# Service difficulty reports: N440SW

A list on [N440SW](https://openairdocs.org/aircraft/N440SW.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 · 245 reports

- [SDR SWIA202163089](https://openairdocs.org/sdr/SWIA202163089.md): None · damaged · Dec 13, 2021 · N440SW · Cndair CL6002B19 · Window/Windshield System
  > D: RECEIVED R WSHLD HEAT CAUTION AFTER TAKEOFF. QRH DID NOT CLEAR THE MESSAGE. / C: 30-41-1A / CAT: 'C' DUE 12/19/21 / ***RH WS HEAT FAILED A/C PRESSURIZATION CHECK AT DELTA P 2.5*** / CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 799677 / RECEIVED R
- [SDR SWIA202054875](https://openairdocs.org/sdr/SWIA202054875.md): Fire Warning · false activation · Dec 29, 2020 · N440SW · Cndair CL6002B19 · Smoke Detection
  > RECEIVED THE SMOKE TOILET CAUTION MESSAGE DESCENDING THROUGH FL200. FA DID NOT SEE OR SMELL SMOKE IN THE LAVATORY, BUT THE ALARM COULD BE HEARD. COMPLIED WITH QRH AND DE-ENERGIZED THE CIRCUIT BREAKERS IN THE QRH. RECEIVED THE AC SERV BUS CAUTION MESSAGE AFT
- [SDR SWIA202053965](https://openairdocs.org/sdr/SWIA202053965.md): Warning Message · illuminated · Nov 16, 2020 · N440SW · Cndair CL6002B19 · Cabin Pressure Control System
  > ON THE CLIMB, PASSING THROUGH 14000 FEET, GOT AN CABIN ALT CAUTION MESSAGE, THEN PROCEED CLIMB TO 17000 FEET THEN GOT CABIN ALT WARNING MESSAGE. FOLLOWED BY DOING QRC AND QRH. THEN CABIN AUTOMATICALLY DEPLOYED OXYGEN MASKS. FOUND MEL MX ACTION TO HAVE BEEN
- [SDR SWIA2020030348969](https://openairdocs.org/sdr/SWIA2020030348969.md): Cap · chafed · Feb 19, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge Flaps
  > ADDITIONAL CHAFING FOUND ON LH INBOARD FLAP, INBOARD FLAP VANE CAP (C-CHECK) RO 2/28/2020 REMOVED CHAFFED LH INBOARD FLAP, INBOARD FLAP VANE CAP AND INSTALLED NEW LH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR
- [SDR SWIA2020030348974](https://openairdocs.org/sdr/SWIA2020030348974.md): Stop Fitting · cracked · Feb 16, 2020 · N440SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD UPPER STOP FITTING IS CRACKED (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED CARGO DOOR FWD UPPER STOP FITTING WITH A NEW FITTING P/N CC670-38706-3. WET INSTALLED NEW FITTING WITH NEW FASTENERS. REF CRJ 200 SRM.
- [SDR SWIA2020030348968](https://openairdocs.org/sdr/SWIA2020030348968.md): Cap · damaged · Feb 2, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE LH INBD FLAP CENTER OTBD LEADING EDGE VANE CAP (C-CHECK) RO 2/28/2020 BLENDED LH INBD FLAP CENTER OTBD LEADING EDGE VANE CAP REF CRJ200 SRM. ORIGINAL THICKESS 0.050", REMAINING THICKNESS 0.00", 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS. REPLAC
- [SDR SWIA2020030348967](https://openairdocs.org/sdr/SWIA2020030348967.md): Frame · corroded · Jan 29, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FS349.00 FRAME LOWER FLANGE FROM 25L TO 25R (C-CHECK) RO 2/28/2020 REPLACED FRAME SECTION PN:601R32005-69 AT FS349 REF DWG, CRJ200 SRM. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020030348966](https://openairdocs.org/sdr/SWIA2020030348966.md): Angle · cracked · Jan 28, 2020 · N440SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH BATT RIB CAP ANGLE CRACKED AT WS48.30 (P/N 600-10389-2) (C-CHECK) RO 2/28/2020 REMOVED CRACKED AND INSTALLED NEW R/H BATT RIB CAP ANGLE AT WS48.30. REF CRJ-200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020030348965](https://openairdocs.org/sdr/SWIA2020030348965.md): Rib · cracked · Jan 23, 2020 · N440SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH BATT RIB @ WS 53.60 CRACKED (UPPER AFT CORNER). (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED THE RH BATT RIB @ WS 53.60 (P/N 601R10203-28) REF DWG, CRJ200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020030348964](https://openairdocs.org/sdr/SWIA2020030348964.md): Rib · cracked · Jan 23, 2020 · N440SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LH BATT RIB @WS 53.60 CRACKED (UPPER AFT CORNER). (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED DAMAGED BATT RIBB ASSY @ LH WS 53.60 REF DWG, CRJ200 SRM AND CRJ200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020030348963](https://openairdocs.org/sdr/SWIA2020030348963.md): Casting · damaged · Jan 22, 2020 · N440SW · Cndair CL6002B19 · Elevator Miscellaneous Structure
  > R/H ELEVATOR MOST OUTBOARD PCU LOCATION HAS IN VICINITY OF SHEAR PIN (DAMAGE) TO SHEAR PIN CASTING.TOOL DAMAGE. (C-CHECK) RO 2/28/2020 THE MOST OUBD PCU LOCATION ON THE R/H ELEVATOR IN THE VICINITY OF THE SHEAR PIN ON THE SHEAR PIN CASTING WAS BLENDED AND
- [SDR SWIA2020030348962](https://openairdocs.org/sdr/SWIA2020030348962.md): Skin · corroded · Jan 21, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > *FS 559.00+32 TO 559.00+80 STR 26LH TO 26RH HAS CORROSION ON EXTERNAL AIRCRAFT SKIN AND FASTENER. (C-CHECK) RO 2/28/2020 COMPLIED WITH PERMENANT REPAIR REO. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020030348961](https://openairdocs.org/sdr/SWIA2020030348961.md): Retainer · chafed · Jan 20, 2020 · N440SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > *CARGO DOOR UPPER FORWARD SEAL RETAINER CHAFED.(INSIDE VIEW MARKED (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED CARGO DOOR UPPER FORWARD SEAL RETAINER WITH A NEW SEAL RETAINER REF DWG AND CRJ-200 SRM SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020030348960](https://openairdocs.org/sdr/SWIA2020030348960.md): Stringer · cracked · Jan 20, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > *PASSENGER CABIN STGR3 L/H AT FS379.0 CRACKED. (MARKED) (C-CHECK) RO 2/28/2020 REPAIRED PASSENGER CABIN STGR3 L/H AT FS379.0 REF CRJ200 SRM. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.
- [SDR SWIA2020030348959](https://openairdocs.org/sdr/SWIA2020030348959.md): Angle · corroded · Jan 19, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CORROSION ON ANGLE ON THE FORWARD SIDE OF FRAME FS394.00, STGR25L - STGR25R. (C-CHECK) RO 2/28/2020 ORDERED AND RECIEVED NEW ANGLE PN: 601R32011-45. REMOVED AND INSTALLED NEW ANGLE REF SRM, DWG, CRJ200 SRM. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK
- [SDR SWIA2020030348958](https://openairdocs.org/sdr/SWIA2020030348958.md): Floorbeam · corroded · Jan 17, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH FLOOR BEAM FS 621-574 LH BL 27 APPROX AS MARKED CORROSION AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 REMOVED CORRODED AND INSTALLED NEW LBL27 CARGO BEAM CAP FS621 TO FS569 AND ENSUSURED ALL OTHER REQUIREMENTS WERE MET REF BOMBARDIER REO, CRJ200 S
- [SDR SWIA2020030348957](https://openairdocs.org/sdr/SWIA2020030348957.md): Casting · cracked · Jan 17, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RBL 9.0 AT FS 460 CASTING HAS CRACK AT UPPER RADIUS.(MARKED) FLOOR SUPPORT STRUCTURE. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED RBL 9.0 AT FS 460 CASTING REF DWG, AND BOMBARDIER. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.
- [SDR SWIA2020030348956](https://openairdocs.org/sdr/SWIA2020030348956.md): Floorbeam · cracked · Jan 17, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RH FLOOR BEAM FS 621-574 RH BL 27 APPROX AS MARKED CORROSION AND CRACKING AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW FLOOR BEAM CAP AT RBL 27 BETWEEN FS 574 - FS 621 REF BOMBARDIER DWG, BOMBARDIER REO, CRJ200 SRM. COMPLIED W
- [SDR SWIA2020030348955](https://openairdocs.org/sdr/SWIA2020030348955.md): Floorbeam · corroded · Jan 17, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH FLOORBEAM HAS CORROSION OUTBOARD SIDE AROUND NUT PLATE FS 605 LH BL 9 APPROX AS MARKED (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM LH FLOORBEAM OUTBOARD SIDE AROUND NUTPLATE FS 605 LH BL 9 REF CRJ200 SRM, BLENDED AREA FOUND TO BE OUT OF LIMITS REF BOM
- [SDR SWIA2020030348954](https://openairdocs.org/sdr/SWIA2020030348954.md): Floorbeam · corroded · Jan 17, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LH FLANGE OF FLOOR BEAM FS 574-559+80 LH BL 27 APPROX AS MARKED CORROSION AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED FLOOR BEAM CAP AND 2EA WEB REPAIR PARTS AT LBL 27 BETWEEN FS 574 AND FS 559+80 REF CRJ200 SRM. RESTORED FINISH A
- [SDR SWIA2020030348994](https://openairdocs.org/sdr/SWIA2020030348994.md): Seat Track · damaged · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *LEFT SIDE SEAT RAIL IS DAMAGED FS449.85 - FS499.00. (MARKED) (C-CHECK) RO 2/28/2020 BLENDED OUT DAMAGE ON LH SIDE SEAT RAIL FS449.85-499.00 REF CRJ200 (TR51-44) SRM. SIDE SEAT RAIL IS OUT OF LIMITS. NO ALLOWABLE DAMAGE TO SIDE SEAT RAIL. REF CRJ200 SRM. I
- [SDR SWIA2020030348953](https://openairdocs.org/sdr/SWIA2020030348953.md): Angle · cracked · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > *RH MLG WELL BATT RIB AT APPROXIMATELY WS53.00 RH POSSIBLE CRACK UPPER SMALL ANGLE (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED RH MLG WELL BATT RIB ANGLE AT APPROX. WS 53.00 (P/N 601R10202-25) REF DWG, CRJ200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020030348952](https://openairdocs.org/sdr/SWIA2020030348952.md): Angle · cracked · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > *LH MLG WELL BATT RIB AT APPROXIMATELY WS53.00 LH POSSIBLE CRACK UPPER SMALL ANGLE ON FWD SIDE (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED DAMAGED ANGLE AT APPROXIMATELY LH WS53.00 REF DWG AND CRJ200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020030348951](https://openairdocs.org/sdr/SWIA2020030348951.md): Floor Skin · cracked · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PRESSURE FLOOR SKIN CRACKED AFT OF INTERCOSTAL FS461.00 BETWEEN BODYLINE ZERO AND LBL9. (C-CHECK) RO 2/28/2020 REPAIRED PRESSURE FLOOR SKIN AFT OF INTERCOSTAL FS461.00 BETWEEN BL0.0 AND LBL9 REF REO. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.
- [SDR SWIA2020030348950](https://openairdocs.org/sdr/SWIA2020030348950.md): Fitting · cracked · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *INBOARD AND OUTBOARD CLIPS ON THE PULLEY BRACKET ARE CRACKED. FS484.00 RBL27 €“ RBL36. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED INBOARD AND OUTBOARD ANGLES ON INTERCOSTAL AT FS484. REF: BOMBARDIER REO, CRJ200 SRM AND DWG. PRESSURE CHECKE
- [SDR SWIA2020030348949](https://openairdocs.org/sdr/SWIA2020030348949.md): Fitting · cracked · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *INBOARD AND OUTBOARD CLIPS ON THE PULLEY BRACKET ARE CRACKED. FS484.00 LBL27 €“ LBL36. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED BOTH I/B & O/B CLIPS FS484.00 LBL27 €“ LBL36 REF REO. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.
- [SDR SWIA2020030348948](https://openairdocs.org/sdr/SWIA2020030348948.md): Seat Track · damaged · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *LEFT SIDE SEAT RAIL IS DAMAGED FS559.00+2 -559.00+80. (C-CHECK) RO 2/28/2020 BLEDNED OUT DAMAGE ON LH SIDE SEAT RAIL FROM FS559.00+2 TO FS559.00+80 REF CRJ200 SRM. MATERAIL LOSS IS NOT ALLOWABLE DAMAGE TO SIDE SEAT RAIL. REF CRJ200 SRM. FABRICATED NEW L/
- [SDR SWIA2020030348947](https://openairdocs.org/sdr/SWIA2020030348947.md): Beam · corroded · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *FS280.00 BEAM UPPER FLANGE IS CORRODED BETWEEN LBL9 & RBL9. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM FS280.00 BEAM UPPER FLANGE BETWEEN LBL9 & RBL9 REF CRJ200 SRM, UPPER FLANGE FOUND TO BE OUT OF LIMITS, REF CRJ200 SRM AND BOMBARDIER REO, CO
- [SDR SWIA2020030348946](https://openairdocs.org/sdr/SWIA2020030348946.md): Skin · corroded · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > *FS 559.00+112 TO 574 STR 25 LH TO 25 RH EXTERNAL SKIN AND FASTENERS HAS CORROSION AS MARKED (C-CHECK) RO 2/28/2020 REPAIRED EXTERNAL SKIN FS 559.00+112 TO 574 STR 25L TO 25R REF REO. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020030348945](https://openairdocs.org/sdr/SWIA2020030348945.md): Skin · corroded · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > * FS 559.00 +80 TO 559.00+112 STR 26RH TO 26LH EXTERNAL AIRCRAFT SKIN AND FASTENERS HAS CORROSION IN AREA (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND REPAIR TO CORROSION ON FS 559.00 +80 TO 559.00+112 STR 26RH TO 26LH EXTERNAL AIRCRAFT SKIN AND FAS
- [SDR SWIA2020030348944](https://openairdocs.org/sdr/SWIA2020030348944.md): Fitting · cracked · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS280.00 RBL9 - CLIP ON THE INSIDE OF THE FLOOR BEAM IS CRACKED. (C-CHECK) RO 2/28/2020 FABRICATED AND INSTALLED INBOARD CLIP AT FS280.00 RBL 9. REF CRJ200 SRM AND PREVIOUSLY INCORPERATED BOMBARDIER REO, FOR FAB AND INSTALL. COMPLIED WITH TASK CARD.
- [SDR SWIA2020030348943](https://openairdocs.org/sdr/SWIA2020030348943.md): Fitting · cracked · Jan 15, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS280.00 LBL9 - CLIP ON THE INSIDE OF THE FLOOR BEAM IS CRACKED. (C-CHECK) RO 2/28/2020 REMOVED CRACKED CLIP AND INSTALLED FABRICATED CLIP AT FS280.00 LBL9 ON THE INSIDE OF THE FLOOR BEAM. REF CRJ200 SRM AND BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAI
- [SDR SWIA2020030348985](https://openairdocs.org/sdr/SWIA2020030348985.md): Seat Track · corroded · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAILS FS 559+80-621 LH BL 27 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACKS REF CRJ 200 AMM. SEE CONTINUATION FOR DETAILS. SEAT TRACK FABRICATED ON MX 20291524
- [SDR SWIA2020030348984](https://openairdocs.org/sdr/SWIA2020030348984.md): Seat Track · corroded · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAILS FS 559+80-621 LH BL 9 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACKS REF CRJ 200 AMM AND CRJ 200 REO. SEE CONTINUATION FOR DETAILS. SEAT TRACK FABRICATED ON MX 20291533
- [SDR SWIA2020030348942](https://openairdocs.org/sdr/SWIA2020030348942.md): Support Angle · cracked · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RIGHT WINDSHIELD SIDE POST SUPPORT ANGLE CRACKED MARKED (C-CHECK) RO 2/28/2020.REMOVED AND REPLACED THE RH WINDSHIELD SIDE POST SUPPORT ANGLE REF CRJ-200 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECKED GOOD, NO LEAKS NOTED.
- [SDR SWIA2020030348941](https://openairdocs.org/sdr/SWIA2020030348941.md): Fitting · cracked · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FOUND CRACK AT WINDSHIELD CTR POST, RH CLIP. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CRACKED RH CLIP FROM WINDSHIELD CTR POST AND INSTALLED NEW REPLACEMENT REF CRJ200 SRM.COMPLIED WITH TASK CARD.
- [SDR SWIA2020030348940](https://openairdocs.org/sdr/SWIA2020030348940.md): Strap · corroded · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT STRAP 559 AS MARKED HAS CORROSION. (C-CHECK) RO 2/28/2020 REPLACED LH FLOOR SUPPORT STRAP AT FS559 BETWEEN LBL36 REF CRJ200 SRM AND DWG. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA2020030348939](https://openairdocs.org/sdr/SWIA2020030348939.md): Frame · corroded · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 605 HAS SPOTS OF CORROSION STR 20L TO STR20R. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED THE FS605.00 FRAME SECTOR REF CRJ 200 SRM. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.
- [SDR SWIA2020030348938](https://openairdocs.org/sdr/SWIA2020030348938.md): Seat Track · corroded · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAILS FS 559+80-621 RH BL 9 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND REINSTALL NEWLY FABRICATED SEAT TRACK FS 559+80-621 RH BL 9. REF CRJ 200 AMM. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020030348937](https://openairdocs.org/sdr/SWIA2020030348937.md): Seat Track · corroded · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAILS FS 559+80-621 RH BL 27 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND REINSTALLED NEWLY FABRICATED SEAT TRACKS FS 559+80-621 RH BL 27. REF CRJ 200 AMM. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020030348936](https://openairdocs.org/sdr/SWIA2020030348936.md): Door Sill · corroded · Jan 14, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH SILL EDGE MEMBER FS621-574 APPROX AS MARKED HAS CORROSION AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 BLENDED OUT CORROSION ON R/H FLOOR SILL MEMBER AT FS574 TO FS621, ORIGINAL PART THICKNESS =.050", MATERIAL REMOVED =.011",MATERIAL REMAINING =.
- [SDR SWIA2020030348935](https://openairdocs.org/sdr/SWIA2020030348935.md): Doubler · corroded · Jan 13, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * THE RH FLOOR SILL PANEL AND ITS PREVIOUS REPAIR DOUBLERS, BETWEEN FS 409+128 AND FS 559, HAVE MULTIPLE SPOTS OF CORROSION. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK) RO 2/28/2020 BLENDED AND REPAIRED CORROSION ON THE RH FLOOR SILL BETWEEN FS 409+128 AND
- [SDR SWIA2020030348934](https://openairdocs.org/sdr/SWIA2020030348934.md): Angle · corroded · Jan 13, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * THE RH FLOOR ANGLE, BETWEEN FS 409+128 AND FS 559, HAS MULTIPLE SPOTS OF CORROSION. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK) RO 2/28/2020 COMPLIED WITH PERMENANT REPAIR REO. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD, ALL CHECKS GOOD.
- [SDR SWIA2020030348933](https://openairdocs.org/sdr/SWIA2020030348933.md): Door Sill · corroded · Jan 13, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * THE LH FLOOR SILL PANEL AND ITS PREVIOUS REPAIR DOUBLERS, BETWEEN FS 409+128 AND FS 559, HAVE MULTIPLE SPOTS OF CORROSION. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK) RO 2/28/2020 REPAIRED THE L/H FLOOR SILL PANEL AND PREVIOUS REPAIR DOUBLERS BETWEEN FS4
- [SDR SWIA2020030348973](https://openairdocs.org/sdr/SWIA2020030348973.md): Attach Angle · cracked · Jan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > * FS 193 FRAME ATTACH ANGLE HAS A SUSPECTED CRACK ON THE LH SIDE, THE ANGLE ATTACHES TO THE FWD SIDE OF THE FRAME AND TO THE TRU BAY FLOOR PANEL. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED FS193.00 LH FRAME ATTACH CLIP. REF
- [SDR SWIA2020030348972](https://openairdocs.org/sdr/SWIA2020030348972.md): Drag Angle · cracked · Jan 10, 2020 · N440SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * THE PASSENGER DOOR'S AFT STAIR WEB DRAG ANGLE HAS A SUSPECTED CRACK NEAR THE PULLEY BRACKET. (C-CHECK) RO 2/28/2020 REMOVED CRACKED ANGLE AND INSTALL NEW PASSENGER DOOR'S AFT STAIR WEB DRAG ANGLE NEAR THE PULLEY BRACKET. REF CRJ200 SRM. SEE CONTINUATION
- [SDR SWIA2020030348971](https://openairdocs.org/sdr/SWIA2020030348971.md): Bracket · cracked · Jan 10, 2020 · N440SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > *NLG DOOR ACTUATOR BRACKET CRACKED AT THE LWR FWD CORNER (MARKED) (C-CHECK) RO 2/28/2020 INSTALLED NEW NLG DOOR ACTUATOR BRACKET, REF. CRJ200 SRM, LEAK CHECK GOOD, NO LEAKS FOUND AT THIS TIME, RIGGING GOOD AT LTHIS TIME, FUNCTIONAL TEST GOOD AT THIS TIME.
- [SDR SWIA2020030348970](https://openairdocs.org/sdr/SWIA2020030348970.md): Stiffener · cracked · Jan 10, 2020 · N440SW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > *RH ENG EXHAUST FAIRING SECOND STIFFENER CRACKED OUTBD LWR SIDE (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED SRS042 DOUBLER REPAIR ON RH ENGINE EXHAUST FAIRING STIFFENER ON OUTBOARD LOWER SIDE REF BOMBARDIER PART#228-50181 CMM. CUT OUT NEW DOUBLER PIECE FROM
- [SDR SWIA2020030348932](https://openairdocs.org/sdr/SWIA2020030348932.md): Attach Fitting · cracked · Jan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > * THE RH WINDSHIELD SIDE POST'S LOWER AFT ATTACH FITTING HAS A SUSPECTED CRACK IN ITS RADIUS. (MARKED WITH RED SHARPIE) (C-CHECK) RO 2/28/2020 REMOVED CRACKED RH WINDSHIELD SIDE POST'S LOWER AFT ATTACH FITTING AND INSTALLED NEW REPLACEMENT P/N: 601R33235-4
- [SDR SWIA2020030348931](https://openairdocs.org/sdr/SWIA2020030348931.md): Attach Fitting · cracked · Jan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > * THE LH WINDSHIELD SIDE POST'S LOWER AFT ATTACH FITTING HAS A SUSPECTED CRACK IN ITS RADIUS. (MARKED WITH RED SHARPIE) (C-CHECK) RO 2/28/2020 REMOVED FITTING AT THE LH WINDSHIELD SIDE POST'S LOWER AFT, LOCATED, DRILLED AND FIT CHECK NEW FITTING REF CRJ200

Next page: https://openairdocs.org/aircraft/N440SW/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 = 'N440SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N440SW/reports

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