# Service difficulty reports: N355CA

A list on [N355CA](https://openairdocs.org/aircraft/N355CA.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 · 245 reports

- [SDR REXA202609241877](https://openairdocs.org/sdr/REXA202609241877.md): Lamp · inoperative · Sep 23, 2026 · N355CA · Cndair CL6002C10 · Emergency Lighting
  > 2 EMERGENCY EXIT FLOODLIGHT LAMPS INOPERATIVE. R & R NR 2 EMERGENCY EXIT FLOODLIGHT LAMPS P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD.
- [SDR REXA2026071001072](https://openairdocs.org/sdr/REXA2026071001072.md): Lamp · inoperative · Jul 10, 2026 · N355CA · Cndair CL6002C10 · Emergency Lighting
  > THREE EMERGENCY FLOODLIGHT LAMPS INOPERATIVE. R & R THE THREE EMERGENCY FLOODLIGHT LAMPS IAW AMM 33-51-05. OPS CHECKED GOOD.
- [SDR REXA2025081200799](https://openairdocs.org/sdr/REXA2025081200799.md): Frame · corroded · Aug 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND FRAME AT FS 1015 BETWEEN STGR 21L-25R. REPAIRED FRAME AT F.S.1015 BETWEEN STGR 21L TO 25R IAW ENDEAVOR AIR EA CRJ753-19701 REV IR DATED 7/10/2025.
- [SDR REXA2025090400847](https://openairdocs.org/sdr/REXA2025090400847.md): Stringer Splice · corroded · Aug 6, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND HEAVY CORROSION ON STGR24R SPLICE AT FS333 REMOVED STGR24R SPLICE AT FS333 FOR REPLACEMENT IAW CRJ700 SRM 51-42-06-001-001-A01 DRILLED AND LOCATED STGR24R SPLICE PN:SH670-32429-2 IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED STGR24R SPLICE PN:SH670-3242
- [SDR REXA2025081200798](https://openairdocs.org/sdr/REXA2025081200798.md): Frame · damaged · Aug 6, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 280 FRAME HAS 5EA OVERSIZED HOLES (PREVIOUS REPAIR) BETWEEN STGR 17L AND STGR 18L. COMPLIED WITH MHIRJ REO 670-53-11-2156 REV -- DATED 2025-07-28 TEMPORARY REPAIR FOR OVERSIZED HOLES ON F.S.280 FRAME BETWEEN STR17L AND STR18L.
- [SDR REXA2025100600907](https://openairdocs.org/sdr/REXA2025100600907.md): Splice Angle · corroded · Jul 29, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF BOTH LATCH PIN INTERCOSTALS AT STGR 27 FOUND CORROSION ON ATTACHED FLANGE OF FS364 BL0. REMOVED AND REPLACED BROKEN SPLICE (SP124) (P/N: M81714/12-20D-2) (P/N: M39029/1-101) IAW CRJ 700 ESPM 20-44-09 AND IAW CRJ 700 ESPM 20-16-43, OPERATIONAL
- [SDR REXA2025082900843](https://openairdocs.org/sdr/REXA2025082900843.md): Frame · corroded · Jul 29, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 319.70 LT IS CORRODED BETWEEN S20L AND S21L. REMOVED FRAME IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, ORIGINAL THICKNESS 0.050", REMAINING THICKNESS 0.036" DAMAGE IS OUT OF LIMITS, FRAME REQUIRES REPLACEMENT. DRIL
- [SDR REXA2025082500831](https://openairdocs.org/sdr/REXA2025082500831.md): Stringer Splice · corroded · Jul 28, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STGR 21L AFT SPLICE AT FS374. UPON FURTHER INVESTIGATION FOUND STGR 21L AFT SPLICE AT FS374 TO BE HEAVILY CORRODED TO THE POINT OF 100% MATERIAL LOSS AND OUT OF LIMITS IAW CRJ700 SRM 53-21-03-101-006-A01. LOCATED AND DRILLED NEW SERVICEABL
- [SDR REXA2025082900842](https://openairdocs.org/sdr/REXA2025082900842.md): Stringer · corroded · Jul 27, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND ELONGATED FASTENER HOLES ON STGR 21L BETWEEN FS 333.00-FS349.00. REMOVED AND REPLACED SKIN RIVETS FROM STGR 21L FS333- FS485 IAW CRJ700 SRM 51-42-06-001-001-A01. REMOVED AND REINSTALLED FLOOR LEVEL INTERCOSTAL AT FS364-FS379 LBL 37, STRAP ON STGR21L AT
- [SDR REXA2025072800762](https://openairdocs.org/sdr/REXA2025072800762.md): Stringer · corroded · Jul 27, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER AT 20R IS CORRODED BETWEEN FS 364.00 AND 409.00. INSTALLED NEW STGR20R PN:SH670-31405-2S BETWEEN FS364 - FS477 IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR REXA2025072800761](https://openairdocs.org/sdr/REXA2025072800761.md): Floorbeam · corroded · Jul 27, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > R/H F.S. 280 BEAM CAP IS CORRODED BETWEEN BL0 TO RBL9. REPAIRED FS 280 CROSSBEAM IAW MHIRJ GREO 670-53-11-579, REV -B, DATED 2013/05/01 AND 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2025072100748](https://openairdocs.org/sdr/REXA2025072100748.md): Stringer · corroded · Jul 21, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND AROUND THE RIVETS ON STRINGER 22R BETWEEN FS 280 AND FS 295. REMOVED CORRODED STRINGER 22R FROM F.S.280 TO F.S.333 AND INSTALLED NEW SERVICABLE STRINGER P/N SH670-31210-2U IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2025120200997](https://openairdocs.org/sdr/REXA2025120200997.md): Stringer · corroded · Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STGR 23L BETWEEN FS 1015-1031. CUT AWAY AND REMOVED SHARP EDGES OF STRINGER 23L AT FS1000+9 AND FS1051+6 FOR REMOVAL IAW CRJ700 SRM 53-00-03-201-001-A01 STEPS 5A(1-2), REPAIR S6232. FABRICATED, LOCATED, AND DRILLED: STRINGER SECTION FS1000+9
- [SDR REXA2025090300846](https://openairdocs.org/sdr/REXA2025090300846.md): Intercostal · corroded · Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT 20R IS CORRODED BETWEEN FS 310.00 AND 319.70. INSTALLED NEW INTERCOSTAL P/N: SH670-32047-1 FROM STR20R BETWEEN FS310.00 TO FS319.70 IAW CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2025072100747](https://openairdocs.org/sdr/REXA2025072100747.md): Intercostal · corroded · Jul 15, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD2 AFT FOUND TO BE CORRODED REQUIRES REPLACEMENT. REMOVED PAX DOOR AFT DD2 INTERCOSTAL IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 INSTALLED NEW SERVICEABLE PAX DOOR AFT DD2 INTERCOSTAL IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 NEW SERVICEABLE PAX DOOR
- [SDR REXA2025071600743](https://openairdocs.org/sdr/REXA2025071600743.md): Stringer · corroded · Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L IS CORRODED BETWEEN FS 265.00 AND 280.00 REPAIRED STRINGER 26L BETWEEN F.S.265 TO F.S.280 IAW MHIRJ REO 670-53-11-2158 REV -- DATED 2025-07-14
- [SDR REXA2025071600742](https://openairdocs.org/sdr/REXA2025071600742.md): Stringer · corroded · Jul 15, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R IS CORRODED BETWEEN FS 295.00 AND 310.00. UPON FURTHER INVESTIGATION, FOUND STR 20R TO BE CORRODED BETWEEN FS 295 AND FS 310. REMOVED STGR 20R FROM FS280-FS319 FOR REPLACEMENT IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED STGR 20R PN:SH670-312
- [SDR REXA2025071500725](https://openairdocs.org/sdr/REXA2025071500725.md): Stringer · corroded · Jul 11, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER AT 19R IS CORRODED BETWEEN FS 394.00 AND 409.00. RECEIVED AND COMPLIED WITH ENDEAVOR AIR EA CRJ753-19649 REV IR DATED 7-1-2025
- [SDR REXA2025120200996](https://openairdocs.org/sdr/REXA2025120200996.md): Hinge · damaged · Jul 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR FUSELAGE SIDE HINGE LUGS (13 OF THE 27 AFT LUGS) EXCEEDS.295"" AND REQUIRES REPAIR OR REPLACEMENT. IAW CRJ 700 SRM 53-21-23-201-A01. COMPLIED WITH MHI RJ REO 670-53-21-2676 REV -.
- [SDR REXA2025082500830](https://openairdocs.org/sdr/REXA2025082500830.md): Stringer · corroded · Jul 7, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 23L IS CORRODED AT FS 581 TO FS 597 (MARKED WITH RED TAPE) REPAIRED STR 23L IAW ENDEAVOR AIR EA CRJ753-19988 REV IR DATED 8-14-25
- [SDR REXA2025080600784](https://openairdocs.org/sdr/REXA2025080600784.md): Angle · damaged · Jul 7, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT SUPPORT ANGLE FOUND EXTRA HOLE FROM PREVIOUS REPAIR REQUIRE REPLACEMENT LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT SUPPORT ANGLE P/N#601R318732-3 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01. REFERENCE HN00249365 FOR INSTALLATION
- [SDR REXA2025070900713](https://openairdocs.org/sdr/REXA2025070900713.md): Former · corroded · Jul 6, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INSIDE ACCESS HOLE 832FL FWD. FORMER IS CORRODED AND APPEARS ALSO TO GO UNDER FORMER REMOVED PAX DOOR FWD FORMER IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01, AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR FWD FORMER P/N: 6
- [SDR REXA2025092300874](https://openairdocs.org/sdr/REXA2025092300874.md): Angle · corroded · Jul 2, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF PASSENGER DOOR SURROUND MID CAP ANGLE FOUND KICK PLATE ANGLE TO BE CORRODED, REMOVED AND REPLACED KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01, LOCATED AND DRILLED UP A SERVICABLE KICKPLATE ANGLE IAW CRJ700 SRM 5
- [SDR REXA2025080600783](https://openairdocs.org/sdr/REXA2025080600783.md): Frame · corroded · Jun 24, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR F.S. BETWEEN FWD DD4 AND DD5 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT REMOVED DAMAGED FRAME. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR FRAME, FS313.56, BETWEEN DD4 & DD5 P/N# 601R318086-1 IAW CRJ-700 SRM TASK 51-40-11-001-00
- [SDR REXA2025080600782](https://openairdocs.org/sdr/REXA2025080600782.md): Former · corroded · Jun 24, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER FOUND TO BE CORRODED REQUIRES REPLACEMENT REMOVED DAMAGED AFT FORMER. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR AFT FORMER FS 347 P/N#601R318034-5 IAW CRJ-700 SRM TASK 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-00
- [SDR REXA2025071100720](https://openairdocs.org/sdr/REXA2025071100720.md): Intercostal · corroded · Jun 24, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR MID DD4 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT INSTALLED NEW SERVICEABLE PAX DOOR MID DD4 INTERCOSTAL P/N:601R318081-1S IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01
- [SDR REXA2025072100746](https://openairdocs.org/sdr/REXA2025072100746.md): Frame · corroded · Jun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 549 FRAME CORRODED BETWEEN STR 17L AND STR 18L. REPAIRED IAW ENDEAVOR AIR EA CRJ753-19587 REV IR DATED 06-24-2025.
- [SDR REXA2025070900712](https://openairdocs.org/sdr/REXA2025070900712.md): Stringer · corroded · Jun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED BETWEEN FS 280.00 AND 319.70. REMOVED CORROSION ON STR 26R BETWEEN FS 280 AND FS 310 IAW CRJ700 SRM 51-21--06-001-001-A01. STR 26R FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS BETWEEN FS 280 AND FS 310 IN MULTIPLE AREAS IAW CR
- [SDR REXA2025070900711](https://openairdocs.org/sdr/REXA2025070900711.md): Stringer · corroded · Jun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R IS CORRODED BETWEEN FS 295.00 AND 310.00 REMOVED CORROSION FROM STR 25R BETWEEN 295 & FS 310 IAW CRJ700 SRM 51-- 21-06-001-001-A01. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM TASK 53-21-- 03-101-002-A01. FOUND DAMAGE TO BE OUT OF LIMITS. R & R STR
- [SDR REXA2025062300675](https://openairdocs.org/sdr/REXA2025062300675.md): Stringer · corroded · Jun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > JOINT PIECE SPLICE (P/N:SH670-32429-2) AT FS333 STR 22R FOUND TO BE CORRODED REMOVED UNSERVICEABLE JOINT PIECE SPLICE (P/N:SH670-32429-2) AT FS333 STGR 22R IAW CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE JO
- [SDR REXA2025062300674](https://openairdocs.org/sdr/REXA2025062300674.md): Stringer · corroded · Jun 22, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER AT 22R IS CORRODED BETWEEN FS 333.00 AND 349.00. REMOVED UNSERVICEABLE STR 22R (P/N:SH670-31379-1) BETWEEN FS333-FS349 IAW CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STR 22R (P/N:SH670-31379-1) BE
- [SDR REXA2025092300872](https://openairdocs.org/sdr/REXA2025092300872.md): Floor Support · corroded · Jun 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT IS CORRODED BETWEEN F.S. 501 - 549. R & R ENTIRE FLOOR SUPPORT RBL 9 FS 477 - 571 IAW MHI RJ REO 670-53-31-1054 REV --. FABRICATED RBL9 FLOOR SUPPORT FROM FS 477 - 571 USING EXTRUSION, LOCATED, DRILLED UPPER & LOWER FLANGE IAW SRM 53-00-4
- [SDR REXA2025072800760](https://openairdocs.org/sdr/REXA2025072800760.md): Floorbeam · corroded · Jun 10, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > F.S. 280 BEAM CAP IS CORRODED BETWEEN LBL9 TO LBL27. REMOVED FS 280.00 L/H CROSSBEAM BETWEEN LBL 0-LBL 42, IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED NEW SERVICEABLE FS 280.00 L/H CROSSBEAM PN CC670-34
- [SDR REXA2025082900841](https://openairdocs.org/sdr/REXA2025082900841.md): Stringer · corroded · Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER AT 24R IS CORRODED BETWEEN BS 333.- 349. BLENDED CORROSION ON STRINGER IAW SRM 51-21-06-001-001-A01. NO DAMAGE IS ALLOWED TO STRINGER 24R IAW SRM 53-21-03-101-006-A01. PERFORMED UT THICKNESS ON REWORKED AREAS ON STRINGER IAW NDTM PT 1 51-20-004-270-
- [SDR REXA2025082600835](https://openairdocs.org/sdr/REXA2025082600835.md): Stringer · corroded · Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER AT 19L IS CORRODED BETWEEN FS 379.00 AND 453.00. BLENDED CORROSION FROM STGR 19L BETWEEN FS379 - FS453 FOUND MULTIPLE SPOT OF 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 51-21-06-001-001-A01, SRM 53-21-03-101-005-A01. REMOVED AND REP
- [SDR REXA2025081800749](https://openairdocs.org/sdr/REXA2025081800749.md): Stringer · corroded · Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 19R IS CORRODED BETWEEN F.S. 565 TO F.S. 581. BLENDED CORROSION IAW SRM 53-31-03-101-004-A04. PERFORMED LPI ON REWORKED AREAS ON S19R BETWEEN BS 565 AND 581 IAW NDTM PT 1 51-20-008-230-A01. NO INDICATIONS NOTED. PERFORMED UT THICKNESS ON REWORKED AREAS
- [SDR REXA2025081300804](https://openairdocs.org/sdr/REXA2025081300804.md): Stringer · corroded · Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER AT 21R IS CORRODED BETWEEN FS 394.00 AND 453.00. REMOVED CORROSION 100% MATERIAL LOSS STRINGER REQUIRE REPLACEMENT IAW CRJ700 SRM 51-21-06-001-001-A01, REMOVED STGR21R FROM FS394 - FS477 FOR REPLACEMENT IAW CRJ700 SRM 51-42-06-001-001-A01 INSTALLE
- [SDR REXA2025071500739](https://openairdocs.org/sdr/REXA2025071500739.md): Stringer · corroded · Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R IS CORRODED BETWEEN FS 295.00 AND 310.00. REMOVED CORROSION ON STR 19R BETWEEN FS 295 AND FS 310 IAW CRJ700 SRM 51-21-06-001-001-A01, FOUND TO HAVE 100% MATERIAL LOSS. REMOVED AND REPLACED STGR 19R FROM FS280-FS310 PN:SH670-31632-1 IAW CRJ700 SRM
- [SDR REXA2025071500723](https://openairdocs.org/sdr/REXA2025071500723.md): Frame · corroded · Jun 9, 2025 · N355CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 319.70 IS CORRODED BETWEEN STGR 25L AND 24R. FS 319 IS FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS DUE TO HAVING 100% MATERIAL LOSE IAW CRJ 700 SRM 53-21-06-101-002-A01 REMOVED PREVIOUS SPLICE REPAIR AND FRAME SEGMENT FROM FS319 STGR25L - STGR23R I
- [SDR REXA2025062500684](https://openairdocs.org/sdr/REXA2025062500684.md): Floor Support · corroded · Jun 7, 2025 · N355CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR BEAM AT LBL 9.00 BETWEEN FS 969.00-1088.20. REPAIRED FLOOR BEAM AT LBL 9.00 BETWEEN FS 969.00-1088.20 IAW ENDEAVOR AIR EA CRJ753-19590 REV IR DATE 06/21/2025. REMOVED AND REINSTALLED CARGO TIE-DOWN TRACK FROM FS988 TO FS1041 IAW CRJ700
- [SDR REXA2025071100719](https://openairdocs.org/sdr/REXA2025071100719.md): Intercostal · corroded · May 23, 2025 · N355CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 IS CORRODED. INSTALLED NEW SERVICEABLE PAX DOOR MID DD3 INTERCOSTAL 601R318056-1 IAW CRJ-700 SRM TASK 51-42-06-001-001-A01 AND TASK 51-42-21-001-001-A01
- [SDR N6WA2017083101](https://openairdocs.org/sdr/N6WA2017083101.md): Warning Message · illuminated · Aug 31, 2017 · N355CA · Cndair CL6002C10 · Door Warning System
  > RIGHT EMERGENCY DOOR CAUTION MESSAGE. OPEN
- [SDR N6WA2017071301](https://openairdocs.org/sdr/N6WA2017071301.md): Warning Message · illuminated · Jul 13, 2017 · N355CA · Cndair CL6002C10 · Door Warning System
  > RIGHT EMERGENCY DOOR CAUTION MESSAGE ON GROUND.
- [SDR N6WA2017070402](https://openairdocs.org/sdr/N6WA2017070402.md): Warning Message · false activation · Jul 4, 2017 · N355CA · Cndair CL6002C10 · Door Warning System
  > RIGHT EMERGENCY EXIT CAUTION MESSAGE ON LANDING. PERFORMED OPS CHECK OF RT EMERG EXIT DOOR IAW AMM 52-21-00. OPS CHECK GOOD.
- [SDR N6WA2017062101](https://openairdocs.org/sdr/N6WA2017062101.md): Warning Light · illuminated · Jun 21, 2017 · N355CA · Cndair CL6002C10 · Door Warning System
  > INTERMITTENT RT EMERGENCY EXIT CAUTION DISPLAYED AFTER LANDING.
- [SDR V0XD201706190003](https://openairdocs.org/sdr/V0XD201706190003.md): Frame · corroded · Jun 2, 2017 · N355CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 863 HAS SIGNS OF CORROSION BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW REO 670-53-51-115, REV A.
- [SDR V0XD201706190002](https://openairdocs.org/sdr/V0XD201706190002.md): Frame · corroded · Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 879 BETWEEN STRINGERS 26L AND 26R HAS SIGNS OF CORROSION. REPAIRED THE FRAME IAW REO 670-53-51-115, REV A.
- [SDR V0XD201706130005](https://openairdocs.org/sdr/V0XD201706130005.md): Seat Track · corroded · Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBD SEAT TRACK FROM BS 581-677 FOUND CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
- [SDR V0XD20170613DP04](https://openairdocs.org/sdr/V0XD20170613DP04.md): Seat Track · corroded · Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRAC,K HAS MULTIPLE SPOTS OF CORROSION FROM BS 485 TO 677. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, SRM 51-40-11, AND REO 670-53-00-343 REV M.
- [SDR V0XD20170613DP03](https://openairdocs.org/sdr/V0XD20170613DP03.md): Seat Track · corroded · Jun 1, 2017 · N355CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE SEAT TRACK FROM BS 669 TO 713 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.

Next page: https://openairdocs.org/aircraft/N355CA/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 = 'N355CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N355CA/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.