# Service difficulty reports: N713SK

A list on [N713SK](https://openairdocs.org/aircraft/N713SK.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 · 190 reports

- [SDR SWIA2026081777535](https://openairdocs.org/sdr/SWIA2026081777535.md): Pressure Deck · corroded · Aug 17, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Structure
  > EVIDENCE OF CORROSION UNDER THE RH OVERWING EMERGENCY EXIT DOOR ON THE PRESSURE DECK AREA IN TWO SPOTS BETWEEN FS 76185 AND FS 78515 MARKED WITH RED GREASE PENCIL C-CHECK RO 10062026REPAIRED CORROSION DAMAGE TO RH PRESSURE FLOOR SILL ANGLE BETWEEN FS75652- F
- [SDR SWIA2026081177533](https://openairdocs.org/sdr/SWIA2026081177533.md): Floorbeam · elongated · Aug 11, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > WHILE LOCATING AND DRILLING NEW SERVICEABLE RH CAP ANGLE PN CC670-34096-1, ELONGATED 1EA NUTPLATE HOLE IN FS 280 BEAM PN CC670-34094JP-2 AT APPROX RBL 38 C-CHECK RO 10062026COMPLIED WITH CUTOUT REPAIR TO ELONGATED NUTPLATE SCREW HOLE IN FS280 CROSSBEAM BETWE
- [SDR SWIA2026080477531](https://openairdocs.org/sdr/SWIA2026080477531.md): Floorbeam · damaged · Aug 4, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH FLOOR SILL AT FS 280 HAS 4EA OVERSIZE HOLES WHERE IT ATTACHES TO FS280 CROSSBEAM C-CHECK RO 10062026REPAIRED LH FLOOR SILL AT FS280 WHERE IT ATTACHES TO FS280 CROSSBEAM IAW REO 670-53-21-2945 REV-- DATED 2026-08-08 COMPLETED TASK CARD 51-900-1003-SKY AND
- [SDR SWIA2026080377541](https://openairdocs.org/sdr/SWIA2026080377541.md): Frame · corroded · Aug 3, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FS1015 FOUND TO HAVE CORROSION BETWEEN STGR 27 TO 25L, STGR 22L TO 21L REQUIRES REPLACEMENT C-CHECK RO 10062026REPLACED FRAME FS1015 BETWEEN STRINGER 26R TO 19L IAW REO 670-53-61-2744 REV-- DATED 2026-08-11 AND CRJ-700 SRM 51-42-06-001-001-A01 AND 51-24-36
- [SDR SWIA2026071277546](https://openairdocs.org/sdr/SWIA2026071277546.md): Crossbeam · corroded · Jul 12, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > WHILE ACCESSING LT FS 280 LWR WEB, FOUND LT CROSSBEAM TO BE CORRODED. REMOVED AND REPLACED THE CROSSBEAM WITH NEW IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR SWIA2026071277545](https://openairdocs.org/sdr/SWIA2026071277545.md): Strap · mismatched · Jul 12, 2026 · N713SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > EXISTING HOLE PATTERN OF BS 280 UPPER SPLICE STRAP WILL NOT LINE UP WITH NEW BS 280 CROSSBEAM. REMOVED AND REPLACED THE BS 280 UPPER SPLICE STRAP IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01.
- [SDR SWIA2026062977547](https://openairdocs.org/sdr/SWIA2026062977547.md): Striker · corroded · Jun 29, 2026 · N713SK · Cndair CL6002C10 · Service Doors
  > THE SERVICE DOOR SILL STRIKER HAS EVIDENCE OF CORROSION ON ITS INTERIOR SIDE IN SEVERAL LOCATIONS BETWEEN BS 310 & 349. REPLACED SERVICE DOOR SILL STRIKER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR SWIA2026062977543](https://openairdocs.org/sdr/SWIA2026062977543.md): Hinge · gouged · Jun 29, 2026 · N713SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE FUSELAGE SIDE LAST LUG LANDING IS GOUGED FROM THE FWD SIDE C-CHECK RO 10062026REPAIRED PAX DOOR HINGE ON FUSELAGE SIDE AT LAST LUG LANDING IAW CRJ 700 SRM 53-21-23-201-010-A01 REPAIR PROCEDURE D TYPE IV COMPLETED AND ATTACHED SKYWEST TASK CARD
- [SDR SWIA2026062977532](https://openairdocs.org/sdr/SWIA2026062977532.md): Slat Track · chafed · Jun 29, 2026 · N713SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 2-2 IS CHAFED C-CHECK RO 10062026EVALUATED DAMAGE PER CRJ700 SRM 51-12-00-001-001-A01 DAMAGE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN REPAIRED SLAT TRACK 2-2 IAW MHIRJ REO 670-57-42-2557 REV --DATED 2026-07-09
- [SDR SWIA2026062877544](https://openairdocs.org/sdr/SWIA2026062877544.md): Angle · corroded · Jun 28, 2026 · N713SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BS 265 FRAME WAS CORRODED BEWEEN STR 27 - 26L. FOUND CORROSION TO BE CENTRALIZED TO THE BS 265 LOWER STIFFENING ANGLE BTWN STR 26-27L. REMOVED AND INSTALLED A NEW SERVICEABLE TIFFENING ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & 51-42-22-001-0
- [SDR SWIA2026062877534](https://openairdocs.org/sdr/SWIA2026062877534.md): Stringer · corroded · Jun 28, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L IS CORRODED BETWEEN FS 295 TO FS 310 C-CHECK RO 10062026REMOVED AND REPLACED STRINGER 25L FROM FS280 TO FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHED COMPLETED FORM 337 NO WE
- [SDR SWIA2026062677550](https://openairdocs.org/sdr/SWIA2026062677550.md): Floorbeam · corroded · Jun 26, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RIGHT BS 280 FLOORBEAM WAS CORRODED INSIDE OF SCRW HOLES. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR SWIA2026061777530](https://openairdocs.org/sdr/SWIA2026061777530.md): Plate · chafed · Jun 17, 2026 · N713SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SACRIFICIAL PLATE AT STRINGER 27AND FS977 HAS CHAFING DAMAGE AND REPAIR DOUBLER HAS FRETTING CORROSION AT FS985 BETWEEN STRINGERS 26L AND 26R C-CHECK RO 10062026REPAIRED SACRIFICIAL PLATE AT BETWEEN STRINGER 26L AND 26R FROM FS 96900 TO 98500 IAW REO 670-53
- [SDR SWIA2026061577542](https://openairdocs.org/sdr/SWIA2026061577542.md): Frame · corroded · Jun 15, 2026 · N713SK · Cndair CL6002C10 · Fuselage Main, Frame
  > EVIDENCE OF CORROSION FORMING IN MULTIPLE SMALL AREAS AT APPROX FS1015-FS1031 STGR 27-STGR 26R BETWEEN THE TAPE C-CHECK RO 10062026REPAIRED CORROSION GOUGE DAMAGE BETWEEN FS1000-1047 STGR27-21R ON THE EXTERNAL SKIN IAW MHIRJ REO 670-53-61-2740 REV-- DATED 2
- [SDR SWIA2026061477549](https://openairdocs.org/sdr/SWIA2026061477549.md): Handle · chafed · Jun 14, 2026 · N713SK · Cndair CL6002C10 · Service Doors
  > THERE IS CHAFING ON THE HANDLE OF THE GALLEY SERVICE DOOR AT THE INNER AREA OF THE HANDLE EXTERIOR HANDLE. INSTALLED A NEW SERVICEABLE SERVICE DOOR HANDLE HOUSING ASSY IAW SRM 51-42-06-001-001-A01.
- [SDR SWIA2026060877548](https://openairdocs.org/sdr/SWIA2026060877548.md): Skin · scratched · Jun 8, 2026 · N713SK · Cndair CL6002C10 · Leading Edge Devices
  > THE RT INBD LE SLAT PANEL HAS MULTIPLE SCRATCHES AND SMALL GOUGES FROM APPROX WS 108 - 148. BLENDED AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED AREA BY COMPLYING WITH REO 670-57-42-2519 REV-A. NO NDT INDICATIONS NOTED.
- [SDR SWIA2025F01348](https://openairdocs.org/sdr/SWIA2025F01348.md): Stringer · no discrepancy · Aug 28, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REMOVED FWD RIVETS ON REMOVED STGR 22L BETWEEN FS193.00 AND FS202.75 TO FOM AS CALLED OUT BY REO 670-53-11-2170 REV -- DATE 9-22-25. SEE CP 30714031 (FILED CLOSED)REINSTALLED REMOVED RIVETS ON STGR 22L BETWEEN FS193.00 AND FS202.75 IAW SRM 51-42-06, SRM 51-42
- [SDR SWIA2025F01347](https://openairdocs.org/sdr/SWIA2025F01347.md): Stringer · no discrepancy · Aug 28, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REMOVED FWD RIVETS ON STGR 21L BETWEEN FS193.00 AND FS202.75 TO FOM AS CALLED OUT BY REO 670-53-11-2170 REV -- DATE 9-22-25.. SEE CP 30714031 (FILED CLOSED)REINSTALLED REMOVED RIVETS ON STGR 21L BETWEEN FS193.00 AND FS202.75 IAW SRM 51-42-06, SRM 51-42-20 AN
- [SDR SWIA202509240828](https://openairdocs.org/sdr/SWIA202509240828.md): Stringer · no discrepancy · Aug 28, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > REMOVED FWD RIVETS ON STGR 19L BETWEEN FS193.00 AND FS202.75 TO FOM AS CALLED OUT BY REO 670-53-11-2170 REV -- DATE 9-22-25. SEE CP 30714031 (FILED CLOSED)REINSTALLED REMOVED RIVETS ON STGR 19L BETWEEN FS193.00 AND FS202.75 IAW SRM 51-42-06, SRM 51-42-20 AND
- [SDR SWI2025F01325](https://openairdocs.org/sdr/SWI2025F01325.md): Panel · dented · Aug 22, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DUE TO BIRDSTRIKE TO LHS HYD BAY FUSELAGE PANEL, FOUND FORWARD DENTED AREA (NO. 1) MEASURES 5.375" L X 3.875" W X 0.375" MAX. DEPTH AND IS LOCATED BETWEEN THE ELECTRICAL BAY DOOR AND HYDRAULIC BAY ACCESS DOOR, JUST FORWARD OF FS193.00.REF. REO-53-11-2169 FOR D
- [SDR SWI2025F01324](https://openairdocs.org/sdr/SWI2025F01324.md): Skin · cracked · Aug 22, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > UPON DRESS BACK OF AFT DENTED AREA (NR. 2), OPERATOR REPORTS THAT THE SKIN PANEL WAS CRACKED OVER A LENGTH OF APPROX. 1.25" LONG. ADDITIONALLY, OPERATOR REPORTS THE INTERNAL UPPER STRAP(DWG: CC670-34124, 0.050" NOMINAL THK, REF) TO HAVE BEEN DEFORMED.REF. REO
- [SDR SWIA202509240822](https://openairdocs.org/sdr/SWIA202509240822.md): Skin · dented · Aug 22, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DUE TO BIRDSTRIKE TO LT HYD BAY FUSELAGE PANEL, THE AFT DENTED AREA (NR 2) MEASURES 11.00" L X 6.00" W X 1.75" MAX. DEPTH AND IS LOCATED BETWEEN FS193.00 - FS202.75 & BETWEEN STR16L - STR21L.REF. REO-53-11-2169 FOR DAMAGE REPORT. (FLIGHT 1300 - FILED CLOS
- [SDR SWI2025F01119](https://openairdocs.org/sdr/SWI2025F01119.md): Panel · dented · Aug 22, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DUE TO BIRDSTRIKE TO LHS HYD BAY FUSELAGE PANEL, FOUND FORWARD DENTED AREA (NO. 1) MEASURES 5.375" L X 3.875" W X 0.375" MAX. DEPTH AND IS LOCATED BETWEEN THE ELECTRICAL BAY DOOR AND HYDRAULIC BAY ACCESS DOOR, JUST FORWARD OF FS193.00.REF. REO-53-11-2169 FOR D
- [SDR SWI2025F01118](https://openairdocs.org/sdr/SWI2025F01118.md): Skin · cracked · Aug 22, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > UPON DRESS BACK OF AFT DENTED AREA (NO. 2), OPERATOR REPORTS THAT THE SKIN PANEL WAS CRACKED OVER A LENGTH OF APPROX. 1.25" LONG. ADDITIONALLY, OPERATOR REPORTS THE INTERNAL UPPER STRAP(DWG: CC670-34124, 0.050" NOMINAL THK, REF) TO HAVE BEEN DEFORMED.REF. REO-
- [SDR SWIA2025082500022](https://openairdocs.org/sdr/SWIA2025082500022.md): Panel · dented · Aug 22, 2025 · N713SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DUE TO BIRDSTRIKE TO LHS HYD BAY FUSELAGE PANEL, THE AFT DENTED AREA (NO. 2) MEASURES 11.00" L X 6.00" W X 1.75" MAX. DEPTH AND IS LOCATED BETWEEN FS193.00 - FS202.75 & BETWEEN STR16L - STR21L.REF. REO-53-11-2169 FOR DAMAGE REPORT. (FLIGHT 1300 - FILED OPE
- [SDR SWIA2025041400005](https://openairdocs.org/sdr/SWIA2025041400005.md): Battery · failed · Apr 10, 2025 · N713SK · Cndair CL6002C10 · Emergency Lighting
  > STRONG ELECTRICAL SMELL VERY LIGHT GREY SMOKE CABIN ROW 8 TO 10 MOSTLY ON THE LEFT SIDE. (FLIGHT 6390 - FILED CLOSED)PLEASE REFERENCE AML 1579363 PLEASE REFERENCE AML 1579365 PLEASE REFERENCE AML 1579367 PLEASE REFERENCE AML 1579368 PLEASE REFERENCE AML 15
- [SDR SWI2025F00271](https://openairdocs.org/sdr/SWI2025F00271.md): Oxygen Bottle · low pressure · Mar 2, 2025 · N713SK · Cndair CL6002C10 · Crew Oxygen System
  > OXY LO PRESS AFTER LEVELING AT CRUISE CAPT OX MASK DEPLETED AIR. (FLIGHT 3699 - FILED CLOSED) FOUND CAPT O2 MASK HOSE BURST. REMOVED AND REPLACED CAPT SIDE O2 MASK REF TO CRJ 700 AMM 35-11-12 OPS TEST GOOD. NO LEAKS FOUND AT THIS TIME A/C OK FOR SERVIC
- [SDR SWIA2024112700019](https://openairdocs.org/sdr/SWIA2024112700019.md): Valve · smoke · Nov 19, 2024 · N713SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > SOON AFTER TAKEOFF BOTH FLIGHT ATTENDANTS REPORTED SMELLING SMOKE AND A HAZE IN THE CABIN. NO MESSAGED APPEARED ON EICAS. JUST PRIOR TO LANDING BACK IN ICT THE FAS SAID THE SMELL AND HAZE HAD DISAPPEARED. LANDED IN ICT AND THE FIRE DEPARTMENT INSPECTED US ON T
- [SDR SWI2024F01281](https://openairdocs.org/sdr/SWI2024F01281.md): Unknown · smoke · Nov 19, 2024 · N713SK · Cndair CL6002C10 · Air Distribution System
  > SOON AFTER TAKEOFF BOTH FLIGHT ATTENDANTS REPORTED SMELLING SMOKE AND A HAZE IN THE CABIN. NO MESSAGED APPEARED ON EICAS. JUST PRIOR TO LANDING BACK IN ICT THE FAS SAID THE SMELL AND HAZE HAD DISAPPEARED. LANDED IN ICT AND THE FIRE DEPARTMENT INSPECTED US ON T
- [SDR SWIA20241101](https://openairdocs.org/sdr/SWIA20241101.md): Unknown · smoke · Nov 1, 2024 · N713SK · Cndair CL6002C10 · Air Distribution System
  > FA REPORTED A SMOKEY HAZE AND THE SMELL OF SMOKE RIGHT AFTER TAKEOFF. RETURNED TO FIELD. (FLIGHT 5010 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29087720 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH SL-21-028.SMOD APPROVAL GRANTED V
- [SDR SWI2023F00523](https://openairdocs.org/sdr/SWI2023F00523.md): Unknown · haze · Nov 19, 2023 · N713SK · Cndair CL6002C10 · Air Distribution System
  > FAS REPORT ODOROUS HAZE (MUSTY) IN CABIN DURING CLIMB OUT. EVENTUALLY CLEARED. SMELL CAME BACK ON DESCENT BUT NO HAZE NOTED. (FLIGHT 4819 FILED CLOSED) PLEASE REFERENCE AML 1249459 PLEASE REFERENCE AML 1249460 PLEASE REFERENCE AML 1249462 PLEASE REFERENCE
- [SDR SWI2023F00477](https://openairdocs.org/sdr/SWI2023F00477.md): Unknown · haze · Nov 19, 2023 · N713SK · Cndair CL6002C10 · Air Distribution System
  > FAS REPORT ODOROUS HAZE (MUSTY) IN CABIN DURING CLIMB OUT. EVENTUALLY CLEARED. SMELL CAME BACK ON DESCENT BUT NO HAZE NOTED. (FLIGHT 4819 FILED OPEN)
- [SDR SWIA20230927](https://openairdocs.org/sdr/SWIA20230927.md): Unknown · smoke · Sep 27, 2023 · N713SK · Cndair CL6002C10 · Passenger Compartment Lighting
  > FORWARD FA REPORTED THIN SMOKE ON THE GALLEY FLOOR DURING THE TAKEOFF ROLL. THE AFT FA ALSO REPORTED VERY THIN SMOKE IN THE AFT CABIN DURING THE SAME TIME. THE FORWARD FA SUSPECTED IT ORIGINATED FROM THE GALLEY LIGHTS AND TURNED THEM OFF FOR THE DURATION OF TH
- [SDR SWIA20230928001](https://openairdocs.org/sdr/SWIA20230928001.md): Unknown · smoke · Sep 27, 2023 · N713SK · Cndair CL6002C10 · Passenger Compartment Lighting
  > FORWARD FA REPORTED THIN SMOKE ON THE GALLEY FLOOR DURING THE TAKEOFF ROLL. THE AFT FA ALSO REPORTED VERY THIN SMOKE IN THE AFT CABIN DURING THE SAME TIME. THE FORWARD FA SUSPECTED IT ORIGINATED FROM THE GALLEY LIGHTS AND TURNED THEM OFF FOR THE DURATION OF TH
- [SDR SWIA20230920019](https://openairdocs.org/sdr/SWIA20230920019.md): Unknown · smoke · Sep 19, 2023 · N713SK · Cndair CL6002C10 · Humidity Control System
  > ON TAKEOFF A LIGHT WHITE SMOKE WAS PRESENT IN THE CABIN. FLIGHT ATTENDANT SAID IT WAS THROUGHOUT THE ENTIRE CABIN DISSIPATED WITHIN FOUR MINUTES. SLIGHT EXHAUST SMELL. (FLIGHT 3064) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27184535 WITH THE FOLLOWING CO
- [SDR SWIA2022111666902](https://openairdocs.org/sdr/SWIA2022111666902.md): Unknown · smoke · Nov 15, 2022 · N713SK · Cndair CL6002C10 · Air Distribution System
  > SMOKE IN THE CABIN ON CLIMB OUT RETURNED TO FIELD FA REPORTED THICK WHITE SMOKE. (FLIGHT 4937) COMPLIED WITH FIM 21-22-00 SMOKE AND/OR ABNORMAL SMELL IN PASSENGER CABIN AND SERVICE LETTER SL-21-028. WHEN THE DFW FIRE FIGHTERS INITIALLY ENTERED THE AIRCR
- [SDR SWIA202265368](https://openairdocs.org/sdr/SWIA202265368.md): None · dented · Apr 12, 2022 · N713SK · Cndair CL6002C10 · Wing Structure
  > DENT #4 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS12.50- ROOT OF WINGLET REQUIRES DAMAGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILEED - CLOSED) EVALUATED DENT #4 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS12.50- ROOT OF WINGLET AND FOUND DEN
- [SDR SWIA202265367](https://openairdocs.org/sdr/SWIA202265367.md): None · dented · Apr 12, 2022 · N713SK · Cndair CL6002C10 · Wing Structure
  > DENT #3 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS21.75-WGLTS12.50 REQUIRES DAMAGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILED - CLOSED) EVALUATED DENT #3 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS21.75-WGLTS12.50 AND FOUND DENT TO BE OUT O
- [SDR SWIA202265366](https://openairdocs.org/sdr/SWIA202265366.md): None · dented · Apr 12, 2022 · N713SK · Cndair CL6002C10 · Wing Structure
  > DENT #2 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS31.25 - WGLTS21.75 REQUIRES DAMGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILED - CLOSED) EVALUATED DENT #2 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS31.25 - WGLTS21.75 AND FOUND DENT TO BE OU
- [SDR SWIA202265365](https://openairdocs.org/sdr/SWIA202265365.md): None · dented · Apr 12, 2022 · N713SK · Cndair CL6002C10 · Wing Structure
  > DENT #1 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS40.50-WGLTS31.25 REQUIRES DAMGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILED - CLOSED) EVALUATED DENT #1 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS40.50-WGLTS31.25 AND FOUND DENT TO BE OUT OF
- [SDR SWIA202264666](https://openairdocs.org/sdr/SWIA202264666.md): None · cracked · Jan 25, 2022 · N713SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR AFT WEB PANEL HAS 3 EACH CRACKS ON STEP ATTACH FLANGES (C CHECK RO 02/22/2022) REMOVED AND REPLACED PAX DOOR AFT WEB PANEL REF. CRJ700 SRM 51-42-06-001-001-A01.
- [SDR SWIA202264646](https://openairdocs.org/sdr/SWIA202264646.md): None · chafed · Jan 24, 2022 · N713SK · Cndair CL6002C10 · Powerplant System
  > RH LOWER TRANSCOWL LATCH DOOR COAMING CHAFED. (C CHECK RO 02/22/2022) REMOVED AND REPLACED RH LOWER TRANSCOWL LATCH DOOR COAMING P/N CN624-2060-207. REF. AND COMPLIED WITH ALL STEPS OF REO 670-54-21-1207 REV A, DATED 2015-08-27 FIGURE 3. COMPLIED WITH SKY
- [SDR SWIA202264645](https://openairdocs.org/sdr/SWIA202264645.md): None · corroded · Jan 23, 2022 · N713SK · Cndair CL6002C10 · Doors
  > PAX DOOR CLOSING FITTING (CUP) FWD HAS EVIDENCE OF CORROSION (C CHECK RO 02/22/2022) REPLACED OUT OF LIMITS FWD HANDRAIL CUP FITTING REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV. AE COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTI
- [SDR SWIA202264675](https://openairdocs.org/sdr/SWIA202264675.md): None · cracked · Jan 21, 2022 · N713SK · Cndair CL6002C10 · Doors
  > PAX DOOR AFT WEB PANEL SIDE PANEL STIFFENER IS CRACKED (C CHECK RO 02/22/2022) REMOVED AND REPLACED PAX DOOR AFT WEB PANEL STIFFENER REF. CRJ700 SRM 51-42-06-001-001-A01.
- [SDR SWIA202264670](https://openairdocs.org/sdr/SWIA202264670.md): None · damaged · Jan 14, 2022 · N713SK · Cndair CL6002C10 · Window/Windshield System
  > REMOVE/REINSTALL FLIGHT COMPARTMENT LH FWD WINDSHIELD TO FOM (C CHECK RO 02/22/2022) REMOVED AND REPLACED FLIGHT COMPARTMENT LH FWD WINDSHIELD WITH NEW SERVICEABLE UNIT AND HARDWARES REF CRJ 700 AMM TASK 56-11-01-400-801-A01 AND 56-220-1000 SKY CARD, LEAK
- [SDR SWIA202264644](https://openairdocs.org/sdr/SWIA202264644.md): None · corroded · Jan 14, 2022 · N713SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL ATTACHED TO STGR 21L BETWEEN FS.310.00 TO FS.333.00. (C CHECK RO 02/22/2022) REMOVED AND REPLACED INTERCOSTAL DAMAGED OUT LIMITS SINCE CORROSION DAMAGE WAS FOUND TO BE ON MORE THAN ONE ELEMENT AND OVERLAPS, MAKING INTERCOSTAL OUT O
- [SDR SWIA202264643](https://openairdocs.org/sdr/SWIA202264643.md): None · corroded · Jan 12, 2022 · N713SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL (AFT) P/N 601R31902-317 CORRODED. (C CHECK RO 02/22/2022) REMOVED AND REPLACED WITH NEW PAX DOOR INTERCOSTAL (AFT) P/N 601R31902-317 IN REF DWG 601R31702, REV -N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-9
- [SDR SWIA202264669](https://openairdocs.org/sdr/SWIA202264669.md): None · damaged · Jan 10, 2022 · N713SK · Cndair CL6002C10 · Window/Windshield System
  > REMOVE/REINSTALL FLIGHT COMPARTMENT RH FWD WINDSHIELD TO FOM (C CHECK RO 02/22/2022) REMOVED AND INSTALLED NEW SERVICEABLE FLIGHT COMPARTMENT RH FWD WINDSHIELD REF CRJ 700 AMM TASK 56-11-01-400-801-A01 AND 56-220-1000 SKY CARD LEAK & OP CHECKS GOOD. SEE CO
- [SDR SWIA202264665](https://openairdocs.org/sdr/SWIA202264665.md): None · corroded · Jan 6, 2022 · N713SK · Cndair CL6002C10 · Ailerons
  > RH INBOARD FLAP MOVEABLE VANE ACTUATORS 1 FWD TRUNNION ATTACH HARDWARE APPEARS CORRODED. (C CHECK RO 02/22/2022) REMOVED RH INBOARD FLAP MOVEABLE VANE ACTUATORS 1 FWD TRUNNION ATTACH HARDWARE REF CRJ700 AMM 27-52--23-000-801-A01 STEP 4(A)(3)(A)(B). REPLACE
- [SDR SWIA202264642](https://openairdocs.org/sdr/SWIA202264642.md): None · cracked · Jan 6, 2022 · N713SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL FOUND CORRODED & CRACKED, LOCATED BETWEEN FS 320.00 - 323.00 AND NEXT TO INTERCOSTAL DD1A. (C CHECK RO 02/22/2022) REMOVED DAMAGED PAX DOOR INTERCOSTAL. FABRICATED AND INSTALLED PAX DOOR INTERCOSTAL P/N 600-31902-257 REF CRJ 700 SRM 51

Next page: https://openairdocs.org/aircraft/N713SK/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 = 'N713SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N713SK/reports

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