N976SW

Service difficulty reports · 197

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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'
  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 SWIA2026032075561Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA105760-REO 601R-57-51-1083 N976SW MXCODEID116263-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 105760. MISDRILLED HOLE AND MISSING RIVET ON WING T/E UPPER SKIN AT SS 241.80, LT. COMPLIED WITH TEMP REPAIR IAW REO 601R-57-Mar 20, 2026 · N976SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025042108Window · arcedDURING CRUISE ARCING OBSERVED ON THE UPPER EDGE OF THE LEFT WINDOW, AFTER FURTHER EXAMINATION A DELAMINATED LINE IS VISIBLE ON THE AFT PORTION OF THE WINDOW. ADDITIONALLY THE FORWARD PORTION OF THE WINDOW WAS EXTREMELY HOT TO THE TOUCH, TO THE POINT IT WOULD BApr 18, 2025 · N976SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWI2025F00311Stall Warning · false activationSTALL FAIL CAUTION AFTER ROTATION (FLIGHT 5118 - FILED CLOSED) CONSULTED THE FLIGHT CREW, THE CAPTAIN INFORMED ME THEY THERE WAS A 24 KNOT CROSSWIND ON TAKEOFF. COMPLIED WITH FMRP, AND APPLICABLE STEPS IN FIM 27-35-00. STALL FAIL CAUTION MESSAGE DID NOT Mar 7, 2025 · N976SW · Cndair CL6002B19 · Central WarningSDR SWIA202501220075Flap System · failedWHEN INTERCEPTING FINAL IN DEN, RECEIVED FLAP FAIL CAUTION MESSAGE WHEN FLAPS WERE SELECTED FROM 0 TO 20. SPEED WAS 190 KNOTS. FLAPS FAILED AT 0. RAN QRH PROCEDURE AND LANDED SUCCESSFULLY IN DEN. RATE OF DESCENT AT TOUCHDOWN WAS 200 FT/M. (FLIGHT 5364) CJan 20, 2025 · N976SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA20240614001Warning Message · illuminatedD: GEAR DISAGREE ON APPROACH FOLLOWED BY NOSE DOOR OPEN. QRH RESOLVED ISSUE.C: MEL 32-30-1CAT A DUE ONE FLIGHT DAY FROM 6/13/24CAT II DOWNGRADEDGEAR DISAGREE ON APPROACH FOLLOWED BY NOSE DOOR OPEN. QRH RESOLVED ISSUE. (FLIGHT 5587 - FILED CLOSED) JUN 14,Jun 14, 2024 · N976SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2024031200104Stiffener · crackedNDT IDENTIFIED A CRACK ON FS409+128 LBL27 I/B FLANGE BOTTOM FASTENER AS MARKED (C-CHECK RO 3/9/2024) REPAIRED FS409+128 LBL27 INBOARD STIFFENER REF. REO 601R-53-41-056 REV. -F DATED 2011/09/02 STEPS 1-17, ALL STEPS COMPLIED WITH. LEAK CHECK GOOD. COMPLIED Jan 4, 2024 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024031200226Hinge Fitting · gougedLH AILERON OUTBD #4 HINGE FITTING, ON THE AILERON, HAS A SMALL GOUGE ON THE LOBE (MARKED) (C-CHECK RO 3/9/2024) REPAIRED DAMAGE AT LH AILERON OUTBD #4 HINGE FITTING, ON THE AILERON SIDE, AIL STA 364.016. REF REO 601R-57-61-850 REV--, DATED 2023-12-28. COMDec 6, 2023 · N976SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWI2024031200225Hinge Fitting · gougedRH AILERON CENTER HINGE #3, ON THE WING, HAS A SMALL GOUGE ON THE LOBE (MARKED) (C-CHECK RO 3/9/2024) BLENDED OUT GOUGE AT RH AILERON HINGE FITTING NO.3, ON THE WING SIDE . REF. CRJ-200 SRM 51-12-00. RECEIVEDAND COMPLIED WITH ALL STEPS OF REO#601R-57-51-1Dec 6, 2023 · N976SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWI202403120224Fitting · gougedLH AILERON CENTER FITTING #3, ON THE WING, HAS A GOUGE ON THE LOWER STRUCTURE OUTBD EDGE (MARKED) (C-CHECK RO 3/9/2024) BLENDED OUT CHAFE/GOUGE ON THE LH AILERON CENTER FITTING#3, ON THE WING LOWER STRUCTURE OUTBD EDGE. REF CRJ 200 SRM 51-12-00. RECEIVED ADec 6, 2023 · N976SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWI2024031200223Skin · crackedPOSSIBLE CRACK ON EXTERNAL SKIN AT FS235 RBL6 (NLG WHEEL WELL CUTOUT) (C-CHECK RO 3/9/2024) REPAIRED EXTERNAL SKIN (NLG WHEEL WELL CUTOUT) AT FS235 RBL6 REF REO 601R-53-11-048 REV. -D DATED 2015-06-10. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOODec 6, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2024031200222Skin · crackedPOSSIBLE CRACK ON EXTERNAL SKIN AT FS235 LBL6 (NLG WHEEL WELL CUTOUT) (C-CHECK RO 3/9/2024) REPAIRED EXTERNAL SKIN (NLG WHEEL WELL CUTOUT) AT FS235 LBL6 REF REO 601R-53-11-048 REV. -D DATED 2015-06-10. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOODec 6, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202403120004Bracket · crackedFS625 AFT PRESSURE BULKHEAD WEB CLIP AT STGR.14 CRACKED. (MARKED) (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW REPLACEMENT CLIP AT FS.625 PRESS. BULKHEAD FRAME BELT & INTERCOSTAL IN LINE WITH STGR 14L PER DWG 601-35012 REV-D AND CRJ 200 SRM 51-42-21. CODec 4, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWI2024031200227Hinge Fitting · damagedLH ELEVATOR CENTER HINGE (#3) ON THE ELEVATOR, HAS TOOLING DAMAGE (MARKED) (C-CHECK RO 3/9/2024) REMOVED DAMAGE ON LH ELEVATOR CENTER HINGE (#3) REF CRJ200 SRM 51-12-00 AND COMPLIED WITH ALL STEPS OF REO 601R-55-21-588 REV--, DATED 2024/01/02. SEE CONTINUADec 3, 2023 · N976SW · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA2024031203Seat Track · missingPILOTS INBD. SEAT TRACK SACRIFICIAL PLATE MISSING RIVET HEADS. (MARKED) (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW PILOTS INBOARD SEAT TRACK REF CRJ-200-SRM 51-42-21 AND DRAWING 600-33100 REV AE. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARDec 3, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024031200232Floor Support · corrodedLEFT SIDE PRESSURE FLOOR SILL HAS CORROSION FROM FS 409+128 TO FS 559 IN MULTIPLE AREAS AS MARKED MX TRANS # 27504393 (C-CHECK RO 3/9/2024) REPAIRED L/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS559 REF REO 601R-53-41-666 REV-C DATE:2012-11-06. COMPLIED WIDec 2, 2023 · N976SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWI2024031200231Vane · chafedL/H INBOARD FLAP CENTER REPAIRED VANE CAP IS CHAFE (AREA MARKED ) (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW LEADING EDGE SKIN CENTER SECTION ON LH INBOARD FLAP VANE PER REF CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY ADec 2, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024031200230Vane · chafedL/H INBOARD FLAP INBOARD REPAIR VANE CAP IS CHAFE (AREA MARKED ) (C-CHECK RO 3/9/2024) REMOVED AND REPLACED LH INBOARD FLAP VANE SKIN WITH NEW REPLACEMENT PART AND RESTORED FINISH CRJ200 SRM 51-42-10,DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY ANDec 2, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024031200229Floor Support · corrodedRIGHT SIDE PRESSURE FLOOR SILL HAS CORROSION FROM FS 409+128 TO FS 559 IN MULTIPLE AREAS AS MARKED MX TRANS# 27504449 (C-CHECK RO 3/9/2024) BLENDED OUT CORROSION ON RIGHT SIDE PRESSURE FLOOR SILL 9 BLENDS TOTAL . REF. CRJ-200 SRM 51-21-06. FOUND ALL BLENDDec 2, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024031200228Vane · chafedL/H INBOARD FLAP OUTBOARD REPAIRED VANE CAP IS CHAFE (AREA MARKED ) (C-CHECK RO 3/9/2024) REMOVED AND NSTALLED NEW L/H INB FLAP OUTBOARD VANE CAP REF CRJ200 SRM 51-42-10, DWG601R14302 REV E DATE 2003-01-23. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATIDec 2, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024F00212Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON L/H SIDE SEAT RAIL FROM 461 TO 499 (C-CHECK RO 3/9/2024) REMOVED AND REPLACED WITH NEW LH SIDE SEAT RAIL FROM FS 461 - 499 REF CRJ 200 AMM 53-01-11-400-802, AND REO 601R-53-00-055 REV C DATED 2017-03-21.Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00206Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON R/H SIDE SEAT RAIL FROM 499 TO 544 (C-CHECK RO 3/9/2024) REMOVED AND REPLACED RH SIDE SEAT RAIL FROM FS 499 - 544 REF CRJ 200 AMM 53-01-11-400-802, AND REO 601R-53-00-055 REV C DATED 2017-03-21 REPAIR B.Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00205Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON R/H SIDE SEAT RAIL FROM 461 TO 499 (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW R/H SIDE SEAT TRACK SECTION REF CRJ 200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802 TOOL USED TUC6230 DUE 03/31/24Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00204Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON R/H SIDE SEAT RAIL FROM 409+112 TO 461 (C-CHECK RO 3/9/2024) REMOVED,AND INSTALLED NEW R/H SIDE SEAT RAIL AT FS 409+112 - 461 REF CRJ200 AMM 53-01-11-000-802 AND CRJ200 AMM 53-01-11-400-802, COMPLIED WITH ALL STEPS OFDec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00203Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON R/H SIDE SEAT RAIL FROM 409+16 TO 409+112 (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW R/H SIDE SEAT RAIL SECTION REF CRJ 200 AMM53-01-11-000-802 AND CRJ 200 AMM53-01-11-400-802.TOOL TUC4238 CAL DUE:31-AUG-24. SEE CODec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00215Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON R/H SIDE SEAT RAIL FROM 364 TO 409+16 (C-CHECK RO 3/9/2024) REMOVED CORROSION ON RH SIDE SEAT RAIL FS364 TO FS409+16 REF. CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-21-49 REMOVED AND INSTALLED A NEDec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00214Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON L/H SIDE SEAT RAIL FROM 544 TO 559+80 (C-CHECK RO 3/9/2024) REMOVED CORROSION ON LH SIDE SEAT RAIL FS544 TO FS559+80 REF. CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-21-49 REMOVED AND INSTALLED A NEDec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWI2024F00213Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON L/H SIDE SEAT RAIL FROM 499 TO 544 (C-CHECK RO 3/9/2024) EVALUATED CORROSION ON LH SIDE SEAT RAIL F499 TO FS554 REF. CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 551-51-49 REMOVED AND INSTALLED A NEW FADec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202403121201Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON L/H SIDE SEAT RAIL FROM 409+112 TO 461 (C-CHECK RO 3/9/2024) REMOVED AND REPLACED LH SIDE SEAT RAIL FROM FS 409+112 - FS 461 REF CRJ 200 AMM 53-01-11-400-802, AND REO 601R-53-00-055 REV C DATED 2017-03-21 REPAIR B.Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00220Seat Track · corrodedMULTIPLE AREAS OF CORROSION FOUND ON L/H SIDE SEAT RAIL FROM F/S 409+16 TO 409+112 (C-CHECK RO 3/9/2024) REMOVED AND REPLACED LH SIDE SEAT RAIL FROM FS 409+16 - FS 409+112 REF CRJ 200 AMM 53-01-11-400-802, AND REO 601R-53-00-055 REV C DATED 2017-03-21 REPADec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024031200219Striker · looseRIGHT ENGINE THRUST TORQUE BOX AFT SIDE UPPER OUTBOARD LATCH STRIKER LOOSE (C-CHECK RO 3/9/2024) REMOVED R/H ENGINE THRUST REVERSER UPPER OUTBOARD LATCH STRIKER AND INSTALLED NEW LATCH STRIKER REF. MHIRJ REO 601R-78-30-4353 REV. €“ DATED 2024-01-26 AND SKDec 1, 2023 · N976SW · Cndair CL6002B19 · Engine Mount SectionSDR SWI2024031200218Floor Support · corrodedEVIDENCE OF PITTING CORROSION FOUND ON FLOOR BEAM LBL9 FROM F/S 589 TO 621 (C-CHECK RO 3/9/2024) REMOVED AND WET INSTALLED NEW REPLACEMENT LBL9 FLOOR BEAM CAP P/N 601R35031-263 BETWEEN FS.569 & FS.610 WITH NEW ORIGINAL & ALTERNATE TYPE FASTENERS REF R.E.O.Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024031200217Floorbeam · crackedFS 280.0 FLOOR BEAM AT LBL 9.00 INBOARD ANGLE CRACKED AT LOWER CORNER (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW INBD ANGLE LBL 9.00 ON THE FS280 FLOOR BEAM. REF CRJ200 SRM 51-42-21 AND REO 601R-53-11-926 REV-B DATED 2006/05/10. USED REO601R-53-11-92Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024031200216Door Sill · corrodedANGLE ON THE PASSENGER DOOR SILL HAS CORROSION AT THE AFT END. (MARKED) (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED PASSENGER DOOR SILL REF DWG 601R31527 REV AM, CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-13 . COMPLIED WITH 51-900-100Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024031200211Door Sill · corrodedPASSENGER DOOR LOWER SILL HAS CORROSION ALONG THE FORWARD AND AFT ENDS. (MARKED) (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW PAX DOOR LOWER SILL (STRAP). REF. CRJ200 SRM 51-42-21, REO 601R-53-21-3671 REV.-- DATED 1/20/2024 AND DWG# 601R31527 REV. AM . Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024031200210Door Sill · corrodedPAX DOOR SILL CORRODED IN MULTIPLE AREAS (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW REPLACE PAX DOOR SILL REF CRJ 200 SRM 51-42-06 AND DWG 600-31535 REV J.COMPLIED WITH 51-900-1003-SKY . PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILSDec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024031200209Angle · corrodedANGLE ON THE SERVICE DOOR SILL HAS CORROSION ON THE FORWARD AND AFT SIDES OF THE DOOR STOP FITTINGS. (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED LOWER SERVICE DOOR SILL REF CRJ200 SRM 51-42-06 AND REF CRJ200 SRM 51-42-21 AND DWG 601R38303 REV-AR. COMPLIDec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024031200208Spar · splitLEFT WING INBOARD GROUND SPOILER INNER SPAR PITTED (C-CHECK RO 3/9/2024) REMOVED CORROSION ON THE LH INBD GROUND SPOILER INBD AND OTBD LANDING AND SUPPORT CHANNELS (INNER SPAR). FOUND INBD CHANNEL OUT OF LIMITS AND OTBD CHANNEL WITHIN LIMITS REF CRJ 200 SDec 1, 2023 · N976SW · Cndair CL6002B19 · SpoilersSDR SWI2024031200207Floorbeam · crackedFS 280.00 FLOOR BEAM AT RBL 9.00 OUTBOARD ANGLE CRACKED AT TOP CORNER (C-CHECK RO 3/9/2024) REMOVED AND INSTALLED NEW OUTBOARD CLIP AT FS 280 FLOOR BEAM RBL 9.0 REF CRJ-200-SRM 51-42-21 AND, REO 601R-53-11-926 REV-B DATED 2006/05/10. COMPLIED WITH 51-900-1Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024031200221Skin · damagedLEFT WING OUTBOARD FLAP UPPER SKIN HAS SEVERAL SMOKING RIVETS AS MARKED (C-CHECK RO 3/9/2024) REPAIRED L/H WING OUTBOARD FLAP UPPER SKIN REF REO 601R-54-53-1287 REV -- DATED 2023-12-27. COMPLIED WITH 51-900-1003-SKY AND ALL STEPS OF REO 601R-57-53-1287 REVNov 30, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20240312003Support · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA72727-601R-53-62-303 N976SW MXCODEID58678-PR - APU INLET DOOR MOUNTING STRUCTURE FOR LINEAR ACTUATOR CRACKED AT FS654.5 STR 4L COMPLIED WITH TEMPORARY REPAIRH PER REO 601R-53-62-303 REV - DATED 2021-09-08.PERMANENT REPOct 3, 2023 · N976SW · Cndair CL6002B19 · APU Cowling/ContainmentSDR SWIA202264778None · failedUPON LANDING GEAR EXTENSION, WE RECEIVED A HYD 3 LO PRESS CAUTION MESSAGE, WITH ASSOCIATED GEAR DISAGREE WARNING MESSAGE. WE COMPLETED THE APPROPRIATE QRH PROCEDURES, AND COMPLETED A PRECAUTIONARY LANDING WITH NO FURTHER INCIDENT. (FLIGHT 5701 - FILED OPEN) Mar 7, 2022 · N976SW · Cndair CL6002B19 · Hydraulic Pressure SensorSDR SWIA2020030248884Fitting · damagedLH MLG TRUNNION FWD FITTING WEB UPPER HOLE HAS AN INDICATION 60% FSH AT THE 6 O'CLOCK POSITION INSIDE EDGE. FAILED NDT INSPECTION. (C-CHECK) RO 2/27/2020 COMPLIED WITH REO REV -- REFERENCE M-337 AND MAJOR REPAIR SKYCARD. NO WEIGHT CHANGE NOTEDJan 25, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWIA2020030248899Structure · corrodedCIRUMFERENTIAL JOINT AT F.S.280 HAS CORROSION IN SEVERAL LOCATIONS BETWEEN STRINGER 25 LEFT TO 22 LEFT. (C-CHECK) RO 2/27/2020 REMOVED CORROSIOIN AND FOUND TO BE OUT OF LIMITS. BLENDED AND REPAIRED AREAS IAW BOMBARDIER REO.Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248898Frame · corrodedFRAME SECTOR AT F.S.349 IS CORRODED BETWEEN STRINGER 25R TO 26L (C-CHECK) RO 2/27/2020 REMOVED CORROSION AT FS 349 BETWEEN 25R TO 26L AND FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM. REPAIRED CORROSION IAW BOMBARDIER REO AND PAINTED AREAS IAW CRJ 200 SRM. SJan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020030248897Floorbeam · corrodedF.S. 589 FLOOR CROSS BEAM IS CORRODED AROUND THE NUTPLATE HOLESBETWEEN LBL9 AND LBL27 (C-CHECK) RO 2/27/2020 REMOVED AND REPLACED CAP STRIP AT FS 589 BETWEEN LBL9 AND LBL27 IAW CRJ200 SRM. (PN 601R35031-165)Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020030248896Seat Track · corrodedLBL9 SEAT TRACK IS CORRODED BETWEEN F.S. 559.00 TO F.S. 559+80 (C-CHECK) RO 2/27/2020 REMOVED AND INSTALLED SERVICEABLE SEAT TRACK IAW CRJ 200 AMM REF CONTINUATION CARD FOR DETAILS OF WORK PREFORMEDJan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030248883Support Angle · crackedF.S. 621 BOTTOM SUPPORT ANGLE IS CRACKED BETWEEN RBL27 TO RBL36. (C-CHECK) RO 2/27/2020 CUT AWAY DAMMAGED AREA AND REPAIRED IAW BOMBARDIER REO AND CRJ 200 SRM COMPLETED SDR AND FORM M-337 SEE ATTACHED CONTINUATION CARD AND SKY CARD FOR DETAILS OF WORK PERFJan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030248882Frame · corrodedF.S. 605 FRAME IS CORRODED BETWEEN STRG27 TO STRG 25L. (C-CHECK) RO 2/27/2020 BLENDED CORRODED AREA AT FS 605 BETWEEN STRG 27 TO 25L IAW BOMBARDIER REO COMPLETED FORM M-337 SEE ATTACHED CONTINUATION CARD AND SKY CARD FOR DETAILS OF WORK PERFORMED. NO WEIGHJan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020030248895Seat Track · corrodedRBL 9 SEAT TRACK IS CORRODED BETWEEN FS 409.00+112 AND 559.00. (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 SWIA2020030248894Seat Track · corrodedLBL 9 SEAT TRACK IS CORRODED BETWEEN FS 409.00+112 AND 559.00. (C-CHECK) RO 2/27/2020 FABBED SEAT TRACK IAW REO AND INSTALLED IAW CRJ 200 AMMJan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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