# Service difficulty reports: N960SW

A list on [N960SW](https://openairdocs.org/aircraft/N960SW.md).

Newest first.

Page 1 of 4 · 183 reports

- [SDR SWIA202505300028](https://openairdocs.org/sdr/SWIA202505300028.md): Warning Message · activated · May 28, 2025 · N960SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > D:ON DEPARTURE SELECTED GEAR UP AND GOT A GEAR DISAGREE FOR THE NOSE GEAR. RAN QRH PROCEDURE AND GOT A GEAR DOWN 3 GREEN.C: MEL 32-30-1CAT:A DUE DATE: 29 MAY 2025? S23 (ARROW DOWN) FAR? S21 (ARROW DOWN) NEAR? S35 (ARROW DOWN) NEAR? S22 (ARROW DOWN) FAR? S30 (A
- [SDR SWI2025F00693](https://openairdocs.org/sdr/SWI2025F00693.md): Landing Gear · warning message · May 28, 2025 · N960SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > D:ON DEPARTURE SELECTED GEAR UP AND GOT A GEAR DISAGREE FOR THE NOSE GEAR. RAN QRH PROCEDURE AND GOT A GEAR DOWN 3 GREEN.C: MEL 32-30-1CAT:A DUE DATE: 29 MAY 2025? S23 (ARROW DOWN) FAR? S21 (ARROW DOWN) NEAR? S35 (ARROW DOWN) NEAR? S22 (ARROW DOWN) FAR? S30 (A
- [SDR SWIA202412300029](https://openairdocs.org/sdr/SWIA202412300029.md): Proximity Sensor · malfunctioned · Dec 29, 2024 · N960SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE AND NOSE GEAR MASTER WARNING WHEN GEAR HANDLE SELECTED UP. RAN QRH/QRH RETURNED TO LNK. UPON ARRIVAL TO AIRCRAFT FOUND NLG CENTERING PROX SENSOR HARNESS DAMAGED. REMOVED AND REPLACED NLG CENTERING PROX SENSOR AND WOW #2 PROX SENSOR HARNESS PER
- [SDR SWIA2024091600011](https://openairdocs.org/sdr/SWIA2024091600011.md): Skin · dented · Sep 11, 2024 · N960SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA92033-601R-53-31-1304 MXCODEID77076-PR - DENT DAMAGE TO FUSELAGE SKIN PANEL BETWEEN FS409.00+80-FS409.00+96 AND STR16R-STR17R. COMPLIED WITH TEMPORARY REPAIR PER 601R-53-31-1304. PERMANENT REPAIR DUE WITHIN 300 FLIGHT
- [SDR SWIA2024071700005](https://openairdocs.org/sdr/SWIA2024071700005.md): Windshield · cracked · Jul 15, 2024 · N960SW · Cndair CL6002B19 · Flight Compartment Windows
  > F.O. WINDSHIELD CRACKED. (FILED CLOSED)REMOVED AND REPLACED FO WINDSHIELD IN REFERENCE TO AMM 56-11-01 UP TO AND INCLUDING SUBTASK 56-11-01-430-007. SEE ML 28528337 FOR CONTINUATION OF INSTALLATION.
- [SDR SWIA2023062601](https://openairdocs.org/sdr/SWIA2023062601.md): Unknown · cracked · Jun 1, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FLANGED STRAP AT FS559.00 BETWEEN BL0.0 TO LBL9 IS CRACKED (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW FLANGED STRAP AT FS559.00 BETWEEN BL0.0 TO LBL9 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13 AND DWG NO 601R31025 REV N. COMPLIED WITH TASK CAR
- [SDR SWIA20230626518](https://openairdocs.org/sdr/SWIA20230626518.md): Unknown · corroded · May 18, 2023 · N960SW · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR LWR INNER PAN SPLICE DOUBLER CORRODED (C-CHECK RO 6/20/2023) REMOVED SERVICE DOOR LWR INNER PAN SPLICE DOUBLER AND INSTALLED NEW SERVICE DOOR LWR INNER PAN SPLICE DOUBLER REF. DRWG 601R38304 REV. BN AND CRJ 200 SRM 51-42-06.LOCATED AND DR
- [SDR SWI2023F00076](https://openairdocs.org/sdr/SWI2023F00076.md): Unknown · corroded · May 14, 2023 · N960SW · Cndair CL6002B19 · Fuel Storage
  > RIGHT WING LOWER PLANK ACCESS HOLE 610BB HAS COROSSION (C-CHECK RO 6/20/2023) CLEANED AND BLENDED OUT CORROSION ON RH WING LOWER PLANK ACCESS HOLE COMMON TO 610BB IAW REO 601R-57-21-030 REV -L DATED 2014-02-05. FOUND TO BE WITH IN LIMITS. COMPLIED WITH
- [SDR SWI2023F00075](https://openairdocs.org/sdr/SWI2023F00075.md): Unknown · corroded · May 14, 2023 · N960SW · Cndair CL6002B19 · Fuel Storage
  > RIGHT WING LOWER PLANK ACCESS HOLE 640BB HAS COROSSION (C-CHECK RO 6/20/2023) CLEANED AND BLENDED OUT CORROSION ON RH WING LOWER PLANK ACCESS HOLE COMMON TO 640BB IAW REO 601R-57-21-030 REV -L DATED 2014-02-05. FOUND TO BE OUT LIMITS. RECEIVED AND COMPL
- [SDR SWI2023F00074](https://openairdocs.org/sdr/SWI2023F00074.md): Unknown · corroded · May 14, 2023 · N960SW · Cndair CL6002B19 · Fuel Storage
  > LEFT WING LOWER PLANK ACCESS HOLE 510AB HAS COROSSION (C-CHECK RO 6/20/2023) CLEANED AND BLENDED OUT CORROSION ON LH WING LOWER PLANK ACCESS HOLE COMMON TO 510AB IAW REO 601R-57-21-030 REV -L DATED 2014-02-05. FOUND TO BE OUT OF LIMITS. RECEIVED AND COM
- [SDR SWIA202306260514](https://openairdocs.org/sdr/SWIA202306260514.md): Unknown · corroded · May 14, 2023 · N960SW · Cndair CL6002B19 · Fuel Storage
  > LEFT WING LOWER PLANK ACCESS HOLE 540BB HAS COROSSION (C-CHECK RO 6/20/2023) CLEANED AND BLENDED OUT CORROSION ON LH WING LOWER PLANK ACCESS HOLE COMMON TO 540BB IAW REO 601R-57-21-030 REV -L DATED 2014-02-05. FOUND TO BE OUT OF LIMITS. RECEIVED AND COM
- [SDR SWIA20230626511](https://openairdocs.org/sdr/SWIA20230626511.md): Unknown · cracked · May 11, 2023 · N960SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR HANDLE DOUBLER HAS 2 CRACKS AT FASTENERS HOLES (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW HANDLE DOUBLER IAW CRJ 200 SRM 51-42-06 AND DWG 601R35027 REV. AY. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.
- [SDR SWI2023F00073](https://openairdocs.org/sdr/SWI2023F00073.md): Unknown · cracked · May 10, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *CRACK NOTED ON INTERCOASTAL SUPPORT BRKT BETWEEN FS621-FS625 AND BETWEEN STRG14L-13L (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW INTERCOSTAL SUPPORT BRACKET P/N: 601R350121-9 BETWEEN FS 621 - FS 625 ON TOP OF STGR 13L REF CRJ200 SRM 51-42
- [SDR SWI2023F00072](https://openairdocs.org/sdr/SWI2023F00072.md): Unknown · gouged · May 10, 2023 · N960SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > *CARGO DOOR HANDLE HOUSING IS GOUGED (MARKED) (C-CHECK RO 6/20/2023) CARGO DOOR HOUSING FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW CARGO DOOR HANDLE HOUSING REF CRJ 200 SRM 51-42-21 AND DWG 601R35027 REV. AY. COMPLIED WITH TASK CARD 51-900-100
- [SDR SWI2023F00071](https://openairdocs.org/sdr/SWI2023F00071.md): Unknown · gouged · May 10, 2023 · N960SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > *CARGO DOOR AFT SOCKET FITTING IS GOUGED (MARKED) (C-CHECK RO 6/20/2023) BLENDED DAMAGE OUT ON CARGO DOOR AFT SOCKET FITTING REF. CRJ 200 SRM 51-12-00, COMPLIED WITH REO 601R-52-31-406 REV-- DATED 2023-05-23 STEPS 1 THROUGH 5. COMPLIED WITH SKYWEST CARD
- [SDR SWI2023F100070](https://openairdocs.org/sdr/SWI2023F100070.md): Unknown · cracked · May 10, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CRACK NOTED ON INTERCOASTAL SUPPORT BRKT BETWEEN FS625-FS621 AT STRG14L (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW INTERCOSTAL SUPPORT BRACKET P/N: 601R350121-5 BETWEEN FS 621 - 625 AT STGR 14L REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-
- [SDR SWI2023F00070](https://openairdocs.org/sdr/SWI2023F00070.md): Unknown · cracked · May 10, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CRACK NOTED ON INTERCOASTAL SUPPORT BRKT BETWEEN FS625-FS621 AT STRG14L (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW INTERCOSTAL SUPPORT BRACKET P/N: 601R350121-5 BETWEEN FS 621 - 625 AT STGR 14L REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-
- [SDR SWI2023F00085](https://openairdocs.org/sdr/SWI2023F00085.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RH SIDE SEAT TRACK FS544.00 - FS559.00+48 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED RH SIDE SEAT TRACK FS544.00 - FS559.00+48 REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00084](https://openairdocs.org/sdr/SWI2023F00084.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RH SIDE SEAT TRACK FS499.00 - FS544.00 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED RH SIDE SEAT TRACK FS499.00 - FS544REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00083](https://openairdocs.org/sdr/SWI2023F00083.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RH SIDE SEAT TRACK FS449.85 - FS499.00 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED RH SIDE SEAT TRACK FS449.85 - FS499REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00082](https://openairdocs.org/sdr/SWI2023F00082.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RH SIDE SEAT TRACK FS409.00+128 - FS449.85 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REPLACED OUT OF LIMITS RH SIDE SEAT TRACK AT FS409.00+128 - FS449.85 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B
- [SDR SWIA202306265109](https://openairdocs.org/sdr/SWIA202306265109.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LH SIDE SEAT TRACK FS544.00 - FS559.00+80 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED LH SIDE SEAT TRACK FS544.00 - FS559.00+80 REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00081](https://openairdocs.org/sdr/SWI2023F00081.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LH SIDE SEAT TRACK FS499.00 - FS544.00 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED LH SIDE SEAT TRACK FS499.00 - FS544. REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00080](https://openairdocs.org/sdr/SWI2023F00080.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LH SIDE SEAT TRACK FS449.85 - FS499.00 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED LH SIDE SEAT TRACK FS449.85 - FS499. REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00079](https://openairdocs.org/sdr/SWI2023F00079.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LH SIDE SEAT TRACK FS409.00+128 - FS427.00 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED LH SIDE SEAT TRACK FS409.00+128 - FS427. REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00078](https://openairdocs.org/sdr/SWI2023F00078.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *RH SIDE SEAT TRACK FS409.00+16 - FS409.00+112 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REPLACED OUT OF LIMITS RH SIDE SEAT TRACK AT FS409.00+16 - FS409.00+112 IAW REO 601R-53-00-055 REV -C DATED 2017-03-21 REPAIR B
- [SDR SWIA2023062600509](https://openairdocs.org/sdr/SWIA2023062600509.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LH SIDE SEAT TRACK FS409.00+16 - FS409.00+112 CORRODED/GOUGED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND REPLACED LH SIDE SEAT TRACK AT FS409.00+16 - FS409.00+112 REF CRJ 200 AMM 53-01-11-400-802 TORQUE WRENCH TUC8619 DUE 31 OCT23
- [SDR SWI2023F00069](https://openairdocs.org/sdr/SWI2023F00069.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *FS409.00+128 - 559.00 RBL9 SEAT TRACK CORRODED/GOUGED ENTIRE LENTH OF STICK (MARKED) (C-CHECK RO 6/20/2023) REMOVED OUT OF LIMITS SEAT TRACK AND INSTALLED NEW ONE AT FS409.00+128 - 559.00 RBL9 IAW CRJ 200 AMM 53-01-11-000-802 & CRJ 200 AMM 53-01-11-400
- [SDR SWI2023F00068](https://openairdocs.org/sdr/SWI2023F00068.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *FS409.00+128 - 559.00 LBL9 SEAT TRACK CORRODED/GOUGED ENTIRE LENTH OF STICK (MARKED) (C-CHECK RO 6/20/2023) REMOVED OUT OF LIMITS SEAT TRACK AND INSTALLED NEW ONE AT FS409.00+128 - 559.00 LBL9 IAW REO 601R-53-00-485 REV -D DATED 2018-01-29
- [SDR SWI2023F00067](https://openairdocs.org/sdr/SWI2023F00067.md): Unknown · cracked · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS280.00 SPLICE ANGLE AT STGR3L CRACKED (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED 1EA NEW SPLICE ANGLE AT FS 280.00, STGR3L REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG# 600-31057 REV P. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2023F00066](https://openairdocs.org/sdr/SWI2023F00066.md): Unknown · cracked · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS484.00 LBL27-36, FLIGHT CONTROL CABLE GUIDE ROLLER ASSY, INBD ATTACH ANGLE CRACKED (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED 1EA NEW INBD ATTACH ANGLE AT FS484.00 LBL27-36, FLIGHT CONTROL CABLE GUIDE ROLLER ASSY REF CRJ200 SRM 51-42-06,
- [SDR SWIA20230626509](https://openairdocs.org/sdr/SWIA20230626509.md): Unknown · elongated · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS559.00 LBL9 BEAM CAP FASTENER HOLE ELONGATED (MARKED) (C-CHECK RO 6/20/2023) REPAIRED ELONGATED HOLES BY OVERSIZED HOLES AND INSTALING LARGER FASTENERS REF REO 601R-53-41-3164, REV - -, 2023-05-16COMPLIED WITH SKY CARD 51-900-1003-SKY
- [SDR SWI2023F00065](https://openairdocs.org/sdr/SWI2023F00065.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FS461.00 - FS484.00 LBL9 BEAM CAP CORRODED (MARKED) (C-CHECK RO 6/20/2023) BLENDED CORROSION AT 2 EA. MARKED LOCATIONS ON THE LBL 9 FLOOR BEAM UPPER CAP ON INBD FLANGE BETWEEN FS 461.00 - 484.00 REF CRJ-200 SRM 51-21-06. CORROSION AT 2 EA. LOCATIONS FO
- [SDR SWI2023F00064](https://openairdocs.org/sdr/SWI2023F00064.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FWD OF 409.00+128 TO AFT OF 559.00 RBL9 BEAM CAP CORRODED IN SEVERAL AREAS (MARKED) (C-CHECK RO 6/20/2023) BLENDED CORRODED AREAS AT MARKED LOCATIONS ON THE RBL 9 FLOOR BEAM UPPER CAP BETWEEN FS 409+128 TO FS 559.00 REF CRJ-200 SRM 51-21-06.FOUND TO B
- [SDR SWI2023F00063](https://openairdocs.org/sdr/SWI2023F00063.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *RH PRESSURE FLOOR SILL PANEL FS409.00+128 - FS559.00, SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK RO 6/20/2023) BLENDED OUT CORROSION ON RH PRESSURE FLOOR PANEL FROM FS 409+128 TO FS 559 AT 17 LOCATIONS REF REO 601R-53-41-666 REV C DATED 2012-11-06 DI
- [SDR SWIA202306260509](https://openairdocs.org/sdr/SWIA202306260509.md): Unknown · corroded · May 9, 2023 · N960SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *LH PRESSURE FLOOR SILL PANEL FS409.00+128 - FS559.00, SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK RO 6/20/2023) BLENDED OUT CORROSION ON LH PRESSURE FLOOR SILL PANEL FROM FS 409+128 TO FS 559 AT 19 LOCATIONS REF REO 601R-53-41-666 REV C DATED 2012-11-
- [SDR SWI2023F00062](https://openairdocs.org/sdr/SWI2023F00062.md): Unknown · cracked · May 9, 2023 · N960SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > *FS484.00 RBL27-36, FLIGHT CONTROL CABLE GUIDE ROLLER ASSY, OUTBD ATTACH ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED1EA NEW OUTBOARD ATTACH ANGLE P/N 601R31171-9 AT FS484.00 RBL27-36, FLIGHT CONTROL CABLE GUIDE ROLLER A
- [SDR SWIA202306260508](https://openairdocs.org/sdr/SWIA202306260508.md): Unknown · elongated · May 8, 2023 · N960SW · Cndair CL6002B19 · Aerodynamic Fairings
  > UPON REMOVAL OF RH MLG BAY UPPER WING SKIN PANEL FOR JOB 27853101 OP 360 MXTRANS# 26587440, FOUND MOST INBOARD FWD HOLE TO BE ELONGATED (1 EA) (C-CHECK RO 6/20/2023) PERFORMED REPAIR TO OVERSIZED FASTENER HOLE ON WING BOX UPPER INBOARD SKIN AT WS48.30 A
- [SDR SWI2023F00061](https://openairdocs.org/sdr/SWI2023F00061.md): Unknown · corroded · May 7, 2023 · N960SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > DURING THE AUDIT 96/72MO TASK CARD 53-900-511, DI OF THE RIGHT LONGERON €ŒT€? BRACKETS AND UPPER SURFACE OF PRESSURE FLOOR SILL STRUCTURE (CPCP), FOUND MULTIPLE AREAS OF CORROSION AND/OR PAINT BUBBLING ALONG THE FLOOR SILL BETWEEN 409+128 €“ 559, SPECIALLY
- [SDR SWIA2023062600507](https://openairdocs.org/sdr/SWIA2023062600507.md): Unknown · corroded · May 7, 2023 · N960SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > DURING THE AUDIT 96/72MO TASK CARD 53-900-510, DI OF THE LEFT LONGERON €ŒT€? BRACKETS AND UPPER SURFACE OF PRESSURE FLOOR SILL STRUCTURE (CPCP), FOUND MULTIPLE AREAS OF CORROSION AND/OR PAINT BUBBLING ALONG THE FLOOR SILL BETWEEN 409+128 €“ 559, SPECIALLY A
- [SDR SWIA20230626506](https://openairdocs.org/sdr/SWIA20230626506.md): Unknown · corroded · May 6, 2023 · N960SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR FWD LWR SEAL RETAINER CORRODED (C-CHECK RO 6/20/2023) REMOVED CORROSION SERVICE DOOR FWD LWR SEAL RETAINER REF CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FWD LWR SEAL RETAINER REF. DWG 601R38304 REV. BN AND C
- [SDR SWIA202306260506](https://openairdocs.org/sdr/SWIA202306260506.md): Unknown · corroded · May 6, 2023 · N960SW · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR LWR OUTER PAN SPLICE DOUBLER CORRODED (C-CHECK RO 6/20/2023) REMOVED CORROSION FROM SERVICE DOOR LWR OUTER PAN SPLICE DOUBLER REF. CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW SERVICE DOOR LWR OUTER PAN SPLICE
- [SDR SWI2023F00060](https://openairdocs.org/sdr/SWI2023F00060.md): Unknown · cracked · May 6, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *CRACK NOTED AT R/H WINDSHIELD SIDE POST SUPPORT FRAME AT APPROX WS228.00 (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW POST SUPPORT FRAME AT RH WINDSHIELD SIDE AT APPROX WS228.00 REF CRJ200 SRM 51-42-06 AND DRW 601R34032 REV -P. COMPLIED WI
- [SDR SWI2023F00059](https://openairdocs.org/sdr/SWI2023F00059.md): Unknown · bent · May 6, 2023 · N960SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > *CARGO DOOR FRAME ASSY AT FS574 IS BENT AT MULTIPLE LOCATIONS (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW CHANNEL ON CARGO DOOR FRAME ASSY AT FS574 REF CRJ200 SRM 51-42-06 AND DWG NO 601R35050 REV AC. COMPLIED WITH TASK CARD 51-900-1003-SK
- [SDR SWI2023F00058](https://openairdocs.org/sdr/SWI2023F00058.md): Unknown · cracked · May 6, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING THE AUDIT OF 1C TASK CARD 53-160-301, INTERNAL ZONAL INSPECTION OF THE RIGHT MAIN LANDING GEAR WHEEL WELL (EWIS), FOUND THE RH HYDRAULIC FUSE BRACKET CRACKED. (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW BRACKET P/N 601R75278-11 FROM RIGHT M
- [SDR SWI2023F00057](https://openairdocs.org/sdr/SWI2023F00057.md): Unknown · missing · May 6, 2023 · N960SW · Cndair CL6002B19 · Passenger/Crew Doors
  > *PAX DOOR MISSING CLIP AT MID DD4 INTERCOASTAL AND FS320.163 (MARKED) (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED DD4 CLIP. REF: REO 601R-52-10-909, REV: -- DATED 2023-05-17,COMPLIED WITH ALL STEPS REO 601R-52-10-909, REV: -- DATED 2023-05-17 COMPLIED
- [SDR SWI2023F00091](https://openairdocs.org/sdr/SWI2023F00091.md): Unknown · cracked · May 5, 2023 · N960SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > * NOSE LANDING GEAR WHEEL WELL, CLIP AT RBL9, FS202 IS CRACKED. (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW FABRICATED CLIP AT NOSE LANDING GEAR WHEEL WELL, AT RBL9, FS202 REFCRJ200 SRM 51-42-06 AND DWG#604-33101 REV-P. COMPLIED WITH TASK CARD 51
- [SDR SWIA202306261505](https://openairdocs.org/sdr/SWIA202306261505.md): Unknown · chafed · May 5, 2023 · N960SW · Cndair CL6002B19 · Wing Structure
  > L/H AILERON L/E CHAFFING MULTIPLE AREA NOTED L/E UPPER FIXED SKIN (MARKED) (C-CHECK RO 6/20/2023) BLENDED OUT CHAFFING DAMAGE IN THE L/H AILERON L/E UPPER FIXED SKIN AT MULTIPLE AREAS. REF: CRJ-200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM
- [SDR SWI2023F00090](https://openairdocs.org/sdr/SWI2023F00090.md): Unknown · gouged · May 4, 2023 · N960SW · Cndair CL6002B19 · Ailerons
  > *R/H INBD FLAP AFT LUG PLATES FOR INBD HINGE ARM GOUGED (2EA) (MARKED) (C-CHECK RO 6/20/2023) BLENDED OUT 2 EA GOUGES ON R/H INBD FLAP AFT LUG PLATES FOR INBD HINGE ARM. REF: CRJ200 SRM 51-12-00. DAMAGE REPAIRED PER REO 601R-57-52-2487, REV: --, 2023
- [SDR SWI2023F00089](https://openairdocs.org/sdr/SWI2023F00089.md): Unknown · damaged · May 4, 2023 · N960SW · Cndair CL6002B19 · Ailerons
  > *R/H INBD FLAP INBD HINGE ARM ASSY. TOP PLATE HAS IMPACT DAMAGE (MARKED) (C-CHECK RO 6/20/2023) DENTS ARE NOT PERMITTED ON HINGE ARM FITTING. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 57-54-00. REMOVED AND INSTALLED NEW BRACKET REF CRJ200 SRM 51-42-06 AN

Next page: https://openairdocs.org/aircraft/N960SW/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 = 'N960SW'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N960SW/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.