# Service difficulty reports: N755SK

A list on [N755SK](https://openairdocs.org/aircraft/N755SK.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 · 171 reports

- [SDR SWIA2026042975957](https://openairdocs.org/sdr/SWIA2026042975957.md): Motor · faulted · Apr 29, 2026 · N755SK · Cndair CL6002C10 · Stabilizer Position Indicating
  > SHORTLY AFTER ENGAGING AUTOPILOT, STAB CH1 STATUS MESSAGE DISPLAYED FOLLOWED BY AN AP PITCH TRIM CAUTION AND STAB TRIM RUNAWAY AURAL WARNING. FOLLOWED QRC AND QRH FOR RUNAWAY AND THE MESSAGES RESULTING IN FLYING AND LANDING WITH STAB TRIM AND MACH TRIM DISENGA
- [SDR SWI2025F00749](https://openairdocs.org/sdr/SWI2025F00749.md): Warning Message · illuminated · Jun 19, 2025 · N755SK · Cndair CL6002C10 · Engine Bleed Air System
  > R BLEED DUCT WARNING RCVD IN CLIMB, QRH COMPLETED HOWEVER BOTH ENG BLEED VALVES CLOSED WITH LOSS OF PRESSURIZATION. (FLIGHT 4994 - FILED CLOSED)PLEASE REFERENCE AML 1634464 AND 1635217 AND 1635200 AND 1633555 FOR ALL WORK ACCOMPLISHED. A/C OK FOR SERVICE.
- [SDR SWIA202506190018](https://openairdocs.org/sdr/SWIA202506190018.md): Elec Connector · damaged · Jun 18, 2025 · N755SK · Cndair CL6002C10 · Fire Detection
  > DURING CLIMB OUT, RECEIVED R BLEED DUCT WARNING MESSAGE. COMPLIED WITH QRH. RETURNED TO KPHX. (FLIGHT 6291 - FILED CLOSED)INTERROGATED MDC AND FOUND B1-007664 FLAGGING R BLEED LOOP B, TROUBLESHOT PER FIM 36-23-03 USING THE AILC BREAKOUT BOX FOUND R BLEED LOO
- [SDR SWIA202411251008](https://openairdocs.org/sdr/SWIA202411251008.md): Structure · gouged · Oct 8, 2024 · N755SK · Cndair CL6002C10 · Passenger/Crew Doors
  > FUSELAGE AT PAX DOOR FWD LOWER CORNER GOUGED. BLENDED OUT DAMAGE ON FUSELAGE AT PAX DOOR LOWER FWD CORNER IAW CRJ700 SRM 51-12-00, 51-26-01 AND MHIRJ AVIATION GROUP EMAIL TICKET#34517 DATED 16OCT2024 AND EVALUATED. NO ALLOWABLE DAMAGE PERMITTED IN THIS AREA I
- [SDR SWI2024F01287](https://openairdocs.org/sdr/SWI2024F01287.md): Bracket · cracked · Aug 25, 2024 · N755SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING #1 SLAT #3 SLAT TRACK BOX BRACKET CRACKED. (C-CHECK RO 11/24/2024) REPAIRED RH WING #1 SLAT #3 SLAT TRACK BOX BRACKET IAW BOMBARDIER R.E.O. 670-57-42-557 REV -- DATE: 2016-12-02 AND CRJ700 AMM 28-11-00.
- [SDR SWIA20241125825](https://openairdocs.org/sdr/SWIA20241125825.md): Bracket · cracked · Aug 25, 2024 · N755SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H WING #1 SLAT #3 SLAT TRACK BOX BRACKET CRACKED (C-CHECK RO 11/24/2024) PERFORMED REPAIR AT L/H WING #1 SLAT #3 SLAT TRACK BOX BRACKET IAW REO 670-57-42-577 REV -- DATED 2016-12-02,CRJ 700 AMM 28-11-00.
- [SDR SWIA202411250824](https://openairdocs.org/sdr/SWIA202411250824.md): Hinge · gouged · Aug 24, 2024 · N755SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE DOOR SIDE HAS A GOUGE AT THE AFT END. REPAIRED PAX DOOR HINGE (DOOR SIDE) IAW BOMBARDIER REO 670-52-11-511 REV. -E DATE: 2017-08-02, CRJ700 SRM 51-21-11, 51-25-06, 51-25-16, AND CRJ700 AMM 52-11-00.
- [SDR SWIA2024112501824](https://openairdocs.org/sdr/SWIA2024112501824.md): Floorbeam · cracked · Aug 24, 2024 · N755SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR BEAM LBL12 CRACKED AT 280 BEAM (C-CHECK RO 11/24/2024) PERFORMED REPAIR TYPE 4 ON COCKPIT FLOOR BEAM LBL12 AT 280 BEAM PER BOMBARDIER REO 670-53-11-896. REV. --. DATE: 2015-03-17. AND CRJ-700 SRM 51-40-11, SRM 51-21-11, SRM 51-25-06, SRM
- [SDR SWIA2024112500813](https://openairdocs.org/sdr/SWIA2024112500813.md): Skin · dented · Aug 13, 2024 · N755SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH IB FLAP BOTTOM SURFACE HAS A DENT EVAL (C-CHECK RO 11/24/2024) PERFORMED REPAIR ON RH IB FLAP BOTTOM SURFACE PER BOMBARDIER REO 670-57-52-160. REV. -A. DATE: 2016-10-21. AND CRJ-700 SRM 51-26-01, SRM 57-52-01, SRM 51-40-11, SRM 51-26-00, SRM 51-25-01
- [SDR SWIA2024112500811](https://openairdocs.org/sdr/SWIA2024112500811.md): Skin · dented · Aug 11, 2024 · N755SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD EDGE DENTED AT THE EDGE. EVAL AND REPAIR (C-CHECK RO 11/24/2024) PERFORMED TEMP REPAIR ON DAMAGE AREA AT AFT CARGO DOOR FWD EDGE IAW CRJ 700 SRM 52-00-01,MHIRJ AVIATION GROUPEMAIL TICKET# 32545 DATED 2024-09-07,SRM 51-12-00,SRM 51-42-
- [SDR SWIA20231026005](https://openairdocs.org/sdr/SWIA20231026005.md): Unknown · cracked · Oct 25, 2023 · N755SK · Cndair CL6002C10 · Flight Compartment Windows
  > IN CLIMB, FO NOTICED HIS WINDOW GETTING BUBBLING AND I TURNED OFF RIGHT WINDOW HEAT, ABOUT 2 MINUTES LATER IT CRACKED THE OUTER PANE, QRH COMPLETED AND DIVERT TO KFAT (FLIGHT 3247 FILED OPEN)
- [SDR SWIA2023010967085](https://openairdocs.org/sdr/SWIA2023010967085.md): Trim System · faulted · Jan 8, 2023 · N755SK · Cndair CL6002C10 · Stabilizer Control System
  > ON CLIMB OUT STAB TRIM RUNAWAY TO THE NOSE DOWN POSITION. DISCONNECTED TRIM. HAND FLEW AIRCRAFT TO LANDING. (FLIGHT 4953 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26049587 WITH THE FOLLOWING CORRECTIVE ACTION: "INTERAGATED MDC FOR CORRA
- [SDR SWIA202155342](https://openairdocs.org/sdr/SWIA202155342.md): Floor Panel · punctured · Jan 3, 2021 · N755SK · Cndair CL6002C10 · Fuselage Floor Panel
  > FOUND PUNCTURE IN COCKPIT FLOOR UNDER CO-PILOT SEAT BETWEEN OUTBOARD SEAT RAIL AND SIDE CONSOLE. C-CHECK RO 1/6/2021. C/W REPAIR OF RT COCKPIT FLOOR PUNCTURE, IAW REO 670-53-11-1639 REV-A DATE 2021-01-05. MAJOR REPAIR TASK 51-900-1002-SKY AND FORM M337 ATTA
- [SDR SWIA202055325](https://openairdocs.org/sdr/SWIA202055325.md): Skin · chafed · Dec 9, 2020 · N755SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CHAFED AT FS 984 TO FS 983 IN PREVIOUSLY BLENDED AREA APPROXIMATELY.060 WIDE BY.-05 DEEP BY 3 IN LONG. ALSO PANEL 196DR NUPLATE CHANNEL IS CHAFED AND WILL NEED THE TO REACCOMPLISHED. C-CHECK RO 1/6/2021 REPAIRED DAMAGE, IAW REO 670-53
- [SDR SWIA202055369](https://openairdocs.org/sdr/SWIA202055369.md): Attach Angle · corroded · Dec 3, 2020 · N755SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > RT CABIN FLOOR SILL ATTACH ANGLE CORRODED AT FS 319.70 AT RBL 36. C-CHECK RO 1/6/2021. REMOVED AND REPLACED ATTACH ANGLE, IAW CRJ 700 SRM 51-42-06-001-001 (A01) AND 51-42-21-001-001 (A01). SEE CONTINUECARD FOR MAINTENANCE PERFORMED.
- [SDR SWIA202055341](https://openairdocs.org/sdr/SWIA202055341.md): Striker · gouged · Dec 3, 2020 · N755SK · Cndair CL6002C10 · Passenger/Crew Doors
  > WHILE REPLACING HINGE ON FUSELAGE FOR PASSENGER DOOR FOUND PASSENGER DOOR LOWER STRIKER TO HAVE NUMEROUS GOUGES ALONG EDGE. C-CHECK RO 1/6/2021. REMOVED AND REPLACED PASSENGER DOOR LOWER STRIKER, IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR SWIA202055322](https://openairdocs.org/sdr/SWIA202055322.md): Hinge · damaged · Dec 2, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE (FUSELAGE SIDE) REQUIRES REPLACEMENT. C-CHECK RO 1/6/2021. C/W REPLACEMENT OF PAX DOOR HINGE, IAW CRJ 700 SRM 53-21-23-201-007 (A01). PRESSURE CHECK GOOD NO LEAKS FOUND. SEE CONTINUE CARD FOR MIANTENANCE PERFORMED.
- [SDR SWIA202055340](https://openairdocs.org/sdr/SWIA202055340.md): Frame · corroded · Dec 1, 2020 · N755SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 319.70 STGR 17L-20L FRAME CORROSION. C-CHECK RO 1/6/2021. REMOVED AND REPLACED FRAME SEGMENT AT FS 319.70 STR 17L TO 20L, IAW CRJ 700 SRM 51-42-06-001-001 (A01) AND 51-42-21-001-001 (A01) LEAK CHECK GOOD. SEE CONTINUE CARD FOR MAINTENANCE PERFORMED.
- [SDR SWIA202055319](https://openairdocs.org/sdr/SWIA202055319.md): Hinge · gouged · Nov 25, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > NUMEROUS PAX DOOR HINGE LUGS ARE GOUGED AND LUG LANDS ARE CHAFED. C-CHECK RO 1/6/2021. REPAIRED GOUGED AND CHAFED PAX DOOR HINGE LUGS, IAW REO 670-52-11-511 REV-E, DATED 2017-08-02.
- [SDR SWIA202055335](https://openairdocs.org/sdr/SWIA202055335.md): Beam · corroded · Nov 23, 2020 · N755SK · Cndair CL6002C10 · Fuselage Main, Structure
  > RT AFT CARGO COMPARTMENT FLOOR SILL IS CORRODED BETWEEN FS 1031.00 AND FS 1051.00 RBL 36. C-CHECK RO 1/6/2021. REMOVED RT SIDE CARGO SILL PLATE BETWEEN FS 1031.00 AND FS 1051.00 RBL 36. LOCATED AND INSTALLED NEW SERVICEABLE FLOOR SILL PLATE, IAW CRJ 200 SRM
- [SDR SWIA202055368](https://openairdocs.org/sdr/SWIA202055368.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE CABIN SIDE SEAT RAIL FS 893 TO 969 CORRODED (TRANSFERRED FROM CAMP 21870750). C-CHECK RO 1/6/2021. INSTALLED REPLACEMENT SEAT RAIL FS 893 TO 969, IAW CRJ700 AMM 53-00-49-400-801 (CONFIG 3). REF CONTINUE CARD FOR DETAILS OF WORK.
- [SDR SWIA202055367](https://openairdocs.org/sdr/SWIA202055367.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE CABIN SIDE SEAT RAIL FS 677 TO 761 CORRODED (TRANSFERRED FROM CAMP 21870745). C-CHECK RO 1/6/2021. REMOVED AND INSTALLED NEW SERVICEABLE RT CABIN SIDE SEAT RAIL FROM FS 677 TO FS 761, IAW CRJ-700 AMM 53-00-49-400-401. REF CONTINUE CARD FOR DETAIL
- [SDR SWIA202055366](https://openairdocs.org/sdr/SWIA202055366.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE CABIN SIDE SEAT RAIL FS 379 TO 485 CORRODED (TRANSFERED FROM CAMP 21870742). C-CHECK RO 1/6/2021. REMOVED AND REPLACED SEAT RAIL AT LOCATION RIGHT FS 565-677, IAW CRJ 700 AMM 53-00-49-000/4000-801 (A03).
- [SDR SWIA202055365](https://openairdocs.org/sdr/SWIA202055365.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE CABIN SIDE SEAT RAIL FS 379 TO 485 CORRODED (TRANSFERRED FROM CAMP 21870738). C-CHECK RO 1/6/2021. REMOVED AND REPLACED FS 379-FS 485 SEAT RAIL, IAW CRJ 700 AMM 53-00-49-000/400-801 (A03). SEE CONTINUE CARD FOR MAINTENANCE PERFORMED.
- [SDR SWIA202055364](https://openairdocs.org/sdr/SWIA202055364.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT CABIN SIDE SEAT RAIL FS 785-FS 863 CORRODED (TRANSFERED FROM CAMP 21870733). C-CHECK RO 1/6/2021. REMOVED AND REPLACED SEAT RAIL AT FS 785-FS 863, IAW CRJ 700 AMM 53-00-49-000/400-801 (A03). SEE CONTINUE CARD FOR MAINTNEANCE PERFORMED.
- [SDR SWIA202055363](https://openairdocs.org/sdr/SWIA202055363.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE CABIN SIDE SEAT RAIL FS 724.08-761.85 CORRODED (TRANSFERED FROM CAMP 21870728). C-CHECK RO 1/6/2021. REMOVED AND INSTALLED FS 724.08-761.85 SEAT RAIL, IAW CRJ 700 AMM 53-00-49-00/400-801 (A03). SEE CONTINUE CARD FOR MAINTENANCE PERFORMED.
- [SDR SWIA202055362](https://openairdocs.org/sdr/SWIA202055362.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN FLOOR SEAT RAIL AT RBL 9 IS CORRODED BETWEEN FS 581.00 AND FS 693.00. C-CHECK RO 1/6/2021. REMOVED AND REPLACED SEAT RAIL WITH A SERVICEABLE UNIT, IAW CRJ-700 AMM 53-00-49-000-801-A03 AND IAW CRJ-700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202055361](https://openairdocs.org/sdr/SWIA202055361.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE CABIN SEAT RAIL FS 677-FS 724.06 CORROSION (TRANSFERRED FORM CAMP 21870717). C-CHECK RO 1/6/2021. REMOVED AND REPLACED TWO SEAT RAILS WITH NEW SERVICEABLE PARTS FS 677 TO FS 724 LT PN: SH670-36255-3 AND670-33558-3, IAW CRJ700 AMM 53-00-49-400-801-A
- [SDR SWIA202055349](https://openairdocs.org/sdr/SWIA202055349.md): Support Bracket · cracked · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Aerodynamic Fairings
  > BODY FAIRING PANEL 194AB RT FWD SUPPORT BRACKET CRACKED. C-CHECK RO 1/6/2021. REMOVED AND REPLACED LT & RT SUPPORT BRACKET, IAW CRJ 700 SRM 51-41-004-001-001-A01.
- [SDR SWIA202055348](https://openairdocs.org/sdr/SWIA202055348.md): Support Bracket · cracked · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Aerodynamic Fairings
  > BODY FAIRING PANEL 194AB LT FWD SUPPORT BRACKET CRACKED. C-CHECK RO 1/6/2021. COMPLIED WITH REPAIR BODY FAIRING PANEL 194AB HAS CENTER SUPPORT BRACKETS CRACKED, IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-06-001-001-A01. REFERENCE ATTACHED CONTINUE CARD.
- [SDR SWIA202055347](https://openairdocs.org/sdr/SWIA202055347.md): Support Bracket · cracked · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Aerodynamic Fairings
  > BODY FAIRING PANEL 194AB HAS CENTER SUPPORT BRACKETS CRACKED. C-CHECK RO 1/6/2021. COMPLIED WITH REPAIR BODY FAIRING PANEL 194AB HAS CENTER SUPPORT BRACKETS CRACKED, IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-06-001-001-A01. REFERENCE ATTACHED CONTINUE CAR
- [SDR SWIA202055334](https://openairdocs.org/sdr/SWIA202055334.md): Seat Track · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN FLOOR SEAT RAIL AT RBL 9 IS CORRODED BETWEEN FS 349.00 AND FS 477.40. C-CHECK RO 1/6/2021. REMOVED AND REPLACED RT CABIN SEAT RAIL AT RBL 9 BETWEEN FS 349.00 AND FS 477.40, IAW CRJ 700 AMM 53-00-49-000/400-801 A03.
- [SDR SWIA202055333](https://openairdocs.org/sdr/SWIA202055333.md): Door Sill · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL ANGLE IS CORRODED BETWEEN FS 310.00 AND FS 349.00. C-CHECK RO 1/6/2021. REMOVED AND REPLACED PASSENGER DOOR LOWER SILL ANGLE BETWEEN FS 310.00 AND FS 349.00, IAW CRJ 700 SRM 51-42-06-001-001-A01. SEE ATTACHED CONTINUATION CARD FOR
- [SDR SWIA202055330](https://openairdocs.org/sdr/SWIA202055330.md): Support · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BACKUP, SILL STGR 21L, FS 310.00 TO FS 333.00 CORROSION REQUIRES REPLACEMENT. C-CHECK RO 1/6/2021. REMOVED AND REPLACED BACKUP, SILL STGR 21L, FS 310.00 TO FS 333.00, AS REQUIRED IAW CRJ 700 SRM 51-42-06-001-001-A01. SEE ATTACHED CONTINUATION CARD FOR WORK
- [SDR SWIA202055324](https://openairdocs.org/sdr/SWIA202055324.md): Support · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BACKUP, SILL (STGR 21L, FS 333.00 TO FS 349.00) CORROSION REQUIRES REPLACEMENT. C-CHECK RO 1/6/2021. REMOVED REPLACED BACKUP SILL, IAW CRJ 700 SRM 51-42-06 AND 51-42-06-001-001 (A01). NO LEAKS AT REPAIR AREA. SEE CONTINUE CARD FOR MAINTENANCE PERFORMED.
- [SDR SWIA202055321](https://openairdocs.org/sdr/SWIA202055321.md): Floor Support · corroded · Nov 22, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT CABIN FLOOR SILL JUST AFT OF FS 349.00 RBL 36 IS CORRODED. C-CHECK RO 1/6/2021. C/W REO 670-53-21-1898 REV- DATE 2020-12-08. MAJOR REPAIR TASK 51-900-1002-SKY & FORM M-337 COMPLETED AND ATTACHED. NEGALABLE WEIGHT CHANGE. REFERENCE CONTINUE CARD FOR DET
- [SDR SWIA202055360](https://openairdocs.org/sdr/SWIA202055360.md): Door Frame · corroded · Nov 21, 2020 · N755SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD BAGGAGE BAY DOOR SURROUND STRUCTURE, STRAP CORRODED AT FS 533 AND APPROXIMATELY STGR 25L. C-CHECK RO 1/6/2021. FOUND STRAP TO BE OUT OF LIMITS, IAW CRJ 700 SRM 53-31-23-101-001-A01. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICABLE FWD BAGGAGE BAY
- [SDR SWIA202055359](https://openairdocs.org/sdr/SWIA202055359.md): Plate · corroded · Nov 21, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY DOOR SURROUND STRUCTURE, PLATE CORRODED AT FS 557 AND LBL 3.4. C-CHECK RO 1/6/2021. PLATE FOUND TO BE OUT OF LIMITS, IAW CRJ700 SRM 53-32-58-101-001-A01. REMOVED CORRODED PLATE FROM FWD BAGGAGE BAY AT FS 557 AND LBL 3.4. INSTALLED NEW PLATE
- [SDR SWIA202055358](https://openairdocs.org/sdr/SWIA202055358.md): Bracket · corroded · Nov 21, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY DOOR SURROUND STRUCTURE, MACHINED BRACKET CORRODED AT FS 533 AND LBL 2.6. C-CHECK RO 1/6/2021. REMOVED BRACKET LOCATED DRILLED AND INSTALLED NEW BRACKET AT FS 533 LBL 2.6, IAW DWG SH670-336000 REV-Y. SEE CONTINUE CARD FOR MAINTENANCE PERFORMED
- [SDR SWIA202055357](https://openairdocs.org/sdr/SWIA202055357.md): Channel · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TCAS LOWER CHANNEL CORRODED BETWEEN FS 295 AND FS 310 AT STGR 27. C-CHECK RO 1/6/2021. LOCATED, DRILLED AND INSTALLED DOUBLER, IAW CRJ 700 SRM 51-40-11-001-001 (A01)/51-42-06-001-001 (A01)/51-45-00-001-001 (A01). SEE CONTINUE CARD FOR MAINTENANCE PERFORMED.
- [SDR SWIA202055356](https://openairdocs.org/sdr/SWIA202055356.md): Cleat · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Passenger/Crew Doors
  > UPPER PAX DOOR HAS A CLEAT CORRODED AT FS 329. C-CHECK RO 1/6/2021. REMOVED AND REPLACED PAX DOOR CLEAT AT FS 329 P/N 600-31902-269, IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 38 7-25-20.
- [SDR SWIA202055355](https://openairdocs.org/sdr/SWIA202055355.md): Cleat · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Passenger/Crew Doors
  > UPPER PAX DOOR HAS (4 EA) CLEATS CORRODED BETWEEN FS 320 & 322. C-CHECK RO 1/6/2021. REMOVED AND REPLACED UPPER PAX DOOR (4 EA) CLEATS P/N 600-31902-269 BETWEEN FS 320 & 322, IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV 38 7-25-20.
- [SDR SWIA202055346](https://openairdocs.org/sdr/SWIA202055346.md): Drag Angle · cracked · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STAB TO FUSELAGE ATTCHMENT AFT DRAG ANGLE ON RT SIDE IS CRACKED. C-CHECK RO 1/6/2021. REMOVED AND REPLACED VERTICAL STAB TO FUSELAGE ATTACHMENT AFT DRAG ANGLE ON RT SIDE, IAW CRJ 700 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-00
- [SDR SWIA202055343](https://openairdocs.org/sdr/SWIA202055343.md): Intercostal · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD1A INTERCOSTAL CORRODED BETWEEN FS 322 & 332. C-CHECK RO 1/6/2021. REMOVED AND REPLACED PAX DOOR DD1A INTERCOSTAL P/N 601R318066-1, IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV 38 7-25-20. MAJOR REPAIR T
- [SDR SWIA202055339](https://openairdocs.org/sdr/SWIA202055339.md): Frame · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 310 CORRODED BETWEEN STGR 26L AND STGR 26R. C-CHECK RO 1/6/2021. PERFORM REPAIR TO FRAME SECTOR AT FS 310 BETWEEN STGR 23L AND 24R, IAW REO 670-53-21-799 REV A DATED: 2016-11-27 REF -202 INSTALL ALL APPLICABLE STEPS 1-20 COMPLETED.
- [SDR SWIA202055332](https://openairdocs.org/sdr/SWIA202055332.md): Tee Fitting · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Aerodynamic Fairings
  > FWD WING TO FUSALGE FAIRING SUPPORT STRUCTURE, MACHINED TEE ATTACHMENT ANGLE CORRODED AT STGR 27 BETWEEN FS 629 AND FS 661. C-CHECK RO 1/6/2021. COMPLIED WITH REPLACEMENT FWD WING TO FUSELAGE FAIRING SUPPORT STRUCTRUE, MACHINED TEE ATTACHMENT ANGLE AT STGR 2
- [SDR SWIA202055329](https://openairdocs.org/sdr/SWIA202055329.md): Intercostal · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR DD2 INTERCOSTAL CORRODED BETWEEN FS 320 & 332. C-CHECK RO 1/6/2021. REMOVED AND REPLACED PAX DOOR DD2 INTERCOSTAL P/N 601R318053-3, IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV 38 7-25-20. PRESSURE CHECK
- [SDR SWIA202055326](https://openairdocs.org/sdr/SWIA202055326.md): Intercostal · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCTURE, INTERCOSTAL CORRODED AT STGR 27R BETWEEN FS 349 AND FS 364. C-CHECK RO 1/6/2021. REMOVED AND REPLACED LATCH PIN INTERCOSTALS AT STR 27 BETWEEN FS 349-FS 364, IAW CRJ 700 SRM 51-42-06-001-001 (A01) 51-42-21-001-001 (A01).
- [SDR SWIA202055323](https://openairdocs.org/sdr/SWIA202055323.md): Intercostal · corroded · Nov 20, 2020 · N755SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT MID INTERCOSTAL CORRODED P/N 601R31902-317. C-CHECK RO 1/6/2021. REMOVED AND REPLACED PAX DOOR AFT MID INTERCOSTAL P/N 601R31902-317A, IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 REV 38 7-25-20. PRESSURE CHECK GOOD NO LEAKS FOUND
- [SDR SWIA202055372](https://openairdocs.org/sdr/SWIA202055372.md): Bearing · out of tolerance · Nov 19, 2020 · N755SK · Cndair CL6002C10 · Leading Edge Slat Control System
  > RT SLAT TRACK 3-2. INBOARD FWD ROLLER (1 EA) BEARING IS OUT OF LIMITS AND REQUIRES REPLACEMENT. C-CHECK RO 1/6/2021. REMOVED UNSERVICEABLE RT SLAT TRACK 3-2 INBOARD FWD ROLLER BEARING AND INSTALLED NEW BEARING, IAW CRJ 700 SRM 51-42-07-001-A01 AND CRJ 700 A

Next page: https://openairdocs.org/aircraft/N755SK/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 = 'N755SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N755SK/reports

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