N821SK

Service difficulty reports · 234

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N821SK' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026041075688Windshield · crackedLEFT WINDSHIELD ARCING DURING DESCENT IN BOTTOM RIGHT HAND CORNER. IMMEDIATELY TURNED IT OFF VERIFIED WITH QRH AND SAW NO CRACKING AND WERE BELOW 28000 BY THAT TIME WITH NO FURTHER ISSUES. (FLIGHT 3715) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32056477 WIApr 10, 2026 · N821SK · Cndair CL6002D24 · Flight Compartment WindowsSDR SWIA2026022675356Engine · odorIN FLIGHT FA REPORTED STRONG EXHAUST ODOR IN THE CABIN CAUSING HER THROAT AND HEAD TO HURT. DESCENDED TO FL240 AND SWAPPED TO THE APU BLEED. FA INITIALLY NOTED THAT THE SMELL IMPROVED BUT LATER CALLED US SAYING THE ODOR WAS BACK. PILOTS CONFIRMED THERE WAS A Feb 26, 2026 · N821SK · Cndair CL6002D24 · Humidity Control SystemSDR SWIA202602275356Unknown · fumesIN FLIGHT FA REPORTED STRONG EXHAUST SMELL IN THE CABIN CAUSING HER THROAT AND HEAD TO HURT. WE DESCENDED TO FL240 AND SWAPPED TO THE APU BLEED. FA INITIALLY NOTED THAT THE SMELL IMPROVED BUT LATER CALLED US SAYING THE SMELL WAS BACK. PILOTS CONFIRMED THERE WAFeb 26, 2026 · N821SK · Cndair CL6002D24 · Air Distribution SystemSDR SWIA2026021475289Unknown · smokeBOTH FAS & SOME PAX REPORTED FOG, SMOKE, FUMES VISIBLE IN CABIN, MORE REAR OF CABIN DURING FULL POWER TAKEOFF ROLL. SLOWLY DISSIPATED DURING CRUISE. REPORTED BURNING EYES AS WELL (FLT 3679). INSPECT & ENG RUNS, COULD NOT VERIFY THE ISSUE. VERIFIED PLANESFeb 14, 2026 · N821SK · Cndair CL6002D24 · Air Distribution SystemSDR SWIA2025122975121Repair · installedPERFORM DEVIATION TO SERVICE BULLETIN 670BA-53-044 REV -G DUE TO EXISTING CAP ANGLE SPLICE REPAIR PER REO 690-53-11-2104. (C-CHECK RO 02/01/2026)PERFORMED DEVIATION TO SERVICE BULLETIN 670BA-53-044 REV -G DUE TO EXISTING CAP ANGLE SPLICE REPAIR PER ALL STEPSDec 29, 2025 · N821SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025121075164Angle · corrodedCORROSION PRESENT ON IMPACT ANGLE AT FWD WASTE WATER SERVICE DOOR INSIDE STRUCTURE BETWEEN FS379 - FS394 STR 23R (C-CHECK RO 02/01/2026)REMOVED AND INSTALLED NEW REPLACEMENT IMPACT ANGLE AT FWD WASTE WATER SERVICE DOOR INSIDE STRUCTURE BETWEEN FS379 - FS394 SDec 10, 2025 · N821SK · Cndair CL6002D24 · Fluid Service DoorsSDR SWIA2025121075163Diaphragm · corrodedCORROSION PRESENT ON LOWER DIAPHRAGM AT FWD WASTE WATER SERVICE DOOR INSIDE STRUCTURE BETWEEN FS379 -FS394 STR 23R (C-CHECK RO 02/01/2026)REMOVED AND INSTALLED NEW LOWER DIAPHRAGM AT FWD WASTE WATER SERVICE DOOR INSIDE STRUCTURE BETWEEN FS379 -FS394 STR 23R Dec 10, 2025 · N821SK · Cndair CL6002D24 · Fuselage, Powerplant Attach FittingsSDR SWIA2025120875162Frame · corrodedFS 379 HAS CORROSION PRESENT ON AFT SIDE AT APPROXIMATELY STR 23R. (C-CHECK RO 02/01/2026)FRAME AT FS 379 HAS INTERGRANULAR CORROSION AND IS EXFOLIATED WITH 100% MATERIAL LOSS IS FOUND TO BE OUT OF LIMITS REPLACE PART. REMOVED AND INSTALLED NEW FRAME FS 379.RDec 8, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2025120675118Pressure Deck · mechanic errorON THE PRESSURE FLOOR MODIFICATION, AN EXISTING FASTENER HOLE HAS SHORT ED. AT FS792, RBL36, THE HOLE COMMON TO THE DIAPHRAGM LOWER FLANGE, THE I/B HOLE AT FS792, RBL36 BEAM AND THE LOWER STRAP (C-CHECK RO 02/01/2026)REMOVED DIAPHRAGM AT RBL36 FS792 TO FOM. PDec 6, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025081675161Hinge · scratchedSCRATCHES NOTED ON PAX DOOR HINGE HALF(DOOR SIDE) LUGS AFT TO FWD LUGS 1-10 AND 27 (MARKED) (C-CHECK RO 02/01/2026)REPAIRED PAX DOOR PIANO HINGE FUSELAGE SIDE OUTER SURFACE LUGS IAW CRJ 900 SRM 52-11-01-201-007-A01 TYPE I STEPS 1, 2, 3, 4. AND COMPLIED WITH TAug 16, 2025 · N821SK · Cndair CL6002D24 · Fuselage, Door HingeSDR SWIA2025081675142Hinge · chafedCHAFING AND CORROSION NOTED ON PAX DOOR HINGE HALF (FUS SIDE) (MARKED) (C-CHECK RO 02/01/2026)BLENDED LANDS ON THE FUSELAGE SIDE PAX DOOR HINGE. BLENDED LANDS MATERIAL LOSS OF 0.007" OR LESS EXCEPT FOR THE AFT LAND. THE AFT LAND BLEND DEPTH MEASURES 0.048" DEAug 16, 2025 · N821SK · Cndair CL6002D24 · Fuselage, Door HingeSDR SWIA2025081675124Stringer · corrodedCORROSION NOTED ON STRG 19R BETWEEN FS437-FS453 (MARKED) (C-CHECK RO 02/01/2026)STRG 19R BETWEEN FS437-FS453 HAS A PREVIOUS REPAIR AND IS IN A NO DAMAGE ALLOWED AREA THEREFORE FOUND TO BE OUT OF LIMITS REPLACE PART REF CRJ-900 SRM 53-21-03-101-007-A04REMOVED Aug 16, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2025081275160Window Post · crackedDURING AUDIT OF 9Y TASK CARD 53-220-504 IT WAS FOUND THE THE RH OUTBOARD WINDOW POST IS CRACKED (C-CHECK RO 02/01/2026)REMOVED AND INSTALLED NEW RH WINDSHIELD POST P/N 601R33223-2 IAW. CRJ 900 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV-F. COMPLIED WITHAug 12, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025080475159Slat Track · wornRH 3-3 SLAT TRACK HAS WEAR MARKS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON RH SLAT TRACK 3-3 IAW CRJ 900 SRM 51-12-00-001-001-A01BLENDS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE REMOVAL LIMITS IN CRJ900 SRMPERFAug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475158Slat Track · damagedRH 2-2 SLAT TRACK HAS PITTING IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON R/H SLAT TRACK 2-2 IAW CRJ 900 SRM 51-12-00-001-001-A01FOUND TO BE OUT OF LIMITS NO ALLOWABLE LIMITS FOUND IN THE CRJ 900 SRMREPAIRED IAW REO 690-57-Aug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475157Slat Track · wornRH 1-3 SLAT TRACK HAS WEAR MARKS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)PERFORMED REPAIR ON R/H SLAT TRACK 1-3 PER REO 690-57-42-1305 REV -- 2025-08-26 SEE CONTINUATION FOR DETAILS COMPLIED WITH TASK CARD 51-900-1002Aug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475141Slat Track · wornRH 3-2 SLAT TRACK HAS WEAR MARKS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON R/H SLAT TRACK 3-2 IAW CRJ 900 SRM 51-12-00-001-001-A01FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN CRJ900 SRMREPAIRED IAW REO 690-57-4Aug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475140Slat Track · wornRH 3-1 SLAT TRACK HAS WEAR MARKS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON R/H SLAT TRACK 3-1 IAW CRJ 900 SRM 51-12-00-001-001-A01 COMPLIED WITH ALL STEPS OF REO 690-57-42-1301 REV -- DATED 2025-08-26.. RIGGING GOOD. OPS Aug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475139Slat Track · wornRH 2-3 SLAT TRACK HAS WEAR MARKS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON R/H SLAT TRACK 2-3 IAW CRJ 900 SRM 51-12-00-001-001-A01FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN CRJ900 SRMREPAIRED IAW REO 690-57-4Aug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475138Slat Track · damagedRH 1-2 SLAT TRACK HAS PITTING IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON R/H SLAT TRACK 1-2 IAW CRJ 900 SRM 51-12-00-001-001-A01FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN CRJ900 SRMREPAIRED IAW REO 690-57-42-1Aug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475137Slat Track · wornRH 1-1 SLAT TRACK HAS WEAR MARKS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON RH SLAT TRACK 1-1 IAW CRJ 900 SRM 51-12-00-001-001-A01BLENDS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE REMOVAL LIMITS IN CRJ900 SRMPERFAug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475123Slat Track · wornRH 2-1 SLAT TRACK HAS WEAR MARKS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON R/H SLAT TRACK 2-1 IAW CRJ 900 SRM 51-12-00-001-001-A01ALL BLENDS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN CRJ900 SRMREPAIRED IAW REAug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080475120Slat Track · chafedRH SLAT TRACK 1-1 HAS CHAFE DAMAGE ON FWD OTBD SIDE. (MARKED) (C-CHECK RO 02/01/2026) PERFORMED REPAIR AT R/H SLAT TRACK 1-1 PER REO 690-57-42-1291 REV-- 2025-08-26 ALL STEPS COMPLIED WITH COMPLIED WITH SKYWEST TASK CARDS 51-900-1002-SKY AND 27-900-1009-SKYAug 4, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080375156Slat Track · wornL/H SLAT TRACK 3-1 HAS WEAR MARKINGS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON L/H SLAT TRACK 3-1 IAW CRJ 900 SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 690-57-42-1288 REV-- DATED 2025-08-22. RIGGING GOOD. OPAug 3, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080375155Slat Track · damagedL/H SLAT TRACK 2-2 HAS PITTING. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON L/H SLAT TRACK 2-2 IAW CRJ 900 SRM 51-12-00-001-001-A01BLEND #1 MEASURED (0.496" L X 1.600" W), ORIGINAL MATERIAL THICKNESS IS 0.250" IAW DWG CC670-12051 REV. C, MATERIALAug 3, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080375154Slat Track · wornL/H SLAT TRACK 2-1 HAS WEAR MARKINGS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)PERFORMED REPAIR AT L/H SLAT TRACK 2-1 PER REO 690-57-42-1297 REV-- 2025-08-25 SEE CONTINUATION FOR DETAILS.COMPLIED WITH TASK CARD 51-900-1002-SKYAug 3, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080375136Slat Track · wornL/H SLAT TRACK 3-3 HAS WEAR MARKINGS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON L/H SLAT TRACK 3-3 IAW CRJ 900 SRM 51-12-00-001-001-A01ALL BLENDS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN CRJ900 SRMREPAIRED IAug 3, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080375135Slat Track · wornL/H SLAT TRACK 1-3 HAS WEAR MARKINGS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)PERFORMED REPAIR ON L/H SLAT TRACK 1-3 PER REO 690-57-42-1296 REV-- DATED 2025-08-25 SEE CONTINUATION FOR DETAILSCOMPLIED WITH TASK CARD 51-900-1002Aug 3, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080375125Slat Track · wornL/H SLAT TRACK 1-1 HAS WEAR MARKINGS IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK RO 02/01/2026)PERFORMED REPAIR ON L/H SLAT TRACK 1-1 PER REO 690-57-42-1290 REV -- 2025-08-22 SEE CONTINUATION FOR DETAILS.COMPLIED WITH TASK CARD51-900-1002-SKYCOMPLIED WITH TASK Aug 3, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080375122Slat Track · damagedL/H SLAT TRACK 1-2 HAS PITTING. (MARKED) (C-CHECK RO 02/01/2026)REMOVED WEAR MARKING ON L/H SLAT TRACK 1-2 IAW CRJ 900 SRM 51-12-00-001-001-A01BLENDS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE REMOVAL LIMITS IN CRJ900 SRMPERFORMED REPAIR OF L/H SLATAug 3, 2025 · N821SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA2025080275134Intercostal · corrodedCORROSION ON INTERCOSTAL STGR24L BETWEEN FS881.00 TO FS897.00 AS MARKED (C-CHECK RO 02/01/2026)CORROSION ON INTERCOSTAL, STRG24L BETWEEN FS881.00 TO FS897.00 IS FOUND TO BE IN A NO ALLOWABLE DAMAGE AREA THEREFORE FOUND TO BE OUT OF LIMITS REF CRJ-900 SRM 53-5Aug 2, 2025 · N821SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025080275133Intercostal · corrodedCORROSION ON INTERCOSTAL, STRG24L BETWEEN FS865 -FS881 (C-CHECK RO 02/01/2026)CORROSION ON INTERCOSTAL, STRG24L BETWEEN FS865 -FS881 IS FOUND TO BE IN A NO ALLOWABLE DAMAGE AREA THEREFORE FOUND TO BE OUT OF LIMITS REF CRJ-900 SRM 53-51-03-101-003-A04REMOVED AAug 2, 2025 · N821SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025073175153Floor Support · crackedPOSSIBLE CRACK ON THE COCKPIT FLOOR SUPPORT, FWD ANGLE (MARKED) (C-CHECK RO 02/01/2026)REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE WITH NEW P/N CC670-34095-1 FS 280 (FWD ANGLE) IAW CRJ 900 SRM 51-42-06-001-001-A01 & CRJ 900 SRM 51-42-21-001-001-A01 AND DWG CJul 31, 2025 · N821SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025073175152Support Angle · corrodedFS280, FLOORBOARD CRAWLWAY SUPPORT ANGLE, HAS 3EA AREAS OF CORROSION (MARKED) (C-CHECK RO 02/01/2026)REMOVED AND INSTALLED NEW FS280, FLOORBOARD CRAWLWAY SUPPORT ANGLE REF CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV Jul 31, 2025 · N821SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025073175151Stringer · corrodedCORROSION ON STGR23L BETWEEN FS1069.75- FS1088.20 AS MARKED (C-CHECK RO 02/01/2026)REMOVED CORROSION ON STGR23L BETWEEN FS1069.75- FS1088.20 REF CRJ-900 SRM 51-21-06-001-001-A01NOMINAL THICKNESS IS: 0.100" REF. BOMBARDIER DWG MM670-35151 REV R MINIMUM REMAINJul 31, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2025073175150Stringer · corrodedCORROSION ON STGR24L BETWEEN FS985.00 - FS1000.00 AS MARKED (C-CHECK RO 02/01/2026)REMOVED CORROSION ON STGR24L BETWEEN FS985 - FS1000. MATERIAL LOSS OF 0.005" IS WITHIN LIMITS OF REO 690-53-61-1656 REV -- DATED 2025-08-07. RESTORED FINISH. SEE CONTINUATJul 31, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2025073175149Door Sill · corrodedAFT BAGGAGE DOOR SILL CORRODED AS MARKED (C-CHECK RO 02/01/2026)AFT BAGGAGE DOOR SILL. P/N MM670-35655-003, NO DAMAGE IS ALLOWED ON THE SURROUND STRUCTURE OF THE AFT BAGGAGE BAY DOOR. IAW. CRJ900 SRM 53-61-23-101-001-A01REMOVED AND REPLACED AFT BAGGAGE DOOR SJul 31, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025073175132Stringer · corrodedCORROSION ON STGR26L BETWEEN FS1000.00 - FS1015.00 AS MARKED (C-CHECK RO 02/01/2026)REMOVED CORROSION ON STGR26L BETWEEN FS1000 - FS1015. MATERIAL LOSS OF 0.010" IS WITHIN LIMITS OF REO 690-53-61-1654 REV -- DATED 2025-08-06. RESTORED FINISH. SEE CONTINUATJul 31, 2025 · N821SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2025072975148Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 02/01/2026)REMOVED CRACKED INBD "A" BRACKET STANDOFF FROM L/H UPPER TRANSCOW AND INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF (WAS P/N CN624-2082-201, IS NOW P/N CN624-2082-S1401) ON L/H Jul 29, 2025 · N821SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA2025072975147Rivet · shearedLEFT LWR TRANSCOWL ZEE STIFFENER RIVETS ARE SHEARED. LT LWR TRANSCOWL ZEE STIFFENER HAS BEEN RE-INSTALLED REF REO# 690-54-21-586, REV --, DATED 8/18/25. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED W/SKYCARD 51-900-1002-SKY.Jul 29, 2025 · N821SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA2025072975131Stiffener · looseR/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 02/01/2026)REPLACED SHEARED RIVETS ON THE Z STIFFENER AND REPAIRED UNDERLYING CRACKS IN THE INNER PERFORATED SKIN ON THE R/H LOWER TRANSCOWL REF MHIRJ REO #690-54-21-582 REV (--) 2025-08-04 STEPS 1-Jul 29, 2025 · N821SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA2025072975130Latch · chafedR/H UPPER TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 02/01/2026)REPAIRED R/H UPPER TRANSCOWL, REF. REO 690-54-21-583, REV. --, 2025-08-14, ALL STEPS COMPLIED WITH. COMPLIED WITH M-337 AND SKYCARD 51-900-1002-SKYJul 29, 2025 · N821SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA2025072975129Stand Off · crackedRIGHT UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 02/01/2026)REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51Jul 29, 2025 · N821SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA2025072675146Stop Fitting · crackedRT FWD EMER EXIT DOOR, UPPER STOP ON THE DOOR, POSSIBLE CRACK IN THE DOOR FRAME (MARKED) (C-CHECK RO 02/01/2026)REPAIRED CRACK ON RH FORWARD EMERGENCY DOOR EXIT UPPER DOOR STOP IAW REO 670-52-21-103 REV. -- DATED 2024-11-06. COMPLIED WITH ALL STEPS OF REO 670Jul 26, 2025 · N821SK · Cndair CL6002D24 · Emergency ExitsSDR SWIA2025072675128Stop Fitting · crackedLH AFT EMER EXIT DOOR, UPPER STOP ON THE DOOR, POSSIBLE CRACK IN THE DOOR FRAME (MARKED) (C-CHECK RO 02/01/2026)FLUORESCENT PENETRANT INSPECTED PER REF CRJ900 NDTM 51-20-008-230-A01. NDT FAILED. ENDS OF CRACK MARKED FOR REPAIR. SEE ATTACHED NDT-11REPAIRED CRJul 26, 2025 · N821SK · Cndair CL6002D24 · Emergency ExitsSDR SWIA2025072675126Stop Fitting · crackedRH AFT EMER EXIT DOOR, UPPER STOP ON THE DOOR, POSSIBLE CRACK IN THE DOOR FRAME (MARKED) (C-CHECK RO 02/01/2026)REPAIRED CRACK ON AFT RH EMERGENCY EXIT DOOR UPPER DOOR STOP IAW REO 670-52-21-103 REV -- 2024-11-06. COMPLIED WITH ALL STEPS OF REO 670-52-21-103Jul 26, 2025 · N821SK · Cndair CL6002D24 · Emergency ExitsSDR SWIA2025072175119Rivet · damagedRT OTBD FLAP HAS SMOKING RIVETS ON TOP SIDE OF FLAP SKIN FROM APPOX. WS.200.00 TO WS.210.00 (MARKED). (C-CHECK RO 02/01/2026)REMOVED AND REPLACED FASTENERS (7 EA) ON RH OB FLAP TOP SIDE SKIN FROM APPOX. WS.200.00 TO WS.210.00. IAW REO 690-57-53-186 REV -- DAJul 21, 2025 · N821SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWIA2025071975145Beam · groovedLEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM HAS A LATERAL GROOVE, FLS140.40. (MARKED & FLAGGED) (C-CHECK RO 02/01/2026)REMOVED DAMAGE FROM THE LEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM AT FLS140.40 IAW CRJ900 SRM 51-12-00-001-001-A01.Jul 19, 2025 · N821SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWIA2025071975144Beam · groovedLEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM HAS A LATERAL GROOVE,FLS65.50. (MARKED & FLAGGED) (C-CHECK RO 02/01/2026)REMOVED DAMAGE FROM THE LEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM AT FLS65.50 IAW CRJ900 SRM 51-12-00-001-001-A01. COMJul 19, 2025 · N821SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWIA2025071975143Beam · groovedLEFT WING INBOARD FLAP INBOARD FLAP VANE ACTUATOR BEAM HAS A LATERAL GROOVE, FLS102.90. (MARKED & FLAGGED) (C-CHECK RO 02/01/2026)COMPLIED WITH REO 670-57-52-257 REV -B DATED 2024-10-17 REPARE OF LH WING IB FLAP IB FLAP VAIN ACTUATOR BEAM GROVE AT FLS 102.90Jul 19, 2025 · N821SK · Cndair CL6002D24 · Trailing Edge Flaps
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