# Service difficulty reports: N472CA

A list on [N472CA](https://openairdocs.org/aircraft/N472CA.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 · 182 reports

- [SDR SWIA202265874](https://openairdocs.org/sdr/SWIA202265874.md): None · open · Jun 3, 2022 · N472CA · Cndair CL6002B19 · Landing Gear Selector
  > NOSE DOOR OPEN WARNING MESSAGE AFTER GEAR RETRACTION ON TAKEOFF. (FLIGHT 4711 - FILED CLOSED) PERFORMED OPS CHECK OF NLG DOOR PER CRJ200 AMM 33-22-01. OPS CHECK GOOD. MESSAGE NORMAL DURING NLG EXTENSION.
- [SDR SWIA2022012464020](https://openairdocs.org/sdr/SWIA2022012464020.md): Flap System · malfunctioned · Jan 22, 2022 · N472CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AFTER TAKEOFF FROM FAT, FLAPS FAIL MESSAGE. RAN QRH. PROCEEDED TO DEN. LANDED WITH 200 FPM, WITHOUT INCIDENT. AFTER TAKEOFF FROM FAT, FLAPS FAIL MESSAGE. RAN QRH. PROCEEDED TO DEN. LANDED WITH 200 FPM, WITHOUT INCIDENT. RESET AND OPERATED FLAPS 5 FULL CYCLE
- [SDR SWIA202161978](https://openairdocs.org/sdr/SWIA202161978.md): None · damaged · Oct 30, 2021 · N472CA · Cndair CL6002B19 · Horizontal Stabilizer, Tab Structure
  > FORM M-337 REQUIRED DUE TO DAMAGE ON RH HORIZONTAL STABILIZER IAW REO 601R-55-11-701 (FILED CLOSED) COMPLIED WITH M-337
- [SDR SWIA202161977](https://openairdocs.org/sdr/SWIA202161977.md): Doubler · damaged · Oct 30, 2021 · N472CA · Cndair CL6002B19 · Horizontal Stabilizer, Tab Structure
  > INSPECTED R/H HORIZONTAL STABILATOR AND FOUND DAMAGE ON FRAME 9 (3/4 INCH HOLES WHERE TWO NUT PLATES BLEW OUT), SKIN IN RIGHT AFT CORNER (1/2 INCH HOLE) AND DAMAGE ON AFT SPAR (3/4 INCH HOLES WHERE ONE NUT PLATE BLEW OUT). (FILED CLOSED) REPAIRED DAMAGE
- [SDR SWIA202158130](https://openairdocs.org/sdr/SWIA202158130.md): Support Angle · corroded · May 3, 2021 · N472CA · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR LOWER ANGLE SEAL SUPPORT, CENTER ANGLE SEAL SUPPORT SPLICE CORRODED. (FILED CLOSED) SERVICE DOOR LOWER SEAL SUPPORT SPLICE CORRODED BEYOND LIMITS. FABRICATED NEW SPLICE IN REF TO DWG 601R38304, REV BJ. REMOVED AND REPLACED SPLICE IN REF TO S
- [SDR SWIA202158133](https://openairdocs.org/sdr/SWIA202158133.md): Bracket · damaged · Apr 30, 2021 · N472CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR SURROUND STRUCTURE, FWD TRACK "CLIP" TO BEAM DAMAGED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR SURROUND STRUCTURE FWD TRACK TO BEAM "CLIP"/BRACKET WITH REFERENCE TO SRM 51-42-21. COMPLETED 51-900-1003-SKY AND M-337.
- [SDR SWIA202158132](https://openairdocs.org/sdr/SWIA202158132.md): Bracket · cracked · Apr 30, 2021 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SURROUND, FS. 574.00, LOWER CHANNEL/BRACKET CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR SURROUND, FS. 574.00, LOWER CHANNEL/BRACKET IN REF TO SRM 51-42-06. COMPLETED 51-900-1003-SKY AND M-337.
- [SDR SWIA202158131](https://openairdocs.org/sdr/SWIA202158131.md): Skin · dented · Apr 29, 2021 · N472CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBOARD FLAP HAS ONE DENT ON LOWER SKIN, APPROX 13 INCHES IN FROM OUTBOARD EDGE. (FILED CLOSED) REPAIRED DENT TO RH I/B FLAP ON LOWER SKIN, APPROX 13 INCHES IN FROM OUTBOARD EDGE IN REF TO SRM 57-52-00-02, REPAIR 3. / COMPLIED WITH TASK CARD 51-900-1
- [SDR SWIA202158129](https://openairdocs.org/sdr/SWIA202158129.md): Beam · corroded · Apr 29, 2021 · N472CA · Cndair CL6002B19 · Service Doors
  > CORROSION FOUND ON SERVICE DOOR LOCATED UNDER SIDE OF BOTTOM PAN. REFER TO SRM 52-41-14 FOR STRUCTURAL IDENTIFICATION. (FILED CLOSED) REMOVED AND REPLACED SERVICE DOOR LOWER AFT BEAM IN REF TO SRM 51-40-11 / 51-42-06 / 51-42-13. COMPLIED WITH TASK C
- [SDR SWIA202156415](https://openairdocs.org/sdr/SWIA202156415.md): Windshield · cracked · Feb 23, 2021 · N472CA · Cndair CL6002B19 · Flight Compartment Windows
  > TRANSFER FROM EAML 584330: CRACK IN LOWER INBOARD CORNER OF PILOTS WINDSHIELD. FLIGHT 5534 - FILED CLOSED REMOVED AND REPLACED LH WINDSHIELD WITH A SERVICEABLE UNIT PER AMM 56-11-01. ALSO COMPLIED WITH TASK CARD 56-220-1000-SKY, COMPLIED WITH PRESSURI
- [SDR SWIA202006161124](https://openairdocs.org/sdr/SWIA202006161124.md): Hose · chafed · Jun 16, 2020 · N472CA · Cndair CL6002B19 · Crew Oxygen System
  > DURING OBSERVER OXYGEN SYSTEM FCD INSPECTION, FOUND OXYGEN FLEXIBLE HOSE CHAFED. FILED CLOSED REMOVED AND REPLACED OBSERVER OXYGEN MASK FLEXIBLE HOSE REFERENCING APPLICABLE STEPS OF AMM. LEAK CHECK GOOD.
- [SDR SWIA2019071046048](https://openairdocs.org/sdr/SWIA2019071046048.md): Angle · corroded · Jun 11, 2019 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE IS CORRODED. (C-CHECK) RO: 07/07/2019 REMOVED AND INSTALLED NEW SERVICE DOOR SILL ANGLE P/N 601R38303-253 IAW SRM.
- [SDR SWIA2019071046047](https://openairdocs.org/sdr/SWIA2019071046047.md): Vane · chafed · Jun 7, 2019 · N472CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP VANE CENTER LEADING EDGE IS CHAFED. (C-CHECK) RO: 07/07/2019 REMOVED AND INSTALLED REPLACEMENT VANE CAP IAW SRM.
- [SDR SWIA2019071046045](https://openairdocs.org/sdr/SWIA2019071046045.md): Frame · corroded · May 30, 2019 · N472CA · Cndair CL6002B19 · Fuselage Main, Frame
  > CARGO COMPARTMENT €“ APPROX. FS 605.00 STGR 27 TO 23 LEFT AND 25 TO 26 RIGHT €“ HAS SIGNS OF CORROSION. (C-CHECK) RO: 07/07/2019 REMOVED AND INSTALLED NEW FRAME SECTION P/N 601R36026-27 AT FS605.0 IAW SRM.
- [SDR SWIA2019407106044](https://openairdocs.org/sdr/SWIA2019407106044.md): Frame · corroded · May 30, 2019 · N472CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS319.00 IS CORRODED ON THE LOWER FLANGE BETWEEN STR26L & STR27. (C-CHECK) RO: 07/07/2019 REMOVED AND INSTALLED NEW LOWER FRAME SECTION IAW SRM.
- [SDR SWIA2019071046043](https://openairdocs.org/sdr/SWIA2019071046043.md): Strap · corroded · May 29, 2019 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS559.00 €“ CORROSION ON STRAP BL27R €“ BL41.5R. (C-CHECK) RO: 07/07/2019 REMOVED AND INSTALLED NEW STRAP AT FS559.00 ON STRAP BL27R €“ BL41.5R. P/N: 601R31025-29 IAW SRM. PERFORMED PRESSURE CHECK IAW AMM, PRESSURE CHECK GOOD.
- [SDR SWIA2019071046042](https://openairdocs.org/sdr/SWIA2019071046042.md): Strap · corroded · May 29, 2019 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS559.00 €“ CORROSION ON STRAP BL27L €“ BL41.5L.(C-CHECK) RO: 07/07/2019 REMOVED AND INSTALLED NEW STRAP AT FS559.00 ON STRAP BL27L €“ BL41.5L. P/N: 601R31025-29, IAW SRM. PERFORMED PRESSURE CHECK IAW AMM, PRESSURE CHECK GOOD.
- [SDR SWIA2019071046049](https://openairdocs.org/sdr/SWIA2019071046049.md): Intercostal · corroded · May 24, 2019 · N472CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR - INTERCOSTAL DD3 CORRODED ON THE WEB BETWEEN FS320.16 AND FS338.96. (C-CHECK) RO: 07/07/2019 REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 IAW SRM. PERFORMED A LEAK CHECK OF WORKED AREAS IAW AMM. LEAK CHECK GOOD.
- [SDR SWIA2019071046041](https://openairdocs.org/sdr/SWIA2019071046041.md): Intercostal · corroded · May 24, 2019 · N472CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR - INTERCOSTAL DD4 CORRODED ON BOTH THE UPPER AND LOWER SURFACE OF THE WEB BETWEEN FS320.16 AND THE AFT FORMER. (C-CHECK) RO: 07/07/2019 INSTALLED NEW PAX DOOR INTERCOSTAL DD4 IAW SRM. PERFORMED A LEAK CHECK OF WORKED AREAS IAW AMM. LEAK CHECK GO
- [SDR SWIA2018061844783](https://openairdocs.org/sdr/SWIA2018061844783.md): Control Handle · failed · Jun 18, 2018 · N472CA · Cndair CL6002B19 · Landing Gear Selector
  > GEAR WOULD NOT COME UP AFTER DEPARTURE. RETURNED TO FIELD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW AMM. OPS CHECKS GOOD IAW AMM. COMPLIED WITH LANDING GEAR EMERGENCY EXTENSION IAW AMM, NO DEFECTS NOTED.
- [SDR SWIA201804304598](https://openairdocs.org/sdr/SWIA201804304598.md): Engine · contaminated · Apr 30, 2018 · N472CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > SMOKE IN THE AFT CABIN. RETURNED TO THE FIELD. PERFORMED AN ENGINE RUN DRY OUT PROCEDURE IAW AMM ON THE RT ENGINE DUE TO COMPRESSOR WASH ON PREVIOUS NIGHT. NO DEFECTS OR SMOKE ODOR IN THE AIRCRAFT WAS NOTED. OPS CHECKED GOOD.
- [SDR SWIA201743359](https://openairdocs.org/sdr/SWIA201743359.md): Angle · cracked · May 7, 2017 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT AND RIGHT OBLIQUE ANGLE AFT SIDE OF BS 621 BULKHEAD ARE CRACKED RBL AND LBL 36.20. REMOVED AND REPLACED THE ANGLES IAW SRM.
- [SDR SWIA201743362](https://openairdocs.org/sdr/SWIA201743362.md): Door Sill · corroded · May 5, 2017 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CARGO DOOR SILL HAS CORROSION FROM BS 574 TO 621. REMOVED AND REPLACED IAW SRM AND REO.
- [SDR SWIA201743361](https://openairdocs.org/sdr/SWIA201743361.md): Nut Plate · broken · May 5, 2017 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ON REMOVAL OF LEFT AND RIGHT WING PANEL FAIRINGS, FOUND TWO BROKEN NUT PLATES AT LT BS 559 +18 AND BS 559 + 62. REMOVED AND REPLACED THE NUTPLATES IAW SRM.
- [SDR SWIA201743358](https://openairdocs.org/sdr/SWIA201743358.md): Floor Support · corroded · May 5, 2017 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT LBL 27 FROM SPLICE AT BS 569 TO 606 IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.
- [SDR SWIA201743357](https://openairdocs.org/sdr/SWIA201743357.md): Floor Support · corroded · May 5, 2017 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CARGO FLOOR SSUPPORT HAS CORROSION BETWEEN BS 559+80 TO 589. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
- [SDR SWIA201743360](https://openairdocs.org/sdr/SWIA201743360.md): Skin · dented · May 4, 2017 · N472CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP HAS A DENT BETWEEN WS 68.138 AND WS 79.062 1 INCH FWD OF THE AFT SPAR. REPAIRED THE RT INBD FLAP SKIN IAW REO.
- [SDR SWIA201541146](https://openairdocs.org/sdr/SWIA201541146.md): Vane · chafed · Apr 19, 2015 · N472CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE CHAFED OTBD SIDE. BLENDED RT INBOARD FLAP VANE CHAFED OTBD SIDE IAW REO. FLAP VANE CAP REPLACED.
- [SDR SWIA201541145](https://openairdocs.org/sdr/SWIA201541145.md): Track · gouged · Apr 19, 2015 · N472CA · Cndair CL6002B19 · Engine Thrust Reverser
  > RT ENGINE THRUST REVERSER LOWER TRACK GOUGED APPROX TWELVE INCHES IN LENGTH. EVALUATED GOUGE FOUND OUT OF LIMITS IAW REO, RT THRUST REVERSER REPLACED. NO FURTHER ACTION REQUIRED.
- [SDR SWIA201541150](https://openairdocs.org/sdr/SWIA201541150.md): Striker · dented · Apr 18, 2015 · N472CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT SEAL STRIKER IS DENTED. COMPLIED WITH REPAIR OF PASSENGER DOOR AFT SEAL STRIKER, IAW REO.
- [SDR SWIA201541149](https://openairdocs.org/sdr/SWIA201541149.md): Striker · chafed · Apr 18, 2015 · N472CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORWARD SEAL STRIKER IS CHAFED. REPAIRED PAX DOOR FWD SEAL STRIKER IAW REO.
- [SDR SWIA201541151](https://openairdocs.org/sdr/SWIA201541151.md): Access Panel · corroded · Apr 17, 2015 · N472CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR ACCESS HOLE 832AL HAS CORROSION AT SCREW HOLES. BLENDED PAX DOOR ACCESS PANEL IAW SRM & EA. BLEND FOUND OUT OF LIMITS.
- [SDR SWIA201541148](https://openairdocs.org/sdr/SWIA201541148.md): Hinge · gouged · Apr 17, 2015 · N472CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR FUSELAGE HINGE GROOVED, ON AFT HINGE LANDING. REMOVED DAMAGE FROM PAX DOOR AFT HINGE LANDING IAW EA.
- [SDR SWIA201541147](https://openairdocs.org/sdr/SWIA201541147.md): Floor Panel · cracked · Apr 17, 2015 · N472CA · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR IS CRACKED AT FS 460 BETWEEN LBL9 AND RBL9, BELOW AIR DUCT, C-CHECK, RO 5/2/15, REPAIRED PRESSURE FLOOR CRACK AT FS 460 BETWEEN LBL9 AND RBL9, BELOW AIR DUCT REF REO.
- [SDR SWIA201541141](https://openairdocs.org/sdr/SWIA201541141.md): Floorbeam · cracked · Apr 17, 2015 · N472CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CRACKED AT BS 484, RBL 27. R & R IAW REO.
- [SDR SWIA201541140](https://openairdocs.org/sdr/SWIA201541140.md): Floorbeam · cracked · Apr 17, 2015 · N472CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CRACKED AT FS 484, LBL 32.0. REPLACED FLOORBEAM ANGLE IAW REO.
- [SDR SWIA201540601](https://openairdocs.org/sdr/SWIA201540601.md): Battery Pack · discharged · Jan 14, 2015 · N472CA · Cndair CL6002B19 · Emergency Lighting
  > THE EMERGENCY LIGHT BATTERY WILL NOT POWER LIGHTS. MX ALLOWED BATTERIES TO CHARGE.
- [SDR SWIA201437812](https://openairdocs.org/sdr/SWIA201437812.md): Filter · failed · May 28, 2014 · N472CA · Cndair CL6002B19 · Cabin Pressure Control System
  > DURING DESCENT, CABIN ALTITUDE CLIMBED UNTIL IT MATCHED AIRCRAFT ALTITUDE. DESCENDED UNPRESSURIZED. REPLACED PRSOV FILTERS.
- [SDR SWIA201437233](https://openairdocs.org/sdr/SWIA201437233.md): Lamp · burned out · Apr 18, 2014 · N472CA · Cndair CL6002B19 · Emergency Lighting
  > SECOND TO LAST OVERHEAD CABIN EMERGENCY LIGHT BURNED OUT. REPLACED LAMP.
- [SDR SWIA201334835](https://openairdocs.org/sdr/SWIA201334835.md): Bulkhead · damaged · Oct 2, 2013 · N472CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > TWO HOLES FOUND TO OVERSIZED ON 621 PRESSURE BULKHEAD LT SIDE IN FIRE BLOCK AREA. C-CHECK REPAIRED IAW REO.
- [SDR SWIA201334838](https://openairdocs.org/sdr/SWIA201334838.md): Lever · chafed · Sep 24, 2013 · N472CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD PULL IN LEVER CHAFED. C-CHECK REPLACED PAX DOOR FWD PULL IN LEVER IAW AMM.
- [SDR SWIA201334837](https://openairdocs.org/sdr/SWIA201334837.md): Stringer Clip · cracked · Sep 24, 2013 · N472CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT EQUIPMENT BAY, FS 625 LT STRINGER 14 CLIP CRACKED. C-CHECK REPLACED CLIP AT FS 625 LT STRINGER 14R IAW REO.
- [SDR SWIA201334836](https://openairdocs.org/sdr/SWIA201334836.md): Stringer Clip · cracked · Sep 24, 2013 · N472CA · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT EQUIPMENT BAY FS 625 RT STRINGER 14 CLIP CRACKED. C-CHECK REPLACED CLIP AT FS 625 RT STRINGER 14L IAW REO.
- [SDR SWIA201334850](https://openairdocs.org/sdr/SWIA201334850.md): Threshold · corroded · Sep 20, 2013 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD IS CORRODED. C-CHECK REPLACED IAW SRM.
- [SDR SWIA201334849](https://openairdocs.org/sdr/SWIA201334849.md): Post · cracked · Sep 20, 2013 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK NOTED & MARKED ON FS409+128 VERTICAL POST OTBD AFT RADIUS AT LBL18.00 WL71.00. C-CHECK REPLACED IAW REO.
- [SDR SWIA201334848](https://openairdocs.org/sdr/SWIA201334848.md): Structure · chafed · Sep 20, 2013 · N472CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR VENT DOOR CHAFED ON INBD SIDE 3 PLACES. C-CHECK BLENDED IAW REO.
- [SDR SWIA201334847](https://openairdocs.org/sdr/SWIA201334847.md): Support Fitting · cracked · Sep 20, 2013 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 RBL 9.0 INBD & OTBD SUPPORT CLIPS CRACKED. C-CHECK REPLACED IAW REO.
- [SDR SWIA201334842](https://openairdocs.org/sdr/SWIA201334842.md): Support Fitting · cracked · Sep 20, 2013 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9.0 FS 280 INBD SUPPORT CLIP CRACKED. C-CHECK REPLACED IAW REO.
- [SDR SWIA201334841](https://openairdocs.org/sdr/SWIA201334841.md): Beam · cracked · Sep 20, 2013 · N472CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 BEAM OTBD OF LBL 9.0 UPPER & LOWER SUPPORT BEAM CRACKED. C-CHECK REPLACED IAW REO.
- [SDR SWIA201334840](https://openairdocs.org/sdr/SWIA201334840.md): Bulkhead · cracked · Sep 20, 2013 · N472CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD WEB FS 280.0 LBL 20.75 RBL 20.75 CRACKED & CORRODED. C-CHECK REPAIRED IAW REO.

Next page: https://openairdocs.org/aircraft/N472CA/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 = 'N472CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N472CA/reports

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