N947SW

Service difficulty reports · 209

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 = 'N947SW' 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.

SDR SWIA2020082151917Pressure Deck · corrodedRH PRESSURE FLOOR SILL PANEL HAS CORROSION MULTIPLE LOCATIONS BETWEEN FS424 AND FS559 (MARKED WITH BLACK GREASE PENCIL). (C-CHECK) RO 8/18/2020 REMOVED CORROSION FROM RH PRESSURE FLOOR SILL PANEL MULTIPLE LOCATIONS BETWEEN FS424 AND FS559, MATERIAL LOSS WJul 8, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020082151916Pressure Deck · corrodedLH PRESSURE FLOOR SILL PANEL HAS CORROSION MULTIPLE LOCATIONS BETWEEN FS424 AND FS559 (MARKED WITH BLACK GREASE PENCIL). (C-CHECK) RO 8/18/2020 REMOVED CORROSION FROM LH PRESSURE FLOOR SILL PANEL AT MULTIPLE LOCATIONS (15EA) BETWEEN FS424 AND FS559 REF CRJul 8, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020082151948Skin · chafedCHAFING NOTED ON RT UPPER LEADING EDGE SURFACE. BLENDED THE RT AILERON LEADING EDGE SKIN OUT OF ALLOWABBLE LIMITS IAW SRM. REPLACED THE SKIN.Jul 7, 2020 · N947SW · Cndair CL6002B19 · AileronsSDR SWIA2020082151947Collar · looseLEFT AFT SIDE OF REAR PRESSURE BULKHEAD APROX LBL 36 HAS LOOSE FASTNERS. INSPECTED THE LOCK FASTENERS, FOUND TO BE TIGHT AND SECURE. FOUND FOUR LOOSE LOCK FASTENER COLLARS. REPLACED THE COLLARS IAW SRM.Jul 7, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020082151946Nut · missingREAR PRESSURE BULKHEAD - AFT FACE - VERTICLE STIFFENER UNDER STRINGER 5L (APPROX LBL25) 1 EA LOCK FASTENER NOT TORQUED AND 1 LOCK FASTENER MISSING THE NUT. INSTALLED THE TWO NEW COLLAR ON THE LOCK FASTENERS AT REAR PRESSURE BULKHEAD VERTICAL STIFFENER STGR5Jul 7, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020082151915Lintel · crackedPASSENGER DOOR SURROUND STRUCTURE UPPER SILL(LINTEL STGR3L) ATTACH ANGLE AT APPROX. FS379: SUSPECT CRACK. (FLAGGED) (C-CHECK) RO 8/18/2020 INSTALLED NEW STRINGER 3L P/N 601R31016-87 WITH NEW FASTENERS BETWEEN FS.379.00 & FS.409.00 REF. CRJ200 SRMREF. BOMBJul 7, 2020 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020082151914Lintel · crackedPASSENGER DOOR SURROUND STRUCTURE €“ UPPER SILL(LINTEL STGR3L) ATTACH ANGLE AT FS280: SUSPECT CRACK OR LOOSE FASTENER(MARKED). (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED CRACKED PASSENGER DOOR UPPER SILL (STGR3L) ATTACH ANGLE AT FS280.00 WITH A NEW CLEAJul 7, 2020 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020082151913Door Frame · crackedSERVICE DOOR SURROUND STRUCTURE - STRINGER AT STGR9R AT FS310.00: SUSPECT CRACK. (C-CHECK) RO 8/18/2020 PERFORMED STRINGER SPLICE REPAIR TO STRINGER AT FS310 STR9R FWD OF THE SERVICE DOOR SURROUND STRUCTURE REF REO. COMPLIED WITH ATTACHED TASK. NO LEAKS NJul 7, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020082151912Skin · corrodedCORROSION ON VARIOUS AREAS BETWEEN FS559.00+80 €“ FS559.00+112, STGR 26L €“ STGR 26R (C-CHECK) RO 8/18/2020 REPAIRED FUSELAGE SKIN BETWEEN FS559+80 AND FS559+112 AND BETWEEN STR26L AND STR26R PER REO AND CRJ200SRM. COMPLETED SKYWEST TASK CARD.Jul 3, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020082151945Guide Plate · chafedLEFT WING INBOARD FLAP INBOARD FAIRING GUIDE PLATE ON THE OUTBOARD HINGE ARM IS CHAFED. REMOVED AND INSTALLED A NEW FAIRING GUIDE PLATE ON THE LEFT WING INBOARD FLAP INBOARD FAIRING GUIDE PLATE ON THE OUTBOARD HINGE ARM REF. SRMJul 1, 2020 · N947SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020082151911Vane · chafedLEFT WING INBD FLAP VANE LEADING EDGE CHAFFED ON INBD SIDE MARKED (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED LH WING INBOARD FLAP VANE CAP REF CRJ200 SRM, AND DWG. SEE ATTACHED TASK. SEE CONTINUE CARD FOR DETAILS.Jun 30, 2020 · N947SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020082151944Stop Fitting · chafedPASSENGER DOOR FITTINGS ON THE FUSELAGE €“ CENTER, AFT, PIN STOP FITTING IS CHAFED. REMOVED AND REPLACED PASSENGER DOOR CENTER, AFT PIN STOP FITTING P/N 601R38388-7 REF. SRM & AMM. OP CHECK GOODJun 28, 2020 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020082151943Stop Fitting · chafedPASSENGER DOOR FITTINGS ON THE FUSELAGE CENTER, FORWARD, PIN STOP FITTING IS CHAFED. REMOVED AND REPLACED PASSENGER DOOR CENTER, FWD, PIN STOP FITTING IAW AMM.Jun 28, 2020 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020082151942Stop Fitting · chafedPASSENGER DOOR FITTINGS ON THE FUSELAGE UPPER, FORWARD, PIN STOP FITTING IS CHAFED. REMOVED AND REPLACED PAX DOOR UPPER FWD PIN STOP FITTING IAW SRM & AMMJun 28, 2020 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020082151941Stop Fitting · chafedMAIN AVIONICS COMPARTMENT DOOR FITTING ON THE FUSELAGE €“ LEFT SIDE, FORWARD, STOP FITTING IS CHAFED. REMOVED AND REPLACED, 1EA. STOP-FITTING WITH NEW FITTING IAW SRM.Jun 28, 2020 · N947SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020082151928Guide · crackedMAIN AVIONICS COMPARTMENT DOOR FITTINGS ON THE FUSELAGE LEFT SIDE, FORWARD POLYMER GUIDE IS CRACKED. (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED POLYMER GUIDE A-BAY DOOR FITTING AT L/H FWD FUSELAGE SIDE REF CRJ-200 SRMJun 28, 2020 · N947SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020082151910Skin · gougedCARGO COMPARTMENT DOOR - EXTERNAL AREA OF THE HANDLE HOUSING HAS GOUGES. (MARKED) (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED CARGO DOOR HANDLE HOUSING REF CRJ200 SRM AND BOMBARDIER DWG. NO LEAKS NOTED. COMPLIED WITH ATTACHED TASK.Jun 28, 2020 · N947SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2020082151909Skin · chafedSERVICE DOOR OUTER SKIN CHAFED AT CUT-OUT FOR OUTER HANDLE (MARKED). (C-CHECK) RO 8/18/2020 BLENDED, INSPECTED AND RESTORED CHAFE DAMAGE PER REO. FOUND TO BE WITHIN LIMITS PER REO. SEE CONTINUE CARD FOR DETAILS.Jun 27, 2020 · N947SW · Cndair CL6002B19 · Galley DoorsSDR SWIA2020082151908Floor Panel · crackedRH FORWARD EQUIPMENT COMPARTMENT (TRU BAY) FLOOR HAS SUSPECTED CRACK NEAR ADG PUMP AT FS 193. (C-CHECK) RO 8/18/2020 REPAIRED RH TRU BAY FLOOR NEAR ADG PUMP REF REO. SEE CONTINUE CARD FOR DETAILSJun 27, 2020 · N947SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2019110846729Warning Message · false indicationFLAP FAIL CAUTION MESSAGE ON APPROACH INTO CAK WHEN FLAPS 8 SELECTED - FLAPS FAILED AT 0. CREW DIVERTED TO CLECREW RESET & OPERATED FLAPS 5 FULL CYCLES. OK TO CONTINUE IN SERVICE FOR 10 FLT CYCLES.Nov 8, 2019 · N947SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA2018101645148Angle · corrodedANGLE (PN 601R31527-221) AT BOTTOM OF PAX DOOR SURROUND STRUCTURE HAS CORROSION. (C-CHECK) RO: 10/14/2018 INSTALLED NEW ANGLE, P/N 601R31527-221 IAW SRM. OPS TEST GOOD.Sep 22, 2018 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018101645147Cap · chafedCHAFED ON LT INBD FLAP, OUTBOARD CENTER FLAP VANE CAP. (C-CHECK) RO: 10/14/2018 INSTALLED NEW LT INBD FLAP, OUTBOARD CENTER FLAP VANE CAP IAW SRM.Sep 18, 2018 · N947SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018101645145Support Angle · corrodedSERVICE DOOR. FRAME FS319.00, STR. 19R, FRAME SUPPORT ANGLE CORRODED. (C-CHECK) RO: 10/14/2018 REMOVED AND AND INSTALLED NEW FRAME SUPPORT ANGLE IAW SRM.Sep 16, 2018 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018101645144Plate · corrodedFLOOR SILL PLATE FORWARD OF SERVICE DOOR CUTOUT IS CORRODED. (C-CHECK) RO: 10/14/2018 REMOVED AND INSTALLED NEW FLOOR SILL PLATE P/N 601R31668-49 AND RELATED HARDWARE FWD OF SERVICE DOOR CUT-OUT IAW SRM.Sep 16, 2018 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018101645143Floorbeam · corrodedTHE FS280 FLOORBEAM HAS CORROSION AROUND NUTPLATE HOLES. (C-CHECK) RO: 10/14/2018 CORRODED PART P/N 600-34017-595 REPLACED IAW SRM.Sep 16, 2018 · N947SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2018101645142Floor Support · corrodedTHE COCKPIT FLOOR SUPPORT AT FS280 IS CORRODED. (C-CHECK) RO: 10/14/2018 COCKPIT FLOOR SUPPORT ANGLE REPLACED IAW SRM.Sep 16, 2018 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642734Circuit Card · failedUNCOMMANDED YAW CONTROL AT REACHING CRUISE ALTITUDE. DECLARED AN EMERGENCY. REMOVED AND REPLACED THE NR 2 FCC CARDOct 24, 2016 · N947SW · Cndair CL6002B19 · Aerodynamic Load AlleviatingSDR SWIA201642622Rib · corrodedCORROSION FOUND ON THE RT BATT RIB INBOARD SUPPORT ANGLE BY ELECTRICAL HARNESS CONNECTORS. REMOVED AND REPLACED THE RIB INBOARD SUPPORT ANGLE NEAR ELECTRICAL HARNESS CONNECTORS WITH NEW RIB IAW SRM.Sep 12, 2016 · N947SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA201642621Intercostal · corrodedPAX DOOR AFT INTERCOSTAL DD1 FOUND CORRODED. REPLACED PAX DOOR AFT INTERCOSTAL AT DD1 IAW SRM. PERFORMED PRESSURE LEAK CHECK, LEAK CHECK GOOD.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642620Intercostal · corrodedPAX DOOR AFT INTERCOSTAL BETWEEN DD1 AND DD2 FOUND CORRODED. (C-CHECK) RO: 09/26/2016 REPLACED PAX DOOR INTERCOSTAL BETWEEN DD1 AND DD2 IAW SRM. PERFORMED PRESSURE LEAK CHECK, LEAK CHECK GOOD.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642619Intercostal · corrodedPAX DOOR AFT INTERCOSTAL DD2 FOUND CORRODED. REPLACED PAX DOOR AFT INTERCOSTAL AT DD2 IAW SRM. PERFORMED PRESSURE LEAK CHECK, LEAK CHECK GOOD.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642618Intercostal · corrodedPAX DOOR AFT INTERCOSTAL DD3 FOUND CORRODED. REPLACED PAX DOOR AFT INTERCOSTAL AT DD3 IAW SRM. PERFORMED PRESSURE LEAK CHECK, LEAK CHECK GOOD.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642617Intercostal · corrodedPAX DOOR AFT INTERCOSTAL DD4 FOUND CORRODED. REPLACED PAX DOOR AFT INTERCOSTAL AT DD4 IAW SRM. PERFORMED PRESSURE LEAK CHECK, LEAK CHECK GOOD.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642616Intercostal · corrodedPAX DOOR AFT INTERCOSTAL DD5 FOUND CORRODED. REPLACED PAX DOOR AFT INTERCOSTAL AT DD5 IAW SRM. PERFORMED LEAK CHECK, LEAK CHECK GOOD.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642615Intercostal · corrodedPAX DOOR CENTER INTERCOSTAL DD6 FOUND CORRODED. REPLACED PAX DOOR CENTER INTERCOSTAL AT DD6 IAW SRM. PERFORMED LEAK CHECK, LEAK CHECK GOOD.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642614Fairing · chafedLEFT FLAP STUB FAIRING CHAFED. REMOVED AND REPLACED L/H FLAP STUB FAIRING WITH NEW STUB FAIRING IAW AMM.Sep 5, 2016 · N947SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642613Web · corrodedPAX DOOR AFT WEB HAS CORROSION AROUND PANEL CUTOUTS, TOP CORNER NEAR HANDRAIL POST AND ON FLANGES COMMON TO THE STAIR PANELS. REPLACED PAX DOOR AFT WEB IAW SRM.Sep 4, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642612Web · corrodedPAX DOOR FWD WEB HAS CORROSION AROUND PANEL CUTOUTS, TOP CORNER NEAR HANDRAIL POST AND ON FLANGES COMMON TO THE STAIR PANELS. REPLACE PAX DOOR FWD WEB IAW SRM.Sep 4, 2016 · N947SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642611Skin · chafedRIGHT AILERON LEADING EDGE PANEL 699BB IS CHAFED. REMOVED DAMAGED RH AILERON LE PANEL AND REPLACED IAW SRM.Sep 2, 2016 · N947SW · Cndair CL6002B19 · AileronsSDR SWIA201642610Nozzle · chafedLEFT EXHAUST NOZZLE HAS SEVERE CHAFING ON FWD EDGE OF NOZZLE JUST AFT OF SEAL. INSTALLED NEW UPPER AND LOWER STIFFENER ON TO THE LEFT HAND EXHAUST NOZZLE FAIRING IAW CMM.Sep 2, 2016 · N947SW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR SWIA201541705Engine · flamed outDURING DEPARTURE, ENCOUNTERED MODERATE TO SEVERE TURBULENCE. HEARD TRIPLE CHIME "ENGINE OIL" WITH POSSIBLE FLAMEOUT. LT ENGINE SPOOLED DOWN SLIGHTLY, ENGAGED CONTINUOUS IGNITION AND ENGINE THRUST RESTORED. ALSO, HAD STICK SHAKER IN NORMAL CLIMB ATTITUDE, IDec 28, 2015 · N947SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA201440295Controller · failedRT WINDSHIELD HEAT CAUTION MESSAGE ILLUMINATED MULTIPLE TIMES DURING FLIGHT. R & R RT WINDSHIELD HEAT CONTROLLER IAW AMM. OPS CHECKED GOOD. OK FOR SERVICE.Dec 5, 2014 · N947SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA201439489Battery Pack · dischargedEMERGENCY OVERHEAD LIGHT INOPERATIVE. R & R FORWARD EMERGENCY LIGHT BATTERY PACK CHARGE ASSY. OPS CHECK GOOD AT THIS TIME IAW AMM.Oct 8, 2014 · N947SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201439488Charger · inoperativeGALLEY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACE BATTERY CHARGER ASSY IAW AMM. OPS CHECK GOOD. (2014NM060066)Oct 7, 2014 · N947SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201439374Lever · chafedRIGHT ENGINE, AUTOTHROTTLE RETURN LEVER CHAFED 1.25 INCHES BELOW CAM FOLLOWER ROLLER END OF LEVER. BLENDED AUTO THROTTLE RETURN LEVER IAW EA.Sep 14, 2014 · N947SW · Cndair CL6002B19 · Auto Throttle SystemSDR SWIA201439366Stringer Clip · crackedBS 625, STRINGER CLIP CRACKED S14R. R & R STRINGER CLIP IAW REO AND SRM.Sep 10, 2014 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201439365Stringer Clip · crackedLEFT BS 625 CRACKED STRINGER CLIP AT 14L, R & R CRACKED STRINGER CLIP IAW REO.Sep 10, 2014 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201439368Bulkhead Web · crackedBS 280 BULKHEAD WEB CRACKED AT LBL 9. PERFORMED REPAIR TO BULKHEAD WEB IAW REO.Sep 9, 2014 · N947SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201439380Floor Support · crackedLEFT SIDE, FLOOR SUPPORT AT BS 621 CRACK EDAT RADIUS. LOCATED, FITTED AND DRILL EDNEW REPAIR ANGLE, BRACKET ASSY AND STRAP IAW REO. INSTALLED IAW SRM.Sep 7, 2014 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201439369Floor Support · corrodedRIGHT OTBD EDGE MEMBER CORRODED AROUND NUTPLATE HOLES FROM BS 559+80 - 559+112. REMOVED CORROSION FROM RT FLOOR SUPPORT AND FOUND TO BE WITHIN LIMITS AND RESTORED FINISH REF REO.Sep 7, 2014 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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