# Service difficulty reports: N692CA

A list on [N692CA](https://openairdocs.org/aircraft/N692CA.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 · 203 reports

- [SDR SWIA2025112800007](https://openairdocs.org/sdr/SWIA2025112800007.md): Windshield · damaged · Nov 27, 2025 · N692CA · Cndair CL6002D24 · Flight Compartment Windows
  > FO FRONT WINDSHIELD CAUGHT FIRE AT 3000 FEET QRH COMPLETE (FLIGHT 3726) AFTER INSPECTION, FOUND RH FO WINDSHEILD OUTBOARD AND MID GLASS PANES TO BE CRACKED WITH SIGNS OF ARCHING AT THE TERMINAL BLOCK. INBOARD GLASS PANES REMAIN INTACT. REF AML #1757968
- [SDR SWI2025F00855](https://openairdocs.org/sdr/SWI2025F00855.md): Proximity Sensor · out of rig · Jul 3, 2025 · N692CA · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE AFTER SELECTING GEAR UP, NOSE WHEEL WOULDN?T SHOW UP. GEAR WAS SELECTED UP AT 195 KNOTS, ALL HYDRAULIC PUMPS ACTIVE. RAN QRH, PUT GEAR DOWN, ALL GEAR SHOWED DOWN AND GREENC: MEL 32-30-1CAT A DUE ONE FLIGHT DAY 07/04/2025**CAT II DOWNGRADED** B1-0
- [SDR SWIA202505270022](https://openairdocs.org/sdr/SWIA202505270022.md): Skin · burned · May 22, 2025 · N692CA · Cndair CL6002D24 · Elevator, Plate/Skin
  > DURING THE EXTERNAL AIRCRAFT LIGHTNING INSPECTION, FOUND ONE BURN MARK ON THE UPPER SKIN OF THE LH ELEVATOR IN BETWEEN RIB 8 AND RIB 9 ON THE TRAILING EDGE IN BETWEEN TWO RIVETS. (FILED CLOSED)PERFORMED A NON FLUSH, REPAIR ON THE UPPER SKIN OF THE LH ELEVATOR
- [SDR SWIA202505230022](https://openairdocs.org/sdr/SWIA202505230022.md): Skin · damaged · May 22, 2025 · N692CA · Cndair CL6002D24 · Elevator, Plate/Skin
  > DURING THE EXTERNAL AIRCRAFT LIGHTNING INSPECTION, FOUND ONE BURN MARK ON THE UPPER SKIN OF THE LH ELEVATOR IN BETWEEN RIB 8 AND RIB 9 ON THE TRAILING EDGE IN BETWEEN TWO RIVETS. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F00468](https://openairdocs.org/sdr/SWI2024F00468.md): Skin · damaged · Apr 24, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90438-REO 690-53-00-495 MXCODEID74141-PR - REPAIRED DAMAGED AREA LOCATED AT FS169.00 ABOVE STGR 17LH PER REO 690-53-00-495 REV -- DATED 9-22-22. REF CP 25542313 FOR REQUIRED NDT. REPAIR IS VALID FOR 3550 HOURS FROM IN
- [SDR SWI2024F00467](https://openairdocs.org/sdr/SWI2024F00467.md): Skin · damaged · Apr 24, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90418-SRM 53-00-00 692CA CP25533450-PR1 - DUE TO TEMPORARY REPAIR OF LIGHTNING STRIKE DAMAGE AT FS265.00 ON THE SECOND RIVET BELOW STGR 20LH IN REF TO CRJ 900 SRM 53-00-00 TYPE 3, COMPLY WITH PERMANENT REPAIR AT THE N
- [SDR SWI2024F00466](https://openairdocs.org/sdr/SWI2024F00466.md): Access Panel · damaged · Apr 24, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90439-REO 690-53-00-495 MXCODEID74143-PR - REPAIRED DAMAGED AREA L LOCATED BETWEEN FUSELAGE ACCESS PANEL 121AL AND FS193.00 ABOVE STGR 23LH PER REO 690-53-00-495 REV -- DATED 9-22-22. REF CP 25542313 FOR REQUIRED NDT.
- [SDR SWI2024F00465](https://openairdocs.org/sdr/SWI2024F00465.md): Skin · damaged · Apr 24, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90440-REO 690-53-00-495 MXCODEID74145-PR - REPAIRED DAMAGED AREA ON FUSELAGE SKIN LOCATED ON FS193.00 BETWEEN THE THIRD AND FOURTH RIVET BELOW STGR 23LH PER REO 690-53-00-495 REV -- DATED 9-22-22. REF CP 25542313 FO
- [SDR SWI2024F00464](https://openairdocs.org/sdr/SWI2024F00464.md): Skin · damaged · Apr 24, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90441-REO 690-53-00-495 MXCODEID74149-PR - REPAIRED DAMAGED AREA ON FUSELAGE SKIN LOCATED ON STRG 26LH BETWEEN THE 7TH AND 8TH RIVET FWD OF FS295.00 PER REO 690-53-00-495 REV -- DATED 9-22-22. REF CP 25542313 FOR REQUI
- [SDR SWI2024F00463](https://openairdocs.org/sdr/SWI2024F00463.md): Skin · damaged · Apr 24, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90436-REO 690-53-00-495 MXCODEID74138-PR - REPAIRED DAMAGED AREA LOCATED AT FS173.00 FWD OF TRU SKIN CUTOUT ABOUT HALF WAY UP PER REO 690-53-00-495 REV -- DATED 9-22-22. REF CP 25542313 FOR REQUIRED NDT. REPAIR IS VALI
- [SDR SWIA2024053000424](https://openairdocs.org/sdr/SWIA2024053000424.md): Skin · damaged · Apr 24, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90415-SRM 53-00-00 692CA CP25533438-PR1 - DUE TO TEMPORARY REPAIR OF LIGHTNING STRIKE DAMAGE AT FS250.00 ON THE FIRST RIVET BELOW STGR 19LH IN REF TO CRJ 900 SRM 53-00-00 TYPE 3, COMPLY WITH PERMANENT REPAIR AT THE NE
- [SDR SWI2024F00483](https://openairdocs.org/sdr/SWI2024F00483.md): Intercostal · corroded · Apr 20, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28121378. PAX DOOR AFT DD4 INTERCOSTAL IS CORRODED JOB # HN00153644 (C-CHECK RO 5/28/2024) CORROSION ON PAX DOOR AFT DD4 INTERCOSTAL IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR AFT DD4 INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DW
- [SDR SWI2024F00482](https://openairdocs.org/sdr/SWI2024F00482.md): Intercostal · corroded · Apr 20, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28121337. PAX DOOR AFT DD2 INTERCOSTAL IS CORRODED JOB # HN00153642 (C-CHECK RO 5/28/2024) PAX DOOR AFT DD2 INTERCOSTAL ORIGINAL MATERIAL THICKNESS 0.050" IAW CRJ 900 SRM 52-11-06-001-001-A01 EXFOLIATED CORROSION EXIST ON 2 ELEMENT OUT OF LIMITS NO
- [SDR SWI2024F00481](https://openairdocs.org/sdr/SWI2024F00481.md): Intercostal · corroded · Apr 20, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28121383. PAX DOOR AFT DD5 INTERCOSTAL IS CORRODED JOB # HN00153646 (C-CHECK RO 5/28/2024) CORROSION ON PAX DOOR AFT DD5 INTERCOSTAL IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR AFT DD5 INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DW
- [SDR SWIA2024052900420](https://openairdocs.org/sdr/SWIA2024052900420.md): Intercostal · corroded · Apr 20, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28121372. PAX DOOR AFT DD3 INTERCOSTAL IS CORRODED JOB # HN00153643 (C-CHECK RO 5/28/2024) CORROSION ON PAX DOOR AFT DD3 INTERCOSTAL IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR AFT DD3 INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DW
- [SDR SWI2024F00474](https://openairdocs.org/sdr/SWI2024F00474.md): Intercostal · corroded · Apr 14, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28091591 PAX DOOR FWD DD3 INTERCOSTAL IS CORRODED JOB # HN00152079 (C-CHECK RO 5/28/2024) REMOVED AND REPLACED WITH NEW PAX DOOR FWD DD3 INTERCOSTAL AND BRACKET IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. LEAK CHECK GOOD. COMPLIED
- [SDR SWI2024F00473](https://openairdocs.org/sdr/SWI2024F00473.md): Channel · corroded · Apr 14, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERNAL STRUCTURE LOWER CHANNEL COMMON TO HINGE HAS HEAVY EXFOLIATING CORROSION AT LOWER & UPPER FLANGES FWD & AFT OF FS.320. (C-CHECK RO 5/28/2024) REMOVED FOR REPLACEMENT DISCREPANT PAX DOOR DATUM 8 FRAME CHANNEL REF. CRJ900 SRM TASK 51-42-06
- [SDR SWI2024F00472](https://openairdocs.org/sdr/SWI2024F00472.md): Bracket · corroded · Apr 14, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28090759 PAX DOOR FWD DD6 INTERCOSTAL AND CLEAT HAS EXFOLIATED CORROSION JOB # HN00151980 (C-CHECK RO 5/28/2024) PAX DOOR FWD DD6 INTERCOSTAL AND CLEAT AND BRACKET ORIGINAL MATERIAL THICKNESS 0.050" IAW CRJ 900 SRM 52-11-06-001-001-A01 EXFOLIATED CO
- [SDR SWI2024F00471](https://openairdocs.org/sdr/SWI2024F00471.md): Intercostal · corroded · Apr 14, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28091614 PAX DOOR FWD DD4 INTERCOSTAL IS CORRODED JOB # HN00152081 (C-CHECK RO 5/28/2024) PAX DOOR FWD DD4 INTERCOSTAL AND CLEAT ORIGINAL MATERIAL THICKNESS 0.050" IAW CRJ 900 SRM 52-11-06-001-001-A01 EXFOLIATED CORROSION EXIST ON 2 ELEMENT OUT OF L
- [SDR SWIA2024053000414](https://openairdocs.org/sdr/SWIA2024053000414.md): Intercostal · corroded · Apr 14, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28091580 PAX DOOR FWD DD5 INTERCOSTAL IS CORRODED JOB # HN00152077 (C-CHECK RO 5/28/2024) PAX DOOR FWD DD5 INTERCOSTAL AND BRACKET ORIGINAL MATERIAL THICKNESS 0.050" IAW CRJ 900 SRM 52-11-06-001-001-A01 EXFOLIATED CORROSION EXIST ON 2 ELEMENT OUT OF
- [SDR SWI2024F00455](https://openairdocs.org/sdr/SWI2024F00455.md): Floorbeam · corroded · Apr 12, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H FS280 CROSSBEAM CORRODED ON UPPER FLANGE AT APPROXIMATELY LBL 13 (C-CHECK RO 5/28/2024) (C-CHECK RO 5/28/2024) BLEND CORROSION ON L/H FS 280.0 CROSSBEAM REF CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW L/H
- [SDR SWI2024F00461](https://openairdocs.org/sdr/SWI2024F00461.md): Skin · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FORWARD BAGGAGE BAY DOOR SURROUND LOWER INNER SKIN CORRODED BETWEEN JOINT PLATES FS519.64 - FS562.64, STGR25L (MARKED) (C-CHECK RO 5/28/2024) BLENDED-OUT CORROSION, INSTALLED (41 EA) NEW FASTENERS AND RESTORED FINISH REWORKED AREAS AT FORWARD BAGGAGE BAY
- [SDR SWI2024F00460](https://openairdocs.org/sdr/SWI2024F00460.md): Plate · bent · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY PLATE BENT. FS661+16 STGR27. (MARKED) (C-CHECK RO 5/28/2024) FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED FORWARD BAGGAGE BAY PLATE AT FS661+16 STGR27 IRT CRJ900 SRM 51-42-06-001-001-A01 & DWG SH690-33600 REV AH. COMPLIED WITH SKYWES
- [SDR SWI2024F00459](https://openairdocs.org/sdr/SWI2024F00459.md): Skin · damaged · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FORWARD BAGGAGE BAY FORWARD DOOR SURROUND LOWER INNER SKIN HAS EDGE DAMAGE AT THE FORWARD AND AFT DOOR HINGE. (MARKED) (C-CHECK RO 5/28/2024) BLENDED OUT EDGE DAMAGE ON FWD BAGGAGE BAY FWD DOOR LOWER INNER SKIN AT FWD AND AFT DOOR HINGE REF CRJ 900 SRM 51
- [SDR SWI2024F00458](https://openairdocs.org/sdr/SWI2024F00458.md): Skin · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Cargo/Baggage Doors
  > FORWARD BAGGAGE BAY FWD DOOR SURROUND INNER SKIN HAS CORROSION FS519.64 STGR25L - STGR24L. (MARKED) (C-CHECK RO 5/28/2024) REMOVED CORROSION ON FORWARD BAGGAGE BAY FWD DOOR SURROUND INNER SKIN FS519.64 STGR25L - STGR24L REF CRJ900 SRM 51-21-06-001-001-A01
- [SDR SWI2024F00453](https://openairdocs.org/sdr/SWI2024F00453.md): Floorbeam · cracked · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR BEAM LBL12 CRACKED IN THE OUTBOARD RADIUS AT THE AFT END OF THE BEAM, FS280.00. (MARKED) (C-CHECK RO 5/28/2024) INSTALLED NEW FLOOR BEAM SECTION BETWEEN FS280.00 - FS265 LBL 12 AND INSTALLED -35 INBD UPPER REPAIR ANGLE, -37 INBD LOWER REPAIR
- [SDR SWI2024F00452](https://openairdocs.org/sdr/SWI2024F00452.md): Floorbeam · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR SUPPORT ANGLE ON THE FORWARD SIDE OF THE FS280.00 BEAM IS CORRODED. LBL9 - RBL9. (C-CHECK RO 5/28/2024) FOUND COCKPIT FLOOR SUPPORT ANGLE OUT OF LIMITS REF CRJ900 SRM 53-00-00-101-001-A01 AND CRJ900 SRM 53-11-43-001-001-A01 AND INSTALLED NEW
- [SDR SWI2024F00451](https://openairdocs.org/sdr/SWI2024F00451.md): Frame · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME FS661+74 LOWER FLANGE HAS CORROSION STGR26L - 26R. (MARKED) (C-CHECK RO 5/28/2024) REPAIRED FRAME FS661+74 LOWER FLANGE AT STGR26L - 26R BY COMPLYING REO 690-53-31-829 REV -- DATED 2024-04-18 AND CRJ900 SRM 51-21-06-001-001-A01. COMPLIED WITH SKYWEST
- [SDR SWI2024F00450](https://openairdocs.org/sdr/SWI2024F00450.md): Bracket · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY BRACKET CORRODED/WORN FS629.00. (MARKED) (C-CHECK RO 5/28/2024) REMOVED CORROSION ON FORWARD BAGGAGE BAY BRACKET FS629.00. REF CRJ900 SRM 51-21-06-001-001-A01.NO DAMAGE ALLOWED IN AREA PER CRJ900 SRM 53-32-58-101-001-A01. REMOVED AND I
- [SDR SWI2024F00449](https://openairdocs.org/sdr/SWI2024F00449.md): Floorbeam · cracked · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR BEAM RBL12, POSSIBLE CRACK IN THE OUTBOARD RADIUS AT THE AFT END OF THE BEAM, FS280.00. (MARKED) (C-CHECK RO 5/28/2024) INSTALLED LOWER ANGLE, UPPER ANGLE AND OUTBOARD WEB ON COCKPIT FLOORBEAM AT RBL 12.00 AND INSTALLED NEW COCKPIT FLOOR SUP
- [SDR SWI2024F00448](https://openairdocs.org/sdr/SWI2024F00448.md): Plate · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY PLATE CORRODED. FS629.00 STGR27. (MARKED) (C-CHECK RO 5/28/2024) REMOVED CORROSION ON FORWARD BAGGAGE BAY PLATE FS629.00 STGR27. REF CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FORWARD BAGGAGE B
- [SDR SWI2024F00447](https://openairdocs.org/sdr/SWI2024F00447.md): Bulkhead Web · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON THE LEFT HAND AFT WEB OF FS280.00 BULKHEAD UNDER THE CORROSION CAP ON TOP OF THE FS280.00 BEAM LBL12. (MARKED) (C-CHECK RO 5/28/2024).CORROSION ON THE LEFT HAND AFT WEB OF FS280.00 BULKHEAD FOUND OUT OF LIMITS REF CRJ900 SRM 53-11-10-201-003-
- [SDR SWI2024F00446](https://openairdocs.org/sdr/SWI2024F00446.md): Skin · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FORWARD BAGGAGE BAY FWD DOOR SURROUND INNER SKIN HAS CORROSION FS562.36 STGR25L - STGR19L. (MARKED) (C-CHECK RO 5/28/2024) REPAIRED FWD BAGGAGE BAY FWD DOOR SURROUND INNER SKIN IAW REO 690-53-31-830 REV. -- DATED 2024-04-22. COMPLIED WITH SKYWEST TASK CARD
- [SDR SWI2024F00445](https://openairdocs.org/sdr/SWI2024F00445.md): Bracket · worn · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY BRACKET CORRODED/WORN FS517.00. (MARKED) (C-CHECK RO 5/28/2024) REMOVED AND INSTALLED 1EA NEW FORWARD BAGGAGE BAY BRACKET P/N SH670-33389-1 PER CRJ-900 SRM 51-45-00-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ-900 SRM 51-42-22-
- [SDR SWI2024F00444](https://openairdocs.org/sdr/SWI2024F00444.md): Bracket · corroded · Apr 11, 2024 · N692CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY BRACKET CORRODED/WORN FS565.00. (MARKED) (C-CHECK RO 5/28/2024) REMOVED DAMAGE ON FORWARD BAGGAGE BAY BRACKET FS565.00 REF.CRJ/900 SRM.51-21-06-001-001-A01. NO DAMAGE IS ALLOWED ON THE FORWARD BAGGAGE BAY STRUCTURE ON REF.CRJ/900 SRM.53
- [SDR SWI2024F00470](https://openairdocs.org/sdr/SWI2024F00470.md): Hinge · chafed · Apr 10, 2024 · N692CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > CAMP # 28069976 PAX DOOR PIANO HINGE (FUSELAGE SIDE) LUGS ARE CHAFED ON THE HINGE LUG LAND JOB # HN00151114 (C-CHECK RO 5/28/2024) REMOVED DAMAGE ON PAX DOOR PIANO HINGE (FUSELAGE SIDE) ON THE HINGE LUG LAND AND PERFORMED REPAIR REF REO 670-53-21-582 REV
- [SDR SWI2024F00469](https://openairdocs.org/sdr/SWI2024F00469.md): Angle · cracked · Apr 10, 2024 · N692CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > OUTBOARD ANGLE OF THE RBL9 TORQUE BOX AT THE 280.00 BEAM IS CRACKED. (C-CHECK RO 5/28/2024) REMOVED AND INSTALLED NEW ANGLE AT RBL9 OUTBOARD SIDE TORQUE BOX & THE 280.00 BEAM REF CRJ900 SRM 51-42-21-001-001-A01 & DWG CC670-34010 REV J. COMPLIED WITH SKYWES
- [SDR SWIA202405300410](https://openairdocs.org/sdr/SWIA202405300410.md): Skin · scratched · Apr 10, 2024 · N692CA · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS COMPARTMENT DOOR, SURROUND STRUCTURE LANDING IS SCRATCHED AND CORRODED. FLAGGED (C-CHECK RO 5/28/2024) REMOVED DAMAGE FROM MAIN AVIONICS COMPARTMENT DOOR SURROUND STRUCTURE LANDING AND COMPLIED WITH WITH ALL STEPS OF REO 690-53-21-032 REV -
- [SDR SWIA2024052900409](https://openairdocs.org/sdr/SWIA2024052900409.md): Support Angle · corroded · Apr 9, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28065387 PAX DOOR FWD SUPPORT ANGLE HAS EXFOLIATED CORROSION AT UPPER TENSION TIE LOCATION JOB # HN00150867 (C-CHECK RO 5/28/2024) REMOVED AND INSTALLED NEW PAX DOOR FWD SUPPORT ANGLE IAW DWG 601R31702 REV -N AND CRJ900 SRM 51-42-06-001-001-A01. COM
- [SDR SWI2024F00434](https://openairdocs.org/sdr/SWI2024F00434.md): Intercostal · cracked · Apr 8, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28061733 PAX DOOR SUSPICIOUS CRACK AT FWD DD1 INTERCOSTAL. JOB # HN00150748 (C-CHECK RO 5/28/2024) NDT FWD DD1 INTERCOSTAL, FOUND CRACK. REMOVED AND INSTALLED NEW PAX DOOR FWD DD1 INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 RE
- [SDR SWI2024F00433](https://openairdocs.org/sdr/SWI2024F00433.md): Intercostal · corroded · Apr 8, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28062274 PAX DOOR DD7A INTERCOSTAL HAS EXFOLIATED CORROSION JOB # HN00150779 (C-CHECK RO 5/28/2024) REMOVED FOR REPLACEMENT DISCREPANT ( HEAVY EXFOLIATING CORROSION OVER ENTIRE SURFACE) INTERCOSTAL DD7A FROM PAX DOOR INTERNAL STRUCTURE REF. CRJ900
- [SDR SWI2024F00432](https://openairdocs.org/sdr/SWI2024F00432.md): Intercostal · cracked · Apr 8, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28061761 PAX DOOR SUSPICIOUS CRACK AT FWD DD7 INTERCOSTAL. JOB # HN00150750 (C-CHECK RO 5/28/2024) NDT FOUND CRACK. REMOVED AND INSTALLED NEW PAX DOOR FWD DD7 INTERCOSTAL AND CLIP IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N LEAK CH
- [SDR SWI2024F00431](https://openairdocs.org/sdr/SWI2024F00431.md): Intercostal · cracked · Apr 8, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR SUSPICIOUS CRACK AT AFT DD1 INTERCOSTAL.JOB # HN00150741 (C-CHECK RO 5/28/2024) NDT FOUND CRACK. REMOVED AND INSTALLED NEW DOOR AFT DD1 INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. LEAK CHECK GOODCOMPLIED WITH SKYWEST
- [SDR SWI2024F00430](https://openairdocs.org/sdr/SWI2024F00430.md): Intercostal · corroded · Apr 8, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28062289 PAX DOOR MID DD3 INTERCOSTAL HAS EXFOLIATED CORROSION JOB # HN00150785 (C-CHECK RO 5/28/2024) REMOVED DISCREPANT INTERCOSTAL DD3 FOR REPLACEMENT REF. CRJ900 SRM TASK 51-42-06-001-001-A01 & SRM TASK 51-42-21-001-001-A01. ORDERED AND RECEIV
- [SDR SWIA2024053000408](https://openairdocs.org/sdr/SWIA2024053000408.md): Intercostal · cracked · Apr 8, 2024 · N692CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CAMP # 28061709 PAX DOOR SUSPICIOUS CRACK AT AFT DD7 INTERCOSTAL JOB # HN00150746 (C-CHECK RO 5/28/2024) REMOVED FOR REPLACEMENT DISCREPANT INTERCOSTAL DD7 AFT FROM PAX DOOR INTERNAL STRUCTURE REF. CRJ900 SRM TASK 51-42-06-001-001-A01. ORDERED AND RECEIVED
- [SDR SWI2024F00429](https://openairdocs.org/sdr/SWI2024F00429.md): Door Frame · corroded · Apr 7, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR FWD FORMER AT F/S 311.75 HAS EXFOLIATED CORROSION AROUND TENSION TIES JOB # HN00150561 (C-CHECK RO 5/28/2024) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER IAW DWG 601R31702 REV. N AND CRJ 900 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD. COMPLIED W
- [SDR SWI2024F00428](https://openairdocs.org/sdr/SWI2024F00428.md): Door Frame · corroded · Apr 7, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR FRAME F/S 320.00 HAS EXFOLIATED CORROSION JOB # HN00150564 (C-CHECK RO 5/28/2024) CORROSION ON PAX DOOR FRAME F/S 320.00 IS OUT OF LIMITS. REMOVED AND WET INSTALLED NEW FS320.00 FRAME. CRJ900 SRM TASK 51-42-06-001-001-A01, SRM TASK 51-42-21-001-00
- [SDR SWI2024F00427](https://openairdocs.org/sdr/SWI2024F00427.md): Door Frame · corroded · Apr 6, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR FRAME FS338.963 CORRODED BETWEEN INTERCOSTAL DD6 AND DD5. (C-CHECK RO 5/28/2024) REMOVED AND REPLACED WITH NEW PAX DOOR FRAME FS338.963 BETWEEN INTERCOSTAL DD6 AND DD5 REF CRJ 900 SRM TASK 51-42-06-001-001-A01, CRJ 900 SRM TASK 51-23-00-001-0
- [SDR SWI2024F00425](https://openairdocs.org/sdr/SWI2024F00425.md): Skin · gouged · Apr 4, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AIRCRAFT LOWER EXTERNAL FUSELAGE IN BETWEEN FS 913 JUST FWD OF FS 927 THERE IS A DEEP SCREW GOUGE ON FUSELAGE SKIN.(MARKED) AT STR27 MX# 28040473 (C-CHECK RO 5/28/2024) REPAIRED AIRCRAFT LOWER EXTERNAL FUSELAGE SKIN BETWEEN FS 913 JUST FWD OF FS 927 REF RE
- [SDR SWIA2024053000402](https://openairdocs.org/sdr/SWIA2024053000402.md): Doubler · gouged · Apr 2, 2024 · N692CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > GOUGING MARKS ON EXTERNAL SKIN OF DOUBLER, FWD ATG ANTENNA MATING SURFACE BETWEEN FS 501.00 - 517.00, STGR 25R - 26R. MARKED. (C-CHECK RO 5/28/2024) REMOVED AND INSTALLED NEW FWD ATG ANTENNA DOUBLER BETWEEN FS501.00 - FS517.00 REF CRJ900 SRM 51-42-20-001

Next page: https://openairdocs.org/aircraft/N692CA/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 = 'N692CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N692CA/reports

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