# Service difficulty reports: N898SK

A list on [N898SK](https://openairdocs.org/aircraft/N898SK.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 · 118 reports

- [SDR SWIA2026072176665](https://openairdocs.org/sdr/SWIA2026072176665.md): Unknown · odor · Jul 21, 2026 · N898SK · Cndair CL6002D24 · Air Distribution System
  > AFT 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
- [SDR SWIA2026041775772](https://openairdocs.org/sdr/SWIA2026041775772.md): Fire Detector · faulted · Apr 17, 2026 · N898SK · Cndair CL6002D24 · Fire Detection
  > IN 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.
- [SDR SWIA2026033075519](https://openairdocs.org/sdr/SWIA2026033075519.md): Pseu · faulted · Mar 16, 2026 · N898SK · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR 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
- [SDR SWIA2026031875519](https://openairdocs.org/sdr/SWIA2026031875519.md): Warning Message · false activation · Mar 16, 2026 · N898SK · Cndair CL6002D24 · Landing Gear Position and Warning
  > GEAR 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 A
- [SDR SWIA202511261021](https://openairdocs.org/sdr/SWIA202511261021.md): Lintel · damaged · Oct 21, 2025 · N898SK · Cndair CL6002D24 · Passenger/Crew Doors
  > COMPLY 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
- [SDR SWI2025F01612](https://openairdocs.org/sdr/SWI2025F01612.md): Stringer · corroded · Jul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION 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.
- [SDR SWI2025F01611](https://openairdocs.org/sdr/SWI2025F01611.md): Channel · corroded · Jul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION 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: 51-90
- [SDR SWI2025F01610](https://openairdocs.org/sdr/SWI2025F01610.md): Stringer Splice · corroded · Jul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 53-00-03
- [SDR SWIA202511260706](https://openairdocs.org/sdr/SWIA202511260706.md): Stringer Splice · corroded · Jul 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 CHE
- [SDR SWIA202511260705](https://openairdocs.org/sdr/SWIA202511260705.md): Frame · corroded · Jul 5, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Frame
  > UPON 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. CO
- [SDR SWIA2025090200620](https://openairdocs.org/sdr/SWIA2025090200620.md): Drag Angle · cracked · Jun 20, 2025 · N898SK · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > DURING 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 2
- [SDR SWIA2025062300020](https://openairdocs.org/sdr/SWIA2025062300020.md): Drag Angle · cracked · Jun 20, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > DURING 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 PROGRESS
- [SDR SWIA202511260612](https://openairdocs.org/sdr/SWIA202511260612.md): Frame · corroded · Jun 12, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Frame
  > SECTION 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-SKY
- [SDR SWIA202511260606](https://openairdocs.org/sdr/SWIA202511260606.md): Floor Support · cracked · Jun 6, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT 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.
- [SDR SWIA202511260604](https://openairdocs.org/sdr/SWIA202511260604.md): Bracket · bent · Jun 4, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > S/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 STE
- [SDR SWI2025F01651](https://openairdocs.org/sdr/SWI2025F01651.md): Hinge · gouged · Jun 3, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > FUSELAGE 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 D
- [SDR SWIA202511260603](https://openairdocs.org/sdr/SWIA202511260603.md): Floor Support · cracked · Jun 3, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH 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.
- [SDR SWI2025F01650](https://openairdocs.org/sdr/SWI2025F01650.md): Skin · chafed · May 28, 2025 · N898SK · Cndair CL6002D24 · Ailerons
  > RIGHT 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. COMPLIED
- [SDR SWIA202511250528](https://openairdocs.org/sdr/SWIA202511250528.md): Frame · cracked · May 28, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Frame
  > BS 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.
- [SDR SWI2025F01647](https://openairdocs.org/sdr/SWI2025F01647.md): Floor Support · corroded · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERNAL 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 LIMI
- [SDR SWI2025F01646](https://openairdocs.org/sdr/SWI2025F01646.md): Floor Support · corroded · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERNAL 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 53-00-41-2
- [SDR SWI2025F01645](https://openairdocs.org/sdr/SWI2025F01645.md): Floor Support · corroded · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERNAL 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 690
- [SDR SWI2025F01644](https://openairdocs.org/sdr/SWI2025F01644.md): Shaft · dented · May 25, 2025 · N898SK · Cndair CL6002D24 · Trailing Edge Flap Control System
  > RIGHT 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
- [SDR SWI2025F01643](https://openairdocs.org/sdr/SWI2025F01643.md): Shaft · dented · May 25, 2025 · N898SK · Cndair CL6002D24 · Trailing Edge Flap Control System
  > RIGHT 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. O
- [SDR SWI2025F01642](https://openairdocs.org/sdr/SWI2025F01642.md): Shaft · dented · May 25, 2025 · N898SK · Cndair CL6002D24 · Trailing Edge Flap Control System
  > RIGHT 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 R
- [SDR SWI2025F01641](https://openairdocs.org/sdr/SWI2025F01641.md): Striker · dented · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Structure
  > BS 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.
- [SDR SWI2025F01640](https://openairdocs.org/sdr/SWI2025F01640.md): Floorbeam · corroded · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FLOORBEAM 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 690-53
- [SDR SWI2025F01639](https://openairdocs.org/sdr/SWI2025F01639.md): Floor Skin · cracked · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LEFT 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.
- [SDR SWI2025F01638](https://openairdocs.org/sdr/SWI2025F01638.md): Tie Down · corroded · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > TIEDOWN 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. COMPLI
- [SDR SWI2025F01637](https://openairdocs.org/sdr/SWI2025F01637.md): Floorbeam · corroded · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > INTERNAL 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 5
- [SDR SWIA202511260525](https://openairdocs.org/sdr/SWIA202511260525.md): Door Frame · cracked · May 25, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Structure
  > R/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 R
- [SDR SWI2025F01636](https://openairdocs.org/sdr/SWI2025F01636.md): Drag Angle · cracked · May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > RIGHT 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 51-42-22-001-0
- [SDR SWI2025F01635](https://openairdocs.org/sdr/SWI2025F01635.md): Frame · corroded · May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Frame
  > BS 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 53-00-06-991
- [SDR SWI2025F01634](https://openairdocs.org/sdr/SWI2025F01634.md): Skin · damaged · May 24, 2025 · N898SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT 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 C
- [SDR SWI2025F01633](https://openairdocs.org/sdr/SWI2025F01633.md): Stiffener · chafed · May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT 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 C
- [SDR SWI2025F01632](https://openairdocs.org/sdr/SWI2025F01632.md): Skin · cracked · May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LEFT 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 WIT
- [SDR SWI2025F01631](https://openairdocs.org/sdr/SWI2025F01631.md): Stringer · corroded · May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 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-
- [SDR SWI2025F01630](https://openairdocs.org/sdr/SWI2025F01630.md): Frame · corroded · May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Frame
  > BS 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. C
- [SDR SWI2025F01629](https://openairdocs.org/sdr/SWI2025F01629.md): Skin · damaged · May 24, 2025 · N898SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT 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. C
- [SDR SWI2025F01628](https://openairdocs.org/sdr/SWI2025F01628.md): Skin · damaged · May 24, 2025 · N898SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT 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-.
- [SDR SWIA202511260524](https://openairdocs.org/sdr/SWIA202511260524.md): Drag Angle · cracked · May 24, 2025 · N898SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LH 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, C
- [SDR SWI2025F01649](https://openairdocs.org/sdr/SWI2025F01649.md): Attach Angle · corroded · May 23, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > PANEL 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. C
- [SDR SWIA202511260523](https://openairdocs.org/sdr/SWIA202511260523.md): Attach Angle · corroded · May 23, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > PANEL 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-A01
- [SDR SWI2025F01609](https://openairdocs.org/sdr/SWI2025F01609.md): Door Frame · cracked · May 22, 2025 · N898SK · Cndair CL6002D24 · Emergency Exits
  > LEFT 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
- [SDR SWI2025F01608](https://openairdocs.org/sdr/SWI2025F01608.md): Floor Support · corroded · May 22, 2025 · N898SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT 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,
- [SDR SWI2025F01607](https://openairdocs.org/sdr/SWI2025F01607.md): Stop Fitting · cracked · May 22, 2025 · N898SK · Cndair CL6002D24 · Emergency Exits
  > LEFT 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.
- [SDR SWI2025F01606](https://openairdocs.org/sdr/SWI2025F01606.md): Stringer · corroded · May 22, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 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, REV
- [SDR SWIA202511260522](https://openairdocs.org/sdr/SWIA202511260522.md): Stop Fitting · cracked · May 22, 2025 · N898SK · Cndair CL6002D24 · Emergency Exits
  > RIGHT 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.
- [SDR SWI2025F01605](https://openairdocs.org/sdr/SWI2025F01605.md): Floorbeam · cracked · May 21, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFT 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 S
- [SDR SWI2025F01604](https://openairdocs.org/sdr/SWI2025F01604.md): Skin · gouged · May 21, 2025 · N898SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > GOUGE 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 GOO

Next page: https://openairdocs.org/aircraft/N898SK/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 = 'N898SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N898SK/reports

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