N898SK

Service difficulty reports · 118

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 = 'N898SK' 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 SWIA2026072176665Unknown · odorAFT FLIGHT ATTENDANT REPORTED STARTING TO SMELL A BURNING ODOR DURING FINAL APPROACH COMING FROM LAVATORY. DESCRIBED IT AS SIMILAR TO OIL BURNING AND SAID IT DID NOT SMELL LIKE VAPING OR CIGARETTE SMOKE. SMOKE DETECTOR DID NOT ACTIVATE. UPON REACHING GATE, HE Jul 21, 2026 · N898SK · Cndair CL6002D24 · Air Distribution SystemSDR SWIA2026041775772Fire Detector · faultedIN FLIGHT RECEIVED RT ENGINE FIRE WARNING MESSAGE, COMPLIED WITH QRC AND QRH. ENGINE WAS SHUTDOWN IN FLIGHT. (FLIGHT 3500) PERFORMED AN INSPECTION OF THE RT ENGINE THAT HAVE SALT WATER OR FIRE EXTINGUISHANT CONTAMINATION IAW AMM 72-00-00, NO DEFECTS NOTED. Apr 17, 2026 · N898SK · Cndair CL6002D24 · Fire DetectionSDR SWIA2026033075519Pseu · faultedGEAR UP DISAGREE FOR NLG UPON RE-TRACTION. RAN QRH, GEAR DEPLOYED AND LOCKED WITH ALL INDICATIONS GREEN. RETURNED TO FIELD. (FLIGHT 4081) FOUND THE FOLLOWING B1 CODES AT TIME OF EVENT 007451 065387 065386 007427 007432. TROUBLESHOT GEAR DISAGREE IAW FIM Mar 16, 2026 · N898SK · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR SWIA2026031875519Warning Message · false activationGEAR UP DISAGREE FOR NLG UPON RETRACTION. RAN QRH, GEAR DEPLOYED & LOCKED WITH ALL INDICATIONS GREEN. RETURNED TO FIELD. FOUND THE FOLLOWING B1 CODES AT TIME OF EVENT 007451 065387 065386 007427 007432. DEFERRED MLG RETRACTION SYSTEM IAW MEL 32-30-1 MX AMar 16, 2026 · N898SK · Cndair CL6002D24 · Landing Gear Position and WarningSDR SWIA202511261021Lintel · damagedCOMPLY WITH REO 670-53-21-493 REV -D 2015-07-10 REPAIRS TO PAX DOOR LINTEL (STR.3L) BTW FS 280 & 295 (C-CHECK) COMPLIED WITH REPAIRS TO PAX DOOR LINTEL (STR.3L) BTW FS 280 & 295 IAW ALL STEPS OF REO 670-53-21-493 REV-D, DATED 2015-07-10. COMPLIED WITH TASK Oct 21, 2025 · N898SK · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWI2025F01612Stringer · corrodedCORROSION ON STRINGER 26R BTWN BS 295 & 310. (C-CHECK) REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31630 REV. K SHEET 1.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. MAJOR REPAIR.Jul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWI2025F01611Channel · corrodedCORROSION ON INTERNAL TCAS LOWER CHANNEL BETWEEN BS 295 AND 310 AND BTWN S26R - 26L. (C-CHECK) REMOVED AND INSTALLED NEW TCAS CHANNEL IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-30023, REV G. COMPLIED WITH SKYWEST TASK CARD: 51-90Jul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01610Stringer Splice · corrodedCORROSION ON STRG 19R BTWN STA 597.00 AND ASTA 613.00 (C-CHECK) COMPLIED WITH DISPOSITION FOR STRINGER SPLICE REPAIR ON STR19R BTWN FS581.00 & FS613.00 (DEVIATION TO SRM 53-00-03-201-001-A02) IAW REO 690-53-31-1032 REV -- DATED 2025-07-14 CRJ900 SRM 53-00-03Jul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA202511260706Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 25L BTWN BS 333 AND 319.70. (C-CHECK) REMOVED AND INSTALLED NEW STRINGER SPLICE 25L AT FS 333 IAW SRM 51-42-06-001-001-A01 AND DRAWING SH670-32420, REV E, SHEETS 1, AND 3. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHEJul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA202511260705Frame · corrodedUPON REMOVAL FRAME SECTION AT FS969 BETWEEN STGR19R AND STRG24R FOUND MULTIPLES SPOTS OF CORROSION ON FRAME. (C-CHECK) COMPLIED WITH REPAIR FOR CORROSION DAMAGE ON LOWER FRAME FS969.00 BETWEEN STR20R-STR25R. REF REO 690-53-51-487 REV -- DATED: 2025-07-28. COJul 5, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2025090200620Drag Angle · crackedDURING RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE REMOVAL FIND CRACK ON RH VERT STAB-TO-FUSELAGE FWD DRAG ANGLE #30352476 (C-CHECK RO 08/29/2025)BLENDED CORRODED AREA OF LH WING FUEL ACCESS PANEL LANDING 510AB IN REFERENCE WITH REO 601R-57-21-030 REV. -L, DATED 2Jun 20, 2025 · N898SK · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR SWIA2025062300020Drag Angle · crackedDURING RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE REMOVAL FIND CRACK ON RH VERT STAB-TO-FUSELAGE FWD DRAG ANGLE #30352476 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSJun 20, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR SWIA202511260612Frame · corrodedSECTION FRAME AT FS 319.70 BETWEEN STGR 18L - STGR 21L HAS CORROSION TRANS #30300252 (C-CHECK) REMOVED AND INSTALLED NEW FRAME FS 319.70 STGR 18L -STGR 21L REF CRJ900 SRM 51-42-06-001-001-A01 DWG SH670-31810 REV AE COMPLIED WITH 51-900-1002-SKYJun 12, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA202511260606Floor Support · crackedRIGHT FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IS CRACKED. (C-CHECK) REMOVED AND REPLACED RT FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IAW SRM 53-11-10-201-006-A01.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY MAJOR REPAIR.Jun 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA202511260604Bracket · bentS/N 0755AFT BAGGAGE BAY UNDERFLOOR, BS 1031 - 1047, STRINGER 27L. THEIRS A BENT BRACKET. (C-CHECK) REMOVED AND REPLACED WITH NEW NEW BRACKET ON AFT BAGGAGE BAY UNDERFLOOR, IAW SRM 51-42-06-001-001-A01, REV 38 AND DWG MM670-36084, REV D. COMPLIED WITH ALL STEJun 4, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01651Hinge · gougedFUSELAGE SIDE AFT LUG LANDING ON PIANO HINGE IS GOUGED. (C-CHECK) REMOVED PAX DOOR PIANO HINGE FUSELAGE SIDE IAW SRM 53-21-23-201-007-A01, AND INSTTALLED NEW PAX DOOR PIANO HINGE OF FUSELAGE SIDE IAW SRM 53-21-23-201-007-A01, SRM 51-42-21-001-001-A01, AND DJun 3, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Door HingeSDR SWIA202511260603Floor Support · crackedLH FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IS CRACKED. (C-CHECK) REMOVED AND REPLACED LT FLOOR SUPPORT ANGLE OF CENTER COCKPIT FLOOR IAW SRM 53-11-10-201-006-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. MAJOR REPAIR.Jun 3, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01650Skin · chafedRIGHT WING AILERON HAS CHAFING ON THE LOWER LEADING EDGE, (C-CHECK) REMOVED AND WET INSTALLED NEW REPLACEMENT INBD & OUTBD L/E LOWER PANELS AT RT AILERON REF. SRM TASK 51-42-06-001-001-A01 & SRM TASK 51-42-21-001-001-A01 AND DWG CC670-13000 REV. D. COMPLIEDMay 28, 2025 · N898SK · Cndair CL6002D24 · AileronsSDR SWIA202511250528Frame · crackedBS 333 CRACKED AT APPROXIMATELY STRINGER 0. (C-CHECK) REPAIRED FRAME AT BS 333 AT APPROXIMATELY STR 0 IAW REO 690-53-21-1972, REV-. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.May 28, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F01647Floor Support · corrodedINTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR SUPPORT FS1015.00 TO FS1098.20 LBL27 FLOOR SUPPORTHAS CORROSION PITTING. (C-CHECK) REMOVED CORROSION AT FLOOR SUPPORT FS1051.00 TO FS1098.20 & LBL27 REF CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMIMay 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01646Floor Support · corrodedINTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR SUPPORT FS985.00 TO FS1098.20, LBL9. FLOOR SUPPORT HAS CORROSION PITTING. (C-CHECK) REMOVED AND INSTALLED NEW FABRICATED FLOOR SUPPORT SECTION LBL 9.0 FROM BS 977 TO BS 1080 AND REPAIR PARTS REF SRM 53-00-41-2May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01645Floor Support · corrodedINTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR SUPPORT BS 985 TO 1098.20, RBL 9, FLOOR SUPPORT HAS CORROSION PITTING. (C-CHECK) REPAIRED CORROSION ON FLOOR SUPPORT AT FS 985 TO1098.2 & RBL 9. IAW SRM 51-42-21-01-01-A01, SRM 53-00-41-201-001-A03 , REO 690May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01644Shaft · dentedRIGHT INBD FLAP, INBD VANE ACTUATOR SHAFT HAS A DENT. (C-CHECK) REMOVED, REPAIRED, AND REINSTALLED RT INBD FLAP INBD VANE ACTUATOR SHAFT IAW SRM 51-41-02-001-001-A01, ALL STEPS (1-5) OF REO 670-57-52-257, REV -A, AND DRAWING CC670-14303, REV -B. OPS TEST OF May 25, 2025 · N898SK · Cndair CL6002D24 · Trailing Edge Flap Control SystemSDR SWI2025F01643Shaft · dentedRIGHT INBD FLAP, SECOND FROM OTBD VANE ACTUATOR SHAFT HAS A DENT. (C-CHECK) REMOVED, REPAIRED, AND REINSTALLED RT INBD FLAP OTBD VANE ACTUATOR SHAFT IAW SRM 51-41-02-001-001-A01, ALL STEPS (1-5) OF REO 670-57-52-257, REV -A,, & DRAWING CC670-14303, REV -B. OMay 25, 2025 · N898SK · Cndair CL6002D24 · Trailing Edge Flap Control SystemSDR SWI2025F01642Shaft · dentedRIGHT INBD FLAP, OTBD VANE ACTUATOR SHAFT HAS INDENT. (C-CHECK) BLENDED OUT THE DAMAGE ON RT INBD FLAP, OTBD VANE ACTUATOR SHAFT IAW REO 670-57-52-257, REV A. FOUND TO BE IN LIMITS IAW REO 670-57-52-257, REV. A. COMPLIED WITH ALL STEP OF REO 670-57-52-257 RMay 25, 2025 · N898SK · Cndair CL6002D24 · Trailing Edge Flap Control SystemSDR SWI2025F01641Striker · dentedBS 310 SEAL STRIKER DENTED.UPPER FWD FITTING. (C-CHECK) REPAIRED PAX DOOR FWD UPPER SEAL STRIKER BS 310 IAW SRM 53-21-23-201-006-A01. COMPLIED WITH 51-900-1002-SKY.May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01640Floorbeam · corrodedFLOORBEAM BS 985 TO 1098.20, RBL 27 HAS CORROSION PITTING. CIRCLE WITH BLACK GREASE PENCIL. (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED CORROSION DAMAGE TO RBL 27.FLOORBEAM BETWEEN BS 1069.75 & 1088.20 IAW SRM 53-00-41-201-001-A03, REV 38. AND REO 690-53May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F01639Floor Skin · crackedLEFT SIDE FWD EQUIPMENT COMPARTMENT TRU BAY FLOOR WEB IS CRACKED IN THE RADIUS. (C-CHECK). REPAIRED LHS FWD EQUIPMENT COMPARTMENT TRU BAY FLOOR WEB IAW GREO 670-53-11-509, REV -E. ALL APPLICABLE STEPS OF GREO COMPLETED FOR A LEFT REPAIR.May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01638Tie Down · corrodedTIEDOWN FITTING AT BS 565 BETWEEN STR 22L - 23L IS CORRODED. (C-CHECK) REMOVED AND REPLACED TIEDOWN FITTING AT BS 565 BETWEEN S22L AND 23L. IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG SH690-33600, REV AH. COMPLIMay 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01637Floorbeam · corrodedINTERNAL STRUCTURE OF THE REAR FUSELAGE - FLOOR CROSS BEAM FS1047 LT HAS PITTING CORROSION. FLAGGED (C-CHECK) REMOVED CORROSION ON FLOOR CROSS BEAM FS1047 BETWEEN LBL27 AND LBL35 REF CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS REF CRJ900 SRM 5May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWIA202511260525Door Frame · crackedR/H SIDE FWD EQUIPMENT COMPARTMENT AFT DOOR LATCH CUTOUT HAS A SUSPECTED CRACK ON THE DOOR LANDING. (C-CHECK RO 11/25/2025)REMOVED AND INSTALLED NEW RT SIDE FWD EQUIPMENT COMPARTMENT AFT DOOR LANDING IAW CRJ900 SRM 51-42-06-001-001-A01 AND REO 690-53-11-2033 RMay 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01636Drag Angle · crackedRIGHT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE AFT END POSSIBLE CRACKED. (C-CHECK) REMOVED AND REPLACED WITH NEW RT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. IAW DWG BA670-35002, REV -F, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-22-001-0May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR SWI2025F01635Frame · corrodedBS 969 FRAME WEB ON THE FWD SIDE AT STRINGER 26R AND THE ATTACHED FLANGE BETWEEN STRINGER 26 - 27R ARE CORRODED. (C-CHECK) PERFORMED CUT-AWAY OF DAMAGED FRAME SECTION ON FRAME BS 969 FROM STR 25R TO STR 25L. IAW SRM 53-00-06-201-001-A03, FIGURE 53-00-06-991May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F01634Skin · damagedRIGHT WING, UNDER PANEL 631BZ HAS TOOLING DAMAGE. (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED TOOL DAMAGE TO RT NR 2 SLAT AFT SKINS BETWEEN SS 261.25, TRACK 2-2, AND BETWEEN SS 315.75, TRACK 2-3 IAW REO 690-57-42-1237, REV-. COMPLIED WITH SKYWEST TASK CMay 24, 2025 · N898SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWI2025F01633Stiffener · chafedAFT PRESSURE BULKHEAD STIFFENER LBL 9, AT THE BOTTOM INNER CHAFFED HOLE (MARKED) (C-CHECK). REPAIRED AFT PRESSURE BULKHEAD STIFFENER LBL 9 AT THE BOTTOM INNER CHAFE HOLE. REF REO 690-53-61-1640 REV-. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CMay 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01632Skin · crackedLEFT TRU BAY ACCESS, LOWER AFT CORNER OF THE FUSELAGE SKIN POSSIBLE CRACK IN RADIUS. (C-CHECK) REPAIRED LT TRU BAY ACCESS THE LOWER AFT CORNER OF THE FUSELAGE SKIN IAW REO 690-53-11-2023 REV-. COMPLIED WITH ALL STEPS OF REO 690-53-11-2023 REV-. COMPLIED WITMay 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWI2025F01631Stringer · corrodedSTR 20L IS CORRODED BETWEEN FS954 - 969. (C-CHECK) BLENDED CORROSION AT STR 20 AT FS954 TO 969 IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS. IAW SRM 53-51-03-101-002-A04. REPAIRED STR 20L REF REO 690-53-51-483 REV-. COMPLIED WITH ALL STEPS OF REO 690-May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWI2025F01630Frame · corrodedBS 942 FRAME WEB ON THE FWD AND AFT SIDES BETWEEN STR 25L &26L AND THE ATTACHED FLANGE BETWEEN STR 25L €“ 25R ARE CORRODED. (C-CHECK) REMOVED AND INSTALLED NEW FRAME SECTION & SPLICES ON BS.942, BETWEEN STGR 25L & 25RT. REF CRJ900 SRM 53-00-06-201-001-A03. CMay 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F01629Skin · damagedRIGHT WING, UNDER PANEL 631CZ HAS TOOLING DAMAGE, (C-CHECK) COMPLIED WITH DISPOSITION FOR BLENDED TOOL DAMAGE TO RT NR 2 SLAT AFT SKINS BETWEEN SS261.25 - TRACK 2-2, AND BETWEEN SS315.75 - TRACK 2-3 IAW REO 690-57-42-1237 REV- AND SRM 51-12-00-001-001-A01. CMay 24, 2025 · N898SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWI2025F01628Skin · damagedRIGHT WING, UNDER PANEL 622CZ HAS TOOLING DAMAGE, (C-CHECK) REPAIRED RIGHT WING SLAT NR 1 AFT SKIN, UNDER PANEL 622CZ REF. REO 690-57-42-1238 REV-.May 24, 2025 · N898SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWIA202511260524Drag Angle · crackedLH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE FWD END POSSIBLE CRACK (MARKED) (C-CHECK RO 11/25/2025)REMOVED AND INSTALLED NEW AFT DRAG ANGLE PN# AV670-21186-003 ON LH VERTICAL STABILIZER REF CRJ900 SRM 51-42-13-001-001-A01, CRJ900 SRM 51-42-22-001-001-A01, CMay 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR SWI2025F01649Attach Angle · corrodedPANEL 542AZ IN THE LT GEAR WELL, THE ATTACH ANGLE ON THE AFT SIDE OF THE AFT WING SPAR, IS CORRODE ON TOP AND BOTTOM. (C-CHECK) REPLACED NEW ATTACH ANGLE TO LT WHEEL WELL ANGLE COMMON TO PANEL 542AZ IAW SRM, 51-42-21-001-001-A01 AND DWG CC670-10320 REV- F. CMay 23, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR SWIA202511260523Attach Angle · corrodedPANEL 642AZ IN THE RH GEAR WELL, THE ATTACH ANGLE ON THE AFT SIDE OF THE AFT WING SPAR, IS CORRODE ON TOP AND BOTTOM (MARKED) (C-CHECK RO 11/25/2025)REPLACED NEW ATTACH ANGLE TO RH WHEEL WELL ANGLE COMMON TO PANEL 642AZ REF. CRJ-900 SRM, 51-42-21-001-001-A01May 23, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR SWI2025F01609Door Frame · crackedLEFT FWD OVERWING EMERGENCY DOOR UPPER STOP FITTING, POSSIBLE CRACKED ON THE DOOR FRAME. (C-CHECK) REPAIRED CRACK FROM LT FWD OVERWING EMERGENCY DOOR UPPER STOP FITTING, ON THE DOOR FRAME IAW REO 670-52-21-103, REV--, NOTES 1-17. COMPLIED WITH SKYWEST TASK May 22, 2025 · N898SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F01608Floor Support · corrodedRIGHT FLOOR SILL IS CORRODED AND SCRATCHED FS280 - 319. (C-CHECK) REMOVED AND REPLACED RT FLOOR SILL IAW SRM 51-42-06-001-001-A01, DWG SH670-32170, REV. V & EDRN SH670-32172 REV D . COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOD,May 22, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01607Stop Fitting · crackedLEFT AFT OVERWING EMER DOOR UPPER STOP FITTING, POSSIBLE CRACK ON THE DOOR FRAME. (C-CHECK) REPAIRED CRACK FROM LH AFT OVERWING EMERGENCY DOOR UPPER STOP FITTING, ON THE DOOR FRAME IAW REO 670-52-21-103, REV. --, COMPLIED WITH TASK CARD 51-900-1002-SKY.May 22, 2025 · N898SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F01606Stringer · corrodedSTRINGER 27 AT BS 280 (ADJACENT TO BUTT STRAP) IS CORRODED, AND APPERS TO HAVE MISSING PIECES ALONG EDGE (C-CHECK) REMOVED AND INSTALLED NEW STRINGER 27 BETWEEN FS280 AND FS299. IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG SH670-31630, REVMay 22, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA202511260522Stop Fitting · crackedRIGHT AFT OVERWING EMER DOOR UPPER STOP FITTING, POSSIBLE CRACK ON THE DOOR FRAME. (C-CHECK) REPAIRED CRACK FROM RT AFT OVERWING EMERGENCY DOOR UPPER STOP FITTING, ON THE DOOR FRAME IAW 670-52-21-103, REV -, NOTES 1-17 SEE CONTINUATION CARD FOR WORK DETAILS. May 22, 2025 · N898SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F01605Floorbeam · crackedAFT SIDE OF FS280.00 CROSS BEAM, THE OUTBD ATTACH ANGLE FOR RBL9 FLOOR BEAM CRACKED. (C-CHECK). REMOVED AND REPLACED ATTACH ANGLE P/N CC670-34099-2 AT BS 280, RBL9. IAW SRM 51-42-21-001-001-A01, AND DWG KBA670-30026 REV. J, SHEET 5, 7 AND 9. COMPLIED WITH SMay 21, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F01604Skin · gougedGOUGE ON OUTER SKIN STGR27 BETWEEN FS913.00 & 927.00. (MARKED) (C-CHECK) COMPLIED WITH REPAIR TO FUSELAGE SKIN AT FS913.00 AND STR 27 REF REO 690-53-51-484 REV -- AND REO 670-53-00-290 REV -F . COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK GOOMay 21, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
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