# Service difficulty reports: N740SK

A list on [N740SK](https://openairdocs.org/aircraft/N740SK.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 4 · 194 reports

- [SDR SWIA2024012219](https://openairdocs.org/sdr/SWIA2024012219.md): Track · damaged · Dec 19, 2023 · N740SK · Cndair CL6002C10 · Wing Miscellaneous Structure
  > DRILL 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, INST
- [SDR SWI2024F00011](https://openairdocs.org/sdr/SWI2024F00011.md): Skin · corroded · Nov 30, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FS801 - 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
- [SDR SWI2024F00010](https://openairdocs.org/sdr/SWI2024F00010.md): Skin · gouged · Nov 30, 2023 · N740SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > GOUGE 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 FOR
- [SDR SWIA20231130](https://openairdocs.org/sdr/SWIA20231130.md): Skin · corroded · Nov 30, 2023 · N740SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FS801 - 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-
- [SDR SWI2024F00009](https://openairdocs.org/sdr/SWI2024F00009.md): Floorbeam · cracked · Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > POSSIBLE 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 PER
- [SDR SWI2024F00008](https://openairdocs.org/sdr/SWI2024F00008.md): Floorbeam · corroded · Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOOR 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 CRJ
- [SDR SWI2024F00007](https://openairdocs.org/sdr/SWI2024F00007.md): Floorbeam · cracked · Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT 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 WITH
- [SDR SWI2024F00006](https://openairdocs.org/sdr/SWI2024F00006.md): Floorbeam · corroded · Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > L/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. COM
- [SDR SWI2024F00005](https://openairdocs.org/sdr/SWI2024F00005.md): Floorbeam · corroded · Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Floor Panel
  > L/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. CO
- [SDR SWI2024F00004](https://openairdocs.org/sdr/SWI2024F00004.md): Floorbeam · cracked · Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > POSSIBLE 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-A01
- [SDR SWIA2023012200129](https://openairdocs.org/sdr/SWIA2023012200129.md): Floorbeam · cracked · Nov 29, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT 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-S
- [SDR SWI2024F00003](https://openairdocs.org/sdr/SWI2024F00003.md): Floorbeam · cracked · Nov 28, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > POSSIBLE 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 COM
- [SDR SWI2024F00002](https://openairdocs.org/sdr/SWI2024F00002.md): Floorbeam · corroded · Nov 28, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOOR 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
- [SDR SWI2024F00001](https://openairdocs.org/sdr/SWI2024F00001.md): Bracket · cracked · Nov 28, 2023 · N740SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > R/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-SKY
- [SDR SWIA2023012200128](https://openairdocs.org/sdr/SWIA2023012200128.md): Floor Support · cracked · Nov 28, 2023 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > POSSIBLE 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 C
- [SDR SWIA20230122125](https://openairdocs.org/sdr/SWIA20230122125.md): Windshield · cracked · Nov 25, 2023 · N740SK · Cndair CL6002C10 · Flight Compartment Windows
  > FLIGHT 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 51-42-21-001-00
- [SDR SWIA2024012200055](https://openairdocs.org/sdr/SWIA2024012200055.md): Skin · dented · Nov 22, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MULTIPLE 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 OF
- [SDR SWIA20240122115](https://openairdocs.org/sdr/SWIA20240122115.md): Plate · corroded · Nov 15, 2023 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD 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 51-4
- [SDR SWIA20230122114](https://openairdocs.org/sdr/SWIA20230122114.md): Repair · corroded · Nov 14, 2023 · N740SK · Cndair CL6002C10 · Fuselage Structure (General)
  > BOTH 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
- [SDR SWIA20231027006](https://openairdocs.org/sdr/SWIA20231027006.md): Unknown · leaking · Oct 26, 2023 · N740SK · Cndair CL6002C10 · Hydraulic System, Main
  > LOCATION AMARILLO TX. DIVERTED.LOSS OF HYD2. ALL FLUID GONE. (FLIGHT 4957 FILED OPEN)
- [SDR SWIA202310190009](https://openairdocs.org/sdr/SWIA202310190009.md): Unknown · dented · Oct 9, 2023 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TRANSFER 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 BE
- [SDR SWI2023F00185](https://openairdocs.org/sdr/SWI2023F00185.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > R/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 --, DA
- [SDR SWI2023F00184](https://openairdocs.org/sdr/SWI2023F00184.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > R/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 --, DA
- [SDR SWI2023F00189](https://openairdocs.org/sdr/SWI2023F00189.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > L/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 --, DA
- [SDR SWIA20230821620](https://openairdocs.org/sdr/SWIA20230821620.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > L/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 --, DA
- [SDR SWI2023F00183](https://openairdocs.org/sdr/SWI2023F00183.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > R/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 --, DATE
- [SDR SWI2023F00182](https://openairdocs.org/sdr/SWI2023F00182.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > R/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 --, DATE
- [SDR SWI2023F00181](https://openairdocs.org/sdr/SWI2023F00181.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > L/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 --, DATE
- [SDR SWIA2023081620](https://openairdocs.org/sdr/SWIA2023081620.md): Unknown · cracked · Jun 20, 2023 · N740SK · Cndair CL6002C10 · Vertical Stabilizer, Spar/Rib
  > L/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 --, DATE
- [SDR SWIA20230412](https://openairdocs.org/sdr/SWIA20230412.md): Unknown · chafed · Apr 12, 2023 · N740SK · Cndair CL6002C10 · Wing Structure
  > RH 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 C
- [SDR SWIA202303310028](https://openairdocs.org/sdr/SWIA202303310028.md): Unknown · damaged · Mar 28, 2023 · N740SK · Cndair CL6002C10 · Flight Compartment Windows
  > TRANSFER 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.
- [SDR SWIA2023010567073](https://openairdocs.org/sdr/SWIA2023010567073.md): Cabin Pressure · malfunctioned · Jan 1, 2023 · N740SK · Cndair CL6002C10 · Cabin Pressure Control System
  > RECEIVED 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 GRO
- [SDR SWIA202266614](https://openairdocs.org/sdr/SWIA202266614.md): None · corroded · Sep 6, 2022 · N740SK · Cndair CL6002C10 · Water and Waste System
  > DURING 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 - COMPLI
- [SDR SWIA2020032749471](https://openairdocs.org/sdr/SWIA2020032749471.md): Angle · corroded · Mar 7, 2020 · N740SK · Cndair CL6002C10 · Aerodynamic Fairings
  > EXTERNAL 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.
- [SDR SWIA2020032749457](https://openairdocs.org/sdr/SWIA2020032749457.md): Angle · cracked · Mar 5, 2020 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE 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.
- [SDR SWIA2020032749456](https://openairdocs.org/sdr/SWIA2020032749456.md): Stringer · damaged · Mar 3, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PERFORM 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 GOOD
- [SDR SWIA2020032749455](https://openairdocs.org/sdr/SWIA2020032749455.md): Stringer · damaged · Mar 3, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PERFORM 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.
- [SDR SWIA2020032749454](https://openairdocs.org/sdr/SWIA2020032749454.md): Stringer · corroded · Feb 26, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 GOOD
- [SDR SWIA2020032749445](https://openairdocs.org/sdr/SWIA2020032749445.md): Stringer · corroded · Feb 23, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR26R 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 DW
- [SDR SWIA2020032749473](https://openairdocs.org/sdr/SWIA2020032749473.md): Angle · corroded · Feb 22, 2020 · N740SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > 4EA 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
- [SDR SWIA2020032749444](https://openairdocs.org/sdr/SWIA2020032749444.md): Angle · corroded · Feb 22, 2020 · N740SK · Cndair CL6002C10 · Service Doors
  > SERVICE 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.
- [SDR SWIA2020032749443](https://openairdocs.org/sdr/SWIA2020032749443.md): Angle · corroded · Feb 22, 2020 · N740SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER 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.
- [SDR SWIA2020032749442](https://openairdocs.org/sdr/SWIA2020032749442.md): Angle · corroded · Feb 22, 2020 · N740SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER 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.
- [SDR SWIA2020032749470](https://openairdocs.org/sdr/SWIA2020032749470.md): Seat Track · corroded · Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *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 S
- [SDR SWIA2020032749469](https://openairdocs.org/sdr/SWIA2020032749469.md): Seat Track · corroded · Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *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 WIT
- [SDR SWIA2020032749468](https://openairdocs.org/sdr/SWIA2020032749468.md): Seat Track · corroded · Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *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 REPLACE
- [SDR SWIA2020032749467](https://openairdocs.org/sdr/SWIA2020032749467.md): Seat Track · corroded · Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *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 FS7
- [SDR SWIA2020032749466](https://openairdocs.org/sdr/SWIA2020032749466.md): Seat Track · corroded · Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *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 CR
- [SDR SWIA2020032749465](https://openairdocs.org/sdr/SWIA2020032749465.md): Seat Track · corroded · Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *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.
- [SDR SWIA2020032749441](https://openairdocs.org/sdr/SWIA2020032749441.md): Skin · gouged · Feb 21, 2020 · N740SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > *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 REWORK

Next page: https://openairdocs.org/aircraft/N740SK/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 = 'N740SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N740SK/reports

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