# Service difficulty reports: N793SK

A list on [N793SK](https://openairdocs.org/aircraft/N793SK.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 2 · 75 reports

- [SDR SWI2025F01467](https://openairdocs.org/sdr/SWI2025F01467.md): Frame · corroded · Sep 2, 2025 · N793SK · Cndair CL6002C10 · Fuselage Main, Frame
  > AFT FUSELAGE - FRAME HAS CORRISON AT FS 1000.00 BETWEEN STRG 25L TO 25R. ACCOMPLISHED REO 670-53-61-2572 FOR REPAIR BLENDED CORROSION DAMAGE TO FS 1000 LOWER FRAME SECTOR BETWEEN STRG 26L/H TO STRG 25 R/H. TASK CARD 53-900-1002-SKY CIMPLETED.
- [SDR SWIA2025110300902](https://openairdocs.org/sdr/SWIA2025110300902.md): Frame · corroded · Sep 2, 2025 · N793SK · Cndair CL6002C10 · Fuselage Main, Frame
  > AFT FUSELAGE - FRAME HAS CORROSION AT FS 863.00 BETWEEN STRG 25L TO STRG 25R. REMOVED AND INSTALLED NEW FRAME AT FS. 863.00 BETWEEN STRG 20 R/H TO STRG 20 LT. IAW SRM 51-42-06, SRM 51-42-21 NO FURTHER ACTION IS REQUIRED, JOB COMPLETED.
- [SDR SWI2025F01469](https://openairdocs.org/sdr/SWI2025F01469.md): Roller · out of limits · May 7, 2025 · N793SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 RH - DISCARD THE RH SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3 (REQUIRES QTY 2 OF PN CC670-12567-1). REMOVE AND REPLACE IAW TASK CARD 27-630-824 (MRB 27-81-43-713), PART NUMB
- [SDR SWI2025F01468](https://openairdocs.org/sdr/SWI2025F01468.md): Roller · out of limits · May 7, 2025 · N793SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 LH - DISCARD THE LH SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3 (REQUIRES QTY 2 OF PN CC670-12567-1). REMOVE AND REPLACE IAW TASK CARD 27-530-824 (MRB 27-81-43-713), PART NUMB
- [SDR SWIA2025110300507](https://openairdocs.org/sdr/SWIA2025110300507.md): Slat Track · out of limits · May 7, 2025 · N793SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 700 RH - DISCARD THE RH SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2 (P/N CC670-12272-1 OR PN YR1319). REMOVE AND REPLACE IAW TASK CARD 27-630-809 (MRB 27-81-43-717), PART NUMBER: -, SERIA
- [SDR SWIA202312260025](https://openairdocs.org/sdr/SWIA202312260025.md): Unknown · smoke · Dec 25, 2023 · N793SK · Cndair CL6002C10 · Air Distribution System
  > DUE TO SMOKE IN THE CABIN REPORTED ENGINE BOROSCPE REQUIRED. SMOD RTS APPROVAL REQUIREDMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5506 - FILED CLOSED) DEC 25, 2023 STATION: SFO--PERFORMED T/S IN REF TO FIM 21-22-00 FOR SMOKE EVENT REPORTED IN AFT CABIN
- [SDR SWIA202266907](https://openairdocs.org/sdr/SWIA202266907.md): Skin · damaged · Oct 17, 2022 · N793SK · Cndair CL6002C10 · Wing, Plate/Skin
  > DURING INTERNAL INSPECTION OF RH WING FIXED LEADING EDGE SKIN PANEL - DAMAGE WAS FOUND ON RIB AT RHS WING LEADING EDGE SS90.89 (PN CC670-12206-4) / CLASSIFIED AS MAJOR REPAIR - FORM M-337 INITIATED - REF CP 25702443 FOR EVALUATION (FILED OPEN) REMOVED A
- [SDR SWIA202266609](https://openairdocs.org/sdr/SWIA202266609.md): Tire · out of limits · Oct 12, 2022 · N793SK · Cndair CL6002C10 · Tire
  > DAMAGE EVALUATED ON RHS STGR 15A MEASURING 4" FROM FS 229.00-FS236.00. PERFORMED GVI OF TORQUE LINKS IAW AMM 32-21-10 AND FOUND TEE HANDLE BROKEN & DAMAGE TO UPPER & LOWER TORQUE LINKS IAW AML 1034698. PERFORMED GVI OF NLG IAW AMM 32-20-00, NO DEFECTS NOTE
- [SDR SWIA202266577](https://openairdocs.org/sdr/SWIA202266577.md): Frame · deformed · Sep 29, 2022 · N793SK · Cndair CL6002C10 · Fuselage Main, Frame
  > DAMAGE EVALUATED ON RH FUSELAGE DEFORMED FRAME MEASURING 7.0"L FROM FS229.00 - FS236.00. THIS HAS BEEN CLASSIFIED AS A MAJOR REPAIR. REMOVED AND REPLACED RT FRAME AT FS 235 IN REFERENCE TO DWG CC670-33030, DWG CC670-33015 REV G, SRM 51-42-06-001-001-A01, PC
- [SDR SWIA202266576](https://openairdocs.org/sdr/SWIA202266576.md): Stringer · damaged · Sep 29, 2022 · N793SK · Cndair CL6002C10 · Fuselage Structure (General)
  > DAMAGE EVALUATED ON RH SIDE STGR 14A P/N: CC670-33164-6, DEFORMED DAMAGE STGR 14A LOCATED AT FS229.00-FS236.00 MEASURING 6.0"L AND A DENT ON STGR 14A LOCATED AT FS247.00-FS250.00 MEASURING 3.0"L. THIS HAS BEEN CLASSIFIED AS A MAJOR REPAIR. REMOVED AND RE
- [SDR SWIA202266575](https://openairdocs.org/sdr/SWIA202266575.md): Skin · dented · Sep 29, 2022 · N793SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DAMAGE EVALUATED ON RH FWD FUSELAGE PANEL P/N: CC670-33101-4, DENT 1 AT FS226.00- FS239.00 MEASURING 13.0"L X6.0"W X 0.375"D AND DENT 2 WITH A CREASE DAMAGE LOCATED AT FS247.00-FS250.00 MEASURING 3.0"L X 4.5"W X 0.10"D.THIS HAS BEEN CLASSIFIED AS A MAJOR REPAI
- [SDR SWIA202266906](https://openairdocs.org/sdr/SWIA202266906.md): Skin · dented · Sep 25, 2022 · N793SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DAMAGE ASSESSMENT OF EXTERIOR STRUCTURE, NOTICED TWO DENTS IN THE RVSM AREA ON THE FWD RH FUSELAGE PANEL. LOCATED BS 194.5, ABOVE S16R. 1.125 X.5 ?W X.013 ?D. JUST FORWARD OF PRESSURE BULKHEAD AT BS 202, 2 ?L X 1.375 ?W X.020 ?D. R & R RT FUSELAGE P
- [SDR SWIA202161789](https://openairdocs.org/sdr/SWIA202161789.md): None · cracked · Oct 17, 2021 · N793SK · Cndair CL6002C10 · Window/Windshield System
  > LEFT WINDSHIELD STARTED STARTED ARCING ON THE BOTTOM EDGE. SHORTLY AFTER THIS THE OUTER LAYER CRACKED IN A WEB-LIKE PATTERN ACROSS THE ENTIRE SURFACE. (FLIGHT 5219 - FILED CLOSED) REMOVED AND REPLACED CA WINDSHIELD, OPS CHECKS GOOD, LEAK CHECK GOOD. REF
- [SDR SWIA202158155](https://openairdocs.org/sdr/SWIA202158155.md): Skin · dented · May 16, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 636913: TRANSFERRED FROM CAMP 22790038. 1-OFF DENT WITH GOUGE ON THE FUSELAGE SKIN BETWEEN 43.75% MID SPAR / DATUM - 55.63% AND BETWEEN STR15R-STR17R (DWG MM670-38101, AL 2024-T42, 0.080" NOMINAL / THK, 0.050" AND 0.045" CHEM-MILL POCKET TH
- [SDR SWIA202156515](https://openairdocs.org/sdr/SWIA202156515.md): Strap · corroded · Feb 12, 2021 · N793SK · Cndair CL6002C10 · Aerodynamic Fairings
  > EVALUATE CORROSION ON STRAP L/H OUTBOARD FOR FRAME AT FS 909 FOR WING TO FUSELAGE PANEL 196DL (C-CHECK) RO 2/28/2021 REMOVED AND REPLACED STRAP WITH NEW FROM STOCK REF CRJ-700 SRM 51-42-06-001-001-A01
- [SDR SWIA202156495](https://openairdocs.org/sdr/SWIA202156495.md): Stringer · chafed · Feb 12, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > R/H PAC WATER LINE CHAFED THROUGH STR 7R BETWEEN FS 1144-1162 DUE TO 2 BROKEN SUPPORT BRACKETS. (MARKED) (C-CHECK) RO 2/28/2021 COMPLIED WITH REPAIR OF STRINGER 7R REF MHIRJ REO 670-53-61-1827 REV -- DATED 2021-02-13, DRAWING MM670-35006 REV AJ AND CRJ-700
- [SDR SWIA202156494](https://openairdocs.org/sdr/SWIA202156494.md): Coaming · chafed · Feb 12, 2021 · N793SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RH UPPER TRANSCOWL DOOR COAMING IS CHAFED (C-CHECK) RO 2/28/2021 INSTALLED NEW R/H UPPER TRANSCOWL DOOR COAMING P/N CN624-2061-205 REF REO 670-54-21-1207 REV A DATED 2015-08-27, COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA202156490](https://openairdocs.org/sdr/SWIA202156490.md): Structure · cracked · Feb 4, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Structure
  > COMPLY WITH SB 670BA-53-040 FOR STR 3L AT 280 LINTEL CRACK (C-CHECK) RO 2/28/2021 COMPLIED WITH STRINGER REPAIR REF SB 670BA-53-040 REV C DATED 09/20/2012 AND REO 670-53-21-493 REV D DATED 2015-07-10 / "SERVICE BULLETIN 670BA-53-040, REVISION C, FUSELAGE -
- [SDR SWIA202156489](https://openairdocs.org/sdr/SWIA202156489.md): Angle · corroded · Feb 4, 2021 · N793SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > NESTING ANGLE ON LOWER FRAME AT FS879 HAS CORROSION (C-CHECK) RO 2/28/2021 REMOVED OUT OF LIMITS NESTING ANGLE AND INSTALLED NEW SERVICEABLE NESTING ANGLE AT FS879.00 LOWER FRAME SECTOR BETWEEN STGR 20L AND STGR 20R REF CRJ700 SRM 51-42-06-001-001-A01, CR
- [SDR SWIA202156517](https://openairdocs.org/sdr/SWIA202156517.md): Fitting · broken · Jan 30, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > BROKEN BULKHEAD FITTING ASSEMBLY AT LBL9.00 FS 991.75 REQUIRES REPLACEMENT. / P/N: CDSP1900-509. (C-CHECK) RO 2/28/2021 REPLACED BULKHEAD FIITTING ASSY AT LBL 9 AT FS 991.75 REF. CRJ 700 SRM 51-41-02-001-001-A01
- [SDR SWIA202156516](https://openairdocs.org/sdr/SWIA202156516.md): Fitting · broken · Jan 30, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > BROKEN BULKHEAD FITTING ASSEMBLY AT LBL9.00 FS 967.50 REQUIRES REPLACEMENT. / P/N: CDSP1900-501. (C-CHECK) RO 2/28/2021 REPLACED BULKHEAD FITTING ASSEMBLY ON LBL 9 AT FS 967.50 REF CRJ 700 SRM 51-41-02-001-001-A01
- [SDR SWIA202156514](https://openairdocs.org/sdr/SWIA202156514.md): Strap · corroded · Jan 30, 2021 · N793SK · Cndair CL6002C10 · Aerodynamic Fairings
  > EVALUATE CORROSION ON STRAP R/H OUTBOARD FOR FRAME AT FS 909 FOR WING TO FUSELAGE PANEL 196DR (C-CHECK) RO 2/28/2021 INSTALLED NEW STRAP. P/N: SH670-39341-3 REF DRAWING SH670-39240 REV NC. INSTALLED RIVETS PER CRJ700 SRM TASK 51-42-06-001-001-A01
- [SDR SWIA202156513](https://openairdocs.org/sdr/SWIA202156513.md): Strap · corroded · Jan 30, 2021 · N793SK · Cndair CL6002C10 · Aerodynamic Fairings
  > EVALUATE CORROSION ON STRAP MID TO FS909 FOR WING TO FUSELAGE PNLS (C-CHECK) RO 2/28/2021 INSTALLED NEW STRAP. P/N: SH670-39338-3 REF DRAWING SH670-39240-M05 REV NC. INSTALLED RIVETS PER CRJ700 SRM TASK 51-42-06-001-001-A01
- [SDR SWIA202156512](https://openairdocs.org/sdr/SWIA202156512.md): Fitting · corroded · Jan 25, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > 2 EA FITTINGS ON FWD SIDE OF FS893.00 @ STGR27 ARE CORRODED (C-CHECK) RO 2/28/2021 REPAIRED 2 EA FITTINGS ON THE FWD SIDE OF FS 893.00 AT STR27 PER REO 670-53-41-509 REV -- DATED 2021-02-08
- [SDR SWIA2021030256487](https://openairdocs.org/sdr/SWIA2021030256487.md): Stinger · corroded · Jan 25, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Keel
  > STGR26R IS CORRODED FROM FS985.00 TO FS1051.00 (C-CHECK) RO 2/28/2021 REPLACED STRINGER 26R BETWEEN FS977 AND FS1098 REF DWG #SH670-37060 REV E, CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND C/W SKYWEST TASK CARD NO. 51-900-1002-SK
- [SDR SWIA202156511](https://openairdocs.org/sdr/SWIA202156511.md): Seat Track · corroded · Jan 23, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, LBL 9, BETWEEN FS863 AND FS1000 HAS CORROSION IN MULTIPLE MARKED LOCATIONS. (C-CHECK) RO 2/28/2021 REPLACED SEAT TRACK WITH NEW REF CRJ-700 AMM 53-00-49-400-801-A03
- [SDR SWIA202156510](https://openairdocs.org/sdr/SWIA202156510.md): Seat Track · corroded · Jan 23, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, RBL 9, BETWEEN FS863 AND FS985 HAS CORROSION IN MULTIPLE MARKED LOCATIONS. (C-CHECK) RO 2/28/2021 REPLACED SEAT TRACK WITH NEW REF CRJ-700 AMM 53-00-49-400-801-A03
- [SDR SWIA2021030256486](https://openairdocs.org/sdr/SWIA2021030256486.md): Frame · corroded · Jan 23, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME, FS879, BETWEEN STGR 24R AND STGR 24L HAS CORROSION (MARKED) (C-CHECK) RO 2/28/2021 REPLACED FRAME SECTION 879.00 REF DWG SH670-37060 REV G, CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900
- [SDR SWIA202156498](https://openairdocs.org/sdr/SWIA202156498.md): Elbow · cracked · Jan 22, 2021 · N793SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR HARNESS ELBOW APPEARS CRACKED. (C-CHECK) RO 2/28/2021 REMOVED AND REPLACED PAX DOOR HARNESS ELBOW IAW CRJ700 AMM 52-11-00-000-802-A01 & 52-11-00-400-802-A01. SYSTEM CHECKS GOOD IAW CRJ700 AMM 52-70-04-710-801-A01
- [SDR SWIA2021030256485](https://openairdocs.org/sdr/SWIA2021030256485.md): Stinger · corroded · Jan 22, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION NOTED ON STGR 26R BETWEEN FS 953.00 AND FS 969.00. (C-CHECK) RO 2/28/2021 STRINGER 26R HAS INTERGRANULAR AND EXFOLIATION CORROSION. NO DAMAGE ALLOWED AT THIS LOCATION REF CRJ 700 SRM 53-51-03-101-003-A01. STRINGER IS OUT OF LIMITS. CUT OUT DAM
- [SDR SWIA2021030256484](https://openairdocs.org/sdr/SWIA2021030256484.md): Stinger · corroded · Jan 22, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION NOTED ON STGR 26L BETWEEN FS 953.00 AND FS 969.00. (C-CHECK) RO 2/28/2021 REPAIRED STRINGER 26L REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND CRJ-700 SRM 53-00-03-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-10
- [SDR SWIA202156497](https://openairdocs.org/sdr/SWIA202156497.md): Fuel Tank · cracked · Jan 21, 2021 · N793SK · Cndair CL6002C10 · Fuel Storage
  > LH WING, INSIDE THE FUEL TANK, SUPSECT CRACK ON THE SLAT TRACK 1-3 CANNISTER AFT ATTACH FLANGE NEAR THE WELD (MARKED). (C-CHECK) RO 2/28/2021 COMPLIED WITH REPAIR OF LH WING 1-3 SLAT TRACK CANNISTER REF BOMBARDIER REO 670-57-42-577 REV -- DATED 2016-12-02.
- [SDR SWIA202156509](https://openairdocs.org/sdr/SWIA202156509.md): Floorbeam · corroded · Jan 20, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFT CARGO UNDER FLOOR FRAME AT F.S.969.00 HAS CORROSION BETWEEN STR. 25L AND 25R (MARKED) (C-CHECK) RO 2/28/2021 COMPLIED WITH APPLICABLE STEPS 1 TO 4 OF MHI RJ REO 670-53-51-200 REV --,DATED 2021-02-05. FOR REMAINING STEPS 5 TO 9 SEE MX TRANS NO 22231073
- [SDR SWIA202156483](https://openairdocs.org/sdr/SWIA202156483.md): Slider · damaged · Jan 20, 2021 · N793SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RH UPPER TRANS COWL I/B NYLON TRACK SLIDER FORWARD MOUNTING HOLE ELONGATED. (C-CHECK) RO 2/28/2021 REPAIRED ELONGATED HOLE AT FORWAR MOUNTING LOCATION FOR RH UPPER TRANS COWL I/B NYLON SLIDER. COMPLIED WITH ALL STEPS OF THE REPAIR. REF BOMBARDIER REO 670-7
- [SDR SWIA202156508](https://openairdocs.org/sdr/SWIA202156508.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK FROM F.S.581.00 TO F.S.677.00 CORRODED IN MULTIPLE SPOTS (MAKRED). (C-CHECK) RO 2/28/2021 INSTALLED NEW SEAT RAIL RH FS581.00-FS677.00 IAW 53-00-49-400-801-A03. TORQUE WITH SCREW GUN ID# MATC1352 DATE 24 JUNE 20 DUE 30 JUNE 21.
- [SDR SWIA202156507](https://openairdocs.org/sdr/SWIA202156507.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK FROM F.S.485.00 TO F.S.581.00 CORRODED IN MULTIPLE SPOTS (MAKRED). (C-CHECK) RO 2/28/2021 INSTALLED NEW SEAT RAIL RH FS485.00-FS581.00 IAW 53-00-49-400-801-A03. TORQUE WITH SCREW GUN ID NO MATC1352 DATE 24V JUEN 20 DUE 30 JUNE 21.
- [SDR SWIA202156506](https://openairdocs.org/sdr/SWIA202156506.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK FROM F.S.349.00 TO F.S.485.00 CORRODED IN MULTIPLE SPOTS (MAKRED). (C-CHECK) RO 2/28/2021 INSTALLED NEW SEAT RAIL FS349.00-FS485.00 IAW 53-00-49-400-801-A03. TORQUE WITH SCREW GUN ID# MATC1352 DATE 24V JUEN 20 DUE 30 JUNE 21.
- [SDR SWIA202156505](https://openairdocs.org/sdr/SWIA202156505.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK FROM F.S.581.00 TO F.S.677.00 CORRODED IN MULTIPLE SPOTS (MAKRED). (C-CHECK) RO 2/28/2021 INSTALLED NEW SEAT RAIL FS581-FS611 IAW 53-00-49-400-801-A03. TORQUE WITH SCREW GUN ID NO MATC1352 DATE 24V JUEN 20 DUE 30 JUNE 21.
- [SDR SWIA202156504](https://openairdocs.org/sdr/SWIA202156504.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK FROM F.S.485.00 TO F.S.581.00 CORRODED IN MULTIPLE SPOTS (MAKRED). (C-CHECK) RO 2/28/2021 INSTALLED NEW SEAT RAIL LH FS485.00-FS581.00 IAW 53-00-49-400-801-A03. TORQUE WITH SCREW GUN ID NO. MATC1352 DATE 24V JUEN 20 DUE 30 JUNE 21.
- [SDR SWIA202156503](https://openairdocs.org/sdr/SWIA202156503.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK FROM F.S.379.00 TO F.S.485.00 CORRODED IN MULTIPLE SPOTS (MAKRED). (C-CHECK) RO 2/28/2021 INSTALLED NEW SEAT RAIL LH FS379.00-FS485.00 IAW 53-00-49-400-801-A03. TORQUE WITH SCREW GUN ID# MATC1352 DATE 24V JUEN 20 DUE 30 JUNE 21.
- [SDR SWIA202156502](https://openairdocs.org/sdr/SWIA202156502.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT EXTRUSION CORRODED AT STR.15L APOX. FS.724.00 (FLAGGED). (C-CHECK) RO 2/28/2021 LH SIDE SEAT EXTRUSION CORROSION REMOVED AT STR.15L APOX. FS.724.00. REF CRJ700 SRM 51-21-06-001-001-A01
- [SDR SWIA202156501](https://openairdocs.org/sdr/SWIA202156501.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT EXTRUSION CORRODED AT STR.15R APOX. FS.708.00 (FLAGGED) (C-CHECK) RO 2/28/2021 REPLACED SEAT TRACK WITH NEW REF CRJ-700 AMM 53-00-49-400-801-A03
- [SDR SWIA202156500](https://openairdocs.org/sdr/SWIA202156500.md): Seat Track · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT TRACK AT STR.15R FROM FS501.00 TO 573.00 CORRODED. (C-CHECK) RO 2/28/2021 REPLACED SEAT TRACK WITH NEW REF CRJ-700 AMM 53-00-49-400-801-A03
- [SDR SWIA202156482](https://openairdocs.org/sdr/SWIA202156482.md): Floor Support · corroded · Jan 19, 2021 · N793SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON R/H FLOOR SILL BETWEEN FS280.00-FS319.70(MARKED) (C-CHECK) RO 2/28/2021 REMOVED AND REPLACED CORRODED RH FLOOR SILL BETWEEN FS280-FS319.70 WITH A NEW ONE REF CRJ700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001
- [SDR SWIA202156499](https://openairdocs.org/sdr/SWIA202156499.md): Angle · corroded · Jan 17, 2021 · N793SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > EVALUATE CORROSION ON SPLICE ANGLE FOR FRAME AT FS 939 FOR WING TO FUSELAGE PNLS. (MARKED) (C-CHECK) RO 2/28/2021 REPLACED ANGLE AT FS 939.00 ON FRAME REF. CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA2021030256481](https://openairdocs.org/sdr/SWIA2021030256481.md): Floor Support · corroded · Jan 16, 2021 · N793SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > PAX DOOR ENTRY WAY, FLOOR SUPPORT MIDDLE CAP ANGLE IS CORRODED. (MARKED) (C-CHECK) RO 2/28/2021 INSTALLED NEW MID CAP ANGLE @PAX DOOR. REF CRJ700 SRM 51-41-00-001-001-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA202156480](https://openairdocs.org/sdr/SWIA202156480.md): Angle · corroded · Jan 16, 2021 · N793SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE, LOWER KICKPLATE ANGLE HAS CORROSION(MARKED). (C-CHECK) RO 2/28/2021 COMPLIED WITH REPLACEMENT OF PAX DOOR SURROUND STRUCTURE LOWER KICKPLATE ANGLE REF CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. COMPLIED WITH SKY
- [SDR SWIA2021030256479](https://openairdocs.org/sdr/SWIA2021030256479.md): Floor Support · corroded · Jan 16, 2021 · N793SK · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT FLOOR SUPPORT ANGLE AT FS280 HAS CORROSION BETWEEN LBL12 AND RBL12 (C-CHECK) RO 2/28/2021 REMOVED CORRODED SUPPORT ANGLE AND INSTALLED NEW FLOOR SUPPORT ANGLE AT FS280 BETWEEN LBL12 AND RBL12 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-00
- [SDR SWIA2021030256478](https://openairdocs.org/sdr/SWIA2021030256478.md): Floorbeam · cracked · Jan 16, 2021 · N793SK · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT FLOORBEAM AT RBL12, AT THE RADIUS OF THE VERTICAL FLANGE ATTACHED AT FS280, HAS THE APPEARANCE OF A POSSIBLE CRACK. (C-CHECK) RO 2/28/2021 REPAIRED COCKPIT FLOORBEAM AT RBL 12, AT THE RADIUS OF THE VERTICAL FLANGE ATTACHED AT FS 280 IAW CRJ 700 SRM
- [SDR SWIA202156519](https://openairdocs.org/sdr/SWIA202156519.md): Cap · dented · Jan 15, 2021 · N793SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT END CAP DENTED (C-CHECK) RO 2/28/2021 PAX DOOR AFT END CAP COVER WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED END CAP COVER P/N 600-31902-288 WITH NEW FASTENERS. REF CRJ 700 SRM 51-42-13-001-001-A01

Next page: https://openairdocs.org/aircraft/N793SK/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 = 'N793SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N793SK/reports

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