# Service difficulty reports: N603SK

A list on [N603SK](https://openairdocs.org/aircraft/N603SK.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 · 224 reports

- [SDR SWIA2026100677526](https://openairdocs.org/sdr/SWIA2026100677526.md): Unknown · fumes · Oct 6, 2026 · N603SK · Cndair CL6002C11 · Air Distribution System
  > ON CLIMB OUT FROM KLNK, AROUND FL260, BEGAN TO SMELL AN ABNORMAL FUME IN THE FLIGHT DECK. OODR WAS REMINISCENT OF FUMES FROM A WILDFIRE. ALL ACFT INDICATIONS IN THE FLIGHT DECK WERE NORMAL & ODOR WOULD DISSIPATE & COME BACK, ASKED THE FLIGHT ATTENDANT TO IN
- [SDR SWIA2025110600029](https://openairdocs.org/sdr/SWIA2025110600029.md): Window Post · cracked · Oct 29, 2025 · N603SK · Cndair CL6002C11 · Fuselage Main, Structure
  > CRACK ON RT COCKPIT WINDSHIELD POST DETERMINED TO BE OUT OF LIMITS AND SIDE POST REQUIRES REPLACEMENT. THIS IS CLASSIFIED AS A MAJOR REPAIR. REMOVED AND REPLACED THE RT WINDSHIELD POST IAW SRM 51-40-11, SRM 51-42-06, SRM 51-42-21, SRM 51-45-00, SRM 51-25-06,
- [SDR SWIA2025103000029](https://openairdocs.org/sdr/SWIA2025103000029.md): Window Frame · cracked · Oct 29, 2025 · N603SK · Cndair CL6002C11 · Fuselage Main, Structure
  > CRACK ON RH COCKPIT WINDSHIELD SIDE POST, DETERMINED TO BE OUT OF LIMITS AND SIDE POST REQUIRES REPLACEMENT. THIS IS CLASSIFIED AS A MAJOR REPAIR. (OPEN)
- [SDR SWIA2025110600028](https://openairdocs.org/sdr/SWIA2025110600028.md): Window Frame · damaged · Oct 28, 2025 · N603SK · Cndair CL6002C11 · Fuselage Main, Structure
  > WHILE REMOVING THE RT WINDSHIELD SIDE POST STRAP, THE WINDSHIELD FRAME STRUCTURE WAS DAMAGED AT THE THIRD FASTERNER HOLE FROM THE CENTER OF THE RT SIDE POST ON THE BOTTOM FASTENER ROW OF THE RT SIDE WINDOW. THE DAMAGE MEASURES.098" IN DEPTH, 0.125" IN WIDTH
- [SDR SWI2025F00770](https://openairdocs.org/sdr/SWI2025F00770.md): Control Valve · faulted · Jun 28, 2025 · N603SK · Cndair CL6002C10 · Cabin Cooling System
  > L BLEED DUCT WARNING AND CAUTION MESSAGE IN FLIGHT. PERFORMED QRH PROCEDURE SUCCESSFULLY. (FLIGHT 6447 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30398967 WITH THE FOLLOWING CORRECTIVE ACTION: "INTERROGATED MDC, FOUND B1-349536, ALSO FOUND L
- [SDR SWIA202506090405](https://openairdocs.org/sdr/SWIA202506090405.md): Hinge · gouged · Apr 5, 2025 · N603SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE GOUGE ON AC SIDE AT KEEPER PIN (C-CHECK RO 06/07/2025)PERFORMED BLEND OUT ON PAX DOOR PIANO HINGE IAW BOMBARDIER REO 670-53-21-582 REV-F DATE: 2017-08-02PERFORMED NDT ET INSPECTION BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S041425-1, P.
- [SDR SWIA20250609403](https://openairdocs.org/sdr/SWIA20250609403.md): Frame · chafed · Apr 3, 2025 · N603SK · Cndair CL6002C10 · Fuselage Main, Frame
  > IN AFT EQUIPMENT BAY, FRAME 1144 IS CHAFED AT STR9L (C-CHECK RO 06/07/2025)REMOVED AND REPAIRED DAMAGED AT AFT EQUIPMENT BAY FRAME 1144, IAW MHI RJ REO-670-53-61-2506 REV -- DATED 2025-05-19, MHI RJ REO-670-53-61-2506 REV --(P1) DATED 2025-05-08, IAW CRJ700 SR
- [SDR SWI2025F00718](https://openairdocs.org/sdr/SWI2025F00718.md): Fitting · gouged · Apr 2, 2025 · N603SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH WING OB FLAP, CENTER HINGE BOX FITTING HAS A GOUGE, AFT FITTING (C-CHECK RO 06/07/2025)PERFORMED REPAIR ON LH WING OB FLAP, CENTER HINGE BOX FITTING, AFT FITTING IAW CRJ700 51-12-00, MHIRJ REO 670-57-21-1053, REV: --, DATE: 2025-05-02.NDT PERFORMED BY BARO
- [SDR SWI2025F00717](https://openairdocs.org/sdr/SWI2025F00717.md): Fitting · gouged · Apr 2, 2025 · N603SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LW WING, IB FLAP, OB HINGE BOX FITTING HAS A GOUGE AFT FITTING (C-CHECK RO 06/07/2025)REPAIRED DAMAGE TO HINGE BOX FITTING ON LH WING, INBD FLAP, OTBD AFT FITTING IAW REO 670-57-21-1053 REV-- DATE 2025-05-02 AND CRJ700 SRM 51-10-06, 51-12-00. NDT PERFORMED BY
- [SDR SWI2025F00716](https://openairdocs.org/sdr/SWI2025F00716.md): Bracket · cracked · Apr 2, 2025 · N603SK · Cndair CL6002C10 · Wing, Attach Fittings
  > L/H SLAT BOX HOUSING BRACKET CRACKED AT LOCATION 1-3 (C-CHECK RO 06/07/2025)PERFORMED REPAIR ON L/H SLAT BOX HOUSING AT LOCATION 1-3 PER BOMBARDIER REO 670-57-42-577. REV.--. DATE: 2016-12-02. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D. REPORT # S0424
- [SDR SWI2025F00715](https://openairdocs.org/sdr/SWI2025F00715.md): Fitting · gouged · Apr 2, 2025 · N603SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH WING OB FLAP, OB HINGE BOX AFT FITTING HAS A GOUGE (C-CHECK RO 06/07/2025)PERFORMED BLEND OUT DAMAGE ON LH WING OB FLAP, OB HINGE BOX IAW MHI RJ REO 670-57-21-1053 REV: --, DATE: 2025-05-02 AND CRJ 700 SRM 51-12-00.NDT PERFORMED INSPECTION BY BARON NDT, L
- [SDR SWIA2025060900402](https://openairdocs.org/sdr/SWIA2025060900402.md): Fitting · gouged · Apr 2, 2025 · N603SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH WING OB FLAP, IB HINGE BOX FITTING HAS A GOUGE, AFT FITTING (C-CHECK RO 06/07/2025)PERFORMED BLEND OUT ON LH WING OB FLAP, IB HINGE BOX FITTING FOUND TO BE LIMITS IAW REO 670-57-21-1053 REV-- DATE:2025-05-02 AND CRJ700 SRM 51-12-00 SRM 51-11-00PERFORMED ND
- [SDR SWIA2025060900327](https://openairdocs.org/sdr/SWIA2025060900327.md): Drag Angle · cracked · Mar 27, 2025 · N603SK · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > LH FWD DRAG ANGLE ON VERTICAL STABILIZER CRACKED (C-CHECK RO 06/07/2025)PERFORMED NEW REPAIR ON LH FWD DRAG ANGLE AT VERTICAL STABILIZER IAW BOMBARDIER REO 670-55-31-018 REV-A DATE: 2016-11-10 PERFORMED NDT ET INSPECTION BY BARON NDT, LLC FAA CRS# 5NDR545
- [SDR SWIA2024010300001](https://openairdocs.org/sdr/SWIA2024010300001.md): Windshield · cracked · Dec 31, 2024 · N603SK · Cndair CL6002C10 · Flight Compartment Windows
  > WINDSHIELD CRACKED ABOUT HALFWAY THROUGH FLIGHT. PRESSURIZATION REMAINED NORMAL. PER MAINTENANCE€™S REQUEST, DIVERTED TO PALM SPRINGS. L WINDOW HEAT AND L WSHLD HEAT MESSAGES CAME ON ABOUT 10 SECONDS AFTER CRACK. RAN QRH FOR BOTH. MESSAGES REMAIN ILLUMINATED
- [SDR SWIA202401021231](https://openairdocs.org/sdr/SWIA202401021231.md): Windshield · cracked · Dec 31, 2024 · N603SK · Cndair CL6002C10 · Flight Compartment Windows
  > WINDSHIELD CRACKED ABOUT HALFWAY THROUGH FLIGHT. PRESSURIZATION REMAINED NORMAL. PER MAINTENANCE€™S REQUEST, DIVERTED TO PALM SPRINGS. L WINDOW HEAT AND L WSHLD HEAT MESSAGES CAME ON ABOUT 10 SECONDS AFTER CRACK. RAN QRH FOR BOTH. MESSAGES REMAIN ILLUMINATED
- [SDR SWIA20240607](https://openairdocs.org/sdr/SWIA20240607.md): Bracket · corroded · Jun 7, 2024 · N603SK · Cndair CL6002C10 · Landing Gear Door Actuator
  > MULTIPLE AREAS OF CORROSION ON STR 27 AFT OF FRAME FS349 REMOVED STR27 AFT OF FRAME FS349 REF CRJ-700-SRM 51-42-06-001-001-A01 AND INSTALLED NEW STR27 AFT OF FRAME FS349 REF CRJ-700-SRM 51-42-06-001-001-A01 AND SH670-31350 REV A. PRESSURE LEAK CHECK GOOD WI
- [SDR SWIA202158966](https://openairdocs.org/sdr/SWIA202158966.md): Latch · cracked · Jun 5, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT HAND ACCESS PANEL 212AR AFT LATCH OPENING HAS CRACK MARKED (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED CRACKED LANDING WITH NEW REPLACEMENT LANDING (P/N CC670-33151-4) ON RH FWD TRU BAY FLOOR, REF MHIRJ REO 670-53-11-1702 REV--, DATED 2021-06-09, BO
- [SDR SWIA2021062358965](https://openairdocs.org/sdr/SWIA2021062358965.md): Doubler · cracked · Jun 5, 2021 · N603SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > IN FORWARD EQUIPMENT COMPARTMENT AT ADG STOW HANDLE PERVIOUS DOUBLER REPAIR CRACKED MARKED (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED PREVIOUS CRACKED DOUBLER WITH NEW FABRICATED DOUBLER AND CLEAT ON FLOOR OF RH FWD EQUIPMENT BAY AT ADG RESTOW HANDLE ASSY
- [SDR SWIA2021062358964](https://openairdocs.org/sdr/SWIA2021062358964.md): Stringer Clip · damaged · May 27, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CLEAT AT STR 20R FS 437 HAS AN OVERSIZED HOLE. (C-CHECK RO: 6/20/21) / REMOVED,FABRICATED, LOCATED AND DRILLED AND INSTALLED THE NEW STRINGER CLEAT FOR FS437, STRG20R, WITH P/N SH670-35625-2 OF MATERIAL 56144-13 0.050" P/O T000060559 I.A.W. CRJ700 SRM 51
- [SDR SWIA2021062358963](https://openairdocs.org/sdr/SWIA2021062358963.md): Fitting · corroded · May 25, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CLOSING FITTING AT FS342.00 CORRODED. (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED PAX DOOR AFT CLOSING FITTING WITH NEW REPALCEMENT CLOSING FITTING (SH670-32475-3) AT FS342.00 USING NEW HARDWARE. REF BOMBARDIER DWG# SH670-31810 REV Y AND CRJ700 S
- [SDR SWIA202158999](https://openairdocs.org/sdr/SWIA202158999.md): Door Sill · corroded · May 24, 2021 · N603SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * PAX DOOR LOWER SILL MID CAP ANGLE CORRODED. (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED CORRODED LOWER MID CAP ANGLE WITH NEW REPLACEMENT MID CAP ANGLE (P/N SH670-31825-9S) USING NEW HARDWARE, REF CRJ700 SRM 51-41-02-001-001 A01. SEE CONTINUATION CARD F
- [SDR SWIA2021062358962](https://openairdocs.org/sdr/SWIA2021062358962.md): Fitting · corroded · May 24, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CLOSING FITTING AT APROX. FS310.00 CORRODED. (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED PAX DOOR FWD CLOSING FITTING WITH NEW REPALCEMENT CLOSING FITTING (SH670-31840-3) AT FS310.00 USING NEW HARDWARE. REF BOMBARDIER DWG# SH670-31810 REV Y AND CR
- [SDR SWIA2021062358961](https://openairdocs.org/sdr/SWIA2021062358961.md): Plate · corroded · May 24, 2021 · N603SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * PAX DOOR LOWER SILL ANGLE KICK PLATE CORRODED IN MULTIPLE SPOTS (MARKED). P/N SH670-31875. (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED CORRODED PAX DOOR LOWER SILL ANGLE WITH NEW REPLACEMENT LOWER SILL ANGLE KICKPLATE (P/N SH670-31875-5) USING ALL NEW HA
- [SDR SWIA2021062358959](https://openairdocs.org/sdr/SWIA2021062358959.md): Plate · gouged · May 19, 2021 · N603SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR SURROUND, JOINT PLATE AT FS581, STGR25L-26L GOUGED. (C-CHECK RO: 6/20/21) /.REMOVED AND INSTALLED NEW PLATE FWD CARGO DOOR SURROUND, JOINT PLATE AT FS581, STGR25L-26L REF DWG SH670-33750 REV AA, CRJ 700 SRM 51-42-22-001-001-A01. COMPLIED
- [SDR SWIA2021062358958](https://openairdocs.org/sdr/SWIA2021062358958.md): Stringer · corroded · May 14, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 20R, FROM FS 319.70 - 349.00, CORRODED AT AFT END. (C-CHECK RO: 6/20/21) / 100% MATERIAL LOSS. - REPLACED THE STGR20R FROM FS319 TO FS349 REF DRAWING SH670-32420 REV. E AND CRJ700 SRM 51-42-06-001-001-A01. PRESSURIZATION LEAK CHECK OF THE REPAIR AREA
- [SDR SWIA2021062358957](https://openairdocs.org/sdr/SWIA2021062358957.md): Angle · cracked · May 12, 2021 · N603SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BULKHEAD ANGLE BL26 AT FS280 R/H FOUND CRACKED. (C-CHECK RO: 6/20/21) / INSTALLED NEW ANGLE RBL26 AT FS280. REF: CRJ700 SRM 51-42-06-001-001-A01, DWG: CC-670-34010 REV: -K. ALSO COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2021062358956](https://openairdocs.org/sdr/SWIA2021062358956.md): Floorbeam · cracked · May 11, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT LH FLOORBEAM AT LBL12 JUST FWD OF FS280.00 WAS CRACKED (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED THE LH COCKPIT FLOORBEAM AT LBL12 JUST FORWARD OF FS280 REF CRJ700 SRM 53-11-43--201-003-A01, SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM
- [SDR SWIA2021062358955](https://openairdocs.org/sdr/SWIA2021062358955.md): Floorbeam · cracked · May 11, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT RH FLOORBEAM AT RBL12 JUST FWD OF FS280.00 WAS CRACKED (C-CHECK RO: 6/20/21) / REMOVED THE CRACKED FLOOR BEAM SECTION AND INSTALLED A NEW COCKPIT RBL12 FLOOR BEAM SECTION FWD OF FS280 AND REINSTALLED THE EXISTING REPAIR PARTS (THE INBD UPPER AND LOW
- [SDR SWIA2021062358998](https://openairdocs.org/sdr/SWIA2021062358998.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-37543-3, R/H SIDE RAIL APPROX FS863.00-FS960.00 (C-CHECK RO: 6/20/21) / FABRICATED NEW R/H SIDE SEAT TRACK P/N SH670-37543-3, USING EXTRUSION 20276-288-0-0A, PO# T59435, REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358997](https://openairdocs.org/sdr/SWIA2021062358997.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-37543-3, L/H SIDE RAIL APPROX FS863.00-FS960.00 (C-CHECK RO: 6/20/21) / FABRICATED NEW L/H SIDE SEAT TRACK P/N SH670-37543-3, USING EXTRUSION 20276-288-0-0A, PO# T59435, REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358996](https://openairdocs.org/sdr/SWIA2021062358996.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-33558-3, R/H SIDE RAIL APPROX FS571.00-FS669.00 (C-CHECK RO: 6/20/21) / FABRICATED NEW SEAT TRACK PN: SH670-33558-3 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59653. REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358995](https://openairdocs.org/sdr/SWIA2021062358995.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-32234-3, R/H SIDE RAIL APPROX FS485.00-FS571.00 (C-CHECK RO: 6/20/21) / FABRICATED NEW R/H SIDE SEAT TRACK P/N SH670-32234-3, USING EXTRUSION 20276-288-0-0A, PO# T59435, REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358994](https://openairdocs.org/sdr/SWIA2021062358994.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-32233-3, RH SIDE RAIL APPROX FS379-FS485 (C-CHECK RO: 6/20/21) / FABRICATED NEW SEAT TRACK PN: SH670-32233-3 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59653. REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358993](https://openairdocs.org/sdr/SWIA2021062358993.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-33558-3, LH SIDE RAIL APPROX FS571-FS669 (C-CHECK RO: 6/20/21) / FABRICATED NEW SEAT TRACK PN: SH670-33558-3 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59435. REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358992](https://openairdocs.org/sdr/SWIA2021062358992.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-32234-3, L/H SIDE RAIL APPROX FS485.00-FS571.00 (C-CHECK RO: 6/20/21) / FABRICATED NEW L/H SIDE SEAT RAIL P/N SH670-32234-3, USING EXTRUSION 20276-288-0-0A, PO# T59435, REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358991](https://openairdocs.org/sdr/SWIA2021062358991.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-32233-3, L/H SIDE RAIL APPROX FS379.00-FS485.00 (C-CHECK RO: 6/20/21) / FABRICATED NEW SEAT TRACK PN: SH670-32233-3 FROM EXTRUSION P/N 20276-288-0-0A, PO# T-59435. REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358990](https://openairdocs.org/sdr/SWIA2021062358990.md): Seat Track · corroded · May 10, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FABRICATE SEAT TRACK PN: SH670-32249-3, LBL9 FROM APPROX FS370.00-FS477.00 (C-CHECK RO: 6/20/21) / FABRICATED NEW LBL9 FLOOR SEAT TRACK P/N SH670-32249-3, USING EXTRUSION 20276-288-0-0A, PO# T55899, REF. CRJ700 SRM 53-00-49-201-002-A01.
- [SDR SWIA2021062358954](https://openairdocs.org/sdr/SWIA2021062358954.md): Stringer Clip · corroded · May 8, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CLEAT CORRODED AT FS 333.00, STGR 20R INTERCOSTAL, FWD SIDE UPPER OF FRAME. (C-CHECK RO: 6/20/21) / INSTALLED NEW CLEAT AT FS349 STGR 20R INTERCOSTAL REF DRAWING SH670-31950 REV. V AND CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY. SEE CO
- [SDR SWIA202158953](https://openairdocs.org/sdr/SWIA202158953.md): Cleat · corroded · May 8, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CLEAT CORRODED AT FS 349.00, STGR 20R INTERCOSTAL, FWD SIDE UPPER OF FRAME. (C-CHECK RO: 6/20/21) / INSTALLED NEW CLEAT AT FS349 STGR 20R INTERCOSTAL REF DRAWING SH670-31950 REV. V AND CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2021062358952](https://openairdocs.org/sdr/SWIA2021062358952.md): Cleat · corroded · May 8, 2021 · N603SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CLEAT CORRODED AT FS 319.70, STGR 20R INTERCOSTAL, AFT SIDE UPPER OF FRAME. (C-CHECK RO: 6/20/21) / REMOVED AND INSTALLED CLEAT AT FS319.70, STGR 20R INTERCOSTAL REF DRAWING SH670-31950 REV. V AN CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-S
- [SDR SWIA2021062358951](https://openairdocs.org/sdr/SWIA2021062358951.md): Intercostal · corroded · May 8, 2021 · N603SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *STRINGER 20R INTERCOSTAL HAS EVIDENCE OF CORROSION FROM FS 319.70 TO FS 349.00. (C-CHECK RO: 6/20/21) / MULTIPLE ELEMENTS OF INTERCOSTAL AT STR20R FS319.7-349 CORRODED, "OUT OF LIMITS." REMOVED AND REPLACED INTERCOSTAL STR20R FS319.7-349 REF DRAWING SH67
- [SDR SWIA2021062358950](https://openairdocs.org/sdr/SWIA2021062358950.md): Former · corroded · May 3, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER CORRODED (C-CHECK RO: 6/20/21)REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER REF CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. LEAK CHECK GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2021062358949](https://openairdocs.org/sdr/SWIA2021062358949.md): Intercostal · corroded · May 3, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID AFT INTERCOSTAL PN: 601R31902-317 CORODDED (C-CHECK RO: 6/20/21) / LOCATED, DRILLED AND INSTALLED NEW REPLACEMENT INTERCOSTAL (P/N 601R31902-317) ONTO PAX DOOR. REF BOMBARDIER DWG# 601R31702 REV N AND CRJ700 SRM 51-42-06-001-001 A01. LEAK CHECK
- [SDR SWIA2021062358948](https://openairdocs.org/sdr/SWIA2021062358948.md): Intercostal · corroded · May 3, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR UPPER AFT INTERCOSTAL PN: 601R31902-317 CORODDED (C-CHECK RO: 6/20/21) / LOCATED AND DRILLED AND INSTALLED NEW REPLACEMENT INTERCOSTAL (P/N 601R31902-317), REF, BOMBARDIER DWG # 601R31702 REV N AND CRJ700 SRM 51-40-11-001-001 A01. LEAK CHECK GOOD
- [SDR SWIA2021062358947](https://openairdocs.org/sdr/SWIA2021062358947.md): Intercostal · corroded · May 3, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL FWD DD4 CORRODED (C-CHECK RO: 6/20/21) / REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 REF CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. LEAK CHECK GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2021062358946](https://openairdocs.org/sdr/SWIA2021062358946.md): Intercostal · corroded · May 3, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL FWD DD5 CORRODED (C-CHECK RO: 6/20/21) / LOCATED AND DRILLED AND INSTALLED NEW REPLACEMENT INTERCOSTAL (P/N 601R318091-5) ONTO PAX DOOR SKIN, REF CRJ700 SRM 51-40-11-001-001 A01. LEAK CHECK GOOD AT THIS TIME. COMPLIED WITH 51-900-1002-S
- [SDR SWIA2021062358989](https://openairdocs.org/sdr/SWIA2021062358989.md): Skin · corroded · May 1, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *PASSENGER DOOR INNER SKIN MATING SURFACE FOR PANEL 832FR HAS AREA OF CORROSION. (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED CORRODED PAX DOOR INNER SKIN WITH NEW PAX DOOR INNER SKIN (PN 601R318024-15) USING ALL NEW FASTENERS REF CRJ700 SRM 51-42-06-001-00
- [SDR SWIA2021062358945](https://openairdocs.org/sdr/SWIA2021062358945.md): Drag Angle · corroded · Apr 28, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > RH VERT STAB TO FUSELAGE AFT DRAG ANGLE HAS CRACK. (C-CHECK RO: 6/20/21) / INSTALLED NEW DRAG ANGLE REF DWG BA670-35002 REV -F, CRJ 700 SRM 51-42-21-001-001-A01,CRJ 700 SRM 51-42-22-001-001-A01,CRJ 700 SRM 51-42-13-001-001-A01. COMPLIED WITH 51-900-1002-SK
- [SDR SWIA2021062358944](https://openairdocs.org/sdr/SWIA2021062358944.md): Drag Angle · corroded · Apr 28, 2021 · N603SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > RH VERT STAB TO FUSELAGE FWD DRAG ANGLE HAS CRACK. (C-CHECK RO: 6/20/21) / FABRICATED AND INSTALLED NEW PARTS OF THE REPAIR AT RH VERT STAB TO FUSELAGE FWD DRAG ANGLE REF CRJ 700 SRM 55-31-00-201-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND COMPLIED WIT
- [SDR SWIA2021062358988](https://openairdocs.org/sdr/SWIA2021062358988.md): Panel · cracked · Apr 25, 2021 · N603SK · Cndair CL6002C10 · Passenger/Crew Doors
  > *PASSENGER DOOR INNER UPPER FIXED PANEL (DOOR OPEN) HAS SUSPECT CRACK. (MARKED) (C-CHECK RO: 6/20/21) / REMOVED AND REPLACED CRACKED PAX DOOR INNER UPPER FIXED PANEL WITH NEW PANEL (P/N 601R317075-3) USING NEW HARDWARE. REF BOMBARDIER DWG# 601R31702 REV J A

Next page: https://openairdocs.org/aircraft/N603SK/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 = 'N603SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N603SK/reports

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