N186SW, cancelled Feb 21, 2006
Service difficulty reports · 71
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 = 'N186SW' AND deregistration_id = 'N186SW-2006-02-21' 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 = 'N186SW' AND deregistration_id = 'N186SW-2006-02-21' 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 SWIA971060Crossbeam · corrodedLEFT FLOOR CROSSBEAM AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED LEFT FLOOR CROSSBEAM AT FRAME 16 IAW SRM 51-40-02.SDR SWIA971059Crossbeam · corrodedRIGHT T-SECTION CROSSBEAM AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED RIGHT T-SECTION CROSSBEAM AT FRAME 16 IAW SRM 51-40-02.SDR SWIA971058Crossbeam · corrodedLEFT T-SECTION CROSSBEAM AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED LEFT T-SECTION CROSSBEAM AT FRAME 16, IAW SRM 51-40-02.SDR SWIA971057Crossbeam · corrodedLEFT T-SECTION CROSSBEAM AT FRAME 20 HAS CORROSION. REMOVED AND REPLACED LEFT T-SECTION CROSSBEAM AT FRAME 20, IAW SRM 51-40-02.SDR SWIA971056Stringer · corrodedSKIN PULLED AWAY FROM 2 RIVETS LOWER LEFT FUSELAGE NEAR LEADING EDGE OF FORWARD WING/FUSELAGE FAIRING ATTACH ANGLE, MARKED. REMOVED STRINGER ABOVE POPPED RIVETS AND FOUND CORROSION ON STRINGER. SPLICED IN NEW SECTION OF STRINGER BETWEEN FRAMES 20 AND 21 AT ASDR SWIA971055Sill · corrodedRIGHT SILL AT LAVATORY AREA HAS CORROSION. REMOVED AND REPLACED RIGHT SILL UNDER LAVATORY AREA, IAW SRM 51-40-02.SDR SWIA97855Hydraulic Syst · reqd serviceGREEN SYSTEM LOW LEVEL AND LOW PRESS LIGHT CAME ON AND GAUGE READS ZERO IN LEVEL FLIGHT. CALLED OUT EMERGENCY EQUIPMENT, MADE NORMAL LANDING WITH NO PROBLEMS. SERVICED GREEN SYSTEM WITH 5606 AND DRAINED WATER OUT OF RESERVOIR, OPS CHECKS GOOD.SDR SWIA97829Actuator · failedAFTER TAKEOFF RETRACTED FLAPS, RIGHT FLAP DISAGREEMENT. RETURNED TO FIELD. REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09 WITH SERVICEABLE UNIT. CYCLED FLAPS SEVERAL TIMES, OPS CHECKS GOOD.SDR SWIA97828Connector · contaminatedUPON FLAP RETRACTION AFTER TAKEOFF, UNABLE TO RETRACT DUE TO FLAP DISAGREEMENT OUTBOARDS. RETURNED TO FIELD. FOUND DE-ICE FLUID IN RIGHT OUTBOARD ACTUATOR CANNON PLUG. CLEANED AND DRIED LEFT AND RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUGS, INSPECTED INBOARD ASDR SWIA97827Connector · contaminatedWHILE RETRACTING FLAPS AFTER TAKEOFF, A FLAPS DISAGREEMENT WAS OBSERVED. COMPLIED WITH APPROPRIATE CHECKLISTS AND RETURNED TO LAND. FOUND RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG FULL OF DE-ICE FLUID AND WATER. CLEANED AND OPERATED FLAPS NUMEROUS TIMES, ALLSDR SWIA97826Steering · malfunctionedUPON RELEASING TILLER STEERING, PEDAL STEER LIGHT CAME ON AND RUDDER STEERING DISABLED. IN ORDER TO MAINTAIN NOSEWHEEL STEERING, IT IS NECESSARY TO ENGAGE TILLER CONSTANTLY. ABORTED TAKEOFF. RESET TILLER WHEEL. TAXIED AIRCRAFT OPERATING AIRCRAFT TILLER ANDSDR SWIA95779Breaker · trippedAURAL WARNING BREAKER POPPED, RESET AS PER CHECKLIST. AURAL WARNING MAP ANNUNICATOR ILLUMINATED, BREAKER STAYED RESET. INSTALLED SERVICEABLE BACK UP BATTERY, RERACKED AURAL WARNING UNIT AND CHECKED CONNECTIONS PINS, POWERED UP A/C AND ALL CKS GOOD.SDR SWIA95776Connector · malfunctionedLT LOW PRESSURE LIGHT ILLUMINATE STEADY ON TAXI OUT. COMPLIED WITH QRH LOW PRESSURE LIGHT STILL ILLUMINATED. REPLACED FUEL LOW PRESSURE SWITCH CANNON PLUG, OPS CKS GOOD.SDR SWIA95771Sensor · malfunctionedRT MAIN A GEAR DOWN LIGHT CAME ON IN FLT, USED OVERRIDE TO GET GEAR DOWN. PERFORMED GEAR SWING SEVERAL TIMES WITHOUT DUPLICATING MALFUNCTION. REPLACED A-SYSTEM RT MLG GEAR SENSORS AND Y-HARNESS AND SYSTEM OPS CKS GOOD.SDR SWIA95741Alarm Contl · malfunctionedLT ENGINE DUCT LEAK LIGHT REMAINS ON. SHUT DOWN AND CALLED SGU MX CONTROL. REMOVED AND REPLACED ALARM LIGHT CONTROLLER WITH SERVICEABLE UNIT. RAN LT ENGINE EXTENSIVELY FOR 15 MINUTES. OPS CHECK GOOD ON GROUND AT THIS TIME.SDR SWIA95694Harness · failedLT 'A' GEAR LIGHT ILLUMINATED IN-FLIGHT. GEAR WOULD NOT EXTEND NORMALLY. USED ELECTRIC OVERRIDE. REMOVED AND REPLACED UP AND DOWNLOCK WIRING HARNESS. PROBLEM STILL EXISTS. REPAIRED WIRING HARNESS ON UP AND DOWNLOCK SWITCHES. CYCLED GEAR UP AND DOWN THREESDR SWIA95589Control Box · malfunctionedON TAKEOFF WHEN FLAPS WERE RAISED, DISAGREEMENT WARNING OCCURRED. RERACKED FLAP CONTROL UNIT CYCLES FLAPS, OPS CKS GOOD, SEE F/L 74638.SDR SWIA95563Relay Box · failedLANDING GEAR WOULD NOT EXTEND NORMALLY. INSTALLED SERVICEABLE LANDING GEAR RELAY BOX. GEAR SWUNG MANY TIMES. OVERRIDE FEATURE AND POSITION INDICATOR SYSTEMS OPERATIONALLY CHECK GOOD.SDR SWIA95562Rib · crackedLEFT WING (UPPER) IN THIRD CELL OUTBOARD OF NACELLE, ONE EACH RIB ATTACH FLANGE SECOND AFT CRACKED. FABRICATED AND REPLACED ONE EACH RIB ATTACH FLANGE AT UPPER SKIN SECOND AFT IN THIRD CELL OUTBOARD OF LEFT NACELLE.SDR SWIA95561Rib · crackedLEFT WING (UPPER) IN FIRST CELL OUTBOARD OF NACELLE, FOUR EACH RIB ATTACH FLANGE RIVETED TO UPPER SKIN CRACKED. FABRICATED AND REPLACED FOUR EACH RIB ATTACH FLANGES AT UPPER SKIN FIRST CELL OUTBOARD OF LEFT NACELLE.SDR SWIA95529Connector · contaminatedRECEIVED A FLAP ASYMMETRY WARNING ON TAXI OUT. RETURNED TO GATE. FOUND WATER AND ICE IN RIGHT IB FLAP ACTUATOR CANNON PLUG. CLEANED WATER OUT AND IT FIXED PROBLEM. FLAPS OPERATED NORMAL FOR 15 CYCLES. SEE FL 73291 FOR SIGN OFF.
Back to N186SW, cancelled Feb 21, 2006