# Service difficulty reports: N471CA

A list on [N471CA](https://openairdocs.org/aircraft/N471CA.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 · 228 reports

- [SDR SWIA2025103000020](https://openairdocs.org/sdr/SWIA2025103000020.md): Bracket · cracked · Oct 20, 2025 · N471CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR, AFT COUNTER BALANCE BRACKET CRACKED AROUND MOUNTING BOLT (FILED CLOSED)REMOVED AND REPLACED AFT CARGO DOOR, AFT COUNTER BALANCE BRACKET IN REFERENCE TO CRJ200 SRM 51-42-06 AND MHI DWG 601R355055 REV.-T. SEE CP #31094541 FOR PRESSURIZATION/LEA
- [SDR SWIA2025102100000](https://openairdocs.org/sdr/SWIA2025102100000.md): Bracket · cracked · Oct 20, 2025 · N471CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR, AFT COUNTER BALANCE BRACKET CRACKED AROUND MOUNTING BOLT (FILED OPEN)
- [SDR SWIA2025100300019](https://openairdocs.org/sdr/SWIA2025100300019.md): Track · gouged · Oct 19, 2025 · N471CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT TRACK NEAR THE MID SECTION HAS DEEP GOUGED AND DAMAGE TO IT ALONG WITH BEING WORN DUE TO AFT CARGO DOOR REPEATEDLY COMING OFF THE TRACKS. REMOVED AND REPLACED CARGO DOOR AFT TRACK IN REFERENCE TO SRM 51-42-06, DWG 601R36008 REV. BC, AND DWG
- [SDR SWIA2025082900008](https://openairdocs.org/sdr/SWIA2025082900008.md): Control Unit · faulted · Aug 28, 2025 · N471CA · Cndair CL6002B19 · Compressor Bleed Valve
  > L 14TH DUCT WARNING DURING CLIMB OUT OF DENVER. QRH RAN AND MESSAGE CLEARED. (FLIGHT 4679 - FILED CLOSED)TROUBLESHOT L WING 14TH DUCT MESSAGE PER CRJ 200 FIM 36-20-00 FIGURE 103. PERFORMED GVI OF LH 10TH AND 14TH STAGE DUCTING AND LEAK DETECTION SYSTEM IN ARE
- [SDR SWIA202508050002](https://openairdocs.org/sdr/SWIA202508050002.md): Skin · dented · May 8, 2025 · N471CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT AT FS295 STGR 26 L/H. DENT BETWEEN FS 280.00-FS295.00 STGR 26 L/H. REPAIR PERFORMED USING FILLER AND DOUBLER MATERIAL #.063 SHEETMETAL 2024T3 LOT# LT20-00865 IAW MHIRJ REO 601R-53-21-3753. TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025080500007](https://openairdocs.org/sdr/SWIA2025080500007.md): Structure · damaged · May 7, 2025 · N471CA · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WING I/B HINGE BOX HAS DAMAGE. AFT SIDE. BLENDED- OUT LIGHT DAMAGE ON LEFT WING I/B HINGE BOX AND FOUND TO BE WITHIN LIMITS. NDT NOTED NO DISCREPANCIES REFERENCE TAILWIND INSPECTION INC WO NO. 14350-2837. APPLIED CADMIUM PLATE AND PRIMER ON REWORKED AREA
- [SDR SWIA2025080500430](https://openairdocs.org/sdr/SWIA2025080500430.md): Seat Track · gouged · Apr 30, 2025 · N471CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLIGHT COMPARTMENT FLOOR SEAT RAILS RH HAS GOUGES COMPLIED WITH REO 601R-53-11-1093 REV -B FOR TEMP REPAIR OF THE FLIGHT COMPARTMENT R/H FLOOR SEAT RAILS TASK CARD 51-900-1002-SKY.
- [SDR SWIA202412160013](https://openairdocs.org/sdr/SWIA202412160013.md): Selector Valve · faulted · Dec 13, 2024 · N471CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON SHORT FINAL GEAR DISAGREE AND NOSE DOOR OPEN. QRH FIXED IT. (FLIGHT 5472 - FILED CLOSED) REMOVE AND REPLACED NLG SELECTOR VALVE PER CRJ 200 AMM 32-33-10. PERFORMED LANDING GEAR EXTENSION AND RETRACTION OPS CHECK PER CRJ 200 AMM 32-30-00 OPS CHECK GOOD
- [SDR SWIA2024120001323](https://openairdocs.org/sdr/SWIA2024120001323.md): Duct · warning message · Dec 1, 2024 · N471CA · Cndair CL6002B19 · Ice/Rain Protection System
  > AT 100 KNOTS ANTI - ICE DUCT WARNING MESSAGE APPEARED. REJECTED TAKEOFF WAS PERFORMED. QRH COMPLETED TAXIED BACK TO GATE. (FLIGHT 5053 - FILED CLOSED) ATTEMPTED TO PREFORMED TROUBLESHOOTING WITH FIM 36-20-00. COULD NOT DUPLICATED ANTI-ICE DUCT WARNING DUR
- [SDR SWIA2024120201321](https://openairdocs.org/sdr/SWIA2024120201321.md): Duct · warning message · Dec 1, 2024 · N471CA · Cndair CL6002B19 · Ice/Rain Protection System
  > AT 100 KNOTS ANTI - ICE DUCT WARNING MESSAGE APPEARED. REJECTED TAKEOFF WAS PERFORMED. QRH COMPLETED TAXIED BACK TO GATE. (FLIGHT 5053 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202402050002](https://openairdocs.org/sdr/SWIA202402050002.md): Warning Message · activated · Feb 2, 2024 · N471CA · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > ANTI ICE DUCT WARNING MESSAGE. (FLIGHT 5050 FILED CLOSED)UPON ARRIVAL TO AIRCRAFT, SPOKE WITH CAPTAIN AND HE MENTIONED THAT AFTER RUNNING QRH THE MESSAGE EXTINGUISHED. BUT AS SOON AS HE TURNED ON WING A/I THE ANTI ICE DUCT WARNING APPEARED AND ON EICAS A/I PA
- [SDR SWIA20230629005](https://openairdocs.org/sdr/SWIA20230629005.md): Unknown · not extended · Jun 25, 2023 · N471CA · Cndair CL6002B19 · Landing Gear System
  > CREW GOT A GEAR DISAGREE GOING INTO SDF AND DID THE ALTERNATE EXTENSION (FLT 5455 FILED CLOSED)AFTER REPAIRS TO 3A AND 3B HYDRAULIC SYSTEM (PLEASE SEE EAML 1163259 FOR REPAIR TO HYDRAULIC SYSTEM), JACKED AND PERFORMED A LANDING GEAR EXTENSION AND RETRACTION IN
- [SDR SWIA2023062900005](https://openairdocs.org/sdr/SWIA2023062900005.md): Unknown · leaking · Jun 25, 2023 · N471CA · Cndair CL6002B19 · Hydraulic Power System
  > HYD 3 LO PRESS IN CRUISE. FOLLOWED QRH. DECLARED EMERGENCY. DIVERTED TO SDF. DID NOT LAND OVERWEIGHT. RESERVOIR 3 EMPTY. FLUID LEAKING VISIBLY. (FLT 5455 FILED CLOSED)PLEASE REFERENCE AML 1164690 FOR HYDRAULIC SYSTEM 3, ACMP 3A SHOCK MOUNT REPLACEMENT. UPON IN
- [SDR SWI2023F00077](https://openairdocs.org/sdr/SWI2023F00077.md): Unknown · not extended · Jun 25, 2023 · N471CA · Cndair CL6002B19 · Landing Gear Door Actuator
  > CREW GOT A GEAR DISAGREE GOING INTO SDF AND DID THE ALTERNATE EXTENSION (FLT 5455 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202306260005](https://openairdocs.org/sdr/SWIA202306260005.md): Unknown · leaking · Jun 25, 2023 · N471CA · Cndair CL6002B19 · Hydraulic Indicating System
  > HYD 3 LO PRESS IN CRUISE. FOLLOWED QRH. DECLARED EMERGENCY. DIVERTED TO SDF. DID NOT LAND OVERWEIGHT. RESERVOIR 3 EMPTY. FLUID LEAKING VISIBLY. (FLT 5455 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2023060502](https://openairdocs.org/sdr/SWIA2023060502.md): Unknown · warning message · Jun 2, 2023 · N471CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WHEN SELECTING GEAR DOWN ON FINAL. COMPLIED WITH QRH AND GOT GEAR TO COME DOWN AND INDICATE 3 GREEN (FLT 5019 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26707430 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 26710512 FOR LAN
- [SDR SWIA20230413](https://openairdocs.org/sdr/SWIA20230413.md): Unknown · scratched · Apr 13, 2023 · N471CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA76851-601R-52-31-365 471CA MXCODEID61148-PR - ON POSTFLIGHT NOTED TWO DEEP SCRATCHES ON TOP OF CARGO DOOR. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-52-31-365. PERMANENT REPAIR DUE WITHIN 1800 FLT HRS WITH ESCALATI
- [SDR SWIA202264091](https://openairdocs.org/sdr/SWIA202264091.md): None · arced · Jan 30, 2022 · N471CA · Cndair CL6002B19 · Window/Windshield System
  > D:ON APPROACH NOT IN ICING CONDITIONS EICAS POSTED MESSAGE OF R WSHLD HEAT. FOLLOWED QRH AND MESSAGE IMMEDIATELY RETURNED. SELECTED R WSHLD SWITCH TO OFF AND NOTED ARCING BETWEEN THE PANES. APPROX 20? OF LENGTH. / C: MEL 30-41-1B / CAT C DUE 02-09-22 / NOTE: M
- [SDR SWIA202163350](https://openairdocs.org/sdr/SWIA202163350.md): None · corroded · Nov 9, 2021 · N471CA · Cndair CL6002B19 · Flight Control System
  > RH ELEVATOR BELLCRANK-TO-LEVER CONTROL ROD ASSEMBLY HAS CORRODED ROD END AND BEARING AND HARDWARE. REQUIRES REPLACEMENT (C CHECK RO 12/28/2021) RH ELEVATOR BELLCRANK-TO-LEVER CONTROL ROD ASSEMBLY WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 200 AMM 27-31
- [SDR SWIA202163349](https://openairdocs.org/sdr/SWIA202163349.md): None · corroded · Nov 9, 2021 · N471CA · Cndair CL6002B19 · Flight Control System
  > LH ELEVATOR BELLCRANK-TO-LEVER CONTROL ROD ASSEMBLY HAS CORRODED BEARING, ROD END AND HARDWARE. REQUIRES REPLACEMENT (C CHECK RO 12/28/2021) LH ELEVATOR BELLCRANK-TO-LEVER CONTROL ROD ASSEMBLY WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 200 AMM 27-31-35-
- [SDR SWIA202163348](https://openairdocs.org/sdr/SWIA202163348.md): None · corroded · Nov 9, 2021 · N471CA · Cndair CL6002B19 · Ailerons
  > LH OUTBOARD HINGE ARMS HAVE CORRODED HARDWARE REQUIRING REPLACEMENT (C CHECK RO 12/28/2021) INSTALLED NEW BOLT AND NUTS ON LH OUTBOARD FLAP HINGE ARM AT W.S. 178.00 IAW CRJ 200 AMM 57-53-02-400-804
- [SDR SWIA202163333](https://openairdocs.org/sdr/SWIA202163333.md): None · gouged · Nov 9, 2021 · N471CA · Cndair CL6002B19 · Aileron Tabs
  > O/B FLAP OUTBARD HINGE ARM IS GOUGED. (C CHECK RO 12/28/2021) REMOVED GOUGED HINGE ARM FITTING ASSEMBLY FROM THE L/H OUTBOARD FLAP AND INSTALLED NEW, SERVICEABLE HINGE ARM FITTING ASSEMBLY ON THE L/H OUTBOARD FLAP HINGE ARM IN THE OUTBOARD POSITION IAW BOM
- [SDR SWIA202163305](https://openairdocs.org/sdr/SWIA202163305.md): None · damaged · Nov 3, 2021 · N471CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > RBL 9 INBD FLOORBEAM WEB BETWEEN FS 409+16 & FS 409+32 HAS A DAMAGED RADIUS ON THE FORWARD SIDE REQUIRING REPLACEMENT. (C CHECK RO 12/28/2021) PERFORMED A MAJOR REPAIR BY REMOVEING AND REPLACING RBL 9 INBD FLOORBEAM WEB BETWEEN FS 409+16 & FS 409+32 IAW CR
- [SDR SWIA202163347](https://openairdocs.org/sdr/SWIA202163347.md): None · damaged · Oct 30, 2021 · N471CA · Cndair CL6002B19 · Engine Exhaust System
  > RH THRUST REVERSER HAS 1 UPPER BLOCKER DOOR THAT REQUIRES BUSHING REPAIR, NEED TO INSTALL NEW BUSHING. (C CHECK RO 12/28/2021) REPLACED BLOCKER DOOR HINGE BUSHINGS IAW CRJ 200 AMM 78-33-21-960-802. DIMENSIONAL INSPECTION PASS OF THE RH THRUST REVERSER B
- [SDR SWIA202163332](https://openairdocs.org/sdr/SWIA202163332.md): None · gouged · Oct 28, 2021 · N471CA · Cndair CL6002B19 · Aileron Tabs
  > RH WING OB FLAP HINGE BOX AT WS.220.00 BUSHINGS AND BOLT ARE GOUGED AND REQUIRE REPLACEMENT (C CHECK RO 12/28/2021) REMOVED AND INSTALLED NEW SERVICABLE IB BUSHINGS AND BOLT ON RH WING OB FLAP HINGE BOX ASSY IAW CRJ 200 AMM 57-21-35-000/400-802. SEE CONTIN
- [SDR SWIA202163346](https://openairdocs.org/sdr/SWIA202163346.md): None · corroded · Oct 25, 2021 · N471CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > SERVICE DOOR CLIP CORRODED AT STGR 17. LOCATED AT CENTER LINE OF DOOR. (C CHECK RO 12/28/2021) REMOVED AND REPLACED CLIP ON SERVICE DOOR WITH NEW CLIP PN: 601R38304-317 AT DATUM 17 AND FS. 334 IAW CRJ 200 SRM 51-42-06 AND REF: DWG: 601R38304 REV: BN. SEE C
- [SDR SWIA202163304](https://openairdocs.org/sdr/SWIA202163304.md): None · corroded · Oct 25, 2021 · N471CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > SERVICE DOOR ANGLE CORRODED AT STGR 15 ABOVE HANDLE. (C CHECK RO 12/28/2021) REPAIRED SERVICE DOOR ANGLE CORROSION AT STGR 15 IAW CRJ 200 SRM 51-21-11, 51-24-16, 51-25-16, 51-40-11, 51-42-06, 51-42-21, AND 52-00-00. COMPLETED TASK CARD 51-900-1003-SKY AND
- [SDR SWIA202163303](https://openairdocs.org/sdr/SWIA202163303.md): None · corroded · Oct 25, 2021 · N471CA · Cndair CL6002B19 · Doors
  > SERVICE DOOR FWD LOWER PAN IS CORRODED ON INNER SURFACE. (C CHECK RO 12/28/2021) -REMOVED AND REPLACED SERVICE DOOR FWD LOWER PAN IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003 AND ATTACHED COMPLETED FORM M-337. NO WEIGHT CHANGE
- [SDR SWIA202163302](https://openairdocs.org/sdr/SWIA202163302.md): None · damaged · Oct 24, 2021 · N471CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > UPON REMOVING RBL27 FLOORBEAM CAP BETWEEN FS574 AND FS605, FOUND 4EA FLOORBEAM WEBS TO HAVE ELONGATED HOLES DUE TO PREVIOUS REPAIR. REPLACEMENT REQUIRED. (C CHECK RO 12/28/2021) PERFORMED MAJOR REPAIR BY REMOVING AND REPLACING RBL27 FLOORBEAM CAP BETWEEN F
- [SDR SWIA202163301](https://openairdocs.org/sdr/SWIA202163301.md): None · cracked · Oct 22, 2021 · N471CA · Cndair CL6002B19 · Fuselage Structure (General)
  > DURING VISUAL INSPECTION OF LITEL REPAIR FOUND SUPPORT ANGLE CRACKED AT UPPER SIDE OF FITTING BETWEEN FS 621 AND FS 625 (C CHECK RO 12/28/2021) REPLACED FS621 LINTEL UPPER SUPPORT ANGLE IAW CRJ200 SRM 51-42-06, 51-42-13, AND 51-42-21.COMPLETED SKY CARD 51-
- [SDR SWIA202163300](https://openairdocs.org/sdr/SWIA202163300.md): None · none · Oct 21, 2021 · N471CA · Cndair CL6002B19 · Fuselage Main, Keel
  > AFTER REMOVING CORRODED F.S. 349.00 LOWER FRAME SEGMENT, FOUND ONE EACH PREVIOUSLY MISDRILLED HOLE COMMON TO F.S.349.00 AND THE OUTBOARD FLANGE OF STR 26L. (C CHECK RO 12/28/2021) COMPLIED WITH MHIRJ REO 601R-53-21-3504 REV-A DATED: 2021-10-29. COMPLETE
- [SDR SWIA202163345](https://openairdocs.org/sdr/SWIA202163345.md): None · corroded · Oct 13, 2021 · N471CA · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > PAX DOOR SURROUND STRUCTURE AT STGR20L CORRODED FS319 AND FS349 (C CHECK RO 12/28/2021) REMOVED AND REPLACED STR 20L INTERCOSTAL BETWEE FS 310 AND FS 333 IAW CRJ-200 SRM 51-42-21 AND 51-42-06, SEE CONTINUATION CARD FOR ALL WORK PERFORMED.
- [SDR SWIA202163299](https://openairdocs.org/sdr/SWIA202163299.md): None · corroded · Oct 13, 2021 · N471CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS349 CORRODED BETWEEN STGR25L AND STGR25R (C CHECK RO 12/28/2021) REMOVED AND REPLACED THE FRAME AT FS 349 BETWEEN STR 25L AND STR25R IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK 51-900-1003-SKY AND ATTACHED COMPLETED FORM M-337. NO
- [SDR SWIA202163298](https://openairdocs.org/sdr/SWIA202163298.md): None · corroded · Oct 13, 2021 · N471CA · Cndair CL6002B19 · Fuselage Structure (General)
  > SKIN CORRODE ON INTERIOR BETWEEN FS349 TO FS 364 AND BETWEEN STGR21R TO STGR22R. (MARKED WITH TAPE) (C CHECK RO 12/28/2021) REPAIRED CORRODED SKIN BETWEEN FS 349 TO FS 364 STR 21R TO 22R IAW MHIRJ REO 601R-53-21-3506 REV -- DATED 2021-11-09. TASK CARD 51-
- [SDR SWIA2021123063297](https://openairdocs.org/sdr/SWIA2021123063297.md): Skin · damaged · Oct 11, 2021 · N471CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING LOWER WING PLANK FUEL BOOST PUMP HAS MULTIPLE INDICATIONS 60%FSH AROUND CIRCUMERENCE OF THE LANDING AND VERTICAL SURFACES(MARKED WITH BLACK SHARPIE). FAILED NDT INSPECTION. (C CHECK RO 12/28/2021) PERFORMED A MAJOR REPAIR BY BLENDING CORROSION DAM
- [SDR SWIA202163344](https://openairdocs.org/sdr/SWIA202163344.md): None · corroded · Oct 9, 2021 · N471CA · Cndair CL6002B19 · Doors
  > PAX DOOR SILL TOP ANGLE FOUND TO BE CORRODED BETWEEN F,S 310 AND 349 (C CHECK RO 12/28/2021) REMOVED AND REPLACED PAX DOOR SILL TOP ANGLE BETWEEN F,S 310 AND 349 IAW CRJ-200 SRM 51-42-06, SEE CONTINUATION CARD FOR ALL WORK PERFORMED.
- [SDR SWIA202163331](https://openairdocs.org/sdr/SWIA202163331.md): None · worn · Oct 9, 2021 · N471CA · Cndair CL6002B19 · Doors
  > L/H OVERWING EMERGENCY EXIT WINDOW AFT BOTTOM STOP BRACKET PAD HOLE WORN BEYOND LIMITS NEEDS TO BE REPLACED IAW CRJ 200 AMM 52-21-00-000-80 (C CHECK RO 12/28/2021) DRILLED UP PILOTED HOLES ON LH O/W EMERGENCY EXIT DOOR AFT BOTTOM STOP BRACKET IAW CRJ200 SR
- [SDR SWIA202163330](https://openairdocs.org/sdr/SWIA202163330.md): None · worn · Oct 9, 2021 · N471CA · Cndair CL6002B19 · Doors
  > L/H OVERWING EMERGENCY EXIT WINDOW FWD MIDDLE STOP BRACKET PAD HOLE WORN BEYOND LIMITS, NEEDS TO BE REPLACED IAW CRJ 200 AMM 52-21-00-000-803 (C CHECK RO 12/28/2021) DRILLED UP PILOTED HOLES ON LH O/W EMERGENCY EXIT DOOR FWD MIDDLE STOP BRACKET IAW CRJ200
- [SDR SWIA202163329](https://openairdocs.org/sdr/SWIA202163329.md): None · worn · Oct 9, 2021 · N471CA · Cndair CL6002B19 · Doors
  > L/H OVERWING EMERGENCY EXIT WINDOW FWD UPPER STOP BRACKET PAD HOLE WORN BEYOND LILMITS NEEDS TO BE REPLACED IAW CRJ 200 AMM 52-21-00-000-803 (C CHECK RO 12/28/2021) DRILLED UP PILOTED HOLES ON LH O/W EMERGENCY EXIT DOOR FWD UPPER STOP BRACKET IAW CRJ200 SR
- [SDR SWIA202163328](https://openairdocs.org/sdr/SWIA202163328.md): None · gouged · Oct 5, 2021 · N471CA · Cndair CL6002B19 · Aileron Tabs
  > R/H WOMG OUT BOARD FLAP, FLAP BOX AT WS178.00 AFT INBOARD MOUNT BOLT AND BUSHING GOUGED NEEDS TO BE REPLACED (C CHECK RO 12/28/2021) REMOVED AND INSTALLED NEW SERVICABLE IB MOUNT BOLT AND BUSHING ON RH WING OB FLAP HINGE BOX AT WS 178 IAW CRJ 200 AMM 57-21
- [SDR SWIA202163343](https://openairdocs.org/sdr/SWIA202163343.md): None · corroded · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS 574 CROSSBEAM CAP CORRODED LBL 9 TO RBL 9. (C CHECK RO 12/28/2021) REMOVED AND REPLACED FS574 CROSSBEAM CAP LBL9 TO RBL9 IAW CRJ 200 SRM 51-42-06.
- [SDR SWIA202163342](https://openairdocs.org/sdr/SWIA202163342.md): None · cracked · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS 604 FRAME TO FLOOR SILL ATTACH ANGLE AT LBL 44 IS CRACKED. (C CHECK RO 12/28/2021) REMOVED AND REPLACED CRACKED FLOOR TO SILL ATTACH ANGLE IAW CRJ 200 SRM 51-42-21
- [SDR SWIA202163327](https://openairdocs.org/sdr/SWIA202163327.md): None · cracked · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Structure (General)
  > 9G BULKHEAD FLOOR MOUNT AT FS 559+88 RFL 9 IS CRACKED. (C CHECK RO 12/28/2021) REMOVED AND REPLACED 9G BULKHEAD FLOOR MOUNT AT FS 559+ 88 RFL 9 IAW CRJ 200 AMM 53-00-49-000-801/400-801.
- [SDR SWIA202163326](https://openairdocs.org/sdr/SWIA202163326.md): None · corroded · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > CARGO FLOOR SEAT TRACK SEGMENT FS 559+86 TO FS 559+95 AT RBL 9 IS CORRODED. (C CHECK RO 12/28/2021) REMOVED AND REPLACED CARGO FLOOR TRACK SEGMENT FS559+86 TO FS559+95 AT RBL 9 IAW CRJ 200 AMM 53-00-49-000-801/400-801.
- [SDR SWIA202163325](https://openairdocs.org/sdr/SWIA202163325.md): None · damaged · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Structure (General)
  > CARGO FLOOR CROSSBEAM CAP FS 589, LBL9 TO LBL 27 HAS ELONGATED FASTENER HOLE. (C CHECK RO 12/28/2021) REPLACED FS589 CROSSBEAM CAP BETWEEN LBL9 & LBL27 IAW CRJ200 SRM 51-40-11, 51-42-06, & 51-42-21 AND MHIRJ REO 601R-53-61-7745 REV-- DATED 2021-11-15.. REF
- [SDR SWIA202163296](https://openairdocs.org/sdr/SWIA202163296.md): None · corroded · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Structure (General)
  > CARGO BAY FLOOR BEAM CAP FS 559+122 TO FS 610 AT RBL 27 IS CORRODED. (C CHECK RO 12/28/2021) REMOVED OLD AND INSTALLED NEW CARGO BEAN CAP FS 599+122 TO FS 610 AT RBL 27 USING ALTERNATE FASTERNERS IAW BOMBARDIAR REO 601-53-61-3778 REV-B DATE 2016-12-19, SRM
- [SDR SWIA2021123063295](https://openairdocs.org/sdr/SWIA2021123063295.md): Floor Support · corroded · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR BEAM CAP FS 559+122 TO FS 610 AT LBL 9 IS CORRODED. (C CHECK RO 12/28/2021) PERFORMED A MAJOR REPAIR BY REPLACING LBL9 CARGO FLOORBEAM CAP BETWEEN FS559+122 & FS621 IAW BOMBARDIER REO 601R-53-00-005 REV -B DATED 2011-01-06, MHIRJ REO 601R-53-61
- [SDR SWIA202163294](https://openairdocs.org/sdr/SWIA202163294.md): None · corroded · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Structure (General)
  > CARGO FLOOR BEAM CAP FS 610 TO FS 619 LBL 9 IS CORRODED AND HAS 1EA. ELONGATED HOLE. (C CHECK RO 12/28/2021) REMOVED AND REPLACED CARGO FLOORBEAM FITTING BETWEEN FS610 & FS621 IAW CRJ200 SRM 51-42-06 & 51-42-21, COMPLETED SKY CARD 51-900-1003-SKY, 337 COMP
- [SDR SWIA2021123063293](https://openairdocs.org/sdr/SWIA2021123063293.md): Floor Support · corroded · Oct 2, 2021 · N471CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR SILL HAS 2EA. CORRODED NUTPLATES, WITH CORROSION SURROUNDING HOLES (BOTTOM SURFACE) AT FS 604. (C CHECK RO 12/28/2021) CARGO DOOR SILL BETWEEN FS 562 AND FS 621 WAS REMOVED AND REPLACED IAW REO 601R-53-61-1574 REV. -B DATED 2012-04-15, FORM 337
- [SDR SWIA202163341](https://openairdocs.org/sdr/SWIA202163341.md): None · corroded · Oct 1, 2021 · N471CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT TRACK FROM FS 409+16 TO FS 409+112 IS CORRODED. (C CHECK RO 12/28/2021) LH SIDE SEAT TRACK FROM FS 409+16 TO FS 409+112 WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 200 SRM 53-01-11-400-802. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK

Next page: https://openairdocs.org/aircraft/N471CA/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 = 'N471CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N471CA/reports

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