# Service difficulty reports: N608SK

A list on [N608SK](https://openairdocs.org/aircraft/N608SK.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 3 · 140 reports

- [SDR SWIA202505160015](https://openairdocs.org/sdr/SWIA202505160015.md): Control Panel · warning message · May 15, 2025 · N608SK · Cndair CL6002C10 · Cabin Pressure Control System
  > AUTO PRESS CAUTION ON DEPARTURE. LED TO CABIN ALT MESSAGE. (FLIGHT 6240 - FILED CLOSED)INTERROGATED THE MDC, FOUND BCODE 006158. TROUBLESHOT TO A FAULTY CABIN PRESSURE CONTROL PANEL IN REF TO CRJ 700 FIM 21-33-01. REMOVED AND REPLACED THE CPCP IN REF TO CRJ 7
- [SDR SWIA2024051500011](https://openairdocs.org/sdr/SWIA2024051500011.md): Sensor · faulted · May 11, 2024 · N608SK · Cndair CL6002C10 · Cabin Cooling System
  > FOLLOWING APU DOOR OPEN & R PACK OFF CAUTION MESSAGES PRESSURIZATION BEGAN STEADILY RISING. STARTED TO DESCEND TO COMBAT RISING CABIN ALTITUDE. CABIN ALT CAUTION MESSAGE APPEARED. DECLARED AN EMERGENCY AND DESCENDED TO 10000 FEET AND MESSAGE EXTINGUISHED. (FLI
- [SDR SWIA202405130011](https://openairdocs.org/sdr/SWIA202405130011.md): Warning Message · illuminated · May 11, 2024 · N608SK · Cndair CL6002C10 · APU Bleed Air System
  > FOLLOWING APU DOOR OPEN & R PACK OFF CAUTION MESSAGES PRESSURIZATION BEGAN STEADILY RISING. STARTED TO DESCEND TO COMBAT RISING CABIN ALTITUDE. CABIN ALT CAUTION MESSAGE APPEARED. DECLARED AN EMERGENCY AND DESCENDED TO 10000 FEET AND MESSAGE EXTINGUISHED. (FLI
- [SDR SWIA202303280002](https://openairdocs.org/sdr/SWIA202303280002.md): Unknown · warning message · Mar 27, 2023 · N608SK · Cndair CL6002C10 · Landing Gear System
  > BRAKE OVHT WARNING IN FLIGHT. RAN QRH, WARNING DID NOT CLEAR LANDED AT NEAREST SUITABLE. (FLIGHT 3607 FILED CLOSED) NO RECENT HISTORY NOTED BY MX. INTERROGATED MDC NO CURRENT FAULTS LISTED. FAULT HISTORY SHOWED #4 MLG BRAKE THERMOCOUPLE POSSIBLE CAUSE REF FIM
- [SDR SWIA2022120566960](https://openairdocs.org/sdr/SWIA2022120566960.md): Door · cracked · Nov 24, 2022 · N608SK · Cndair CL6002C10 · Emergency Exits
  > FOUND CRACK ON RH OW EMER EXIT DOOR (FILED CLOSED) REMOVED AND REPLACED RH OW EMER EXIT DOOR IAW AMM 52-21-00 OPS CHECK GOOD AT THIS TIME SEE CP 25839384 FOR LEAK CHECK, SEE CP 25860190-1 FOR PAINT. SEE CP 25860210-1 FOR PLACARD.
- [SDR SWIA202266623](https://openairdocs.org/sdr/SWIA202266623.md): None · cracked · Oct 24, 2022 · N608SK · Cndair CL6002C10 · Window/Windshield System
  > OUTER PANE LEFT WINDSHIELD CRACKED ON CLIMB OUT (FLIGHT #3560 FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2022081666296](https://openairdocs.org/sdr/SWIA2022081666296.md): Mount · corroded · Jul 9, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > GALLEY FLOOR MOUNT BETWEEN LH FS280.00 €“ FS295.00, LBL20 HAS CORROSION. (C-CHECK RO 8/14/2022) EVALUATED GALLEY FLOOR MOUNT AND FOUND IT OUT OF LIMITS. REMOVED AND REPLACED FITTING PN# SH670-32148-3 PER REFERENCE DRAWING# SH670-32120 REV D, AND CRJ 70
- [SDR SWIA2022081666295](https://openairdocs.org/sdr/SWIA2022081666295.md): Mount · corroded · Jul 9, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > GALLEY FLOOR MOUNT BETWEEN RH FS280.00 €“ FS2950.00, RBL18 HAS CORROSION (C-CHECK RO 8/14/2022) REMOVED AND REPLACED GALLEY FLOOR FITTING PN# SH670-32148-3 PER REFERENCE DRAWING# SH670-32120 REV D, AND CRJ 700 SRM 51-42-21-001-001-A01 FOR INTERCOSTAL
- [SDR SWIA2022081666294](https://openairdocs.org/sdr/SWIA2022081666294.md): Mount · corroded · Jul 9, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > GALLEY FLOOR MOUNT BETWEEN RH FS280.00 €“ FS295.00, RBL27 HAS CORROSION. (C-CHECK RO 8/14/2022) REMOVED AND INSTALLED NEW GALLEY FLOOR MOUNT BETWEEN RH FS280.00 - FS295.00, RBL27. REF CRJ-700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-32120 REV
- [SDR SWIA2022081666293](https://openairdocs.org/sdr/SWIA2022081666293.md): Stringer · corroded · Jul 2, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 CORRODED (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 23R SPLICE AT FS333.00 REF. DRWG SH670-32420 REV. E AND CRJ 700 SRM 51-42-06-001-001-A01. PRESSURIZATION LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-90
- [SDR SWIA2022081666292](https://openairdocs.org/sdr/SWIA2022081666292.md): Frame · corroded · Jul 1, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY FS333.00 FRAME CORRODED BETWEEN STR 27 AND STR 26R ON MULTIPLE ELEMENTS (C-CHECK RO 8/14/2022) REMOVED AND REPLACED FS333.00 FRAME FROM STR 25L TO STR 20R REF. DRWG SH670-32420 REV. E, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 5
- [SDR SWIA2022081666291](https://openairdocs.org/sdr/SWIA2022081666291.md): Bulkhead Web · cracked · Jul 1, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS.280 LOWER BULKHEAD WEB. STIFFENER AT RBL27 CRACKED AT LOWER HOLE. (C-CHECK RO 8/14/2022) REMOVED AND REPLACED FS.280 LOWER BULKHEAD WEB STIFFENER AT RBL27 WITH A NEW SERVICEABLE UNIT (P/N CC670-34117-6) REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG CC
- [SDR SWIA2022081666290](https://openairdocs.org/sdr/SWIA2022081666290.md): Drag Angle · cracked · Jun 30, 2022 · N608SK · Cndair CL6002C10 · Vertical Stabilizer
  > R/H VERTICAL STABILIZER/FUSELAGE JOINT, FOUND FWD DRAG ANGLE CRACKED (C-CHECK RO 8/14/2022) RH VERTICAL STABILIZER FUSELAGE JOINT FWD DRAG ANGLE REPAIRED REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2022081666289](https://openairdocs.org/sdr/SWIA2022081666289.md): Stringer · corroded · Jun 30, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 26R CORRODED AROUND SEVERAL FASTENER HOLES BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 8/14/2022) REPLACED STR 26R FROM FS280 TO FS333 WITH NEW UNIT. REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG: SH6
- [SDR SWIA2022081666288](https://openairdocs.org/sdr/SWIA2022081666288.md): Drag Angle · cracked · Jun 28, 2022 · N608SK · Cndair CL6002C10 · Vertical Stabilizer
  > R/H VERTICAL STABILIZER AFT DRAG ANGLE CRACKED (C-CHECK RO 8/14/2022) REPAIRED RH VERTICAL STABILIZER AFT DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2022081666287](https://openairdocs.org/sdr/SWIA2022081666287.md): Web · cracked · Jun 28, 2022 · N608SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > L/H TRU BAY WEB CRACKED AT APPROX FS193.00 (C-CHECK RO 8/14/2022) CUT OUT CRACK AND INSTALLED DOUBLER, SHIM, AND CLEAT REF REO 670-53-11-509 REV E DATED 2018-02-08. ALSO COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2022081666286](https://openairdocs.org/sdr/SWIA2022081666286.md): Web · cracked · Jun 28, 2022 · N608SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > R/H TRU BAY WEB CRACKED AT APPROX FS193.00 (C-CHECK RO 8/14/2022) PERFORMED REPAIR AT R/H TRU BAY WEB AT APPROX FS193.00 REF REO 670-53-11-509 REV-E DATE 2018-02-08, COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2022081666285](https://openairdocs.org/sdr/SWIA2022081666285.md): Skin · gouged · Jun 28, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE BETWEEN FS969.00 TO FS985.00 AT STGR27 IS GOUGED (WHERE AFT TO BODY FAIRING IS LOCATED) (C-CHECK RO 8/14/2022) PERFORMED REPAIRS TO EXTERNAL FUSELAGE FS969.00 TO FS985.00. @ STGR27 IAW REO 670-53-00-695, REV: --, 2022-07-05, REO 670-53
- [SDR SWIA2022081666284](https://openairdocs.org/sdr/SWIA2022081666284.md): Crossbeam · corroded · Jun 27, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FS1051.00- CORROSION FOUND ON R/H FLOOR CROSSBEAM AT FLOOR BOARD FASTENER HOLE (MARKED IN RED INK) (C-CHECK RO 8/14/2022) REPAIRED RH FLOOR CROSSBEAM AT FS1051.00 REF MHIRJ REO 670-53-61-2083 REV -- DATED 2022-07-18 AND CRJ-700 SRM 51-42-06-001-001-A01.
- [SDR SWIA2022081666283](https://openairdocs.org/sdr/SWIA2022081666283.md): Former · cracked · Jun 24, 2022 · N608SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER AT FS347.27 CRACKED AT MOTOR ASSIST CABLE PULLEY BRACKET. (C-CHECK RO 8/14/2022) REPLACED PAX DOOR AFT FORMER AT FS347.27 WITH NEW UNIT. REF CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG 601R31702 REV N. PRESSURE LE
- [SDR SWIA2022081666282](https://openairdocs.org/sdr/SWIA2022081666282.md): Attach Fitting · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON SERVICE DOOR LOWER SURROUND SECTION ON ATTACH FITTING AT FS319.70 AT FLOOR LEVEL (C-CHECK RO 8/14/2022) REPLACED SERVICE DOOR LOWER SURROUND SECTION ATTACH FITTING(BRACKET) AT FS319.70 AT FLOOR LEVEL REF. CRJ700 SRM 51-42-21-001-001-A01 AND
- [SDR SWIA2022081666281](https://openairdocs.org/sdr/SWIA2022081666281.md): Stringer · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 19L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 19L FROM FS310.00 TO FS349.00 REF. DRWG SH670-31810 REV. AE, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. PRESSURI
- [SDR SWIA2022081666280](https://openairdocs.org/sdr/SWIA2022081666280.md): Intercostal · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT 26R FS 349.00 €“ FS364.00 HAS CORROSION ON THE LOWER FLANGE AND WEB. (MARKED) (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 26R ATTACH ANGLE (INTERCOSTAL) FROM FS349.00 TO FS364.00 REF. DRWG SH670-32050 REV. J, CRJ 700 SRM 51-42-06-001
- [SDR SWIA2022081666279](https://openairdocs.org/sdr/SWIA2022081666279.md): Frame · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY FRAME FS333.00 CORRODED AROUND GROUND STUDS APPROX TO STR 19L (C-CHECK RO 8/14/2022) REMOVED AND REPLACED FS333.00 FRAME SECTION FROM STR 18L TO STR 21L REF. DRWG SH670-31810 REV. Y, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51
- [SDR SWIA2022081666278](https://openairdocs.org/sdr/SWIA2022081666278.md): Stringer · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS349.00 AND FS364.00 (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 24R FROM FS333.00 TO FS372.00 REF. DRWG SH690-31350 REV. M, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 53-00-03-201-001-A01. PRESSURIZ
- [SDR SWIA2022081666277](https://openairdocs.org/sdr/SWIA2022081666277.md): Stringer · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS319.00 AND FS333.00 (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 23R FROM FS280.00 TO FS333.00 REF. DRWG SH670-31630 REV. K, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. PRESSURIZ
- [SDR SWIA2022081666276](https://openairdocs.org/sdr/SWIA2022081666276.md): Stringer · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 22L CORRODED BETWEEN FS319.00 AND FS333.00 (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 22L FROM FS280.00 TO FS333.00 REF. DRWG SH670-31630 REV. K, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. PRESSURIZ
- [SDR SWIA2022081666275](https://openairdocs.org/sdr/SWIA2022081666275.md): Door Frame · corroded · Jun 23, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR SURROUND STRUCTURE FWD CLOSING FITTING HAS SEVERE CORROSION. (C-CHECK RO 8/14/2022) EVALUATED REPAIR AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FWD CLOSING FITTING. REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-41
- [SDR SWIA2022081666274](https://openairdocs.org/sdr/SWIA2022081666274.md): Door Frame · corroded · Jun 22, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR SURROUND STRUCTURE FWD. AND MID CAP ANGLES ARE CORRODED. (C-CHECK RO 8/14/2022) REMOPVED AND REPLACED CORRODED PAX DOOR FWD AND MID CAP ANGLES WITH NEW UNITS. REF CRJ700 SRM 51-41-02-001-001-A01 AND DWG SH670-31810 REV Y. COMPLIED WITH
- [SDR SWIA2022081666273](https://openairdocs.org/sdr/SWIA2022081666273.md): Stringer · corroded · Jun 20, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 27 HAS CORROSION ON STRINGER LOWER FLANGE BETWEEN FS 310.00 TO FS 339.00 (AS MARKED) (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 27 FROM FS308.00 TO FS333.00 REF. DRWG SH670-31630 REV. K, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21
- [SDR SWIA2022081666272](https://openairdocs.org/sdr/SWIA2022081666272.md): Bracket · cracked · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > L/H LOWER TRANSCOWL I/B "A" BRACKET IS CRACKED. (C-CHECK RO 8/14/2022) INSTALLED 1 EA NEW L/H LOWER TRANSCOWL I/B "A" STANDOFF P/N CN624-2082-201, REF. BOMBARDIER GREO 670-54-21-971, REV. (A) 2017-05-11 STEPS 1-3. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2022081666271](https://openairdocs.org/sdr/SWIA2022081666271.md): Frame · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY FS319.70 FRAME CORRODED BETWEEN STR 18L AND STR 21L (C-CHECK RO 8/14/2022) REMOVED AND REPLACED FS319.70 FRAME SECTION FROM STR 18L TO STR 21L REF. DRWG SH670-31810 REV. AE, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001
- [SDR SWIA2022081666270](https://openairdocs.org/sdr/SWIA2022081666270.md): Frame · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Frame
  > MAIN AVIONICS BAY FS295.00 FRAME CORRODED BETWEEN STR 23L AND STR 24L (C-CHECK RO 8/14/2022) REMOVED AND REPLACED FS295.00 FRAME SECTION FROM STR 20L TO STR 25L REF. DRWG SH670-31630 REV. K, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-
- [SDR SWIA2022081666269](https://openairdocs.org/sdr/SWIA2022081666269.md): Crossbeam · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Structure
  > RH FS.280 FLOOR CROSS BEAM HAS CORROSION BETWEEN RBL12 AND BL0 (TOP FLANGE AND FWD WEB). (C-CHECK RO 8/14/2022) REMOVED AND INSTALLED NEW RH FS.280 FLOOR CROSS BEAM. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG CC670-34010 REV -K. COMPLIED WITH SKYWEST
- [SDR SWIA2022081666268](https://openairdocs.org/sdr/SWIA2022081666268.md): Stringer · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS333.00 AND FS379.00 (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 23R FROM FS333.00 TO FS379.00 REF. DRWG SH670-31350 REV. A AND CRJ 700 SRM 51-42-06-001-001-A01. PRESSURIZATION LEAK CHECK GOOD. COMPLIED WI
- [SDR SWIA2022081666267](https://openairdocs.org/sdr/SWIA2022081666267.md): Stringer · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS364.00 AND FS379.00 (C-CHECK RO 8/14/2022) REPLACED STR 21R FROM FS333.00 TO FS379.00. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV M. PRESSURIZATION LEAK CHECK GOOD. COMPLIED WITH TASK CARD
- [SDR SWIA2022081666266](https://openairdocs.org/sdr/SWIA2022081666266.md): Crossbeam · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LH FS.280 FLOOR CROSS BEAM HAS CORROSION BETWEEN LBL12 AND BL0 (TOP FLANGE AND FWD WEB). (C-CHECK RO 8/14/2022) REMOVED AND INSTALLED NEW LH FS.280 FLOOR CROSS BEAM. REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG #CC670-34010 REV.-K. COMPLIED WITH SKYWEST
- [SDR SWIA2022081666265](https://openairdocs.org/sdr/SWIA2022081666265.md): Intercostal · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY LH LATCH-PIN INTERCOSTAL BETWEEN FS349.00 AND FS364.00 CORRODED (C-CHECK RO 8/14/2022) REMOVED AND REPLACED LH LATCH-PIN INTERCOSTAL FROM FS349.00 TO FS364.00 REF. DRWG SH670-32050 REV. J, CRJ 700 SRM 51-42-21-001-001-A01 AND CRJ 700 S
- [SDR SWIA2022081666264](https://openairdocs.org/sdr/SWIA2022081666264.md): Window Post · cracked · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LH WINDSHEILD AFT POST LOWER FITTTING AFT CORNER HAS A CRACK. (C-CHECK RO 8/14/2022) REMOVED AND REPLACED L/H WINDSHIELD AFT LOWER POST. REF. DWG GC219-0600 REV. H, AND CRJ 700 SRM 51-42-21-001-001-A01. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORM
- [SDR SWIA2022081666263](https://openairdocs.org/sdr/SWIA2022081666263.md): Intercostal · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MAIN AVIONICS BAY RH LATCH-PIN INTERCOSTAL BETWEEN FS349.00 AND FS364.00 CORRODED (C-CHECK RO 8/14/2022) REMOVED AND REPLACED RH LATCH-PIN INTERCOSTAL FROM FS349.00 TO FS364.00 REF. DRWG SH670-32050 REV. J, CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 S
- [SDR SWIA2022081666262](https://openairdocs.org/sdr/SWIA2022081666262.md): Doubler · corroded · Jun 18, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MAIN AVIONICS BAY TCAS ANTENNA DOUBLER BETWEEN FS295.00 AND FS310.00 CORRODED (C-CHECK RO 8/14/2022) REMOVED AND REPLACED DAMAGED TCAS DOUBLER. REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-30023 REV G. SEE CONTINUATION CARD FOR DETAILS OF WORK PE
- [SDR SWIA2022081666261](https://openairdocs.org/sdr/SWIA2022081666261.md): Floorbeam · cracked · Jun 17, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH COCKPIT FLOOR BEAM AT RBL12 ATTACHING FLANGE TO FS.280 LOWER BULKHEAD IS CRACKED. (C-CHECK RO 8/14/2022) REPLACED RH COCKPIT FLOOR BEAM WEB ANGLE AND GUSSET AT RBL 12 REF CRJ700 SRM 53-11-43-201-003-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2022081666260](https://openairdocs.org/sdr/SWIA2022081666260.md): Bulkhead Web · corroded · Jun 17, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LH FS.280 LOWER BULKHEAD WEB. HAS CORROSION AT FLOOR LEVEL LBL12. (C-CHECK RO 8/14/2022) REMOVED AND INSTALLED NEW LH FS.280 LOWER BULKHEAD WEB. REF CRJ-700 SRM 53-11-10-201-004-A01. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY.
- [SDR SWIA2022081666259](https://openairdocs.org/sdr/SWIA2022081666259.md): Floorbeam · corroded · Jun 17, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR SUPPORT ANGLE FWD OF FS.280 BETWEEN LBL12 AND RBL12 HAS CORROSION. (C-CHECK RO 8/14/2022) REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE WITH NEW REF.CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG CC670-33052 REV-G, COMP
- [SDR SWIA2022081666258](https://openairdocs.org/sdr/SWIA2022081666258.md): Web · corroded · Jun 16, 2022 · N608SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON RH LOWER WEB AT FS 280.00 (C-CHECK RO 8/14/2022) REMOVED AND INSTALLED NEW RH LOWER WEB AT FS280.00. REF CRJ-700 SRM 53-11-10-201-004-A01. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2022081666257](https://openairdocs.org/sdr/SWIA2022081666257.md): Bracket · corroded · Jun 16, 2022 · N608SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY SURROUND STRUCTURE HAS A BRACKET CORRODED ON THE FWD BOTTOM (MARKED) (C-CHECK RO 8/14/2022) INSTALLED FWD CARGO SURROUND DOOR NEW BRACKET ( FWD BOTTOM SECTION CORNER BRACKET) REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DWG. SH670-3360
- [SDR SWIA2022081666256](https://openairdocs.org/sdr/SWIA2022081666256.md): Frame · corroded · Jun 15, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS349.00 IS CORRODED ON THE LOWER FLANGE AND WEB BETWEEN STGR26L & 26R. (MARKED) (C-CHECK RO 8/14/2022) REMOVED AND REPLACED FS349.00 FRAME FROM STR 23L TO STR 24R REF. DRWG SH690-31350 REV. M AND CRJ 700 SRM 51-42-06-001-001-A01. PRESSURIZATION
- [SDR SWIA2022081666255](https://openairdocs.org/sdr/SWIA2022081666255.md): Stringer · corroded · Jun 15, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR27 FROM FS349.00 AFT IS CORRODED. (MARKED) (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 27 FROM FS333.00 TO FS352.00 REF. DRWG SH690-31350 REV. M AND CRJ 700 SRM 51-42-06-001-001-A01. PRESSURIZATION LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-90
- [SDR SWIA2022081666254](https://openairdocs.org/sdr/SWIA2022081666254.md): Stringer · corroded · Jun 15, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > BACK-UP SILL STGR21L FROM FS333.00 €“ FS349.00 IS CORRODED. (C-CHECK RO 8/14/2022) REMOVED AND INSTALLED NEW BACK-UP SILL FROM FS333.00 TO FS349.00 REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG:SH670-31810 REV Y. COMPLIED WITH TASK CARD 51-900-1002-S
- [SDR SWIA2022081666253](https://openairdocs.org/sdr/SWIA2022081666253.md): Stringer · corroded · Jun 15, 2022 · N608SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > BACK-UP SILL STGR21L FROM FS310.00 €“ FS319.00 IS CORRODED. (C-CHECK RO 8/14/2022) REMOVED AND REPLACED STR 21L BACK-UP SILL FROM FS310.00 TO FS333.00 REF. DRWG SH670-31810 REV. Y AND CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-100

Next page: https://openairdocs.org/aircraft/N608SK/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 = 'N608SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N608SK/reports

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