# Service difficulty reports: N954SW

A list on [N954SW](https://openairdocs.org/aircraft/N954SW.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 5 · 250 reports

- [SDR SWIA20250613521](https://openairdocs.org/sdr/SWIA20250613521.md): Plate · cracked · May 21, 2025 · N954SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR RESTRAINT NETTING CENTER FITTING PLATE CRACKED. (FILED CLOSED)REMOVED AND REPLACED CARGO DOOR RESTRATINT NETTING CENTER FITTING PLATE WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337. REF CP
- [SDR SWI2025F00650](https://openairdocs.org/sdr/SWI2025F00650.md): Plate · cracked · May 21, 2025 · N954SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR RESTRAINT NETTING CENTER FITTING PLATE CRACKED. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20250613509](https://openairdocs.org/sdr/SWIA20250613509.md): Frame Angle · cracked · May 9, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME ANGLE @ FS 605.00 NEAR STR17L - STR18L NEAR WL 73.00 THAT CONNECTS THE FRAME SECTOR TO THE CARGO BAY DOOR SILL PLATE IS CRACKED AND REQUIRES REPLACEMENT. (C-CHECK RO 06/12/2025)REMOVED AND REPLACED FRAME ANGLE AT FS 605.00 NEAR STR17L - STR18L NEAR WL 7
- [SDR SWIA20250613508](https://openairdocs.org/sdr/SWIA20250613508.md): Frame · cracked · May 8, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 605.00 IS CRACKED IN TWO LOCATIONS(ANGLE AND RADIUS) ON STR18L IN-BETWEEN STR17L ABOVE THE CURRENT REPAIR FOR REO 601R-53-61-8326. (FILED CLOSED)REMOVED AND REPLACED FRAME SECTOR FS 605.00 BETWEEN STR17L -STR20L WITH REFERENCE TO SRM 51-42-06 AND REO
- [SDR SWI2025F00720](https://openairdocs.org/sdr/SWI2025F00720.md): Tie Down · no discrepancy · Apr 28, 2025 · N954SW · Cndair CL6002B19 · Standard Practices/Structures
  > CENTER CARGO NET TIE DOWN RIGN ASSEMBLY AND ASSOACIATED INBOARD AND OUTBOARD ANGLE (REFERENCE SRM 53-61-43 ITEMS 6 & 8) REMOVED TO F.O.M. WITH REFERENCE TO SRM 51-42-21. (C-CHECK RO 06/12/2025)REINSTALLED THE CENTER CARGO NET TIE DOWN RING ASSEMBLY AND ASSOAC
- [SDR SWIA20250612428](https://openairdocs.org/sdr/SWIA20250612428.md): Frame · cracked · Apr 28, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR FS605.00 CRACKED BETWEEN STR18L - STR19L. (FILED CLOSED)REF CP 30108469 FOR FRAME SECTOR FS 605 REPLACEMENT FROM STR17L - STR21L AND ALTERNATE FASTENER REO.
- [SDR SWI2025F00596](https://openairdocs.org/sdr/SWI2025F00596.md): Frame · cracked · Apr 28, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR FS605.00 CRACKED BETWEEN STR18L - STR19L. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20250613419](https://openairdocs.org/sdr/SWIA20250613419.md): Skin · corroded · Apr 19, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF THE APU AFT SHIELD ASSEMBLY, 8 SPOTS OF PITTING CORROSION/CHAFFING DAMAGE WERE FOUND ON THE EXTERNAL FUSELAGE SKIN AT THE MOUNTING POINTS AT VARIOUS LOCATIONS FROM FS 682.00 +10 €“ FS 700.00 IN BETWEEN STR12R-STR15R. (C-CHECK RO 06/12/2025)UPO
- [SDR SWIA20250613413](https://openairdocs.org/sdr/SWIA20250613413.md): Retainer · bent · Apr 13, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Structure
  > MAIN CABIN DOOR BOTTOM SEAL RETAINER BENT. (C-CHECK RO 06/12/2025)REMOVED AND REPLACED MAIN CABIN DOOR BOTTOM SEAL RETAINER WITH REFERENCE TO REO 601R-52-11-915 REV "--" DATED JAN 04 2006 AND SRM 51-42-13. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED
- [SDR SWI2025F00730](https://openairdocs.org/sdr/SWI2025F00730.md): Bearing · failed · Apr 12, 2025 · N954SW · Cndair CL6002B19 · Elevator Structure
  > L/H ELEVATOR REQUIRES REPLACEMENT DUE TO FAILED BEARING BACKLASH CHECK. (C-CHECK RO 06/12/2025)REMOVED L/H ELEVATOR IN REFERENCE WITH AMM 27-34-01. REMOVED AND REPLACED ALL L/H ELEVATOR HINGE BUSHINGS ON THE HORIZONTAL STABILIZER IN REFERENCE WITH AMM 20-26-
- [SDR SWIA20250613412](https://openairdocs.org/sdr/SWIA20250613412.md): Frame · corroded · Apr 12, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS589.00 BETWEEN STRINGERS 19L AND 18R HAS MISSING PAINT AND SURFACE CORROSION ON FLANGE/WEB. (C-CHECK RO 06/12/2025)COMPLIED WITH REO 601R-53-61-8328 DATED: 2025-05-06 REV:A REPAIR FOR CORROSION DAMAGE TO FRAME FS589.00 BTW STR18R-19R. COMPLIED WITH TASK CAR
- [SDR SWIA20250613411](https://openairdocs.org/sdr/SWIA20250613411.md): Pressure Deck · corroded · Apr 11, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RH PRESSURE FLOOR HAS NUMEROUS AREAS OF CORROSION, BETWEEN FS409.00 +128 AND FS559.00. (FILED CLOSED)BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 - RBL 42.00 AND BETWEEN FS409.00 +128 AND FS559.00 WITH REFERENCE TO SRM 51-21-06. PE
- [SDR SWI2025F00719](https://openairdocs.org/sdr/SWI2025F00719.md): Pressure Deck · corroded · Apr 11, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LH PRESSURE FLOOR BETWEEN FS409+128 AND FS559.00 HAS NUMEROUS AREAS OF CORROSION. (FILED CLOSED)BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL ASSY APPROX LBL 36.00 - LBL 42.00 AND BETWEEN FS409.00 +128 AND FS559.00 WITH REFERENCE TO SRM 51-21-06. PERFORM
- [SDR SWI2025F00445](https://openairdocs.org/sdr/SWI2025F00445.md): Pressure Deck · corroded · Apr 11, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LH PRESSURE FLOOR BETWEEN FS409+128 AND FS559.00 HAS NUMEROUS AREAS OF CORROSION. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025041400011](https://openairdocs.org/sdr/SWIA2025041400011.md): Pressure Deck · corroded · Apr 11, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RH PRESSURE FLOOR HAS NUMEROUS AREAS OF CORROSION, BETWEEN FS409.00 +128 AND FS559.00. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20250613409](https://openairdocs.org/sdr/SWIA20250613409.md): Skin · damaged · Apr 9, 2025 · N954SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 1 OFF ELONGATED / DAMAGED ANTENNA INSTALLATION FASTENER HOLE MEASURING 0.281" DIAMETER AT APPROX. FS 409 + 12 AND STR 27 IN FOOTPRINT OF VHF2 ANTENNA. (C-CHECK RO 06/12/2025)COMPLIED WITH REO 601R-53-31-1329 REV "--" DATED 2025-05-22 TEMPORARY REPAIR FOR ELON
- [SDR SWIA20250613402](https://openairdocs.org/sdr/SWIA20250613402.md): Skin · damaged · Apr 2, 2025 · N954SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WINGLET FWD, IB SKIN FOUND TO HAVE PREVIOUSLY ELONGATED AND DENTED HOLE (C-CHECK RO 06/12/2025)REMOVED AND REPLACED LH WINGLET FWD IB SKIN WITH REFERENCE TO SRM 51-42-13, SRM 51-42-22 AND REO 601R-57-31-1450 REV "--" DATED 2025-04-10. COMPLIED WITH TASK
- [SDR SWIA20250613330](https://openairdocs.org/sdr/SWIA20250613330.md): Intercostal · cracked · Mar 30, 2025 · N954SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ON LH Z-MEMBER RUNNING BETWEEN LH STGR 14A AND VERTICAL STIFFENER @ LBL 36.20, FS 625.30 (SRM 53-61-101 FIG. 1 ITEM #51) (C-CHECK RO 06/12/2025)REMOVED AND REPLACED INTERCOSTAL ON LH Z-MEMBER RUNNING BETWEEN LH STGR 14A AND VERTICAL STIFF
- [SDR SWI2025F00728](https://openairdocs.org/sdr/SWI2025F00728.md): Intercostal · cracked · Mar 30, 2025 · N954SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUSPECTED CRACK IN INTERCOSTAL AFT OF REAR PRESSURE BULKHEAD FRAME, WHERE IT ATTACHES TO FUSELAGE SKIN @ STGR 15A BETWEEN FS621.00 AND FS625.30 (SRM 53-61-17-00 FIG. 1, ITEM 48) (C-CHECK RO 06/12/2025)COMPLIED WITH REO 601R-53-61-8333 DATED:2025-05-07 REV--.
- [SDR SWIA20250613328](https://openairdocs.org/sdr/SWIA20250613328.md): Access Panel · corroded · Mar 28, 2025 · N954SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING FUEL CELL ACCESS PANEL (510AB) LANDING HAS TWO SPOTS OF MINOR CORROSION AT THE 12 O'CLOCK & 3 O'CLOCK POSITION, MEASURING APPROX 2.75 INCHES AND 3 INCHES RESPECTIVELY. (C-CHECK RO 06/12/2025)REPAIRED LH WING FUEL CELL ACCESS PANEL LANDING(510AB) LAND
- [SDR SWI2025F00727](https://openairdocs.org/sdr/SWI2025F00727.md): Seat · damaged · Mar 3, 2025 · N954SW · Cndair CL6002B19 · Flight Compartment Equipment
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA81722-601R-53-11-1093 N945SW MXCODEID65337-PR - UNABLE TO MOVE CAPTAIN SEAT FULLY FORWARD. COMPLIED WITH TEMPORARY DISPOSITION FOR LOOSE OR DAMAGED ALIGNMENT RIVETS IN REFERENCE TO REO 601R-53-11-1093 REV-B DATED 201
- [SDR SWIA20250613303](https://openairdocs.org/sdr/SWIA20250613303.md): Skin · punctured · Mar 3, 2025 · N954SW · Cndair CL6002B19 · Wing, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA94069-REO 601R-57-31-1443 MXCODEID104781-PR - APPEARS TO BE A SMALL PUNCTURE ON TOP OF LEFT WINGLET.COMPLIED WITH REO 601R57-31-1443, COVERED DISCREPANT AREA WITH SPEED TAPE PER REO, PERMANENT REPAIR WITHIN 1600 FLIGHT
- [SDR SWIA202410221028](https://openairdocs.org/sdr/SWIA202410221028.md): Retainer · cracked · Oct 21, 2024 · N954SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR BOTTOM SEAL RETAINER CRACKED. (FILED CLOSED)REMOVED AND REPLACED PASSENGER DOOR BOTTOM SEAL RETAINER WITH REFERENCE TO SRM 51-42-13 AND REO 601R-52-11-915 REV "--" DATED JAN 04 2006. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. REF
- [SDR SWIA202410220001](https://openairdocs.org/sdr/SWIA202410220001.md): Retainer · cracked · Oct 21, 2024 · N954SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVING PASSENGER DOOR SEAL FOUND LWR AFT RETAINER SEAL CORNER TO BE CRACKED. (FILED CLOSED)REMOVED AND REPLACED PASSENGER DOOR LOWER AFT SEAL RETAINER WITH REFERENCE TO SRM 51-42-06, SRM 51-42-13 AND REO 601R-52-11-915 REV "--" DATED JAN 04 2006. COMP
- [SDR SWIA2024050100428](https://openairdocs.org/sdr/SWIA2024050100428.md): Window · cracked · Apr 28, 2024 · N954SW · Cndair CL6002B19 · Flight Compartment Windows
  > WHILE SITTING ON THE GROUND THE FOS SIDE WINDOW CRACKED THROUGH OUT THE ENTIRE AREA. (FLIGHT 5641 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28159166 WITH THE FOLLOWING CORRECTIVE ACTION: "RIGHJT SIDE WINDOW REMOVED AND REPLACED IAW TASK CARD 5
- [SDR SWIA202305300026](https://openairdocs.org/sdr/SWIA202305300026.md): Unknown · unknown · May 26, 2023 · N954SW · Cndair CL6002B19 · Landing Gear System
  > GEAR DISAGREE WITH GEAR LEVER SELECTED UP. NOSE GEAR STAYED DOWN (FLT 5365 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26676624 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 26676947 FOR INTERROGATION OF THE PSEU AND RESULTS OF THE GEAR DISAGREE
- [SDR SWIA202265277](https://openairdocs.org/sdr/SWIA202265277.md): None · failed · Apr 6, 2022 · N954SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > ENROUTE FROM SFO TO ACV RECEIVED NUMEROUS GEARDISAGREE WARNING MESSAGES, WHICH PERSISTED. RAN QRH. WARNING EXTINGUISHED AFTER GEAR WAS MANUALLY DEPLOYED PER QRH. THE PREVIOUS ISSUE WITH THE ANTI SKID OUTBOARD CAUTION MESSAGE ALSO RETURN WHILE PERFORMING QRH.
- [SDR SWIA202161554](https://openairdocs.org/sdr/SWIA202161554.md): None · cracked · Sep 27, 2021 · N954SW · Cndair CL6002B19 · Water and Waste System
  > LAV POTABLE WATER TANK AFT ATTACHMENT BRACKET CRACKED. (C-CHECK RO 10/4/2021) REMOVED AND REPLACED LAV POTABLE WATER TANK AFT ATTACHMENT BRACKET REF CRJ200 SRM 51-42-06 AND DWG 601R43101 REV-R. COMPLIED WITH ATTACHED TASK 51-900-1003-SKY
- [SDR SWIA202161553](https://openairdocs.org/sdr/SWIA202161553.md): None · cracked · Sep 27, 2021 · N954SW · Cndair CL6002B19 · Water and Waste System
  > LAV POTABLE WATER TANK FORWARD ATTACHMENT BRACKET CRACKED. (C-CHECK RO 10/4/2021) REMOVED AND REPLACED LAV POTABLE WATER TANK FWD ATTACHMENT BRACKET REF CRJ200 SRM 51-42-06 AND DWG 601R43101 REV-N. COMPLIED WITH ATTACHED TASK 51-900-1003-SKY
- [SDR SWIA202161552](https://openairdocs.org/sdr/SWIA202161552.md): None · cracked · Aug 30, 2021 · N954SW · Cndair CL6002B19 · Fuselage Main, Frame
  > ATTACHING BRACKET FOR PANEL 344BB HAS A CRACK. (C-CHECK RO 10/4/2021) REMOVED AND REPLACED 1EA NEW FABRICATED ATTACHING BRACKET P/N 600-24054-116 PO# T55917 FOR PANEL 344BB CRJ-200 REO 601R-55-21-555 REV-- DATE 2021-09-04 AND DWG 600-24054 REV-N / COMPL
- [SDR SWIA202161551](https://openairdocs.org/sdr/SWIA202161551.md): None · grooved · Aug 13, 2021 · N954SW · Cndair CL6002B19 · Doors
  > PASSENGER DOOR FORWARD AND AFT PULL IN LEVER CAMS ON FUSELAGE GROOVED. (C-CHECK RO 10/4/2021) REMOVED AND REPLACED PASSENGER DOOR FORWARD AND AFT PULL IN LEVER CAMS ON FUSELAGE GROOVED P/N 600-31688-17 AND P/N 600-31688-18. REF. CRJ 200 SRM 51-42-21 AN
- [SDR SWIA202161550](https://openairdocs.org/sdr/SWIA202161550.md): None · chafed · Aug 13, 2021 · N954SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > *LH OUTBOARD FLAP CENTER HINGE ARM €“ INBOARD GUIDE PLATE CHAFED. (C-CHECK RO 10/4/2021) REPAIR CHAFED DAMAGE ON LH OUTBOARD FLAP CENTER HINGE ARM €“ INBOARD GUIDE PLATE REF REO 601R-57-54-336 REV -- DATED 2021-08-28.ORIGINAL THICKNESS.050", REMAII
- [SDR SWIA202161549](https://openairdocs.org/sdr/SWIA202161549.md): None · corroded · Aug 13, 2021 · N954SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON LBL 27 FLOOR BEAM END FITTING BETWEEN FS 605 AND FS 621 ON BOTH INB`D AND OUTB`D FLANGES (C-CHECK RO 10/4/2021) LBL 27 FLOOR BEAM END FITTING BETWEEN FS605 AND FS621 REPAIRED REF MHIRJ REO 601R-53-61-7699 REV A DATED 2021-09-09. / COM
- [SDR SWIA202161548](https://openairdocs.org/sdr/SWIA202161548.md): None · gouged · Aug 10, 2021 · N954SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * THE FUSELAGE-TO-WING ATTACHMENT FITTING AT FS 513 AND RBL 13 HAS GOUGES ON ITS AFT FLANGE FACE. (C-CHECK RO 10/4/2021) BLENDED NOTED DAMAGE ON FUSELAGE-TO-WING ATTACHMENT FITTING AT FS 513 AND RBL 13 AFT FLANGE FACE TO A SMOOTH FINISH, NDT INSPECTED N
- [SDR SWIA202161603](https://openairdocs.org/sdr/SWIA202161603.md): None · corroded · Aug 9, 2021 · N954SW · Cndair CL6002B19 · Flight Control System
  > FOUND CORROSION ON THE RH AILERON OTBD PCU AT LINK ATTACHMENT POINT (C-CHECK RO 10/4/2021) REMOVED AND REPLACED WITH A NEW PART. RH AILERON OUTBOARD PCU. REF. CRJ200 AMM 27-14-01-000-801 AND CRJ200 AMM 27-14-01-400-801 SEE CONTINUE CARD FOR FURTHER DE
- [SDR SWIA202161602](https://openairdocs.org/sdr/SWIA202161602.md): None · corroded · Aug 9, 2021 · N954SW · Cndair CL6002B19 · Flight Control System
  > FOUND CORROSION ON THE RH AILERON INBD PCU AT LINK ATTACHMENT POINT (C-CHECK RO 10/4/2021) REMOVED AND REPLACED RH AIL/INBD PCU W/NEW PARTS IAW CRJ200 AMM 27-14-01-400-801. COMPLIED WITH TASK CARD 27-900-1002-SKY.
- [SDR SWIA202161601](https://openairdocs.org/sdr/SWIA202161601.md): None · corroded · Aug 9, 2021 · N954SW · Cndair CL6002B19 · Flight Control System
  > FOUND CORROSION ON THE LH AILERON OTBD PCU AT LINK ATTACHMENT POINT (C-CHECK RO 10/4/2021) REMOVED AND REPLACED LH OUTBOARD AILERON PCU WITH SERVICABLE PART AS PER CRJ 200 AMM 27-14-01-000-801 AND CRJ 200 AMM 27-14-01-400-801 CALIBRATED TOOL USED TUC48
- [SDR SWIA202161600](https://openairdocs.org/sdr/SWIA202161600.md): None · corroded · Aug 9, 2021 · N954SW · Cndair CL6002B19 · Flight Control System
  > FOUND CORROSION ON THE LH AILERON INBD PCU AT LINK ATTACHMENT POINT (C-CHECK RO 10/4/2021) REMOVED AND REPLACED WITH A NEW PART THE LH INBOARD PCU ASSEMBLY. IAW CRJ200 AMM 27-14-01-000-801 AND THE CRJ200 AMM 27-14-01-400-801 SEE CONTINUE CARD FOR FURTH
- [SDR SWIA202161547](https://openairdocs.org/sdr/SWIA202161547.md): None · worn · Aug 9, 2021 · N954SW · Cndair CL6002B19 · Doors
  > PAX DOOR LATCH MECHANISM UPPER STOP FITTING CONTACT SURFACE FOUND WORN BEYOND REPAIR. (C-CHECK RO 10/4/2021) INSTALLED NEW REPLACEMENT UPPER STOP FITTING P/N 601R38926-3 AT PAX DOOR LATCH-LOCK MECHANISM PER CRJ200 SRM 51-41-02 REF. CRJ200 AMM TASK 52-
- [SDR SWIA202161599](https://openairdocs.org/sdr/SWIA202161599.md): None · corroded · Aug 8, 2021 · N954SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * THE RH WING BATT RIB INBOARD ANGLE DOUBLER AT WS 53.60 HAS CORROSION AROUND THE CANNON PLUG CONNECTORS. (REFER TO CRJ 200 SRM 57-21-12 FIGURE 6 ITEM 9) (C-CHECK RO 10/4/2021) RH WING BATT RIB INBOARD ANGLE DOUBLER AT WS53.60 CORROSION AROUND CANNON PL
- [SDR SWIA202161598](https://openairdocs.org/sdr/SWIA202161598.md): None · corroded · Aug 8, 2021 · N954SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * THE LH WING BATT RIB INBOARD ANGLE DOUBLER AT WS 53.60 HAS CORROSION AROUND THE CANNON PLUG CONNECTORS. (REFER TO CRJ 200 SRM 57-21-12 FIGURE 6 ITEM 9) (C-CHECK RO 10/4/2021) LH WING BATT RIB INBOARD ANGLE DOUBLER AT WS53.60 CORROSION AROUND CANNON PL
- [SDR SWIA202161578](https://openairdocs.org/sdr/SWIA202161578.md): None · cracked · Aug 8, 2021 · N954SW · Cndair CL6002B19 · Wing Structure
  > * THE RH WING BATT RIB CAP AT WS 48.30 IS CRACKED. (C-CHECK RO 10/4/2021) REMOVED AND INSTALLED NEW BATT RIB CAP AT RH WING, WS 48.30. REF CRJ-200 SRM 51-42-21 AND DWG 601R10204 REV -J. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH ATTACHED TASK 51-900-1
- [SDR SWIA202161577](https://openairdocs.org/sdr/SWIA202161577.md): None · cracked · Aug 8, 2021 · N954SW · Cndair CL6002B19 · Wing Structure
  > * THE LH WING BATT RIB CAP AT WS 48.30 IS CRACKED. (C-CHECK RO 10/4/2021) REMOVED AND REPLACED THE LH, CRACKED BATT RIB CAP AT WS 48.30 WITH A NEW CAP (P/N 600-10389-1) REF CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-40-11 AND DWG# 601R10204 REV-J. COMPLIED WI
- [SDR SWIA202161576](https://openairdocs.org/sdr/SWIA202161576.md): None · cracked · Aug 8, 2021 · N954SW · Cndair CL6002B19 · Fuselage Main, Keel
  > * IN THE CABIN, FUSELAGE STRINGER 3L IS CRACKED JUST FWD OF FS 379 WHERE IT ATTACHES TO THE PAX DOOR'S UPPER SILL FITTING. (C-CHECK RO 10/4/2021) PERFORMED SPLICE REPAIR OF STR 3L AT FS379. WET INSTALLED ALL REPAIR PARTS REF CRJ200 SRM 53-00-03 PG204. N
- [SDR SWIA202161546](https://openairdocs.org/sdr/SWIA202161546.md): None · gouged · Aug 8, 2021 · N954SW · Cndair CL6002B19 · Fuselage Structure (General)
  > * L/H WING TO FUSELAGE ATTACH FITTING AT FS513.0, FUSELAGE SIDE, HAS GOUGES IN THE AFT LUG, OUTBOARD SIDE, MARKED. (C-CHECK RO 10/4/2021) BLENDED NOTED DAMAGE ON L/H WING TO FUSELAGE ATTACH FITTING AT FS513.0, FUSELAGE SIDE TO A SMOOTH FINISH, NDT INSP
- [SDR SWIA202161597](https://openairdocs.org/sdr/SWIA202161597.md): None · corroded · Aug 7, 2021 · N954SW · Cndair CL6002B19 · Doors
  > *PASSENGER DOOR SURROUND: AFT HANDRAIL €ŒCUP€? ASSEMBLY IS CORRODED. (MARKED) (C-CHECK RO 10/4/2021) REMOVED CORROSION ON THE PAX DOOR SILL AFT HANDRAIL CUP REF CRJ 200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS. REPLACED THE FWD PAX DOOR SILL HANDRAIL CU
- [SDR SWIA202161596](https://openairdocs.org/sdr/SWIA202161596.md): None · corroded · Aug 7, 2021 · N954SW · Cndair CL6002B19 · Doors
  > *PASSENGER DOOR SURROUND: FS310, ANGLE/BRACKET REINFORCING THE ANCHOR FITTING IS CRACKED. (MARKED) (C-CHECK RO 10/4/2021) INSTALLED NEW PASSENGER DOOR SURROUND: FS310, ANGLE/BRACKET REF CRJ200 AMM 52-11-17-400-802. NO DEFECTS NOTED, TORQUE TUC4822 DUE
- [SDR SWIA202161595](https://openairdocs.org/sdr/SWIA202161595.md): None · corroded · Aug 7, 2021 · N954SW · Cndair CL6002B19 · Doors
  > *PASSENGER DOOR SURROUND: FS310 SERRATED PLATE UNDER THE FWD ANCHOR FITTING HAS CORROSION IN THE UPPER FORWARD EDGE, RUNNING UNDER THE REINFORCEMENT ANGLE/BRACKET. (MARKED) (C-CHECK RO 10/4/2021) INSTALLED NEW PASSENGER DOOR SURROUND FS310 SERRATED PLAT
- [SDR SWIA202161585](https://openairdocs.org/sdr/SWIA202161585.md): None · chafed · Aug 7, 2021 · N954SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LH SIDE SEAT TRACK HAS CHAFING BETWEEN FS513 AND FS529. (C-CHECK RO 10/4/2021) BLENDED OUT GOUGED AT LH SIDE SEAT TRACK BETWEEN FS513 AND FS529 REF CRJ 200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FABRICATED SEAT TRACK REF CR
- [SDR SWIA202161584](https://openairdocs.org/sdr/SWIA202161584.md): None · chafed · Aug 7, 2021 · N954SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > *LH SIDE SEAT TRACK HAS CHAFING BETWEEN FS424 AND FS439. (C-CHECK RO 10/4/2021) BLENDED OUT GOUGED AT LH SIDE SEAT TRACK BETWEEN FS424 AND FS439 REF CRJ 200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FABRICATED SEAT TRACK REF CR

Next page: https://openairdocs.org/aircraft/N954SW/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 = 'N954SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N954SW/reports

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