# Service difficulty reports: N707SK

A list on [N707SK](https://openairdocs.org/aircraft/N707SK.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 6 · 282 reports

- [SDR SWIA2026071576654](https://openairdocs.org/sdr/SWIA2026071576654.md): Elevator System · faulted · Jul 15, 2026 · N707SK · Cndair CL6002C10 · Elevator Control System
  > FLIGHT CREW REPORTS CO-PILOT TRIM QUIT WORKING AT APPROX 5000' AGL, RECEIVED AN ELEVATOR SPLIT MASTER WARNING. ENGAGED AUTOPILOT AC BEGAN PORPOSING, DISCONNECTED TO AP, DISCONNECTED THE ELEVATOR TRIM AND DECLARED AN EMERGENCY AND RETURNED TO THE CITY OF ORIGIN
- [SDR SWI2025F00643](https://openairdocs.org/sdr/SWI2025F00643.md): Bonding Strap · sheared · May 15, 2025 · N707SK · Cndair CL6002C10 · Wing System Wiring
  > DURING REPAIR OF THE BONDING STRAP FOR THE LH WING OBD SPOILER FOUND INB SIDE BONDING STRAP TAB SHEARED OFF. (FILED CLOSED)COMPLIED WITH ALL STEPS OF PERMANENT REPAIR REO 670--57-73-062 REV-- DATED 2025-05-15 REPAIR TOLH WING O/B MULTI FUNCTION SPOILER GROUND
- [SDR SWIA2025040400303](https://openairdocs.org/sdr/SWIA2025040400303.md): Cleat · damaged · Mar 3, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD AND AFT CLEAT UNDER END CAPS HAVE ELONGATED HOLES. (MARKED). (C-CHECK RO 04/04/2025)FABRICATED PAX DOOR FWD AND AFT CLEAT UNDER END CAPS P/N: 600-31902-55 AND P/N: 600-31902-56 REF. CRJ-700 SRM 51-24-36-001-001-A01, SRM 51-24-16-001-001-A01, AND B
- [SDR SWIA2025040400223](https://openairdocs.org/sdr/SWIA2025040400223.md): Access Panel · cracked · Feb 23, 2025 · N707SK · Cndair CL6002C10 · Wing, Plate/Skin
  > DURING "OK TO CLOSE" INSPECTION OF THE LEFT WING FUEL PNLS, DISCOVERED A POSSIBLE CRACK IN THE LEFT WING RIB AT LBL 22.50. (MARKED) (C-CHECK RO 04/04/2025)COMPLIED WITH ALL THE STEPS OF REO 670-57-11-226 REV -- DATED 2025-03-24. INSTALLED -1 REPAIR ANGLE - SH
- [SDR SWI2025F00432](https://openairdocs.org/sdr/SWI2025F00432.md): Skin · gouged · Feb 19, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGE FOUND ON PAX DOOR SURROUND, FWD LOWER CORNER. (C-CHECK RO 04/04/2025)COMPLIED WITH REO 670-53-21-2589 REV -- DATED 2025-03-12 STEP 1 TO 3. ON FWD LOWER CORNER. ENSURED BLEND OUT HAS SMOOTH CONTOUR, ENSURED COMPLETE DAMAGE REMOVAL, ENSURED MINIMUM REMAINI
- [SDR SWI2025F00431](https://openairdocs.org/sdr/SWI2025F00431.md): Fitting · corroded · Feb 19, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT HANDRAIL FITTING FS343 IS CORRODED (C-CHECK RO 04/04/2025)REPLACED PAX DOOR AFT HANDRAIL FITTING WITH NEW PART REF. DWG# SH670-31810 REV:AE AND CRJ700 SRM 51-42-21-001-001-A01, COMPLIED WITH 51-900-1002-SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR (*
- [SDR SWIA2025040400219](https://openairdocs.org/sdr/SWIA2025040400219.md): Fitting · corroded · Feb 19, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD HANDRAIL FITTING FS315 CORRODED (C-CHECK RO 04/04/2025)REPLACED PAX DOOR FWD HANDRAIL FITTING WITH NEW PART REF. DWG# SH670-31810 REV:AE CRJ700 SRM 51-42-21-001-001-A01COMPLIED WITH ST CARD 51-900-1002-SKY
- [SDR SWI2025F00433](https://openairdocs.org/sdr/SWI2025F00433.md): Floorbeam · corroded · Feb 15, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON TOP FLANGE OF LBL9 FLOOR BEAM AT FS581 (C-CHECK RO 04/04/2025)REPAIRED CORRODED LBL 9 BEAM SECTION BETWEEN FS571.45 - FS591.60 WITH BEAM SPLICE REPAIR, REF CRJ-700 SRM 53-00-41-201-001-A01 FIGURE 53-00-41-991-830 AND REO 670-53-31-1008 REV -
- [SDR SWIA202504040215](https://openairdocs.org/sdr/SWIA202504040215.md): Floorbeam · corroded · Feb 15, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND SEVERALSL SPOT OF CORROSION AT LBL9 FLOOR BEAM AT FS477 TO FS577 (C-CHECK RO 04/04/2025)CORROSION FOUND TO BE OUT OF LIMITS, INSTALLED NEW SECTION OF FLOORBEAM FROM FS512.00 TOFS571.45, NO CORROSION NOTED FROM FS477 TO FS 512. WITH 8 EA -11 CLEATS, 4 EA
- [SDR SWIA202504040214](https://openairdocs.org/sdr/SWIA202504040214.md): Floorbeam · corroded · Feb 14, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON TOP FLANGE OF RBL 9 FLOOR BEAM APPRX FS 581 (C-CHECK RO 04/04/2025)REPAIRED CORRODED RBL 9 BEAM SECTION BETWEEN FS 571.45 AND FS 587.60 WITH BEAM SLICE REPAIR REF CRJ 700 SRM 53-00-41-201-001-A01 FIG 53-00-41-991-830 AND REO 670-53-31-1009 R
- [SDR SWI2025F00436](https://openairdocs.org/sdr/SWI2025F00436.md): Diaphragm · damaged · Feb 8, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND ELONGATED HOLES AT DIAPHRAGM UNDER PASSENGER DOOR AFT UPPER END CAP P/N 601R38122-2. (C-CHECK RO 04/04/2025)REMOVED AND REPLACED PAX DOOR AFT UPPER END CAP DIAPHRAGM REF. CRJ-700 SRM 51-42-06-001-001-A01 AND IAW DWG 601R31702 REV-N AND PERFORMED LEAK TE
- [SDR SWI2025F00435](https://openairdocs.org/sdr/SWI2025F00435.md): Diaphragm · damaged · Feb 8, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND ELONGATED HOLES AT DIAPHRAGM UNDER PASSENGER DOOR AFT UPPER END CAP P/N 601R38122-1. (C-CHECK RO 04/04/2025)REMOVED AND REPLACED PAX DOOR AFT UPPER END CAP DIAPHRAGM REF. CRJ-700 SRM 51-42-06-001-001-A01 AND IAW DWG 601R31702 REV-N AND PERFORMED LEAK TE
- [SDR SWI2025F00434](https://openairdocs.org/sdr/SWI2025F00434.md): Diaphragm · cracked · Feb 8, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND CRACKS IN ONE HOLE AT DIAPHRAGM UNDER PASSENGER DOOR FWD UPPER END CAP P/N 601R38122-2. PART REPLACEMENT REQUIRED. (C-CHECK RO 04/04/2025)REMOVED AND REPLACED FORWARD DIAPHRAGM UNDER PAX DOOR FORWARD UPPER END CAP REF. CRJ-700 SRM51-42-06-001-001-A01 AND
- [SDR SWIA202504040208](https://openairdocs.org/sdr/SWIA202504040208.md): Retainer · damaged · Feb 8, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND RETAINER SEAL PAX DOOR AFT CORNER WITH ELONGATED HOLES. (C-CHECK RO 04/04/2025)REMOVED AND REPLACED PAX DOOR AFT SEAL RETAINER P/N 600-31902-289 REF. CRJ-700 SRM 51-42-06-001-001-A01 AND IAW DWG 601R31702 REV-N AND TASK CARD 51-900-1002-SKY AND PERFORME
- [SDR SWIA202504040206](https://openairdocs.org/sdr/SWIA202504040206.md): Web · corroded · Feb 6, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS 280 RH LOWER WEB CORRODED (C-CHECK RO 04/04/2025)INSTALLED -2 RHS LOWER WEB, -4 RHS BUTTSTRAP -6 AND -8 SHIMS AT FS 280 REF CRJ 700 SRM 53-11-10-201-004-A01. COMPLIED WITH SKY WEST TASK CARD 51-900-1002 SKY (CL600-2C10) STRUCTURAL MAJOR REPAIR. SEE CONTINUA
- [SDR SWIA202504040201](https://openairdocs.org/sdr/SWIA202504040201.md): Floor Support · corroded · Feb 1, 2025 · N707SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL FORWARD OF SERVICE DOOR CORRODED (C-CHECK RO 04/04/2025) INSTALLED NEW R/H FLOOR SILL BETWEEN FS280.00 - FS319.70 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DWG.NO. SH670-32170 REV-K
- [SDR SWI2025F00438](https://openairdocs.org/sdr/SWI2025F00438.md): Frame · cracked · Jan 25, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FS333.00 STRG 1RH - 2RH, FRAMED CRACKED BOTTOM AREA (MARKED) (C-CHECK RO 04/04/2025)PERFORMED REPAIR TO FRAME SECTOR AT FS333.00 BETWEEN STR 1R & STR 2R REF. REO 670-53-21-2552 REV -- DATED 2025-02-28 ALL STEPS COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS. COM
- [SDR SWI2025F00437](https://openairdocs.org/sdr/SWI2025F00437.md): Door Sill · damaged · Jan 25, 2025 · N707SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > REPLACE PAX DOOR LOWER FLOOR SILL ANGLE (C-CHECK RO 04/04/2025)REPLACED PAX DOOR LOWER FLOOR SILL ANGLE WITH NEW PART. REF DWG# SH670-31810 REV: AE AND CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 REV:38 DATE: JUL 25/2020, COMPLIED WITH
- [SDR SWIA202504040125](https://openairdocs.org/sdr/SWIA202504040125.md): Skin · scratched · Jan 25, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > VHF ANTENNA NUMBER 2 SKIN HAS SURFACE SCRATCHES (C-CHECK RO 04/04/2025)BLEND IS OUT OF LIMITS REF CRJ700 SRM 53-21-01-101-006-A01 AND RECEIVED REO 670-53-21-2564 REV -- 2025-02-16, FOUND ACCEPTABLE TO ENGINEERING, AND PERFORMED OPERATIONAL TEST OF THE VHF SYS
- [SDR SWIA202504040122](https://openairdocs.org/sdr/SWIA202504040122.md): Attach Fitting · cracked · Jan 22, 2025 · N707SK · Cndair CL6002C10 · Wing, Attach Fittings
  > RH SLAT TRACK 1-3 CANNISTER ATTACH FITTING INSIDE FUEL PANEL 651AB, IS CRACKED (MARKED) (C-CHECK RO 04/04/2025)COMPLIED WITH REO 670-57-42-577 REV-- DATED: 2016-12-02, APPLIED FINISH AT CUT LINE EDGES AND FABRICATED ALL REPAIR PARTS AND MAINTAINED 2D MINIMUM E
- [SDR SWI2025F00425](https://openairdocs.org/sdr/SWI2025F00425.md): Rivet · sheared · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 04/04/2025)REPAIRED R/H UPPER TRANSCOWL INNER SKIN SHEARED Z STIFFENER RIVETS REF MHIRJ REO 670-54-21-1715 REV -- 2025-03-03. COMPLIED WITH SKYCARD 51-900-1002-SKY
- [SDR SWI2025F00424](https://openairdocs.org/sdr/SWI2025F00424.md): Stand Off · cracked · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 04/04/2025)REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER INBD TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-
- [SDR SWI2025F00423](https://openairdocs.org/sdr/SWI2025F00423.md): Stand Off · cracked · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 04/04/2025)REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER OUTBD TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 5
- [SDR SWI2025F00422](https://openairdocs.org/sdr/SWI2025F00422.md): Rivet · sheared · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 04/04/2025)ON R/H LOWER TRANSCOWL, 3 EA. HOLES AT SHEARED FASTENERS COMMON TO ZED STIFFENER P/N CN624-2038-203 ON INNER SKIN FOUND TO BE CRACK FREE WITH NO DAMAGE NOTED. ENGINEERING RECEIVED FOR ALTE
- [SDR SWI2025F00421](https://openairdocs.org/sdr/SWI2025F00421.md): Frame · corroded · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS517.00 LOWER FLANGE, FORWARD AND AFT WEBS ARE CORRODED BETWEEN STGR25L & 26L (MARKED) (C-CHECK RO 04/04/2025)REMOVED CORROSION ON FRAME FS517.00 LOWER FLANGE, FORWARD AND AFT WEBS REF CRJ700 SRM 51-21-06-001-001-A01. REMOVED AND REPLACED LH FRAME FS517
- [SDR SWIA202504040121](https://openairdocs.org/sdr/SWIA202504040121.md): Floorbeam · cracked · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH COCKPIT FLOOR BEAM RBL 12 IS CRACKED AT THE FS280 CROSS BEAM ATTACH POINT, AT THE LOWER INNER RADIUS (MARKED) (C-CHECK RO 04/04/2025)REPAIRED RBL 12 COCKPIT FLOORBEAM FWD OF FS280 REF CRJ 700 SRM 53-11-43-201-003-A01, COMPLIED WITH SKYCARD 51-900-1002-SKY
- [SDR SWI2025F00439](https://openairdocs.org/sdr/SWI2025F00439.md): Stand Off · cracked · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 04/04/2025)REMOVED AND REPLACED L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF REF REO# 670-54-21-971, REV B, DATED 11/28/23. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY W/SKYCARD
- [SDR SWI2025F00430](https://openairdocs.org/sdr/SWI2025F00430.md): Stiffener · loose · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL Z STIFFENER RIVETS ARE PULLED LOOSE (C-CHECK RO 04/04/2025)REPAIRED L/H LWR TRANSCOWL INNER SKIN REF MHIRJ REO 670-54-21-1713 REV -- 2025-02-14 COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWI2025F00428](https://openairdocs.org/sdr/SWI2025F00428.md): Coaming · chafed · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL COAMING IS CHAFED INTO DISHING @ FWD LATCH (C-CHECK RO 04/04/2025)BLENDED DISHING CHAFE @ FWD. LATCH ON L/H LOWER TRANSCOWL COAMING. REF. CRJ700 SRM 51-12-00-001-001-A01 AND REPAIRED PER REO 670-54-21-1713 REV -- 2025-02-14, COMPLIED WITH SKY
- [SDR SWI2025F00427](https://openairdocs.org/sdr/SWI2025F00427.md): Repair · gouged · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AFT LOWER EXTERNAL SKIN REPAIR DOUBLER GOUGED FS969-FS985 (C-CHECK RO 04/04/2025)COMPLIED WITH ALL STEPS OF REO # 670-53-00-290 REV - F DATED 2019/04/26 AND PERFORMED PRESSURIZATION OF THE AIR CONDITIONING DISTRIBUTION SYSTEM WITH THE APU REF. CRJ-700 AMM 21-5
- [SDR SWI2025F00426](https://openairdocs.org/sdr/SWI2025F00426.md): Window Post · cracked · Jan 21, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CO-PILOT WINDSHIELD POST UPPER ATTACH SUPPORT FITTING CRACKED, UPPER CANOPY AREA (MARKED) (C-CHECK RO 04/04/2025)INSTALLED NEW ATTACH SUPPORT FITTING AT CO-PILOT WINDSHIELD POST UPPER REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. AND DWG# CC6
- [SDR SWI2025F00420](https://openairdocs.org/sdr/SWI2025F00420.md): Floorbeam · corroded · Jan 20, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 CROSSBEAM L/H FWD SIDE IS CORRODED. 29507506 (C-CHECK RO 04/04/2025)FS280 CROSSBEAM L/H FWD SIDE FOUND OUT OF LIMITS. REMOVED AND REPLACED BEAM REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, CRJ
- [SDR SWIA2025040400120](https://openairdocs.org/sdr/SWIA2025040400120.md): Floorbeam · corroded · Jan 20, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 CROSSBEAM R/H FWD SIDE IS CORRODED. 29506868 (C-CHECK RO 04/04/2025) INSTALLED NEW R/H FS 280 CROSS BEAM P/N CC670-34094-4SB REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-22-00
- [SDR SWIA2025040400119](https://openairdocs.org/sdr/SWIA2025040400119.md): Stringer · corroded · Jan 19, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 25R BETWEEN APPROXIMATELY FS 295.0 AND FS310.0 AS MARKED (C-CHECK RO 04/04/2025)STGR 25R FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STGR 25R FS280 - FS363 REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 REV 38 DATED JU
- [SDR SWI2025F00441](https://openairdocs.org/sdr/SWI2025F00441.md): Roller · worn · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 3 - 2 ALL ROLLERS WORN. (C-CHECK RO 04/04/2025)INSTALLED 4 EA R/H SLAT TRACK 3-2 ROLLERS (2 EA P/N: CC670-12459-4 AND 2 EA P/N: CC670-12459-3) REF. CRJ700 AMM 27-81-44-400-803-A01, GAP CHECK GOOD. TORQUE WRENCH USED: TUC7831 CAL DUE: 30-APR-
- [SDR SWI2025F00440](https://openairdocs.org/sdr/SWI2025F00440.md): Roller · worn · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 2-2 ROLLERS, OUTBOARD FWD AND INBOARD FWD WORN (C-CHECK RO 04/04/2025)INSTALLED NEW SERVICEABLE OUTBOARD FWD AND INBOARD FWD R/H SLAT 2-2 TRACK ROLLERS (P/N: CC670-12048-3WD) REF. CRJ700 AMM 27-81-44-400-802-A01 GAP CHECK GOOD. TORQUE WRENCH
- [SDR SWIA2025040703](https://openairdocs.org/sdr/SWIA2025040703.md): Roller · worn · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING SLAT TRACK 1-2 ROLLERS, OUTBOARD FWD, OUTBOARD AFT AND INBOARD AFT WORN. (C-CHECK RO 04/04/2025)INSTALLED NEW SIDE ROLLERS AT R/H WING SLAT TRACK 1-2, OUTBOARD FWD, OUTBOARD AFT AND INBOARD AFT PER CRJ 700 AMM 27-81-44-000-801-A01. OPS CHECK GOOD NO D
- [SDR SWIA2025040702](https://openairdocs.org/sdr/SWIA2025040702.md): Roller · worn · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 3-2 ROLLERS OUTBOARD FWD, INBOARD FWD AND INBOARD AFT WORN. (C-CHECK RO 04/04/2025)REMOVED WORN SLAT-TRACK SIDE ROLLERS FROM L/H WING SLAT-TRACK 3-2 3E/A (OUTBD FWD,INBD FWD, & INBD AFT) REF CRJ-700 AMM 27-81-44-000-803-A01 AND INSTALLED NEW
- [SDR SWIA2025040701](https://openairdocs.org/sdr/SWIA2025040701.md): Slat Track · worn · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 2-2 ROLLERS OUTBOARD FWD AND INBOARD AFT WORN. (C-CHECK RO 04/04/2025)REMOVED THE L/H WING SLAT TRACK 2-2 OUTBOARD FWD AND INBOARD AFT SIDE ROLLERS REF. CRJ700 AMM 27-81-44-000-802-A01 INSTALLED A NEW SERVICEABLE L/H WING SLAT TRACK 2-2 OUTB
- [SDR SWIA202504070118](https://openairdocs.org/sdr/SWIA202504070118.md): Roller · worn · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 1-2 ALL ROLLERS WORN (C-CHECK RO 04/04/2025)REMOVED LH WING SLAT TRACK 1-2 SIDE ROLLERS REF CRJ700 AMM 27-81-44-000-801 (CONFIG A01) AND INSTALLED AND GAPPED NEW SIDE ROLLERS REF CRJ700 AMM 27-81-44-400-801-A01. USED CALIBRATED TORQUE WRENCH
- [SDR SWI2025F00419](https://openairdocs.org/sdr/SWI2025F00419.md): Splice Strap · corroded · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Structure
  > FS319 FRAME SPLICE STRAP (FWD SIDE OF THE SERVICE DOOR) IS CORRODED AT THE FLOOR LEVEL (C-CHECK RO 04/04/2025)BLENDED AND REMOVED CORROSION AT FS319 FRAME SPLICE STRAP (FWD OF SERVICE DOOR). FOUND TO BE ACCEPTABLE AT THIS TIME REF REO 670-53-21-2576 REV -- DA
- [SDR SWIA2025040400118](https://openairdocs.org/sdr/SWIA2025040400118.md): Cup · corroded · Jan 18, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > THE PAX DOOR FWD HANDRAIL CUP IS CORRODED (C-CHECK RO 04/04/2025)REPLACED THE PAX DOOR FWD HANDRAIL CUP WITH NEW PART. REF DWG SH670-31810 REV: AE; CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA2025040400117](https://openairdocs.org/sdr/SWIA2025040400117.md): Floorbeam · corroded · Jan 17, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL27 FLOOR BEAM IS CORRODED FS1010-1031 (C-CHECK RO 04/04/2025)BLENDED/REMOVED CORROSION AT LBL27 FS1010 - FS1031 FLOOR BEAM AND FOUND TO BE OUT OF LIMITS. REPLACED CORRODED FLOOR BEAM REF CRJ700 SRM 53-00-41-201-001-A01, COMPLIED WITH SKYCARD 51-900-1002- S
- [SDR SWI2025F00418](https://openairdocs.org/sdr/SWI2025F00418.md): Striker · dented · Jan 16, 2025 · N707SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR SURROUND, SEAL STRIKER IS DENTED ABOVE AFT PULL-IN LEVER BRACKET. (C-CHECK RO 04/04/2025)REPLACED PAX DOOR AFT SIDE SEAL STRIKER REF. CRJ-700 SRM 53-21-23-201-003-A01 AND PERFORMED LEAK TEST OF THE DOORS IN PRESSURIZED AREAS REF. CRJ-700 AMM 52-00-00-
- [SDR SWI2025F00417](https://openairdocs.org/sdr/SWI2025F00417.md): Floorbeam · corroded · Jan 16, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOORBOARD SUPPORT ANGLE ON THE FWD SIDE OF THE FS280 BEAM IS CORRODED (C-CHECK RO 04/04/2025)BLENDED AND REMOVED CORROSION AT COCKPIT FLOORBOARD SUPPORT ANGLE FS280 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SUPPORT ANGLE REF CRJ700 SRM 51-4
- [SDR SWIA2025040400116](https://openairdocs.org/sdr/SWIA2025040400116.md): Floorbeam · cracked · Jan 16, 2025 · N707SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 CLIP IS CRACKED RBL12 OB SIDE (C-CHECK RO 04/04/2025)REMOVED, REPLACED AND INSTALLED NEW CLIP P/N CC670-34099-2SB AT FS 280 RBL 12 REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. CC670-34010 REV -K, COMPLIED WITH SKY WEST SKY CARD 51-900-1002-SKY (CL60
- [SDR SWI2025F00416](https://openairdocs.org/sdr/SWI2025F00416.md): Hinge Fitting · gouged · Jan 10, 2025 · N707SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE LUGS ON AIRFRAME SIDE GOUGED AS MARKED (C-CHECK RO 04/04/2025)BLENDED OUT TYPE 1 DAMAGE (GOUGING) ON PASSENGER DOOR HINGE LUGS ON AIRFRAME SIDE WITHIN LIMITS PER CRJ700 SRM 53-21-23-201-010-A01 AND COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2025040400110](https://openairdocs.org/sdr/SWIA2025040400110.md): Vane · gouged · Jan 10, 2025 · N707SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT WING OUTBOARD FLAP VANE MULTIPLE BUTTE DOOR CAMS GOUGED AS MARKED (C-CHECK RO 04/04/2025)INSTALLED NEW BUTE DOOR CAM FITTING AT FLS296.07 AND APPLIED AERODYNAMIC SEALANT REF CRJ 700 SRM 57-53-02-201-002-A01 REPAIR TYPE 1 AND REPAIRED ALL OTHER LOCATION
- [SDR SWIA2025040401211](https://openairdocs.org/sdr/SWIA2025040401211.md): Skin · dented · Dec 11, 2024 · N707SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA62022-670-53-61-1716 N707SK MXCODEID52967-PR - AFT FUSELAGE OUTSIDE SKINR/H SIDE BETWEEN FS 1015.00 AND FS 1051.30 AND BETWEEN STR 27R AND STR 23R THERE ARE VARIOUS DENTS AND GOUGES AND NICKS. REPAIRED AFT FUSELAGE O
- [SDR SWIA2024031800015](https://openairdocs.org/sdr/SWIA2024031800015.md): Anti-Ice Valve · faulted · Mar 15, 2024 · N707SK · Cndair CL6002C10 · Airfoil Anti/De-ice System
  > TROUBLE SHOOT HISTORY OF R WING A/I CAUTION MESSAGESMCI TYPE: TROUBLESHOOTING PRIORITY 1R WING A/I CAUTION MESSAGE WITH WING ANTI ICE ON IN ICING CONDITIONS WITH POWER SET NEAR 80 PERCENT N2. ICE FOUND ACCUMULATING ON RIGHT WING LEADING EDGE BY VISUAL INSPECTI

Next page: https://openairdocs.org/aircraft/N707SK/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 = 'N707SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N707SK/reports

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