# Service difficulty reports: N957SW

A list on [N957SW](https://openairdocs.org/aircraft/N957SW.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 6 · 264 reports

- [SDR SWIA2026091777216](https://openairdocs.org/sdr/SWIA2026091777216.md): Pressure Panel · scratched · Sep 17, 2026 · N957SW · Cndair CL6002B19 · Fuselage Main, Structure
  > TRANSFER FROM EAML 1993541 TRANSFERRED FROM CAMP 33010415 IDENTIFIED A GOUGE ON LT PRESSURE FLOOR STRUCTURE PANEL AT FS549 APPROXIMATELY 12 X 132 X 003 FLIGHT 1. BLENDED SURFACE SCRATCH ON THE PAINTED LH PRESSURE FLOOR SILL STRUCTURE PANEL AT FS549 IAW SRM 5
- [SDR SWIA20241027](https://openairdocs.org/sdr/SWIA20241027.md): Skin · gouged · Oct 27, 2024 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1458910: IN REFERENCE TO EAML# 1458203, 1458228. DAMAGE DESCRIPTION AFTER INSPECTION.MULTIPLE GOUGES/NICKS (MAXIMUM OF 100-OFF LOCATIONS, REF)AND DENTS (9-OFF LOCATIONS, REF) TO FUSELAGE SKIN (DWG: 601R35005, 0.058€? +/-0.002€? THK PAD UP
- [SDR SWI2024F00017](https://openairdocs.org/sdr/SWI2024F00017.md): Floor Support · corroded · Dec 20, 2023 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00 +128 TO F.S. 559.00. (C-CHECK RO 1/22/2024) REMOVED CORROSION FROM LH FLOOR SILL FROM F.S. 409.00 +128 TO F.S. 559.00. NDT INSPECTED NO DEFECTS NOTED, APPLIED FINISHES, FOUND TO BE STRUCTURALL
- [SDR SWIA2024012320](https://openairdocs.org/sdr/SWIA2024012320.md): Hinge · gouged · Dec 20, 2023 · N957SW · Cndair CL6002B19 · Ailerons
  > LH AILERON, #1 HINGE, INBD BUSHING BORE IS GOUGED. (C-CHECK RO 1/22/2024) REPAIRED INBD BUSHING BORE AT LH AILERON, #1 HINGE. REF - MHIRJ REO 601R-57-51-1040, REV -A, DATED 2024-01-04 STEPS 1 THROUGH 9.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA202401230015](https://openairdocs.org/sdr/SWIA202401230015.md): Bulkhead · cracked · Dec 15, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FS625.00, STRINGER 13 HAS A CRACKED ANGLE. (C-CHECK RO 1/22/2024) LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL ANGLE P/N 601-35012-52 AT FS625 / STGR 13R. REF: CRJ200 SRM 51-42-21 REV 39 DATED 07/20/2022 AND DWG 601-35012, REV: D.
- [SDR SWIA2024012314](https://openairdocs.org/sdr/SWIA2024012314.md): Door · corroded · Dec 14, 2023 · N957SW · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR FWD LOWER CORNER AND SPLICE PLATE CORRODED. (C-CHECK RO 1/22/2024) REMOVED AND INSTALLED NEW SERVICE DOOR LOWER FWD CORNER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-13 AND CRJ 200 SRM 51-42-21 AND DWG 601R38304 REV. BN. COMPLIED WITH
- [SDR SWI2024F00016](https://openairdocs.org/sdr/SWI2024F00016.md): Skin · dented · Dec 13, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS589.00 STRG 26LH - STRG 27, EXTERIOR SKIN DENT (MARKED) (C-CHECK RO 1/22/2024) COMPLIED WITH REO 601R-53-61-8133 REV --, DATED 2023-12-18 STEPS 1 THRU 10, AND ENSURED ALL OTHER REQUIREMENTS OF REO 601R-51-00-309 REV A DATED 2017-08-23 WERE MET.
- [SDR SWI2024F00015](https://openairdocs.org/sdr/SWI2024F00015.md): Skin · dented · Dec 13, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS574.00 - FS605.00 STRG 24LH - 26LH, 5EA INTERIOR DENTS PROTRUDING EXTERNALLY ON THE FUSELAGE SKIN (MARKED) (C-CHECK RO 1/22/2024) COMPLIED WITH REO 601R-53-61-8133 REV--, DATED 2023-12-18, STEP 1 THRU 10, ENSURED ALL OTHER REQUIREMENTS OF REO 601R-51-00
- [SDR SWI2024F00014](https://openairdocs.org/sdr/SWI2024F00014.md): Door · corroded · Dec 13, 2023 · N957SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR LOWER AFT CORNER IS CORRODED. FLAGGED (C-CHECK RO 1/22/2024) REMOVED AND INSTALLED NEW SERVICE DOOR LOWER AFT CORNER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-13 AND CRJ 200 SRM 51-42-21 AND DWG 601R38304 REV. BN. COMPLIED WITH 51-90
- [SDR SWIA2024012313](https://openairdocs.org/sdr/SWIA2024012313.md): Skin · chafed · Dec 13, 2023 · N957SW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H SIDE INBOARD FLAP VANE SKIN INBOARD HAS CHAFE (MARKED) (C-CHECK RO 1/22/2024) FOUND DAMAGE ON RH SIDE INBOARD FLAP VANE IB SKIN OUT OF LIMITS REF CRJ 200 SRM 57-00-31 AND INSTALLED A NEW VANE SKIN REF CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E.
- [SDR SWI2024F00013](https://openairdocs.org/sdr/SWI2024F00013.md): Window Post · cracked · Dec 12, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Structure
  > L/H SIDE WINDSHIELD POST AFT LOWER ATTACHMENT CLIP HAS CRACK AT RADIUS. (C-CHECK RO 1/22/2024) REMOVED AND REPLACED L/H SIDE WINDSHIELD POST, AFT LOWER ATTACHMENT CLIP FITTING REF CRJ200 SRM 51-42-21 AND DWG#601R33007 REV-U. COMPLIED WITH 51-900-1003-SKY (
- [SDR SWI2024F00012](https://openairdocs.org/sdr/SWI2024F00012.md): Seat Track · worn · Dec 12, 2023 · N957SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PILOTS INBOARD AND OUTBOARD SEAT TRACKS HAVE WEAR GROOVES WORN INTO TRACK. (C-CHECK RO 1/22/2024) INSTALLED NEW PILOT INBOARD/OUTBOARD SEAT TRACK REF CRJ200 SRM 51-42-21 AND DWG NO 600-33100 REV AE.
- [SDR SWIA20240123012](https://openairdocs.org/sdr/SWIA20240123012.md): Skin · worn · Dec 12, 2023 · N957SW · Cndair CL6002B19 · Ailerons
  > L/H AILERON HAS WARE AND GOUGES ON L/E INBD TO JUST PAST CENTER (MARKED WITH RED) (C-CHECK RO 1/22/2024) REMOVED AND REPLACED L/H AILERON L/E UPPER SKIN WITH NEW REF. CRJ 200 SRM 51-42-21, 51-42-13, 51-42-06 AND DWG #601R1300 REV. P. COMPLIED WITH SKYWEST
- [SDR SWIA20240123010](https://openairdocs.org/sdr/SWIA20240123010.md): Hinge · damaged · Dec 10, 2023 · N957SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > DURING AUDIT OF 1C TASK CARD 52-840-101 (DETAILED INSPECTION OF THE RIGHT OVERWING EMERGENCY-EXIT EES), FOUND EMERGENCY EXIT DOOR LOWER FWD. DOOR HINGE FITTING I/B SIDE HAS IMPACT DAMAGE (C-CHECK RO 1/22/2024) BLENDED OUT DAMAGE ON RH EMERGENCY EXIT DOOR L
- [SDR SWIA202401230001](https://openairdocs.org/sdr/SWIA202401230001.md): Skin · dented · Dec 1, 2023 · N957SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADM# N957SW-7273 - RIGHT SIDE OF UPPER CENTER SKIN PANEL ON FUSELAGE NOSE BETWEEN FS169.00 TO 193.00. SINGLE DENT MEASURING 1.75 IN L X 1.5 IN W X 0.04 IN D. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STAN
- [SDR SWIA202310170015](https://openairdocs.org/sdr/SWIA202310170015.md): Unknown · warning message · Oct 15, 2023 · N957SW · Cndair CL6002B19 · Crew Oxygen System
  > OXY LO PRESS CAUTION MSG IN FLIGHT €” 29,000FT/-40*C/1390 PSI. RAN QRH & DESCENDED. PSI HELD STEADY AT 1360 PSI AT LOWER ALTITUDE. CAUTION MSG REMAINED ON THROUGHOUT FLT. ACFT WAS SVC€™D AT SGF, PRIOR TO DEPARTURE. INDICATED 1510 PSI AT 11*C AT GATE. ON
- [SDR SWIA202155644](https://openairdocs.org/sdr/SWIA202155644.md): Floor Panel · corroded · Jan 8, 2021 · N957SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LT PRESSURE FLOOR SILL PANEL CORROSION HAS BEEN FOUND TO BE OUT OF ALLOWABLE LIMITS, PER REO 601R-53-41-666 REV -C DATED 2012-11-06 AT 4 EA LOCATIONS BETWEEN FS 424 AND FS 529 DUE TO THE DISTANCE BETWEEN ADJACENT BLENDS. PERMANENT REPAIR REQUIRED. C-CHECK RO
- [SDR SWIA202155635](https://openairdocs.org/sdr/SWIA202155635.md): Washer · scratched · Jan 4, 2021 · N957SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LT MAIN LANDING GEAR WING TO FUSELAGE SIDE BRACE FITTING AT LBL 13, FS 513.00 HAS SCRATCHES IN LOWER CORNER BELOW ATTACHMENT BOLT. C-CHECK RO 1/28/2021. REPAIRED LT MLG WING TO FUSE SIDE BRACE FITTING AT LBL 13 FS 513.00, IAW REO 601R-57-21-3999 REV- DATED 2
- [SDR SWIA202055656](https://openairdocs.org/sdr/SWIA202055656.md): Nut Plate · elongated · Dec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LT FLOOR SILL 1.5" AFT OF FS 559.00 HAS 1 EA ELONGATED NUTPLATE HOLE. C-CHECK RO 1/28/2021. REMOVED AND REPLACED LT FLOOR SILL AFT OF FS 559, IAW CRJ 200 SRM-51-42-06 AND 51-42-21 REV 38, DATED 7/10/19. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY CO
- [SDR SWIA202055655](https://openairdocs.org/sdr/SWIA202055655.md): Former · corroded · Dec 30, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORMER AT FS 329.76 CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FORMER, IAW CRJ200 SRM 51-42-06 REV 38, B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION C
- [SDR SWIA202055643](https://openairdocs.org/sdr/SWIA202055643.md): Stiffener · cracked · Dec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED STIFFNER AT FS 621.00/STGR 16L. C-CHECK RO 1/28/2021. REMOVED AND REPLACED STIFFENER, IAW CRJ200 SRM 51-42-06 REV 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION
- [SDR SWIA202055642](https://openairdocs.org/sdr/SWIA202055642.md): Web · corroded · Dec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR AFT WEB FOUND TO BE CORRODED AND CRACKED IN MULTIPLE PLACES. C-CHECK RO 1/28/2021. REPLACED PAX DOOR AFT WEB, IAW CRJ 200 SRM 51-40-11.
- [SDR SWIA202055641](https://openairdocs.org/sdr/SWIA202055641.md): Web · corroded · Dec 30, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FWD WEB FOUND TO BE CORRODED AND CRACKED IN MULTIPLE PLACES. C-CHECK RO 1/28/2021. REPLACED PAX DOOR FWD WEB, IAW CRJ 200 SRM 51-40-11.
- [SDR SWIA202055654](https://openairdocs.org/sdr/SWIA202055654.md): Panel · chafed · Dec 23, 2020 · N957SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER WING PLANK IS CHAFED AT RBL 45 APPROXIMATLY FS 513 FROM CONTACT WITH MLG FAIRING. C-CHECK RO 1/28/2021. REPAIRED RT WING LOWER PLANK CHAFE AT RBL 45 FS 513, IAW REO 601R-57-21-880 REV -D DATED 2017-03-06. COMPLETED TASK CARD 51-900-1003-SKY
- [SDR SWIA202055662](https://openairdocs.org/sdr/SWIA202055662.md): Bracket · cracked · Dec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 621 TO FS 625 OBLIQUE ANGLE AT STR 14R IS CRACKED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED ANGLE AT FS 621 TO FS 625, IAW CRJ200 SRM 51-42-20. REFER TO CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202055661](https://openairdocs.org/sdr/SWIA202055661.md): Bracket · cracked · Dec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 621 TO FS 625 OBLIQUE ANGLE AT STR 15 IS CRACKED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED OBLIQUE ANGLE LOCATED ON STGR 15L AT FS 621 TO FS 625, IAW CRJ200 SRM51-42-21. REFER TO CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202055660](https://openairdocs.org/sdr/SWIA202055660.md): Bracket · cracked · Dec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 621 TO FS 652 OBLIQUE ANGLE AT STR 14 IS CRACKED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 621-625 OBLIQUE ANGLE AT STR 14L, IAW CRJ200 SRM 51-42-20, 51-40-11 AND 51-20-00. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.
- [SDR SWIA202055629](https://openairdocs.org/sdr/SWIA202055629.md): Intercostal · cracked · Dec 21, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS 621 TO FS 625 INTERCOSTAL IS CRACKED AT STR 16L. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL AT STR 16L AT FS 621-FS 625, IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CH
- [SDR SWIA202055630](https://openairdocs.org/sdr/SWIA202055630.md): Fitting · gouged · Dec 19, 2020 · N957SW · Cndair CL6002B19 · Emergency Exits
  > LEFT EMERGENCY EXIT DOOR UPPER FORWARD LATCH FITTING IS GOUGED IN CORNER. C-CHECK RO 1/28/2021. REPAIRED LT EMERGENCY EXIT UPPER FORWARD LATCH FITTING, IAW REO 601R-52-21-122 REV-, DATED 12/30/2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLE
- [SDR SWIA202055659](https://openairdocs.org/sdr/SWIA202055659.md): Angle · cracked · Dec 18, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Frame
  > STANDOFF ANGLE CRACKED AT FS 589.00 BETWEEN STR 26R AND STR 25R. C-CHECK RO 1/28/2021. REMOVED AND INSTALLED SERVICABLE STANDOFF ANGLE AT FS 589.00 BETWEEN STR 26R AND STR 25R, IAW CRJ 200 SRM 51-42-06. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PER
- [SDR SWIA202055653](https://openairdocs.org/sdr/SWIA202055653.md): Bulkhead · misinstalled · Dec 17, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LT INLET PANDOWN IS INSTALLED INCORRECTLY. WHILE C/W NDT TASK 54-430-602, NOTED A REPAIR DOUBLER IN THE INSPECTION AREA PREVENTING THE INSPECTION FROM BEING ABLE TO BE DONE AS WRITTEN. AFTER INVESTIGATION, FOUND THAT PANDOWN IS INSTALLED WITH THE MOUNTING FL
- [SDR SWIA202055677](https://openairdocs.org/sdr/SWIA202055677.md): Hinge Fitting · corroded · Dec 16, 2020 · N957SW · Cndair CL6002B19 · Rudder/Tab, Attach Fittings
  > UPPER RUDDER HINGE FITTING CONNECT HARDWARE HAS CORROSION. C-CHECK RO 1/28/2021. RECEIVED NEW SERVICEABLE HARDWARE, SEE CAMP 21748747 FOR INSTALL.
- [SDR SWIA202055631](https://openairdocs.org/sdr/SWIA202055631.md): Skin · dented · Dec 16, 2020 · N957SW · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB, RT SKIN HAS MULTIPLE DENTS. C-CHECK RO 1/28/2021. DISCREPANCY HAS A TYPOGRAPHICAL ERROR, SHOULD READ LT SIDE SKIN. REPAIRED SKIN MHIRJ REO 601R-55-31-368 REV-, DATED 12/29/2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED A
- [SDR SWIA202055652](https://openairdocs.org/sdr/SWIA202055652.md): Bracket · corroded · Dec 15, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Frame
  > INTERCOSTAL AT STR 20 FORM FS 310-FS 333 IS CORRODED. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL AT STR 20 AT FS 310-FS 333, IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT C
- [SDR SWIA202055651](https://openairdocs.org/sdr/SWIA202055651.md): Intercostal · corroded · Dec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 IS CORRODED BETWEEN FS 347 AND FS 320. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL, IAW CRJ200 SRM 51-42-06 AND 51-42-21 REV 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHE
- [SDR SWIA202055650](https://openairdocs.org/sdr/SWIA202055650.md): Intercostal · corroded · Dec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 IS CORRODED BETWEEN FS 347 AND FS 338. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL IAW CRJ200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHE
- [SDR SWIA202055645](https://openairdocs.org/sdr/SWIA202055645.md): Frame · cracked · Dec 13, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333 FRAME IS CRACKED AT STGR 1L. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 333 FRAME AT STGR 1L, IAW CRJ 200 SRM 51-42-06, DRAWING 601R32004 AND 51-42-21 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE AND FORM 337 IS ATTACHED. REF ATTACHED CONTINUATIO
- [SDR SWIA202055640](https://openairdocs.org/sdr/SWIA202055640.md): Skin · corroded · Dec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERSKIN IS CORRODED BETWEEN DD5-DD6 AND FS 347-FS 338. C-CHECK RO 1/28/2021. REMOVED AND REPLACED PAX DOOR INNER SKIN, IAW CRJ 200 SRM 51-42-06 AND 51-42-13.
- [SDR SWIA202055636](https://openairdocs.org/sdr/SWIA202055636.md): Intercostal · corroded · Dec 13, 2020 · N957SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD6 IS CORRODED BETWEEN FS 311 AND FS 347. C-CHECK RO 1/28/2021. REMOVED AND REPLACED INTERCOSTAL, IAW CRJ200 SRM TASKS 51-42-06 AND 51-42-21 REV 38B DATED 25 NOV 2020. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND A
- [SDR SWIA202055676](https://openairdocs.org/sdr/SWIA202055676.md): Seat Track · corroded · Dec 12, 2020 · N957SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK FS 547-FS 559+80 SEGMENT IS CORRODED. C-CHECK RO 1/28/2021. TECH REPLACED RT SIDE SEAT TRACK BETWEEN FS 547-FS 559+80, IAW CRJ 200 AMM 53-01-11-400-802.
- [SDR SWIA202055675](https://openairdocs.org/sdr/SWIA202055675.md): Seat Track · corroded · Dec 12, 2020 · N957SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT TRACK FS 547-FS 559+80 SEGMENT IS CORRODED. C-CHECK RO 1/28/2021. TECH REPLACED LT SIDE SEAT TRACK BETWEEN FS 547-FS 559+80, IAW CRJ 200 AMM 53-01-11-400-802.
- [SDR SWIA202055674](https://openairdocs.org/sdr/SWIA202055674.md): Strap · corroded · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN LBL 27 AND LBL 45 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REPLACED LT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN LBL 27 AND LBL 45, IAW CRJ-200 SRM 51-42-06 AND 51-42-10.
- [SDR SWIA202055673](https://openairdocs.org/sdr/SWIA202055673.md): Strap · corroded · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27 AND RBL 45 HAS MULTIPLE SPOTS OF CORROSION. C-CHECK RO 1/28/2021. REMOVED AND REPLACED RT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27 AND RBL 45, IAW CRJ-200 SRM 51-42-06 AND 51-42-10.
- [SDR SWIA202055658](https://openairdocs.org/sdr/SWIA202055658.md): Fitting · cracked · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS 484.00 RT INTERCOSTAL CLIP CRACKED BETWEEN RBL 27 AND RBL 36. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 484.00 RT INTERCOSTAL CLIP BETWEEN RBL 27 AND RBL 36, IAW CRJ 200 SRM 51-42-21. REFERENCE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202055657](https://openairdocs.org/sdr/SWIA202055657.md): Fitting · cracked · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS 484.00 LT INTERCOSTAL CLIP CRACKED BETWEEN LBL 27 AND LBL 36. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FS 484.00 LT INTERCOSTAL CLIP CRACKED BETWEEN LBL 27 AND LBL 36, IAW CRJ 200 SRM 51-42-02. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202055649](https://openairdocs.org/sdr/SWIA202055649.md): Nut Plate · corroded · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > MINOR CORROSION AROUND NUTPLATE ON FLOORBEAM AT RBL 9 BETWEEN FS 409.00 TO FS 409.00 +16. C-CHECK RO 1/28/2021. REMOVED AND REPLACED FLOORBEAM CAP, IAW REO 601R-53-31-1166 REV- DATED 2021-01-08. COMPLIED WITH TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED
- [SDR SWIA202055648](https://openairdocs.org/sdr/SWIA202055648.md): Floor Support · corroded · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPAIRED IAW REO 601R-53-41-666 REV C DATED 2012-11-06. MAJOR REPAIR TASK CARD 51-900-1003-SKY & FORM M337 COMPLETED. NO MEASUREABLE WEIGHT CHANGE, REFER
- [SDR SWIA202055639](https://openairdocs.org/sdr/SWIA202055639.md): Floor Support · corroded · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPAIRED IAW REO 601R-53-41-666 REV C DATED 2012-11-06. MAJOR REPAIR TASK 51-900-1003-SKY & FORM M337 COMPLETED AND ATTACHED. NO MEASUREABLE WEIGHT CHANGE
- [SDR SWIA202055638](https://openairdocs.org/sdr/SWIA202055638.md): Angle · corroded · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RT FLOOR SILL ANGLE HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPAIRED RT FLOOR SILL ANGLE CORROSION FROM FS 409.00+128 TO FS 559.00, IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06, REF ATTACHED CONTINU
- [SDR SWIA202055634](https://openairdocs.org/sdr/SWIA202055634.md): Floorbeam · corroded · Dec 10, 2020 · N957SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT RBL 9 HAS MULTIPLE SPOTS OF MINOR CORROSION FROM FS 409.00 +128 TO FS 559.00. C-CHECK RO 1/28/2021. REPLACED FLOORBEAM CAP AT RBL 9 AT FS 409+128 TO FS 559, IAW MHIRJ REO 601R-53-41-2835 REV- DATED 2021-01-17. COMPLETED TASK CARD 51-900-1003-S

Next page: https://openairdocs.org/aircraft/N957SW/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 = 'N957SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N957SW/reports

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