N752SK

Service difficulty reports · 212

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 = 'N752SK' 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 SWIA2026081576867Duct · leakingLEFT BLEED DUCT WARNING MESSAGE ON CLIMB OUT AT 12000 (FLIGHT 6234). ON ARRIVAL TO ACFT NO CURRENT WARNING MESSAGE WAS PRESENT. INTERROGATED MDC FOUND B1 007182. PERFORMED BLEED LEAK TEST IAW FIM 36-21-01. BLEED LEAK TEST PASSED. CHECKED EVENT LOCATION HISTAug 15, 2026 · N752SK · Cndair CL6002C10 · Pneumatic Distribution SystemSDR SWIA202404290322Bulkhead · corrodedLH FS. 280 LOWER BULKHEAD HAS CORROSION (LBL10 FLOOR LEVEL). (C-CHECK RO 4/26/2024) REPLACED THE LH FS280 LOWER BULKHEAD WEB. REF CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Mar 22, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA202404290319Floorbeam · corrodedCORROSION FOUND ON L/H CROSSBEAM AT FS 280.0 UPON REMOVAL OF FLOOR SUPPORT ANGLE LBL 9.0 - RBL 9.0 (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW L/H CROSSBEAM AT FS 280.0 UPON REMOVAL OF FLOOR SUPPORT ANGLE LBL 9.0 - RBL 9.0 IAW DWG CC670-34010 REV. K Mar 19, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI202404290346Intercostal · corrodedPASSENGER DOOR INTERCOSTAL MID DD4 CORRODED (C-CHECK RO 4/26/2024) INSTALLED NEW MID DD4 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024042900345Intercostal · corrodedPASSENGER DOOR INTERCOSTAL FWD DD5 CORRODED (C-CHECK RO 4/26/2024) REPLACED PAX DOOR FWD DD5 INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024042900344Intercostal · corrodedPASSENGER DOOR INTERCOSTAL AFT DD3 CORRODED (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR AFT DD3 INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024042900343Intercostal · corrodedPASSENGER DOOR INTERCOSTAL FWD DD3 CORRODED (C-CHECK RO 4/26/2024) REPLACED PAX DOOR FWD DD3 INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTEDMar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024042900342Intercostal · corrodedPASSENGER DOOR INTERCOSTAL DD7A CORRODED (C-CHECK RO 4/26/2024) INSTALLED NEW MID DD7A INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024042900341Door Frame · corrodedPASSENGER DOOR FRAME FS313.56 AND CLEAT BETWEEN DD4 & DD5 CORRODED (C-CHECK RO 4/26/2024) REPLACED PAX DOOR FRAME SECTION AND ATTACHING CLEAT AT FS 313.56 BETWEEN DD4 AND DD5 REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CMar 13, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI20240429000340Doubler · crackedPASSENGER DOOR AFT PULL-IN CAM DOUBLER IS CRACKED (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW AFT PULL-IN CAM DOUBLER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020 AND DWG 601R31702 REV. N. COMPLIEMar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024042900339Doubler · crackedPASSENGER DOOR FWD PULL-IN CAM DOUBLER IS CRACKED (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW FWD PULL-IN CAM DOUBLER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020 AND DWG 601R31702 REV. N. COMPLIEMar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202404290313Frame · chafedFS1144.00 STRG 9RH FRAME IS CHAFFED BY THE WATER INJECTION LINE (MARKED) (C-CHECK RO 4/26/2024) REPAIRED CHAFFE ON FRAME AT FS 1144.00 STRG 9R REF REO 670-53-61-2251 REV -- DATED 2024-04-10. ALL STEPS OF REO COMPLIED WITH. M337 AND SKYWEST TASK CARD 51-90Mar 13, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202404290312Window Post · crackedCO-PILOTS WINDSHIELD POST APPEARS CRACKED AT THE TOP BARREL NUT. (C-CHECK RO 4/26/2024) REMOVED CO-PILOT WINDSHIELD POST IAW CRJ 700 SRM 51-42-21-001-001-A01 AND NEW CO-PILOT WINDSHIELD POST P/N 601R33223-2 INSTALLED ALONG WITH NEW BARRELL NUTS P/N NAS577BMar 12, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2024042900310Intercostal · corrodedPAX DOOR AFT DD5 INTERCOSTAL HAS EXFOLIATED CORROSION ON TWO ELEMENT REQUIRE REPLACEMENT JOB # HN00144727 (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR AFT DD5 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CAMar 10, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2024042900308Window Post · crackedPILOT SIDE WNDSHIELD POST IS CRACKED AT THE TOP BARREL-NUT HOLE. (MARKED) (C-CHECK RO 4/26/2024) REMOVED CRACKED PILOT SIDE WINDSHIELD POST REF CRJ700 SRM51-42-21-001-001-A01 AND INSTALLED NEW PILOT SIDE WINDSHIELD POST REF CRJ700 SRM 51-42-21-001-001-A01 Mar 8, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA20240429306Floorbeam · crackedRH COCKPIT FLOOR BEAM (RBL12) CRACKED AT THE BOTTOM OF THE AFT END FS280.00 CROSSBEAM (MARKED) (C-CHECK RO 4/26/2024) REMOVED CRACKED, RIGHT-HAND COCKPIT FLOOR BEAM (RBL 12), AT FS280.00, AND INSTALLED NEW FLOOR BEAM. REF. CRJ 700 SRM 53-11-43-201-003-A01Mar 6, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024042900338Cargo Net · corrodedFWD CARGO RESTRAINT NET AFT TIE DOWN PAD HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 4/26/2024) INSTALLED NEW TIE DOWN FITTING P/N SH670-33390-2. REF: DWG SH670-33600, REV: AD, CRJ700 SRM 51-42-21-001-001-A01 CRJ 700 SRM 51-42-06-001-001-A01, ANDMar 5, 2024 · N752SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWI2024042900337Door Sill · corrodedAFT CARGO DOOR SILL HAS CORROSION (C-CHECK RO 4/26/2024) REMOVED CORROSION FROM THE AFT BAGGAGE BAY DOOR SILL AND EVALUATED AS OUT-OF-LIMITS. REMOVED CORRODED SILL AND REPLACED WITH NEW SILL. REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-0Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI20240429000336Stringer · corrodedSTRINGER23L FS1000-FS985 HAS AREAS OF CORROSION (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED FORWARD SPLICE ANGLE, DRAIN LINE BRACKET AND NEW SECTION STRINGER 23L BETWEEN FS 977.00 - FS 1015.00 REF CRJ 700 SRM 53-00-03-201-001-A01 CRJ700 SRM 51-42-06-001-0Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWI202404290335Floor Support · corrodedFLOOR BEAM AT RBL9 FS1031- FS1051 HAS LIGHT AREAS OF CORROSION (C-CHECK RO 4/26/2024) REPAIRED FLOOR BEAM AT RBL 9.0 BETWEEN F/S 985.00 TO F/S 1075.75 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2242 REV. -- DATED 2024-03-12 AND COMPLIED WITH SKMar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024042900334Floor Support · corrodedFLOOR SUPPORT AT LBL9 FS1015- FS1051 HAS AREAS OF CORROSION (C-CHECK RO 4/26/2024) REPAIRED FLOOR SUPPORT AT LBL 9.0 BETWEEN F/S 985.00 TO F/S 1075.75 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2242 REV. -- DATED 2024-03-12 AND COMPLIED WITH SKMar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00333Floor Support · corrodedFLOOR SUPPORT AT LBL27 FS1015- FS1051 HAS AREAS OF CORROSION. PERFORMED FLOOR SUPPORT CUTOUT REPAIR. IAW SRM 51-42-21-001-001-A01, REF SRM 53-00-41-201-001-A01 REV 38, REO 670-53-61-2247 REV--, AND DWG MM690-35041 REV AB. COMPLIED WITH SKYWEST TASK CARD.Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024042900332Frame · corrodedFRAME AT FS1015 STGR20L -STGR26L HAS SEVERAL AREAS OF CORROSION (C-CHECK RO 4/26/2024) REPLACED NEW LOWER FRAME SECTION FS.1015 BETWEEN STGR26R TO STGR20LH ERF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG MM670-36062 REV -E. COMMar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI2024042900331Door · corrodedPAX DOOR FWD DD4 HAS CORROSION (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR FWD DD4 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.Mar 5, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI202404290330Former · corrodedPAX DOOR AFT FORMER BETWEEN DD5 AND DD7 HAS CORROSION (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR AFT FORMER IAW DWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.Mar 5, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202404290305Channel · crackedAFT CARGO DOOR AFT TRACK FORWARD LOWER SUPPORT FOR THE DOOR TRACK IS CRACKED. (MARKED) (C-CHECK RO 4/26/2024) REMOVED AND REPLACED WITH NEW CHANNEL P/N MM670-35552-005 ON AFT CARGO DOOR, LOWER AFT TRACK FRAME. REF; DWG MM670-35060, REV: W, CRJ700 SRM 51-Mar 5, 2024 · N752SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202404290301Skin · gougedAFT LOWER FUSELAGE SKIN IS CHAFED/GOUGED AT APPROX FS972 AT BL 0. (C-CHECK RO 4/26/2024) REPAIRED AFT LOWER FUSELAGE SKIN AT APPROX FS972 AT BL0 IRT REO 670-53-00-723 REV-- DATED 2024-03-29, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK PASSEDMar 1, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI202404290329Slat Track · wornRIGHT WING LEADING EDGE SLAT TRACK ASSEMBLY NO. 3-3 HAS WARE MARKS, HN00142274 (C-CHECK RO 4/26/2024) REPAIRED RH WING SLAT TRACK ASSEBLY 3-3. PER REO 670-57-42-1495 REV -- DATED 2024-03-07 STEPS 1-8. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900Feb 29, 2024 · N752SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWI202404290328Slat Track · wornLEFT WING LEADING EDGE SLAT TRACK ASSEMBLY NO. 3-3 HAS WARE MARKS, HN00142273 (C-CHECK RO 4/28/2024) REPAIRED LEFT WING LEADING EDGE SLAT TRACK ASSEMBLY NO. 3-3 BY COMPLYING WITH REO 670-57-42-1494 REV -- DATED 2024-03-07, COMPLIED WITH 51-900-1002-SKYFeb 29, 2024 · N752SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWI202404290327Stand Off · crackedR/H LWR TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REMOVED CRACKED INBD "A" BRACKET STANDOFF FROM R/H LWR TRANSCOWL REF CRJ 700 SRM 51-42-14-001-001-A01. INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON R/H LWR TRANSCOWLFeb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2024042900326Latch · chafedR/H UPPER TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 4/26/2024) REPAIRED R/H UPPER TRANS COWL OUTER SKIN / FWD. DISHING AND COMPLIED WITH ALL STEPS OF NEW FINAL REO 670-54-21-1622, REV. --, 2024-03-28. COMPLIED WITH M-337 & SKY CARD 51-900-1Feb 29, 2024 · N752SK · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR SWI202404290325Stand Off · crackedR/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.Feb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI20240429000324Bracket · crackedL/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) INSTALLED A NEW O/B "A" BRACKET (PN CN624-2082-201) INTO L/H LWR TRANSCOWL REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION SHEET Feb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2024042900323Skin · crackedL/H LWR TRANSCOWL OUTER SKIN IS CRACKED @ LATCH SCREW HOLE. (C-CHECK RO 4/26/2024) L/H LWR TRANSCOWL OUTER SKIN HAS BEEN REPAIRED REF REO# 670-54-21-1623, REV --, DATED 3/18/24. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. REFER TO CONTINUATION SHEET FOR DETAFeb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA20240229Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REMOVED AND REPLACED L/H UPPER TRANSCOWL I/B "A" BRACKET W/A NEW "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKFeb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2024042900322Pressure Switch · cracked*R/H EMER EXIT HAS SUSPECTED CRACK AT THE BASE OF UPPER AFT FITTING (PROX SENSOR STRIKER FITTING). (C-CHECK RO 4/26/2024) THE CRACK ON UPPER FRAME WEB OF RH EMERGENCY EXIT WAS REPAIRED BY REINFORCEMENT PLATE (DOUBLER) AND REPAIR FILLER PER REO 670-52-21-09Feb 28, 2024 · N752SK · Cndair CL6002C10 · Emergency ExitsSDR SWIA202404290228Fitting · cracked*L/H EMER EXIT HAS SUSPECTED CRACK AT THE BASE OF UPPER AFT FITTING (PROX SENSOR STRIKER FITTING). (C-CHECK RO 4/26/2024) THE CRACK ON UPPER FRAME WEB OF LH EMERGENCY EXIT WAS REPAIRED BY REINFORCEMENT PLATE (DOUBLER) AND REPAIR FILLER PER REO 670-52-21-09Feb 28, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA202404290227Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 4/26/2024) PERFORMED LH VERTICAL STAB FWD DRAG ANGLE REPAIR. PER CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Feb 27, 2024 · N752SK · Cndair CL6002C10 · Vertical StabilizerSDR SWI202404290321Stiffener · bentFS 280 BULKHEAD, AFT LEFT SIDE UPPER STIFFENER ANGLE IS BENT. (C-CHECK RO 4/26/2024) REMOVED DAMAGED ANGLE AND REPLACED WITH NEW ANGLE P/N CC670-32449-1 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 AND DWG CC670-34010 REV-K, RII REQUIREMENTFeb 25, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA202404290225Landing · crackedRIGHT TRU BAY ( FORWARD EQUIPMENT COMPARTMENT ) AFT DOOR LATCH CUTOUT HAS POSSIBLE CRACK. (C-CHECK RO 4/26/2024) VERIFIED AND CONFIRMED CRACK ON THE RIGHT-HAND TRU BAY DOOR LANDING. REPLACED RIGHT-HAND TRU DOOR LANDING REF. REO 670-53-11-1935 REV. -- DATE:Feb 25, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI20240429000320Housing · gougedAFT BAGGAGE BAY DOOR HANDLE HOUSING HAS NUMEROUS GOUGES (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW DOOR HANDLE HOUSING P/N 119992-5. REF: CRJ-700 AMM 52-31-03-400-801-A01 REVISION 71: DEC 16/2022, CRJ700 SRM 51-42-21-001-001-A01 REVISION 38: JUL 25/Feb 23, 2024 · N752SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA2024042900223Retainer · bentAFT BAGGAGE BAY DOOR LOWER CENTER SEAL RETAINER BENT IN AT FWD AND AFT STOP FITTINGS (C-CHECK RO 4/26/2024) REMOVED AND REPLACED WITH NEW AFT CARGO DOOR LOWER CENTER SEAL RETAINER REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-38702, REV -F. LEAK CHECK Feb 23, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2024042900219Skin · dentedADM# N752SK-8069 L/H LOWER FUSELAGE TAIL AREA FS 1144.00, SMOOTH DENT L-2.8" W-1.55" D-.020". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 4/26/2024) REPAIRED DENT ATFeb 19, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202404291004Skin · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA77176-670-53-11-1790 752SK MXCODEID61274-PR - FOUND CRACK ON THE LOWER AFT CORNER OF THE THE LH FORWARD ELECTRICAL BAY (TRU BAY). COMPLIED WITH REO 670-53-11-1790, REV.--, DATED 2022-02-15 FOR TEMPORARY DISPOSITION FOOct 4, 2023 · N752SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2024F00097Stud · missingPASSENGER SEAT 12AB IB FWD SEAT TRACK MOUNTING STUD IS MISSING THE LOCKING PLATE. PN 41031038-503 MR2184015 (FILED CLOSED)REMOVED AND REPLACED SEAT 12AB INBOARD FWD SEAT TRACK MOUNTING STUD IAW SAFRAN CMM 25-26-24.Sep 1, 2023 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00098Stud · missingPASSENGER SEAT 6AB IB FWD SEAT TRACK MOUNTING STUD IS MISSING THE LOCKING PLATE. PN 41031038-503 MR2184015 (FILED CLOSED)REMOVED AND REPLACED SEAT 6AB INBOARD FWD SEAT TRACK MOUNTING STUD IAW SAFRAN CMM 25-26-24.Sep 1, 2023 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202161975None · chafedFORM M-337, "REPORT OF AIRCRAFTMAJOR REPAIR. REQUIRED FOR REPAIR ON FRAME FS1162 HAS DAMAGE RH SIDE FROM CHAFFING (FILED CLOSED) COMPLIED WITH FORM M-337Oct 28, 2021 · N752SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202161976None · chafedFRAME FS1162 HAS DAMAGE RH SIDE FROM CHAFFING. (FILED CLOSED) REPAIRED FRAME FS1162 BETWEEN STGR 7R AND STGR 8R IN ACCORDANCE WITH REO 670-53-71-084Oct 27, 2021 · N752SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020061051070Threshold · crackedCOCKPIT FLOORBOARD THRESHOLD IS CRACKED. (C-CHECK) RO 4/24/2020 ORDERED, RECEIVED, AND INSTALLED 1 NEW COCKPIT THRESHOLD REF SRM.Jun 3, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020061051068Floor Support · crackedRT COCKPIT FLOOR SUPPORT ANGLE AT BL 12 (P/N CC670-33199-4) IS CRACKED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED CRACKED RT COCKPIT FLOOR SUPPORT ANGLE WITH NEW FLOOR SUPPORT ANGLE (P/N CC670-33199-4) AT RBL 12, FS 259.20 TO FS 280.00 REF SRM, DWG. RESTOREMay 15, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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