# Service difficulty reports: N800SK

A list on [N800SK](https://openairdocs.org/aircraft/N800SK.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 7 · 325 reports

- [SDR SWIA2026061476221](https://openairdocs.org/sdr/SWIA2026061476221.md): Hydraulic Line · leaking · Jun 14, 2026 · N800SK · Cndair CL6002D24 · Hydraulic System, Main
  > HYD 1 LOW PRESS CAUTION AT CRUISE. QUANTITY 0 PERCENT PRESSURE 2700, 18 DEGREES C. RAN QRH THEN HAD HYD EDP 1A CAUTION MESSAGE AND RAN QRH, NO CHANGE. (FLIGHT 4024) FOUND PINHOLE IN HYD SYS NR 1 RETURN LINE IN MAIN LANDING GEAR NR1 WHEEL BIN. REPAIRED HYDRAU
- [SDR SWIA2025070100623](https://openairdocs.org/sdr/SWIA2025070100623.md): Buttstrap · damaged · Jun 23, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Structure
  > REPAIR FS 280 LOWER BUTT-STRAP BETWEEN STR25L (C-CHECK RO 06/29/2025)PERFORMED REPAIR FS 280 LOWER BUTT-STRAP BETWEEN STR25L BY COMPLYING WITH REO 690-53-21-1936 REV-- DATED 2025-06-27, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK PASSED
- [SDR SWI2025F00772](https://openairdocs.org/sdr/SWI2025F00772.md): Skin · chafed · Apr 29, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE EXTERNAL LOWER SKIN PANEL CHAFED BETWEEN FS897 AND FS913 STR27 (MARKED). 30056481 (C-CHECK RO 06/29/2025)REPAIRED AFT FUSELAGE EXTERNAL LOWER SKIN PANEL CHAFED BETWEEN FS897 AND FS913 STR27 PER REO 690-53-51-467 REV-- DATE 2025-05-20. SEE CONTINU
- [SDR SWIA2025070100429](https://openairdocs.org/sdr/SWIA2025070100429.md): Skin · damaged · Apr 29, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE BURN MARK ON THE SKIN BETWEEN FS661+16 AND FS661+32 BETWEEN STR 18R AND 19R. REPAIRED LIGHTNING STRIKE AT FUSELAGE SKIN BETWEEN FS661+16 AND FS661+32 BETWEEN STR 18R AND 19R. REMOVING ALL DAMAGE REF CRJ900 SRM 53-00-00-201-003-A03 AND CRJ90
- [SDR SWIA2025070100425](https://openairdocs.org/sdr/SWIA2025070100425.md): Hinge · gouged · Apr 25, 2025 · N800SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > MULTIPLE GOUGES ON THE PASSENGER DOOR PIANO HINGE(DOOR SIDE). CAMP # 30038062. (C-CHECK RO 06/29/2025)INSPECTED PASSENGER DOOR PIANO HINGE FOR MULTIPLE GOUGES. REMAINING THICKNESS OF LUG #1 IS 0.109", REMAINING THICKNESS OF LUG #2 IS 0.113", REMAINING THICKN
- [SDR SWIA2025070100415](https://openairdocs.org/sdr/SWIA2025070100415.md): Skin · corroded · Apr 15, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL SKIN BETWEEN FS1031 - FS1051 STR26R - STR26L ( 29979184) (C-CHECK RO 06/29/2025)REPAIRED CORROSION ON EXTERNAL SKIN BETWEEN FS1031- FS1051, STR 26L REF REO 690-53-61-1558, REV:--, DATED 2025-04-21 AND CRJ900 SRM 51-21-06-001-001-A01, SE
- [SDR SWIA2025070200414](https://openairdocs.org/sdr/SWIA2025070200414.md): Roller · worn · Apr 14, 2025 · N800SK · Cndair CL6002D24 · Leading Edge Devices
  > LH SLAT TRACK 3-3 UPPER OUTBOARD AFT ROLLER WORN. REMOVED AND REPLACED LH SLAT TRACK 3-3 TOP OUTBOARD AFT ROLLER REF AMM 27-81-43-000-806-A01 AND 27-81-43-400-806-A01.
- [SDR SWI2025F00774](https://openairdocs.org/sdr/SWI2025F00774.md): Beam · damaged · Apr 9, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge Flaps
  > LH INBOARD FLAP FLS 140.40 VANE ACTUATOR BEAM HAS ROLLER INDENTIONS (C-CHECK RO 06/29/2025)LH INBOARD FLAP FLS 140.40 VANE ACTUATOR BEAM PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. OPERATIONAL TEST PASSED. COMPLIED WITH M-337 AND
- [SDR SWI2025F00773](https://openairdocs.org/sdr/SWI2025F00773.md): Frame · corroded · Apr 9, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON REINFORCING ANGLE OF FRAME FS549.00 BETWEEN STGR 17L AND 18L. (29947227). (C-CHECK RO 06/29/2025)REMOVED AND REPLACED CLEAT PN: SH670-33796-1 AT FS549 BETWEEN STGR 17 AND STGR 18 PER CRJ 900 SRMS 51-42-06-001-001-A01 AND 51-42-22-001-001-A0
- [SDR SWIA2025070100409](https://openairdocs.org/sdr/SWIA2025070100409.md): Roller · damaged · Apr 9, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge Flaps
  > LH INBOARD FLAP FLS 24.0 VANE ACTUATOR BEAM HAS ROLLER INDENTIONS (C-CHECK RO 06/29/2025)LH INBOARD FLAP FLS 24.0 VANE ACTUATOR BEAM REPAIRED PER REO 670-57-52-257 REV -A DATED 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 AND TASK CARD 51-900-10
- [SDR SWI2025F00785](https://openairdocs.org/sdr/SWI2025F00785.md): Rod · damaged · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 102.90. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR ROD AT APPROX FLS 102.90. REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. OPERATIONAL TEST PASSED. COMPLIED WITH
- [SDR SWI2025F00784](https://openairdocs.org/sdr/SWI2025F00784.md): Fitting · chafed · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Emergency Exits
  > RH FWD EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS CHAFFED. CAMP # 29942099. (C-CHECK RO 06/29/2025)PERFORMED BLEND OUT REPAIR ON RH FWD EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS. REF. REO 690-52-21-192 REV.-- DATED 2025-04-21. COMPLIED WITH TASK CARD
- [SDR SWI2025F00783](https://openairdocs.org/sdr/SWI2025F00783.md): Rod · grooved · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 140.40. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR AT APPROX FLS 140.40 REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 AND TASK CA
- [SDR SWI2025F00782](https://openairdocs.org/sdr/SWI2025F00782.md): Rod · damaged · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBD FLAP VANE ACTUATOR AT APPROX FLS 24.00 HAS A GROOVE ON THE ACTUATOR ROD. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR AT APPROX FLS 24.00 REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 AN
- [SDR SWI2025F00781](https://openairdocs.org/sdr/SWI2025F00781.md): Frame · corroded · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME FS533.00 BETWEEN STGR 17L AND 18L WEB PORTION AND ATTACHING FLANGE. (29941771) (C-CHECK RO 06/29/2025)PERFORMED SPLICE REPAIR ON FRAME FS533.00 BETWEEN STGR 17L AND 18L. REF CRJ-900 SRM 53-00-06-201-001-A03, CRJ-900 SRM 51-42-06-001-
- [SDR SWI2025F00780](https://openairdocs.org/sdr/SWI2025F00780.md): Rod · grooved · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 65.50. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR ROD AT APPROX FLS 65.50 REPAIRED PER REO 670-57-52-257 REV-A DATE 2024-08-20. WITHIN LIMITS. OPERATIONAL TEST PASSED. COMPLIED WITH M-337
- [SDR SWI2025F00779](https://openairdocs.org/sdr/SWI2025F00779.md): Angle · corroded · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ANGLE FOR LH TIRE BURST PANEL 542AZ IS CORRODED. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED LH TIRE BURST PANEL 542AZ ANGLE REF CRJ900 SRM 51-42-21-001-001-A01 REVISION 38,DATED JULY 25/2020 AND DWG CC670-10320 REV FCOMPLIED WITH SKYWEST TASK CARD 51-900-100
- [SDR SWI2025F00778](https://openairdocs.org/sdr/SWI2025F00778.md): Fitting · chafed · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Emergency Exits
  > RIGHT AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS CHAFFED. PERFORMED BLEND OUT REPAIR ON RH AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS. REF. REO 690-52-21-193 REV.-- ISSUED 2025-04-21.COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F00777](https://openairdocs.org/sdr/SWI2025F00777.md): Fitting · chafed · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Emergency Exits
  > LH AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS CHAFFED. CAMP # 29942073. (C-CHECK RO 06/29/2025)PERFORMED BLEND OUT REPAIR ON LH AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS. REF REO 690-52-21-194 REV -- DATED 2025-04-21. COMPLIED WITH TASK CARD 51
- [SDR SWI2025F00776](https://openairdocs.org/sdr/SWI2025F00776.md): Angle · corroded · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ANGLE FOR RH TIRE BURST PANEL 642AZ IS CORRODED. REMOVED AND REPLACED RH TIRE BURST PANEL 642AZ ANGLE REF CRJ 200 SRM 51-42-21-001-001-A01 AND DWG CC670-10320 REV. F. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWI2025F00775](https://openairdocs.org/sdr/SWI2025F00775.md): Repair · cracked · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK IN THE RADIUS OF THE REPAIR DOUBLER ON THE TRU BAY FLOOR, RIGHT SIDE UNDER THE ADG PUMP, AT FS193.00 FRAME INBOARD AFT CORNER. REPLACED THE REPAIR DOUBLER ON THE RIGHT TRU BAY FLOOR. REF REO 670-53-11-509 REV-E DATE 2018-02-08.
- [SDR SWIA2025070100408](https://openairdocs.org/sdr/SWIA2025070100408.md): Track · damaged · Apr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RH INBD FLAP HAS GROOVES ON THE VANE ACTUATOR CAM TRACKS AT APPROX FLS 102.90. REPAIRED RH INBD FLAP ON THE VANE ACTUATOR CAM TRACKS AT APPROX FLS 102.90 BY COMPLYING WITH ALL STEPS OF REO 670-57-52-259 REV -.
- [SDR SWIA2025070100407](https://openairdocs.org/sdr/SWIA2025070100407.md): Frame · corroded · Apr 7, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME IN MULTIPLE LOCATIONS AT FS613 BETWEEN STGR 26L AND STGR 26R. (C-CHECK RO 06/29/2025)PERFORMED FRAME FLANGE SPLICE REPAIR ON FS613 BETWEEN STRG27 AND STRG26R REF CRJ900 SRM 53-00-06-201-001-A03 AND CRJ-900 SRM 51-42-06-001-001-A01. COMPLIE
- [SDR SWI2025F00790](https://openairdocs.org/sdr/SWI2025F00790.md): Frame · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS613 BETWEEN STGR 18L AND STGR 19L. (MARKED) (C-CHECK RO 06/29/2025)REMOVED CORRODED FRAME AT FS613- BETWEEN STGR18L AND STGR19L REF CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 INSTALLED NEW FRAME AT FS613- BETWEEN STGR
- [SDR SWI2025F00789](https://openairdocs.org/sdr/SWI2025F00789.md): Frame Angle · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME ANGLE AT APPROX FS645 STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)REMOVED AND REPLACED FRAME ANGLE/CLEAT PN SH670-33796-1 AT FS 645.00 STGR 18L PER CRJ900 SRMS 51-42-06-001-001-A01 AND 51-42-22-001-001-A01 USING DWG NO SH690-33750 REV AF. CO
- [SDR SWI2025F00788](https://openairdocs.org/sdr/SWI2025F00788.md): Frame · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS661+32 BETWEEN STGR 18L AND STGR 19L. (MARKED) (C-CHECK RO 06/29/2025)REMOVED DAMAGE STUB FRAME AND INSTALLED NEW STUB FRAME AT FS661+32 BETWEEN STR 18L AND STR19L REF DWG# SH690-33750 REV: AF AND CRJ900 SRM 51-42-06-001-001-A01; 51-42
- [SDR SWI2025F00787](https://openairdocs.org/sdr/SWI2025F00787.md): Stringer · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 26R ATTACH FLANGE BETWEEN FS1015 €“ 1031 (C-CHECK RO 06/29/2025)REPAIRED CORROSION DAMAGE ON STR 26R ATTACH FLANGE BETWEEN FS1015 AND FS1031 BY COMPLETING ALL STEPS (1-13) OF REO 690-53-61-1555, REV --, DATED 2025-05-01. LEAK CHECK GOOD. SE
- [SDR SWI2025F00786](https://openairdocs.org/sdr/SWI2025F00786.md): Frame Angle · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME ANGLE AT APPROX FS613 STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)PERFORMED FRAME SPLICE REPAIR PERCRJ900 SRM 53-00-06-201-001-A03, CRJ900 SRM 51-42-06-001-001-A01AND CRJ900 SRM 51-42-21-001-001-A01. SEE CONTINUE CARD FOR DETAILS. COMPLIED W
- [SDR SWI2025F00799](https://openairdocs.org/sdr/SWI2025F00799.md): Door Sill · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Structure
  > SERVICE DOOR SILL BOTTOM ANGLE HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED MOUNTING ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND DRAWING# SH670-31950, REV Y. AND REMOVED AND REPLACED 4 EA WEB FLOOR PROTECTORS ON SERVICE
- [SDR SWI2025F00798](https://openairdocs.org/sdr/SWI2025F00798.md): Frame · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS645 BETWEEN STGR 17L AND STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)REPLACED FRAME SECTION FS645 STGR16L-18L REF CRJ 900 SRM 53-00-06-201-001-A03 AND CRJ900 SRM 51-42-06-001-001-A01.SEE CONTINUE CARD FOR WORK PERFORMED. COMPLIED WITH
- [SDR SWI2025F00797](https://openairdocs.org/sdr/SWI2025F00797.md): Frame · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS501 BETWEEN STGR 27 AND STGR 26L. (C-CHECK RO 06/29/2025)BLENDED OUT CORROSION ON FRAME FS501 BETWEEN STGR 27 AND 26L. FOUND WITHIN LIMITS. REF. REO 690-53-31-959 REV.-- ISSUED 2025-04-18.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SK
- [SDR SWI2025F00796](https://openairdocs.org/sdr/SWI2025F00796.md): Plate · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD CARGO FWD H-PLATE ON OPEINING SILL HAS CORROSION AT APPROX FS517 STGR 24L.(MARKED) (C-CHECK RO 06/29/2025)BLENDED CORRODED AREA ON FWD CARGO FWD H-PLATE FS517 STGR 24L. REF CRJ-900 SRM 51-21-06-001-001-A01. COMPLIED WITH REO 690-53-31-960 REV -- DATE: 2
- [SDR SWI2025F00795](https://openairdocs.org/sdr/SWI2025F00795.md): Floorbeam · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AVIONICS BAY FLOOR SUPPORT ANGLE AT FS.280.00 CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 06/29/2025)REMOVED AND REPLACED WITH NEW AVIONICS BAY FLOOR SUPPORT ANGLE AT FS280.00 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND DW
- [SDR SWI2025F00794](https://openairdocs.org/sdr/SWI2025F00794.md): Floor Support · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL IS CORRODED FS280 €“ 319 (C-CHECK RO 06/29/2025)REPAIRED RH FLOOR SILL CORROSION AT FS280-FS319 REF CRJ 900 SRM TASK 51-40-06-001-001-A01, CRJ 900 SRM TASK 51-42-21-001-001-A01, CRJ 900 SRM TASK 51-42-06-001-001-A01, CRJ 900 SRM TASK 51-42-1
- [SDR SWI2025F00793](https://openairdocs.org/sdr/SWI2025F00793.md): Floorbeam · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LBL9 FLOOR BEAM IS CORRODED FS1031 (C-CHECK RO 06/29/2025)REPAIRED FLOOR BEAM NEW SECTION AT LBL 9.0 BETWEEN F/S 1025 TO F/S 1037 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND CRJ 900 SRM 51-42-21-001-001-A01.COMPLIED WITH 51-900-1002-SKY.
- [SDR SWI2025F00792](https://openairdocs.org/sdr/SWI2025F00792.md): Frame Angle · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME ANGLE AT APPROX FS581 STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)PERFORMED FRAME SPLICE REPAIR REF CRJ900 SRM 53-00-06-201-001-A03, CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND BOMBARDIER DRAWING SH690-33100, REV N.
- [SDR SWI2025F00791](https://openairdocs.org/sdr/SWI2025F00791.md): Frame · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS581 BETWEEN STGR 27 AND STGR 26R. (C-CHECK RO 06/29/2025)REPAIRED CORROSION ON FRAME AT FS581 BETWEEN STGR 27 AND STGR 26R. CRJ900 SRM 53-00-06-201-001-A03 AND 51-42-06-001-001-A01. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CAR
- [SDR SWIA20250701406](https://openairdocs.org/sdr/SWIA20250701406.md): Stringer · corroded · Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 24R IN MULTIPLE LOCATIONS BETWEEN FS581 AND FS597. PERFORMED STRINGER SPLICE REPAIR AND INSTALLED ALL REPAIR PARTS AT STGR 24R BETWEEN FS565 AND FS661+32. REF. CRJ900 SRM 53-00-03-201-001-A02 FIGURE 53-00-03-995-806 SHEET 1, REO 690-53-31-95
- [SDR SWI2025F00806](https://openairdocs.org/sdr/SWI2025F00806.md): Floorbeam · cracked · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RBL12 FS280 CLIP IS CRACKED (C-CHECK RO 06/29/2025)REMOVED AND REPLACED CLIP P/N CC670-34099-2 AT RBL 12 FS,280 REF. CRJ900 SRM 51-42-21-001-001-A01 AND DWG# KBA670-30026 REV. J SHT 7. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2D24) STRUCTURAL M
- [SDR SWI2025F00805](https://openairdocs.org/sdr/SWI2025F00805.md): Floorbeam · corroded · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR BOARD SUPPORT ANGLE ON THE FWD SIDE OF FS280 IS CORRODED (C-CHECK RO 06/29/2025)FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED COCKPIT FLOOR BOARD SUPPORT ANGLE ON THE FWD SIDE OF FS280 REF DWG CC670-33052 REV G, CRJ900 SRM 51-42-21-001-001-A01
- [SDR SWI2025F00804](https://openairdocs.org/sdr/SWI2025F00804.md): Door Sill · corroded · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Structure
  > PAX DOOR LOWER SILL LOWER ANGLE HAS CORROSION IN MULITPLE LOCATIONS. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED NEW PAX DOOR LOWER SILL LOWER ANGLE REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG# SH670-31810 REV AE. LEAK CHECK GOOD. ( SEE CONTINUE CARD FOR WO
- [SDR SWI2025F00803](https://openairdocs.org/sdr/SWI2025F00803.md): Striker · chafed · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR SEAL STRIKER IS CHAFED AT FS310 APPROX STGR 9L. (C-CHECK RO 06/29/2025)REPAIRED PAX DOOR STRIKER REF CRJ 900 SRM 53-21-23-201-006-A01. SEE CONTINUE CARD FOR DETAILS.COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWI2025F00802](https://openairdocs.org/sdr/SWI2025F00802.md): Floorbeam · cracked · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LBL12 FS280 CLIP IS CRACKED (C-CHECK RO 06/29/2025)REMOVED AND REPLACED CLIP P/N CC670-34099-1 REF CRJ 900 SRM 51-42-21-001-001-A01 WITH DRAWING BA670-31057 REV -L FOR FASTENER CALL-OUT. COMPLIED WITH TASK CARD 51-900-1002-SKY, SEE CONTINUE CARD FOR WORK DET
- [SDR SWI2025F00801](https://openairdocs.org/sdr/SWI2025F00801.md): Striker · corroded · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Service Doors
  > SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AROUND MULTIPLE FASTENER HOLES. REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SEAL STRIKER REF CRJ900 SRM 51-42-06-001-001-A01, AND DRAWING SH670-31950, REV Y. LEAK CHECK GOOD. SEE CONTINUE CARD FOR MORE DETAIL
- [SDR SWI2025F00800](https://openairdocs.org/sdr/SWI2025F00800.md): Fitting · chafed · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD AND AFT CAM FITTINGS ON FUSELAGE SIDE ARE CHAFED. CHAFES FOUND TO BE OUT OF LIMITS REF RJ 900 SRM 53-21-23-101-001-A02. INSTALLED NEW FWD AND AFT PAX DOOR CAM FITTINGS ON FUSELAGE SIDE IAW CRJ900 SRM 53-21-27-001-001-A01 AND CRJ900 SRM 51-42-21-
- [SDR SWIA2025070100405](https://openairdocs.org/sdr/SWIA2025070100405.md): Door Frame · gouged · Apr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Structure
  > 4EA GOUGES ON UPPER PAX DOOR SURROUND AT APPROX STGR 4L BEHIND NUTPLATE BRACKETS. COMPLETED REO 690-53-21-1925 REV.--, DATED 2025-04-21 FOR GOUGE DAMAGE TO UPPER LINTEL DOUBLER ABOVE PAX DOOR BETWEEN FS333.00-FS337.50 AT STR 3L. (#3 DOUBLER BLEND). ENSURED G
- [SDR SWI2025F00811](https://openairdocs.org/sdr/SWI2025F00811.md): Bracket · cracked · Apr 4, 2025 · N800SK · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED (C-CHECK RO 06/29/2025)REMOVED AND INSTALLED NEW L/H LWR TRANSCOWL O/B BRACKET REF REO# 670-54-21-971, REV B, DATED 11/28/23 AND CRJ900 AMM 78-33-03-400-801-A01. OPS CHECK GOOD AT THIS TIME. SEE CONTINUE CARD FOR
- [SDR SWIA2025070100404](https://openairdocs.org/sdr/SWIA2025070100404.md): Transcowl · sheared · Apr 4, 2025 · N800SK · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE SHEARED. REPAIRED LEFT UPPER TRANSCOWL AT SHEARED RIVETS ON INNER SKIN COMMON TO ZED STIFFENER, REF. REO 690-54-21-552, REV. --, COMPLIED WITH MAJOR REPAIR M-337, SKY CARD 51-900-1002-SKY.
- [SDR SWI2025F00810](https://openairdocs.org/sdr/SWI2025F00810.md): Structure · corroded · Apr 3, 2025 · N800SK · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > S/N 0462BETWEEN FS1069.75 AND FS1088.20 INTERNAL OF LH PYLON (LUNCH BOX), THEIRS A FUEL LINE THAT LEAKED AND AREA HAS CORROSION. FLAGGED (C-CHECK RO 06/29/2025)REMOVED CORROSION BETWEEN FS1069.75 AND FS1088.20 INTERNAL OF LH PYLON (LUNCH BOX) PER CRJ900 SRM
- [SDR SWI2025F00809](https://openairdocs.org/sdr/SWI2025F00809.md): Receiver · cracked · Apr 3, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Structure
  > S/N 0444EXTERNAL INSPECTION OF THE RH AFT FUSELAGE TRU BAY LATCH RECEIVER HAS A POSSIBLE CRACK. FLAGGED (C-CHECK RO 06/29/2025)REMOVED AND REPLACED RH TRU LATCH RECEIVER (LANDING PN CC670-33151-6) PER DWG CC670-33040 REV-G, CRJ 900 SRM 51-42-06-001-001-A01 RE

Next page: https://openairdocs.org/aircraft/N800SK/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 = 'N800SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N800SK/reports

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