# Service difficulty reports: N752SK

A list on [N752SK](https://openairdocs.org/aircraft/N752SK.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 5 · 212 reports

- [SDR SWIA2026081576867](https://openairdocs.org/sdr/SWIA2026081576867.md): Duct · leaking · Aug 15, 2026 · N752SK · Cndair CL6002C10 · Pneumatic Distribution System
  > LEFT BLEED DUCT WARNING MESSAGE ON CLIMB OUT AT 12000 (FLIGHT 6234). ON ARRIVAL TO ACFT NO CURRENT WARNING MESSAGE WAS PRESENT. INTERROGATED MDC FOUND B1 007182. PERFORMED BLEED LEAK TEST IAW FIM 36-21-01. BLEED LEAK TEST PASSED. CHECKED EVENT LOCATION HIST
- [SDR SWIA202404290322](https://openairdocs.org/sdr/SWIA202404290322.md): Bulkhead · corroded · Mar 22, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LH FS. 280 LOWER BULKHEAD HAS CORROSION (LBL10 FLOOR LEVEL). (C-CHECK RO 4/26/2024) REPLACED THE LH FS280 LOWER BULKHEAD WEB. REF CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202404290319](https://openairdocs.org/sdr/SWIA202404290319.md): Floorbeam · corroded · Mar 19, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON L/H CROSSBEAM AT FS 280.0 UPON REMOVAL OF FLOOR SUPPORT ANGLE LBL 9.0 - RBL 9.0 (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW L/H CROSSBEAM AT FS 280.0 UPON REMOVAL OF FLOOR SUPPORT ANGLE LBL 9.0 - RBL 9.0 IAW DWG CC670-34010 REV. K
- [SDR SWI202404290346](https://openairdocs.org/sdr/SWI202404290346.md): Intercostal · corroded · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL MID DD4 CORRODED (C-CHECK RO 4/26/2024) INSTALLED NEW MID DD4 INTERCOSTAL REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWI2024042900345](https://openairdocs.org/sdr/SWI2024042900345.md): Intercostal · corroded · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL FWD DD5 CORRODED (C-CHECK RO 4/26/2024) REPLACED PAX DOOR FWD DD5 INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWI2024042900344](https://openairdocs.org/sdr/SWI2024042900344.md): Intercostal · corroded · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL AFT DD3 CORRODED (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR AFT DD3 INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWI2024042900343](https://openairdocs.org/sdr/SWI2024042900343.md): Intercostal · corroded · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL FWD DD3 CORRODED (C-CHECK RO 4/26/2024) REPLACED PAX DOOR FWD DD3 INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED
- [SDR SWI2024042900342](https://openairdocs.org/sdr/SWI2024042900342.md): Intercostal · corroded · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INTERCOSTAL DD7A CORRODED (C-CHECK RO 4/26/2024) INSTALLED NEW MID DD7A INTERCOSTAL REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWI2024042900341](https://openairdocs.org/sdr/SWI2024042900341.md): Door Frame · corroded · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR FRAME FS313.56 AND CLEAT BETWEEN DD4 & DD5 CORRODED (C-CHECK RO 4/26/2024) REPLACED PAX DOOR FRAME SECTION AND ATTACHING CLEAT AT FS 313.56 BETWEEN DD4 AND DD5 REF DWG 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK C
- [SDR SWI20240429000340](https://openairdocs.org/sdr/SWI20240429000340.md): Doubler · cracked · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT PULL-IN CAM DOUBLER IS CRACKED (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW AFT PULL-IN CAM DOUBLER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020 AND DWG 601R31702 REV. N. COMPLIE
- [SDR SWI2024042900339](https://openairdocs.org/sdr/SWI2024042900339.md): Doubler · cracked · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR FWD PULL-IN CAM DOUBLER IS CRACKED (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW FWD PULL-IN CAM DOUBLER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020 AND DWG 601R31702 REV. N. COMPLIE
- [SDR SWIA202404290313](https://openairdocs.org/sdr/SWIA202404290313.md): Frame · chafed · Mar 13, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FS1144.00 STRG 9RH FRAME IS CHAFFED BY THE WATER INJECTION LINE (MARKED) (C-CHECK RO 4/26/2024) REPAIRED CHAFFE ON FRAME AT FS 1144.00 STRG 9R REF REO 670-53-61-2251 REV -- DATED 2024-04-10. ALL STEPS OF REO COMPLIED WITH. M337 AND SKYWEST TASK CARD 51-90
- [SDR SWIA202404290312](https://openairdocs.org/sdr/SWIA202404290312.md): Window Post · cracked · Mar 12, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CO-PILOTS WINDSHIELD POST APPEARS CRACKED AT THE TOP BARREL NUT. (C-CHECK RO 4/26/2024) REMOVED CO-PILOT WINDSHIELD POST IAW CRJ 700 SRM 51-42-21-001-001-A01 AND NEW CO-PILOT WINDSHIELD POST P/N 601R33223-2 INSTALLED ALONG WITH NEW BARRELL NUTS P/N NAS577B
- [SDR SWIA2024042900310](https://openairdocs.org/sdr/SWIA2024042900310.md): Intercostal · corroded · Mar 10, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR AFT DD5 INTERCOSTAL HAS EXFOLIATED CORROSION ON TWO ELEMENT REQUIRE REPLACEMENT JOB # HN00144727 (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR AFT DD5 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CA
- [SDR SWIA2024042900308](https://openairdocs.org/sdr/SWIA2024042900308.md): Window Post · cracked · Mar 8, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PILOT SIDE WNDSHIELD POST IS CRACKED AT THE TOP BARREL-NUT HOLE. (MARKED) (C-CHECK RO 4/26/2024) REMOVED CRACKED PILOT SIDE WINDSHIELD POST REF CRJ700 SRM51-42-21-001-001-A01 AND INSTALLED NEW PILOT SIDE WINDSHIELD POST REF CRJ700 SRM 51-42-21-001-001-A01
- [SDR SWIA20240429306](https://openairdocs.org/sdr/SWIA20240429306.md): Floorbeam · cracked · Mar 6, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH COCKPIT FLOOR BEAM (RBL12) CRACKED AT THE BOTTOM OF THE AFT END FS280.00 CROSSBEAM (MARKED) (C-CHECK RO 4/26/2024) REMOVED CRACKED, RIGHT-HAND COCKPIT FLOOR BEAM (RBL 12), AT FS280.00, AND INSTALLED NEW FLOOR BEAM. REF. CRJ 700 SRM 53-11-43-201-003-A01
- [SDR SWI2024042900338](https://openairdocs.org/sdr/SWI2024042900338.md): Cargo Net · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD CARGO RESTRAINT NET AFT TIE DOWN PAD HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 4/26/2024) INSTALLED NEW TIE DOWN FITTING P/N SH670-33390-2. REF: DWG SH670-33600, REV: AD, CRJ700 SRM 51-42-21-001-001-A01 CRJ 700 SRM 51-42-06-001-001-A01, AND
- [SDR SWI2024042900337](https://openairdocs.org/sdr/SWI2024042900337.md): Door Sill · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL HAS CORROSION (C-CHECK RO 4/26/2024) REMOVED CORROSION FROM THE AFT BAGGAGE BAY DOOR SILL AND EVALUATED AS OUT-OF-LIMITS. REMOVED CORRODED SILL AND REPLACED WITH NEW SILL. REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-0
- [SDR SWI20240429000336](https://openairdocs.org/sdr/SWI20240429000336.md): Stringer · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER23L FS1000-FS985 HAS AREAS OF CORROSION (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED FORWARD SPLICE ANGLE, DRAIN LINE BRACKET AND NEW SECTION STRINGER 23L BETWEEN FS 977.00 - FS 1015.00 REF CRJ 700 SRM 53-00-03-201-001-A01 CRJ700 SRM 51-42-06-001-0
- [SDR SWI202404290335](https://openairdocs.org/sdr/SWI202404290335.md): Floor Support · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT RBL9 FS1031- FS1051 HAS LIGHT AREAS OF CORROSION (C-CHECK RO 4/26/2024) REPAIRED FLOOR BEAM AT RBL 9.0 BETWEEN F/S 985.00 TO F/S 1075.75 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2242 REV. -- DATED 2024-03-12 AND COMPLIED WITH SK
- [SDR SWI2024042900334](https://openairdocs.org/sdr/SWI2024042900334.md): Floor Support · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT LBL9 FS1015- FS1051 HAS AREAS OF CORROSION (C-CHECK RO 4/26/2024) REPAIRED FLOOR SUPPORT AT LBL 9.0 BETWEEN F/S 985.00 TO F/S 1075.75 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2242 REV. -- DATED 2024-03-12 AND COMPLIED WITH SK
- [SDR SWI2024F00333](https://openairdocs.org/sdr/SWI2024F00333.md): Floor Support · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT LBL27 FS1015- FS1051 HAS AREAS OF CORROSION. PERFORMED FLOOR SUPPORT CUTOUT REPAIR. IAW SRM 51-42-21-001-001-A01, REF SRM 53-00-41-201-001-A01 REV 38, REO 670-53-61-2247 REV--, AND DWG MM690-35041 REV AB. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWI2024042900332](https://openairdocs.org/sdr/SWI2024042900332.md): Frame · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS1015 STGR20L -STGR26L HAS SEVERAL AREAS OF CORROSION (C-CHECK RO 4/26/2024) REPLACED NEW LOWER FRAME SECTION FS.1015 BETWEEN STGR26R TO STGR20LH ERF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG MM670-36062 REV -E. COM
- [SDR SWI2024042900331](https://openairdocs.org/sdr/SWI2024042900331.md): Door · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD4 HAS CORROSION (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR FWD DD4 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWI202404290330](https://openairdocs.org/sdr/SWI202404290330.md): Former · corroded · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER BETWEEN DD5 AND DD7 HAS CORROSION (C-CHECK RO 4/26/2024) INSTALLED NEW PAX DOOR AFT FORMER IAW DWG 601R31702 REV. N AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWIA202404290305](https://openairdocs.org/sdr/SWIA202404290305.md): Channel · cracked · Mar 5, 2024 · N752SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT TRACK FORWARD LOWER SUPPORT FOR THE DOOR TRACK IS CRACKED. (MARKED) (C-CHECK RO 4/26/2024) REMOVED AND REPLACED WITH NEW CHANNEL P/N MM670-35552-005 ON AFT CARGO DOOR, LOWER AFT TRACK FRAME. REF; DWG MM670-35060, REV: W, CRJ700 SRM 51-
- [SDR SWIA202404290301](https://openairdocs.org/sdr/SWIA202404290301.md): Skin · gouged · Mar 1, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE SKIN IS CHAFED/GOUGED AT APPROX FS972 AT BL 0. (C-CHECK RO 4/26/2024) REPAIRED AFT LOWER FUSELAGE SKIN AT APPROX FS972 AT BL0 IRT REO 670-53-00-723 REV-- DATED 2024-03-29, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK PASSED
- [SDR SWI202404290329](https://openairdocs.org/sdr/SWI202404290329.md): Slat Track · worn · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > RIGHT WING LEADING EDGE SLAT TRACK ASSEMBLY NO. 3-3 HAS WARE MARKS, HN00142274 (C-CHECK RO 4/26/2024) REPAIRED RH WING SLAT TRACK ASSEBLY 3-3. PER REO 670-57-42-1495 REV -- DATED 2024-03-07 STEPS 1-8. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900
- [SDR SWI202404290328](https://openairdocs.org/sdr/SWI202404290328.md): Slat Track · worn · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING LEADING EDGE SLAT TRACK ASSEMBLY NO. 3-3 HAS WARE MARKS, HN00142273 (C-CHECK RO 4/28/2024) REPAIRED LEFT WING LEADING EDGE SLAT TRACK ASSEMBLY NO. 3-3 BY COMPLYING WITH REO 670-57-42-1494 REV -- DATED 2024-03-07, COMPLIED WITH 51-900-1002-SKY
- [SDR SWI202404290327](https://openairdocs.org/sdr/SWI202404290327.md): Stand Off · cracked · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REMOVED CRACKED INBD "A" BRACKET STANDOFF FROM R/H LWR TRANSCOWL REF CRJ 700 SRM 51-42-14-001-001-A01. INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON R/H LWR TRANSCOWL
- [SDR SWI2024042900326](https://openairdocs.org/sdr/SWI2024042900326.md): Latch · chafed · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > R/H UPPER TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 4/26/2024) REPAIRED R/H UPPER TRANS COWL OUTER SKIN / FWD. DISHING AND COMPLIED WITH ALL STEPS OF NEW FINAL REO 670-54-21-1622, REV. --, 2024-03-28. COMPLIED WITH M-337 & SKY CARD 51-900-1
- [SDR SWI202404290325](https://openairdocs.org/sdr/SWI202404290325.md): Stand Off · cracked · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.
- [SDR SWI20240429000324](https://openairdocs.org/sdr/SWI20240429000324.md): Bracket · cracked · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) INSTALLED A NEW O/B "A" BRACKET (PN CN624-2082-201) INTO L/H LWR TRANSCOWL REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION SHEET
- [SDR SWI2024042900323](https://openairdocs.org/sdr/SWI2024042900323.md): Skin · cracked · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL OUTER SKIN IS CRACKED @ LATCH SCREW HOLE. (C-CHECK RO 4/26/2024) L/H LWR TRANSCOWL OUTER SKIN HAS BEEN REPAIRED REF REO# 670-54-21-1623, REV --, DATED 3/18/24. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. REFER TO CONTINUATION SHEET FOR DETA
- [SDR SWIA20240229](https://openairdocs.org/sdr/SWIA20240229.md): Stand Off · cracked · Feb 29, 2024 · N752SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 4/26/2024) REMOVED AND REPLACED L/H UPPER TRANSCOWL I/B "A" BRACKET W/A NEW "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SK
- [SDR SWI2024042900322](https://openairdocs.org/sdr/SWI2024042900322.md): Pressure Switch · cracked · Feb 28, 2024 · N752SK · Cndair CL6002C10 · Emergency Exits
  > *R/H EMER EXIT HAS SUSPECTED CRACK AT THE BASE OF UPPER AFT FITTING (PROX SENSOR STRIKER FITTING). (C-CHECK RO 4/26/2024) THE CRACK ON UPPER FRAME WEB OF RH EMERGENCY EXIT WAS REPAIRED BY REINFORCEMENT PLATE (DOUBLER) AND REPAIR FILLER PER REO 670-52-21-09
- [SDR SWIA202404290228](https://openairdocs.org/sdr/SWIA202404290228.md): Fitting · cracked · Feb 28, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > *L/H EMER EXIT HAS SUSPECTED CRACK AT THE BASE OF UPPER AFT FITTING (PROX SENSOR STRIKER FITTING). (C-CHECK RO 4/26/2024) THE CRACK ON UPPER FRAME WEB OF LH EMERGENCY EXIT WAS REPAIRED BY REINFORCEMENT PLATE (DOUBLER) AND REPAIR FILLER PER REO 670-52-21-09
- [SDR SWIA202404290227](https://openairdocs.org/sdr/SWIA202404290227.md): Drag Angle · cracked · Feb 27, 2024 · N752SK · Cndair CL6002C10 · Vertical Stabilizer
  > LH VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 4/26/2024) PERFORMED LH VERTICAL STAB FWD DRAG ANGLE REPAIR. PER CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI202404290321](https://openairdocs.org/sdr/SWI202404290321.md): Stiffener · bent · Feb 25, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS 280 BULKHEAD, AFT LEFT SIDE UPPER STIFFENER ANGLE IS BENT. (C-CHECK RO 4/26/2024) REMOVED DAMAGED ANGLE AND REPLACED WITH NEW ANGLE P/N CC670-32449-1 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 AND DWG CC670-34010 REV-K, RII REQUIREMENT
- [SDR SWIA202404290225](https://openairdocs.org/sdr/SWIA202404290225.md): Landing · cracked · Feb 25, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT TRU BAY ( FORWARD EQUIPMENT COMPARTMENT) AFT DOOR LATCH CUTOUT HAS POSSIBLE CRACK. (C-CHECK RO 4/26/2024) VERIFIED AND CONFIRMED CRACK ON THE RIGHT-HAND TRU BAY DOOR LANDING. REPLACED RIGHT-HAND TRU DOOR LANDING REF. REO 670-53-11-1935 REV. -- DATE:
- [SDR SWI20240429000320](https://openairdocs.org/sdr/SWI20240429000320.md): Housing · gouged · Feb 23, 2024 · N752SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR HANDLE HOUSING HAS NUMEROUS GOUGES (C-CHECK RO 4/26/2024) REMOVED AND INSTALLED NEW DOOR HANDLE HOUSING P/N 119992-5. REF: CRJ-700 AMM 52-31-03-400-801-A01 REVISION 71: DEC 16/2022, CRJ700 SRM 51-42-21-001-001-A01 REVISION 38: JUL 25/
- [SDR SWIA2024042900223](https://openairdocs.org/sdr/SWIA2024042900223.md): Retainer · bent · Feb 23, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Structure
  > AFT BAGGAGE BAY DOOR LOWER CENTER SEAL RETAINER BENT IN AT FWD AND AFT STOP FITTINGS (C-CHECK RO 4/26/2024) REMOVED AND REPLACED WITH NEW AFT CARGO DOOR LOWER CENTER SEAL RETAINER REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-38702, REV -F. LEAK CHECK
- [SDR SWIA2024042900219](https://openairdocs.org/sdr/SWIA2024042900219.md): Skin · dented · Feb 19, 2024 · N752SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > ADM# N752SK-8069 L/H LOWER FUSELAGE TAIL AREA FS 1144.00, SMOOTH DENT L-2.8" W-1.55" D-.020". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 4/26/2024) REPAIRED DENT AT
- [SDR SWIA202404291004](https://openairdocs.org/sdr/SWIA202404291004.md): Skin · cracked · Oct 4, 2023 · N752SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA77176-670-53-11-1790 752SK MXCODEID61274-PR - FOUND CRACK ON THE LOWER AFT CORNER OF THE THE LH FORWARD ELECTRICAL BAY (TRU BAY). COMPLIED WITH REO 670-53-11-1790, REV.--, DATED 2022-02-15 FOR TEMPORARY DISPOSITION FO
- [SDR SWI2024F00097](https://openairdocs.org/sdr/SWI2024F00097.md): Stud · missing · Sep 1, 2023 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER SEAT 12AB IB FWD SEAT TRACK MOUNTING STUD IS MISSING THE LOCKING PLATE. PN 41031038-503 MR2184015 (FILED CLOSED)REMOVED AND REPLACED SEAT 12AB INBOARD FWD SEAT TRACK MOUNTING STUD IAW SAFRAN CMM 25-26-24.
- [SDR SWI2024F00098](https://openairdocs.org/sdr/SWI2024F00098.md): Stud · missing · Sep 1, 2023 · N752SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER SEAT 6AB IB FWD SEAT TRACK MOUNTING STUD IS MISSING THE LOCKING PLATE. PN 41031038-503 MR2184015 (FILED CLOSED)REMOVED AND REPLACED SEAT 6AB INBOARD FWD SEAT TRACK MOUNTING STUD IAW SAFRAN CMM 25-26-24.
- [SDR SWIA202161975](https://openairdocs.org/sdr/SWIA202161975.md): None · chafed · Oct 28, 2021 · N752SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FORM M-337, "REPORT OF AIRCRAFTMAJOR REPAIR. REQUIRED FOR REPAIR ON FRAME FS1162 HAS DAMAGE RH SIDE FROM CHAFFING (FILED CLOSED) COMPLIED WITH FORM M-337
- [SDR SWIA202161976](https://openairdocs.org/sdr/SWIA202161976.md): None · chafed · Oct 27, 2021 · N752SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS1162 HAS DAMAGE RH SIDE FROM CHAFFING. (FILED CLOSED) REPAIRED FRAME FS1162 BETWEEN STGR 7R AND STGR 8R IN ACCORDANCE WITH REO 670-53-71-084
- [SDR SWIA2020061051070](https://openairdocs.org/sdr/SWIA2020061051070.md): Threshold · cracked · Jun 3, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > COCKPIT FLOORBOARD THRESHOLD IS CRACKED. (C-CHECK) RO 4/24/2020 ORDERED, RECEIVED, AND INSTALLED 1 NEW COCKPIT THRESHOLD REF SRM.
- [SDR SWIA2020061051068](https://openairdocs.org/sdr/SWIA2020061051068.md): Floor Support · cracked · May 15, 2020 · N752SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT COCKPIT FLOOR SUPPORT ANGLE AT BL 12 (P/N CC670-33199-4) IS CRACKED. (C-CHECK) RO 4/24/2020 REMOVED AND REPLACED CRACKED RT COCKPIT FLOOR SUPPORT ANGLE WITH NEW FLOOR SUPPORT ANGLE (P/N CC670-33199-4) AT RBL 12, FS 259.20 TO FS 280.00 REF SRM, DWG. RESTORE

Next page: https://openairdocs.org/aircraft/N752SK/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 = 'N752SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N752SK/reports

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