N740SK

Service difficulty reports · 194

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 = 'N740SK' 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 SWIA2024012219Track · damagedDRILL STOP NOTED ON RHS FIXED LEADING EDGE TRACK 2-3 ON OUTBD RIB COMPLY WITH MHIRJ REO 670-57-41-519 (C-CHECK RO 1/19/2024) REPAIRED NOTED DAMAGE ON RHS FIXED LEADING EDGE TRACK 2-3 ON OUTBD RIB, CUT OUT DAMAGED AREA, NDT INSPECTED NO DEFECTS NOTED, INSTDec 19, 2023 · N740SK · Cndair CL6002C10 · Wing Miscellaneous StructureSDR SWI2024F00011Skin · corrodedFS801 - FS847 LH APRON SKIN TOP ROW SMOKING FASTENERS SHOWING SIGNS OF FRETTING CORROSION. (C-CHECK RO 1/19/2024) REMOVED 45EA SMOKING RIVETS LOCATED ON THE LH APRON SKIN, TOP ROW BTWN FS.801-FS.847. REF. CRJ700 SRM 51-42-06-001-001-A01. PERFORMED REPAIR Nov 30, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2024F00010Skin · gougedGOUGE ON FWD CARGO DOOR AREA, FUSELAGE SKIN AFT TOP CORNER. (C-CHECK RO 1/19/2024) REMOVED GOUGING FROM FWD CARGO DOOR AREA, FUSELAGE SKIN AFT TOP CORNER AND REPAIRED REF. REO 670-53-31-838 REV.-A DATED 2023-12-29 STEPS 1-7. COMPLIED WITH SKYWEST M-337 FORNov 30, 2023 · N740SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA20231130Skin · corrodedFS801 - FS847 RH APRON SKIN TOP ROW SMOKING FASTENERS SHOWING SIGNS OF FRETTING CORROSION. (C-CHECK RO 1/19/2024) REMOVED 47EA SMOKING SOLID RIVETS & 2EA HI-LITE FASTENERS LOCATED ON THE RH APRON SKIN, TOP ROW BTWN FS.801-FS.847. REF. CRJ700 SRM 51-42-06-Nov 30, 2023 · N740SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWI2024F00009Floorbeam · crackedPOSSIBLE CRACK ON COCKPIT FLOOR BEAM AT FS.280.00 AND RBL12.(FLAGGED). (C-CHECK RO 1/19/2024) REPAIRED COCKPIT FLOOR BEAM SECTION AT FS.280.00 AND RBL12 REF CRJ 700 SRM 53-11-43-201-003-A01. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUATION CARD FOR WORK PERNov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00008Floorbeam · corrodedFLOOR POST AT FS.280.00 AND RBL12 WL.72. CORRODED (FLAGGED). (C-CHECK RO 1/19/2024) REMOVED CORROSION ON FLOOR POST AT FS 280.00 RBL 12 REF CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REF: CRJ-700 SRM 53-11-10-001-003-A01. REPAIRED REF CRJNov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00007Floorbeam · crackedCOCKPIT FLOOR PANEL LANDING CRACKED AT FS.280.00 AND RBL12.(FLAGGED). (C-CHECK RO 1/19/2024) REMOVED AND INSTALLED NEW COCKPIT FLOOR PANEL LANDING AT FS.280.00 AND RBL12 REF CRJ 700 SRM 51-42-06-001-001-A01 / BOMBARDIER DWG CC670-33199 REV B. COMPLIED WITHNov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00006Floorbeam · corrodedL/H INBD FLOOR BEAM @ FS1031.0 HAS CORROSION (TOP SIDE) (C-CHECK RO 1/19/2024) REPAIRED FLOOR BEAM WITH NEW SECTION AT (LH IB) LBL 9.0 BETWEEN FS1026.00 TO FS1038.00 REF: CRJ700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2218 REV-- DATED 2023-12-18 . COMNov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00005Floorbeam · corrodedL/H OTBD FLOOR BEAM @ FS1031.0 HAS CORROSION (TOP SIDE) (C-CHECK RO 1/19/2024) REPAIRED FLOOR BEAM WITH NEW SECTION AT (LH IB) LBL 27.0 BETWEEN FS1026.00 TO FS1038.00 REF: CRJ700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2218 REV-- DATED 2023-12-18 . CONov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Floor PanelSDR SWI2024F00004Floorbeam · crackedPOSSIBLE CRACK ON COCKPIT FLOOR BEAM AT FS.280.00 AND LBL12.(FLAGGED). (C-CHECK RO 1/19/2024) REPAIRED COCKPIT FLOOR BEAM AT FS.280.00 AND LBL12. REF: CRJ-700 SRM 53-11-43-201-003-A01Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2023012200129Floorbeam · crackedCOCKPIT FLOOR PANEL LANDING CRACKED AT FS.280.00 AND LBL12.(FLAGGED). (C-CHECK RO 1/19/2024) INSTALLED NEW COCKPIT FLOOR PANEL LANDING AT FS280 LBL 12 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG.NO. CC670-33052 REV-G. COMPLIED WITH TASK CARD 51-900-1002-SNov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00003Floorbeam · crackedPOSSIBLE CRACK ON FLOOR PANEL LANDING GUSSET COMMON TO THE FS,280.00 FLOOR BEAM AT LBL12 (MARKED) (C-CHECK RO 1/19/2024) INSTALLED NEW COCKPIT FLOOR PANEL LANDING GUSSET AT FS280 LBL 12 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG.NO. CC670-33052 REV-G COMNov 28, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00002Floorbeam · corrodedFLOOR PANEL LANDING COMMON TO THE FS,280.00 BEAM BETWEEN RBL12 AND LBL12 CORRODED (MARKED). (C-CHECK RO 1/19/2024) INSTALLED NEW FLOOR SUPPORT ANGLE ASSY. P/N CC670-34095 AT FS 280.00 BEAM BETWEEN LBL12 AND RBL 12 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ Nov 28, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00001Bracket · crackedR/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED. (C-CHECK RO 1/19/2024) INSTALLED 1EA. NEW A-BRACKET P/N CN624-2082-201 ON R/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. B, DATED 2023-11-28. COMPLIED WITH SKYCARD 51-900-1002-SKYNov 28, 2023 · N740SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2023012200128Floor Support · crackedPOSSIBLE CRACK ON FLOOR PANEL LANDING GUSSET COMMON TO THE FS,280.00 FLOOR BEAM AT RBL12 (MARKED) (C-CHECK RO 1/19/2024) REMOVED AND INSTALLED NEW COCKPIT FLOOR PANEL LANDING GUSSET AT FS.280.00 RBL12 REF CRJ 700 SRM 51-42-06-001-001-A01 / BOMBARDIER DWG CNov 28, 2023 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20230122125Windshield · crackedFLIGHT DECK L/H SIDE WINDSHIELD SIDE POST HAS CRACK BOTH INBOARD AND OUT BOARD SIDE OF UPPER MOST BARREL NUT LOCATION.VISIBLE. (C-CHECK RO 1/19/2024) REMOVED AND REPLACED FLIGHT DECK L/H SIDE WINDSHIELD SIDE POST WITH NEW REF. CRJ 700 SRM 51-42-21-001-00Nov 25, 2023 · N740SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2024012200055Skin · dentedMULTIPLE DENTS, NICKS AND GOUGES ON AFT FUSELAGE FROM FS1000 TO FS1051, BETWEEN STRINGERS 21R-27 (C-CHECK RO 1/19/2024) REMOVED DAMAGED AREAS ON FUSELAGE SKIN BETWEEN FS1000 - FS1051, STGR21R - STGR27 REF CRJ700 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OFNov 22, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA20240122115Plate · corrodedFORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE FORWARD JOINT PLATE, FS533.00, HAS CORROSION AROUND FASTENERS. (MARKED) (C-CHECK RO 1/19/2024) REMOVED & REPLACED FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE FORWARD JOINT PLATE, AT FS533.00 REF CRJ700 SRM 51-4Nov 15, 2023 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20230122114Repair · corrodedBOTH REPAIR PLATES UNDER SS PLATE ARE CORRODED. FS969.00 - FS989.00 STGR27. (MARKED) (C-CHECK RO 1/19/2024) EVALUATED. NO ALLOWABLE LIMITS FOR DAMAGE ON PREVIOUS REPAIR. REF CRJ700 SRM 51-13-02-001-001-A01. REMOVED AND INSTALLED NEW 1EA BOTTOM DOUBLER, 1 Nov 14, 2023 · N740SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA20231027006Unknown · leakingLOCATION AMARILLO TX. DIVERTED.LOSS OF HYD2. ALL FLUID GONE. (FLIGHT 4957 FILED OPEN)Oct 26, 2023 · N740SK · Cndair CL6002C10 · Hydraulic System, MainSDR SWIA202310190009Unknown · dentedTRANSFER FROM EAML 1225301 : REF EAML 1225150 FOR DENT FOUND AT FS1015.00 - FS1031.00AND BETWEEN STRINGER 24L-25L MEASURING 0.016D" X 4.00L" X 3.50W" WITH SMOOTH CREASE. DENT IS IS 0.075" FROM STRG 24L RIVET CENTER LINE. (FILED CLOSED)REPAIRED FUSELAGE SKIN BEOct 9, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2023F00185Unknown · crackedR/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO RH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DAJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWI2023F00184Unknown · crackedR/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO RH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DAJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWI2023F00189Unknown · crackedL/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO LH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DAJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWIA20230821620Unknown · crackedL/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO LH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DAJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWI2023F00183Unknown · crackedR/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO RH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATEJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWI2023F00182Unknown · crackedR/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO RH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATEJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWI2023F00181Unknown · crackedL/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO LH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATEJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWIA2023081620Unknown · crackedL/H FWD DRAG ANGLE IS CRACKED ON AFT END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED OPEN)COMPLIED WITH REPAIRS TO LH FWD VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATEJun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/RibSDR SWIA20230412Unknown · chafedRH AILERON OUTBOARD PCU LUGS HAVE CHAFING DAMAGE. (FILED CLOSED) REPLACED RH AILERON WITH NEW SERVICABLE UNIT IN REFERENCE TO MIP TASK CARD 27-900-1001-SKY CAL TOOLS USED TORQUE WRENCH S/N: 0917103017CAL DUE: 6-30-2023SAFETY CABLE GUN CApr 12, 2023 · N740SK · Cndair CL6002C10 · Wing StructureSDR SWIA202303310028Unknown · damagedTRANSFER FROM EAML 1110834 : DESCENDING THROUGH FL200 LH SIDE WINDSCREEN OUTSIDE PLY SHATTERED. RAN QRH. (FILED CLOSED)REMOVED, AND REPLACED LH WINDSHIELD AS REQUIRED REF AMM AMM 56-11-01 SEE CARD 56-220-1000-SKY NO LEAKS NOTED OPS CHECKS GOOD.Mar 28, 2023 · N740SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2023010567073Cabin Pressure · malfunctionedRECEIVED CABIN ALT WARNING MESSAGE DURING CLIMB OUT. CAB ALTITUDE REACHED 10,000FT. PERFORMED QRH PROCEDURES AND RETURNED TO LAX. PERFORMED CPC TEST IN THE MDC TEST PASSED PRESSURIZED AIRCRAFT PER AMM 21-31-00-910-801 PRESSURIZATION CHECKS GOOD ON THE GROJan 1, 2023 · N740SK · Cndair CL6002C10 · Cabin Pressure Control SystemSDR SWIA202266614None · corrodedDURING REMOVAL OF WASTE TANK LOWER DRAIN TUBE, FOUND CORROSION DAMAGE TO LAV WASTE SERVICING SURROUND STRUCTURE (FOR REFERENCE SEE SRM 53-51-23), DAMAGE IS BETWEEN FS953.00 AND 969.00 AND BETWEEN STR23R AND STR24R. (FILED CLOSED) STRUCTURAL REPAIR - COMPLISep 6, 2022 · N740SK · Cndair CL6002C10 · Water and Waste SystemSDR SWIA2020032749471Angle · corrodedEXTERNAL SUPPORT STRUCTURE AFT WING TO FUSELAGE FAIRING FS939.00 ANGLE IS CORRORED (AS MARKED) (C-CHECK) RO 3/25/2020 REMOVED AND REPLACED NEW ANGLE P/N SH670-39189-1 AT EXTERNAL SUPPORT STRUCTURE AFT WING TO FUSELAGE FAIRING FS932.00 REF CRJ700 SRM.Mar 7, 2020 · N740SK · Cndair CL6002C10 · Aerodynamic FairingsSDR SWIA2020032749457Angle · crackedANGLE CRACKED INSIDE OF RBL 12 FLOOR BEAM AFT INSIDE ANGLE AT FS280 (C-CHECK) RO 3/25/2020 REMOVED AND INSTALLED NEW ANGLE INSIDE RBL12 FLOORBEAM AFT INSIDE ANGLE AT FS280 REF-CRJ-700 SRM & DWG.Mar 5, 2020 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020032749456Stringer · damagedPERFORM REPAIR OF FS453.00 @ STGR16R FOR REMOVAL OF STGR19R (C-CHECK) RO 3/25/2020 PERFORMED REPAIR OF FS453 AT STGR16R FOR REMOVAL OF STGR19R REF CRJ-700 SRM AND REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOODMar 3, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020032749455Stringer · damagedPERFORM REPAIR OF FS469.00 @ STGR16R FOR REMOVAL OF STGR19R (C-CHECK) RO 3/25/2020 PERFORMED REPAIR OF FS469.00 @ STGR16R REF-CRJ-700 BOMBARDIER REO, LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.Mar 3, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020032749454Stringer · corrodedCORROSION ON STRINGER 19R BETWEEN FS 364 - 379 AS MARKED (C-CHECK) RO 3/25/2020 REPLACED STRINGER AT STGR19R BETWEEN FS349 - FS3477 REF CRJ-700 SRM, DWG. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**). LEAK CHECK GOODFeb 26, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020032749445Stringer · corrodedSTGR26R JOINT PIECE IS CORRODED AFT OF FS333.00 (C-CHECK) RO 3/25/2020 STGR 26R JOINT PIECE HAS INTERGRANULAR CORROSION NEAR FASTENER HOLES OUT OF LIMITS REF CRJ 700 SRM. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE STGR 26R FS333 REF CRJ 700 SRM AND DWFeb 23, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020032749473Angle · corroded4EA ANGLES ON SERVICE DOOR LOWER SILL ATTACHED TO FLOOR WEB PROTECTOR CORRODED FROM FS310 TO FS349 (C-CHECK) RO 3/25/2020 4EA ANGLES ON SERVICE DOOR LOWER SILL ATTACHED TO FLOOR WEB PROTECTOR OUT OF LIMITS FROM FS310 TO FS349 REF CRJ 700 SRM. REMOVED AND Feb 22, 2020 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020032749444Angle · corrodedSERVICE DOOR MID CAP ANGLE CORRODED (C-CHECK) RO 3/25/2020 SERVICE DOOR MID CAP ANGLE OUT OF LIMITS REF- CRJ-700 SRM. REMOVED AND INSTALLED NEW SERVICE DOOR MID CAP ANGLE REF CRJ 700 SRM.Feb 22, 2020 · N740SK · Cndair CL6002C10 · Service DoorsSDR SWIA2020032749443Angle · corrodedPASSENGER DOOR AFT CAP ANGLE HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 PASSENGER DOOR AFT CAP ANGLE WAS REMOVED AND NEW ONE INSTALLED, PER REF CRJ-700 SRM, BOMBARDIER DRAWING.Feb 22, 2020 · N740SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020032749442Angle · corrodedPASSENGER DOOR MID CAP ANGLE HAS EVIDENCE OF CORROSION (C-CHECK) RO 3/25/2020 PASSENGER DOOR MID CAP ANGLE WAS REMOVED AND NEW ONE INSTALLED, PER REF CRJ-700 SRM, DRAWING.Feb 22, 2020 · N740SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020032749470Seat Track · corroded*RIGHT HAND SIDE SEAT RAIL FS861.00 €“ FS969 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM FS861 TO FS969 CORROSION OUT OF LIMITS. SEE JOB 710196114 OP 61 MX TRANS# 20496830 FOR EVALUATION. REMOVED FABRICATED AND REPLACED WITH NEW RH SIDE SFeb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749469Seat Track · corroded*RIGHT HAND SIDE SEAT RAIL FS785.00 - FS861.00 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM APROX TO FS785.00 TO FS861.00 CORROSION OUT OF LIMITS. SEE JOB 710196114 OP 61 MX TRANS# 20496830 FOR EVALUATION. REMOVED FABRICATED AND REPLACED WITFeb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749468Seat Track · corroded*LEFT HAND SIDE SEAT RAIL FS713.00 €“ 761.85 IS CORRODED. (C-CHECK) RO 3/25/2020 LH SIDE SEAT RAIL FROM APROX TO FS713.00 TO FS761.00 CORROSION OUT OF LIMITS. SEE JOB 710196114 OP 60 MX TRANS# 20496818 FOR EVALUATION AND FABRICATION. REMOVED AND REPLACEFeb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749467Seat Track · corroded*LEFT HAND SIDE SEAT RAIL FS675.00-713.00 IS CORRODED. (C-CHECK) RO 3/25/2020 LH SIDE SEAT RAIL FROM APROX FS675.00 TO FS713.00 EVALUATED AND FABRICATED ON JOB 710196114 OP 60 MX TRANS# 20496818 INSTALLED NEW LH SIDE SEAT RAIL FROM APROX FS675.00 TO FS7Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749466Seat Track · corroded*RIGHT HAND SIDE SEAT RAIL FS713.00 €“ 761.85 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM APROX FS713.00 TO FS761.85 CORROSION FOUND TO BE OUT OF LIMITS. REF CRJ700 SRM. REMOVED AND FABRICATED NEW REPLACEMENT PART. REF CRJ700 AMM AND CRFeb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749465Seat Track · corroded*RIGHT HAND SIDE SEAT RAIL FS675.00-713.00 IS CORRODED. (C-CHECK) RO 3/25/2020 RH SIDE SEAT RAIL FROM APROX FS675 TO FS 713 CORROSION FOUND TO BE OUT OF LIMITS. REF CRJ700 SRM. REMOVED AND FABRICATED NEW REPLACEMENT PART. REF CRJ700 AMM AND CRJ700 SRM. Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020032749441Skin · gouged*TWO DENTS WITH A GOUGE AND MULTIPLE GOUGES IN EXTERNAL SKIN. FS1031.00 €“ FS1051.00 STGR22R €“ STGR26R. (C-CHECK) RO 3/25/2020 DRESSED BACK DENTS AND BLENDED MULTIPLE GOUGES IN THE EXTERNAL SKIN AT FS1031.00 €“ FS1051.00 STGR22R €“ STGR26R. ALL REWORKFeb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
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