# Service difficulty reports: N803SK

A list on [N803SK](https://openairdocs.org/aircraft/N803SK.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 6 · 276 reports

- [SDR SWIA2026080176709](https://openairdocs.org/sdr/SWIA2026080176709.md): Fitting · damaged · Aug 1, 2026 · N803SK · Cndair CL6002D24 · Horizontal Stabilizer Structure
  > FOUND HSTAB RT UPPER FITTING ASSY (AIPC 27-42-01, ITEM 30) TO HAVE DAMAGE. BLENDED DAMAGE ON HSTA RT UPPER HORIZONTAL STAB FITTING ASSY IAW REO 690-55-11-231 REV-. PERFORMED EDDY CURRENT OF THE REWORKED AREA IAW NDTM 51-20-006 AND CONFIRMED AREA IS CRACK FRE
- [SDR SWIA2026080176710](https://openairdocs.org/sdr/SWIA2026080176710.md): Fitting · damaged · Aug 1, 2026 · N803SK · Cndair CL6002D24 · Horizontal Stabilizer Miscellaneous Structure
  > FOUND HORIZONTAL STAB LT UPPER FITTING ASSEMBLY (AIPC 27-42-01, ITEM 28) TO HAVE DAMAGE. BLENDED DAMAGE ON HSTA LT UPPER HORIZONTAL STAB FITTING ASSY IAW REO 690-55-11-231, REV-. PERFORMED EDDY CURRENT OF REWORKED AREA IAW NDTM 51-20-006 AND CONFIRMED AREA
- [SDR SWIA2026080376709](https://openairdocs.org/sdr/SWIA2026080376709.md): Fitting · damaged · Aug 1, 2026 · N803SK · Cndair CL6002D24 · Horizontal Stabilizer Miscellaneous Structure
  > FOUND HORIZONTAL STAB RT UPPER FITTING ASSEMBLY (AIPC 27-42-01, ITEM 30) TO HAVE DAMAGE OPEN.
- [SDR SWIA20260107231](https://openairdocs.org/sdr/SWIA20260107231.md): Selector Valve · warning message · Dec 31, 2025 · N803SK · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > HAD GEAR DISAGREE RED WARNING MESSAGE AFTER TAKEOFF. RAN QRH. MESSAGE DISAPPEARED AND RETURNED TO NEAREST SUITABLE AIRPORT (FLIGHT 3787). REF CP31463815, CP31463817, CP31463868, CP31463869, CP31464141, CP31464560, CP31465126, CP31465652, CP31465667, CP31469
- [SDR SWI2026F00001](https://openairdocs.org/sdr/SWI2026F00001.md): Warning Message · illuminated · Dec 31, 2025 · N803SK · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > HAD GEAR DISAGREE RED WARNING MESSAGE AFTER TAKEOFF. RAN QRH. MESSAGE DISAPPEARED AND RETURNED TO NEAREST SUITABLE AIRPORT (FLIGHT 3787) OPEN,
- [SDR SWIA2025110300730](https://openairdocs.org/sdr/SWIA2025110300730.md): Floor Support · cracked · Jul 30, 2025 · N803SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT ANGLE AT LBL12.00 BETWEEN FS 260.00 - 280.00 HAS CRACK #30576663 (C-CHECK RO 11/01/2025)REMOVED AND REPLACED LH FLOOR SUPPORT ANGLE AT LBL 12.0, BETWEEN FS 260- FS 280 WITH NEW PN CC670-33199-3 AND LH FLOOR GUSSET AT LBL 12.0, FS 280 WI
- [SDR SWIA2025110300726](https://openairdocs.org/sdr/SWIA2025110300726.md): Stand Off · cracked · Jul 26, 2025 · N803SK · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL OUTBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED NEW L/H UPPER TRANSCOWL O/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23.,OPS TEST OF TRANSCOWL LATCHES GOOD.COMPLIED WITH 51
- [SDR SWIA2025110300725](https://openairdocs.org/sdr/SWIA2025110300725.md): Floor Support · corroded · Jul 25, 2025 · N803SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FLOOR SILL FOR ACCESS TO FS.613 FRAME REPAIR FOUND HEAVY CORROSION ON SILL ATTACH FLANGE AT STGR 17L BETWEEN FS.613 - FS.629. (C-CHECK RO 11/01/2025)REPAIRED LH FLOOR SILL BETWEEN FS597 TO FS629 REF REO 690-53-31-1051 REV.-- DATED 2025-09-04
- [SDR SWI2025F01479](https://openairdocs.org/sdr/SWI2025F01479.md): Roller · failed insp · Jul 20, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > R/H SLAT TRACK 3-2 SIDE ROLLERS AT FWD I/B, FWD O/B, AFT I/B AND AFT O/B FAILED INSPECTION. (S/N 00774) (C-CHECK RO 11/01/2025)REPLACED R/H SLAT TRACK 3-2 SIDE ROLLERS AT FWD I/B, FWD O/B, AFT I/B AND AFT O/B REF CRJ 900 AMM 27-81-44-400 -803-A01,REF CRJ9
- [SDR SWI2025F01478](https://openairdocs.org/sdr/SWI2025F01478.md): Roller · failed insp · Jul 20, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > R/H SLAT TRACK 2-2 SIDE ROLLERS AT FWD O/B AND AFT O/B FAILED INSPECTION. (S/N 00773) (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED NEW SIDE ROLLERS PN: CC670-12027-3 1(EA) AND PN: CC670-12048-3 1(EA) REF CRJ900 AMM 27-81-44-400-802-A01,REF CRJ900 AMM 27-81-
- [SDR SWI2025F01477](https://openairdocs.org/sdr/SWI2025F01477.md): Roller · failed insp · Jul 20, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > R/H SLAT TRACK 1-2 SIDE ROLLERS AT FWD I/B AND AFT I/B FAILED INSPECTION. (S/N 00772) (C-CHECK RO 11/01/2025)REPLACED R/H SLAT TRACK 1-2 SIDE ROLLERS AT FWD I/B AND AFT I/B REF CRJ900 AMM 27-81-44-400-801-A01, REF CRJ900 AMM 27-81-44-000-801-A01 TUC8616 CA
- [SDR SWIA2025110300720](https://openairdocs.org/sdr/SWIA2025110300720.md): Floor Support · cracked · Jul 20, 2025 · N803SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL12.00 FLOORBEAM COCKPIT HAS CRACK. BETWEEN FS270 AND FS280. TRANS #30519326 (C-CHECK RO 11/01/2025)REPARED LBL12.00 FLOORBEAM COCKPIT REF CRJ900 SRM 53-11-43-201-003-A01. SEE CONTNINUE CARD FOR MORE DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FO
- [SDR SWI2025F01482](https://openairdocs.org/sdr/SWI2025F01482.md): Roller · failed insp · Jul 19, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > L/H SLAT TRACK 1-2 SIDE ROLLERS AT FWD I/B AND FWD O/B FAILED INSPECTION. (S/N 00770) (C-CHECK RO 11/01/2025)REPLACED SIDE ROLLERS WITH NEW AT L/H SLAT TRACK 1-2 SIDE ROLLERS AT FWD I/B AND FWD O/B REF CRJ900 AMM 27-81-44-400-801-A01,REF CRJ900 AMM 27-81-
- [SDR SWI2025F01481](https://openairdocs.org/sdr/SWI2025F01481.md): Roller · failed insp · Jul 19, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > L/H SLAT TRACK 3-2 SIDE ROLLERS AT FWD I/B, FWD O/B AND AFT O/B FAILED INSPECTION. (S/N 00769) (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED L/H SLAT TRACK 3-2 SIDE ROLLERS AT FWD I/B, FWD O/B AND AFT O/B.(3EA NEW ROLLERS) REF CRJ-900 AMM 27-81-44-400-803-A0
- [SDR SWI2025F01480](https://openairdocs.org/sdr/SWI2025F01480.md): Roller · failed insp · Jul 19, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > L/H SLAT TRACK 2-2 SIDE ROLLERS AT FWD I/B, FWD O/B AND AFT O/B FAILED INSPECTION. (S/N 00768) (C-CHECK RO 11/01/2025)REPLACED SIDE ROLLERS PN: CC670-12027-3 1(EA) AND PN: CC670-12048-3 2(EA) WITH NEW REF CRJ900 AMM 27-81-44-400-802-A01,REF CRJ900 AMM 27-81
- [SDR SWIA2025110300719](https://openairdocs.org/sdr/SWIA2025110300719.md): Roller · failed insp · Jul 19, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > L/H SLAT TRACK SIDE ROLLERS AT FWD I/B AND FWD O/B FAILED INSPECTION. (S/N 00767) (C-CHECK RO 11/01/2025)DEFECT DESCRIPTION MISSING SLAT TRACK LOCATION OF FAULTY ROLLERS. PLEASE SEE CAMP 30516910 (HN00253759)
- [SDR SWI2025F01484](https://openairdocs.org/sdr/SWI2025F01484.md): Hinge · chafed · Jul 16, 2025 · N803SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > ( MX 30497653) UPON VISUAL INSPECTION OF PAX DOOR PIANO HINGE FUSELAGE SIDE, FOUND MULTIPLE CHAFES MARKS ON LUG LANDS AND LUGS. (C-CHECK RO 11/01/2025)REPAIRED F PAX DOOR PIANO HINGE FUSELAGE SIDE ORIGINAL THICKNESS 0.134" IAW DWG SH670-31876 REV G REMOVED T
- [SDR SWIA20251103716](https://openairdocs.org/sdr/SWIA20251103716.md): Stand Off · cracked · Jul 16, 2025 · N803SK · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/01/2025)REMOVED CRACKED INBD "A" BRACKET STANDOFF AND INSTALLED 1 EA NEW "A" BRACKET STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF MHIRJ GREO #670-54-21-971 REV (-B) 2023-11-28
- [SDR SWI2025F01483](https://openairdocs.org/sdr/SWI2025F01483.md): Hinge · scratched · Jul 16, 2025 · N803SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > (MX 30497765) DURING VISUAL INSPECTION OF PAX DOOR PIANO FUSELAGE DOOR SIDE FOUND MULTIPLE SCRATCHES AND CHAFES ON INBOARD HINGE FLANGE AND LUGS (C-CHECK RO 11/01/2025)REPAIRED PAX DOOR PIANO FUSELAGE DOOR SIDE PAX DOOR PIANO HINGE LUGS MINIMUM MATERIAL WAL
- [SDR SWI2025F01485](https://openairdocs.org/sdr/SWI2025F01485.md): Hinge · nicked · Jul 15, 2025 · N803SK · Cndair CL6002D24 · Ailerons
  > LH AILERON AFT SPAR HINGES FOUND TO BE NICKED. HINGE #2, 4, & 5 #30488376 (C-CHECK RO 11/01/2025)BLENDED DAMAGE ON LH AILERON AFT SPAR HINGES #2, 4, & 5 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 690-57-51-454 REV -- DATE 2025-07-28. COMPLIED WITH ALL S
- [SDR SWIA202511030715](https://openairdocs.org/sdr/SWIA202511030715.md): Hinge · nicked · Jul 15, 2025 · N803SK · Cndair CL6002D24 · Ailerons
  > RH AILERON AFT SPAR HINGES FOUND TO BE NICKED. HINGE #4, 6, & 8 #30488383 (C-CHECK RO 11/01/2025)REMOVED DAMAGE FROM RH AILERON AFT SPAR HINGES #4, 6, AND 8. COMPLIED WITH REO 690-57-51-453, REV --. DATE: 2025-07-28. COMPLIED WITH 51-900-1002-SKY (CL600-2D24
- [SDR SWI2025F01492](https://openairdocs.org/sdr/SWI2025F01492.md): Hinge · gouged · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Trailing Edge Flaps
  > R/H O/B FLAP HAS A GOUGE ON THE HINGE ASSEMBLY BELOW THE HINGE APEX AT WS178.00 (MARKED). (S/N#00633) (C-CHECK RO 11/01/2025)REPAIRED R/H O/B FLAP HINGE ASSEMBLY BELOW THE HINGE APEX AT WS178.00 PER REO 690-57-53-181 REV-- DATED: 2025-07-23 STEPS 1 - 4 ( SE
- [SDR SWI2025F01491](https://openairdocs.org/sdr/SWI2025F01491.md): Frame · corroded · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME 597 BETWEEN STRINGERS 18L AND 19L. (S/N#00610) (C-CHECK RO 11/01/2025)REPLACED FRAME 597 BETWEEN STRINGERS 18L AND 19L REF DWG SH690-33750 REV. AF AND CRJ900 SRM 51-42-06-001-001-A01, AND CRJ900 SRM 51-42-21-001-001-A01. LEAK CHECK GO
- [SDR SWI2025F01490](https://openairdocs.org/sdr/SWI2025F01490.md): Frame · corroded · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME 533 BETWEEN STRINGERS 17L AND 18L. (S/N#00608) (C-CHECK RO 11/01/2025)REPAIRED FRAME 533 BETWEEN STRINGERS 17L AND 18L REF REO 690-53-31-1044 REV -- DATED 2025-07-30 COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2025F01489](https://openairdocs.org/sdr/SWI2025F01489.md): Stringer · corroded · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 18R BETWEEN FS517 AND 533. (S/N#00600) (C-CHECK RO 11/01/2025)REPAIRED STRINGER 18R BETWEEN FS477 AND FS606 REF CRJ900 SRM 51-42-06-001-001-A01, DWG SH690-33101 REV. M, AND DWG SH670-30006 REV. A. LEAK CHECK GOOD. COMPLIED WITH TAS
- [SDR SWI2025F01488](https://openairdocs.org/sdr/SWI2025F01488.md): Skin · gouged · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Trailing Edge Flaps
  > R/H O/B FLAP HAS A GOUGE ON THE HINGE ASSEMBLY BELOW THE HINGE APEX AT WS220.00 (MARKED). (S/N#00634) (C-CHECK RO 11/01/2025)REMOVED DAMAGE ON R/H OUTBOARD HINGE ASSY BELOW HINGE APPROX. WS220.00 REF CRJ-900 SRM 51-12-00-001-001-A01 AND PERFORMED REPAIRS PER
- [SDR SWI2025F01487](https://openairdocs.org/sdr/SWI2025F01487.md): Frame · corroded · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME 645 BETWEEN STRINGERS 17L AND 18L. (S/N#00612) (C-CHECK RO 11/01/2025)REPLACED FRAME 645 BETWEEN STGRS 18L AND 14L REF CRJ900 SRM 53-00-06-201-001-A03, AND DWG SH690-33100 REV. N. LEAK CHECK GOOD. COMPLETED SKYWEST TASK CARD 51-900-1
- [SDR SWI2025F01486](https://openairdocs.org/sdr/SWI2025F01486.md): Skin · chafed · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Ailerons
  > L/H AILERON HAS SIGNS OF CHAFFING ACROSS THE UPPER LEADING EDGE. (S/N#00627) (C-CHECK RO 11/01/2025)REMOVED AND REPLACED L/H AILERON UPPER LEADING EDGE REF CRJ900 SRM TASK 51-23-00-001-001-A01, SRM TASK 51-42-21-001-001-A01 & SRM TASK 51-42-06-001-001-A01
- [SDR SWIA202511030712](https://openairdocs.org/sdr/SWIA202511030712.md): Frame · corroded · Jul 12, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME 613 BETWEEN STRINGERS 17L AND 18L. (S/N#00611) (C-CHECK RO 11/01/2025)REPAIRED FRAME 613 BETWEEN STGRS 18L TO 14L REF CRJ900 SM 53-00-06-201-001-A01 AND DWG SH690-33100 REV. N. LEAK CHECK GOOD. COMPLETED 51-900-1002-SKY.
- [SDR SWIA202511030711](https://openairdocs.org/sdr/SWIA202511030711.md): Floorbeam · corroded · Jul 11, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS280.00 FWD FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION. (S/N#00568) (C-CHECK RO 11/01/2025)REMOVED AND REPLACED NEW ANGLE FLOOR SUPPORT ON FS 280.00 FWD REF CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG# CC670-34326 REV -A COMPLIED
- [SDR SWI2025F01495](https://openairdocs.org/sdr/SWI2025F01495.md): Restraint · corroded · Jul 10, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > FWD BAGGAGE BAY CARGO RESTRAINT NET MOUNT BRACKET HAS MULTIPLE SPOTS OF CORROSION AT APPOX. FS565.00 AND STR.23L (MARKED) 30466400 (C-CHECK RO 11/01/2025)BLENDED CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED WITH NEW MOUNT BRACKET. REF. CRJ900 SRM
- [SDR SWI2025F01494](https://openairdocs.org/sdr/SWI2025F01494.md): Retainer · damaged · Jul 10, 2025 · N803SK · Cndair CL6002D24 · Cargo/Baggage Doors
  > CENTER CARGO DOOR LOWER SEAL RETAINER PN LE670-39644-1 HAS RIVETS INSTALLED INCORRECTLY. SHOULD BE DOUBLE FLUSH PER DWG NO. LE670-39610 REV L. (C-CHECK RO 11/01/2025)REPAIRED THE OVERSIZED LOWER RETAINERATTATCHMENT HOLES ON THE CENTER BAGGAGE BAY DOOR STRUCT
- [SDR SWI2025F01493](https://openairdocs.org/sdr/SWI2025F01493.md): Restraint · corroded · Jul 10, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > FWD BAGGAGE BAY CARGO RESTRAINT NET MOUNT BRACKET HAS MULTIPLE SPOTS OF CORROSION AT APPOX. FS565.00 AND STR.26L (MARKED). (C-CHECK RO 11/01/2025)BLENDED CORROSION AND FOUND OUT OF LIMITS. INSTALLED NEW MOUNT BRACKET REF. CRJ900 SRM 51-42-21-001-001-A01 REV
- [SDR SWIA202511030710](https://openairdocs.org/sdr/SWIA202511030710.md): Restraint · corroded · Jul 10, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > FWD BAGGAGE BAY CARGO RESTRAINT NET MOUNT BRACKET HAS MULTIPLE SPOTS OF CORROSION AT APPOX. FS517.00 STR27 (MARKED). (C-CHECK RO 11/01/2025)REPLACED WITH NEW FWD BAGGAGE BAY CARGO RESTRAINT NET MOUNT BRACKET PER DWG SH670-33600 REV AD, CRJ900 SRM 51-42-2
- [SDR SWIA202511030709](https://openairdocs.org/sdr/SWIA202511030709.md): Door Sill · corroded · Jul 9, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED NEW KICKPLATE ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV. AE AND COMPLIED WITH TASK CARD 51-900
- [SDR SWIA202511030706](https://openairdocs.org/sdr/SWIA202511030706.md): Slat Track · dented · Jul 6, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > LH SLAT TRACK 3-3 HAS ROLLER INDENTATIONS ON LWR SIDE. (CAMP#30441807) (C-CHECK RO 11/01/2025)PERFORMED BLEND OUT ON LH SLAT TRACK 3-3 HAS ROLLER INDENTATIONS ON LWR SIDE REF CRJ900 SRM 51-12-00-001-001-A01 AND PERFORMED REPAIRS PER REO 690-57-42-1253 REV --
- [SDR SWI2025F01497](https://openairdocs.org/sdr/SWI2025F01497.md): Stand Off · cracked · Jul 2, 2025 · N803SK · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL OUTBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED NEW R/H UPPER TRANSCOWL OUTBD "A" BRAKET (P/N CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23, OPS TEST OF TRANSCOWL LATCHES GOOD. COMPLIED WI
- [SDR SWI2025F01496](https://openairdocs.org/sdr/SWI2025F01496.md): Support · corroded · Jul 2, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Structure
  > NOSE GEAR JACK PAD LEFT HAND SUPPORT LOWER FLANGE IS CORRODED.(MARKED) (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED NEW NOSE GEAR JACK PAD LH SUPPORT REF. DWG CC670-32050 REV-NC, CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01. COMPLIED WI
- [SDR SWIA202511030702](https://openairdocs.org/sdr/SWIA202511030702.md): Stand Off · cracked · Jul 2, 2025 · N803SK · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H LOWER TRANSCOWL INBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 11/01/2025)L/H LWR TRANSCOWL I/B "A"BRACKET HAS BEEN REMOVED AND REPLACED (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWI2025F01476](https://openairdocs.org/sdr/SWI2025F01476.md): Slat Track · corroded · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-3 HAS CORROSION AS MARKED (C-CHECK RO 11/01/2025)COMPLIED WITH REO 690-57-42-1253 REV-- DATED: 2025-07-16 STEP 1-7 NO ADJUSTMENT NECESSARY AND ENSURED SLAT RIGGING REQUIREMENT ARE MET. REF CRJ900 AMM 27-81-43-820-802-A01,REF CRJ900 AMM
- [SDR SWI2025F01475](https://openairdocs.org/sdr/SWI2025F01475.md): Slat Track · gouged · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-1 GOUGED AS MARKED (C-CHECK RO 11/01/2025)REMOVED DAMAGED LEFT WING SLAT TRACK 1-1 REF. CRJ 900 SRM 51-12-00-001-001-A01, COMPLIED WITH WITH REO 690-57-42-1252 REV-- DATED: 2025-07-16 STEPS 1 TO 7, OPS TEST OF FLAPS/SLATS GOOD. COMPLY
- [SDR SWI2025F01474](https://openairdocs.org/sdr/SWI2025F01474.md): Slat Track · gouged · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING SLAT TRACK 3-3 GOUGED AS MARKED (C-CHECK RO 11/01/2025) REMOVED GOUGES FROM RH WING SLAT TRACK 3-3 REF. CRJ 900 SRM 51-12-00-001-001-A01. AND PERFORMED REPAIR PER REO 690-57-42-1255 REV-- DATED: 2025-07-16. ALL CHECKS GOOD. COMPLIED WITH TASK CARD
- [SDR SWI2025F01473](https://openairdocs.org/sdr/SWI2025F01473.md): Rod · dented · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBOARD FLAP, INBOARD VANE ACTUATOR ROD HAS INDENT. (C-CHECK RO 11/01/2025)REMOVED DAMAGE ON RH IB FLAP -IB VANE ACTUATOR ROD TO SMOOTH CONTOUR PER REO 670-57-52-257 REV B DATED 2024-10-17 AND DWG CC670-14303 REV B. ALL STEPS OF REO COMPLIED WITH. ALL CH
- [SDR SWI2025F01472](https://openairdocs.org/sdr/SWI2025F01472.md): Rod · dented · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBOARD FLAP, SECOND TO INBOARD VANE ACTUATOR ROD HAS INDENT. (C-CHECK RO 11/01/2025)REMOVED DAMAGE FROM RH INBOARD FLAP, SECOND TO INBOARD VANE ACTUATOR ROD, REF, CRJ-900, SRM 51-12-00-001-001-A01, AND PERFORMED REPAIRS PER REO 670-57-52-257 REV -B DATED
- [SDR SWI2025F01499](https://openairdocs.org/sdr/SWI2025F01499.md): Rod · dented · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBOARD FLAP, OUTBOARD VANE ACTUATOR ROD HAS INDENT. (C-CHECK RO 11/01/2025) REMOVED INDENT ON RH INBOARD FLAP, OUTBOARD VANE ACTUATOR ROD IAW CRJ900 SRM 51-12-00-001-001-A01 AND PERFORMED REPAIR PER REO 670-57-52-257 REV B DATED 2024-10-17. ALL CHECKS GO
- [SDR SWI2025F01498](https://openairdocs.org/sdr/SWI2025F01498.md): Slat Track · damaged · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-2 PITTED ON CONTACT SURFACE AS MARKED (C-CHECK RO 11/01/2025)REMOVED DAMAGE ON LEFT WING SLAT TRACK 1-2 ON CONTACT SURFACE REF CRJ900 SRM 51-21-06-001-001-A01, COMPLIED WITH REO 690-57-42-1265 REV -- DATED 2025-07-22 STEPS 1-7.OPS TEST
- [SDR SWIA202511030701](https://openairdocs.org/sdr/SWIA202511030701.md): Bracket · corroded · Jul 1, 2025 · N803SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > RIGHT MAIN LANDING GEAR WHEEL WELL, TIRE BURST COVER MOUNTING "L" BRACKET IS CORRODED. HN00250973 (C-CHECK RO 11/01/2025)MLG ELECTRICAL/HYDRAULIC PROTECTIVE COVER ANGLE P/N CC670-10338-1 ON THE R/H WING'S REAR SPAR HAS MULTIPLE AREAS OF PITTING ACROSS TH
- [SDR SWI2025F01503](https://openairdocs.org/sdr/SWI2025F01503.md): Skin · damaged · Jun 28, 2025 · N803SK · Cndair CL6002D24 · Trailing Edge Flaps
  > S/N 0153LH OUTBD FLAP, BACKSIDE/TOP HAS SMOKING RIVETS. CIRCLED WITH GREASE PENCIL. (C-CHECK RO 11/01/2025)REPLACED SMOKING RIVETS ON LH OUTBD FLAP, BACKSIDE/TOP IAW REO#690-57-53-183, REV --, DATE: 2025-07-30. COMPLIED WITH TASK CARD 51-900-1002-SKY AND M-33
- [SDR SWI2025F01502](https://openairdocs.org/sdr/SWI2025F01502.md): Drag Angle · cracked · Jun 28, 2025 · N803SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)PERFORMED SRM REPAIR TO CRACKED RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01501](https://openairdocs.org/sdr/SWI2025F01501.md): Drag Angle · cracked · Jun 28, 2025 · N803SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED REPAIR ANGLES ON LH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. REF. CRJ900 SRM 55-31-00-201-001-A01 REV 38 JUL 25/2020. COMPLIED WITH 51-900-1002-SKY.

Next page: https://openairdocs.org/aircraft/N803SK/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 = 'N803SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N803SK/reports

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