# Service difficulty reports: N753SK

A list on [N753SK](https://openairdocs.org/aircraft/N753SK.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 · 176 reports

- [SDR SWIA2026090777101](https://openairdocs.org/sdr/SWIA2026090777101.md): Window · cracked · Sep 7, 2026 · N753SK · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT SIDE WINDOW HAS A 6-8 INCH CRACK ABOUT MIDWAY ON THE BOTTOM OF THE RT SIDE WINDOW (FLIGHT 6456). REMOVED AND REPLACED RT SIDE WINDOW IAW AMM 56-12-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA202505060001](https://openairdocs.org/sdr/SWIA202505060001.md): Pcu · broken · May 1, 2025 · N753SK · Cndair CL6002C10 · Rudder Control System
  > DURING TROUBLESHOOTING OF STIFF RUDDER DURING OPERATION, FOUND #1 RUDDER PCU ROD END BROKEN. (FLIGHT 6425) REMOVED AND REPLACED NO.1 RUDDER PCU IAW CRJ 700 AMM 27-23-01. RIGGED RUDDER SYSTEM IAW CRJ 700 AMM 27-21-00. OPS CHECKS GOOD IAW CRJ 700 AMM 27-32-01.
- [SDR SWIA20250501001](https://openairdocs.org/sdr/SWIA20250501001.md): Rod End · broken · May 1, 2025 · N753SK · Cndair CL6002C10 · Rudder Control System
  > REFERENCE AML 1594668 DURING TROUBLESHOOTING OF STIFF RUDDER DURING OPERATION, FOUND #1 RUDDER PCU ROD END BROKEN. (FLIGHT 6425 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202503190012](https://openairdocs.org/sdr/SWIA202503190012.md): Window · arced · Mar 12, 2025 · N753SK · Cndair CL6002C10 · Flight Compartment Windows
  > DURING APPROACH, NOTICED SPARKS ON THE BOTTOM OF THE LEFT SIDE WINDOW, THEN A MINUTE LATER RECEIVED A L WINDOW HEAT CAUTION MESSAGE ACCOMPANIED BY 2 NOTICEABLE CRACKS INSIDE THE SIDE WINDOW. (FLIGHT 4910 - FILED CLOSED) REMOVED AND REPLACED L/H COCKPIT WI
- [SDR SWIA202503180012](https://openairdocs.org/sdr/SWIA202503180012.md): Window · arced · Mar 12, 2025 · N753SK · Cndair CL6002C10 · Flight Compartment Windows
  > DURING APPROACH, NOTICED SPARKS ON THE BOTTOM OF THE LEFT SIDE WINDOW, THEN A MINUTE LATER RECEIVED A L WINDOW HEAT CAUTION MESSAGE ACCOMPANIED BY 2 NOTICEABLE CRACKS INSIDE THE SIDE WINDOW. (FLIGHT 4910 - FILED CLOSED) REMOVED AND REPLACED RIGHT WING LEA
- [SDR SWIA2025031300012](https://openairdocs.org/sdr/SWIA2025031300012.md): Window · arced · Mar 12, 2025 · N753SK · Cndair CL6002C10 · Flight Compartment Windows
  > DURING APPROACH, NOTICED SPARKS ON THE BOTTOM OF THE LEFT SIDE WINDOW, THEN A MINUTE LATER RECEIVED A L WINDOW HEAT CAUTION MESSAGE ACCOMPANIED BY 2 NOTICEABLE CRACKS INSIDE THE SIDE WINDOW. (FLIGHT 4910 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202404250319](https://openairdocs.org/sdr/SWIA202404250319.md): Door Frame · corroded · Mar 14, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FS320.163 FRAME 2EA LOWER ATTACH CLIPS CORRODED (C-CHECK RO 4/24/2024) REMOVED AND REPLACED PAX DOOR FS320.163 FRAME 2EA LOWER ATTACH CLIPS REF. CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKY WEST TC 51-900-1002-SKY.
- [SDR SWIA20240425314](https://openairdocs.org/sdr/SWIA20240425314.md): Door Frame · corroded · Mar 14, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FORMER AT FS320.163 CORRODED IN SEVERAL AREAS ON MORE THAN ONE ELEMENT. (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR FORMER AT FS320.163 REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD. SEE CONTINUE CA
- [SDR SWIA2024042500313](https://openairdocs.org/sdr/SWIA2024042500313.md): Cap · cracked · Mar 13, 2024 · N753SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR BOTTOM AFT CORNER CLOSE OUT CAP (PN:601R319983-4) CRACKED (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR BOTTOM AFT CORNER CLOSE OUT CAP REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01, LEAK CHECK GOOD. SEE CONTINUE CARD
- [SDR SWIA202404250298](https://openairdocs.org/sdr/SWIA202404250298.md): Door Frame · corroded · Mar 11, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FRAME AT FS313.56 FROM DD4 TO DD5 IS CORRODED (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR FRAME, AT FS 313.56 FROM DD4 TO DD5, REF. DRWG 601R31702, REV. N, CRJ 700, SRM 51-42-06-001-001-A01, REV. 38. LEAK CHECK GOOD. SEE CONTINUE CAR
- [SDR SWIA20240425311](https://openairdocs.org/sdr/SWIA20240425311.md): Support Angle · corroded · Mar 11, 2024 · N753SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER SUPPORT ANGLE CORRODED (C-CHECK RO 4/24/2024) REMOVED & INSTALLED NEW PAX DOOR AFT FORMER SUPPORT ANGLE REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01, LEAK CHECK GOOD. SEE CONTINUATION
- [SDR SWIA202404250303](https://openairdocs.org/sdr/SWIA202404250303.md): Former · cracked · Mar 9, 2024 · N753SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER CRACKED AT PULLEY BRACKET LOCATION. (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. SEE CONTINUATI
- [SDR SWI2024F00302](https://openairdocs.org/sdr/SWI2024F00302.md): Angle · corroded · Mar 9, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR ANGLE AT DD7A BETWEEN FS327.70 AND FS338.90 CORRODED. (C-CHECK RO 4/24/2024) REMOVED AND REPLACED PAX DOOR ANGLE AT DD7A BETWEEN FS327.70 AND FS338.90 REF.DRWG 601R317040 REV. C AND CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST TASK CARD
- [SDR SWIA202404250301](https://openairdocs.org/sdr/SWIA202404250301.md): Intercostal · corroded · Mar 9, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON PAX DOOR INTERCOSTAL FWD DD6 (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD6, REF. DRWG 601R31702 REV. N, CRJ 700, SRM 51-42-06-001-001-A01 AND CRJ 700,SRM 51-42-10-001-001-A01, REV. 38.LEAK CHECK GOOD, SEE CONTINUE C
- [SDR SWIA20240425309](https://openairdocs.org/sdr/SWIA20240425309.md): Intercostal · corroded · Mar 9, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON PAX DOOR INTERCOSTAL FWD DD5 (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD5, REF. DRWG 601R31702 REV. N, CRJ 700, SRM 51-42-06-001-001-A01, REV. 38. LEAK CHECK GOOD. SEE CONTINUE CARD FOR WORK ACCOMPLISHED. COMPLIED
- [SDR SWIA202404250318](https://openairdocs.org/sdr/SWIA202404250318.md): Frame · corroded · Mar 7, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Frame
  > (MX# 27918611) MULTIPLE SPOT OF CORROSION ON FS280.00 FRAME AFT WEB BETWEEN STGR 25L TO 25R. (MARKED) (C-CHECK RO 4/24/2024) REPAIRED FS280.00 FRAME AFT WEB BETWEEN STGR 25L TO 25R (2EA SPOTS). COMPLIED WITH ALL STEPS OF REO 670-53-11-1931 REV -- DATE 2024
- [SDR SWIA20240425307](https://openairdocs.org/sdr/SWIA20240425307.md): Hinge · worn · Mar 7, 2024 · N753SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASS DOOR HINGE ON DOOR SIDE WORN IN MULTIPLE LUG LANDING (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR HINGE (DOOR SIDE) REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. SEE C
- [SDR SWIA202404250297](https://openairdocs.org/sdr/SWIA202404250297.md): Door Frame · corroded · Mar 6, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON PAX DOOR FORMER AT APPROX FS 327.763 BETWEEN DD4 AND DD5 (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW PAX DOOR FORMER AT FS 327.763 BETWEEN DD4 AND DD5 REF. DRWG 601R31702 REV. N AND CRJ 700 SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. SEE C
- [SDR SWIA202404250296](https://openairdocs.org/sdr/SWIA202404250296.md): Hinge Arm · gouged · Mar 6, 2024 · N753SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT INBOARD FLAP INBOARD HINGE ARM AT LOWER LUG TO HINGE BOX GOUGED FROM OLD LOOSE STUCK SCREW IN LUG AREA MX TRANS 27912411 (C-CHECK RO 4/24/2024) BLENDED AND FOUND OUT OF LIMITS REPAIRED PER MHIRJ REO 670-57-52-553 REV -A DATE 2024-03-16. SEE CONTINUAT
- [SDR SWIA202404250295](https://openairdocs.org/sdr/SWIA202404250295.md): Intercostal · corroded · Mar 6, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON PAX DOOR INTERCOSTAL MID DD3 (C-CHECK RO 4/24/2024) REMOVED & INSTALLED PAX DOOR INTERCOSTAL DD3 MID REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR
- [SDR SWIA202404250294](https://openairdocs.org/sdr/SWIA202404250294.md): Track · damaged · Mar 6, 2024 · N753SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > REPLACE AFT CARGO DOOR AFT TRACK CAMP 27912351 (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW AFT CARGO DOOR AFT-TRACK P/N: CC670-38726-5PP. REF. CRJ 700 SRM 51-41-02-001-001-A01 AND REO NO. 670-53-62-102 REV. -A, DATED 2016-10-12. M-337 AND SKYWEST TASK
- [SDR SWI202404250293](https://openairdocs.org/sdr/SWI202404250293.md): Door Frame · corroded · Mar 6, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON PAX DOOR FRAME FS 320.00 BETWEEN DD4 AND DD5 (C-CHECK RO 4/24/2024) INSTALLED NEW PAX DOOR FRAME AT FS 320.00 REF. DRWG 601R31702 REV. N, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. LEAK CHECK GOOD, SEE CONTINUATION
- [SDR SWIA2024042500306](https://openairdocs.org/sdr/SWIA2024042500306.md): Intercostal · corroded · Mar 6, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON PAX DOOR INTERCOSTAL FWD DD3 (C-CHECK RO 4/24/2024) REMOVED & INSTALLED NEW PAX DOOR INTERCOSTAL DD3, REF. DRWG 601R31702 REV. N, CRJ 700, SRM 51-42-06-001-001-A01, REV. 38. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. COMPLIE
- [SDR SWIA202404250311](https://openairdocs.org/sdr/SWIA202404250311.md): Bracket · corroded · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MACHINED BRACKET FOR CARGO SYSTEM BETWEEN FS549.00 - 565.00 ON INTERCOSTAL BETWEEN STGR25R - 24R IS CORRODED. (MARKED) (C-CHECK RO 4/24/2024) BLENDED-OUT CORROSION ON MACHINED BRACKET FOR CARGO SYSTEM BETWEEN FS549.00 - 565.00 ON INTERCOSTAL BETWEEN STGR
- [SDR SWIA202404250310](https://openairdocs.org/sdr/SWIA202404250310.md): Pan · corroded · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT SIDE DRIP PAN AT FS 280.0 RBL9 AFT SUPPORT CLIP CORNER CORRODED AND DAMAGED (C-CHECK RO 4/24/2024) REMOVED AND REPLACED WITH NEW SUPPORT CLIP. REF. CRJ700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020 AND BOMBARDIER DWG SH690-32120 REV AL. COMPLIED WIT
- [SDR SWIA202404250309](https://openairdocs.org/sdr/SWIA202404250309.md): Plate · corroded · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CARGO DOOR SURROUND LOWER AFT JOINT PLATE HAS CORROSION AROUND MULTIPLE FASTENERS, FS578.00 & STGR25L. (MARKED) (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW JOINT PLATE ON CARGO DOOR SURROUND LOWER AFT FS562.00 & STGR25L. REF CRJ700 SRM 51-42-22-001-00
- [SDR SWIA202404250308](https://openairdocs.org/sdr/SWIA202404250308.md): Seal · gouged · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FORWARD BAGGAGE BAY DOOR EXTERNAL SURROUND STRUCTURE HAS 3 GOUGES AS MARKED (C-CHECK RO 4/24/2024) REPLACED AFT SEAL STRIKER WHERE 3 GOUGES WHERE LOCATED ON FORWARD BAGGAGE BAY DOOR EXTERNAL SURROUND STRUCTURE REF. CRJ700 SRM 51-42-06-001-001-A01 REV. 38 J
- [SDR SWIA202404250307](https://openairdocs.org/sdr/SWIA202404250307.md): Window Post · cracked · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Structure
  > COCKPIT RIGHT-HAND WINDOW POST CRACKED AT THE TOP THRU HOLE FOR THE FASTENER BARREL NUT. (MARKED) (C-CHECK RO 4/24/2024) REMOVED AND REPLACED R/H SIDE POST. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# CC670-33055 REV. F COMPLIED WITH SKYWEST TASK CARD 51
- [SDR SWIA202404250306](https://openairdocs.org/sdr/SWIA202404250306.md): Bracket · corroded · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MACHINED BRACKET FOR CARGO SYSTEM BETWEEN FS581.00 - 597.00 ON INTERCOSTAL BETWEEN STGR27 - 26L IS CORRODED. (MARKED) 27892424 (C-CHECK RO 4/24/2024) REPLACED MACHINED BRACKET FOR CARGO SYSTEM BETWEEN FS581.00 - 597.00 ON INTERCOSTAL BETWEEN STGR27 - 26L R
- [SDR SWIA202404250305](https://openairdocs.org/sdr/SWIA202404250305.md): Window Post · cracked · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Structure
  > COCKPIT LEFT-HAND WINDOW POST CRACKED AT THE TOP THRU HOLE FOR THE FASTENER BARREL NUT. (MARKED) (C-CHECK RO 4/24/2024) REMOVED AND REPLACED LH SIDE POST. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# CC670-33055 REV. F COMPLIED WITH SKYWEST TASK CARD 51-
- [SDR SWIA202404250304](https://openairdocs.org/sdr/SWIA202404250304.md): Plate · corroded · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CARGO DOOR SURROUND LOWER FORWARD JOINT PLATE HAS CORROSION AROUND MULTIPLE FASTENERS, FS535.00 & STGR25L. (MARKED) (C-CHECK RO 4/24/2024) REMOVED & INSTALLED NEW JOINT PLATE ON LOWER FORWARD CARGO DOOR SURROUND FS535.00 & STGR25L REF CRJ700 SRM 51-42-22-0
- [SDR SWIA20240425301](https://openairdocs.org/sdr/SWIA20240425301.md): Floorbeam · cracked · Mar 1, 2024 · N753SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 FLOOR BEAM FORWARD SIDE HAS SUSPECTED CRACK ON ANGLE AT FS 280.0 LBL 9 AS MARKED (C-CHECK RO 4/24/2024) INSTALLED NEW LOWER GUSSET P/N CC670-33467-1 AT FS 280.00 LBL9 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-34010 REV K. M-337 AND SKYWEST T
- [SDR SWIA202404250300](https://openairdocs.org/sdr/SWIA202404250300.md): Support Bracket · cracked · Feb 28, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH EMER DOOR UPPER MOUNT SUPPORT BRACKET HAS SUSPECTED CRACK (MARKED). (C-CHECK RO 4/24/2024) REPAIRED RH EMER DOOR UPPER MOUNT SUPPORT BRACKET REF REO 670-52-21-097 REV.-- DATED 2024-04-03COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202404250299](https://openairdocs.org/sdr/SWIA202404250299.md): Floor Panel · corroded · Feb 28, 2024 · N753SK · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT FLOOR PANEL AFT LANDING AT FS.280.00 HAS SPOTS OF CORROSION (MARKED). (C-CHECK RO 4/24/2024) REMOVED CORROSION FROM TOP COCKPIT FLOOR PANEL AFT LANDING AT FS.280.00 REF. CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS REF. CRJ 700 SRM 5
- [SDR SWIA20240425228](https://openairdocs.org/sdr/SWIA20240425228.md): Fitting · gouged · Feb 28, 2024 · N753SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SURROUND STRUCTURE FS349 FITTING CAM GOUGED (C-CHECK RO 4/24/2024) REMOVED AND INSTALLED NEW CAM FITTING P/N: SH670-31913-3 AT FS349.0 PAX DOOR SURROUND STRUCTURE WITH 5EA NEW HI-LITE FASTENERS AND COLLARS. REF. CRJ 700 SRM 51-42-21-001-001-
- [SDR SWIA202404250315](https://openairdocs.org/sdr/SWIA202404250315.md): Stand Off · cracked · Feb 27, 2024 · N753SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/24/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWIA202404250314](https://openairdocs.org/sdr/SWIA202404250314.md): Transcowl · cracked · Feb 27, 2024 · N753SK · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > R/H UPPER TRANSCOWL PERFORATED SKIN UNDER Z STIFFENER IS CRACKED (C-CHECK RO 4/24/2024) CUT AWAY DAMAGED SECTION, FABRICATED AND INSTALLED ALL REPAIR PARTS, REF. REO670-54-21-1617, REV. --, 2024-03-06.COMPLIED WITH MAJOR REPAIR M-337 AND /SKY CARD 51-900-
- [SDR SWIA202404250313](https://openairdocs.org/sdr/SWIA202404250313.md): Plate · chafed · Feb 27, 2024 · N753SK · Cndair CL6002C10 · Galley Doors
  > GALLEY SERVICE DOOR SURROUND STRUCTURE LOWER FORWARD SEAL STRIKER SPLICE PLATE CHAFFED (C-CHECK RO 4/24/2024) FOUND TO BE OUT OF LIMITS, RECEIVED NEW SPLICE PLATE P/N: SH670-31422-1. REMOVED DAMAGE SPLICE PLATE AND INSTALLED NEW SPLICE PLATE P/N: SH670-314
- [SDR SWIA202404250312](https://openairdocs.org/sdr/SWIA202404250312.md): Transcowl · cracked · Feb 27, 2024 · N753SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL PERFORATED SKIN UNDER Z STIFFENER IS CRACKED (C-CHECK RO 4/24/2024) R/H LWR TRANSCOWL SKIN CRACK UNDER "Z" STIFFENER HAS BEEN REPAIRED REF REO# 670-54-21-1619, REV --, DATED 3/12/24 ALL STEPS COMPLIED WITH. SEE CONTINUATION SHEET FOR DET
- [SDR SWIA20240425227](https://openairdocs.org/sdr/SWIA20240425227.md): Transcowl · pulled · Feb 27, 2024 · N753SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL 3 EA FASTENERS ARE PULLED IN Z STIFFENER (C-CHECK RO 4/24/2024) REPAIRED CRACK DAMAGE TO THE L/H UPPER TRANS COWL INNER SKIN COMMON TO ZED STIFFENER, REF REO 670-54-21-1616, REV. --, 2024-03-05. COMPLIED WITH MAJOR REPAIR M-337 AND SKY
- [SDR SWIA20240425224](https://openairdocs.org/sdr/SWIA20240425224.md): Rib · cracked · Feb 24, 2024 · N753SK · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > * R/H WING FIXED LEADING EDGE RIB AT SS57.16 HAS A CRACK IN THE UPPER ATTACH FLANGE NEAR THE FRONT SPAR, MARKED. (C-CHECK RO 4/24/2024) REPAIRED R/H WING FIXED LEADING EDGE RIB CRACK IN THE UPPER ATTACH FLANGE NEAR THE FRONT SPAR AT SS57.16 REF. REO 670-57
- [SDR SWIA202404250316](https://openairdocs.org/sdr/SWIA202404250316.md): Skin · buckled · Feb 23, 2024 · N753SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP LOWER SIDE SKIN APPROXIMATELY FLS209 BUCKLING, HN00140933 (C-CHECK RO 4/24/2024) LEFT WING OUTBOARD FLAP LOWER SIDE SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3, PERMANENT NON FLUSH REPAIR. REFER TO CONTI
- [SDR SWI202404250316](https://openairdocs.org/sdr/SWI202404250316.md): Skin · buckled · Feb 23, 2024 · N753SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP LOWER SIDE SKIN APPROXIMATELY FLS209 BUCKLING, HN00140933 (C-CHECK RO 4/24/2024) LEFT WING OUTBOARD FLAP LOWER SIDE SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-53-01-201-001-A01, TYPE 3, PERMANENT NON FLUSH REPAIR. REFER TO CONTI
- [SDR SWI2024F00317](https://openairdocs.org/sdr/SWI2024F00317.md): Panel · cracked · Feb 22, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK IN THE FORWARD EQUIPMENT BAY FLOOR IN THE LEFT CUTOUT AFT RADIUS AROUND THE 193.00 FRAME. (MARKED) (C-CHECK RO 4/24/2024) COMPLETED THE CRACK REPAIR IN FWD EQUIPMENT BAY FLOOR ON THE LH SIDE PER BOMBARDIER GREO 670-53-11-509 REV E, DATED 2018-02-08
- [SDR SWIA20240425222](https://openairdocs.org/sdr/SWIA20240425222.md): Angle · cracked · Feb 22, 2024 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD EQUIPMENT COMPARTMENT RIGHT SIDE HAS A CRACK AT THE FLOOR ANGLE AT THE AFT CUT OUT FOR THE CLOSING LATCH ON PANEL 212AR. (MARKED)
- [SDR SWIA20240425919](https://openairdocs.org/sdr/SWIA20240425919.md): Skin · cracked · Sep 19, 2023 · N753SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA67573-670-53-11-1675 753SK MXCODEID55224-PR - CRACK FOUND IN THE LEFT SIDE LOWER AFT CORNER OF THE FORWARD ELECTRICAL BAY DOOR CUTOUT ON THE SKIN PANEL. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-11-1675 REV:-- DATE
- [SDR SWIA20230603](https://openairdocs.org/sdr/SWIA20230603.md): Unknown · warning message · Jun 3, 2023 · N753SK · Cndair CL6002C10 · Landing Gear System
  > A/SKID INBD CAUTION DISPLAYED ON DESCENT APPROX 50MILES OUT FROM DESTINATION. FLAPS WERE 0° AND LANDING GEAR UP. COMPLIED WITH QRH PROCEDURES FOR LANDING. (FLT 3249 FILED CLOSED)INTEGRATED MDC FOUND B1 007489. T/S PER FIM 32-45-13. SUSPECT PARKING BRAKE SHUT
- [SDR SWIA202053855](https://openairdocs.org/sdr/SWIA202053855.md): Windshield · cracked · Nov 5, 2020 · N753SK · Cndair CL6002C10 · Flight Compartment Windows
  > CA SIDE WINDSHIELD CRACKED AT FL 280 LOOKS LIKE IT IS THE OUTBOARD PLY, COMPLIED WITH QRH. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 21792428 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED CA WINDSHIELD. OPERATIONS CHECK GOOD. LEAK CHECK GOO
- [SDR SWIA2020040649967](https://openairdocs.org/sdr/SWIA2020040649967.md): Attach Fitting · worn · Apr 1, 2020 · N753SK · Cndair CL6002C10 · Rudder/Tab, Attach Fittings
  > EXCESSIVE PLAY NOTED IN #3 RUDDER ATTACH FITTING ON VERTICAL STABIIZER REAR SPAR; FITTING REQUIRES REPLACEMENT. (C-CHECK) RO 4/3/2020 REPLACED RUDDER # 3 FITTING ON VERTICAL STABILIZER REAR SPAR PER DRAWING, SRM COMPLIED WITH TASK CARD.
- [SDR SWIA2020040649966](https://openairdocs.org/sdr/SWIA2020040649966.md): Lug · gouged · Mar 20, 2020 · N753SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH UPPER C-DUCT HINGE BEAM, MIDDLE HINGE LUG AT AFT POSITION HAS A GOUGE WITH HIGH METAL (C-CHECK) RO 4/3/2020 REPAIRED LH UPPER C-DUCT HINGE BEAM, MIDDLE HINGE LUG AT AFT POSITION REF. BOMBARDIER REO. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CAR

Next page: https://openairdocs.org/aircraft/N753SK/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 = 'N753SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N753SK/reports

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