# Service difficulty reports: N896SK A list on [N896SK](https://openairdocs.org/aircraft/N896SK.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 3 · 135 reports - [SDR SWIA2026062476309](https://openairdocs.org/sdr/SWIA2026062476309.md): Windshield · cracked · Jun 24, 2026 · N896SK · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal > DURING DESCENT THE RIGHT WINDSHIELD HEATING ELEMENT SHORT CIRCUITED AND THE WINDSHIELD CRACKED AND DELAMINATED (FLIGHT 4991)THIS IS CURRENTLY A WORK IN PROGRESS. - [SDR SWIA2025009090611](https://openairdocs.org/sdr/SWIA2025009090611.md): Rib · mechanic error · Jun 11, 2025 · N896SK · Cndair CL6002D24 · Wing, Rib/Bulkhead > UPON REMOVAL OF THE RT WING OTBD FLAP, INBD LATERAL SEAL & SHIM FOUND INBD RIB FOUND 2 MISDRILLED HOLES. REPLACED RT OUTBOARD FLAP INBOARD CLOSING RIB IAW SRM 51-42-13-001-001-A01, REO 690-57-53-173 REV-A AND DWG. 601R14501, REV.K. COMPLIED WITH SKYWEST TAS - [SDR SWIA2025090900602](https://openairdocs.org/sdr/SWIA2025090900602.md): Stringer · out of limits · Jun 2, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > COMPLY WITH: 670BA-53-040 - CENTER FUSELAGE, PRIMARY STRUCTURE BS 280 TO 295, INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF MAIN PASSENGER DOOR. REV C PART(S) B. SERVICE BULLETIN 670BA-53-040 REVISION C,- CENTER FUSELAGE, INCORPORATED COMPLIED WITH - [SDR SWI2025F01210](https://openairdocs.org/sdr/SWI2025F01210.md): Cleat · corroded · May 22, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION ON CLEAT ATTACHED TO INTERCOSTAL ON STGR 23L BETWEEN FS913.00 AND FS927.00 (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW FRAME CLEAT AT FS927 AT STR 23L REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH690-37060 REV AC. COMPLIED WITH SKYWEST TASK - [SDR SWI2025F01209](https://openairdocs.org/sdr/SWI2025F01209.md): Intercostal · corroded · May 22, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL AT STGR 23L BETWEEN FS913.00 AND FS927.00 (C-CHECK RO 09/07/2025)INSTALLED NEW INTERCOSTAL AT STGR 23L BETWEEN FS913.00 AND FS927.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG. NO. SH690-37060 REV. R. COMPLIED WITH SKY WEST TC 51-900 - [SDR SWIA2025090900522](https://openairdocs.org/sdr/SWIA2025090900522.md): Skin · dented · May 22, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin > FUSELAGE DENTED AT AFT L/H CORNER OF NOSE LANDING GEAR DOOR OPENING (C-CHECK RO 09/07/2025)COMPLIED WITH ALL THE STEPS OF REO 690-53-11-2007 REV -- DATED 2025-06-16 WET INSTALLED ALL FASTENERS AND -1 REPAIR DOUBLER, -2 REPAIR TRIPLER, -3 REPAIR QUADRUPLER, -4 - [SDR SWI2025F01228](https://openairdocs.org/sdr/SWI2025F01228.md): Angle · corroded · May 20, 2025 · N896SK · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR LWR ANGLE KICKPLATE (BTWN STR 17L-18L) IS CORRODED AT FS310 -FS349 (C-CHECK RO 09/07/2025)LOCATED AND DRILLED NEW ANGLE KICKPLATE REF CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND WET INSTALLED NEW KICKPLATE ANGLE. REF CRJ- - [SDR SWI2025F01232](https://openairdocs.org/sdr/SWI2025F01232.md): Floor Support · corroded · May 8, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION NOTED AT R/H PRESSURE FLOOR SILL ANGLE AT APPROX. FS712.00 - FS769.00 (MARKED) (C-CHECK RO 09/07/2025)REMOVED CORROSION FROM RH PRESSURE FLOOR SILL ANGLE. REPAIRED PER REO 690-53-41-536 REV -- DATE 2025-05-19. SEE CONTINUATION CARD FOR DETAILS. COM - [SDR SWIA2025090900508](https://openairdocs.org/sdr/SWIA2025090900508.md): Floor Support · corroded · May 8, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION NOTED AT L/H PRESSURE FLOOR SILL ANGLE AT APPROX. FS712.00 - FS769.00 (MARKED) (C-CHECK RO 09/07/2025)REMOVED CORROSION FROM LH PRESSURE FLOOR SILL ANGLE. REPAIRED PER REO 690-53-41-536 REV -- DATE 2025-05-19. SEE CONTINUATION CARD FOR DETAILS. CO - [SDR SWI2025F01248](https://openairdocs.org/sdr/SWI2025F01248.md): Floor Support · cracked · Apr 29, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > COCKPIT FLOOR SUPPORT BETWEEN FS 259.16 - FS280.00 LBL 12 CRACKED (C-CHECK RO 09/07/2025) INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE P/N CC670-33199-3 BETWEEN FS 259.16 - FS280.00 LBL 12 REF CRJ 900 SRM 51-42-06-001-001-A01 AND DWG.NO. CC670-33052 REV.G. C/W - [SDR SWIA2025090900429](https://openairdocs.org/sdr/SWIA2025090900429.md): Skin · corroded · Apr 29, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CORROSION ON EXTERNAL SKIN LOCATED BETWEEN FS1031 TO FS1047 AND STR27 TO STR26R (C-CHECK RO 09/07/2025)PERFORMED REPAIR ON EXTERNAL SKIN LOCATED BETWEEN FS1031 TO FS1047 AND STR27 TO STR26R PER REO 690-53-61-1584 REV -- DATED 2025-05-20. ALL STEPS COMPLIED W - [SDR SWIA2025090900427](https://openairdocs.org/sdr/SWIA2025090900427.md): Stringer · corroded · Apr 27, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STR 21L BETWEEN FS310 - FS295 HAS CORROSION (C-CHECK RO 09/07/2025)REPAIRED STRG 21L BETWEEN FS310- FS295 COMPLIED WITH ALL THE STEPS OF REO 690-53-21-1937 REV-- DATED 2025-05-22 WET INSTALLED -1 REPAIR ANGLE AND -2 STRINGER INSERT. REF - CRJ900 SRM 51-4-06 - [SDR SWI2025F01205](https://openairdocs.org/sdr/SWI2025F01205.md): Door Frame · cracked · Apr 24, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Structure > RH FWD EMER DOOR HAS SUSPECTED CRACK AT UPPER AFT STOP. (MARKED) (C-CHECK RO 09/07/2025)PERFORMED REPAIR OF THE RH FWD EMERGENCY EXIT DOOR FRAME LOCATED AT THE BASE OF THE AFT PROXIMITY SENSOR STRIKER AS PER REO 670-52-21-103 REV --, 2024-11-06. SEE CONTINU - [SDR SWI2025F01200](https://openairdocs.org/sdr/SWI2025F01200.md): Floor Support · cracked · Apr 23, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > COCKPIT FLOOR SUPPORT BETWEEN FS 259.16 - FS280.00 RBL 12 CRACKED (C-CHECK RO 09/07/2025)INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE P/N CC670-33199-4 BETWEEN FS 259.16 - FS280.00 RBL 12 REF CRJ 900 SRM 51-42-06-001-001-A01 AND DWG.NO. CC670-33052 REV,-G. COMPL - [SDR SWI2025F01251](https://openairdocs.org/sdr/SWI2025F01251.md): Drain · corroded · Apr 9, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Structure > LOWER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 23R HAS CORROSION ( 29949074) (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW LOWER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 23R REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH - [SDR SWI2025F01250](https://openairdocs.org/sdr/SWI2025F01250.md): Angle · damaged · Apr 9, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Structure > FWD LAV DRAIN BOX ANGLE IMPACT BETWEEN FS379 - FS394 AT STR23R HAS CORROSION ( 29949078) (C-CHECK RO 09/07/2025)INSTALLED NEW FWD LAV DRAIN BOX ANGLE IMPACT BETWEEN FS379 - FS394 AT STR23R REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32280 REV H. COMPL - [SDR SWIA2025090900409](https://openairdocs.org/sdr/SWIA2025090900409.md): Frame · corroded · Apr 9, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Frame > LOWER FRAME SECTION AT FS379 BETWEEN STR 23R - STR 21R IS CORRODED (29947635) (C-CHECK RO 09/07/2025)INSTALLED NEW LOWER FRAME SECTION AT FS379 BETWEEN STR 25R - STR 20R REF CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-32280 RE - [SDR SWI2025F01249](https://openairdocs.org/sdr/SWI2025F01249.md): Drain · corroded · Apr 9, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Structure > UPPER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 21R HAS CORROSION ( 29949033) (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW UPPER DIAPHRAGM AT FWD LAV DRAIN BOX BETWEEN FS379 - FS394 STR 21R REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH6 - [SDR SWI2025F01252](https://openairdocs.org/sdr/SWI2025F01252.md): Skin · cracked · Apr 8, 2025 · N896SK · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR SKIN CRACKED AT PAX DOOR PANEL 832AL CUT OUT DURING INSTALL OF FWD PULL IN LEVER (MARKED) (C-CHECK RO 09/07/2025)REPAIRED PAX DOOR SKIN CRACKED AT PAX DOOR PANEL 832AL CUT OUT. PER REO 690-52-11-1033 REV -- DATE 2025-05-19. SEE CONTINUATION TASK FOR - [SDR SWIA2025090900408](https://openairdocs.org/sdr/SWIA2025090900408.md): Support Angle · corroded · Apr 8, 2025 · N896SK · Cndair CL6002D24 · Wing Main, Frame Structure > MULTIPLE CORRODED FASTENERS, LH OUTBOARD TRAILING EDGE, LOWER SUPPORT ANGLE. SEE ATTACHED PICS. (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW CHANNEL CC670-17224-1 REF. CRJ 900 SRM 51-42-06-001-001-A01, 51-42-28-001-001-A01, AND DWG CC670-17227 REV. B. SE - [SDR SWIA2025090900407](https://openairdocs.org/sdr/SWIA2025090900407.md): Drag Angle · cracked · Apr 7, 2025 · N896SK · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR AFT DRAG ANGLE CRACKED. (C-CHECK RO 09/07/2025)CUT AWAY DAMAGED PAX DOOR AFT DRAG ANGLE SECTION BETWEEN DOOR DATUM 2 AND DOOR DATUM 5 AND INSTALL NEW REPAIR PARTS PER CRJ 900 SRM 52-11-04-201-002-A01 REPAIR TYPE II. SEE CONTINUATION TASKS FOR MORE DE - [SDR SWIA2025090900406](https://openairdocs.org/sdr/SWIA2025090900406.md): Window Frame · cracked · Apr 6, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Structure > LH UPPER SIDE FRAME SECTOR AT FS235 BELOW SIDE WINDOW SILL IS CRACKED (C-CHECK RO 09/07/2025) INSTALLED NEW LH UPPER SIDE FRAME SECTOR AT FS235 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG#CC670-34040 REV-C. COMPLIED WITH REO - [SDR SWI2025F01253](https://openairdocs.org/sdr/SWI2025F01253.md): Frame · cracked · Apr 6, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Frame > RH UPPER SIDE FRAME SECTOR AT FS235 BELOW SIDE WINDOW SILL IS CRACKED (C-CHECK RO 09/07/2025)INSTALLED NEW RH UPPER FRAME SECTOR FS235.00 (PN CC670-34133-6) REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG#CC670-34040 REV-C. COMPL - [SDR SWIA2025009090405](https://openairdocs.org/sdr/SWIA2025009090405.md): Bracket · cracked · Apr 5, 2025 · N896SK · Cndair CL6002D24 · Wing, Attach Fittings > LEFT WING FUEL CANNISTER FOR SLAT TRACK 1-3 MOUNT BRACKET IS CRACKED. (MARKED) (C-CHECK RO 09/07/2025)COMPLIED WITH REPAIR OF LH WING FUEL CANISTER AT SLAT TRACK 1-3 MOUNT BRACKET. LEAK CHECK GOOD. REF - CRJ900 REO 670-57-42-577 REV -- DATED 2016-12-02. COMPL - [SDR SWIA2025090900404](https://openairdocs.org/sdr/SWIA2025090900404.md): Structure · chafed · Apr 4, 2025 · N896SK · Cndair CL6002D24 · Cargo/Baggage Doors > FORWARD CARGO DOOR MAIN HANDLE CUT OUT CHAFFED IN LOWER CORNER AS MARKED (C-CHECK RO 09/07/2025)REPAIRED DAMAGE TO FORWARD CARGO DOOR SKIN AT MAIN HANDLE CUTOUT REF. REO 690-52-35-506 REV. -- DATED 2025-04-18 - [SDR SWI2025F01255](https://openairdocs.org/sdr/SWI2025F01255.md): Floorbeam · cracked · Mar 31, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Floor Beam > LHS COCKPIT FLOOR BEAM IS CRACKED @ LBL12.0, FS280.00 (C-CHECK RO 09/07/2025) INSTALLED NEW BEAM SECTION P/N 690-53-11-228-003. -35 INBOARD UPPER ANGLE, -37 INBOARD LOWER ANGLE, -39 OUTBOARD WEB ANGLE AND -41 LOWER ANGLE AT LBL 12.0 FS 280.00 REF CRJ 900 SRM - [SDR SWIA2025090900331](https://openairdocs.org/sdr/SWIA2025090900331.md): Floorbeam · cracked · Mar 31, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Floor Beam > RHS COCKPIT FLOOR BEAM IS CRACKED @ RBL12.0, FS280.00 (C-CHECK RO 09/07/2025)INSTALLED NEW BEAM SECTION P/N 690-53-11-228-004. -36 INBOARD UPPER ANGLE, -38 INBOARD LOWER ANGLE, -40 OUTBOARD WEB ANGLE AND -42 LOWER ANGLE AT RBL 12.0 FS 280.00 REF CRJ 900 SRM 5 - [SDR SWI2025F01254](https://openairdocs.org/sdr/SWI2025F01254.md): Hinge Fitting · chafed · Mar 31, 2025 · N896SK · Cndair CL6002D24 · Spoilers > LEFT WING OUTBD GROUND SPOILER CENTER HINGE FITTING CHAFED (C-CHECK RO 09/07/2025)REPAIRED DAMAGE TO LH OB GROUND SPOILER CENTER HINGE FITTING REF. REO 690-57-51-418 REV. -- DATED 2025-04-17. ALL STEPS COMPLIED WITH.C/W T/C 51-900-1002-SKY - [SDR SWIA2025090900327](https://openairdocs.org/sdr/SWIA2025090900327.md): Intercostal · corroded · Mar 27, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INTERCOSTAL @ STGR24R FS913.00 - FS927.00 IS CORRODED (C-CHECK RO 09/07/2025) INSTALLED NEW INTERCOSTAL AT STGR24R BETWEEN FS913.00 - FS927.00. REF. CRJ-900 SRM 51-42-06-001-001-A01 AND DRAWING SH690-37060 REV L. ALSO COMLPIED WITH 51-900-1002-SKY - [SDR SWI2025F01257](https://openairdocs.org/sdr/SWI2025F01257.md): Coaming · cracked · Mar 26, 2025 · N896SK · Cndair CL6002D24 · Engine Thrust Reverser > R/H LOWER TRANSCOWL COAMING IS CRACKED (C-CHECK RO 09/07/2025)REMOVED AND REPLACED COAMING P/N CN624-2060-209 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-1207, REV. A, 2015-08-27. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY. CAMP 29865263. - [SDR SWI2025F01256](https://openairdocs.org/sdr/SWI2025F01256.md): Door · chafed · Mar 26, 2025 · N896SK · Cndair CL6002D24 · Emergency Exits > LH AFT EMER EXIT DOOR HAS CHAFES AROUND 2EA FASTENER HOLES BELOW WINDOW. (MARKED) (C-CHECK RO 09/07/2025)PERFORMED A BLEND REPAIR AND FOUND WITHIN LIMITS PER REO 690-52-21-190 REV. -- DATED 2025-04-12. - [SDR SWIA2025090900326](https://openairdocs.org/sdr/SWIA2025090900326.md): Door · cracked · Mar 26, 2025 · N896SK · Cndair CL6002D24 · Emergency Exits > LH AFT EMER EXIT DOOR HAS CRACK NEXT TO AFT MICROSWITICH BRACKET. (MARKED) (C-CHECK RO 09/07/2025)PERFORMED REPAIR OF THE LH AFT EMERGENCY EXIT DOOR FRAME LOCATED AT THE BASE OF THE AFT PROXIMITY SENSOR STRIKER AS PER REO 670-52-21-103 REV --, 2024-11-06. SE - [SDR SWI2025F01271](https://openairdocs.org/sdr/SWI2025F01271.md): Stringer · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 24R BETWEEN FS927.00 AND FS942.00 (MARKED) (C-CHECK RO 09/07/2025)INSTALLED NEW STRINGER STGR24R FS847.00 - FS977.00 AND -3 AND -4 ANGLES. REF: REO 690-53-51-460 REV A 2025-06-13, DRAWING SH690-37060 REV AC, CRJ-900 SRM 51-42-06-001-001-A01, - [SDR SWI2025F01270](https://openairdocs.org/sdr/SWI2025F01270.md): Attach Angle · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Wing, Attach Fittings > THE RH MLG TIRE BURST PANEL 642AZ ATTACHMENT ANGLE IS CORRODED. (C-CHECK RO 09/07/2025)COMPLIED WITH REPAIR OF RH MLG TIRE BURST PANEL 642AZ ATTACHMENT ANGLE. LEAK TEST GOOD. REF - CRJ900 SRM 51-42-21-001-001-A01 AND DWG NO CC670-10320 REV -F. COMPLIED WITH - [SDR SWI2025F01269](https://openairdocs.org/sdr/SWI2025F01269.md): Door · cracked · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Emergency Exits > LH FWD EMER DOOR HAS CRACK NEXT TO AFT MICROSWITICH BRACKET. (MARKED) (C-CHECK RO 09/07/2025)PERFORMED REPAIR OF THE LH FWD EMERGENCY EXIT DOOR FRAME LOCATED AT THE BASE OF THE AFT PROXIMITY SENSOR STRIKER AS PER REO 670-52-21-103 REV --, 2024-11-06. SEE CONT - [SDR SWI2025F01268](https://openairdocs.org/sdr/SWI2025F01268.md): Intercostal · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AVIONICS BAY INTERCOSTAL AT STR.20R BETWEEN FS.333.00 AND FS.349.00 CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 09/07/2025)INSTALLED NEW AVIONICS BAY INTERCOSTAL AT STR.20R BETWEEN FS.319.00 AND FS.349.00 REF CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51- - [SDR SWI2025F01267](https://openairdocs.org/sdr/SWI2025F01267.md): Stringer · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > AVIONICS BAY STR.21L BETWEEN FS.310.00 AND FS.319.70 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 09/07/2025) INSTALLED NEW AVIONICS BAY INTERCOSTAL AT STGR21L BETWEEN FS333 - FS310 REF CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND - [SDR SWI2025F01266](https://openairdocs.org/sdr/SWI2025F01266.md): Stringer · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 26L BETWEEN FS969.00 AND FS977.00 (MARKED) (C-CHECK RO 09/07/2025)REMOVED/INSTALLED NEW STR 26L FROM FS954 TO FS977 REF CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DWG SH690-37060 REV AC AND REF REO 690-53-51-456 REV -- DATE - [SDR SWI2025F01265](https://openairdocs.org/sdr/SWI2025F01265.md): Frame · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME AT FS927.00 BETWEEN STGR 25L AND STGR 26L (MARKED) (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW LOWER FRAME SECTOR FS927 BETWEEN STR 20L - STR23R REF: CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01 AND DWG SH690 - [SDR SWI2025F01264](https://openairdocs.org/sdr/SWI2025F01264.md): Stringer · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 26R BETWEEN FS881.00 AND FS897.00. (MARKED) (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW INTERCOSTAL AT STGR 26R BETWEEN FS881.00 AND FS897.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG. NO.SH690-37060 REV. R. COMPLIED WITH SKYWEST TA - [SDR SWI2025F01263](https://openairdocs.org/sdr/SWI2025F01263.md): Intercostal · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RH INTERCOSTAL HAS CORROSION AT STGR 24R BETWEEN FS881.00 AND FS897.00. (MARKED) (C-CHECK RO 09/07/2025)FOUND RH INTERCOSTAL OUT OF LIMITS. REF: CRJ-900 SRM 53-51-03-101-003-A02 AND INSTALLED NEW INTERCOSTAL AT STGR24RH BETWEEN FS881.00 - FS897.00. REF. CRJ-9 - [SDR SWIA2025090900325](https://openairdocs.org/sdr/SWIA2025090900325.md): Intercostal · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AVIONICS BAY INTERCOSTAL AT STR.20R BETWEEN FS.349.00 AND FS.364.00 CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 09/07/2025)REMOVED, REPLACED AND INSTALLED NEW INTERCOSTAL AT STGR.20R BETWEEN FS 349.00 - FS364.00 REF CRJ 900 SRM 51-42-06-001-001-A01, CRJ - [SDR SWI2025F01262](https://openairdocs.org/sdr/SWI2025F01262.md): Frame · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME AT FS969.00 BETWEEN STGR 25L AND STGR 26L (MARKED) (C-CHECK RO 09/07/2025)INSTALLED NEW FRAME SECTOR FS969.00, P/N SH690-37074-3S. REF: CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01, AND DRAWING SH690-37060 REV AC. COMP - [SDR SWI2025F01261](https://openairdocs.org/sdr/SWI2025F01261.md): Support Angle · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > PANEL 542AZ FWD SUPPORT ANGEL HAS SPOTS OF CORROSION (MARKED). (C-CHECK RO 09/07/2025)REMOVED DAMAGED AND INSTALLED NEW SUPPORT ANGLE P/N CC670-10338-1 FOR PANEL 542AZ REF CRJ 900 SRM 51-42-21-001-001-A01 AND DWG. NO. CC670-10320 REV -F. COMPLIED WITH SKY WE - [SDR SWI2025F01260](https://openairdocs.org/sdr/SWI2025F01260.md): Skin · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CORROSION ON INNER SKIN BETWEEN FS847.00 +16.00 AND FS 847 +32.00 AND BETWEEN STGR26R AND STGR26L. (MARKED). (C-CHECK RO 09/07/2025)COMPLIED WITH ALL THE STEPS OF REO 690-53-51-452 REV-- DATED 2025-04-02. ENSURED BLEND OUT ON INNER SKIN (DOUBLER) BETWEEN FS8 - [SDR SWI2025F01259](https://openairdocs.org/sdr/SWI2025F01259.md): Stringer · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 26L BETWEEN FS847.00 +32.00 AND FS847.00 +48.00. (MARKED) (C-CHECK RO 09/07/2025)REMOVED AND REPLACED STRINGER 26L FROM FS847 - FS977. LEAK TEST GOOD. REF - CRJ900 REO 690-53-51-457 REV -- DATED 2025-06-10 SEE CONTINUATION CARD FOR MAINTENAN - [SDR SWI2025F01258](https://openairdocs.org/sdr/SWI2025F01258.md): Intercostal · corroded · Mar 25, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > MULTIPLE SPOTS OF CORROSION ON LH INTERCOSTAL AT STGR 22L BETWEEN FS865.00 AND FS881.00. (MARKED) (C-CHECK RO 09/07/2025)INSTALLED NEW INTERCOSTAL AT STGR22LH BETWEEN FS865.00 - FS881.00. REF. CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH690-37060 REV AC. COMPL - [SDR SWIA2025090900324](https://openairdocs.org/sdr/SWIA2025090900324.md): Mount · corroded · Mar 24, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > FWD CARGO BAGGAGE NET RESTRAINT MOUNT PLATE AT STR.26L FS.629.00.00 HAS SPOTS OF CORROSION (MARKED). (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW MOUNT PLATE ON FS 629 FRAME AT STGR 26L PER REF CRJ 900 SRM 51-42-21-001-001-A01, CRJ 900 SRM 51-42-22-001-0 - [SDR SWI2025F01296](https://openairdocs.org/sdr/SWI2025F01296.md): Floor Support · corroded · Mar 22, 2025 · N896SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RH FLOOR SILL IS CORRODED FS280 €“ 319 (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED RH FLOOR SILL BETWEEN FS280.00 - FS319.00. PRESSURE LEAK TEST GOOD. REF - CRJ900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-13-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01. - [SDR SWI2025F01295](https://openairdocs.org/sdr/SWI2025F01295.md): Crossbeam · corroded · Mar 22, 2025 · N896SK · Cndair CL6002D24 · Fuselage Main, Structure > CROSSBEAM AT FS1031.00 CORRODED BETWEEN LBL9.00 AND LBL27.0 AS MARKED (C-CHECK RO 09/07/2025)PERFORMED A BUILDUP REPAIR PER TO CROSSBEAM FS 1031.00 BETWEEN LBL9.00 AND LBL27.0 PER REO 690-53-61-1572 REV-A DATED 2025-05-28. COMPLIED WITH SKYWEST TASK CARD 51 Next page: https://openairdocs.org/aircraft/N896SK/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 = 'N896SK' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N896SK/reports --- 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.