N406SW, cancelled Jun 8, 2017

Service difficulty reports · 116

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 = 'N406SW' AND deregistration_id = 'N406SW-2017-06-08'
  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.

SDR SWIA971912Shutoff Valve · leakingJUST AFTER ROTATION RECEIVED TWO MESSAGES ''ANTI ICE DUCT AND 14TH DUCT FAIL''. AFTER ACCOMPLISHING ALL QRH CHECKLISTS, RETURNED TO SLC. FOUND LEAK AT RIGHT 14TH SOV. REPLACED BOTH FORWARD AND AFT CLAMPS. NO LEAKS ON GROUND RUN UP.Aug 2, 2000 · N406SW · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR SWIA971429Skin · dirtyAIRCRAFT NEEDS LEFT AILERON TRIM WHEN FLAPS SET TO 45 DEGREES. DISCOVERED LEADING EDGE OF FLAP HAD RIDGE OF PAINT BUILD-UP FROM RECENT AIRCRAFT RE-PAINTING. RE-SURFACED LEADING EDGE OF FLAP IAW SERVICE LETTER RJ-SL-27-022 DATED 8/28/96.Mar 9, 1999 · N406SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA971325Engine · failedDURING TAKEOFF, LEFT ENGINE ITT WAS IN YELLOW RANGE. DURING CLIMB ITT HAD A 877 FT RED EXCURSION FOR ABOUT 2 SEC. ICING CONDITIONS WERE ENCOUNTERED AND ITT WENT RED 888 FT WITH N21 PERCENT HIGHER THAN RIGHT, FUEL FLOWS 90 LBS HIGHER. ABOUT 3 TO 4 SECONDS, LNov 29, 1998 · N406SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971210Switch · out of adjustSERVICE DOOR CAUTION MESSAGE IN FLIGHT. RETURNED TO FIELD. FOUND DOOR CLOSED, MICROSWITCH SLIGHTLY OUT OF ADJUSTMENT AND DOOR SEAL FLANGE BENT. CONFIRM DOOR CLOSED, MEL 52-70-5.Jun 8, 1998 · N406SW · Cndair CL6002B19 · Door Warning SystemSDR SWIA971097Clamp · failedRIGHT 14TH STAGE BLEED AIR DUCT LEAK MSG OUT OF 18000 FT ON CLIMBOUT. SYNOPTIC PAGE SHOWED RED INSIDE OF VALVE. FOLLOWED QRH CLOSING 14TH STAGE VALVE, MSG WENT OUT. RETURNED TO SLC. SECURED AND SEALED RIGHT 14TH STAGE SHUT OFF VALVE THERMAL BLANKET. SECURMar 9, 1998 · N406SW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR SWIA97926Smoke Detector · failedSMOKE CARGO WARNING DURING CLIMB. PROCEEDED VIA QRH. RETURNED TO FIELD. REMOVED AND REPLACED BOTH LEFT AND RIGHT SMOKE DETECTORS.Sep 9, 1997 · N406SW · Cndair CL6002B19 · Smoke DetectionSDR SWIA97917Transducer · failedAFTER TAKEOFF, RIGHT OIL PRESSURE WENT FROM 27 PSI TO 138 PSI AND FLUCTUATED FOR 2 TO 3 MINUTES. RETURNED TO SLC. REMOVED AND REPLACED RIGHT ENGINE OIL PRESSURE TRANSDUCER PER MM 70-31-05, OPS AND LEAK CHECKS OK.Aug 9, 1997 · N406SW · Cndair CL6002B19 · Engine Oil PressureSDR SWIA97901Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.Jun 4, 1997 · N406SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA97950Angle · corrodedFLOOR SUPPORT ANGLE IN SERVICE DOOR OPENING HAS CORROSION. FABRICATED, INSTALLED FLOOR SUPPORT ANGLE ON SERVICE DOOR IAW MM SRM 51-42-01.May 4, 1997 · N406SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97949Beam · corrodedLBL 27.00 HAS TWO SPOTS OF CORROSION ON WINGS OF BEAM AT FS 325, (ONE SPOT ON INBOARD SIDE, ONE SPOT OUTBOARD SIDE). FABRICATED AND INSTALLED A DOUBLER REPAIR OVER THE CORRODED AREA.May 4, 1997 · N406SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA97951Angle · corrodedFLOOR SUPPORT ANGLE IN PASSENGER DOOR OPENING HAS CORROSION. FABRICATED AND INSTALLED NEW ANGLE FROM S3992 MATERIAL AND INSTALLED ON PASSENGER DOOR FUSELAGE LOWER FRAME IAW SRM 51-40-02.May 3, 1997 · N406SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA97948Seat Track · corrodedFORWARD SEAT TRACKS AT AISLE LEFT AND RIGHT HAVE CORROSION AT FORWARD END. REMOVED CORROSION IAW SRM 51-21-00 AND TESTED BY PRESSURE AND PAINTED BOTTOMS OF TRACKS.May 3, 1997 · N406SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA95687Clamp · failedLT 14TH STAGE DUCT WARNING, FOLLOWED BY LT JET PIPE OVERHEAT MESSAGE. REPLACED AFT CLAMP ON LT 14TH STAGE BLEED AIR SHUT-OFF VALVE. RAN LT 14TH STAGE BLEED AIR AND LEAK CHECK GOOD.Nov 29, 1995 · N406SW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR SWIA95626Start Vlv Light · illuminatedRT ENGINE START LIGHT ON AND RT ENGINE START EICAS MESSAGE ON, CLIMBING THROUGH 15,000 FT. PROBLEM INTERMITTENT ON ABOUT 60 PERCENT OF THE TIME. PROBLEM APPEARED THROTTLE SENSITIVE. RETARDING RT THROTTLE, LIGHT GOES OUT AND ADVANCING THROTTLE LIGHT COMES ONSep 14, 1995 · N406SW · Cndair CL6002B19 · Engine Start Valves/ControlsSDR SWIA95573Anti-Ice Duct · splitANTI-ICE DUCT RED EICAS MESSAGE WITH WING ANTI-ICE SELECTED ON. FOUND LEFT WING OUTBOARD DUCT SPLIT AT OUTBOARD END. LEADING EDGE AND DUCT REMOVED. INSTALLED SERVICEABLE ANTI-ICE DUCT IN LEFT OUTBOARD LEADING EDGE. INSTALLED LEADING EDGE IAW MM 51-41-01. OMay 1, 1995 · N406SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA95538Structure · vibrationDURING CLIMB AS AIRSPEED APPROACHED 280 KTS, AIRPLANE BEGAN TO VIBRATE (LIKE OUT OF BAL NOSEWHEEL). IT ALSO YAWED LEFT (ABOUT 1/2 BALL OUT OF TRIM) AIRSPEED CHANGES OF 100 PLUS KNOTS HAD NO EFFECT ON VIBRATION OR YAW. THE SAME RUDDER TRIM KEPT EVERYTHING CENTEMar 2, 1995 · N406SW · Cndair CL6002B19 · Aircraft Structures
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