# Service difficulty reports: N962SW

A list on [N962SW](https://openairdocs.org/aircraft/N962SW.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 · 173 reports

- [SDR SWIA2025090900008](https://openairdocs.org/sdr/SWIA2025090900008.md): Thrust Reverser · warning message · Sep 8, 2025 · N962SW · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT REV UNLOCKED MESSAGE IN FLIGHT. LT REV UNLOCKED IN FLIGHT. RAN QRC AND QRH. IN GRB. IS NOT DEPLOYED. DEFERRED LEFT THRUST REVERSER PER MEL 78-30-1. MX PROCEDURE COMPLIED WITH. PLACARDED AS REQUIRED.
- [SDR SWI2025F00414](https://openairdocs.org/sdr/SWI2025F00414.md): Stop Fitting · gouged · Mar 6, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SURROUND LOWER AFT STOP FITTING IS GOUGED (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW AFT LOWER STOP FITTING P/N:601R35203-5 & SHIM LAMINATED P/N: 601R35207-9. REF DWG 601R35207 REV -W AND REF CRJ 200 SRM 51-41-02. COMPLIED WITH SKYWEST TASK CA
- [SDR SWIA2025033106](https://openairdocs.org/sdr/SWIA2025033106.md): Stop Fitting · gouged · Mar 6, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SURROUND LOWER FWD STOP FITTING IS GOUGED (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW CARGO DOOR SURROUND FWD LOWER STOP FITTING P/N:601R35203-5 & SHIM LAMINATED P/N: 601R35207-9 IAW CRJ 200 SRM 51-41-02 AND DWG 601R35203 REV -A. TORQUE WRENCH
- [SDR SWIA20250331206](https://openairdocs.org/sdr/SWIA20250331206.md): Skin · chafed · Feb 6, 2025 · N962SW · Cndair CL6002B19 · Wing, Plate/Skin
  > S/N 0412RIGHT WING LOWER WING PLANK ACCESS HOLE 640BB HAS CHAFING AND PIN HOLES AROUND IT'S CIRCUMFRANCE. FLAGGED (C-CHECK RO 03/30/2024)REPAIRED RH WING LOWER WING PLANK ACCESS HOLE 640BB IAW REO 601R-57-21-030 REV -L DATED: 2014-02-05 AND REO 601R-57-21-3899
- [SDR SWI2025F00413](https://openairdocs.org/sdr/SWI2025F00413.md): Attach Angle · cracked · Jan 25, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CRACK NOTED ON CLIP ANGLE ATTACHED TO FRAME 625.30 AT APPROX STRG 14R (MARKED) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW CLIP ANGLE (INTERCOSTAL) P/N 601-35012-52, ON FS 625.30 AT APPROX. STRG 14R, REF. CRJ-200, SRM 51-42-21 AND DWG 601-35012, REV. D. C
- [SDR SWIA20250331025](https://openairdocs.org/sdr/SWIA20250331025.md): Attach Angle · cracked · Jan 25, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CRACK NOTED ON CLIP ANGLE ATTACHED TO FRAME 625.30 AT APPROX STRG 14L (MARKED) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED CLIP ANGLE CRACKED FROM FRAME 625.30 AT APPROX. STRG 14L, REF. CRJ-200, SRM 51-42-21 AND DWG 601-35012, REV. D. COMPLIED WITH TASK CARD
- [SDR SWIA20250331124](https://openairdocs.org/sdr/SWIA20250331124.md): Floor Support · corroded · Jan 24, 2025 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FS409+128 - FS559.00. (MARKED) (C-CHECK RO 03/30/2024)REMOVED CORROSION ON L/H PRESSURE FLOOR SILL FS409+128 - FS559.00 AT 14 EA LOCATIONS REF CRJ200 SRM 51-21-06. FOUNS TO BE OUT OF LIMITS. RECEIVED AND
- [SDR SWIA202503310124](https://openairdocs.org/sdr/SWIA202503310124.md): Floor Support · corroded · Jan 24, 2025 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FS409+128 - FS559.00. (MARKED) (C-CHECK RO 03/30/2024)REMOVED CORROSION ON R/H FLOOR SILL AT 14EA LOCATIONS FROM FS 409+128 TO FS 559 REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. RECEIVED AND COM
- [SDR SWIA20250331123](https://openairdocs.org/sdr/SWIA20250331123.md): Door Sill · corroded · Jan 23, 2025 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW AFT CARGO DOOR FLOOR SILL. REF REO 601R-53-61-1574 REV B DATED 2012-04-15 ALL STEPS, DWG 601R35011 REV R & CRJ200 SRM 51-42-06. SRM 51-42-21. COMPLIED WIT
- [SDR SWI2025F00410](https://openairdocs.org/sdr/SWI2025F00410.md): Mount · cracked · Jan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RH MLG VOLUMETRIC FUSE MOUNT IS CRACKED INSIDE WHEEL WELL (UNDERSIDE OF PRESSURE FLOOR) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW RH MLH VOLUMETRIC FUSE MOUNTING BRACKET REF CRJ200 SRM 51-41-02, CRJ200 SRM 51-42-06 AND BOMBARDIER DWG: 601R75278 REV -G.
- [SDR SWI2025F00409](https://openairdocs.org/sdr/SWI2025F00409.md): Floorbeam · cracked · Jan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAM RBL9 INBOARD CLIP ON THE FS280.00 BEAM IS CRACKED IN THE RADIUS AT THE TOP OF THE CLIP. (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW FLOOR BEAM RBL9 INBOARD CLIP ON THE FS280.00 BEAM REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21 AND DWG. 601R
- [SDR SWI2025F00408](https://openairdocs.org/sdr/SWI2025F00408.md): Mount · corroded · Jan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > GALLEY 1 FORWARD INBOARD, AFT AND AFT INBOARD MOUNTS ON THE CABIN FLOOR STRUCTURE ARE CORRODED. (MARKED) (C-CHECK RO 03/30/2024)REMOVED AND REPLACED GALLEY 1 AFT INBD FLOOR MOUNT PLATE REF CRJ 200 SRM 51-42-06 AND DWG NO 601R38669 REV -N. BLENDED AND EVAL'D GA
- [SDR SWI2025F00407](https://openairdocs.org/sdr/SWI2025F00407.md): Mount · cracked · Jan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LH MLG VOLUMETRIC FUSE MOUNT IS CRACKED INSIDE WHEEL WELL (UNDERSIDE OF PRESSURE FLOOR) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW LH MLG VOLUMETRIC FUSE MOUNTING BRACKET REF DWG 601R75278 REV G, CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-41-02. COMPLIED WITH
- [SDR SWIA2025033100120](https://openairdocs.org/sdr/SWIA2025033100120.md): Mount · damaged · Jan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LH MLG PRESSURE TRANSDUCER MOUNTING ANGLE INSIDE WHEEL WELL (UNDERSIDE OF PRESSURE FLOOR) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW LH MLG PRESSURE TRANSDUCER MOUNTING ANGLE P/N 601R75262-159. REF: CRJ-200 SRM 51-42-06 AND DWG. 601R75261 REV -N. COMPLIE
- [SDR SWI2025F00412](https://openairdocs.org/sdr/SWI2025F00412.md): Skin · chafed · Jan 18, 2025 · N962SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CHAFFE ON AFT CARGO DOOR UPPER SKIN (MIDDLE ABOVE EXISTING DOUBLER) CAMP 29497077. (C-CHECK RO 03/30/2024) REMOVED AND REPLACED CHAFED DOUBLER ON THE AFT CARGO DOOR UPPER SKIN WITH NEW FABRICATED DOUBLER, PER MHIRJ REO 601R-52-31-340 REV -- DATED 2021-02-16.
- [SDR SWI2025F00411](https://openairdocs.org/sdr/SWI2025F00411.md): Fitting · gouged · Jan 18, 2025 · N962SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT UPPER AND LOWER FITTING GOUGED ON AFT CARGO DOOR CAMP 29497087. (C-CHECK RO 03/30/2024)DISCREPANCY SHOULD READ, AFT LOWER CARGO DOOR STOP FITTING AND CARGO DOOR SURROUND LOWER AFT STOP FITTING IS GOUGED. INSTALLED NEW AFT LOWER STOP FITTING ON CARGO DOOR P
- [SDR SWIA202503310118](https://openairdocs.org/sdr/SWIA202503310118.md): Fitting · gouged · Jan 18, 2025 · N962SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD UPPER AND LOWER FITTING GOUGED ON AFT CARGO DOOR CAMP 29497081. (C-CHECK RO 03/30/2024)DISCREPANCY SHOULD READ, FWD LOWER CARGO DOOR STOP FITTING AND CARGO DOOR SURROUND LOWER FWD STOP FITTING IS GOUGED. INSTALLED NEW FWD LOWER CARGO DOOR STOP FITTING IAW
- [SDR SWI2025F00406](https://openairdocs.org/sdr/SWI2025F00406.md): Handle · no test · Jan 8, 2025 · N962SW · Cndair CL6002B19 · Emergency Exits
  > DURING OPERATIONAL TEST OF THE CREW ESCAPE HATCH (EES), THE OUTER HANDLE DOESN'T OPERATE PROPERLY. (29444062) (C-CHECK RO 03/30/2024)REMOVED AND REPLACED NEW OUTER HANDLE OF THE CREW ESCAPE HATCH REF CRJ200 SRM 51-42-06 AND DWG CC670-38002 REV -E. COMPLIED WIT
- [SDR SWIA20250331106](https://openairdocs.org/sdr/SWIA20250331106.md): Skin · gouged · Jan 6, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADM# N962SW-7829 FS 640.00--FS 654.5 RH STRINGER 4-5. FOUND GOUGE 1.6" AFT OF FS 640.00 AND 1.5" ABOVE RH STRINGER 5. GOUGE IS.0019" DEEP, WIDTH.44", LENGTH.58". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USI
- [SDR SWI202402270177](https://openairdocs.org/sdr/SWI202402270177.md): A/C Pack · pressure loss · Feb 23, 2024 · N962SW · Cndair CL6002B19 · Cabin Cooling System
  > R PACK HI PRESS CAUTION AT 10000. WHEN IT FAULTED, L PACK HI TEMP CAUTION CAME ON. (FLIGHT 5291 FILED CLOSED)TROUBLESHOT PER CRJ 200 FIM 21-50-00. REMOVED AND REPLACED PRESSURE REGULATING SOV REF CRJ 200 AMM 21-51-43. OPERATIONAL TEST GOOD AT THIS TIME.PLEASE
- [SDR SWIA202402190018](https://openairdocs.org/sdr/SWIA202402190018.md): Landing Gear · warning message · Feb 18, 2024 · N962SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > ****AIRCRAFT DOWNGARDED FROM CAT 2 *****D:GEAR DISAGREE WARNING MESSAGE FOLLOWED BY NOSE DOOR OPEN WARNING MESSAGE AFTER SELECTING GEAR UP AFTER TAKEOFF. RAN EMERGENCY QRH 13-13 AND RETURNED TO AIRPORT.C:MEL 32-30-1CAT A DUE 02/19/24*** DUE TO ODI REQUIRES SM
- [SDR SWIA202266661](https://openairdocs.org/sdr/SWIA202266661.md): None · failed · Oct 25, 2022 · N962SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > NOSE DOOR AND GEAR DISAGREE RED MESSAGES DURING GEAR EXTENSION. FOLLOWED QRH WHICH WORK TO CLEAR THE MESSAGES (FLIGHT 5911 - FILED CLOSED) INTERROGATED PSEU FOR TROUBLESHOOTING OF NOSE DOOR AND GEAR DISAGREE CAUTION MESSAGES AND FOUND FAULT CODE D044 STO
- [SDR SWIA202156899](https://openairdocs.org/sdr/SWIA202156899.md): Angle · cracked · Feb 17, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CLIP CRACKED AT FS193.00 FRAME WS80.00 AT OUTBOARD FASTENER LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED CLIP AT FS193.00 FRAME WS 80.00 LH. REF CRJ 200 SRM 51-42-06 AND DWG 600-33101 REV-R
- [SDR SWIA202156897](https://openairdocs.org/sdr/SWIA202156897.md): Skin · dented · Feb 17, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENT W/GOUGE ADJACENT TO FS 295 BETWEEN STGR 24L AND 25L. (C-CHECK) RO 3/10/2021 REPAIRED FUSELAGE SKIN DENT W/GOUGE ADJACENT TO FS 295 BETWEEN STGR 24L AND 25L. REF REO 601R-53-21-3401 REV. -- DATED 2021-03-01. ALL CHECKS GOOD. COMPLIED W
- [SDR SWIA202156919](https://openairdocs.org/sdr/SWIA202156919.md): Plate · chafed · Feb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * LH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED DAMAGE ON LH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE REF CRJ200 SRM 51-12-00 SEE CONTINUATION FOR WORK PERFORMED
- [SDR SWIA202156918](https://openairdocs.org/sdr/SWIA202156918.md): Plate · chafed · Feb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * LH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED DAMAGE ON LH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE REF CRJ200 SRM 51-12-00 SEE CONTINUATION FOR WORK PERFORMED
- [SDR SWIA202156917](https://openairdocs.org/sdr/SWIA202156917.md): Plate · chafed · Feb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * RH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED CHAFE ON I/B GUIDE PLATE OF R/H I/B FLAP I/B HINGE ARM REF CRJ 200 SRM 51-12-00. PART WAS OUT OF LIMITS PER REF CRJ 200 SRM 57-40-00 FIG 101. REMOVED AND REPLA
- [SDR SWIA202156916](https://openairdocs.org/sdr/SWIA202156916.md): Plate · chafed · Feb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * RH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED CHAFE ON R/H I/B FLAP O/B HINGE ARM I/B GUIDE PLATE REF CRJ 200 SRM 51-12-00. PART WAS OUT OF LIMITS PER REF CRJ 200 SRM 57-40-00 FIG 101. REMOVED AND REPLACE
- [SDR SWIA202156898](https://openairdocs.org/sdr/SWIA202156898.md): Plate · cracked · Feb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * LH INBOARD FLAP INBOARD HINGE ARM OUTBOARD GUIDE PLATE CRACKED. (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW 1EA. GUIDE PLATE, 4EA NUTPLATES, 10EA SOLID RIVETS AND 8EA BLIND NUTPLATE RIVETS, REF: CRJ 200, SRM 51-45-00, SRM 51-42-06, SRM 51-42-15
- [SDR SWIA202156896](https://openairdocs.org/sdr/SWIA202156896.md): Hinge Arm · gouged · Feb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * RH INBOARD FLAP INBOARD HINGE ARM GOUGED AT ATTACH LUG COMMON TO HINGE BOX. (C-CHECK) RO 3/10/2021 BLENDED GOUGE ON R/H I/B FLAP I/B HINGE ARM ATTACH LUG COMMON TO HINGE BOX REF CRJ 200 SRM 51-12-00. PART IS WITHIN LIMTS PER MHI-RJ REO 601R-57-54-319, R
- [SDR SWIA202156895](https://openairdocs.org/sdr/SWIA202156895.md): Housing · damaged · Feb 12, 2021 · N962SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > WHILE REMOVING CARGO DOOR HANDLE HOUSING, MISDRILLED ONE FASTNER LOCATION INTO THE SKIN AND INNER DOUBLER. (C-CHECK) RO 3/10/2021 REPLACED CARGO DOOR HANDLE HOUSING DOUBLER AND REPAIRED THE FASTENERS HOLE REF REO 601R-52-31-341 REV -- DATED 2021-03-05, CR
- [SDR SWIA202156912](https://openairdocs.org/sdr/SWIA202156912.md): Floor Support · corroded · Feb 10, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * FLOOR SILL FWD OF THE SERVICE DOOR CORRODED AT APROX. F.S.331.00. (C-CHECK) RO 3/10/2021 FLOOR SILL FWD OF SERVICE DOOR REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, 51-42-13, 51-45-00
- [SDR SWIA202156915](https://openairdocs.org/sdr/SWIA202156915.md): Coaming · chafed · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > * AFT CARGO DOOR COMING CHAFED IN MULTIPLE SPOTS. (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW LOWER CARGO DOOR COAMING, REF: CRJ 200, SRM 51-41-02 / PERFORMED PRESSURE CHECK ON CARGO DOOR SEAL COAMING. REF CRJ200 AMM 21-32-00-863-801. CHECK FAILED DU
- [SDR SWIA202156911](https://openairdocs.org/sdr/SWIA202156911.md): Seat Track · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * FS 559+80 TO FS 621.0 RBL 27 HAS SEAT TRACK CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED FS 559+80 TO FS 621.0 RBL 27 P/N 601R386631-3, P/N 601R386631-9 AND P/N 601R38779-9 AT FS 559+80 TO FS 621.0 TOOL USED: TUC5657 DUE 31-MAR-21. REF. CR
- [SDR SWIA202156910](https://openairdocs.org/sdr/SWIA202156910.md): Seat Track · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * BETWEEN FS 559+80 AND FS 559+96 RBL 9 AND LBL 9 TWO SMALL SECTIONS OF SEAT TRACK HAVE CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW CARGO TIE DOWN SEAT TRACK SECTION FROM FS 559+80 TO FS617 ON RBL 9 AND LBL 9 PART # 601R386631-3, 601R3866
- [SDR SWIA202156909](https://openairdocs.org/sdr/SWIA202156909.md): Seat Track · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * LBL 27 FS 559+80 TO FS 617.0 SEAT TRACK HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED CORRODED SEAT TRACKS, AND INSTALLED NEW SEAT TRACKS (P/N'S: 601R386631-3, 601R386631-9, AND 601R38779-9) WITH NEW HARDWARE ON LBL27 FROM FS559 +80 TO FS617.00 REF CRJ20
- [SDR SWIA202156908](https://openairdocs.org/sdr/SWIA202156908.md): Bolt · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Spoilers
  > * R/H SPOILERON ALL ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED R/H SPOILERON ALL ATTACHING HARDWARE REF CRJ 200 AMM 27-64-01-400-801 OPS CHECK GOOD
- [SDR SWIA202156907](https://openairdocs.org/sdr/SWIA202156907.md): Bolt · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Spoilers
  > * R/H FLIGHT SPOILER ALL ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW R/H FLIGHT SPOILER ALL ATTACHING HARDWARE REF CRJ 200 AMM 27-64-05-400-801. OPS CHECK GOOD
- [SDR SWIA202156906](https://openairdocs.org/sdr/SWIA202156906.md): Bolt · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Spoilers
  > * L/H FLIGHT SPOILER ALL ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW L/H FLIGHT SPOILER ATTACHING HARDWAR. REF CRJ 200 AMM 27-64-05-400-801. OPS CHECK GOOD SEE CONTINUE CARD FOR DETAILS
- [SDR SWIA202156905](https://openairdocs.org/sdr/SWIA202156905.md): Bolt · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Spoilers
  > * L/H SPOILERON ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW L/H SPOILERON ATTACHING HARDWARE REF CRJ 200 AMM 27-64-01-400-801. OPS CHECK GOOD
- [SDR SWIA202156894](https://openairdocs.org/sdr/SWIA202156894.md): Pressure Deck · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * LH PRESSURE FLOOR SILL PANEL FROM F.S. 409+128 TO F.S.559.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED).BLENDED OUT 11 SPOT OF CORROSION ON LH PRESS FLOOR SILL PANEL BETWEEN FS409-128 AND FS559 PER REF CRJ 200 SRM 51-21-06. FOUND 4 OF THEM OUT OF LIMITS DUE TO
- [SDR SWIA202156893](https://openairdocs.org/sdr/SWIA202156893.md): Pressure Deck · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * RH PRESSURE FLOOR SILL PANEL FROM F.S. 409+128 TO F.S.559.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK) RO 3/10/2021 REMOVED CORROSION FROM RH PRESSURE FLOOR SILL PANEL FROM F.S. 409+128 TO F.S.559.00. REF REO 601R-53-41-666 REV. -C DATED 2012-
- [SDR SWIA202156892](https://openairdocs.org/sdr/SWIA202156892.md): Floorbeam · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > * FS 559+80 RBL 9 TO RBL 27 TOP CAP HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW CAP PN 601R32215-43. REF. CRJ200 SRM 51-42-06 AND DWG 601R32215 REV. M. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202156891](https://openairdocs.org/sdr/SWIA202156891.md): Support · damaged · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * LH SILL AT FS 559.0+16 TO FS 559.0+32 HAS A MISDRILLED HOLE (C-CHECK) RO 3/10/2021 REPAIRED LH SILL AT FS 559.0+16 TO FS 559.0+32. REF REO 601R-53-51-560 REV. -- DATED 2021-02-12. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA202156890](https://openairdocs.org/sdr/SWIA202156890.md): Strap · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * LH TOP STRAP @ FS 559.0 RBL 27 TO SILL HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED CORROSION ON L/H STOP STAP AT FS559 LBL27 TO FLOOR SILL REF CRJ 200 SRM 51-21-06, PART WAS OUT OF LIMITS PER 53-00-00, REMOVED AND REPLACED STRAP REF CRJ 200 SRM 51-42-0
- [SDR SWIA202156889](https://openairdocs.org/sdr/SWIA202156889.md): Strap · corroded · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RH TOP STRAP @ FS 559.0 RBL 27 TO SILL HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED CORROSION ON R/H STOP STAP AT FS559 RBL27 TO FLOOR SILL REF CRJ 200 SRM 51-21-06, REMOVED AND REPLACED STRAP REF CRJ 200 SRM 51-42-06, & BOMBARDIER DWG # 601R31025, REV
- [SDR SWIA202156888](https://openairdocs.org/sdr/SWIA202156888.md): Lintel · cracked · Feb 9, 2021 · N962SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * PAX DOOR UPPER LINTEL CRACKED AT F.S.379.00 STR.3L. (C-CHECK) RO 3/10/2021 REPAIRED PAX DOOR UPPER LINTEL AT F.S.379.00 STR.3L. REF DRAWING 601R31016 REV D AND CRJ200 SRM 53-00-03. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA202156904](https://openairdocs.org/sdr/SWIA202156904.md): Bolt · corroded · Feb 8, 2021 · N962SW · Cndair CL6002B19 · Elevator Structure
  > * LH ELEVATOR HINGES ATTACH AND BONDING HARDWARE HAS CORROSION ( ALL THREE HINGES) (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW BONDING JUMPER HARDWARE 33EA NUTS, 8EA SCREWS, 19 WASHERS/LOCKWASHERS REF. CRJ-200 AMM 51-80-00-400-803. / PERFORMED BONDIN
- [SDR SWIA202156903](https://openairdocs.org/sdr/SWIA202156903.md): Bolt · corroded · Feb 8, 2021 · N962SW · Cndair CL6002B19 · Elevator Structure
  > * RH ELEVATOR HINGES ATTACH AND BONDING HARDWARE HAS CORROSION ( ALL THREE HINGES) (C-CHECK) RO 3/10/2021 ORDERED AND RECEIVED 10EA NUTS, 8EA WASHERS 4EA SCREWS 4EA LOCK WASHERS FOR RH ELEVATOR HINGES SEE TRANS# 22107719 JOB 2785990 OP 517 FOR INSTALLATIO
- [SDR SWIA202156887](https://openairdocs.org/sdr/SWIA202156887.md): Angle · cracked · Feb 8, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RH FS 625.0 UPPER CLIP CRACKED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED FS 625.0 UPPER CLIP AT STR 14 REF CRJ-200-SRM 51-42-21.AND REO 601R-53-61-422 REV NC DATED 2001-08-23. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Next page: https://openairdocs.org/aircraft/N962SW/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 = 'N962SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N962SW/reports

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