# Service difficulty reports: N751SK

A list on [N751SK](https://openairdocs.org/aircraft/N751SK.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 · 172 reports

- [SDR SWIA2025052975500](https://openairdocs.org/sdr/SWIA2025052975500.md): Shaft · scored · May 29, 2025 · N751SK · Cndair CL6002C10 · Engine Mount Section
  > LEFT ENG AFT THRUST SHAFT SCORED WHERE SPHERICAL BUSHING ATTACHES (FILED CLOSED)REPLACED LH ENGINE AFT THRUST SHAFT WITH SERVICEABLE SHAFT PER AMM 71-22-01 SEE CP 30214479 FOR INSTALL OF LH ENGINE.
- [SDR SWIA202410140012](https://openairdocs.org/sdr/SWIA202410140012.md): Ballast · failed · Oct 12, 2024 · N751SK · Cndair CL6002C10 · Passenger Compartment Lighting
  > SHORT FINAL FA REPORTED SMOKE IN FIRST CLASS COMING FROM LEFT SIDE OVERHEAD BINS, SMOKE AND SMELL WENT AWAY UPON LANDING AND RETURNED AS SOON AS WE PARKED AT GATE. SMOKE WAS VERY LIGHT AND CLEAR WITH ELECTRICAL SMELL. (FLIGHT 6239 - FILED CLOSED)AFTER TALKING
- [SDR SWIA2024022001226](https://openairdocs.org/sdr/SWIA2024022001226.md): Skin · chafed · Dec 26, 2023 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR OUTER SKIN CHAFFED AT FWD AND AFT CAUSED BY HINGE PIN.JOB # HN00130384 (C-CHECK RO 2/19/2024) REPAIRED PAX DOOR OUTER SKIN FWD AND AFT IAW REO 670-52-11-1360 REV. -- DATED 2024-01-04 STEPS 1, 2, 3, 4 AND COMPLIED WITH TASK CARD 51-900-1002-SKY (C
- [SDR SWI202402200171](https://openairdocs.org/sdr/SWI202402200171.md): Fitting · gouged · Dec 22, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR SURROUND STRUCTURE AFT LOWER SHOOT BOLT FITTING GOUGED (C-CHECK RO 2/19/2024) REPAIRED PASSENGER DOOR SURROUND STRUCTURE AFT LOWER SHOOT BOLT FITTING BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2352 REV -- DATED 2023-12-29
- [SDR SWI202402200170](https://openairdocs.org/sdr/SWI202402200170.md): Housing · gouged · Dec 22, 2023 · N751SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT DOOR HANDLE HOUSING HAS NUMEROUS GOUGES (C-CHECK RO 2/19/2024) REPLACED AFT CARGO COMPARTMENT DOOR HANDLE HOUSING (PN# 119992-5) IAW CRJ700 SRM 51-42-21-001-001-A01, AND DWG# CC670-38702 REV-F. COMPLIED WITH SKYWEST TASK CARD 51-900-1
- [SDR SWI2024021900169](https://openairdocs.org/sdr/SWI2024021900169.md): Fitting · gouged · Dec 22, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR SURROUND STRUCTURE FORWARD LOWER SHOOT BOLT FITTING GOUGED (C-CHECK RO 2/19/2024) REPAIRED PASSENGER DOOR SURROUND STRUCTURE FORWARD LOWER SHOOT BOLT FITTING BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2352 REV -- DATED 2023-12-29 COMPLIED
- [SDR SWI2024022000118](https://openairdocs.org/sdr/SWI2024022000118.md): Hinge · gouged · Dec 15, 2023 · N751SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR FUSELAGE PIANO HINGE #1 LUG LANDING GOUGED HORIZONTAL SIDE (C-CHECK RO 2/19/2024) FOUND PAX DOOR PIANO HINGE OUT OF LIMITS PER REO 670-53-21-582 REV. F DATED 2017-08-02. REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE FUSELAGE SIDE IAW CRJ 70
- [SDR SWIA202402201212](https://openairdocs.org/sdr/SWIA202402201212.md): Mount · damaged · Dec 12, 2023 · N751SK · Cndair CL6002C10 · Engine Mount Section
  > DURING AUDIT OF 1C TASK CARD 54-440-301 (INTERNAL ZONAL INSPECTION OF THE RIGHT NACELLE), FOUND RH ENGINE FWD. ENGINE MOUNT HAS RUB MARKS ON LOWER SURFACES FROM HINGE LINE FAIRING PANELS. (C-CHECK RO 2/19/2024) COMPLIED WITH OF REO 670-71-21-094 REV.-- DAT
- [SDR SWI2024022000138](https://openairdocs.org/sdr/SWI2024022000138.md): Intercostal · corroded · Dec 11, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AT STR 21L INSIDE AVIONICS BAY IN BETWEEN FS310.0 AND FS 319.70 INTERCOSTAL HAS CORROSION. (C-CHECK RO 2/19/2024) REMOVED AND REPLACED INTERCOSTAL AT LH STGR21L BETWEEN FS.310 AND FS.333 WITH NEW REF. CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-
- [SDR SWI2024022000137](https://openairdocs.org/sdr/SWI2024022000137.md): Frame · corroded · Dec 11, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Frame
  > AT STR21L AVIONICS BAY AT FS 319.70 FRAME HAS CORROSION. (C-CHECK RO 2/19/2024) INSTALLED NEW FRAME FS. 319.70 BETWEEN STGR17L AND STGR21L REF. CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG #SH670-31810 REV. AE. COMPLIED WITH SKYWEST TASKC
- [SDR SWI202402190136](https://openairdocs.org/sdr/SWI202402190136.md): Skin · chafed · Dec 11, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING AUIDT OF 1C TASK CARD 53-150-502 (GENERAL VISUAL INSPECTION OF THE FORWARD BAGGAGE BAY DOOR, EXTERNAL SURROUND STRUCTURE AND FITTINGS €“ FS535.64 TO FS578.36, STGR19L TO STGR25L), FOUND CHAFFING ON FWD CARGO DOOR AREA, FUSELAGE SKIN UPPER EDGE. (C-C
- [SDR SWI2024022000172](https://openairdocs.org/sdr/SWI2024022000172.md): Structure · corroded · Dec 10, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND AT APPROXIMATELY FS 977.00 BETWEEN STGR 27 AND STGR 26L AS MARKED (C-CHECK RO 2/19/2024) REPAIRED CORROSION AT FS977 BETWEEN STGR 27 AND STGR 26L REF REO 670-53-00-715 REV -- DATE 2023-12-22 AND REO 670-53-00-290 REV -F DATE 2019/04/26. SEE
- [SDR SWIA202402201210](https://openairdocs.org/sdr/SWIA202402201210.md): Stop Fitting · worn · Dec 10, 2023 · N751SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR INTERNAL SURROUND STRUCTURE ALL FOUR DOOR STOP FITTINGS WORN (C-CHECK RO 2/19/2024) REMOVED/BLENDED DAMAGE FROM ALL FOUR DOOR STOP FITTINGS. REF: REO 670-53-61-2220 REV -- DATED 2023-12-29 STEPS 1-8. ALL LEAK AND OP CHECKS GOOD AT TH
- [SDR SWI2024022000135](https://openairdocs.org/sdr/SWI2024022000135.md): Angle · corroded · Dec 9, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY DOOR INTERNAL SURROUND HAS CORRODED CLIP APPROXIMATELY BETWEEN FS 533.0 AND FS 549.00 STGR 18L AS MARKED (C-CHECK RO 2/19/2024) INSTALLED NEW CLIP P/N: SH670-33796-1 AT FWD BAGGAGE BAY DOOR INTERNAL SURROUND, FS 549.00 STGR 18L REF. CR
- [SDR SWI2024022000134](https://openairdocs.org/sdr/SWI2024022000134.md): Door Frame · corroded · Dec 9, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD BAGGAGE BAY LOWER SURROUND CORRODED AS MARKED (C-CHECK RO 2/19/2024) REPAIRED 2 EA. CORRODED AREAS ON THE FORWARD BAGGAGE BAY SURROUND AT MARKED AREAS REF REO 670-53-31-844 REV --,DATED 2024-01-09. SEE CONTINUATION FOR DETAILS.
- [SDR SWI202402200133](https://openairdocs.org/sdr/SWI202402200133.md): Angle · corroded · Dec 9, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY INTERNAL SURROUND HAS CORRODED CLIP APPROXIMATELY BETWEEN FS 533.00 AND FS 549.00 STGR 18L AS MARKED (C-CHECK RO 2/19/2024) REMOVED CORRODED AND INSTALLED NEW "CLIP"/ STUB FRAME P/N-SH670-33177-1. REF: CRJ-700 S.R.M.51-42-06-001-001-A0
- [SDR SWI2024022000132](https://openairdocs.org/sdr/SWI2024022000132.md): Floorbeam · damaged · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT FS 1000.00 LBL 21 HAS PITTING AS MARKED (C-CHECK RO 2/19/2024) INSTALLED NEW SECTION FLOOR BEAM AT LBL 27.00 FS 1000.00 TO FS 1051.00 REF CRJ700 SRM 53-00-41-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR
- [SDR SWI2024022000131](https://openairdocs.org/sdr/SWI2024022000131.md): Bolt · corroded · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SILL CORROSION (C-CHECK RO 2/19/2024) INSTALLED NEW GALLEY SERVICE DOOR SILL SEAL STRIKER REF: CRJ-700 SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01 & DWG-SH670-31412 REV-C. PERFORMED PRESSURE LEAK CHECK OF GALLEY SERVICE DOOR SEAL STR
- [SDR SWI2024022000130](https://openairdocs.org/sdr/SWI2024022000130.md): Angle · corroded · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT HAND PRESSURE FLOOR ANGLE HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 2/19/2024) REPAIRED LEFT HAND PRESSURE FLOOR ANGLE BY PERFORMING REO 670-53-41-652 REV -- DATED 2023-12-27 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWI202402200129](https://openairdocs.org/sdr/SWI202402200129.md): Floor Support · corroded · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT SIDE FLOOR SILL AT APPROXIMATE FS 989.00 HAS A CORRODED SPOT AS MARKED (C-CHECK RO 2/19/2024) CUT AWAY DAMAGED LEFT SIDE FLOOR SILL AT APPROXIMATE BETWEEN FS969 - FS989.00, FABRICATED AND INSTALLED ALL REPAIR PARTS REF REO 670-53-51-274 REV. -- DATE:
- [SDR SWI202402200128](https://openairdocs.org/sdr/SWI202402200128.md): Floorbeam · cracked · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 CLIP CRACKED ON FLOOR BEAM RBL12 (C-CHECK RO 2/19/2024) INSTALLED NEW CLIP P/N CC670-34099-2 ON RBL12 FS280 FLOOR BEAM REF CRJ700 SRM 51-42-21-001-001-A01, DWG CC670-34010 REV J AND DWG BA670-31057 REV L. COMPLIED WITH SKYWEST TASCK CARD 51-900-1002
- [SDR SWI202402200127](https://openairdocs.org/sdr/SWI202402200127.md): Pressure Deck · corroded · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT HAND PRESSURE FLOOR HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 2/19/2024) REPAIRED LEFT HAND PRESSURE FLOOR BY PERFORMING REO 670-53-41-652 REV -- DATED 2023-12-27 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWI202402200126](https://openairdocs.org/sdr/SWI202402200126.md): Floor Support · corroded · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT SILL CORROSION FS280.0 - FS319.7 (C-CHECK RO 2/19/2024) INSTALLED REPLACEMENT SILL REF DRW. SH670-32170 REV. N, REF CRJ700 SRM 51-42-06-001-001-A01, REF CRJ700 SRM 51-42-13-001-001-A01, AND REF CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH SKYWEST T
- [SDR SWI20240219000125](https://openairdocs.org/sdr/SWI20240219000125.md): Skin · gouged · Dec 8, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING AUDIT OF 1C TASK CARD 53-900-304 (EXTERNAL ZONAL INSPECTION OF THE REAR FUSELAGE - FS977.00 TO FS1098.20 BELOW WL72.50), FOUND A GOUGE IN THE EXTERNAL SKIN APPROXIMATELY 2" LONG AT STRG 27 JUST AFT OF FS977.00. (C-CHECK RO 2/19/2024) REPAIRED GOUGE
- [SDR SWI2024022000123](https://openairdocs.org/sdr/SWI2024022000123.md): Slider · chafed · Dec 6, 2023 · N751SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > R/H LWR TRANSCOWL OTBD SLIDER IS CHAFED. (C-CHECK RO 2/19/2024) REPAIRED R/H LWR TRANSCOWL O/B SLIDER BY COMPLYING W/ALL STEPS OF REO 670-54-21-1606, REV -- DATED 2023-12-26. AS WELL AS COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWI2024022000122](https://openairdocs.org/sdr/SWI2024022000122.md): Bracket · cracked · Dec 6, 2023 · N751SK · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > R/H LWR TRANSCOWL INBD "A" BRACKET IS CRACKED. (C-CHECK RO 2/19/2024) INSTALLED NEW I/B "A" BRACKET (PN CN624-2082-201) INTO R/H LWR TRANSCOWL REF REO# 670-54-21-971, REV B, DATED 11/28/23, CRJ 700 SRM 51-42-14-001-001-A01, AND SRM 51-42-20-001-001-A01
- [SDR SWI2024022000119](https://openairdocs.org/sdr/SWI2024022000119.md): Bulkhead · bent · Dec 2, 2023 · N751SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > BULKHEAD ASSEMBLY FS280.0 LEFT AFT FACE VARIOUS BENT AREAS (C-CHECK RO 2/19/2024) REPAIRED FS280 BULKHEAD AFT SIDE STIFFENERS REF REO 670-53-11-1909 REV -- DATED 2023-12-19 STEPS 1-5 AND REF REO 670-53-11-1910 REV -- DATED 2023-12-19 STEPS 1-14. ALL STEPS
- [SDR SWIA2024022031202](https://openairdocs.org/sdr/SWIA2024022031202.md): Unknown · cracked · Dec 2, 2023 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH TRU BAY, AFT LANDING IS POSSIBLY CRACKED. FLAGGED (C-CHECK RO 2/19/2024) REMOVED, FABRICATED AND INSTALLED NEW -7 REPAIR DOUBLER ONLY, ON R/H TRU BAY FLOOR REF CRJ 700 SRM 51-42-06-001-001-A01 AND PREVIOSLY INCORPERATED REO 670-53-11-509 REV.-E DATED
- [SDR SWIA202402201201](https://openairdocs.org/sdr/SWIA202402201201.md): Skin · gouged · Dec 1, 2023 · N751SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FORWARD BAGGAGE BAY DOOR INNER SKIN GOUGED FORWARD LOWER SIDE (C-CHECK RO 2/19/2024) REPAIRED GOUGED DAMAGE ON FORWARD BAGGAGE BAY DOOR INNER SKIN AT FORWARD LOWER SIDE REO 670-52-35-473 REV -- DATED 2024-01-02. REWORKED AREA ON EDGE HAS DIMENSION.450"
- [SDR SWIA2024022001130](https://openairdocs.org/sdr/SWIA2024022001130.md): Arm · worn · Nov 30, 2023 · N751SK · Cndair CL6002C10 · Emergency Exits
  > CREW ESCAPE HATCH LH AND RH HINGE ARMS CONTACT POINTS FOR HINGE BOLTS WORN/ELONGATED (C-CHECK RO 2/19/2024) REPAIRED CREW ESCAPE HATCH LH AND RH HINGE ARMS CONTACT POINTS FOR HINGE BOLTS REF. REO 670-52-22-017 REV -- DATED 2023-12-14 COMPLIED WITH SKYWEST
- [SDR SWIA202402201128](https://openairdocs.org/sdr/SWIA202402201128.md): Vane · chafed · Nov 28, 2023 · N751SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED BETWEEN FLAP ACTUATORS 2 AND 3 (COUNTING FROM THE INBOARD END). (C-CHECK RO 2/19/2024) DAMAGE IS LOCATED ON RUB CAP, NO ALLOWABLE LIMITS GIVEN AND PART REQUIRES REPLACEMENT. REMOVED BAD CAP REF CRJ700 SR
- [SDR SWIA2021081960374](https://openairdocs.org/sdr/SWIA2021081960374.md): Handle · failed · Aug 17, 2021 · N751SK · Cndair CL6002C10 · Landing Gear Selector
  > LANDING GEAR DISAGREE WARNING MESSAGE ON APPROACH. GEAR WOULD NOT COME DOWN. RAN QRH PROCEDURE AND IT FINALLY CAME DOWN WITH THE MANUAL EXTENSION. SUSPECT THE NOSE GEAR TO BE THE PROBLEM AS IT TOOK THE LONGEST TO COME DOWN AND THERE WAS NO PREVIOUS SOUND FROM
- [SDR SWIA2021062959181](https://openairdocs.org/sdr/SWIA2021062959181.md): Window · glazed · Jun 28, 2021 · N751SK · Cndair CL6002C10 · Flight Compartment Windows
  > FO SIDE WINDOW GLAZED, REQUIRES REPLACEMENT. REMOVED FO SIDE WINDOW REFERENCING AMM 56-12-01. SEE ML 23037834 FOR INSTALLATION OF NEW WINDOW AND PARTS INFO.
- [SDR SWIA202155453](https://openairdocs.org/sdr/SWIA202155453.md): Window Post · cracked · Jan 8, 2021 · N751SK · Cndair CL6002C10 · Fuselage Main, Structure
  > TRANSFER FROM EAML 556587: DURING THE REPLACEMENT OF SIDE WINDOW, FOUND A CRACK ON LT SIDE POST (P/N 601R33223-1 REF). THE CRACK GOES THROUGH THE FULL THICKNESS OF THE WEB FROM FWD SURFACE TILL THE BARREL NUT HOLE. LOWER PORTION OF THE WEB BELOW BARREL NUT H
- [SDR SWIA202155101](https://openairdocs.org/sdr/SWIA202155101.md): Windshield · cracked · Jan 6, 2021 · N751SK · Cndair CL6002C10 · Flight Compartment Windows
  > CAPT REPORTED CAPT'S FWD W/S SHATTERED AT 370' AND DIVERTED TO ICT. REMOVED LT SIDE COCKPIT WINDSHIELD REFERENCING CRJ700 AMM 56-11-01. DURING INSPECTION OF LT SIDE WINDSHIELD SILL AND SIDE POST, FOUND CRACK FORMING AROUND THE OUTBOARD WEB (WEB ABOVE BARREL
- [SDR SWIA202005110594](https://openairdocs.org/sdr/SWIA202005110594.md): Support Angle · cracked · Apr 22, 2020 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH COCKPIT FLOOR SUPPORT ANGLE FOUND CRACKED DURING FS274 LBL12 BEAM REPAIR. (C-CHECK) RO 5/7/2020 REMOVED AND REPLACED NEW L/H COCKPIT FLOOR SUPPORT ANGLE AT FS259.16 €“ FS280.00 LBL12 REF CRJ700 SRM AND CRJ700 SRM.
- [SDR SWIA202005110592](https://openairdocs.org/sdr/SWIA202005110592.md): Angle · corroded · Apr 21, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR ANGLE @ DD7A NEAR HOUSING FOR OUTER HANDLE IS CORRODED (C-CHECK) RO 5/7/2020 REPLACED PAX DOOR ANGLE AT DD7A NEAR HOUSING FOR OUTER HANDLE AS PER CRJ 700 SRM. COMPLIED WITH -SKY.LEAK CHECKS GOOD.
- [SDR SWIA202005110591](https://openairdocs.org/sdr/SWIA202005110591.md): Former · corroded · Apr 21, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER FS329.41 DD5 AND DD6 HAS CORROSION (C-CHECK) RO 5/7/2020 REPLACED PAX DOOR FORMER AT FS 329.41 DD5 AND DD6 AS PER CRJ 700 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA202005110590](https://openairdocs.org/sdr/SWIA202005110590.md): Intercostal · corroded · Apr 21, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 FS323.00 TO FS335.00 IS CORRODED (C-CHECK) RO 5/7/2020 INSTALLED NEW INTERCOSTAL DD1 P/N 601R318067-5 ON PAX DOOR REF BOMBARDIER DWG AND CRJ700 SRM. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.
- [SDR SWIA202005110589](https://openairdocs.org/sdr/SWIA202005110589.md): Intercostal · cracked · Apr 19, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 P/N 601R31902-318 IS CRACKED (C-CHECK) RO 5/7/2020 REPLACED INTERCOSTAL DD1 ON PAX DOOR REF CRJ 700 SRM AND BOMBARDIER DWG
- [SDR SWIA202005110588](https://openairdocs.org/sdr/SWIA202005110588.md): Intercostal · corroded · Apr 17, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS338.963 AND FS347.25 HAS CORROSION. (C-CHECK) RO 5/7/2020 REPLACED PAX DOOR INTERCOSTAL AT DD5 PER SRM & BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.
- [SDR SWIA202005110587](https://openairdocs.org/sdr/SWIA202005110587.md): Intercostal · corroded · Apr 17, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD4 BETWEEN FS338.963 AND FS347.25 HAS CORROSION. (C-CHECK) RO 5/7/2020 REPLACED PAX DOOR INTERCOSTAL AT DD4 PER SRM & BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD
- [SDR SWIA202005110586](https://openairdocs.org/sdr/SWIA202005110586.md): Floorbeam · cracked · Apr 16, 2020 · N751SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH COCKPIT FLOOR SUPPORT FLOOR BEAM CRACKED AT FS274, LBL12 AT AFT RADIUS (C-CHECK) RO 5/7/2020 CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND APPLIED REPAIR TO LH COCKPIT FLOOR SUPPORT BEAM AT FS274.00, LBL12.00. SEE ATTACHED CONTINUE CARD FOR DETAILS OF WO
- [SDR SWIA202005110593](https://openairdocs.org/sdr/SWIA202005110593.md): Support · cracked · Apr 15, 2020 · N751SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR RH SUPPORT FOUND TO BE CRACKED (C-CHECK) RO 5/7/2020 REPLACED COCKPIT FLOOR RH SUPPORT REF CRJ-700 SRM
- [SDR SWIA202005110585](https://openairdocs.org/sdr/SWIA202005110585.md): Intercostal · corroded · Apr 15, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD2 PN.601R318053-3 HAS CORROSION (C-CHECK) RO 5/7/2020 REPLACED PAX DOOR INTERCOSTAL DD2 PER SRM & BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD
- [SDR SWIA202005110584](https://openairdocs.org/sdr/SWIA202005110584.md): Floorbeam · corroded · Apr 15, 2020 · N751SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > * FLOOR SUPPORT STRUCTURE - FLOOR BEAM - LBL27 AT APPROXIMATELY FS1031.00: SIGNS OF CORROSION MARKED. (C-CHECK) RO 5/7/2020 COMPLIED WITH BEAM SPLICE REPAIR REF CRJ-700 SRM AND BOMBARDIER REO. COMPLIED WITH SKYWEST TASK CARD AND FORM M-337.
- [SDR SWIA202005110583](https://openairdocs.org/sdr/SWIA202005110583.md): Floorbeam · cracked · Apr 15, 2020 · N751SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH COCKPIT FLOOR SUPPORT FLOOR BEAM CRACKED AT FS274, RBL12 AT AFT RADIUS (C-CHECK) RO 5/7/2020 PERFORMED REPAIR TO RH COCKPIT FLOOR SUPPORT FLOOR BEAM AT FS274, RBL12 REF CRJ-700 SRM PERMANENT REPAIR TYPE 4. COMPLIED WITH TASK CARD (CL600-2C10) STRUCTURAL
- [SDR SWIA202005110582](https://openairdocs.org/sdr/SWIA202005110582.md): Intercostal · corroded · Apr 15, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR: INTERCOSTAL DD5 P/N 601R318091-5 HAS CORROSION (C-CHECK) RO 5/7/2020 REPLACED PAX DOOR INTERCOSTAL DD5 PER SRM & BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD
- [SDR SWIA202005110581](https://openairdocs.org/sdr/SWIA202005110581.md): Door Frame · corroded · Apr 15, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR: FRAME LOCATED AT FS313.56 BETWEEN DD4 AND DD5 IS CORRODED. (C-CHECK) RO 5/7/2020 REPLACED PASSENGER DOOR FRAME AT FS 313.56 BETWEEN DD4 AND DD5 AS PER CRJ 700 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.
- [SDR SWIA202005110580](https://openairdocs.org/sdr/SWIA202005110580.md): Former · corroded · Apr 14, 2020 · N751SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *PAX DOOR FWD FORMER HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO 5/7/2020 REMOVED AND REPLACED PAX DOOR FWD FORMER REF CRJ 700 SRM & BOMBARDIER DWG. CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD.

Next page: https://openairdocs.org/aircraft/N751SK/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 = 'N751SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N751SK/reports

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