# Service difficulty reports: N374CA

A list on [N374CA](https://openairdocs.org/aircraft/N374CA.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 · 193 reports

- [SDR SWIA2026091377139](https://openairdocs.org/sdr/SWIA2026091377139.md): Acm · seized · Sep 13, 2026 · N374CA · Cndair CL6002C11 · Cabin Cooling System
  > AIRCRAFT POWERED DOWN ONCE POWERED UP BOTH PACKS WORKED BUT AFTER A FEW SECONDS SMOKE STARTED FILLING THE CABIN. FLIGHT 4263. FOUND RT ACM SEIZED. REMOVED AND REPLACED THE RT ACM, REF CP 33027018 FOR PARTS AND WORK PERFORMED. PERFORMED OPS TEST OF RT PACK
- [SDR SWIA2026091377138](https://openairdocs.org/sdr/SWIA2026091377138.md): Acm · seized · Sep 13, 2026 · N374CA · Cndair CL6002C11 · Cabin Cooling System
  > RIGHT PACK NOT WORKING WHEN PACK WAS ON IT WAS PUTTING OUT AN ELECTRICAL BURNING ODOR. FLIGHT 4263. FOUND RT ACM SEIZED. R & R THE RT ACM, REF CP 33027018 FOR PARTS AND WORK PERFORMED. PERFORMED OPS TEST OF RT PACK IN REF AMM 21-51-00, OPS TEST, LEAK CHKD
- [SDR SWIA2026011075501](https://openairdocs.org/sdr/SWIA2026011075501.md): Shaft · wrong part · Jan 10, 2026 · N374CA · Cndair CL6002C11 · Engine Thrust Reverser
  > LEFT ENGINE THRUST SHAFT REQUIRES REPLACEMENT DUE TO NO SERIAL NUMBER. (FILED CLOSED)REMOVED AND REPLACED LH ENGINE THRUST SHAFT AMM 71-22-01. SEE CP 31515585 FOR ENGINE INSTALLATION TASK CARD.TORQUE WRENCH: SERIAL NUMBER 0423601500 EXPIRATION DATE: 06/30/2026
- [SDR SWIA2025101500004](https://openairdocs.org/sdr/SWIA2025101500004.md): Landing Gear · warning message · Oct 14, 2025 · N374CA · Cndair CL6002C11 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE. (FLIGHT 4234) CREW STATES THAT UPON LANDING AND POST FLIGHT INSPECTION, A NLG GEAR PIN WAS FOUND IN THE NLG CAUSING THE LANDING GEAR DISAGREE. PERFORMED A GVI OF THE NLG AND SURROUNDING STRUCTURES PER AMM 32-20-00 WITH NO D
- [SDR SWIA202412241121](https://openairdocs.org/sdr/SWIA202412241121.md): Panel · damaged · Nov 21, 2024 · N374CA · Cndair CL6002C10 · Fuselage Structure (General)
  > PANEL 323BT HAS ELONGATED HOLES ON UPPER ROW. (C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED PANEL 323BT PER REO 670-55-32-354 REV-- DATE: 2024-12-07. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2025010601120](https://openairdocs.org/sdr/SWIA2025010601120.md): Doubler · cracked · Nov 20, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > THERE APPEARS TO BE A CRACK IN THE LH ENGINE PYLON DOUBLER BEHIND THE HYDRAULIC PRESSURE LINE QD FITTING (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED WITH NEW DOUBLER ON LH ENGINE PYLON DOUBLER BEHIND THE HYDRAULIC PRESSURE LINE QD FITTING. REF.
- [SDR SWIA202412241120](https://openairdocs.org/sdr/SWIA202412241120.md): Doubler · cracked · Nov 20, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > THERE APPEARS TO BE A CRACK IN THE LH ENGINE PYLON DOUBLER BEHIND THE HYDRAULIC PRESSURE LINE QD FITTING (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND REPLACED WITH NEW DOUBLER ON LH ENGINE PYLON DOUBLER BEHIND THE HYDRAULIC PRESSURE LINE QD FITTING. REF. C
- [SDR SWIA202501061018](https://openairdocs.org/sdr/SWIA202501061018.md): Skin · dented · Oct 18, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT LOCATED BETWEEN FS 1015.00 - FS 1031.00 AND BETWEEN STR 27 AND STR 26L(C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED DENTED LOCATION BETWEEN FS1015.00-FS1031.00 BETWEEN STR 27 AND STR 26L REF REO 670-53-61-2397 REV.-- DATED 2024-10-29. LEAK CHECK. COMPLIE
- [SDR SWIA2024122401018](https://openairdocs.org/sdr/SWIA2024122401018.md): Skin · dented · Oct 18, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT LOCATED BETWEEN FS 1015.00 - FS 1031.00 AND BETWEEN STR 27 AND STR 26L(C-CHECK RO 12/21/2024) (FILED OPEN)REPAIRED DENTED LOCATION BETWEEN FS1015.00-FS1031.00 BETWEEN STR 27 AND STR 26L REF REO 670-53-61-2397 REV.-- DATED 2024-10-29. LEAK CHECK. COMPLIED
- [SDR SWIA2025010601013](https://openairdocs.org/sdr/SWIA2025010601013.md): Drain Valve · mislocated · Oct 13, 2024 · N374CA · Cndair CL6002C10 · Fuselage Structure (General)
  > DURING INCORPORATION OF SB 670BA-53-57 FUSELAGE, CENTER FUSELAGE MODIFICATION OF THE DRAIN VALVES IN THE CENTER FUSELAGE BETWEEN FS280.00 AND FS33.00 REV C PARTS(S) MISLOCATED LH DRAIN HOLE DOUBLER PLATE. (C-CHECK RO 12/21/2024) (FILED CLOSED)COMPLIED WITH REO
- [SDR SWIA202412241013](https://openairdocs.org/sdr/SWIA202412241013.md): Drain Valve · mislocated · Oct 13, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING INCORPORATION OF SB 670BA-53-57 FUSELAGE, CENTER FUSELAGE MODIFICATION OF THE DRAIN VALVES IN THE CENTER FUSELAGE BETWEEN FS280.00 AND FS33.00 REV C PARTS(S) MISLOCATED LH DRAIN HOLE DOUBLER PLATE. (C-CHECK RO 12/21/2024) (FILED OPEN)COMPLIED WITH REO 6
- [SDR SWIA20241012](https://openairdocs.org/sdr/SWIA20241012.md): Frame · corroded · Oct 12, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS517 FRAME AFT SIDE LOWER FLANGE HAS CORROSION FROM 26L TO 25R (C-CHECK RO 12/21/2024) (FILED OPEN)REPAIRED FS517 FRAME AFT LOWER FLANGE STR 26L-25R REF REO 670-53-31-956 REV.-- DATED 2024-11-04. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-S
- [SDR SWIA2025010600009](https://openairdocs.org/sdr/SWIA2025010600009.md): Stringer · damaged · Oct 9, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REMOVE FRAME FS909 STGR 20L-25L TO FACILITATE STGR 20L REPAIR. (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED FRAME FS909 STGR 20L-25L AND INSTALLED NEW FRAME WITH NEW FRAME SPLICE REF REO 670-53-51-317 REV.-- DATED 2024-10-27, CRJ700 SRM 51-42-06-001-001-A01,
- [SDR SWIA202412241009](https://openairdocs.org/sdr/SWIA202412241009.md): None · none · Oct 9, 2024 · N374CA · Cndair CL6002C10 · Standard Practices/Structures
  > REMOVE FRAME FS909 STGR 20L-25L TO FACILITATE STGR 20L REPAIR. (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED FRAME FS909 STGR 20L-25L AND INSTALLED NEW FRAME WITH NEW FRAME SPLICE REF REO 670-53-51-317 REV.-- DATED 2024-10-27, CRJ700 SRM 51-42-06-001-001-A01, DW
- [SDR SWIA202501060927](https://openairdocs.org/sdr/SWIA202501060927.md): Intercostal · corroded · Sep 27, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD EQUIPMENT BAY DOOR SURROUND STRUCTURE, INTERCOSTALS FOR STRINGERS 25 RT AND 26RT CORRODED AT ATTACH POINTS ON FS 364, FORWARD FRAME. (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACED FS364 FRAME SECTION REF DWG SH670-32050 REV. J, CRJ700 SRM 51-42-06-001-
- [SDR SWIA202412240927](https://openairdocs.org/sdr/SWIA202412240927.md): Door Frame · corroded · Sep 27, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD EQUIPMENT BAY DOOR SURROUND STRUCTURE, INTERCOSTALS FOR STRINGERS 25 RT AND 26RT CORRODED AT ATTACH POINTS ON FS 364, FORWARD FRAME. (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED FS364 FRAME SECTION REF DWG SH670-32050 REV. J, CRJ700 SRM 51-42-06-001-00
- [SDR SWIA202501060923](https://openairdocs.org/sdr/SWIA202501060923.md): Angle · corroded · Sep 23, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING PAX DOOR THRESHOLD MIDCAP ANGLE REMOVAL, IT WAS FOUND CORROSION ON MULTIPLE AREAS ON THE KICKPLATE ANGLE P/N: SH670-31875-3 AT VERTICAL FLANGE OUTBOARD AND INBOARD FACES (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED WITH NEW KICKPLATE ANGLE
- [SDR SWIA202412240923](https://openairdocs.org/sdr/SWIA202412240923.md): Angle · corroded · Sep 23, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING PAX DOOR THRESHOLD MIDCAP ANGLE REMOVAL, IT WAS FOUND CORROSION ON MULTIPLE AREAS ON THE KICKPLATE ANGLE P/N: SH670-31875-3 AT VERTICAL FLANGE OUTBOARD AND INBOARD FACES (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND REPLACED WITH NEW KICKPLATE ANGLE P
- [SDR SWIA20240913](https://openairdocs.org/sdr/SWIA20240913.md): Support Fitting · corroded · Sep 13, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CORRODED SUPPORT FITTING ON LOWER FRAME FLANGE AT FS.863 JUST RH OF STGR.27 (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED CORROSION FROM THE AFT MACHINED FITTING (SUPPORT FITTING) AT FS863.00 STGR27 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO ALLOWABLE
- [SDR SWIA2025010600034](https://openairdocs.org/sdr/SWIA2025010600034.md): Bracket · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED CLOSED)INSTALLED 1 EA. NEW 'A'-BRACKET P/N CN 624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2025010600033](https://openairdocs.org/sdr/SWIA2025010600033.md): Bracket · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED L/H LWR TRANSCOWL I/B "A" BRACKET REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY SKYCARD 51-900-1002-SKY.
- [SDR SWIA2025010600032](https://openairdocs.org/sdr/SWIA2025010600032.md): Bracket · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED CLOSED)INSTALLED NEW L/H LWR TRANSCOWL O/B "A" BRACKET STANDOFF REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION SHEE
- [SDR SWIA2025010600031](https://openairdocs.org/sdr/SWIA2025010600031.md): Bracket · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND
- [SDR SWIA2025010600910](https://openairdocs.org/sdr/SWIA2025010600910.md): Bracket · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED CLOSED)INSTALLED NEW R/H LWR TRANSCOWL "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY SKYCARD 51-900-1002-SKY. SEE CONTINUATIO
- [SDR SWI2024F01405](https://openairdocs.org/sdr/SWI2024F01405.md): Stand Off · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED OPEN)INSTALLED 1 EA. NEW 'A'-BRACKET P/N CN 624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWI2024F01404](https://openairdocs.org/sdr/SWI2024F01404.md): Transcowl · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND REPLACED L/H LWR TRANSCOWL I/B "A" BRACKET REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY SKYCARD 51-900-1002-SKY.
- [SDR SWI2024F01403](https://openairdocs.org/sdr/SWI2024F01403.md): Transcowl · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED OPEN)INSTALLED NEW L/H LWR TRANSCOWL O/B "A" BRACKET STANDOFF REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION SHEET
- [SDR SWI2024F01402](https://openairdocs.org/sdr/SWI2024F01402.md): Transcowl · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED OPEN)REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SK
- [SDR SWIA202412240910](https://openairdocs.org/sdr/SWIA202412240910.md): Transcowl · cracked · Sep 10, 2024 · N374CA · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/21/2024) (FILED OPEN)INSTALLED NEW R/H LWR TRANSCOWL "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY SKYCARD 51-900-1002-SKY. SEE CONTINUATION
- [SDR SWIA202412240909](https://openairdocs.org/sdr/SWIA202412240909.md): Frame · corroded · Sep 9, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS280 BETWEEN STR25L AND STR25R HAS CORROSION ON TOP IN MULTIPLE LOCATIONS. (C-CHECK RO 12/21/2024) (FILED CLOSED)BLENDED DAMAGE AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ EO CL-600-2C10-53-L08266 REV IR DATE 9/17/2024. SEE CONTINUATION CARD FOR DETA
- [SDR SWIA2025010600030](https://openairdocs.org/sdr/SWIA2025010600030.md): Stringer · corroded · Sep 8, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERNAL CABIN L/H FS 349 - 364 STR 19L HAS CORROSION AROUND SEVERAL FASTNERS (C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED INTERNAL CABIN LH FS349-364 19L REF CRJ700 SRM 53-00-03-201-001-A01 REPAIR S6295 TYPE Z10 AND CRJ700 SRM 51-42-06-001-001-A01. LEAK CHE
- [SDR SWIA2025010600908](https://openairdocs.org/sdr/SWIA2025010600908.md): Panel · cracked · Sep 8, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SIDE WHEEL WELL AT APPROX RW 48.95 STRUCTURE HAS SUSPECT CRACK.(MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)RH SIDE WHEEL WELL APPROX. WS48.95 RIB REPLACED REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-23-00-001-001-A01, DWG CC670-10610 REV. D, AND R
- [SDR SWI2024F01401](https://openairdocs.org/sdr/SWI2024F01401.md): Stringer · corroded · Sep 8, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERNAL CABIN L/H FS 349 - 364 STR 19L HAS CORROSION AROUND SEVERAL FASTNERS (C-CHECK RO 12/21/2024) (FILED OPEN)REPAIRED INTERNAL CABIN LH FS349-364 19L REF CRJ700 SRM 53-00-03-201-001-A01 REPAIR S6295 TYPE Z10 AND CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK
- [SDR SWIA202412240908](https://openairdocs.org/sdr/SWIA202412240908.md): Structure · cracked · Sep 8, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SIDE WHEEL WELL AT APPROX RW 48.95 STRUCTURE HAS SUSPECT CRACK.(MARKED) (C-CHECK RO 12/21/2024) (FILED OPEN)RH SIDE WHEEL WELL APPROX. WS48.95 RIB REPLACED REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-23-00-001-001-A01, DWG CC670-10610 REV. D, AND REO
- [SDR SWIA2025010600029](https://openairdocs.org/sdr/SWIA2025010600029.md): Floor Support · corroded · Sep 7, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL9 LONGITUDINAL FLOOR SUPPORT IS CORRODED ON OUTBD FLANGE AT APPROX. FS515 €“ 517 (C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED RBL9 LONGITUDINAL FLOOR SUPPORT FS515-517 REF REO 670-53-31-940 REV.-- DATED 2024-09-18, CRJ700 SRM 53-00-41-201-001-A01, CRJ700
- [SDR SWIA2025010600028](https://openairdocs.org/sdr/SWIA2025010600028.md): Attach Angle · corroded · Sep 7, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON FRAME ATTACH FLANGE FS863 BETWEEN STR 26L AND STR 26R (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACED FRAME SECTION FS863 BETWEEN STR 25L-25R REF REO 670-53-51-314 REV.-- DATED 2024-10-21 AND CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD. COMPLI
- [SDR SWIA20250106907](https://openairdocs.org/sdr/SWIA20250106907.md): Stringer · corroded · Sep 7, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 20L BETWEEN FS879 - 893 (C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED STR 20L BETWEEN FS863.00-FS923.00 REF REO 670-53-51-315 REV.-- DATED 2024-10-24. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2024F01400](https://openairdocs.org/sdr/SWI2024F01400.md): Floor Support · corroded · Sep 7, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL9 LONGITUDINAL FLOOR BEAM IS CORRODED ON OUTBD FLANGE AT APPROX. FS515 €“ 517 (C-CHECK RO 12/21/2024) (FILED OPEN)REPAIRED RBL9 LONGITUDINAL FLOOR BEAM FS515-517 REF REO 670-53-31-940 REV.-- DATED 2024-09-18, CRJ700 SRM 53-00-41-201-001-A01, CRJ700 SRM 51-
- [SDR SWI2024F01399](https://openairdocs.org/sdr/SWI2024F01399.md): Attach Angle · corroded · Sep 7, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON FRAME ATTACH FLANGE FS863 BETWEEN STR 26L AND STR 26R (C-CHECK RO 12/21/2024) (FILED OPEN)REPLACED FRAME SECTION FS863 BETWEEN STR 25L-25R REF REO 670-53-51-314 REV.-- DATED 2024-10-21 AND CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD. COMPLIED
- [SDR SWIA202412240907](https://openairdocs.org/sdr/SWIA202412240907.md): Stringer · corroded · Sep 7, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 20L BETWEEN FS879 - 893 (C-CHECK RO 12/21/2024) (FILED OPEN)REPAIRED STR 20L BETWEEN FS863.00-FS923.00 REF REO 670-53-51-315 REV.-- DATED 2024-10-24. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA202501060027](https://openairdocs.org/sdr/SWIA202501060027.md): Stringer · corroded · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STINGER STGR 26L BETWEEN 1088.00 - 1098.00 (C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED STGR 26L AT FS1088-FS1098 REF CRJ700 SRM 53-00-03-201-001-A01, REO 670-53-61-2377 REV.-- DATED 2024-10-11 AND DWG: MM670-35007 REV W. LEAK CHECK GOOD. COMP
- [SDR SWIA202501060026](https://openairdocs.org/sdr/SWIA202501060026.md): Angle · corroded · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD MIDCAP ANGLE CORRODED AT MULTIPLE SPOTS BETWEEN FS310-FS349 (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW REPLACEMENT MID CAP ANGLE AT PAX DOOR THRESHOLD PER CRJ700 SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-
- [SDR SWIA202501060025](https://openairdocs.org/sdr/SWIA202501060025.md): Stringer · corroded · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION NOTED ON STRG 23L BETWEEN FS517.00-FS489.00 (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACED STGR 23L BETWEEN FS517.00-FS489.00 REF CRJ700 SRM 53-00-03-201-001-A01, CRJ700 SRM 51-42-06-001-001-A01,, DWG SH670-30006 REV. A., DWG SH670-33200 RE
- [SDR SWIA202501060024](https://openairdocs.org/sdr/SWIA202501060024.md): Plate · corroded · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION NOTED AT FWD BAG BAY TIE DOWN PLATE BTWN STRG22L-23L AND FS581 (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW BRACKET (TIE DOWN PLATE) P/N: SH670-33390-2 AT FS581 BETWEEN STGR 22L - 23L REF. CRJ700 SRM 51-42-21-001-001-A01
- [SDR SWIA202501060023](https://openairdocs.org/sdr/SWIA202501060023.md): Plate · corroded · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION NOTED AT FWD BAG BAY TIE DOWN PLATE BTWN STRG22L-23L AND FS533 (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED CORROSION FROM TIE DOWN PLATE FOUND OUT OF LIMITS, REMOVED AND REPLACED TIE DOWN PLATE P/N SH670-33390-1 BTWN TSRG22L- STRG23L AND F
- [SDR SWIA202501060022](https://openairdocs.org/sdr/SWIA202501060022.md): Floorbeam · cracked · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACK NOTED AT FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT RBL 9 (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT RBL 9 WITH NEW PN CC670-34144-1 REF CRJ700 SRM 51-42-21-001-001-A01, DWG CC670
- [SDR SWIA202501060021](https://openairdocs.org/sdr/SWIA202501060021.md): Floorbeam · cracked · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACK NOTED AT FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT LBL 9 (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED FLOOR BEAM CLIP ATTACHED TO 280 CROSSBEAM AT LBL 9 WITH NEW PN CC670-34144-1 REF CRJ700 SRM 51-42-21-001-001-A01, DWG CC670
- [SDR SWIA202501060020](https://openairdocs.org/sdr/SWIA202501060020.md): Floorbeam · cracked · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *CRACK FOUND ON FS 280 FLOOR BEAM-VERTICAL WEB AT RBL 9. (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACED FS 280 RH FLOOR BEAM SECTION WITH NEW REF CRJ 700 SRM 53-11-41-201-003-A01 AND REPLACED FS 280 BULKHEAD RH LOWER WEB A REF CRJ700 SRM 53-11-10-201-004-A01
- [SDR SWIA202501060019](https://openairdocs.org/sdr/SWIA202501060019.md): Plate · corroded · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION NOTED ON FWD BAG BAY TIE DOWN PLATE AT FS581 BTWN STRG26L-27 (MARKED)(C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACED FWD BAG BAY TIE DOWN PLATE AT FS581 BETWEEN STGR 26L-27 REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-33600 REV. AD. LEAK CHECK GO
- [SDR SWIA202501060018](https://openairdocs.org/sdr/SWIA202501060018.md): Frame · corroded · Sep 6, 2024 · N374CA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION NOTED ON FRAME FLANGE AT FS517.00 BTWN STRG 24L-25L (MARKED) (C-CHECK RO 12/21/2024) (FILED CLOSED)REPLACE FRAME SECTOR AT FS517.00 BETWEEN STR 25L-19L REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-20-001-001-A01 AND DWG SH670-33200 REV. G. L

Next page: https://openairdocs.org/aircraft/N374CA/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 = 'N374CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N374CA/reports

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