# Service difficulty reports: N823SK

A list on [N823SK](https://openairdocs.org/aircraft/N823SK.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 · 163 reports

- [SDR SWIA202509150007](https://openairdocs.org/sdr/SWIA202509150007.md): Warning Message · illuminated · Sep 7, 2025 · N823SK · Cndair CL6002D24 · Central Warning
  > AT CRUISE ALTITUDE HAD WING AND COWL A/I ON,RECIEVED DUCT MON FAULT STATUS MESSAGE THEN RECIEVED LH BLEED DUCT WARNING MESSAGE. LOST CABIN PRESSURIZATION AND STARTED DECENT 10,000 FT DID NOT LAND OVERWEIGHT. (FLIGHT 3601) REFERENCE CP 30807192, 30807206, 3081
- [SDR SWI2025F01193](https://openairdocs.org/sdr/SWI2025F01193.md): Cabin Pressure · failed · Sep 7, 2025 · N823SK · Cndair CL6002D24 · Cabin Pressure Control System
  > AT CRUISE ALTITUDE HAD WING AND COWL A/I ON,RECIEVED DUCT MON FAULT STATUS MESSAGE THEN RECIEVED LH BLEED DUCT WARNING MESSAGE. LOST CABIN PRESSURIZATION AND STARTED DECENT 10,000 FT DID NOT LAND OVERWEIGHT. (FLIGHT 3601 - FILED OPEN)
- [SDR SWIA2024061700424](https://openairdocs.org/sdr/SWIA2024061700424.md): Structure · ground damage · Apr 24, 2024 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > TRANSFER FROM EAML 1337245: PRIOR TO ATTACHING JET BRIDGE TO AIRCRAFT, RAMP CREW DROVE THE BELT LOADER INTO THE AIRCRAFT NEAR BIN 3. ENTIRE AIRCRAFT SHOOK. UPON INSPECTION FRAME APPEARS BENT DIRECTLY UNDER BIN 3. AIRCRAFT SHORED REF ISE-STR-24-023. AIRCRAFT S
- [SDR 2024F00104](https://openairdocs.org/sdr/2024F00104.md): Yoke · damaged · Mar 29, 2024 · N823SK · Cndair CL6002D24 · Engine Mount Section
  > ABNORMAL INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-21-101 PART 4.
- [SDR SWIA20240301228](https://openairdocs.org/sdr/SWIA20240301228.md): Control Panel · faulted · Feb 28, 2024 · N823SK · Cndair CL6002D24 · Rudder Actuator
  > ON CLIMB OUT, RUDDER TRIM RAN AWAY NOSE RIGHT, COMPENSATED WITH RUDDER, WE RAN IT BACK TO CENTER, BEGAN TO RUN AWAY AGAIN AFTER RE-CENTERING. NO LONGER RAN AWAY, QRH RUN, RETURNED TO FIELD. (FLIGHT 3785 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITE
- [SDR SWIA202402290008](https://openairdocs.org/sdr/SWIA202402290008.md): Trim System · malfunctioned · Feb 28, 2024 · N823SK · Cndair CL6002D24 · Rudder Actuator
  > ON CLIMB OUT, RUDDER TRIM RAN AWAY NOSE RIGHT, COMPENSATED WITH RUDDER, WE RAN IT BACK TO CENTER, BEGAN TO RUN AWAY AGAIN AFTER RE-CENTERING. NO LONGER RAN AWAY, QRH RUN, RETURNED TO FIELD. (FLIGHT 3785 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.
- [SDR SWIA2023101200024](https://openairdocs.org/sdr/SWIA2023101200024.md): Unknown · cracked · Sep 24, 2023 · N823SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SCRATCH LOCATED ON LH SIDE OF FUSELAGE BETWEEN FS581.00 AND FS597.00 AND STR16L AND STR17L FOUND TO HAVE CRACKS IN TWO LOCATIONS 2.750 INCHES AFT OF FS581.00 AND 4.25 INCHES AFT OF FS581.00 WHICH WILL REQUIRE REPAIR. THIS HAS BEEN CLASSIFIED AS A MAJOR REPAIR.
- [SDR SWIA202265539](https://openairdocs.org/sdr/SWIA202265539.md): None · cracked · Apr 27, 2022 · N823SK · Cndair CL6002D24 · Window/Windshield System
  > IN FLIGHT RECEIVED A RH WSHLD HEAT CAUTION MESSAGE RAN QRH AND MESSAGE CLEARED. SHORT TIME LATER 2 CRACKS WERE NOTICED ON THE RH WSHLD. ONE CRACK IS APPROXIMATELY 15 INCHES LONG, THE OTHER IS SMALLER LOCATED BOTTOM LEFT HAND CORNER. APPEARS BOTH CRACKS ARE ON
- [SDR SWIA202264454](https://openairdocs.org/sdr/SWIA202264454.md): None · cracked · Feb 5, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > LH JACK PAD INTERCOSTAL ATTACH ANGLE AT FS280.00 CRACKED (C-CHECK RO 2/16/2022) REMOVED AND REPLACED LH JACK PAD INTERCOSTAL ATTACH ANGLE AT FS280.00, LBL1. REF. CRJ 900 SRM 51-42-21-001-001-A01 AND DWG# CC670-32050 REV. NC / COMPLIED WITH SKYWEST TASK
- [SDR SWIA202264453](https://openairdocs.org/sdr/SWIA202264453.md): None · cracked · Feb 5, 2022 · N823SK · Cndair CL6002D24 · Wing Structure
  > NOSE JACKING FITTING AT FS279.00 CRACKED (C-CHECK RO 2/16/2022) REMOVED AND REPLACED NOSE JACKING FITTING AT FS279.00, BL0 REF. CRJ 900 SRM 51-42-21-001-001-A01 AND DWG# CC670-32050 REV. NC / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY / PRESSURE
- [SDR SWIA202264452](https://openairdocs.org/sdr/SWIA202264452.md): None · damaged · Feb 1, 2022 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > FOUND WITH DOUBLE HOLE ANGLE P/N: CC670-34153-4 AT BL 33.00, FS 280.00. (C-CHECK RO 2/16/2022) REMOVED AND REPLACED STIFFENER AT FS280 RBL33.00 REF. CRJ-900 SRM, 51-42-06-001-001-A01 AND DWG CC670-34010 REV-K. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202264451](https://openairdocs.org/sdr/SWIA202264451.md): None · corroded · Jan 14, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 26L SPLICE AT FS333.00 CORRODED (C-CHECK RO 2/16/2022) REMOVED AND REPLACED DAMAGED STRINGER 26L SPLICE. REF. CRJ 900 SRM 51-42-06-001-001-A01 AND DRWG SH670-32420 REV. E. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900
- [SDR SWIA202264450](https://openairdocs.org/sdr/SWIA202264450.md): None · corroded · Jan 13, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 27 SPLICE AT FS333.00 CORRODED (C-CHECK RO 2/16/2022) REMOVED AND REPLACED STR 27 SPLICE AT FS333.00 CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD
- [SDR SWIA202264449](https://openairdocs.org/sdr/SWIA202264449.md): None · corroded · Jan 7, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 22R CLEAT AT FS319.70 CORRODED (C-CHECK RO 2/16/2022) REMOVED AND REPLACED STR 22R CLEAT AT FS319.70 REF. DRWG SH670-31630 REV. K AND CRJ 900 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY. SEE CONTINUATIO
- [SDR SWIA202264448](https://openairdocs.org/sdr/SWIA202264448.md): None · corroded · Jan 7, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 22R SPLICE AT FS333.00 CORRODED (C-CHECK RO 2/16/2022) REMOVED AND INSTALLED NEW STR 22R SPLICE AT FS333.00. REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY. SEE CONTIN
- [SDR SWIA202264447](https://openairdocs.org/sdr/SWIA202264447.md): None · corroded · Jan 6, 2022 · N823SK · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > *CORROSION FOUND ON R/H FLOORSILL NEAR NUTPLATE JUST FWD OF FS1015.00 (MARKED) (C-CHECK RO 2/16/2022) REMOVED CORROSION FOR RH FLOOR SILL JUST FWD OF FS 1015.00 AS MARKED PER REFERENCE CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE WITHIN LIMITS PER REO
- [SDR SWIA202264446](https://openairdocs.org/sdr/SWIA202264446.md): None · corroded · Jan 6, 2022 · N823SK · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > *CORROSION FOUND ON R/H FLOORSILL CORNER AT FS1015.00 (MARKED) (C-CHECK RO 2/16/2022) REMOVED CORROSION FOR RH FLOOR SILL AT FS 1015.00 PER REFERENCE CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE WITHIN LIMITS PER REO 670-53-00-390 REV -- DATED 22 JAN 2
- [SDR SWIA202264445](https://openairdocs.org/sdr/SWIA202264445.md): None · damaged · Jan 6, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > TECHNICAIN DROPS BUCKING BAR ON INTERNAL SKIN DURING REPAIR PROCEDURES FOR FS280 CROSSBEAM REPAIR. DENT LOCATED BETWEEN FS280 - FS295, BETWEEN STGR-24L AND STGR-25L. (C-CHECK RO 2/16/2022) REPAIRED LOWER FUSELAGE SKIN BETWEEN FS265.00 AND FS295.00 AND
- [SDR SWIA202264444](https://openairdocs.org/sdr/SWIA202264444.md): None · incorrect · Jan 5, 2022 · N823SK · Cndair CL6002D24 · Doors
  > AFT BAGGAGE BAY DOOR SILL HAS BEEN INSTALLED WITH NUMEROUS INCORRECT FASTENERS. (C-CHECK RO 2/16/2022) INSTALLED CORRECT FASTENERS ONTO AFT BAGGAGE BAY DOOR SILL REF REO 690-53-61-1054 REV.-- DATED 2022-01-08 STEPS 1-5 FOR DISPOSITION FOR ALTERNATE FAST
- [SDR SWIA202264443](https://openairdocs.org/sdr/SWIA202264443.md): None · corroded · Jan 5, 2022 · N823SK · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > *CORROSION FOUND IN SEVERAL SPOTS ON R/H FLOORSILL BETWEEN FS1069.75 AND FS1088.00 (MARKED) (C-CHECK RO 2/16/2022) PERFORMED REO REPAIR OF FLOOR SILL BETWEEN FS 1069.75 AND FS 1088.00 R/H SIDE. FLOOR SILL REPAIRED PER REO 690-53-61-1056 REV -- DATED 20
- [SDR SWIA202264442](https://openairdocs.org/sdr/SWIA202264442.md): None · corroded · Jan 5, 2022 · N823SK · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > *CORROSION FOUND ON R/H FLOORSILL BETWEEN FS1031.00 AND FS1051.00 (MARKED) (C-CHECK RO 2/16/2022) ORIGINAL THICKNESS 0.063" REF CRJ900 SRM 53-61-43-001-001-A01. REMAINING THICKNESS 0.058", MATERIAL LOSS 0.005", ALLOWED 0.020" FOUND TO BE WITHIN LIMITS R
- [SDR SWIA202264441](https://openairdocs.org/sdr/SWIA202264441.md): None · corroded · Jan 5, 2022 · N823SK · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > *CORROSION FOUND IN SEVERAL SPOTS ON L/H FLOORSILL BETWEEN FS985.00 AND FS1000 (MARKED) (C-CHECK RO 2/16/2022) REPLACED LH FLOOR SILL BETWEEN FS985.00 TO FS1000.00 REF MHIRJ REO 690-53-61-1057 REV.-- DATED 2022-01-10. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202264440](https://openairdocs.org/sdr/SWIA202264440.md): None · corroded · Jan 5, 2022 · N823SK · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > *CORROSION FOUND ON FLOOR BEAM SUPPORT AT FS985.00 AT APPROX LBL42 (MARKED) (C-CHECK RO 2/16/2022) REPLACED FLOOR BEAM SUPPORT AT FS985.00 AT APPROX. LBL 42 REF DWG MM670-35041 REV. Y AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202264439](https://openairdocs.org/sdr/SWIA202264439.md): None · corroded · Jan 5, 2022 · N823SK · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > *CORROSION FOUND AROUND NUTPLATE ON L/H FLOORSILL BETWEEN FS927.00 AND FS942.00 (MARKED) (C-CHECK RO 2/16/2022) REMOVED CORROSION AROUND NUTPLATE ON LH FLOOR SILL BETWEEN FS927.00 AND FS 942.00. OMPLIED WITH ALL STEPS OF MHIRJ GREO 670-53-00-390 REV --,
- [SDR SWIA202264438](https://openairdocs.org/sdr/SWIA202264438.md): None · corroded · Jan 4, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 27 CORRODED ON MORE THAN ONE ELEMENT BETWEEN FS280.00 AND FS286.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. CRJ 900 SRM 51-42-06-001-0
- [SDR SWIA202264437](https://openairdocs.org/sdr/SWIA202264437.md): None · dented · Jan 3, 2022 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > TECHNICAIN DROPS BUCKING BAR ON INTERNAL SKIN DURING REPAIR PROCEDURES FOR FS280 CROSSBEAM REPAIR. DENT LOCATED BETWEEN FS280 - FS295, BETWEEN STGR-26R AND STGR-25R. (C-CHECK RO 2/16/2022) REPAIRED LOWER FUSELAGE SKIN BETWEEN FS280.00 AND FS295.00 AND
- [SDR SWIA202164436](https://openairdocs.org/sdr/SWIA202164436.md): None · corroded · Dec 31, 2021 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > FWD LAV DRAIN VALVE PLATE HAS EVIDENCE OF CORROSION ON THE OUTER SKIN. BEHIND PANEL 142BR (C-CHECK RO 2/16/2022) REMOVED CORROSION REF. CRJ 900 SRM 51-21-06-001-001-A01.ORIGINAL MATERIAL THICKNESS OF FWD WATER-WASTE CLOSING PLATE BETWEEN FS379.00 AND FS
- [SDR SWIA202164435](https://openairdocs.org/sdr/SWIA202164435.md): None · corroded · Dec 30, 2021 · N823SK · Cndair CL6002D24 · Fuselage Floor Panel
  > COCKPIT FLOOR SUPPORT ANGLE LOCATED AT LBL12.00 BETWEEN FS259.16 & FS280 IS CORRODED (C-CHECK RO 2/16/2022) COCKPIT FLOOR SUPPORT ANGLE LOCATED AT LBL12.00 BETWEEN FS259.16 & FS280 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ900 SRM 51-42-06
- [SDR SWIA202164434](https://openairdocs.org/sdr/SWIA202164434.md): None · cracked · Dec 29, 2021 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > FOUND WITH CRACK ANGLE P/N: CC670-34099-2SB AT FS 280, RBL 12 (C-CHECK RO 2/16/2022) REPLACED FS280 RBL 12 ANGLE P/N: CC670-34099-2SB REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV. J. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202164433](https://openairdocs.org/sdr/SWIA202164433.md): None · corroded · Dec 23, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 21R SPLICE AT FS333.00 CORRODED (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER SPLICE. REF. CRJ 900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420
- [SDR SWIA202164432](https://openairdocs.org/sdr/SWIA202164432.md): None · corroded · Dec 23, 2021 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-4
- [SDR SWIA202164431](https://openairdocs.org/sdr/SWIA202164431.md): None · corroded · Dec 23, 2021 · N823SK · Cndair CL6002D24 · Fuselage Internal Stairs
  > SERVICE DOOR LOWER SILL FLOOR SUPPORT ANGLE IS CORRODED. / (C-CHECK RO 2/16/2022) REMOVED AND REPLACED DAMAGED SVC. DOOR LOWER SILL FLOOR SUPPORT ANGLE WITH NEW PART. REF. CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-
- [SDR SWIA202164430](https://openairdocs.org/sdr/SWIA202164430.md): None · corroded · Dec 23, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 22R CORRODED BETWEEN FS280.00 AND FS295.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001
- [SDR SWIA202164429](https://openairdocs.org/sdr/SWIA202164429.md): None · corroded · Dec 23, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS310.00 AND FS333.00REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01 AND DRWG SH670
- [SDR SWIA202164428](https://openairdocs.org/sdr/SWIA202164428.md): None · corroded · Dec 23, 2021 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 22L SPLICE AT FS333.00 CORRODED (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER SPLICE. REF. CRJ 900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 R
- [SDR SWIA202164427](https://openairdocs.org/sdr/SWIA202164427.md): None · corroded · Dec 23, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 22L CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 53-0
- [SDR SWIA202164426](https://openairdocs.org/sdr/SWIA202164426.md): None · corroded · Dec 21, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Frame
  > MAIN AVIONICS BAY FS319.70 FRAME CORRODED AT STR 21L (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FRAME. REF. CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DW
- [SDR SWIA202164425](https://openairdocs.org/sdr/SWIA202164425.md): None · gouged · Dec 21, 2021 · N823SK · Cndair CL6002D24 · Ailerons
  > LH INBOARD FLAP, FLAP HINGE ARM GOUGED JUST AFT OF INBOARD HINGE BOX (C-CHECK RO 2/16/2022) REPAIRED GOUGE DAMAGE TO L/H INBD FLAP HINGE ARM REF. MHIRJ REO 690-57-54-034 REV €“ DATED 2021-12-28. ALL STEPS 1-4 OF MHIRJ REO 690-57-54-034 REV €“ DATED 2
- [SDR SWIA202164424](https://openairdocs.org/sdr/SWIA202164424.md): None · damaged · Dec 21, 2021 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > FOUND WITH DOUBLE HOLE ANGLE P/N: CC670-34153-2 AT BL33.00 FS 280.00 (C-CHECK RO 2/16/2022) REMOVED AND REPLACED STIFFENER AT FS280 RBL33.00 REF. CRJ-900 SRM, 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202164423](https://openairdocs.org/sdr/SWIA202164423.md): None · corroded · Dec 19, 2021 · N823SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > FOUND CORROSION ON EXSISTING REPAIR LHS BULKHEAD LOWER WEB FS280.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGED L/H FS280.00 LOWER WEB AND REPLACED WITH NEW. REF. CRJ900 SRM 53-11-10-201-004-A01 REV 38 JUL 25/2020, CRJ900 SRM 51-42-10-001-001-A01 REV 38 JUL
- [SDR SWIA202164422](https://openairdocs.org/sdr/SWIA202164422.md): None · cracked · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Doors
  > *LEFT AFT EMERGENCY-EXIT DOOR HAS POSSIBLE CRACK IN THE TOP EDGE MEMBER. LOCATION MARKED. (C-CHECK RO 2/16/2022) PERFOMED REPAIR TO THE LEFT AFT EMERGENCY-EXIT DOOR AT CRACKED LOCATION REF. MHIRJ REO 690-52-21-112 REV -- DATED 2021-12-30. ALL STEPS OF R
- [SDR SWIA202164421](https://openairdocs.org/sdr/SWIA202164421.md): None · corroded · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. DRWG SH670-31630 REV, K, CRJ 900 SRM 51-42-06-001-
- [SDR SWIA202164420](https://openairdocs.org/sdr/SWIA202164420.md): None · corroded · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 21L CORRODED BETWEEN FS280.00 AND FS295.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER 21L FROM FS280 TO FS333 REF. CRJ-900 SRM, 51-42-21-001-0
- [SDR SWIA202164419](https://openairdocs.org/sdr/SWIA202164419.md): None · corroded · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 CORRODED (C-CHECK RO 2/16/2022) REMOVED AND INSTALLED NEW MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASKCARD 51-900-1
- [SDR SWIA202164418](https://openairdocs.org/sdr/SWIA202164418.md): None · corroded · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS333.00 AND FS364.00 (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. CRJ 900 SRM 51-42-06-001-001-A01 AND DWG SH670-313
- [SDR SWIA202164417](https://openairdocs.org/sdr/SWIA202164417.md): None · corroded · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 2/16/2022) REMOVED AND INSTALLED NEW MAIN AVIONICS BAY STR 24R BETWEEN FS333.00 AND FS372.00, AND INSTALLED NEW STR24R SPLICE AND SHIM AT FS372.00. REF CRJ-900 CRJ-900 SRM 51-4
- [SDR SWIA202164416](https://openairdocs.org/sdr/SWIA202164416.md): None · corroded · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Keel
  > MAIN AVIONICS BAY STR 24R SPLICE AT FS333.00 CORRODED (C-CHECK RO 2/16/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED STRINGER. REF. CRJ 900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E,.
- [SDR SWIA202164415](https://openairdocs.org/sdr/SWIA202164415.md): None · corroded · Dec 17, 2021 · N823SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > FOUND CORROSION ON EXSISTING REPAIR RHS BULKHEAD LOWER WEB FS 280 (C-CHECK RO 2/16/2022) CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED RH LOWER WEB FS280 REF. CRJ-900 SRM, 51-42-06-001-001-A01, CRJ-900 SRM, 53-11-10-201-004-A01 AND DWG CC670
- [SDR SWIA202164414](https://openairdocs.org/sdr/SWIA202164414.md): None · corroded · Dec 16, 2021 · N823SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON TOP SIDE OF BEAM, LONGITUDINAL FS295.00 LBL9 (C-CHECK RO 2/16/2022) REMOVED CORROSION ON TOP SIDE OF BEAM LONGITUDINAL FS295.00 LBL9 REF. CRJ-900 SRM, 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS REF. CRJ-900 SRM, 53-21-43-101-001-
- [SDR SWIA202164413](https://openairdocs.org/sdr/SWIA202164413.md): None · corroded · Dec 15, 2021 · N823SK · Cndair CL6002D24 · Fuselage Structure (General)
  > *MULTIPLE AREAS OF CORROSION ON FUSELAGE INTERIOR SKIN AVIONICS BAY DOOR CUTOUT AROUND DOOR SEAL MATING SURFACE. AREAS MARKED. (C-CHECK RO 2/16/2022) BLENDED CORROSION DAMAGE FROM INTERIOR FUSELAGE SKIN @ AVIONICS BAY DOOR CUTOUT AROUND DOOR SEAL MATING

Next page: https://openairdocs.org/aircraft/N823SK/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 = 'N823SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N823SK/reports

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