# Service difficulty reports: N758SK

A list on [N758SK](https://openairdocs.org/aircraft/N758SK.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 5 · 215 reports

- [SDR SWIA2026081276841](https://openairdocs.org/sdr/SWIA2026081276841.md): Aoa · faulted · Aug 12, 2026 · N758SK · Cndair CL6002C10 · Stall Warning System
  > IMMEDIATELY AFTER TAKEOFF GOT A STICK SHAKER WITH CONTINUOUS IGNITION WITH STALL LIGHT FLASHING. FOS SIDE AIRSPEED TAPE HAD RED BARBER POLE FROM BOTTOM HIGHER THAN NORMAL. ALSO GOT AUDIO WARBLER. NEVER GOT STICK PUSHER. DURING FLIGHT HIGH AIRSPEED BARBER P
- [SDR SWIA2026072576676](https://openairdocs.org/sdr/SWIA2026072576676.md): Motor · faulted · Jul 25, 2026 · N758SK · Cndair CL6002C10 · Stabilizer Position Indicating
  > DURING CRUISE AT F360/M.77, STAB TRIM RUNAWAY AURAL SOUNDED WITH ASSOCIATED STAB CH1 INOP STATUS MSG. COMPLIED WITH IMMEDIATE ACTION ITEMS. WITH THE AUTOPILOT & TRIM DISENGAGED, ACFT SLIGHTLY OUT OF TRIM NOSE DOWN AT 2.3. EXITED RVSM AIRSPACE & ACFT FELT TRIMM
- [SDR SWIA2025122400003](https://openairdocs.org/sdr/SWIA2025122400003.md): Window · cracked · Dec 23, 2025 · N758SK · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAINS SIDE WINDOW SHATTERED AT FL370. NO PRESSURE ISSUES. CREW COMPLIED WITH QRH (FLIGHT 6355) R & R CA SIDE WINDOW IAW SKYWEST TASK CARD 56-20-1000-SKY, OPS AND LEAK CHECK GOOD.
- [SDR SWIA2025102000019](https://openairdocs.org/sdr/SWIA2025102000019.md): Ballast · failed · Oct 19, 2025 · N758SK · Cndair CL6002C10 · Lighting System
  > ON DECENT PASSENGERS MENTIONED A BURNT ORDER. CONFIRMED BY THE FLIGHT ATTENDANT. PASSENGERS IN ROW 16 COMPLAINED THAT THE FLOOR WAS €ŒREALLY HOT€? AT THE SAME TIME. AFTER DEPLANING THE SMELL REMAINED. (FLIGHT 6468) APON ARRIVAL TO ACFT COULD SMELL A SLIGHT
- [SDR SWIA202503030002](https://openairdocs.org/sdr/SWIA202503030002.md): Landing Gear · warning message · Mar 2, 2025 · N758SK · Cndair CL6002C10 · Landing Gear Position and Warning
  > *REPEAT ODI EVENT SMOD APPROVAL REQUIRED* *CAT II DOWNGRADED*D:AFTER TAKEOFF GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH AND RETURNED FOR NORMAL LANDING. B1-007427, 007432, 007451, 065387, 065386C:MEL 32-30-1CAT "A" DUE 1 FLIGHT DAY.MX ACTIONS COMPLIED W
- [SDR SWIA202502240003](https://openairdocs.org/sdr/SWIA202502240003.md): Landing Gear · warning message · Feb 23, 2025 · N758SK · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > FLIGHT CREW REPORTS GEAR DISAGREE WARNING ED1 DURING DEPARTURE AFTER GEAR RETRACTION. NO OVERWEIGHT NO HARD LANDING QRH COMPLETED. (FLIGHT 6400 - FILED CLOSED) UPON ARRIVAL TO AIRCRAFT, TALKED TO THE CREW AND THEY SAID THAT THE NLG WHEN RETRACTING TURNE
- [SDR SWIA202408230627](https://openairdocs.org/sdr/SWIA202408230627.md): Hinge · misinstalled · Jun 27, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > LOW EDGE DISTANCE FOUND ON BOTH OF NLG HINGE FITTING DURING INCORPORATING OF THE SB 670BA-32-056 ON CAMP 28136144 BARCODE ID HR00423694. (CAMP 28136144) (C-CHECK RO 8/22/2024) PREPARED HOLES PER SRM 51-42-21 FOR INSTALLATION OF REQUIRED HI-LITE (HST110A
- [SDR SWIA2024082300622](https://openairdocs.org/sdr/SWIA2024082300622.md): Door Sill · corroded · Jun 22, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR STRIKER SILL HAS MULTIPLE SPOTS OF CORROSION NEAR FASTENER HOLES (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW SERVICE DOOR STRIKER SILL REF DWG. SH670-31950 REV Y., REF CRJ700 SRM 51-42-06-001-001-A01.LEAK CHECK GOODCOMPLIED WITH TASK
- [SDR SWIA2024082300621](https://openairdocs.org/sdr/SWIA2024082300621.md): Door Sill · corroded · Jun 21, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE HAVE MULTIPLE SPOTS OF CORROSION. (C-CHECK RO 8/22/2024) REPLACED SERVICE DOOR LOWER SILL ANGLE REF DRW. SH670-31950 REV Y, REF CRJ700 SRM 51-42-06-001-001-A01, AND REF CRJ700 SRM 51-42-21- 001-001-A01. SEE CONTINUE CARD FO
- [SDR SWI202408230735](https://openairdocs.org/sdr/SWI202408230735.md): Floor Support · cracked · Jun 20, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT LBL 12 FS 250.00 - FS 280.00 CRACKED #28412625 (C-CHECK RO 8/22/2024) REMOVED AND INSTALL NEW SERVICEABLE FLOOR SUPPORT AT LBL12 FS250-280 REF CRJ 700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND DWG CC670-33052 REV -G. COMPLIED WITH
- [SDR SWIA2024082300620](https://openairdocs.org/sdr/SWIA2024082300620.md): Floor Support · cracked · Jun 20, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT PANEL AT RBL 12 BETWEEN FS 250.00 - FS 280.00 MX#28412643 (C-CHECK RO 8/22/2024) REMOVED AND REPLACED THE ANGLE FLOOR SUPPORT AT RBL12 BETWEEN FS250.00 AND FS280.00 REF CRJ 700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND BOMBA
- [SDR SWIA2024082300619](https://openairdocs.org/sdr/SWIA2024082300619.md): Retainer · bent · Jun 19, 2024 · N758SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CENTER SEAL RETAINER IS BENT (BOTTOM SIDE) MX#28409942 (C-CHECK RO 8/22/2024) INSTALLED NEW PAX DOOR CENTER SEAL RETAINER REF CRJ700 SRM 51-42-13-001-001-A01, DWG NO 601R31871 REV -D AND REO 670-52-11-022 REV C DATED 2013-02-01. SEE CAMP MX#283
- [SDR SWI202408230729](https://openairdocs.org/sdr/SWI202408230729.md): Drag Angle · cracked · Jun 17, 2024 · N758SK · Cndair CL6002C10 · Vertical Stabilizer
  > VERTICAL STABILIZER RH AFT DRAG ANGLE AT STABILIZER ROOT HAVE SMOKING RIVETS AND POSSIBLE CRACKS (C-CHECK RO 8/22/2024) COMPLIED WITH VERTICAL STAB RH AFT DRAG ANGLE REPAIR REF CRJ700 SRM 55-31-00-201-001-A01COMPLIED WITH TASK 51-900-1002-SKY
- [SDR SWI202408230728](https://openairdocs.org/sdr/SWI202408230728.md): Drag Angle · cracked · Jun 17, 2024 · N758SK · Cndair CL6002C10 · Vertical Stabilizer
  > VERTICAL STABILIZER RH FWD DRAG ANGLE AT STABILIZER ROOT HAVE SMOKING RIVETS AND POSSIBLE CRACKS (C-CHECK RO 8/22/2024) VERTICAL STABILIZER R/H FWD DRAG ANGLE REPAIRED REF. CRJ-700 SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-10
- [SDR SWIA202408230612](https://openairdocs.org/sdr/SWIA202408230612.md): Floorbeam · cracked · Jun 12, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CENTER COCKPIT FLOOR BEAM AT LBL12 IS CRACKED (C-CHECK RO 8/22/2024) REMOVED DAMAGED SECTION AND FABRICATED AND INSTALLED CENTER COCKPIT FLOOR BEAM, LBL12 BETWEEN FS250 - FS280 REF CRJ700 SRM 53-11-43-201-003-A01 REPAIR TYPE IVCOMPLIED WITH SKYWEST TASK
- [SDR SWI202408230738](https://openairdocs.org/sdr/SWI202408230738.md): Skin · scratched · Jun 11, 2024 · N758SK · Cndair CL6002C10 · Leading Edge Devices
  > LH OUTBOARD SLAT LEADING EDGE SCRATCHED IN 2 LOCATIONS AT OUTBOARD SIDE WHEN MOVING POWER LIFT (C-CHECK RO 8/22/2024) BLENDED OUT DAMAGE FROM LH #3 SLAT OUTER SKIN REF CRJ700 SRM 51-12-00-001-001-A01 AND REPAIRED LH #3 SLAT OUTER SKIN DAMAGE BY COMPLYIN
- [SDR SWIA202408230611](https://openairdocs.org/sdr/SWIA202408230611.md): Skin · damaged · Jun 11, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TOOL MARKS ON EXTERNAL TOP SKIN COVERED BY MID AND FWD DORSAL STRAKE FAIRINGS BETWEEN APROX. FS.939.00 TO FS.1000.00 (C-CHECK RO 8/22/2024) REMOVED DAMAGED FROM EXTERNAL TOP SKIN UNDER THE MID AND FWD DORSAL STRAKE FAIRINGS BETWEEN FS939 - 1000 REF REO
- [SDR SWIA202408230610](https://openairdocs.org/sdr/SWIA202408230610.md): Hinge · gouged · Jun 10, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE (AIRCRAFT SIDE) FOUND GOUGE ON LANDING AFT OF LUG 27 (C-CHECK RO 8/22/2024) GOUGE ON PAX DOOR PIANO HINGE (AIRCRAFT FUSELAGE SIDE) ON LANDING AFT OF LUG 27, BLENDED IAW CRJ 700 SRM 53-21-23-201-010-A01 REPAIR TYPE LV(4).BLENDED AREA
- [SDR SWIA202408230609](https://openairdocs.org/sdr/SWIA202408230609.md): Structure · corroded · Jun 9, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON INTERNAL STRUCTURE BETWEEN FS394.00 AND FS409.00 ON STGR21L (AS MARKED) CAMP# 28360070 (C-CHECK RO 8/22/2024) INSTALLED NEW STGR 21L BETWEEN STA FS364-379 AND FS394-409 REF CRJ700 REO 670-53-21-2431, REV --, DATED 2024-07-15,SRM 51-42-06-0
- [SDR SWI202408230734](https://openairdocs.org/sdr/SWI202408230734.md): Stringer · corroded · Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION AT APPROXIMATELY FS285.00 ON STGR25R AS MARKED (C-CHECK RO 8/22/2024) INSTALLED NEW FS295 FRAME SPLICE SECTION BETWEEN STGR 26R AND STGR 25R. REPAIRED. IAW ALL STEPS OF REO 670-53-21-2430 REV:--. DATE:2024-07-01 AND CRJ700 SRM 51-42-21-001-00
- [SDR SWI202408230733](https://openairdocs.org/sdr/SWI202408230733.md): Joint · corroded · Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS CORROSION AS MARKED BETWEEN APPROXIMATELY STGR21R AND STGR22R (C-CHECK RO 8/22/2024) BLENDED CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-53-21-2434
- [SDR SWI202408230732](https://openairdocs.org/sdr/SWI202408230732.md): Joint · corroded · Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS CORROSION AS MARKED BETWEEN APPROXIMATELY STGR20R AND STGR21R (C-CHECK RO 8/22/2024) BLENDED AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-53-21-2434 REV -- DATE 2024-07-04. AND COMPLIED WITH ALL
- [SDR SWI2024082300731](https://openairdocs.org/sdr/SWI2024082300731.md): Crossbeam · corroded · Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FS280 R/H CROSSBEAM BETWEEN BL 0 AND RBL 9 HAS CORROSION (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW RH CROSSBEAM AT FS 280.00 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 REV. 38 JUL 25
- [SDR SWI2024082300730](https://openairdocs.org/sdr/SWI2024082300730.md): Joint · corroded · Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS CORROSION AS MARKED BETWEEN APPROXIMATELY STGR24L AND STGR25L (C-CHECK RO 8/22/2024) BLENDED CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-53-21-2434
- [SDR SWIA2024082300608](https://openairdocs.org/sdr/SWIA2024082300608.md): Floorbeam · corroded · Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 L/H CROSSBEAM BETWEEN BL 0 AND LBL 9 HAS CORROSION (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW LH CROSSBEAM AT FS 280.00 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 REV. 38 JUL 25
- [SDR SWI2024F00727](https://openairdocs.org/sdr/SWI2024F00727.md): Floorbeam · corroded · Jun 7, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFT FUSELAGE T CAP CORRODED IN MULTIPLE LOCATIONS ON LBL27 BETWEEN APPROXIMATELY F1005.00 AND FS1040.00 AS MARKED (C-CHECK RO 8/22/2024) REMOVED CORROSION FROM FLOOR SUPPORT BEAM (T CAP) AT RBL27 BETWEEN APPROX FS1005 TO FS1040. FOUND OUT OF LIMITS PER
- [SDR SWIA2024082300607](https://openairdocs.org/sdr/SWIA2024082300607.md): Frame · corroded · Jun 7, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Frame
  > REAR FUSELAGE INTERNAL STRUCTURE AT FS1015.00 APPROXIMATELY STGR22L TO STGR24L CORRODED AS MARKED (C-CHECK RO 8/22/2024) INSTALLED NEW FRAME SECTOR FS1015, FROM STR19L-STR26L IAW REO 670-53-61-1669 REV- 2020-05-08 AND CRJ 700 SRM 53-00-06-201-001-A03 AN
- [SDR SWI202408230737](https://openairdocs.org/sdr/SWI202408230737.md): Door Sill · corroded · Jun 6, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR SILL VERTICLE FACE HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 8/22/2024) REMOVED CORROSION OFF SILL BRACKET IAW CRJ 700 SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS PER CRJ 700 SRM 53-61-06-101-002
- [SDR SWI2024082300736](https://openairdocs.org/sdr/SWI2024082300736.md): Landing · corroded · Jun 6, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Structure
  > SURFACE CORROSION ON LOWER PAN INSIDE RT FUSELAGE TO PYLON SYSTEM ACCESS PANEL 282AZ. (C-CHECK RO 8/22/2024) BLENDED CORROSION ON LOWER PAN INSIDE RT FUSELAGE TO PYLON SYSTEM ACCESS PANEL 282AZ REF. CRJ700 SRM 51-21-06-001-001-A01. RECEIVED AND COMPLETE
- [SDR SWIA202408230606](https://openairdocs.org/sdr/SWIA202408230606.md): Tie Down · corroded · Jun 6, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY NET HOLD DOWN PLATE AT FS 581.0 APROX BL 0 CORRODED (C-CHECK RO 8/22/2024) BLENDED AREA AT FORWARD BAGGAGE BAY NET HOLD DOWN PLATE AT FS 581.0 APPROX. BL 0 IS OUT OF LIMITS.INSTALLED NEW FWD CARGO TIEDOWN PLATE P/N SH670-33389-2 AT F
- [SDR SWI2024F00726](https://openairdocs.org/sdr/SWI2024F00726.md): Floorbeam · corroded · Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 CROSSBEAM UPPER SPLICE STRIP HAS MULTIPLE AREAS OF CORROSION AS MARKED (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW UPPER SPLICE STRIP AT FS280 CROSSBEAM REF-CRJ-700 SRM 51-42-06-001-001 A01, SRM 51-42-13-001-001 A01 AND DWG CC670-34010 RE
- [SDR SWI2024F00725](https://openairdocs.org/sdr/SWI2024F00725.md): Fitting · chafed · Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND UPPER FWD PIN FITTING CHAFED (FLAGGED) (C-CHECK RO 8/22/2024) REPAIRED PAX DOOR SURROUND UPPER FWD PIN FITTING REF. REO 670-53-21-2427 REV. --, DATED 2024-06-24 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR
- [SDR SWI2024F00724](https://openairdocs.org/sdr/SWI2024F00724.md): Stringer · corroded · Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR.20R HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS.517.00 TO FS.549.00 (MARKED). (C-CHECK RO 8/22/2024) INSTALLED THE NEW STRINGER 20RH BETWEEN FS.501.00 AND FS.547.00 REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DWG SH670-33
- [SDR SWI2024F00723](https://openairdocs.org/sdr/SWI2024F00723.md): Fitting · gouged · Jun 5, 2024 · N758SK · Cndair CL6002C10 · Galley Doors
  > GALLEY SERVICE DOOR LOWER AFT GUIDE ROLLER FITTING GOUGED (FLAGGED). (C-CHECK RO 8/22/2024) BLENDED CHAFE ON GALLEY SERVICE DOOR LOWER AFT GUIDE ROLLER FITTING REF. CRJ700 SRM 51-12-00-001-001-A01. REPAIRED DAMAGE BY COMPLYING WITH ALL STEPS OF REO 670-
- [SDR SWI2024F00722](https://openairdocs.org/sdr/SWI2024F00722.md): Bracket · cracked · Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BRACKET AT APPROXIMATELY FS280.00 RBL9 CROSSBEAM AS MARKED (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW BRACKET CRJ700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020 AND DWG CC670-34010 REV -K. COMPLIED WITH ALL STEPS OF TASK CARD 51-
- [SDR SWI2024F00721](https://openairdocs.org/sdr/SWI2024F00721.md): Floor Panel · corroded · Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Floor Panel
  > FS280.00 FLOOR PANEL SUPPORT ANGLE HAS MULTIPLE AREAS OF CORROSION AS MARKED (C-CHECK RO 8/22/2024) REMOVED AND REPLACED SUPPORT ANGLE AT FS280.00 BETWEEN LBL12 AND RBL12 REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIE
- [SDR SWIA20240605](https://openairdocs.org/sdr/SWIA20240605.md): Structure · corroded · Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS MULTIPLE AREAS OF CORROSION BETWEEN APPROXIMATELY STGR26L AND STGR24R AS MARKED (C-CHECK RO 8/22/2024) BLENDED CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ R
- [SDR SWI2024F00703](https://openairdocs.org/sdr/SWI2024F00703.md): Hinge Fitting · gouged · Jun 1, 2024 · N758SK · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > THE RH AILERON HINGE FITTING #3 ON THE WING SIDE HAS MULTIPLE GOUGES. (MARKED). REJECTION COMMENTS:SDR MUST BE YES (C-CHECK RO 8/22/2024) BLENDED OUT MULTIPLE GOUDES AT RH AILERON HINGE FITTING # 3 REF-CRJ-700 REO 670-57-51-555 REV -- 2024-07-01. COMPLI
- [SDR SWI2024F00702](https://openairdocs.org/sdr/SWI2024F00702.md): Hinge Fitting · gouged · Jun 1, 2024 · N758SK · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > THE RH AILERON HINGE FITTING #2 ON THE WING SIDE HAS MULTIPLE GOUGES. (MARKED). (C-CHECK RO 8/22/2024) BLENDED OUT MULTIPLE GOUDES AT RH AILERON HINGE FITTING # 2 REF-CRJ-700 REO 670-57-51-555 REV -- 2024-07-01. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWI2024F00720](https://openairdocs.org/sdr/SWI2024F00720.md): Slat Track · worn · May 29, 2024 · N758SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H #1 SLAT INBD SLAT TRACK HAS WEAR IN SEVERAL AREA'S ((MKD IN RED) S/N 00527) (C-CHECK RO 8/22/2024) REPAIRED RH #1 SLAT INBD SLAT TRACK (1-1) PER REO 670-57-42-1597, REV.--, DATE 2024-06-27. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTI
- [SDR SWI2024F00719](https://openairdocs.org/sdr/SWI2024F00719.md): Slat Track · corroded · May 29, 2024 · N758SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > R/H #1 SLAT MID SLAT TRACK HAS SEVERAL AREA'S OF PITTING CORROSION (S/N 00526) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM RH WING SLAT TRACK 1-2 REF-CRJ-700 SRM 51-12-00-001-001 A01,REPAIRED REF REO 670-57-42-1598 REV -- DATE 2024-06-27, DWG CC670
- [SDR SWI2024F00718](https://openairdocs.org/sdr/SWI2024F00718.md): Slat Track · corroded · May 29, 2024 · N758SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > R/H # 2 SLAT MID SLAT TRACK HAS PITTING CORROSION AND SEVERAL AREA'S OF WEAR (S/N 00521) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM RH WING SLAT TRACK 2-2 REF. CRJ-700 SRM 51-12-00-001-001-A01, DWG CC670-12050 REV.-C, AND COMPLIED WITH REO 670-57-42-
- [SDR SWIA202408723529](https://openairdocs.org/sdr/SWIA202408723529.md): Retainer · bent · May 29, 2024 · N758SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR SEAL RETAINER IS BENT (BOTTOM SIDE OR CLOSEST TO HINGE) MX#28302443 (C-CHECK RO 8/22/2024) INSTALLED NEW AFT LOWER CORNER PAX DOOR SEAL RETAINER REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01 AND DWG NO 601R31871 REV -D.
- [SDR SWI2024F00717](https://openairdocs.org/sdr/SWI2024F00717.md): Slat Track · damaged · May 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H @1 SLAT INBD SLAT TRACK HAS SLIGHT PITTING ( MKD IN RED) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM SLAT TRACK 1-1 REF. CRJ-700 SRM 51-12-00-001-001-A01 AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1595 REV.--, DATED 2024-06-27 AND 51-900-1002-SKY
- [SDR SWI2024F00716](https://openairdocs.org/sdr/SWI2024F00716.md): Slat Track · worn · May 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H #1 SLAT OTBD SLAT TRACK HAS WORN AREA (MKD IN RED) (C-CHECK RO 8/22/2024) REMOVED DAMAGE ON SLAT TRACK 1-3 REF CRJ-700 SRM 51-12-00-001-001-A01 AND COMPLIED WITH REO 670-57-42-1600, REV--, DATE 2024-07-05.SLAT RIGGING REQUIREMENTS ARE MET.COMPLIED
- [SDR SWI2024F00715](https://openairdocs.org/sdr/SWI2024F00715.md): Slat Track · damaged · May 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H #3 SLAT OTBD SLAT TRACK HAS SLIGHT PITTING LOWER SIDE (C-CHECK RO 8/22/2024) BLENDED DAMAGE ON LH #3 SLAT OTBD SLAT TRACK AND REPAIRED REF REO 670-57-42-1596 REV.--, DATED 2024-06-27, SRM 51-12-00-001-001-A01 REV 38 DATED 25-JUL-2020 AND DWG CC670-1
- [SDR SWIA20240528](https://openairdocs.org/sdr/SWIA20240528.md): Slat Track · worn · May 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H #3 SLAT MID SLAT TRACK HAS AREA WORN (MKD IN RED) (C-CHECK RO 8/22/2024) REMOVED DAMAGE ON SLAT TRACK 3-2 REF CRJ-700 SRM 51-12-00-001-001-A01 SLAT 3-2 SLAT- FWD FLANGE AND WAS FOUND TO BE OUT OF LIMITS AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1
- [SDR SWI2024F00714](https://openairdocs.org/sdr/SWI2024F00714.md): Hinge · gouged · May 25, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR AFT HINGE LUG, THE HOLE FOR THE ROLL PIN IS GAUGED / WORN. COMPLIED WITH REO 670-52-11-1391 REV --, DATED 2024-06-24 STEPS 1-7, OPENED UP AND/OR REAMED LUG HOLE ON UPPER AND LOWER SURFACES TO 0.125" - 0.129", RESTORED FINISH, INSTALLED NEW SPRING
- [SDR SWI2024F00713](https://openairdocs.org/sdr/SWI2024F00713.md): Hinge · scratched · May 25, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > ALL LUGS OF PAX DOOR HINGE ARE SCRATCHED AND PITTED. (DOOR SIDE) LUGS OF PAX DOOR HINGE BLENDED, REPAIRED AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 52-11-01-201-007-A01 REPAIR TYPES L (1) AND LV (4) AND (REFERENCE DWG 601R318073 REV. -E). SURFACE FINIS
- [SDR SWIA20240823525](https://openairdocs.org/sdr/SWIA20240823525.md): Lug · damaged · May 25, 2024 · N758SK · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > INBOARD FLAP, OUTBOARD HINGE ARM, FORWARD LUG HAS IMPACT DAMAGE. (C-CHECK RO 8/22/2024) BLENDED OUTB HINGE ARM REF CRJ-700 SRM 51-12-00-001-001-A01 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-57-52-560 REV -- DATE 2024-07-09 ALL STEPS OF REO COM

Next page: https://openairdocs.org/aircraft/N758SK/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 = 'N758SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N758SK/reports

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