# Service difficulty reports: N221PS

A list on [N221PS](https://openairdocs.org/aircraft/N221PS.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 · 175 reports

- [SDR SWIA2026100477486](https://openairdocs.org/sdr/SWIA2026100477486.md): Windshield · cracked · Oct 4, 2026 · N221PS · Cndair CL6002B19 · Flight Compartment Windows
  > DIVERTED DUE TO LH WINDSHIELD CRACKED SMALL SPARK CAME FROM WINDSHIELD HEAT WIRING LEADS NO PRESSURIZATION ISSUES. FLIGHT 6077. R & R LT WINDSHIELD PER AMM 56-11-01 AND COMPLIED WITH TASK CARD MIP 56-220-1000-SKY, OPS CHECK AND LEAK CHECKED GOOD, REFERENCE
- [SDR SWIA2025121776360](https://openairdocs.org/sdr/SWIA2025121776360.md): Rib · cracked · Dec 17, 2025 · N221PS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA93275-601R-57-51-1052 REV -. COMPLY WITH PERMANENT REPAIR ON RA ID: 93275THE LHS WING TE RIB AT WS130.10 HAS BEEN REPAIRED DUE TO BEND AND CRACK DAMAGE PER REO 601R-57-51-1052 REV -- DATED 2024-08-29. PERMANENT REPAIR
- [SDR SWIA2025121776359](https://openairdocs.org/sdr/SWIA2025121776359.md): Cover · open · Dec 17, 2025 · N221PS · Cndair CL6002B19 · Accessory Compartment Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA104215-REO 601R-53-61-8367 COMPLIED WITH PERMANENT REPAIR FOUND DAMAGE FROM LOW PRESSURE AIR CAP MISSING. SUSPECTED GROUND AIR COVER LEFT OPEN. REFERENCE AML 1675134COMPLIED WITH REO 601R-53-61-8367 STEPS 1 AND 2 PE
- [SDR SWIA2025121776358](https://openairdocs.org/sdr/SWIA2025121776358.md): Frame · corroded · Dec 17, 2025 · N221PS · Cndair CL6002B19 · Fuselage Main, Frame
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA94505-601R-53-61-8235 MXCODEID105229-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 94505CW TEMPORARY DISPOSITION: FOR BLENDED CORROSION DAMAGE TO FRAME ASSY. FS589.00 ASSY. BETWEEN STR 21R - STR 22R. PERMANENT REPAIR:
- [SDR SWIA2025070300622](https://openairdocs.org/sdr/SWIA2025070300622.md): Warning Message · illuminated · Jun 22, 2025 · N221PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > D:GEAR DISAGREE ON FINAL APPROACH INTO IAD, QRH CLEARED MESSAGEC: MEL 32-30-1CAT A DUE WITHIN 1 FLIGHT DAY FROM 06/22/2025CAT II DOWNGRADEGEAR DISAGREE ON FINAL APPROACH INTO IAD, QRH CLEARED MESSAGE (FLIGHT 5062 - FILED CLOSED)JUN 22, 2025 STATION: IAD--DEF
- [SDR SWI2025F00747](https://openairdocs.org/sdr/SWI2025F00747.md): Landing Gear · warning message · Jun 22, 2025 · N221PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > D:GEAR DISAGREE ON FINAL APPROACH INTO IAD, QRH CLEARED MESSAGEC: MEL 32-30-1CAT A DUE WITHIN 1 FLIGHT DAY FROM 06/22/2025CAT II DOWNGRADEGEAR DISAGREE ON FINAL APPROACH INTO IAD, QRH CLEARED MESSAGE (FLIGHT 5062 - FILED OPEN)JUN 22, 2025 STATION: IAD--DEFER
- [SDR SWIA2024110809](https://openairdocs.org/sdr/SWIA2024110809.md): Frame · corroded · Oct 9, 2024 · N221PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CORROSION ON FORWARD FACE OF FRAME AT FS589.00 AT BETWEEN STGR21R AND STGR22R. (FILED CLOSED)COMPLIED WITH TEMPORARY REPAIR REO 601R-53-61-8235 DATED: 2024-10-05 REV --. REPLACED 7 RIVETS ON FRAME 6 GOING TO THE OUTER PART OF FUSELAGE. REF CHILD FOR LEAK
- [SDR SWIA202410210029](https://openairdocs.org/sdr/SWIA202410210029.md): Frame · corroded · Oct 9, 2024 · N221PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CORROSION ON FORWARD FACE OF FRAME AT FS589.00 AT BETWEEN STGR21R AND STGR22R. (FILED OPEN)COMPLIED WITH TEMPORARY REPAIR REO 601R-53-61-8235 DATED: 2024-10-05 REV --. REPLACED 7 RIVETS ON FRAME 6 GOING TO THE OUTER PART OF FUSELAGE. REF CHILD FOR LEAK C
- [SDR SWIA20241002](https://openairdocs.org/sdr/SWIA20241002.md): Floor Support · corroded · Oct 2, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON RH PRESSURE FLOOR SILL AT FS537.00 (MARKED WITH TAPE). (FILED CL;OSED)REPAIRED CORROSION ON RH PRESSURE FLOOR SILL AT FS537.00 WITH REFERENCE TO REO 601R-53-41-3266 REV "--" DATED 2024-10-08. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE
- [SDR SWI2024F00902](https://openairdocs.org/sdr/SWI2024F00902.md): Floor Support · corroded · Oct 2, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON RH PRESSURE FLOOR SILL AT FS537.00 (MARKED WITH TAPE). (FILED OPEN)
- [SDR SWI2024F01131](https://openairdocs.org/sdr/SWI2024F01131.md): Angle · corroded · Sep 24, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SILL ANGLE AT BOTTOM OF PASSENGER DOOR CUTOUT HAS MULTIPLE SPOTS OF CORROSION AND MISSING PAINT IN BETWEEN FS310.00 AND FS349.00 (MARKED WITH TAPE) (FILED CLOSED)REMOVED AND REPLACED PASSENGER DOOR SILL ANGLE AT BOTTOM OF PASSENGER DOOR CUTOUT B
- [SDR SWIA2024102100924](https://openairdocs.org/sdr/SWIA2024102100924.md): Door Sill · corroded · Sep 24, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SILL ANGLE AT BOTTOM OF PASSENGER DOOR CUTOUT HAS MULTIPLE SPOTS OF CORROSION AND MISSING PAINT IN BETWEEN FS310.00 AND FS349.00 (MARKED WITH TAPE) (FILED OPEN)REMOVED AND REPLACED PASSENGER DOOR SILL ANGLE AT BOTTOM OF PASSENGER DOOR CUTOUT BET
- [SDR SWI2024F01140](https://openairdocs.org/sdr/SWI2024F01140.md): Floor Support · corroded · Sep 23, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSIOIN ON RH PRESSURE FLOOR SILL AT FS439.00 (FILED CLOSED) REPAIRED CORROSION DAMAGE ON RH PRESSURE FLOOR SILL AT FS439.00 WITH REFERENCE TO REO 601R-53-41-666 REV "C" DATED 2012-11-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE
- [SDR SWI2024F01139](https://openairdocs.org/sdr/SWI2024F01139.md): Floor Support · corroded · Sep 23, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON LH PRESSURE FLOOR SILL AT FS499.00 (FILED CLOSED)REPAIRED CORROSION DAMAGE ON LH PRESSURE FLOOR SILL AT FS499.00 WITH REFERENCE TO REO 601R-53-41-666 REV "C" DATED 2012-11-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO N
- [SDR SWI2024F01138](https://openairdocs.org/sdr/SWI2024F01138.md): Floor Support · corroded · Sep 23, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON RH PRESSURE FLOOR SILL AT FS529.00 (MARKED WITH TAPE) (FILED CLOSED)REPAIRED CORROSION ON RH PRESSURE FLOOR SILL AT FS529.00 WITH REFERENCE TO REO 601R-53-41-666 REV "-C" DATED 2012-11-06 AND REO 601R-53-41-3266 REV "--" DATED 2024-10-08. P
- [SDR SWI20241021027](https://openairdocs.org/sdr/SWI20241021027.md): Floor Support · corroded · Sep 23, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSIOIN ON RH PRESSURE FLOOR SILL AT FS439.00 (FILED OPEN)REPAIRED CORROSION DAMAGE ON RH PRESSURE FLOOR SILL AT FS439.00 WITH REFERENCE TO REO 601R-53-41-666 REV "C" DATED 2012-11-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO ND
- [SDR SWI2024F01026](https://openairdocs.org/sdr/SWI2024F01026.md): Floor Support · corroded · Sep 23, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON LH PRESSURE FLOOR SILL AT FS499.00 (FILED OPEN)REPAIRED CORROSION DAMAGE ON LH PRESSURE FLOOR SILL AT FS499.00 WITH REFERENCE TO REO 601R-53-41-666 REV "C" DATED 2012-11-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDT
- [SDR SWIA20241021923](https://openairdocs.org/sdr/SWIA20241021923.md): Floor Support · corroded · Sep 23, 2024 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON RH PRESSURE FLOOR SILL AT FS529.00 (MARKED WITH TAPE) (FILED OPEN)REPAIRED CORROSION ON RH PRESSURE FLOOR SILL AT FS529.00 WITH REFERENCE TO REO 601R-53-41-666 REV "-C" DATED 2012-11-06 AND REO 601R-53-41-3266 REV "--" DATED 2024-10-08. PER
- [SDR SWIA202309200010](https://openairdocs.org/sdr/SWIA202309200010.md): Unknown · worn · Sep 10, 2023 · N221PS · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > REMOVED FRAME SPLICE @ FS 265 STR 23LH TO FOM REF CRJ 200 SRM 51-42-06. (FILED CLOSED) INSTALLED SAME SERVICEABLE FRAME SPLICE @ FS 265 STR 23LH TO FOM REF CRJ 200 SRM 51-42-06. COMPLETED 51-900-1003-SKY AND M-337.
- [SDR SWIA20230920828](https://openairdocs.org/sdr/SWIA20230920828.md): Unknown · dented · Aug 28, 2023 · N221PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1199891: FOUND DENT TO MEASURE 7"L X 2.75"W X 0.080"D, WITH SEVERAL PAINT SCRATCHES ON FUSELAGE SKIN PANEL (DWG. 601R33010, 0.043" THK IN AFFECTED CHEM-MILL AREA, REF) BETWEEN FS265 - FS280 AND STR. 21L - STR.22L. DAMAGE IS OUT OF LIMIT
- [SDR SWIA202308290028](https://openairdocs.org/sdr/SWIA202308290028.md): Unknown · dented · Aug 28, 2023 · N221PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1199891: FOUND DENT TO MEASURE 7"L X 2.75"W X 0.080"D, WITH SEVERAL PAINT SCRATCHES ON FUSELAGE SKIN PANEL (DWG. 601R33010, 0.043" THK IN AFFECTED CHEM-MILL AREA, REF) BETWEEN FS265 - FS280 AND STR. 21L - STR.22L. DAMAGE IS OUT OF LIMIT
- [SDR SWIA202162657](https://openairdocs.org/sdr/SWIA202162657.md): None · failed · Nov 17, 2021 · N221PS · Cndair CL6002B19 · Engine Indicating System
  > WHILE IN CRUSE AT ALT FL280 LH ENGINE FAILED. NO HIGH EGT OR HIGH PRESSURE EXPERIENCED. RAN QRC AND QRH PROCEDURES BEFORE DIVERTING TO ALO. NO OVERWEIGHT LANDING. (FLIGHT 5184 - FILED CLOSED) UPON INSPECTION OF LH ENGINE, UNABLE TO ROTATE AGB USING CRANK
- [SDR SWIA202161792](https://openairdocs.org/sdr/SWIA202161792.md): None · cracked · Oct 19, 2021 · N221PS · Cndair CL6002B19 · Window/Windshield System
  > IN FLIGHT L WSHLD HEAT CAUTION AND NEW CRACK IN LEFT WINDSHIELD (FLIGHT 5979 - FILED CLOSED) TORQUE WRENCH INFO: / S/N: 0906300068 / DUE CAL: 03/2022 / REMOVED AND REPLACED LH WINDSHIELD REFERENCE SKYWEST TASK CARD, CARD COMPLETED AND LINKED IN THIS EAML
- [SDR SWIA202053243](https://openairdocs.org/sdr/SWIA202053243.md): Hinge · cracked · Sep 30, 2020 · N221PS · Cndair CL6002B19 · Trailing Edge Flaps
  > ON OUTBOARD FLAP HINGE ARM AND WHERE PANEL 595BB IS PLACED THE TOP ANGLE THAT SITS ON THE TOP OUTBOARD SIDE OF IT IS CRACKED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED BRACKET 601R14629-109, IAW CRJ 200 SRM.
- [SDR SWIA202053296](https://openairdocs.org/sdr/SWIA202053296.md): Bushing · corroded · Sep 16, 2020 · N221PS · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP INBOARD HINGE BOLT BUSHING FOUND TO BE CORRODED. C-CHECK RO 10/13/2020. RECEIVED NEW SERVICEABLE BUSHING FOR LT INBOARD FLAP INBOARD HINGE, REF CAMP 21380330 FOR INSTALLATION OF HARDWARE AND OPS.
- [SDR SWIA202053295](https://openairdocs.org/sdr/SWIA202053295.md): Lever · corroded · Sep 11, 2020 · N221PS · Cndair CL6002B19 · Elevator Structure
  > LT ELEVATOR SYSTEM MECHANICAL-CONTROL PATH VERTICAL TORQUE TUBE LOWER BEARING APPEARS TO HAVE CORROSION (RUST) AFT END OF CANTED RIB AREA. NOT IN WORKSCOPE/2C TASKCARD. C-CHECK RO 10/13/2020. REMOVED LT ELEVATOR CONTROL LEVER ASSEMBLY AND INSTALLED NEW SERV
- [SDR SWIA202053294](https://openairdocs.org/sdr/SWIA202053294.md): Bushing · corroded · Sep 11, 2020 · N221PS · Cndair CL6002B19 · Elevator Structure
  > LEFT ELEVATOR HINGE FITTINGS (BRASS BUSHINGS) APPEARS TO HAVE PITTING AND CORROSION ON THE THREE INBOARD ATTACH POINTS 55-330-507. C-CHECK RO 10/13/2020. REMOVED AND REPLACED 3 CORRODED HAT BUSHINGS ON LT ELEVATOR STRUCTURE AT PCU ATTACH POINTS, IAW CRJ-200
- [SDR SWIA202053235](https://openairdocs.org/sdr/SWIA202053235.md): Fitting · gouged · Sep 6, 2020 · N221PS · Cndair CL6002B19 · Fuselage Main, Structure
  > COPILOTS WINDSHIELD SIDE POST LOWER FORWARD FITTING IS GOUGED AT FORWARD END FROM CONTACT WITH WINDSHIELD STRAP SCREW. C-CHECK RO 10/13/2020. REMOVED AND REPLACED COPILOTS WINDSHIELD SIDE POST LOWER FORWARD FITTING, IAW CRJ-200 SRM AND DRAWING 601R33007. SK
- [SDR SWIA202053293](https://openairdocs.org/sdr/SWIA202053293.md): Strap · corroded · Sep 3, 2020 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT STRAP RBL 9.0 TO RBL 27.0 AT FS 559+96 HAS 3 AREAS OF MINOR CORROSION. C-CHECK RO 10/13/2020. REMOVED AND REPLACED FLOOR SUPPORT STRAP AT FS 559+96 RBL 9.0 TO RBL 27.0, IAW CRJ-200 SRMS. APPLIED FINISH IAW SRM.
- [SDR SWIA202053292](https://openairdocs.org/sdr/SWIA202053292.md): Floorbeam · corroded · Sep 3, 2020 · N221PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CABIN FLOOR SUPPORT STRAP UPPER SURFACE HAS MINOR CORROSION FS 559+80 RBL 9.0 TO LBL 9.0. C-CHECK RO 10/13/2020. CABIN FLOOR SUPPORT STRAP UPPER SURFACE CORROSION AT FS 559+80 RBL 9.0 TO LBL 9.0. REMOVED AND PAINTED. REFERENCE CONTINUATION CARD FOR THE WOR
- [SDR SWIA202053291](https://openairdocs.org/sdr/SWIA202053291.md): Strap · corroded · Sep 3, 2020 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT STRAP HAS MINOR CORROSION ON UPPER SURFACE AT FS 559+96 JUST OUTBOARD OF LBL 9.0. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED FABRICATED STRAP 601R32216-47, IAW CRJ 200 SRM. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202053290](https://openairdocs.org/sdr/SWIA202053290.md): Floorbeam · corroded · Sep 3, 2020 · N221PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CABIN FLOOR SUPPORT STRAP UPPER SURFACE CORRODED AROUND NUTPLATE HOLES LBL 9.0 TO LBL 27.0 FS 589.00. C-CHECK RO 10/13/2020. REMOVED AND REPLACED CABIN FLOOR SUPPORT STRAP AT FS 589.00 LBL 9.0 TO LBL 27.0, IAW CRJ-200 SRMS. APPLIED FINISH IAW SRM.
- [SDR SWIA202053289](https://openairdocs.org/sdr/SWIA202053289.md): Floorbeam · corroded · Sep 3, 2020 · N221PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT STRAP FS 589.00 RBL 27.0 TO RBL 42.0 CORRODED ON UPPER SURFACE. C-CHECK RO 10/13/2020. REMOVED AND REPLACED FLOOR SUPPORT STRAP AT FS 589 RBL 27 TO 42, IAW SRM CRJ 200.
- [SDR SWIA202053236](https://openairdocs.org/sdr/SWIA202053236.md): Floor Support · corroded · Sep 3, 2020 · N221PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > OUTBOARD FLANGE OF FLOORBEAM CAP AT RBL 9.0 BETWEEN FS 559+96 AND FS 559+112 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RBL 9 FLOOR BEAM CAP FROM FS 559 TO 569, IAW CRJ-200 SRM AND MHIRJ REO. FABRICATED, LOCATED AND DRILLED FLOOR BEAM CAP, IAW
- [SDR SWIA202053288](https://openairdocs.org/sdr/SWIA202053288.md): Attach Fitting · corroded · Sep 1, 2020 · N221PS · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > RIGHT ELEVATOR INBOARD PCU ATTACH FITTING AND THE NUMBER ONE HINGE HAS CORRODED HILITE COLLARS INSIDE THE ELEVATOR. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED NEW FASTENERS, REFERENCE CONTINUATION CARD FOR THE WORK PERFORMED.
- [SDR SWIA202053241](https://openairdocs.org/sdr/SWIA202053241.md): Former · cracked · Sep 1, 2020 · N221PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER IS CRACKED AT PULLEY BRACKET LOCATION, REQUIRES REPLACEMENT. C-CHECK RO 10/13/2020. REMOVED DAMAGED PAX DOOR AFT FORMER AND REPLACED WITH SERVICEABLE FORMER, IAW CRJ 200 SRM. COMPLETED TASK CARD AND ATTACHED COMPLETED FORM 337. NO WEIGH
- [SDR SWIA202053287](https://openairdocs.org/sdr/SWIA202053287.md): Seat Track · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT CABIN SEAT RAIL BETWEEN FS 544.00 AND FS 559.00+80 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED NEW FABBED SERVICEABLE LT CABIN SEAT RAIL BETWEEN FS 544.00 AND FS 559.00+80, REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202053286](https://openairdocs.org/sdr/SWIA202053286.md): Seat Track · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT CABIN SEAT RAIL BETWEEN FS 499.00 AND FS 544.00 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED NEW FABBED SERVICEABLE LT CABIN SEAT RAIL BETWEEN FS 499.00 AND FS 544.00, REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202053285](https://openairdocs.org/sdr/SWIA202053285.md): Seat Track · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT CABIN SEAT RAIL BETWEEN FS 449.00+85 AND FS 499.00 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED LT CABIN SEAT RAIL BETWEEN FS 449.00+85 AND FS 499.00 IAW CRJ 200 AMM.
- [SDR SWIA202053284](https://openairdocs.org/sdr/SWIA202053284.md): Seat Track · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT CABIN SEAT RAIL BETWEEN FS 409.00+112 AND FS 449.00+85 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED CORRODED SEAT RAIL ON LT CABIN SEAT RAIL BETWEEN FS 409.00+112 AND FS 449.00+85, IAW CRJ200 AMM.
- [SDR SWIA202053283](https://openairdocs.org/sdr/SWIA202053283.md): Seat Track · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN SEAT RAIL BETWEEN FS 554.00 AND FS 559.00+80 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT CABIN SEAT RAIL BETWEEN FS 554.00 TO FS 559.00+80, IAW CRJ-200 AMM. REPLACEMENT SEAT TRACK WAS FABRICATED ON CAMP 21531733.
- [SDR SWIA202053282](https://openairdocs.org/sdr/SWIA202053282.md): Seat Track · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN SEAT RAIL BETWEEN FS 499.00 AND FS 554.00 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT CABIN SIDE SEAT RAIL BETWEEN FS 499.00 TO FS 554.00 WITH FABRICATED SEAT RAIL, IAW BOMBARDIER REO AND CRJ-200 AMM.
- [SDR SWIA202053281](https://openairdocs.org/sdr/SWIA202053281.md): Seat Track · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN SEAT RAIL BETWEEN FS 449.00+85 AND FS 499.00 IS CORRODED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT SIDE SEAT RAIL BETWEEN FS 449.00+85 AND FS 499.00, IAW CRJ200 AMM.
- [SDR SWIA202053255](https://openairdocs.org/sdr/SWIA202053255.md): Skin · corroded · Aug 31, 2020 · N221PS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING, LOWER WING PLANK FUEL ACCESS CUTOUT 540CB HAS PITTING CORROSION AROUND CIRCUMFERENCE OF CUTOUT. C-CHECK RO 10/13/2020. REPAIRED CORROSION ON LT LOWER WING PLANK FUEL ACCESS CUTOUT 540CB, IAW BOMBARDIER REO. REFERENCE CONTINUATION FOR WORK PERFORMED
- [SDR SWIA202053300](https://openairdocs.org/sdr/SWIA202053300.md): Seat Track · gouged · Aug 28, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACKS GOUGED IN SEVERAL LOCATION BETWEEN FS 409+128 TO FS 559 AT LBL 9. C-CHECK RO 10/13/2020. REMOVED AND REPLACED SEAT TRACK FROM FS 409+128 TO FS 559 LBL 9, IAW CRJ-200 AMM. REPLACEMENT TRACK FABRICATED ON CAMP 21531672.
- [SDR SWIA202053299](https://openairdocs.org/sdr/SWIA202053299.md): Seat Track · gouged · Aug 28, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACKS GOUGED IN SEVERAL LOCATION BETWEEN FS 409+128 TO FS 559 AT RBL 9. C-CHECK RO 10/13/2020. REMOVED AND REPLACED SEAT TRACK FROM FS 409+128 TO FS 559 AT RBL 9, IAW CRJ-200 AMM. SEAT TRACK WAS FABRICATED ON CAMP 21445111.
- [SDR SWIA202053280](https://openairdocs.org/sdr/SWIA202053280.md): Seat Track · corroded · Aug 28, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED BETWEEN FS 409 TO FS 409+128 AT RBL 9. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED NEW SERVICEABLE SEAT TRACK FROM FS 409-FS 409+128 AT RBL 9, IAW CRJ 200 AMM.
- [SDR SWIA202053279](https://openairdocs.org/sdr/SWIA202053279.md): Seat Track · corroded · Aug 28, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED BETWEEN FS 409 TO FS 409+128 AT LBL 9. C-CHECK RO 10/13/2020. REMOVED DAMAGED FLOOR TRACK AND REPLACED WITH NEW SERVICEABLE TRACK, IAW CRJ200 AMM.
- [SDR SWIA202053278](https://openairdocs.org/sdr/SWIA202053278.md): Seat Track · corroded · Aug 28, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED BETWEEN FS 349 TO FS 409 AT LBL 9. C-CHECK RO 10/13/2020. INSTALLED NEW SECTION SEAT TRACK FS 349 TO FS 409 AT LBL 9, IAW CRJ 200 AMM.
- [SDR SWIA202053277](https://openairdocs.org/sdr/SWIA202053277.md): Seat Track · corroded · Aug 28, 2020 · N221PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED BETWEEN FS 349 TO FS 409 AT RBL 9. C-CHECK RO 10/13/2020. INSTALLED NEW, SERVICEABLE FLOOR SEAT TRACK BETWEEN FS 349 TO FS 409 AT RBL 9, IAW CRJ 200 AMM. SEE CONTINUATION CARD FOR WORK PERFORMED.

Next page: https://openairdocs.org/aircraft/N221PS/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 = 'N221PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N221PS/reports

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