N758SK

Service difficulty reports · 215

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 = 'N758SK' 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 SWIA2026081276841Aoa · faultedIMMEDIATELY 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 PAug 12, 2026 · N758SK · Cndair CL6002C10 · Stall Warning SystemSDR SWIA2026072576676Motor · faultedDURING 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 TRIMMJul 25, 2026 · N758SK · Cndair CL6002C10 · Stabilizer Position IndicatingSDR SWIA2025122400003Window · crackedCAPTAINS 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.Dec 23, 2025 · N758SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2025102000019Ballast · failedON 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 SLIGHTOct 19, 2025 · N758SK · Cndair CL6002C10 · Lighting SystemSDR SWIA202503030002Landing Gear · warning message*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 WMar 2, 2025 · N758SK · Cndair CL6002C10 · Landing Gear Position and WarningSDR SWIA202502240003Landing Gear · warning messageFLIGHT 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 TURNEFeb 23, 2025 · N758SK · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR SWIA202408230627Hinge · misinstalledLOW 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 (HST110AJun 27, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2024082300622Door Sill · corrodedSERVICE 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 Jun 22, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2024082300621Door Sill · corrodedSERVICE 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 FOJun 21, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI202408230735Floor Support · crackedFLOOR 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 WITHJun 20, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2024082300620Floor Support · crackedCRACK 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 BOMBAJun 20, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2024082300619Retainer · bentPAX 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#283Jun 19, 2024 · N758SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI202408230729Drag Angle · crackedVERTICAL 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-SKYJun 17, 2024 · N758SK · Cndair CL6002C10 · Vertical StabilizerSDR SWI202408230728Drag Angle · crackedVERTICAL 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 51-900-10Jun 17, 2024 · N758SK · Cndair CL6002C10 · Vertical StabilizerSDR SWIA202408230612Floorbeam · crackedCENTER 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 TASKJun 12, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI202408230738Skin · scratchedLH 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 COMPLYINJun 11, 2024 · N758SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202408230611Skin · damagedTOOL 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 REOJun 11, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202408230610Hinge · gougedPAX 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 AREAJun 10, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA202408230609Structure · corrodedCORROSION 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 51-42-06-0Jun 9, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI202408230734Stringer · corrodedCORROSION 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 51-42-21-001-00Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWI202408230733Joint · corrodedCIRCUMFERENTIAL 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 Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI202408230732Joint · corrodedCIRCUMFERENTIAL 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 Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2024082300731Crossbeam · corrodedFS280 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 25Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2024082300730Joint · corrodedCIRCUMFERENTIAL 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 Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2024082300608Floorbeam · corrodedFS280 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 25Jun 8, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00727Floorbeam · corrodedAFT 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 Jun 7, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2024082300607Frame · corrodedREAR 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 ANJun 7, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI202408230737Door Sill · corrodedAFT 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 53-61-06-101-002Jun 6, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024082300736Landing · corrodedSURFACE 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 COMPLETEJun 6, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202408230606Tie Down · corrodedFORWARD 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 FJun 6, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00726Floorbeam · corrodedFS280.00 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 REJun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00725Fitting · chafedPAX 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 FORJun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00724Stringer · corrodedSTR.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 SH670-33Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWI2024F00723Fitting · gougedGALLEY 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-Jun 5, 2024 · N758SK · Cndair CL6002C10 · Galley DoorsSDR SWI2024F00722Bracket · crackedCRACKED 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-Jun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00721Floor Panel · corrodedFS280.00 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 BOMBARDIEJun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Floor PanelSDR SWIA20240605Structure · corrodedCIRCUMFERENTIAL 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 RJun 5, 2024 · N758SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2024F00703Hinge Fitting · gougedTHE 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. COMPLIJun 1, 2024 · N758SK · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR SWI2024F00702Hinge Fitting · gougedTHE 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-SKYJun 1, 2024 · N758SK · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR SWI2024F00720Slat Track · wornR/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 CONTIMay 29, 2024 · N758SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00719Slat Track · corrodedR/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 CC670May 29, 2024 · N758SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWI2024F00718Slat Track · corrodedR/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-May 29, 2024 · N758SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202408723529Retainer · bentPAX 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. May 29, 2024 · N758SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024F00717Slat Track · damagedL/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-SKYMay 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00716Slat Track · wornL/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 May 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00715Slat Track · damagedL/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 CC670-1May 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA20240528Slat Track · wornL/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 670-57-42-1May 28, 2024 · N758SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00714Hinge · gougedPAX 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 May 25, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWI2024F00713Hinge · scratchedALL 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 FINISMay 25, 2024 · N758SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA20240823525Lug · damagedINBOARD 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 COMMay 25, 2024 · N758SK · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
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