# Service difficulty reports: N340CA

A list on [N340CA](https://openairdocs.org/aircraft/N340CA.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 · 209 reports

- [SDR REXA2026042300312](https://openairdocs.org/sdr/REXA2026042300312.md): Charger · inoperative · Apr 20, 2026 · N340CA · Cndair CL6002C10 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHTS INOP R/R CABIN EMER LT CHARGER IAW AMM 33-51-17. OPS CHECK GOOD. P/N ON: 11-0049 S/N ON: 26622 P/N OFF: 11-0049 S/N OFF: 20136R
- [SDR REXA2025093000897](https://openairdocs.org/sdr/REXA2025093000897.md): Oxygen Mask · no deploy · Sep 26, 2025 · N340CA · Cndair CL6002C10 · Passenger Oxygen System
  > DURING CRUISE CREW REPORTED R BLEED DUCT WARNING WITH CABIN DEPRESSURIZATION. FOLLOWING QRH PROCEDURES THE DESCENDED AND DECLARED EMERGENCY. PASSENGER OXYGEN MASKS WERE DEPLOYED WITH A FEW NOT DEPLOYED, ROWS 7 C7D AND 16 A&B. INSPECTED SEAT 7 C/D AND 16 A/B OX
- [SDR REXA2025063000702](https://openairdocs.org/sdr/REXA2025063000702.md): Hinge Fitting · chafed · Jun 30, 2025 · N340CA · Cndair CL6002C10 · Rudder Miscellaneous Structure
  > VERTICAL STABILIZER MID LOWER HINGE ASSY., LOWER HINGE HALF P/N AV670-21140-001 HAS AN EXCESSIVELY WORN BEARING LANDING. COMPLIED WITH MHIRJ REO 670-55-31-192 REV-- DATED 2025-06-20. INSTALLED NEW SERVICABLE LOWER HINGE P/N AV670-21081-013.
- [SDR REXA2025061800668](https://openairdocs.org/sdr/REXA2025061800668.md): Floorbeam · corroded · Jun 17, 2025 · N340CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS333 FLOOR CROSSBEAM IS CORRODED BETWEEN LBL9 AND LBL24. REPAIRED F.S.333 FLOOR CROSSBEAM BETWEEN LBL9 AND LBL24 IAW MHIRJ REO 670-53-21-2630 REV -- DATED 2025-06-16.
- [SDR REXA2025062700701](https://openairdocs.org/sdr/REXA2025062700701.md): Floorbeam · corroded · Jun 7, 2025 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND THE R/H F.S. 280 CROSSBEAM TO HAVE MULTIPLE SPOTS OF CORROSION. REMOVED R/H FS 280 CROSSBEAM IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-- 001-0010A01, 51-42-21-001-001-A01, 51-40-11-- 001-001-A01. REF. BARCODE IDENTIFIER HN00243776 FOR COMPLETION OF
- [SDR REXA2025061700660](https://openairdocs.org/sdr/REXA2025061700660.md): Floorbeam · corroded · May 21, 2025 · N340CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > "LH F.S.280 CROSSBEAM HAS MULTIPLE AREAS OF CORROSION. UPON FURTHER EVALUATION FOUND L/H FS280.00 CROSSBEAM TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS. FABRICATED LOCATED AND DRILLED REPAIR ITEMS -3, -4, -5, -6, -7, -8, -9, -21, -22, -31, -32 IAW BOMBARDIER
- [SDR REXA2024072200558](https://openairdocs.org/sdr/REXA2024072200558.md): Fan · inoperative · Jul 17, 2024 · N340CA · Cndair CL6002C10 · Air Distribution Fan
  > AFTER TAKEOFF, AT APPROX 500 FT ALTITUDE, CREW REPORTED SMOKE SMELL IN CABIN. RETURNED TO ATL. R&R GALLEY/LAV EXHAUST FAN IAW CRJ 700 AMM 21-23-93. OPS CHECK GOOD AT THIS TIME.
- [SDR REXA2022011900012](https://openairdocs.org/sdr/REXA2022011900012.md): Angle · corroded · Jan 8, 2022 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH MLG WHEEL WELL BLOW OUT PNL ATTACHING ANGLES ARE CORRODED. - REMOVED & REPLACED ANGLE IAW CRJ 700 SRM 51-42-210-001-001-A01. CURE CHECK OF SEALANT IN FUEL TANK GOOD. POINTED FASTENERS IAW CRJ 700 SRM 51-25-00-001-001-A01. LEAK CHECK OF REPAIR AREA PERFORMED
- [SDR REXA2022011900051](https://openairdocs.org/sdr/REXA2022011900051.md): Bushing · worn · Jan 7, 2022 · N340CA · Cndair CL6002C10 · Main Landing Gear
  > UPON REMOBAL OF RH MLG SIDE FOUND IN BOARD PINTLE PIN BUSHING BORE TO BE OUT OF TOLERANCE. - COMPLIED WITH REPAIR OF R/H MLH SIDE STAY PINTLE PIN BUSHING BORE IAW MHIRJ REO 670-57-11-186 REV--DATE 2021-12-01.
- [SDR REXA2022011900011](https://openairdocs.org/sdr/REXA2022011900011.md): None · corroded · Jan 7, 2022 · N340CA · Cndair CL6002C10 · Main Landing Gear
  > RH MLG SIDE STAY IS CORRODED AT HINGE JOINT AND ALONG LWR AFT EDGE OF UPPER BEAM. - REMOVED APEX BOLT AND STOP COMMON TO OLD SIDE STAY IAW CMM GOODRICH 32-11-12 REMOVED AND REPLACED R/H MLG SIDE STAY IAW CRJ 700 AMM 32-11-12-000/400-801-A01 BLEED LEAK AND OPS
- [SDR REXA2022011900018](https://openairdocs.org/sdr/REXA2022011900018.md): None · corroded · Jan 3, 2022 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL BETWEEN FS 280 AND FS 319 IS CORRODED IN MULTIPLE PLACES. - REMOVED AND INSTALLED RH FLOOR SILL BETWEEN FS 280 TO FS 319 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01 AND LOCATED AND DRILLED NEW RH FLOOR SIL
- [SDR REXA2022011900017](https://openairdocs.org/sdr/REXA2022011900017.md): Angle · corroded · Jan 3, 2022 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL MOUNTING ANGLE IS CORRODED - PLACED EWIS PROTECTION IAW CRJ 700 AMM 20-70-00-910-801-A01 REMOVED AND INSTALLED DOOR SILL ATTACHED BRACKETS IAW CRJ 700 51-42-06-001-001-A01 REMOVED AND INSTALLED DOOR SILL ATTACHED ANGLE IAW CRJ700 SRM 51
- [SDR REXA2022011900024](https://openairdocs.org/sdr/REXA2022011900024.md): Stringer · corroded · Dec 30, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 24L CORRODED BETWEEN FS 585.00 AND FS 613.00 - REPAIRED STRINGER 24L BETWEEN F.S. 585.00 & F.S. 613.00 IAW ENDEAVOR AIR EA# CK5753-12504 DATED 12-2-21 REV IR WVAC EMP STAMP # 722 MTC
- [SDR REXA2022011900022](https://openairdocs.org/sdr/REXA2022011900022.md): Stringer · corroded · Dec 30, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 24L CORRODED BETWEEN FS 517.00 AND FS 533.00 - REPAIRED STRINGER 24L BETWEEN FS 517.00 TO 533.00 IAW ENDEAVOR AIR EA# CRJ753-12503 DATED 12-2-21 REV IR WVAC EMP STAMP # 722 MTC
- [SDR REXA2022011900021](https://openairdocs.org/sdr/REXA2022011900021.md): Stringer · corroded · Dec 30, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 26L CORRODED AT FS 453.00 TO FS 469.00 - REMOVED AND REPLACED FASTENERS ON STR 26L FROM FS 453.00-469 IAW CJR 700 SRM 51-42-06-0901-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT O LIMITS. REPAIRED IAW ENDEAVOR AIR EA CRJ 753
- [SDR REXA2022011900050](https://openairdocs.org/sdr/REXA2022011900050.md): Seat Track · corroded · Dec 24, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > L/H SIDE SEAT RAIL IS CORRODED FROM FS 675 TO FS 713. - FABRICATED AND REPLACED LH SIDE SEAT RAIL FS 675-713 IAW CRJ 900 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01 AND AMM 53-00-49-400-801-A1
- [SDR REXA2022011900014](https://openairdocs.org/sdr/REXA2022011900014.md): Skin · chafed · Dec 24, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > EXTERNAL FUSELAGE SKIN BETWEEN FS 977.50 AND FS 985 HAS A CHAFE MEAS. 3"L. - REPAIRED AREA OF EXTERNAL SKIN FS. 977.5-985 IAW EA CRJ753-12527 REV.IR DATED 12/17/2021. WVAC EMP STAMP # 711 MTC
- [SDR REXA2022011900043](https://openairdocs.org/sdr/REXA2022011900043.md): Bushing · none · Dec 22, 2021 · N340CA · Cndair CL6002C10 · Wing Structure
  > RH AILERON BUSHING LUG MARKED C IS DAMAGED AND OVERSIZED. - REPAIRED LUG AND REPLACED BUSHING IAW REO 670-57-61-107 REV B DATED 2019-01-14.
- [SDR REXA2022011900023](https://openairdocs.org/sdr/REXA2022011900023.md): Stringer · corroded · Dec 22, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STGR 26R CORRODED BETWEEN FS 517.00 AND FS 533.00 - REPAIRED STRINGER 26R BETWEEN FS 517 AND FS 533 IAW ENDEAVOR EA# CRJ 753-12505 REV IR DATED 12/2/21 REMOVED TAPE. COMPLIED WITH EA CRJ 753-12505 REV IR DATED 12/2/21 WVAC EMP STAMP # 711 MTC
- [SDR REXA2022011900048](https://openairdocs.org/sdr/REXA2022011900048.md): Channel · cracked · Dec 20, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > L/H SIDE SEAT RAIL CHANNEL CRACKED BETWEEN FS 477.00 AND FS 573.00. - REPLACED SEAT TRACK RETAINER AND INSTALLED SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A03.
- [SDR REXA2022011900049](https://openairdocs.org/sdr/REXA2022011900049.md): Frame · corroded · Dec 18, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FRAME FS 333 IS CORRODED AT LOWER FLANGE AND WEB BETWEEN STR 26L TO STR 27 IN AVIONICS BAY. TCI 53-20-320. - REMOVED CORROSION ON FRAME FS 333 BETWEEN STR 26L AND STR 27 IAW CRJ 700 SRM 51-21-06-001-001-A01. NO DAMAGE ALLOWED PER CRJ 700 SRM 53-21-00-101-002-A
- [SDR REXA2022011900020](https://openairdocs.org/sdr/REXA2022011900020.md): Stringer · corroded · Dec 18, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 22R JUST FORWARD OF FS 349 IS CORRODED. - FOUND STRINGER 22R OUT OF LIMITS R/R UNSERVICEABLE STRINGER 22R WITH A SERVICEABLE STRINGER IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-23-00-001-001-A01. WVAC EMP STAMP #722 MTC
- [SDR REXA2022011900019](https://openairdocs.org/sdr/REXA2022011900019.md): Stringer · corroded · Dec 18, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 22R JUST FORWARD OF FS 349 IS CORRODED. - FOUND STRINGER 22R OUT OF LIMITS R/R UNSERVICEABLE STRINGER 22R WITH A SERVICEABLE STRINGER IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-23-00-001-001-A01. WVAC EMP STAMP #722 MTC
- [SDR REXA2022011900013](https://openairdocs.org/sdr/REXA2022011900013.md): Angle · corroded · Dec 17, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LIGHTENING DIVERTER ATTATCHING ANGLE BRACKET AT RBL 27.00 FROM FS 310 - FS 333 IS BENT AND REQUIRES REPLACEMENT. - REPLACED ATACHING ANGLE BRACKET @ RBL 27.00 FROM FS 310 - FS 333 WITH A SERVICEABLE ANGLE AND 2 EA CLIPS IAW CRJ 700 SRM 51-42-06-001-001(A01) AN
- [SDR REXA2022011900047](https://openairdocs.org/sdr/REXA2022011900047.md): Strap · corroded · Dec 16, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PANEL 196DR STRAP HAS MULTIPLE SPOTS OF CORROSION. - LOCATED AND DRILLED AFT AND FWD C CHANNELS AND STRAP IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED C CHANNELS TO STRAP IAW CRJ 700 SRM 51-42-13-001-001-A01 AND SRM 51-25-00-001-001-A01. INSTALLED ASSY TO P
- [SDR REXA2022011900026](https://openairdocs.org/sdr/REXA2022011900026.md): Bracket · corroded · Dec 16, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MACHINED BRACKET AT FS 581.00 BETWEEN STGR 26L AND STGR 27 IS CORRODED - REMOVED AND REPLACED MACHINED BRACKET AT FS 581.00 BETWEEN STR 26L AND 27 IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022011900040](https://openairdocs.org/sdr/REXA2022011900040.md): Seat Track · corroded · Dec 15, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SEAT TRACK AT LBL 9 FROM APPROX FS 830 TO FS 985 IS CORRODED IN MULTIPLE SPOTS. - AFTER FURTHER EVALUATION CORROSION EXISTS IN MORE THAN ONE CROSS SECTIONAL AREA MAKING SEAT TRACK OUT OF LIMITS IAW CRJ 700 SRM 53-51-49-101-001-A01. LOCATED, DRILLED AND INSTALL
- [SDR REXA2022011900032](https://openairdocs.org/sdr/REXA2022011900032.md): Seat Track · corroded · Dec 15, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 857 AND FS 961 - REMOVED AND REPLACED SEAT TRACK ON RH SIDE BETWEEN FS 857-961 IAW CRJ 700 AMM 53-00-49-000/400-801-A17.
- [SDR REXA2022011900046](https://openairdocs.org/sdr/REXA2022011900046.md): Plate · corroded · Dec 14, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH OVERWING EXIT SILL STEP PLATE HAS CORROSION BETWEEN FS 761.85-785.15, PON SH670-36552-7. - REMOVED STEP PLATE IAW CRJ 700 SRM 51-41-02-001-001-A01, CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-41-23-101-001-A01. DAMAGE THROUGH PART, INSTALLED NEW
- [SDR REXA2022011900025](https://openairdocs.org/sdr/REXA2022011900025.md): Bracket · corroded · Dec 14, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MACHINED BRACKET AT FS 533.00 BETWEEN STGR 26L AND STGR 27 IS CORRODED - REMOVED AND INSTALLED NEW SERVICEABLE MACHINED BRACKET P/N: SH670-33389-1 AT FS 333 BETWEEN STR 26L AND STR 27 IAW CRJ 700 SRM 51-42-21-001-001-A01. WVAC EMP #89190
- [SDR REXA2022011900038](https://openairdocs.org/sdr/REXA2022011900038.md): Seat Track · corroded · Dec 13, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 379 AND FS 483. - REMOVED & REPLACED L/H SIDE SEAT RAIL AT FS 379 TO 483 IAW CRJ 700 AMM 53-00-49-000/400-801(A17).
- [SDR REXA2022011900042](https://openairdocs.org/sdr/REXA2022011900042.md): Seat Track · corroded · Dec 12, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 581 TO F.S. 677. - REMOVED CORROSION FLOOR SLAT TRACK RBL 9 BETWEEN FS 581 TO 677 IN MORE THAN ONE CROSS-SECTIONAL AREA. FOUND TO BE OUT OF LIMITS IAW CRJ SRM 51-21-06-001-001-A01 AND SRM 53-31-49-101-001-A01. RE
- [SDR REXA2022011900041](https://openairdocs.org/sdr/REXA2022011900041.md): Seat Track · corroded · Dec 12, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 581 TO FS 677. - REMOVED CORROSION AT FLOOR SEAT TRACK LBL 9 BETWEEN FS 581 TO 677 MORE THAN ONE CROSS SECTIONAL AREA FOUND SEAT TRACK OUT OF LIMITS IAW CRJ 700 SRM 51-21-06-001-001-A01 AND SRM 53-31-49-101-001-A01.
- [SDR REXA2022011900033](https://openairdocs.org/sdr/REXA2022011900033.md): Seat Track · corroded · Dec 12, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 573 AND FS 675. - AFTER FURTHER EVALUATION CORROSION EXISTS ON MORE THAN ONE CROSS SECTION AND AREA THEREFORE SEAT TRACK IS OUT OF LIMITS. IAW CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND REPLACED SEAT TRACK P/N 670-33586
- [SDR REXA2022011900031](https://openairdocs.org/sdr/REXA2022011900031.md): Seat Track · corroded · Dec 12, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 787 AND FS 857. - AFTER FURTHER EVALUATION, CORROSION EXISTS ON MORE THAN ONE CROSS-SECTIONAL AREA MAKING SLAT TRACK OUT OF LIMITS IAW CRJ700 SRM 53-42-49-101-001-A01. REMOVED AND REPLACED SLAT TRACK ON RH AT FS 787 AND FS
- [SDR REXA2022011900030](https://openairdocs.org/sdr/REXA2022011900030.md): Seat Track · corroded · Dec 12, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 857 AND FS 961. - REMOVED AND REPLACED SEAT TRACK P/N: SH670-37543-3 ON LH SIDE FS 857 TO FS 961 IAW CRJ 700 AMM 53-00-49-000/400-801-A17.
- [SDR REXA2022011900029](https://openairdocs.org/sdr/REXA2022011900029.md): Seat Track · corroded · Dec 12, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 787 AND FS 857. - AFTER FURTHER EVALUATION, CORROSION EXISTS ON MORE THAN ONE CROSS SECTIONAL AREA MAKING SLAT TRACK OUT OF LIMITS IAW CRJ700 SRM 53-41-49-101-001-A01. REMOVED AND REPLACED SLAT TRACK RAIL ON LH BETWEEN FS
- [SDR REXA2022011900028](https://openairdocs.org/sdr/REXA2022011900028.md): Seat Track · corroded · Dec 12, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 713 AND FS 763. - REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS 713 AND FS 763 IAW CRJ700 AMM 53-00-49-000/400-801-A17. WVAC EMP STAMP # 703 MTC
- [SDR REXA2022011900039](https://openairdocs.org/sdr/REXA2022011900039.md): Seat Track · corroded · Dec 9, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SEAT TRACK AT RBL 9 FROM APPROX FS 830 TO FS 978 IS CORRODED IN MULTIPLE SPOTS. - AFTER FURTHER INVESTIGATION SEAT TRACK IS OUT OF LIMITS IAW CRJ 700 SRM 53-51-49-101-001-A01 DUE TO CORROSION IN MORE THAN ONE CROSS SECTIONAL AREA REMOVED AND REPLACED SEAT TRAC
- [SDR REXA2022011900035](https://openairdocs.org/sdr/REXA2022011900035.md): Seat Track · corroded · Dec 9, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 378 AND FS 483 - REMOVED & REPLACED R/H SEAT RAIL BETWEEN F.S. 378 TO 483 IAW CRJ700 AMM 53-00-49-000/400-801(A17) WVAC EMP # 56399
- [SDR REXA2022011900015](https://openairdocs.org/sdr/REXA2022011900015.md): Seat Track · corroded · Dec 9, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 9 SEAT TRACK FROM FS 379 TO FS 485 IS CORRODED - AFTER FURTHER EVALUATION, CORROSION EXISTS IN MORE THAN ONE CROSS SECTIONAL AREA MAKING SEAT TRACK OUT OF LIMITS IAW CRJ700 SRM 53-21-49-101-001-A01. REMOVED AND REPLACED SEAT TRACK P/N SH670-32249-3 AT FS 3
- [SDR REXA2022011900036](https://openairdocs.org/sdr/REXA2022011900036.md): Seat Track · corroded · Dec 8, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL CORRODED BETWEEN FS 573 AND FS 675. - INSTALLED NEW SEAT TRACK RAIL PN SH670-33558-3 ON LH SIDE FS 573 TO FS 675 IAW CRJ 700 AMM 53-00-49-400-801-A17.
- [SDR REXA2022011900037](https://openairdocs.org/sdr/REXA2022011900037.md): Seat Track · corroded · Dec 7, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT REAIL CORRODED BETWEEN FS 483 AND FS 573. - BLENDED CORROSION AT LH SIDE SEAT RAIL AT FS 483 ADN FS 571 IAW CRJ 700 SRM 53-00-101-001-A01. BLENDED AREAS TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND REPLACED L/H SEAT SIDE R
- [SDR REXA2022011900027](https://openairdocs.org/sdr/REXA2022011900027.md): Plate · corroded · Dec 7, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SUPPORT PLATE AT FS 533.00 STGR 25R IS CORRODED. - REMOVED AND REPLACED CORRODED SUPPORT PLATE AT FS 533.00 STR 25R IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-15-001-001-A0
- [SDR REXA2022011900034](https://openairdocs.org/sdr/REXA2022011900034.md): Seat Track · corroded · Dec 4, 2021 · N340CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SIDE SEAT RAIL CORRODED BETWEEN FS 48 AND FS 573. - AFTER FURTHER EVALUATION, CORROSION EXISTS IN MORE THAN ONE CROSS-SECTIONAL AREA THEREFORE SEAT TRACK IS OUT OF LIMITS IAW CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND REPLACED RH SIDE SEAT RAIL FS 483-57
- [SDR V0XD202002190001](https://openairdocs.org/sdr/V0XD202002190001.md): Floorbeam · corroded · Feb 19, 2020 · N340CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH F.S. 280.00 FLOOR BEAM CORRODED AND RH F.S. 280.00 FLOOR BEAM CRACKED AND CORRODED. CORRECTIVE ACTION TO BE ACCOMPLISHED AVMAX W/O 80799 W/C 1126.
- [SDR V0XD20200209601](https://openairdocs.org/sdr/V0XD20200209601.md): Drag Angle · cracked · Feb 6, 2020 · N340CA · Cndair CL6002C10 · Vertical Stabilizer
  > LH FWD AND AFT VERTICAL STAB DRAG ANDGLES CRACKED. CORRECTIVE ACTION: REPAIRED LH FWD AND AFT DRAG ANGLE IAW BOMBARDIER REO# 670-55-31-018 REV A DATED 2016-11-10, BOMBARDIER REO# 670-55-31-128 DATED 2020-01-29 AND GOJET EO C700-55MR-001O DATED 11-24-2018.
- [SDR V0XD20200502001](https://openairdocs.org/sdr/V0XD20200502001.md): Bulkhead Web · corroded · Feb 5, 2020 · N340CA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > R/H BULKHEAD WEB AT F.S. 280.00 CORRODED. CORRECTIVE ACTION: REPAIRED R/H BULKHEAD WEB AT F.S. 280.00 BY REMOVING CORREDED BULKHEAD WEB, FABRICATING AND INSTALLING NEW BULKHEAD WEB IAW BOMBARDIER REO# 670-53-11-594 REV A DATED: 2015/06/26
- [SDR V0XD20200217002](https://openairdocs.org/sdr/V0XD20200217002.md): Drag Angle · cracked · Jan 31, 2020 · N340CA · Cndair CL6002C10 · Vertical Stabilizer
  > RH FWD AND AFT VERTICAL STABILIZER DRAG ANGLES CRACKED. CORRECTIVE ACTION: REPAIRED RH FWD AND AFT DRAG ANGLES IAW BOMBARDIER REO# 670-55-31-018 REV A DTED 2019-11-10, BOMBARDIER REO# 670-55-31-128 DATED 2020-01-29, AND GOJET EO C700-55MR -001-O DATED 11-24-20
- [SDR V0XD20200217001](https://openairdocs.org/sdr/V0XD20200217001.md): Skin · dented · Jan 31, 2020 · N340CA · Cndair CL6002C10 · Trailing Edge Flaps
  > RH INBRD FLAP DENTED ON LOWER SKIN AND RIB BETWEEN FLS. 30.00 AND 36.00 APPOXIMATLEY 9.1 INCHES FROM TRAILING EDGE. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR TO RH INBRD FLAP LOWER SKIN BY CUTTING OUT DAMAGED SKIN, FABRICATING AND INSTALLING REPPAIR PA

Next page: https://openairdocs.org/aircraft/N340CA/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 = 'N340CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N340CA/reports

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