N584SW
Service difficulty reports · 104
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 = 'N584SW' 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 = 'N584SW' 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 SWIA200819414Bolt · corrodedRIGHT INBOARD FLAP ACTUATOR ROD END BEARING AND BOLT IS CORRODED, FOUND AT C-CHECK. REPLACED ACTUATOR ROD END AND BOLT IAW CMM 27-50-23.
SDR SWIA200819413Bearing · corrodedFOUND AT C-CHECK, RIGHT OUTBOARD FLAP ACTUATOR ROD END BEARING AND BOLT IS CORRODED. REPLACED ACTUATOR ROD END AND BOLT IAW CMM 25-50-23.
SDR SWIA200819412Stringer · crackedLEFT WING AREA NEAR THE NR 2 FUEL PANEL HAS A LEAKING RIVET, FOUND AT C-CHECK. REPAIRED STRINGER 10 IAW EMB 120 SRM 57-20-03.
SDR SWIA200718302Hydraulic Line · leakingLOST GREEN SYSTEM HYDRAULIC FLUID. REPLACED BAD SECTION OF HYDRAULIC PRESSURE LINE IN LEFT OUTBOARD NACELLE. SERVICED HYDRAULIC FLUID TO PROPER LEVEL. OPS AND LEAK CHECKS ARE GOOD.SDR SWIA200718232Inverter · malfunctionedBOTH CAPTAIN AND FIRST OFFICER RECEIVED YELLOW HEADING FLAGS. THEN RED HEADING FLAG. BOTH EHSI'S WERE BETWEEN 50-70 DEGREES OFF OF COMPASS. RETURNED TO SLC, REPLACED NR 1 STATIC INVERTER IAW MM 24-20-01. OPS CHECK GOOD.SDR SWIA200718036Stringer · crackedRT WING IB FIRST PANEL FROM NACELLE HAS SEVERAL LEAKING RIVETS . FOUND STRINGER 8 CRACKED BETWEEN RIBS 7 AND 8. C/W STRINGER 8R REPAIR IAW SRM 57-20-03 AND IAW RII 57-900-1000.SDR SWIA200616623Servo · malfunctionedFLIGHT DIRECTOR WILL NOT FOLLOW COMMAND BARS (+10 TO -5 DEG DISCREP INFLIGHT). REPLACED ELEVATOR PRIMARY SERVO IAW 22-10-05. OPERATIONAL CHECK GOOD.SDR SWIA200616238Fcu · malfunctionedCONTROL FAULT ON FCP DURING FLAP EXTENSION. REPLACED FLAP CONTROL UNIT, OPERATIONAL CHECK GOOD.SDR SWIA200616083Connector · dirtySEGMENT OF EMERGENCY EXIT LIGHTS FAIL TEST. CLEANED CONNECTOR FOR CENTER EMERGENCY LIGHTS BATTERY PACK, OPERATIONAL CHECK GOOD.SDR SWIA200516016Battery · inoperativeFWD "E" LIGHTS GO OUT DURING OPERATIONAL CHECK AFTER THREE SECONDS. REPLACED FORWARD EMERGENCY LIGHT BATTERY IAW MM 33-50-02. OPERATIONAL CHECK GOOD.SDR SWIA200516013Servo · malfunctionedWITH AUTOPILOT SELECTED TO EITHER SIDE "TRIM FAIL" ON MAP AND THEN TRIM STARTED TO ROLL FORWARD. REPLACED ELEVATOR TRIM SERVO MOTOR IAW MM 22-10-05.SDR SWIA200515740Socket · smokeSIDEWALL LIGHT ABOVE SEAT 6A EMITS SMOKE, STRONG ELECTRICAL ODOR AND BURN MARK IN CEILING PANEL. REPLACED LIGHT FIXTURE IN CEILING ABOVE SEAT 6A. OPERATIONAL CHECK GOOD.SDR SWIA200515410Smoke Warning · false activation"SMOKE" LIGHT ON THE MAP ILLUMINATED DURING FLIGHT AS WELL AS THE SMOKE LIGHT AND ALARM IN THE REAR OF THE CABIN. ALL LIGHTS AND ALARMS CEASED AFTER ABOUT 4 MINUTES. FLIGHT ATTENDANT REPORTED NO ODOR OF SMOKE OR FIRE INDICATION IN THE LAV OR CABIN AREA. NO SDR SWIA200515411Seal · dirtyMAIN CABIN DOOR IS DIFFICULT TO OPEN OR CLOSE. REMOVED FOD FROM AROUND DOOR SEAL. NO OTHER DEFECTS FOUND. CYCLED DOOR SEVERAL TIMES. OPERATIONAL CHECK GOOD.SDR SWIA200514796Connector · failedFLAP CONTROL FAULT. REPLACED CONNECTOR ON LEFT AND RIGHT OUTBOARD ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-00.SDR SWIA200514667Actuator · malfunctionedSELECTING FLAPS TO 15 DEGREES GOT A CONTROL FAULT. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09. OPERATIONAL CHECK GOOD.SDR SWIA200514628Actuator · malfunctionedREPEATED FLAP CONTROL FAULTS (APPROX 5) DURING CLIMB, CRUISE, DESCENT. REPLACED LEFT FLAP OUTBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPERATIONAL CHECK GOOD.SDR SWIA200514530Annunciator · malfunctionedREPEATED FLAP CONTROL FAULTS DURING FLIGHT. REMOVED AND REPLACED ANNUNCIATOR WITH SERVICEABLE UNIT IAW 27-50-10. OPERATIONAL CHECK GOOD.SDR SWIA200413690Wire · damagedEMERGENCY EXIT ROW LIGHTING IN ROW 6 INTERMITTENT, BOTH SIDES. REPAIRED WIRING BEHIND (EXIT) SIGN AT ROW 6A. OPERATIONAL CHECK GOOD.SDR SWIA200413646Lamp · burned outRIGHT HAND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED IAW MM 33-52-01, OPERATIONAL CHECK GOOD.SDR SWIA200413425Connector · dirtyAT 500 FT, FLAP AND ADVANCED SWS LIGHTS ON MAP ILLUMINATED. CLEANED AND RE-SAFETIED FLAP CONNECTORS. OPERATIONAL CHECK GOOD.SDR SWIA200413354Selector · malfunctionedDURING FLAP RETRACTION, RECEIVED CONTROL FAULT MESSAGE NUMEROUS TIMES. WOULD NOT RESET. REMOVED AND REPLACED FLAP SELECTOR LEVER ASSY WITH SERVICEABLE. OPS CHECK GOOD.SDR SWIA200413077Control Handle · malfunctionedON APPROACH GOT A CONTROL FAULT ON THE OUTBOARD FLAPS WHEN SELECTING 15 DEGREES. ALSO GOT 2 CONTROL FAULTS ON THE OUTBOARD FLAPS WHILE IN CRUISE. REPLACED FLAP SELECTOR HANDLE. OPS CHECK GOOD.SDR SWIA200413001Control Unit · malfunctionedCAPTAIN REPORTS OUTBOARD FLAPS HAD CONTROL FAULT MESSAGE DISPLAYED 2 TIMES IN A ROW. REMOVED AND REPLACED FLAP CONTROL UNIT AS REQUIRED. SYSTEM OPS CHECKS GOOD.SDR SWIA200412877Inverter · malfunctionedPILOT REPORTS SEVERAL AUTO PILOT FAILURES ON BOTH SIDES WITH ASSOCIATED FD AND OTHER FLAGS. REMOVED AND REPLACED NR 1 INVERTER DUE TO POSSIBLE A/C POWER PROBLEMS TO AHRS AND AUTOPILOT COMPUTERS. OPS CHECK OF INVERTER AND A/P GOOD. REF EMB MM 120 24-21-01.SDR SWIA200312733Fdau · malfunctionedON DEPARTURE, SMOKE EMITTED FROM FDAU CB ON OVERHEAD PANEL, CEASED WHEN CIRCUIT BREAKER WAS OPENED. REPLACED FDAU CB. SPLICED IN WIRE NR WE01-0023-22 ON RIGHT HAND SIDE. REMOVED AND REPLACED FDAU. SYSTEM OPS CHECK GOOD.SDR SWIA200312606Contactor · failedEMERGENCY LIGHT CIRCUIT BREAKER POPPED. REPLACED EMERGENCY BUS CONTACTOR K0028. OPS CHECKS GOOD.SDR SWIA200312445Structure · crackedLT ENGINE NACELLE DECK CRACKED BY ENGINE DRIVEN HYD LINE. (DISCOVERED DURING E005 INSPECTION) REPAIRED LEFT ENGINE NACELLE DECK CRACK IAW IC 2003-120/3178 2A AND SRM 51-40-00.SDR SWIA200312263Control Handle · faultyCREW REPORTS MULTIPLE FLAP FAILURES WITH CONTROL FAULTS.REMOVED AND REPLACED FLAP HANDLE IAW MM 27-50-00. OPS CHECK GOOD.SDR SWIA200312210Hydraulic Line · brokenLOST ALL GREEN SYSTEM HYDRAULIC PRESSURE AND FLUID ENROUTE FROM CDC TO SLC. REPLACED BROKEN HYDRAULIC LINE AT LEFT RESERVOIR FOR ENGINE DRIVEN HYDRAULIC PUMP. FLUSHED SYSTEM & REPLACED ENGINE DRIVEN HYDRAULIC PUMP IAW 29-10-00. OPS AND LEAK CHECKS GOOD.SDR SWIA200211504Landing Gear · contaminatedON DEPARTURE OUT OF CPR, LANDING GEAR WOULD NOT RETRACT AND HAD RT MLG DISAGREEMENT. PERFORMED QRH AND GEAR EXTENDED. RETURNED TO CPR. INSPECTED LANDING GEAR DUE TO ICE ACCUMULATION. PERFORMED GEAR SWINGS IAW MM 32-30-00. OPS CHECK GOOD. NO DEFECTS NOTESDR SWIA200211269Indicator · malfunctionedABORTED TAKEOFF DUE TO A RED FLAG ON THE FIRST OFFICER'S RMI. RETURNED TO THE GATE. REMOVED AND REPLACED FO'S RMI IAW 34-26-01. OPS CHECK GOOD IAW MM 34-21-00 AND USED NAV 402 TEST SET TO VERIFY VOR STATION INDICATION.SDR SWIA200211298Support · crackedCOCKPIT LEFT SIDE, JUST AFT OF DIRECT VISION WINDOW, FOUND CRACK IN INTERCOSTAL. FOUND DURING C CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-00-00 & 51-40-02.SDR SWIA200211297Clip · crackedRIGHT NACELLE INBOARD AND OUTBOARD FRAME 17 CLIPS CRACKED AT BOTTOM RIVET HOLES. FOUND DURING C CHECK INSPECTION. STOP-DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS ON THE FRAMES IAW EMB SRM 51-40-02.SDR SWIA200211296Angle · crackedFRAME 13, LOWER RIGHT HAND ANGLE AND CHANNEL CRACKED. FOUND DURING C CHECK INSPECTION. REMOVED CRACKED ANGLE AND CHANNEL. FABRICATED NEW ANGLE AND SPLICED IN A SECTION OF THE CHANNEL. INSTALLED BOTH IAW EMB SRM 51-70-05 AND 51-40-02.SDR SWIA200211294Frame · crackedFRAME 13 LEFT AND RIGHT SIDES OF STEP INTO COCKPIT CRACKED INSIDE AND OUTSIDE OF VERTICAL BRACE. FOUND ON C-CHECK INSPECTION. REMOVED ANGLES, FABRICATED AND INSTALLED A NEW ANGLES AND A DOUBLERS IAW SRM 51-00-00 AND 51-40-02.SDR SWIA200211293Frame · crackedLEFT AND RIGHT NACELLE INBOARD AND OUTBOARD EXHAUST MOUNTS HAVE INTERNAL FRAME CRACKS AT NUTPLATES. FOUND ON C-CHECK INSPECTION. STOP-DRILLED CRACKS AND INSTALLED A REPAIR DOUBLERS ON FRAMES IAW EMB SRM 51-70-05.SDR SWIA200211291Clip · crackedLEFT NACELLE OUTBOARD SIDE FRAME 17 CLIP CRACKED. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW EMB120 SRM 51-40-02.SDR SWIA200211290Bracket · crackedLOWER BRACKET AT RIB 16 APPEARS TO BE CRACKED ALONG OUTBOARD, AFT AREA OF BRACKET. RIGHT FUEL CELL. FOUND ON C-CHECK INSPECTION. REMOVED CRACKED CLIP AND FABRICATED NEW CLIP AND INSTALLED NEW SKIN CLIP IAW EMB SRM 51-40-02.SDR SWIA200211289Bracket · crackedSMALL LOWER BRACKET AT RIB 15 IN RIGHT FUEL CELL IS CRACKED. CRACK IS ON INBOARD SIDE OF FRAME. FOUND ON C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED SKIN CLIP IAW EMB SRM 51-40-02.SDR SWIA200211288Stiffener · crackedLEFT NACELLE AFT SIDE OF HYDRAULIC BULKHEAD APPEARS TO HAVE A CRACKED VERTICAL STIFFENER. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02.SDR SWIA200211287Stiffener · crackedRIGHT NACELLE AFT SIDE OF HYDRAULIC BULKHEAD HAS A CRACKED HORIZONTAL STIFFENER. FOUND ON C-CHECK INSPECTION. FABRICATED AND INSTALLED A DOUBLER IAW SRM 51-00-00 AND 51-40-02.SDR SWIA200210657Warning System · malfunctionedABORTED TAKEOFF DUE TO ERRONEOUS TRIM WARNING, ALTHOUGH TRIM WAS SET IN THE GREEN. PERFORMED TRIM WARNING FUNCTIONAL CHECK IAW 27-32-00. OPS CHECK GOOD.SDR SWIA200210689Access Panel · missingAPU ACCESS PANEL MISSING UPON ARRIVAL AT SLC. INSTALLED SERVICEABLE PANEL ASSEMBLY AS NEEDED. P/N ON 145-33351-401.SDR SWIA200210605Controller · malfunctionedON CLIMB THROUGH 16,000 FEET, ALT WARNING LIGHT CAME ON. QRH ACCOMPLISHED. MANUAL MODE WOULD NOT HOLD ALT LOW OR AUTO MODE. REMOVED AND REPLACED PRESSURIZATION AUTO CONTROLLER. OPS CHECKS GOOD. S/N ON 478, S/N OFF 437.SDR SWIA972609Latch · unlatchedABORTED TAKEOFF AND RETURNED TO GATE BECAUSE SERVICE DOOR LIGHT CAME ON. RESECURED FUEL DOOR LATCH. OPS CHECK GOOD.SDR SWIA972267Indicator · failedON TAKEOFF, PASSING THROUGH 80 KNOTS RIGHT NP GAUGE FLUCTUATED FROM 100 PERCENT DOWN TO 50 PERCENT A FEW TIMES. ABORTED TAKEOFF. REPLACED RIGHT NP INDICATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON B939, S/N OFF 105AB.SDR SWIA972266Warning System · illuminatedPROP DEICE FAILURE IN BOTH CYCLES. CIRCUIT BREAKER TRIPPED. FOLLOWED QRH PROCEDURES. PROP STILL FAILED. RETURNED TO LAX. RAN DEICE SYSTEM IAW 20-10-00. ALL CHECKS OK AT THIS TIME.SDR SWIA972241Warning System · false activationWHILE APPLYING TAKEOFF POWER RAN BOTH ENGINES. COULD NOT DUPLICATE. CHECKED ENGINE CONTROL CHIME WITH EECS OFF. CHECK GOOD.SDR SWIA972191Filter · failedALT 400 FEET WE ENCOUNTERED WAKE TURBULENCE WITH AN UNCOMMANDED LEFT ROLL. THE WAKE TURBULENCE PERSISTED AND IN ORDER TO REGAIN STABILITY CONTROL AND CLIMB ABOVE IT, I ADDED POWER. I OBSERVED 132 PERCENT TORQUE WHEN I REDUCED THE POWER TO LIMITS. THE OVERTO
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