# Service difficulty reports: N809CA, cancelled Nov 3, 2023

A list on [N809CA, cancelled Nov 3, 2023](https://openairdocs.org/deregistered/N809CA-2023-11-03.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 · 180 reports

- [SDR SWIA202266699](https://openairdocs.org/sdr/SWIA202266699.md): None · fault message · Oct 31, 2022 · N809CA · Cndair CL6002B19 · Smoke Detection
  > LEFT FIRE FAIL CAUTION MESSAGE CAME ON AND OFF TWICE INFLIGHT. PERFORMED QRH. (FLIGHT #5336 FILED CLOSED) T/S L/H FIRE FAIL CAUTION MSG, FOUND ENGINE NACELLE AND FIREWALL SENSING ELEMENT A END CONNECTOR DAMAGED. REMOVED AND REPLACED WIRING END CONNECTOR AS
- [SDR SWIA202265554](https://openairdocs.org/sdr/SWIA202265554.md): None · failed · May 3, 2022 · N809CA · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING MESSAGE. NOSE GEAR STUCK DOWN. RAN QRH AND ALL 3 GEARS CAME DOWN WITH THE MANUAL RELEASE HANDLE. (FLIGHT 5454 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24763990 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 247702
- [SDR SWIA2020033149779](https://openairdocs.org/sdr/SWIA2020033149779.md): Nut Plate · broken · Mar 10, 2020 · N809CA · Cndair CL6002B19 · Wing, Plate/Skin
  > PANEL 571LL ON L/H WING HAS ONE BROKEN NUTPLATE. (C CHECK) RO 3/27/2020 REMOVED BROKEN NUTPLATE AND INSTALLED NEW P/N NAS1789-3 NUTPLATE IAW CRJ 200 SRM.
- [SDR SWIA2020033149770](https://openairdocs.org/sdr/SWIA2020033149770.md): Fitting · broken · Feb 27, 2020 · N809CA · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING BROKEN. (C CHECK) RO 3/27/2020 REMOVED BROKEN AVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING. LOCATED AND DRILLED NEWAVIONICS BAY DOOR FWD R/H NYLON GUIDE FITTING REF. CRJ-200 [TR51-42] SRM. INSTALLATION PERFORM
- [SDR SWIA2020033049586](https://openairdocs.org/sdr/SWIA2020033049586.md): Angle · cracked · Feb 26, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *ANGLE ATTACHED TO TOP AFT EDGE OF FRAME AT FS 682 IS CRACKED BETWEEN STGR25R AND STGR26R. (C CHECK) RO 3/27/2020 REPAIRED ANGLE ATTACHED TO TOP AFT EDGE OF FRAME AT FS 682 BETWEEN STGR25R AND STGR26R PER BOMBARDIER REO COMPLIED WITH ALL STEP OF REO.
- [SDR SWIA2020033049584](https://openairdocs.org/sdr/SWIA2020033049584.md): Fitting · cracked · Feb 25, 2020 · N809CA · Cndair CL6002B19 · Flight Compartment Windows
  > *R/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED R/H WINDSHIELD SIDE POST FITTING REFERENCE CRJ 200 SRM AND DRAWING. COMPLIED WITH. SEE CONTINUATION FOR DETAILS.
- [SDR SWIA2020033049583](https://openairdocs.org/sdr/SWIA2020033049583.md): Fitting · cracked · Feb 25, 2020 · N809CA · Cndair CL6002B19 · Flight Compartment Windows
  > *L/H WINDSHIELD SIDE POST AFT LWR CLIP (FITTING) IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND REPLACED CRACKED L/H WINDSHEILD SIDE POST AFT LOWER FITTING WITH NEW FITTING. REF DRAWING AND CRJ 200 SRM. SEE CONTINUATION FOR DETAILS.
- [SDR SWIA2020033049582](https://openairdocs.org/sdr/SWIA2020033049582.md): Frame · cracked · Feb 24, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605.0 FRAME FLANGE LEFT HAND SIDE, JUST OVER AFT CARGO DOOR HAS SUSPECT CRACK AT RIVET LOCATION JUST ABOVE AND BELOW STR 9. (MARKED) (C CHECK) RO 3/27/2020 REPAIRED DAMAGE AREA AND COMPLIED WITH ALL STEPS OF BOMBARDIER REO. PRESSURE CHECK GOOD. SEE CONT
- [SDR SWIA2020033049581](https://openairdocs.org/sdr/SWIA2020033049581.md): Rib · damaged · Feb 20, 2020 · N809CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBOARD FLAP VANE LEADING EDGE INBOARD RIB REQUIRES REPLACEMENT (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AND RESTORED FINISH ON RH INBOARD FLAP VANE LEADING EDGE INBOARD RIB. REF: CRJ200 SRM. FOUND TO BE OUT OF LIMITS ON CAMP 20427303 JOB 2736661 OP
- [SDR SWIA2020033149753](https://openairdocs.org/sdr/SWIA2020033149753.md): Channel · corroded · Feb 19, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AVIONICS BAY DOOR POSITION SENSOR MOUNTING CHANNEL AT FS.364.00, STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM AVIONICS BAY DOOR POSITION SENSOR CHANNELS AT FS364.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED N
- [SDR SWIA2020033049580](https://openairdocs.org/sdr/SWIA2020033049580.md): Floor Skin · cracked · Feb 19, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PRESSURE FLOOR SKIN IS CRACKED AT 2EA LOCATIONS AT APPROX FS 461 BETWEEN BL0 AND LBL 9 AND BL0 TO RBL9. SUSPECT AREAS ARE MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REPAIRED PRESSURE FLOOR SKIN @ 2EA LOCATIONS AT APPROX FS.461.00 BETWEEN BL0 AN
- [SDR SWIA2020033049579](https://openairdocs.org/sdr/SWIA2020033049579.md): Frame Splice · corroded · Feb 19, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND ON UPPER SPLICE ANGLE FOR LOWER FRAME SECTOR AT FS.364.00 AND STGR 27. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION ON UPPER SPLICE ANGLE FOR LOWER FRAME SECTOR AT FS364.00 STGR 27 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NE
- [SDR SWIA2020033049578](https://openairdocs.org/sdr/SWIA2020033049578.md): Fitting · cracked · Feb 17, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *AFT LINTEL CLIP IS POSSIBLY CRACKED. FLAGGED (C CHECK) RO 3/27/2020 REMOVED AND REPLACED AFT LINTEL CLIP REF. CRJ-200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020033149764](https://openairdocs.org/sdr/SWIA2020033149764.md): Not Reported · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS559.00+80 €“ 559.00+112 STGR 26L €“ 26R CORROSION AROUND SEVERAL FASTENERS (MARKED) (C CHECK) RO 3/27/2020 REPAIRED CORROSION DAMAGE AT FS559+80 TO FS574 STGR25L TO STGR26R COMPLIED WITH ALL APPLICABLE STEPS OF BOMBARDIER REO. LEAK CHECK GOOD. SEE CO
- [SDR SWIA2020033149752](https://openairdocs.org/sdr/SWIA2020033149752.md): Floor Support · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO APPROX.€¦ FS.559.00+118 TO FS. 621.00 LEFT HAND LBL 27.00 FLOOR BEAM HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 COMPLIED WITH REO FOR THE REMOVAL OF CORROSION FROM FLOOR BEAM FS. 559.00+118 TO FS. 621.00 LBL 27.
- [SDR SWIA2020033149751](https://openairdocs.org/sdr/SWIA2020033149751.md): Hinge · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Rudder Structure
  > *RUDDER CENTER HINGE AREA, UPPER AND LOWER GROUND STUD AND HARDWARE ON RUDDER, CORRODED (MARKED, OUT OF SCOPE) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW RUDDER CENTER HINGE, UPPER AND LOWER GROUND STUD AND HARDWARE REF CRJ 200 AMM.
- [SDR SWIA2020033149750](https://openairdocs.org/sdr/SWIA2020033149750.md): Seat Track · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT RBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL9 FS409+128 TO FS559.00 REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK. REF: BOMBAR
- [SDR SWIA2020033149749](https://openairdocs.org/sdr/SWIA2020033149749.md): Seat Track · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT LBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORRODED SET TRACK LBL BETWEEN FS. 409.00+128 AND FS. 559.00 AND INSTALLED NEWLY FABRICATED SEAT TRACK IAW CRJ 200 AMM AND
- [SDR SWIA2020033149748](https://openairdocs.org/sdr/SWIA2020033149748.md): Stand Off · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * THE LH FLOOR SILL HAS 3EA ELECTRICAL STANDOFFS THAT ARE CORRODED BETWEEN FS409.00+64 TO FS409.00+80. (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED 3 EACH STAND OFFS PER REFERENCE CRJ 200 SRM.
- [SDR SWIA2020033049576](https://openairdocs.org/sdr/SWIA2020033049576.md): Bracket · cracked · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS621.00 - 625.30 STGR APPROX. 14R ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.30 STRINGER 14R AND INSTALLED NEW ANGLE BRACKET IAW CRJ 200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020033049575](https://openairdocs.org/sdr/SWIA2020033049575.md): Bracket · cracked · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS621.00 - 625.30 STGR APPROX. 14L ANGLE CRACKED (MARKED) (C CHECK) RO 3/27/2020 REMOVED CRACKED ANGLE BRACKET FROM FS. 625.3.0 STRINGER 14L AND INSTALLED NEW ANGLE BRACKET IAW CRJ 200 SRM. COMPLIED WITH TASK CARD.
- [SDR SWIA2020033049574](https://openairdocs.org/sdr/SWIA2020033049574.md): Frame · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT L/H FS 513 WL73 (FLOOR LEVEL) HAS SMALL AREA OF CORROSION. (C CHECK) RO 3/27/2020 REMOVED CORROSION ON FRAME @ FS.513 WL.73. FOUND TO BE OUT OF LIMITS. COMPLIED WITH ALL APPLICABLE STEPS OF REO. SEE CONTINUATION FOR FURTHER DETAILS.
- [SDR SWIA2020033049570](https://openairdocs.org/sdr/SWIA2020033049570.md): Door Sill · cracked · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FRAME FROM PAX DOOR UPPER SILL TO STGR 0 AT FS 333 IS CRACKED. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FRAME @ FS.333.00 FROM PAX DOOR UPPER SILL TO STRG 0 REF CRJ 200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD. SEE CO
- [SDR SWIA2020033049568](https://openairdocs.org/sdr/SWIA2020033049568.md): Intercostal · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON R/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND REINSTALLED A NEW INTERCOSTAL AT STRG 27 RH FROM FS.394.00 TO FS.409.00 REF CRJ 200 SRM AND BOMBARDIER DWG. PRESSURE CHECK GOOD. COMPLIED WIT
- [SDR SWIA2020033049566](https://openairdocs.org/sdr/SWIA2020033049566.md): Intercostal · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *CORROSION FOUND ON INTERCOSTAL AFT OF AVIONICS BAY DOOR ON L/H SIDE OF STGR27. (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW INTERCOSTAL AFT OF AVIONICS BAY DOOR ON THE LH SIDE OF STRG 27 REF BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH TASK CARD. P
- [SDR SWIA2020033049563](https://openairdocs.org/sdr/SWIA2020033049563.md): Stringer Clip · cracked · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FWD CABIN - APPROX.€¦ FS280.00 STGR 3 €“ STRINGER CLIP HAS SIGNS OF A CRACK AND WORKING RIVETS (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED A NEW FWD CABIN STRINGER CLIP ON RH STRG 3 @ FS.280.00 REF CRJ 200 SRM AND BOMBARDIER DWG.LEAK CHECK GOOD
- [SDR SWIA2020033049560](https://openairdocs.org/sdr/SWIA2020033049560.md): Panel · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE RH FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (MARKED) (C CHECK) RO 3/27/2020 BLENDED MULTIPLE AREAS OF CORROSION FROM R/H FLOOR SILL PANEL FROM FS. 409.00+128 TO FS. 559.00 IAW REO CRJ-200 SRM.
- [SDR SWIA2020033049559](https://openairdocs.org/sdr/SWIA2020033049559.md): Not Reported · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS559.00 STGR 26L €“ 26R HAS CORROSION ON FASTENERS AND AROUND THE FASTENERS(MARKED) (C CHECK) RO 3/27/2020 REPAIRED FS559.00 STR26L -26R REFERENCING REO. ALL STEPS COMPLIED WITH.
- [SDR SWIA2020033049556](https://openairdocs.org/sdr/SWIA2020033049556.md): Floorbeam · corroded · Feb 13, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE FLOORBEAM AT LBL9.00 FROM FS409.00 TO FS409.00+128 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM FLOOR BEAM AT LBL 9.00 FROM FS. 409.00 TO FS. 409.00+128 IAW REO ( SEE CONTINUATION CARD FOR DETAILS).
- [SDR SWIA2020033149776](https://openairdocs.org/sdr/SWIA2020033149776.md): Hinge Fitting · gouged · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Ailerons
  > *LH SPOILERON THIRD HINGE FITTING GOUGED ON THE OUTBD UPPER AFT EDGE (MARKED) (C CHECK) RO 3/27/2020 REMOVED GOUGE ON THE LH SPOILERON THIRD HINGE FITTING OUTBD UPPER AFT EDGE. FOUND TO BE OUT OF LIMITS. RECEIVED REO. FOUND TO BE IN LIMITS. COMPLIED WITH
- [SDR SWIA2020033149747](https://openairdocs.org/sdr/SWIA2020033149747.md): Seat Track · chafed · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS409 TO FS409+128 AT RBL9 (C CHECK) RO 3/27/2020 REPLACED SEAT RAIL FROM FS409 TO FS409+128 AT RBL9 WITH A NEW FABRICATED PART REF REO, SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020033149746](https://openairdocs.org/sdr/SWIA2020033149746.md): Seat Track · chafed · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *NUMEROUS AREAS OF CHAFEING, FRETTING, AND CORROSION ON SEAT RAIL FROM FS364 TO FS409 AT RBL9. (C CHECK) RO 3/27/2020 BLENDED SEAT TRACK AT RBL 9.00 FROM FS 364.00 TO FS 409.00. REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK. REF:
- [SDR SWIA2020033149745](https://openairdocs.org/sdr/SWIA2020033149745.md): Fastener · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *RH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACH POINT AT RH SPOILERON OUTBOARD PCU REF CRJ200 AMM. OPS TEST GOOD, SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149744](https://openairdocs.org/sdr/SWIA2020033149744.md): Fastener · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *RH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON BOTTOM ATTACHING OINTS ON RH FLIGHT SPOILER PCU REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149743](https://openairdocs.org/sdr/SWIA2020033149743.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *RH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE HARDWARE WITH NEW ON THE RH SPOILERON HINGE ATTACH POINTS. REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149742](https://openairdocs.org/sdr/SWIA2020033149742.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *RH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON RH FLIGHT SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149741](https://openairdocs.org/sdr/SWIA2020033149741.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *RH OUTBD GROUND SPOILER INBD/OUTBD HINGE ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED THE ATTACHING HARDWARE ON THE RIGHT OUTBOARD GROUND SPOILER HINGES, REF CRJ 200 AMM. OPERATIONAL TEST OF GROUND SPOILERS CHECKED G
- [SDR SWIA2020033149740](https://openairdocs.org/sdr/SWIA2020033149740.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *RH INBD GROUND SPOILER OUTBD HINGE ATTACH HARDWARE NUT CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND REPLACED HARDWARE OF THE RH INBOARD GROUND SPOILER OUTBOARD HINGE WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST OF THE GROUND SPOILERS CHECKED GOOD.
- [SDR SWIA2020033149739](https://openairdocs.org/sdr/SWIA2020033149739.md): Fastener · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *LH SPOILERON BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE ON LH INBOARD SPOILER PCU BOTTOM ATTACH POINT REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149738](https://openairdocs.org/sdr/SWIA2020033149738.md): Fastener · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *LH FLIGHT SPOILER BOTH PCU, BOTTOM ATTACH HARDWARE CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE AT BOTTOM ATTACHING POINTS OF THE LH FLIGHT SPOILER PCU'S REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149737](https://openairdocs.org/sdr/SWIA2020033149737.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *LH SPOILERON HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH SPOILERON END HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149736](https://openairdocs.org/sdr/SWIA2020033149736.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *LH FLIGHT SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 LEFT FLIGHT SPOILER CENTER HINGES HARDWARE REMOVED AND REPLACED WITH NEW, REF CRJ 200 AMM. OPERATIONAL TEST CHECKED GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149735](https://openairdocs.org/sdr/SWIA2020033149735.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *LH OUTBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH OUTBOARD GROUND SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033149734](https://openairdocs.org/sdr/SWIA2020033149734.md): Nut · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Spoilers
  > *LH INBD GROUND SPOILER HINGES ATTACH HARDWARE NUTS CORRODED (MARKED) (C CHECK) RO 3/27/2020 REMOVED AND INSTALLED NEW HARDWARE (NUTS) ON LH INBOARD GROUND SPOILER HINGES REF CRJ200 AMM. OPS TEST GOOD. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020033049554](https://openairdocs.org/sdr/SWIA2020033049554.md): Frame · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT CARGO APPROX.€¦ FS.574.00 LEFT HAND STGR 25 TO STGR 18 - FRAME HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CARGO APPROX FS574.00 LEFT HAND STGR25 TO STGR18 FRAME REF CRJ 200 SRM AND BOMBARDIER DWG LEAK TEST GOOD. SEE C
- [SDR SWIA2020033049553](https://openairdocs.org/sdr/SWIA2020033049553.md): Door Sill · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *R/H FLOOR SILL HAS 4EA AREAS OF CORROSION BETWEEN FS310 AND FS319.70. AREAS MARKED WITH RED GREASE PENCIL. (C CHECK) RO 3/27/2020 REMOVED AND REPLACE RH FLOOR SILL BETWEEN FS310 AND FS319.70 REF DWG 601R31148 REV Y. SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA2020033049551](https://openairdocs.org/sdr/SWIA2020033049551.md): Door Sill · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CABIN APPROX. FS 559.00 TO 559.00 +96 RIGHT HAND FLOOR SILL BL 42.90 HAS NUMEROUS SPOTS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPROX FS559.00 TO FS559.00+16 RIGHT HAND FLOOR SILL INTERCOSTAL BL42.90 REF BOMBARDIER DWG, CRJ 20
- [SDR SWIA2020033049550](https://openairdocs.org/sdr/SWIA2020033049550.md): Strap · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CABIN APPROX. FS 559.00 RIGHT HAND RBL 42.90 TO RBL27.00- INTERCOSTAL STRAP HAS SIGNS OF CORROSION (MARKED) (C CHECK) RO 3/27/2020 REPLACED AFT CABIN APPROX FS559.00 RIGHT HAND RBL 42.90 INTERCOSTAL STRAP WITH NEW REF BOMBARDIER DWG, CRJ 200 SRM. SEE C
- [SDR SWIA2020033049548](https://openairdocs.org/sdr/SWIA2020033049548.md): Plate · corroded · Feb 12, 2020 · N809CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE PLATE UNDER THE TRANSMITTER ANTENNA NO.2 HAS CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM PLATE UNDER TRANSMITTER ANTENNA #2 REF CRJ 200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW PLATE UNDER THE TRANSMITTER ANTEN
- [SDR SWIA2020033149772](https://openairdocs.org/sdr/SWIA2020033149772.md): Trim Panel · cracked · Feb 11, 2020 · N809CA · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH TRIM ASSY CRACKED IN SEVERAL AREAS (C CHECK) RO 3/27/2020 REPAIRED THE CREW ESCAPE HATCH TRIM ASSEMBLY USING PO# 24268 PER BOMBARDIER REO.

Next page: https://openairdocs.org/deregistered/N809CA-2023-11-03/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 = 'N809CA' AND deregistration_id = 'N809CA-2023-11-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N809CA-2023-11-03/reports

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