# Service difficulty reports: N441SW

A list on [N441SW](https://openairdocs.org/aircraft/N441SW.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 · 199 reports

- [SDR SWIA202266458](https://openairdocs.org/sdr/SWIA202266458.md): None · arced · Sep 12, 2022 · N441SW · Cndair CL6002B19 · Window/Windshield System
  > WHILE DESCENDING THROUGH 20,000 FT, THE CA WINDSHIELD STARTED ARCING AT THE BOTTOM JUST LEFT OF CENTER. SELECTED WINDSHIELD HEAT OFF AND THE ARCING STOPPED. (FLIGHT #4311 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25482491 WITH THE FOLLOW
- [SDR SWIA202054582](https://openairdocs.org/sdr/SWIA202054582.md): Connector · detached · Dec 10, 2020 · N441SW · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER TAKEOFF AND RETRACTING THE GEAR WE RECEIVED NOSE GEAR DOOR OPEN WARNING MESSAGE. AFTER COMPLYING WITH THE QRH THE MESSAGE REMAINED. NO AIRSPEED OR STRUCTURAL LIMITATIONS WERE EXCEEDED, LANDING WAS NORMAL. FLIGHT 4264-FILED CLOSED. FOUND CANNON PLUG T
- [SDR SWIA202054311](https://openairdocs.org/sdr/SWIA202054311.md): Panel · corroded · Oct 25, 2020 · N441SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FIXED STAIR PANEL IS CORRODED UNDER LOWER NUTPLATE HOLES AND INTERIOR STIFFENERS. C-CHECK RO 11/21/2020. REMOVED CORROSION ON PAX DOOR FIXED STAIR PANEL, REF CRJ200 SRM. EVALUATED AND FOUND TO OUT OF LIMITS, REF CRJ200 SRM. REPLACED STEP PANEL WIT
- [SDR SWIA202054310](https://openairdocs.org/sdr/SWIA202054310.md): Step · corroded · Oct 25, 2020 · N441SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STEP 832BT IS CORRODED UNDER LOWER NUTPLATE HOLES AND INTERIOR STIFFENERS. C-CHECK RO 11/21/2020. REMOVED CORROSION ON PAX DOOR STEP 832BT, REF CRJ200 SRM. EVALUATED AND FOUND TO OUT OF LIMITS, REF CRJ200 SRM. REPLACED STEP PANEL WITH NEW P/N 601R
- [SDR SWIA202054309](https://openairdocs.org/sdr/SWIA202054309.md): Angle · chafed · Oct 22, 2020 · N441SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVING PAX DOOR FWD PULL-IN LEVER FOUND CHAFE DAMAGE TO FWD FORMER REINFORCEMENT ANGLE CAUSED DUE TO EXCESS WEAR DAMAGE ON THE PULL-IN LEVER. C-CHECK RO 11/21/2020. REPAIRED CHAFE DAMAGED AT PAX DOOR FWD FORMER REINFORCEMENT ANGLE COMMON TO FWD PULL I
- [SDR SWIA202054308](https://openairdocs.org/sdr/SWIA202054308.md): Skin · dented · Oct 21, 2020 · N441SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LT FUSELAGE SKIN HAS 2" X 4" DENT WITH A MILD CREASE BETWEEN FS 409 AND FS 409+16 & STGR 16L AND 17L. C-CHECK RO 11/21/2020. PERFORMED DOUBLER REPAIR TO LT FUSELAGE SKIN AREA BETWEEN APPROXIMATELY FS 409 TO FS 409+16 STGR 16L AND 17L, REF CRJ-200 SRM. REPAI
- [SDR SWIA202054307](https://openairdocs.org/sdr/SWIA202054307.md): Bracket · cracked · Oct 21, 2020 · N441SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER FWD ROLLER FITTING BRACKET CRACKED IN THE RADIUS. C-CHECK RO 11/21/2020. REMOVED CRACKED CARGO DOOR UPPER FWD ROLLER FITTING BRACKET P/N CC670-38706-3 AND INSTALLED NEW CARGO DOOR UPPER FWD ROLLER FITTING BRACKET P/N CC670-38706-3, REF CRJ20
- [SDR SWIA202054306](https://openairdocs.org/sdr/SWIA202054306.md): Fitting · chafed · Oct 21, 2020 · N441SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING, FLAP STUB FAIRING FITTING, MOUNTED TO THE WING TRAILING EDGE IS CHAFED, FLAGGED. C-CHECK RO 11/21/2020. REMOVED EXISTING FLAP STUB P/N 601R10371-1, REF CRJ 200 SRM. RECEIVED NEW PART P/N 601R10371-1, FIT AND DRILLED NEW PART, REF CRJ 200 SRM. IN
- [SDR SWIA202054305](https://openairdocs.org/sdr/SWIA202054305.md): Attach Angle · cracked · Oct 19, 2020 · N441SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR NET ATTACHMENT BEAM ANGLE PN 601R35050-109 AT FS 621 CRACKED. C-CHECK RO 11/21/2020. REMOVED CARGO DOOR NET ATTACHMENT BEAM CRACKED ANGLE P/N 601R35050-109, REF CRJ200 SRM. DRILLED AND LOCATED NEW ANGLE, REF CRJ200 SRM. INSTALLED CARGO DOOR NET
- [SDR SWIA202054304](https://openairdocs.org/sdr/SWIA202054304.md): Strap · corroded · Oct 19, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE REMOVING FLOOR SUPPORT STRAP, FOUND CORROSION ON PRESSURE FLOOR SILL (PANEL) BETWEEN LBL 27-LBL 42 AT FS 559.00. C-CHECK RO 11/21/2020. REPAIRED PRESSURE FLOOR SILL (PANEL) BETWEEN LBL 27-LBL 42 AT FS 559.00, REF REO. COMPLIED WITH TASK CARD, REF REO.
- [SDR SWIA202054303](https://openairdocs.org/sdr/SWIA202054303.md): Strap · corroded · Oct 19, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE REMOVING FLOOR SUPPORT STRAP, FOUND CORROSION ON RBL 27.0 FLOOR BEAM CAP OUTBOARD LIP AT FS 559.00. C-CHECK RO 11/21/2020. REMOVED CORROSION FLOOR SUPPORT STRAP ON RBL 27.0 FLOOR BEAM CAP OUTBOARD LIP AT FS 559.00. COMPLIED WITH MHIRJ REO.
- [SDR SWIA202054302](https://openairdocs.org/sdr/SWIA202054302.md): Pressure Blkhd · cracked · Oct 17, 2020 · N441SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE BULKHEAD AFT OF FS 621.0 STIFFENER IS CRACK. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW STIFFENER, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA202054301](https://openairdocs.org/sdr/SWIA202054301.md): Track · chafed · Oct 15, 2020 · N441SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR, AFT CARGO DOOR TRACK CHAFED, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW AFT CARGO TRACK, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202054300](https://openairdocs.org/sdr/SWIA202054300.md): Hinge Fitting · chafed · Oct 15, 2020 · N441SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > RT ELEVATOR HINGE FITTING (HORIZONTAL STAB SIDE) HAS CHAFE ON LOWER SURFACE FROM CONTACT WITH ELEVATOR ACCESS PANEL 344CB. C-CHECK RO 11/21/2020. COMPLIED WITH PERMANENT REPAIR ELEVATOR HINGE FITTING, REF REO. ALL APPLICABLE STEPS COMPLIED WITH, NO OTHER DE
- [SDR SWIA202054299](https://openairdocs.org/sdr/SWIA202054299.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE SEAT RAIL CHANNEL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 349.00-364.00, AREAS MARKED. C-CHECK RO 11/21/2020. BLENDED CORROSION ON LT SIDE SEAT RAIL CHANNEL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 349.00-364.00, REF CRJ 200 SRM. E
- [SDR SWIA202054298](https://openairdocs.org/sdr/SWIA202054298.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE SEAT RAIL CHANNEL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 364.00-409.00+16, AREAS MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION ON LEFT-HAND SEAT RAIL CHANNEL BETWEEN FS 364.00-FS 409.00+16, AND EVALUATED AS OUT-OF-LIMITS, REF CRJ2
- [SDR SWIA202054297](https://openairdocs.org/sdr/SWIA202054297.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGE ON RT SIDE SEAT RAIL AND SEAT RAIL CHANNEL AT APPROXIMATELY FS 409.00+80, AREAS MARKED. C-CHECK RO 11/21/2020. REPLACED SEAT RAIL AT RT APPROXIMATELY FS 409.00 +80, REF CRJ200-AMM.
- [SDR SWIA202054296](https://openairdocs.org/sdr/SWIA202054296.md): Seat Track · gouged · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SIDE SEAT RAIL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 409.00+16-409.00+112, AREAS MARKED. C-CHECK RO 11/21/2020. INSTALLED NEW SEAT TRACK AT RT SIDE FS 409.00 TO 428.00, REF CRJ200-AMM.
- [SDR SWIA202054295](https://openairdocs.org/sdr/SWIA202054295.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SIDE SEAT RAIL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 364.00-409.00+16, AREAS MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION DAMAGE ON SEAT TRACK AT FS 364-FS 409+16, REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REF CRJ 20
- [SDR SWIA202054294](https://openairdocs.org/sdr/SWIA202054294.md): Seat Track · worn · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLIGHT COMPARTMENT PILOT SEAT TRACK LOCK PINS ARE WORN. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW THE PILOTS SEAT TRACK LOCK PINS (2 EACH) AND SPRINGS (2 EACH), REF CRJ-200 CMM.
- [SDR SWIA202054293](https://openairdocs.org/sdr/SWIA202054293.md): Coaming · worn · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR COAMING WORN WITH A GROOVE ALONG BOTTOM OF THRESHOLD OF AIRCRAFT FS 574 TO FS 621. C-CHECK RO 11/21/2020. LOWER AFT CARGO DOOR COAMING REMOVED AND REPLACED WITH NEW, REF CRJ 200 SRM. OPERATIONAL TEST CHECKED GOOD. NO LEAKS NOTED.
- [SDR SWIA202054292](https://openairdocs.org/sdr/SWIA202054292.md): Frame · bent · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR MID FWD FS 574 TRACK FRAME ASSEMBLY ON AFT FACING SIDE BENT CORNER. C-CHECK RO 11/21/2020. REMOVED CRACKED CHANNEL P/N 601R35050-25 AT AFT CARGO DOOR TRACK ASSEMBLY FS 574, REF CRJ200 SRM. INSTALLED NEW CHANNEL PN 601R35050-25 AT CARGO DOOR FWD T
- [SDR SWIA202054291](https://openairdocs.org/sdr/SWIA202054291.md): Frame · gouged · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR UPPER FWD TRACK FRAME ASSEMBLY ON AFT FACING SIDE BENT AND GOUGED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW CARGO DOOR UPPER FWD TRACK ASSEMBLY, REF DWG AND CRJ 200 SRM.
- [SDR SWIA202054290](https://openairdocs.org/sdr/SWIA202054290.md): Bracket · cracked · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR FWD THREASHOLD STEP PLATE BRACKET CRACKED AND RIVET HEAD POPPED OFF. C-CHECK RO 11/21/2020. MODIFIED AFT CARGO DOOR FWD THRESHOLD STEP PLATE BRACKET, REF BOMBARDIER MODSUM.
- [SDR SWIA202054289](https://openairdocs.org/sdr/SWIA202054289.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559.80 TO FS 621, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW LBL 27 SEAT TRACK FROM APPROXIMATELY FS 559.80 TO FS 621, REF CRJ 200 AMM.
- [SDR SWIA202054288](https://openairdocs.org/sdr/SWIA202054288.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559+96 TO FS 621, MARKED. C-CHECK RO 11/21/2020. INSTALLED NEW SEAT TRACK AT LBL 9, FS 559+96 TO FS 621.00, REF CRJ200 AMM.
- [SDR SWIA202054287](https://openairdocs.org/sdr/SWIA202054287.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559.0 TO FS 559+88, MARKED. C-CHECK RO 11/21/2020. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW ONE AT APPROXIMATELY FS 559.0 TO 559+88, REF CRJ200 AMM.
- [SDR SWIA202054286](https://openairdocs.org/sdr/SWIA202054286.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559 +88 TO FS 559+95, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW SEAT TRACK FROM FS 559.00+88 TO FS 559.00+95, REF CRJ200 AMM.
- [SDR SWIA202054285](https://openairdocs.org/sdr/SWIA202054285.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559.+95 TO FS 610, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW ONE SEAT TRACK AT RBL 9 FS 559+ 95 TO FS 610, REF CRJ200-AMM.
- [SDR SWIA202054284](https://openairdocs.org/sdr/SWIA202054284.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 610 TO FS 621, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW ONE SEAT TRACK AT RBL 9 FS 559+112 TO FS 621 RBL 9, REF CRJ200-AMM.
- [SDR SWIA202054283](https://openairdocs.org/sdr/SWIA202054283.md): Floor Support · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR BEAM INBOARD LIP CORRODED FROM FS 605 TO 621, MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION FROM DISCREPANT AREA, REF CRJ200 SRM. FLOOR BEAM ORIGINAL THICKNESS.050, REMOVED.012, REMAINING.038 OUT OF LIMITS. REMOVED AND INSTALLED NEW FLOOR
- [SDR SWIA202054282](https://openairdocs.org/sdr/SWIA202054282.md): Plate · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage Main, Structure
  > MID CARGO HOLD DOWN PLATE CORRODED BETWEEN FRAMES 589.0 AND 605.0, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW MID CARGO HOLD DOWN PLATE BETWEEN FRAMES 589.0 AND 605.0 CRJ200 SRM.
- [SDR SWIA202054281](https://openairdocs.org/sdr/SWIA202054281.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT LBL 9 SEAT TRACK CORRODED FROM FS 559.0 TO FS 559+84, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED RAIL SEAT TRACK AT LT LBL 9 FS 559.0 TO FS 559+84, REF CRJ200-AMM.
- [SDR SWIA202054280](https://openairdocs.org/sdr/SWIA202054280.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE WALL SEAT RAIL HAS CORROSION FROM APPROXIMATELY FS 409.+128 TO FS 559.0+80, MARKED. C-CHECK RO 11/21/2020. REMOVED CORRODED LEFT-HAND SIDE WALL SEAT RAIL FROM FS 409+128 TO FS 559.0+80 AND INSTALLED NEW SIDE SEAT RAIL, REF CRJ200 AMM.
- [SDR SWIA202054279](https://openairdocs.org/sdr/SWIA202054279.md): Seat Track · corroded · Oct 13, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT RAIL STRUCTURE HAS CORROSION FROM APPROXIMATELY FS 409.0+128 AFT TO FS 559.0+80, MARKED. C-CHECK RO 11/21/2020. INSTALLED NEW SIDE SEAT TRACK CHANNEL AT LT FS.559.00+32 TO FS 559.00+80, REF CRJ200-AMM.
- [SDR SWIA202054278](https://openairdocs.org/sdr/SWIA202054278.md): Floorbeam · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LT FLOOR BEAM LBL 27 INBOARD LIP CORRODED AT APPROXIMATELY FS 409.48, MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION FROM LT FLOOR BEAM, IAW CRJ SRM. RESTORED FINISH, IAW CRJ SRM.
- [SDR SWIA202054277](https://openairdocs.org/sdr/SWIA202054277.md): Floor Support · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR BEAM INBOARD LIP CORRODED LBL 9 FROM FS 409.0 TO FS 409.128, MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION FROM DISCREPANT AREA, REF CRJ200 SRM. ORIGINAL THICKNESS OF FLOOR BEAM LIP.050, IAW CRJ 200 SRM. REMOVED.023 REMAINING OF.027 OUT OF L
- [SDR SWIA202054276](https://openairdocs.org/sdr/SWIA202054276.md): Floor Support · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR BEAM INBOARD LIP CORRODED RBL 9 FROM FS 409.0 TO FS 409.128, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW RT FLOORBEAM CAP FROM APPROXIMATELY FS 409 TO FS 409+128 RBL 9, REF REO SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA202054275](https://openairdocs.org/sdr/SWIA202054275.md): Anchor Fitting · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT ANCHOR FITTING, FS 349.00 IS CORRODED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW AFT PAX DOOR ANCHOR FITTING, REF CRJ 200 AMM.
- [SDR SWIA202054274](https://openairdocs.org/sdr/SWIA202054274.md): Anchor Fitting · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORWARD ANCHOR FITTING, FS 310.00 IS CORRODED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW FWD PAX DOOR ANCHOR FITTING, REF CRJ 200 AMM.
- [SDR SWIA202054273](https://openairdocs.org/sdr/SWIA202054273.md): Hinge · gouged · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE, FUSELAGE SIDE, LUG 15 IS GOUGED, MARKED. C-CHECK RO 11/21/2020. COMPLIED WITH REO: DISPOSITION FOR THE OUTER SURFACE OF LUGS. EVALUATED DAMAGE REMOVAL ON FUSELAGE SIDE OF PAX DOOR HINGE, MINIMUM ALLOWABLE REMAINING WALL THICKNESS ON OU
- [SDR SWIA202054272](https://openairdocs.org/sdr/SWIA202054272.md): Arm · chafed · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SUPPORT WHEEL ARM IS CHAFED, MARKED. C-CHECK RO 11/21/2020. CHAFED PASSENGER DOOR SUPPORT WHEEL ARM FOUND TO BE OUTSIDE ALLOWABLE DAMAGE LIMITS. DOOR SUPPORT WHEEL ARM MOVED AND REPLACED WITH NEW, REF CRJ200 AMM.
- [SDR SWIA202054271](https://openairdocs.org/sdr/SWIA202054271.md): Panel · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT UPPER WING PLANK LANDINGS FOR PANELS 640AT, 640BT, AND 640CT HAVE FRETTING CORROSION. C-CHECK RO 11/21/2020. REPAIRED RT UPPER WING PLANK LANDINGS FOR PANELS 640AT, 640BT, AND 640CT, REF MHIRJ REO.
- [SDR SWIA202054270](https://openairdocs.org/sdr/SWIA202054270.md): Panel · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LT UPPER WING PLANK LANDINGS FOR PANELS 540AT, 540BT, AND 540CT HAVE FRETTING CORROSION. C-CHECK RO 11/21/2020. REPAIRED LT UPPER WING PLANK LANDINGS FOR PANELS 540AT, 540BT, AND 540CT, REF MHIRJ REO.
- [SDR SWIA202054269](https://openairdocs.org/sdr/SWIA202054269.md): Bolt · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING MANIFOLD BANJO BOLTS APPEAR TO BE CORRODED, REF 1C TASK CARD. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW STEERING MANIFOLD BANJO BOLTS, REF CRJ200 AMM. LEAK AND FUNCTIONAL CHECKS GOOD.
- [SDR SWIA202054268](https://openairdocs.org/sdr/SWIA202054268.md): Doubler · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER MOUNT DOUBLER COMMON TO TAIL STINGER HAS CORRODED HARDWARE, MARKED. C-CHECK RO 11/21/2020. REPLACED WITH NEW BOLTS (2 EACH), NEW WASHERS (2 EACH) AND NEW NUTS (2 EACH) ON THE VERTICAL STAB MOUNT DOUBLER COMMON TO TAIL STINGER, REF CRJ-200
- [SDR SWIA202054267](https://openairdocs.org/sdr/SWIA202054267.md): Strap · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SUPPORT STRAP AT FS 559.0 CORRODED FROM LBL 27 TO LBL 45, MARKED. C-CHECK RO 11/21/2020. RECEIVED NEW SUPPORT STRAP P/N (601R31025-29). LOCATE AND DRILLED NEW STRAP CRJ200 SRM. INSTALLED NEW STRAP CRJ200 SRM. COMPLIED WITH TASK CARD, REF DWG.
- [SDR SWIA202054266](https://openairdocs.org/sdr/SWIA202054266.md): Strap · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT STRAP AT FS 559.0 CORRODED FROM RBL 27 TO RBL 45, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW FLOOR SUPPORT STRAP AT FS 559.0 RBL 27 TO RBL 45, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA202054265](https://openairdocs.org/sdr/SWIA202054265.md): Floor Support · corroded · Oct 12, 2020 · N441SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT PRESSURE FLOOR ANGLE CORRODED FROM FS 409.128 TO FS 559.0, MARKED. C-CHECK RO 11/21/2020. BLENDED CORROSION AND RESTORED FINISH 30 EA LOCATIONS ON LT PRESSURE FLOOR ANGLE FROM FS 409.128 TO FS 559.0, REF REO.
- [SDR SWIA202054264](https://openairdocs.org/sdr/SWIA202054264.md): Panel · cracked · Oct 10, 2020 · N441SW · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH TRIM PANEL (831AZ) TWO AFT MOUNTING SCREW HOLES ARE CRACKING, MARKED. C-CHECK RO 11/21/2020. REPAIRED CREW ESCAPE HATCH TRIM PANEL (831AZ) WHERE TWO AFT MOUNTING SCREW HOLES ARE CRACKING, MARKED BY USING SATTO REPAIR KIT PN: SA20-21 P/O W71

Next page: https://openairdocs.org/aircraft/N441SW/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 = 'N441SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N441SW/reports

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