N976SW

Service difficulty reports · 197

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 = 'N976SW' 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 SWIA2020030248893Strap · corrodedFLOOR SUPPORT STRAP IS CORRODED AT FS 559.00 BETWEEN LBL 27 AND 42. (C-CHECK) RO 2/27/2020 REMOVED CORROSION FROM FLOOR SUPPORT STRAP AND FOUND TO BE OUT OF LIMITS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SUPPORT STRAP IAW CRJ 200.Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248892Strap · corrodedFLOOR SUPPORT STRAP IS CORRODED AT FS 559.00 BETWEEN RBL 27 AND 42. (C-CHECK) RO 2/27/2020 REMOVED CORROSION AND FOUND SUPPORT STRAP TO BE OUT OF LIMITS. REMOVED SUPPORT STRAP AND LOCATED AND DRILLED NEW SUPPORT STRAP IAW CRJ 200.Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248891Seat Track · corrodedRBL 9 SEAT TRACK IS CORRODED BETWEEN FS 409.00 AND 409.00+112. (C-CHECK) RO 2/27/2020 FABBED SEAT TRACK IAW REO AND INSTALLED IAW CRJ 200 AMM.Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030248890Seat Track · corrodedLBL 9 SEAT TRACK IS CORRODED BETWEEN FS 409.00 AND 409.00+112. (C-CHECK) RO 2/27/2020 FABBED SEAT TRACK IAW REO AND INSTALLED IAW CRJ 200 AMM.Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030248889Seat Track · corrodedRBL 9 SEAT TRACK IS CORRODED BETWEEN FS 364.00 AND 409.00. (C-CHECK) RO 2/27/2020 FABBED SEAT TRACK IAW REO AND INSTALLED IAW CRJ 200 AMM.Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030248888Seat Track · corrodedLBL 9 SEAT TRACK IS CORRODED BETWEEN FS 364.00 AND 409.00. (C-CHECK) RO 2/27/2020 FABBED SEAT TRACK IAW REO AND INSTALLED IAW CRJ 200 AMM.Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030248881Door Sill · corrodedR/H PRESSURE FLOOR SILL DECK IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 409.00+128 AND 559.00. (C-CHECK) RO 2/27/2020 REMOVED AND INSTALLED FASTENERS AND BLENDED AREAS IAW CRJ 200 SRM. REPAIRED AREAS IAW BOMBARDIER REO. COMPLIED WITH SKYCARD AND FORM M-3Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248880Door Sill · corrodedL/H PRESSURE FLOOR SILL DECK IS CORRODED IN MULTIPLE LOCATIONS BETWEEN FS 409.00+128 AND 559.00. (C-CHECK) RO 2/27/2020 REWORKED AND REPAIRED LH SILL DECK BETWEEN FS 409+128 AND 559 IAW REO. REFER TO CONTINUE CARD FOR STEPS ACCOMPLISHED. COMPLIED WITH SKY Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248879Floorbeam · corrodedRBL 9 FLOOR BEAM CAP IS CORRODED BETWEEN FS 409.00+128 AND 424.00. (C-CHECK) RO 2/27/2020 REMOVED CORROSION FROM RBL 9 FLOOR BEAM AND FOUND IT WAS OUT OF LIMITS. REMOVED DAMAGED SECTION AND FABRICATED FILLER AND ANGLE AND INSTALLED REPAIR IAW BOMBARDIER REJan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020030248878Beam · corrodedFS 280..00 BEAM IS CORRODED BETWEEN LBL 18 AND RBL 9. (C-CHECK) RO 2/27/2020 REMOVED CORROSION BY REPAIRING FS 280.00 BEAM IAW BOMBARDIER REOS. COMPLETED AND ATTACHED MAJOR REPAIR TASK CARD AND FORM M-337. TOTAL WEIGHT CHANGE +1.13 LBS. REFERENCE CONTINUATJan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020030248877Intercostal · corrodedPAX DOOR INTERCOSTAL DOOR DATUM 2 IS CORRODED. (C-CHECK) RO 2/27/2020 REMOVED AND INSTALLED SERVICABLE INTERCOSTAL DD2 IAW CRJ-200 SRM COMPLETED FORM M-337, M-131 AND SKYWEST TASK CARD. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE.Jan 9, 2020 · N976SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020030248886Support Fitting · crackedL/H AFT WINDSHIEL SUPPORT CLIP IS CRACKED. (C-CHECK) RO 2/27/2020 REMOVED, LOCATED, DRILLED AND INSTALLED L/H AFT WINDSHIELD CLIP IAW CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED AND RELATED OPS CHECKS. ALL CHECKS GOOD.Jan 8, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248876Intercostal · crackedL/H LOWER WINDSHIELD SUPPORT SIDE POST IS CRACKED. (C-CHECK) RO 2/27/2020 UPON REMOVAL OF L/H LOWER WINDSHIELD SUPPORT SIDE POST FOUND POST NOT TO BE CRACKED FOUND INTERCOSTAL ADJACENT TO POST CRACKED. REINSTALLED SAME SERVICEABLE L/H LOWER WINDSHIELD SIDEJan 8, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248901Hinge · chafedR/H MLG DOOR AFT HINGE SECTOR ANTI-ROTATION TAB IS CHAFED OFF. (C-CHECK) RO 2/27/2020 REMOVED AND INSTALLED SERVICABLE HINGE SECTORS IAW AMM.Jan 6, 2020 · N976SW · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA2020030248900Hinge · chafedL/H MLG DOOR AFT HING ANTI ROTATION TAB IS CHAFED OFF. (C-CHECK) RO 2/27/2020 REMOVED AND INSTALLED SERVICEABLE HINGE SECTOR IAW AMM.Jan 6, 2020 · N976SW · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA2020030248875Post · damagedFS409+128 RBL18 OUTBD VERTICAL POST HAS AN INDICATION .15" LONG BY 60%FSH IN THE UPPER AFT RADIUS @ WS69. FAILED NDT INSPECTION. (C-CHECK) RO 2/27/2020 REMOVED AND REPLACED FS409+RBL18 POST IAW CRJ 200 SRM AND BOMBARDIER REO. FORMS M-337 AND M-131 AND SKYJan 4, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248874Post · damagedFS409+128 BL0 LH VERTICAL POST HAS AN INDICATION .2" LONG BY 60%FSH IN THE UPPER AFT RADIUS @ WS69. FAILED NDT INSPECTION. (C-CHECK) RO 2/27/2020 REMOVED UNSERVICABLE POST AND INSTALLED SERVICABLE POST AT FS 409+128 BL0 IAW CRJ 200 SRM AND BOMBARDIER REO Jan 4, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248873Post · damagedFS409+128 VERTICAL POST LBL18 HAS INDICATIONS .15" LONG BY 60%FSH IN THE OUTBD V-POST, AND .15" LONG BY 55% IN THE INBD V-POST UPPER AFT RADIUS @ WS69. FAILED NDT INSPECTION. (C-CHECK) RO 2/27/2020 REMOVED AND REPLACED FS409+128 IAW CRJ 200 SRM, AND BOMBAJan 4, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248872Stringer · crackedSTRINGER 3L IS CRACKED AT F.S. 379.00. (C-CHECK) RO 2/27/2020 REPAIRED STRINGER 3L AT FS 379.00 BY COMPLYING WITH BOMBARDIER REO AND CRJ 200 SRM COMPLETED FORM M-337,M-131 TOTAL WEIGHT CHANGE +0.12 LBS SEE ATTACHED CONTINUATION CARD AND SKYCARD FOR DETAILJan 4, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020030248885Seal · crackedMETAL SEAL ON TRAILING EDGE OF L/H WING FOR FLIGHT SPOILER BETWEEN LWS 191.44 TO LWS 183.00 IS CRACKED. (C-CHECK) RO 2/27/2020 REMOVED AND REINSTALLED L/H FLIGHT SPOILER IAW CRJ 200 AMM, REMOVED UNSERVICABLE TRAILING EDGE METAL SEAL AND REPLACED WITH SJan 3, 2020 · N976SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2020030248887Bolt · corrodedFORWARD KEEL BEAM ATTACHING HARDWARE IS CORRODED. THE TWO FORWARD BOLTS/NUTS AND THE L/H AFT BOLT/NUT BETWEEN FS 409+112 AND 409+128. (C-CHECK) RO 2/27/2020 REMOVED AND INSTALLED SERVICEABLE FWD KEEL BEAM ATTACHING HARDWARE BETWEEN FS 409+112 AND FS 409+ 1Jan 2, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA2020030248871Skin · dentedLEFT FLIGHT SPOILER LOWER SURFACE HAS 2 EA. DENTS. #1 DENT IS APPROX. .750 INCHES BY .500 INCHES BY.021 INCHES DEEP. #2 DENT IS APPROX. .5 ICHES BY .5 INCHES BY .015 INCHES DEEP. (C-CHECK) RO 2/27/2020 UPON FURTHER REVIEW FOUND A TOTAL OF 4 DENTS. EVALUDec 30, 2019 · N976SW · Cndair CL6002B19 · SpoilersSDR SWIA2018012944191Floor Support · corrodedRIGHT FLOOR SUPPORT SECTION FROM BS 559+80 TO 559+112 CORRODED. INSTALLED A NEW FLOOR SUPPORT IAW SRM.Jan 12, 2018 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018012944192Bulkhead · damagedAFT BS 621 PRESSURE BULKHEAD FWD FACE HAS SCREW DAMAGE AT LBL 9 , 18,27. REPAIRED THE BULKHEAD IAW REO.Jan 2, 2018 · N976SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2018012944194Striker · gougedPAX DOOR AFT SEAL STRIKER IS GOUGED UPPER MIDWAY UP. REPAIRED IAW REO. PERFORMED PRESSURE LEAK CHECK IAM AMM. NO LEAKS NOTED.Dec 30, 2017 · N976SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018012944195Cap · chafedPAX DOOR FWD END CAP HAS CHAFING DAMAGE FROM HANDRAIL. REMOVED AND REPLACED THE CAP IAW SRM.Dec 27, 2017 · N976SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018012944193Cap · chafedPAX DOOR AFT END CAP CHAFED FROM HANDRAIL. REMOVED AND REPLACED THE END CAP IAW SRM.Dec 27, 2017 · N976SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2017120544006Control Handle · failedLANDING GEAR DID NOT RETRACT, WITH A/SKID INB CAUT AND PARK BRAKE SOV CAUTION. (FLT 5197) CLOSED REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW AMM. REMOVED AND REPLACED PSEU IAW AMM. OPS CHECK GOOD AT THIS TIME.Nov 24, 2017 · N976SW · Cndair CL6002B19 · Landing Gear SelectorSDR SWIA201743794Selector Valve · failedRETURN TO FIELD FOR A GEAR DISAGREE AFTER TAKEOFF. NOSE GEAR DID NOT COME UP. REPLACED THE LANDING GEAR HANDLE AND MLG SELECTOR VALVE IAW AMM. OPS CHECKED GOOD.Sep 28, 2017 · N976SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201541700Skin · dentedSMALL DENT IN FUSELAGE FWD OF BS 250 AND ABOVE STRINGER 23. REPAIRED THE SKIN IAW REO.Dec 3, 2015 · N976SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201439079Skin · dentedSMALL DENT IN FUSELAGE FWD OF BS 250 ABOVE STRINGER 23 AND FOUND OUT OF LIMITS IAW SRM.Aug 4, 2014 · N976SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201438910Target · out of adjustRIGHT MAIN GEAR DISAGREE AFTER TAKEOFF. ADJUSTED TARGET AND PERFORMED MULTIPLE EXTENSION AND RETRACTION IAW AMM.Jul 6, 2014 · N976SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201438428O-Ring · leakingACFT INTERIOR HAS AN ODOR OF JET FUEL. R & R O-RING ON ELBOW BETWEEN APU FUEL SHUTOFF VALVE AND FUEL CONTROL UNIT, PN: M25988-2-904 IAW AMM.Jun 24, 2014 · N976SW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR SWIA201437211Fitting · crackedFS 621 COCKPIT AIR SUPPLY BULKHEAD DUCT FITTING HAS CRACKS ON FLANGE THAT REQUIRE WELD REPAIR. C-CHECK, REPAIRED CRACK ON FS 621.0 AIR SUPPLY DUCT BULKHEAD FITTING IAW REO.Apr 11, 2014 · N976SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201437212Structure · chafedLEFT INBD FLAP ACTUATOR TUBE ASSEMBLY GOUGED AND FLAP REQUIRES REPLACEMENT DUE TO OUT OF LIMITS CHAFE. C-CHECK, REPLACED LT INBD FLAP IAW AMM.Apr 7, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437217Attach Angle · crackedAFT PRESSURE BULKHEAD LT THIRD INTERCOSTAL FROM BOTTOM HAS CRACKED SKIN TO INTERCOSTAL ATTACH ANGLE. C-CHECK, REPLACED FS 621, STR14L INTERCOSTAL IAW SRM.Apr 6, 2014 · N976SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201437216Attach Angle · crackedAFT PRESSURE BULKHEAD LT 4TH INTERCOSTAL FROM BOTTOM HAS CRACKED SKIN TO INTERCOSTAL ATTACH ANGLE. C-CHECK, R & R INTERCOSTAL ANGLE BETWEEN STR 13L AND 14L FS 621- FS 624 IAW SRM.Apr 6, 2014 · N976SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201437215Tube · gougedRIGHT INBD FLAP, INBD FLAP VANE CENTER ACTUATOR TUBE ASSY HAS A GOUGE ON THE BOTTOM SIDE. C-CHECK, BLENDED GOUGED AREA ON RT INBD FLAP, INBD FLAP VANE CENTER ACTUATOR TUBE ASSY IAW REO.Apr 6, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437214Tube · gougedRT INBD FLAP, INBD FLAP VANE CENTER ACTUATOR TUBE ASSY HAS A GOUGE ON THE BOTTOM SIDE. C-CHECK, BLENDED GOUGED AREA OF RT INBD FLAP, INBD FLAP VANE CENTER ACTUATOR TUBE ASSY IAW REO.Apr 6, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437213Tube · gougedLEFT INBD FLAP, THE CENTER FLAP ACTUATOR TUBE HAS A GOUGE ON THE BOTTOM SIDE. C-CHECK, BLENDED GOUGED AREA ON LT INBD FLAP, CENTER ACTUATOR TUBE ASSY IAW REO.Apr 6, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437218Bulkhead · crackedCRACK ON LT LOWER BS 202 WEB AT OTBD SIDE OF BRAKE CABLE. C-CHECK, REPAIRED FS 202 BULKHEAD WEB IAW REO.Apr 5, 2014 · N976SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201437226Vane · chafedLT INBD FLAP VANE L/E CHAFED, OTBD AREA. C-CHECK, REPAIRED LT INBD FLAP VANE L/E OTBD AREA IAW REO.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437225Vane · chafedRT FLAP VANE L/E CHAFED, INBD AREA. C-CHECK, REPAIRED RT FLAP VANE L/E INBD AREA IAW REO.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437224Vane · chafedRIGHT FLAP VANE L/E CHAFED, ID AREA BEYOND LIMITS. C-CHECK, REPLACED IAW SRM.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437223Wire Harness · chafedSERVICE DOOR HARNESS SHEATHING CHAFED. C-CHECK, REPAIRED DAMAGED HEAT SHRINK ON SERVICE DOOR WIRE HARNESS CONVELEX TUBING IAW REO.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Door System WiringSDR SWIA201437222Support Arm · chafedSERVICE DOOR MAIN SUPPORT ARM CHAFED FROM SERVICE DOOR INNER HANDLE. C-CHECK, BLENDED 2 AREAS ON THE INBD FACE OF THE HINGE ARM AND THE UPPER PORTION OF THE -59 PLATE OF THE SERVICE DOOR IAW STS EA.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Service DoorsSDR SWIA201437221Vane · chafedLT INBD FLAP VANE MID AREA L/E CHAFED BEYOND LIMITS. C-CHECK, REPLACED LT INBD FLAP AND VANE IAW SRM.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437220Vane · chafedRT FLAP VANE L/E MID AREA IS CHAFED BEYOND LIMITS. C-CHECK, REPLACED RT INBD FLAP VANE L/E MIDDLE AREA SKIN IAW SRM.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437219Vane · chafedRIGHT FLAP VANE L/E OTBD AREA CHAFED AND REQUIRES REPLACEMENT. C-CHECK, REPLACED RT INBD FLAP VANE L/E OTBD SKIN IAW SRM.Apr 4, 2014 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437229Rod · chafedRT MLG DOOR ROD TO BELCRANK CHAFED. C-CHECK, R & R RT MLG DOOR ROD IAW AMM.Apr 3, 2014 · N976SW · Cndair CL6002B19 · Landing Gear Door Retract Section
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