROPS PER MINUTE. ACFT GROUNDED. R & R RT VSV ACTUATOR, REF AMM 75-31-01. ACCOMPLISHED VSV ACTUATOR LEAK TEST ON NR 2 ENGINE, RT VSV ACTUATOR NO LEAKS NOTED, REF AMSDR ASAA2016082717825Engine · faultedFOUND ECONOMIC FAULT NR 1 ENGINE 73-31371 UPPER EGT SECTORS READING HIGH. ACFT GROUNDED. FOUND FAULT ON LEG 6 ONLY. ACCOMPLISHED NR 1 ENGINE EGT INDICATING SYSTEM CLEANING IAW AMM 77-21-00-140-801. INTERROGATED NR 1 EEC, NO RECENT FAULTS LOGGED.SDR ASAA2016071417386Charger · failedDURING PREFLIGHT, DISCOVERED ELECTRIC LIGHT ILLUMINATED. ACFT GROUNDED. BITE CHECK OF P5-13 SHOWS AUX BATTERY CHARGER INOPERATIVE. REPLACED AUX BATTERY CHARGER IAW AMM 24-31-31. INSTALLATION TEST NORMAL.SDR ASAA2016071417385Charger · warning messageELECTRIC LIGHT WITH MASTER CAUTION ELECTRIC LIGHT ILLUMINATED ON GROUND AFTER LANDING. ACFT GROUNDED. ACCOMPLISHED SUCCESSFUL GROUND VERIFICATION, PERFORMED ELEC LIGHT MESSAGE BITE IAW FIM 24-31 TASK 801, FAULTED "AUX BATTERY CHARGER INOPERATIVE CLEARED FAUSDR ASAA2016070817325Egt Indication · reads highWHILE PERFORMING TC 78273000, FOUND NR 1 ENGINE TO HAVE ECONOMIC MESSAGE 73-31371 ON FLIGHT LEG 2. NO HISTORY 90 DAYS. ACFT GROUNDED. NOT SHOWING ANY RECENT FAULTS OR LOGGING ANY FAULTS IN FAULT HISTORY. FAULT CODE 73-31371 UPPER EGT SECTORS READING HIGH
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