# Service difficulty reports: N976SW

A list on [N976SW](https://openairdocs.org/aircraft/N976SW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 197 reports

- [SDR SWIA2026032075561](https://openairdocs.org/sdr/SWIA2026032075561.md): Skin · damaged · Mar 20, 2026 · N976SW · Cndair CL6002B19 · Wing, Plate/Skin
  > COMPLY 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-
- [SDR SWIA2025042108](https://openairdocs.org/sdr/SWIA2025042108.md): Window · arced · Apr 18, 2025 · N976SW · Cndair CL6002B19 · Flight Compartment Windows
  > DURING 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 B
- [SDR SWI2025F00311](https://openairdocs.org/sdr/SWI2025F00311.md): Stall Warning · false activation · Mar 7, 2025 · N976SW · Cndair CL6002B19 · Central Warning
  > STALL 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
- [SDR SWIA202501220075](https://openairdocs.org/sdr/SWIA202501220075.md): Flap System · failed · Jan 20, 2025 · N976SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > WHEN 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) C
- [SDR SWIA20240614001](https://openairdocs.org/sdr/SWIA20240614001.md): Warning Message · illuminated · Jun 14, 2024 · N976SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > D: 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,
- [SDR SWIA2024031200104](https://openairdocs.org/sdr/SWIA2024031200104.md): Stiffener · cracked · Jan 4, 2024 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NDT 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
- [SDR SWI2024031200226](https://openairdocs.org/sdr/SWI2024031200226.md): Hinge Fitting · gouged · Dec 6, 2023 · N976SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LH 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. COM
- [SDR SWI2024031200225](https://openairdocs.org/sdr/SWI2024031200225.md): Hinge Fitting · gouged · Dec 6, 2023 · N976SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > RH 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-57-51-1
- [SDR SWI202403120224](https://openairdocs.org/sdr/SWI202403120224.md): Fitting · gouged · Dec 6, 2023 · N976SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LH 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 A
- [SDR SWI2024031200223](https://openairdocs.org/sdr/SWI2024031200223.md): Skin · cracked · Dec 6, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > POSSIBLE 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 GOO
- [SDR SWI2024031200222](https://openairdocs.org/sdr/SWI2024031200222.md): Skin · cracked · Dec 6, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > POSSIBLE 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 GOO
- [SDR SWIA202403120004](https://openairdocs.org/sdr/SWIA202403120004.md): Bracket · cracked · Dec 4, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS625 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. CO
- [SDR SWI2024031200227](https://openairdocs.org/sdr/SWI2024031200227.md): Hinge Fitting · damaged · Dec 3, 2023 · N976SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > LH 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 CONTINUA
- [SDR SWIA2024031203](https://openairdocs.org/sdr/SWIA2024031203.md): Seat Track · missing · Dec 3, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PILOTS 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 CAR
- [SDR SWI2024031200232](https://openairdocs.org/sdr/SWI2024031200232.md): Floor Support · corroded · Dec 2, 2023 · N976SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LEFT 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 WI
- [SDR SWI2024031200231](https://openairdocs.org/sdr/SWI2024031200231.md): Vane · chafed · Dec 2, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge Flaps
  > L/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 A
- [SDR SWI2024031200230](https://openairdocs.org/sdr/SWI2024031200230.md): Vane · chafed · Dec 2, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge Flaps
  > L/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 AN
- [SDR SWI2024031200229](https://openairdocs.org/sdr/SWI2024031200229.md): Floor Support · corroded · Dec 2, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT 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 BLEND
- [SDR SWI2024031200228](https://openairdocs.org/sdr/SWI2024031200228.md): Vane · chafed · Dec 2, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge Flaps
  > L/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 CONTINUATI
- [SDR SWI2024F00212](https://openairdocs.org/sdr/SWI2024F00212.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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.
- [SDR SWI2024F00206](https://openairdocs.org/sdr/SWI2024F00206.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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.
- [SDR SWI2024F00205](https://openairdocs.org/sdr/SWI2024F00205.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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 03/31/24
- [SDR SWI2024F00204](https://openairdocs.org/sdr/SWI2024F00204.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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 OF
- [SDR SWI2024F00203](https://openairdocs.org/sdr/SWI2024F00203.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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 CO
- [SDR SWI2024F00215](https://openairdocs.org/sdr/SWI2024F00215.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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 NE
- [SDR SWI2024F00214](https://openairdocs.org/sdr/SWI2024F00214.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > MULTIPLE 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 NE
- [SDR SWI2024F00213](https://openairdocs.org/sdr/SWI2024F00213.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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 FA
- [SDR SWIA202403121201](https://openairdocs.org/sdr/SWIA202403121201.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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.
- [SDR SWI2024F00220](https://openairdocs.org/sdr/SWI2024F00220.md): Seat Track · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE 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 REPA
- [SDR SWI2024031200219](https://openairdocs.org/sdr/SWI2024031200219.md): Striker · loose · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Engine Mount Section
  > RIGHT 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 SK
- [SDR SWI2024031200218](https://openairdocs.org/sdr/SWI2024031200218.md): Floor Support · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EVIDENCE 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.
- [SDR SWI2024031200217](https://openairdocs.org/sdr/SWI2024031200217.md): Floorbeam · cracked · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 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-53-11-92
- [SDR SWI2024031200216](https://openairdocs.org/sdr/SWI2024031200216.md): Door Sill · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE 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 51-900-100
- [SDR SWI2024031200211](https://openairdocs.org/sdr/SWI2024031200211.md): Door Sill · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER 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.
- [SDR SWI2024031200210](https://openairdocs.org/sdr/SWI2024031200210.md): Door Sill · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX 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 DETAILS
- [SDR SWI2024031200209](https://openairdocs.org/sdr/SWI2024031200209.md): Angle · corroded · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE 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. COMPLI
- [SDR SWI2024031200208](https://openairdocs.org/sdr/SWI2024031200208.md): Spar · split · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Spoilers
  > LEFT 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 S
- [SDR SWI2024031200207](https://openairdocs.org/sdr/SWI2024031200207.md): Floorbeam · cracked · Dec 1, 2023 · N976SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 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 51-900-1
- [SDR SWI2024031200221](https://openairdocs.org/sdr/SWI2024031200221.md): Skin · damaged · Nov 30, 2023 · N976SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT 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 REV
- [SDR SWIA20240312003](https://openairdocs.org/sdr/SWIA20240312003.md): Support · cracked · Oct 3, 2023 · N976SW · Cndair CL6002B19 · APU Cowling/Containment
  > COMPLY 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 REP
- [SDR SWIA202264778](https://openairdocs.org/sdr/SWIA202264778.md): None · failed · Mar 7, 2022 · N976SW · Cndair CL6002B19 · Hydraulic Pressure Sensor
  > UPON 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)
- [SDR SWIA2020030248884](https://openairdocs.org/sdr/SWIA2020030248884.md): Fitting · damaged · Jan 25, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LH 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 NOTED
- [SDR SWIA2020030248899](https://openairdocs.org/sdr/SWIA2020030248899.md): Structure · corroded · Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CIRUMFERENTIAL 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.
- [SDR SWIA2020030248898](https://openairdocs.org/sdr/SWIA2020030248898.md): Frame · corroded · Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 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. S
- [SDR SWIA2020030248897](https://openairdocs.org/sdr/SWIA2020030248897.md): Floorbeam · corroded · Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > F.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)
- [SDR SWIA2020030248896](https://openairdocs.org/sdr/SWIA2020030248896.md): Seat Track · corroded · Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 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 PREFORMED
- [SDR SWIA2020030248883](https://openairdocs.org/sdr/SWIA2020030248883.md): Support Angle · cracked · Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > F.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 PERF
- [SDR SWIA2020030248882](https://openairdocs.org/sdr/SWIA2020030248882.md): Frame · corroded · Jan 12, 2020 · N976SW · Cndair CL6002B19 · Fuselage Main, Frame
  > F.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 WEIGH
- [SDR SWIA2020030248895](https://openairdocs.org/sdr/SWIA2020030248895.md): Seat Track · corroded · Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 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.
- [SDR SWIA2020030248894](https://openairdocs.org/sdr/SWIA2020030248894.md): Seat Track · corroded · Jan 11, 2020 · N976SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 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

Next page: https://openairdocs.org/aircraft/N976SW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N976SW/reports

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