# Service difficulty reports: N784SK

A list on [N784SK](https://openairdocs.org/aircraft/N784SK.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 · 150 reports

- [SDR SWIA2026082477121](https://openairdocs.org/sdr/SWIA2026082477121.md): Repair · out of limits · Aug 24, 2026 · N784SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > REMOVED REO 670-53-21-1611 REPAIR DOUBLER AT LT FUSELAGE SKIN BTWN BS 394 - 437, STR 14L - 17L DUE TO CLOSE POXIMITY OF ATG 4 WIFI ANTENNA LOCATION. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT REPAIR OF DOUBLER AT LH FUSELAGE SKIN IAW REO 670-53-21-2
- [SDR SWIA2026081877120](https://openairdocs.org/sdr/SWIA2026081877120.md): Skin · demodification · Aug 18, 2026 · N784SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581 - 597, STR 24R - 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED A PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCA
- [SDR SWIA2026081877119](https://openairdocs.org/sdr/SWIA2026081877119.md): Skin · demodification · Aug 18, 2026 · N784SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 1000 - 1015, STR 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED A PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN L
- [SDR SWIA2026081877118](https://openairdocs.org/sdr/SWIA2026081877118.md): Skin · demodification · Aug 18, 2026 · N784SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLE
- [SDR SWIA2026081877117](https://openairdocs.org/sdr/SWIA2026081877117.md): Skin · demodification · Aug 18, 2026 · N784SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847, STR 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAG
- [SDR SWIA2024092301](https://openairdocs.org/sdr/SWIA2024092301.md): Detector · false indication · Sep 21, 2024 · N784SK · Cndair CL6002C10 · Fire Protection System
  > R BLEED WARNING MSG IN FLIGHT. (FLIGHT 5726 - FILED CLOSED) CAPTAIN CONFIRMED L BLEED WARNING MESSAGE WAS THE ISSUE, NOT R BLEED WARNING. HAD CAPTAIN CREATE A NEW WRITE-UP WITH THE CORRECT DISCREPANCY. PLEASE REFERENCE AML#1435403 FOR CORRECT DISCREPANCY.
- [SDR SWIA20240920037](https://openairdocs.org/sdr/SWIA20240920037.md): Slat Track · cracked · Aug 12, 2024 · N784SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > SUSPECTED CRACK AT LH SLAT TRACK FUEL CANISTER 1-3 (C-CHECK RO 9/19/2024) PERFORMED REPAIR AT LH SLAT TRACK FUEL CANISTER 1-3 CRACKED BRACKET, REF REO 670-57-42-577 REV-- DATE: 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECK GOOD, LEA
- [SDR SWIA20240920035](https://openairdocs.org/sdr/SWIA20240920035.md): Slat Track · cracked · Aug 12, 2024 · N784SK · Cndair CL6002C10 · Leading Edge Devices
  > SUSPECTED CRACK AT RH SLAT TRACK FUEL CANISTER 1-3 (C-CHECK RO 9/19/2024) PERFORMED REPAIR AT AT RH SLAT TRACK FUEL CANISTER 1-3 AND PERFORMED REO 670-57-42-577 REV-- DATE: 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECK GOOD
- [SDR SWIA20240920034](https://openairdocs.org/sdr/SWIA20240920034.md): Stringer · cracked · Jul 16, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L AT FS280 IS CRACKED (C-CHECK RO 9/19/2024) REPAIRED STGR3L FS280.00 IAW REO 670-53-21-493 REV. D DATE 2015-07-10. SEE CONTINUE CARD FOR WORK PERFORMED. PRESSURE CHECK OF REPAIR AREA GOOD IAW CRJ700 AMM 21-31-00-910-801-A01SERVICE BULLETIN 6
- [SDR SWIA20240920033](https://openairdocs.org/sdr/SWIA20240920033.md): Window Post · cracked · Jul 15, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LH WINDSHIELD POST LOWER OUTBD CLIP APPEARS TO BE CRACKED (C-CHECK RO 9/19/2024) REMOVED AND REPLACED LH WINDSHIELD POST LWR OB CLIP WITH NEW, REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV -F AND DWG GC212-0045 REV -ACOMPLIED WITH SKYWEST
- [SDR SWIA2024092032](https://openairdocs.org/sdr/SWIA2024092032.md): Buttstrap · corroded · Jul 13, 2024 · N784SK · Cndair CL6002C10 · Aerodynamic Fairings
  > MLG FAIRING PANEL 194AB R/H TOP BUTTSTRAP FUSELAGE MULTIPLE AREA HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE M/C BEAM AT RBL48 BETWEEN FS826 - FS836 REF REO 670-53-42-100 REV -- 2024-08-28. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA20240920031](https://openairdocs.org/sdr/SWIA20240920031.md): Frame · cracked · Jul 13, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME CRACKED AT FS333.00 BETWEEN STGR 1R AND STGR 2R (MARKED) (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO FRAME SECTOR FS333 BETWEEN STR 1R & STR 2R REF REO 670-53-21-2437 REV -- 2024-07-24. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWI20240920030](https://openairdocs.org/sdr/SWI20240920030.md): Latch · cracked · Jul 13, 2024 · N784SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > RH TRU BAY DOOR, THE AFT DOOR LATCH CUTOUT POSSIBLE CRACK IN THE ANGLE RADIUS (MARKED) (C-CHECK RO 9/19/2024) REPLACED THE RH TRU BAY DOOR LANDING REF REO 670-53-11-2003 REV -A 2024-08-26, REO 670-53-11-1996 REV -- 2024-08-05, DWG: CC670-33151 REV -D, C
- [SDR SWIA20240920029](https://openairdocs.org/sdr/SWIA20240920029.md): Door · cracked · Jul 13, 2024 · N784SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > LH TRU BAY DOOR, THE AFT DOOR LATCH CUTOUT POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 9/19/2024) REPAIRED LH TRU BAY DOOR LANDING REF. REO 670-53-11-1996 REV-- DATED: 2024-08-05. REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG NO: CC670-33040 REV -
- [SDR SWIA202409200028](https://openairdocs.org/sdr/SWIA202409200028.md): Strut · gouged · Jul 13, 2024 · N784SK · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/Axle
  > NLG SHOCK STRUT, THE AFT SIDE OF CHROME PISTON HAS A VERTICLE GOUGE (MARKED) (C-CHECK RO 9/19/2024) REPAIRED NLG SHOCK STRUCT AFT SIDE OF CHROME PISTON GOUGE BY COMPLLYING WITH ALL STEPS OF REO # 670-32-21-237, REV. D, DATED: 2020-07-28 AND GOODRICH SCR
- [SDR SWIA20240920028](https://openairdocs.org/sdr/SWIA20240920028.md): Spar · gouged · Jul 12, 2024 · N784SK · Cndair CL6002C10 · Wing Spar
  > RH WING AFT FACE OF REAR WING SPAR HAS GOUGES AROUND 2ND LIGHTNING HOLE BETWEEN WS350.25 AND WS370.25 (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO RH WING AFT FACE OF REAR WING SPAR BETWEEN WS350.25 AND WS370.25 REF REO 670-57-21-987 REV-- DATE 2024-0
- [SDR SWIA20240920027](https://openairdocs.org/sdr/SWIA20240920027.md): Floorbeam · corroded · Jul 12, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CABIN FLOOR LEFT T CAP LBL27 BETWEEN APPROXIMATELY FS1000.00 AND FS1050.00 CORRODED AS MARKED (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE CABIN FLOOR BEAM AT LBL27, APPROX FS1000 - FS1050 REF REO 670-53-61-2337 REV -A 2024-08-22 AND CRJ-700 SRM
- [SDR SWIA20240920026](https://openairdocs.org/sdr/SWIA20240920026.md): Floorbeam · corroded · Jul 12, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CABIN FLOOR RIGHT T CAP RBL9 BETWEEN FS1007.00 AND FS1045.00 CORRODED AS MARKED (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO THE RBL9 FLOOR BEAM AT FS1007 - FS1045 REF CRJ-700 SRM 53-00-41-201-001-A01, REO 670-53-61-2340 REV -- 2024-08-06, AND REO 670
- [SDR SWIA2024092000117](https://openairdocs.org/sdr/SWIA2024092000117.md): Fitting · corroded · Jul 12, 2024 · N784SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR FITTING, CLOSING CORROSION BETWEEN FS319 AND FS333.00 (MARKED) (C-CHECK RO 9/19/2024) REMOVED CORROSION ON PAX DOOR FITTING, CLOSING. BLEND FOUND TO BE OUT OF LIMITS AT 32% MATERIAL LOSS. REMOVED AND REPLACED PAX DOOR FITTING, CLOSING. N
- [SDR SWIA202492000012](https://openairdocs.org/sdr/SWIA202492000012.md): Door Sill · corroded · Jul 12, 2024 · N784SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SILL LOWER SEAL STRIKER CORRODED AT SCREW HOLES AS (MARKED) (C-CHECK RO 9/19/2024) INSTALLED NEW SERVICE DOOR SILL LOWER SEAL STRIKER P/N SH670-31412-7 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-31950 REV-Y. ALL CHECKS GOOD.
- [SDR SWIA20240920025](https://openairdocs.org/sdr/SWIA20240920025.md): Floorbeam · corroded · Jul 11, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > L/H FLOOR BEAM LBL 9 HAS CORROSION APPROXIMATELY BETWEEN FS549.00 TO FS565.00 (MARKED) (C-CHECK RO 9/19/2024) PERFORMED FLOOR BEAM SPLICE REPAIR APPROX. FS549.00 TO FS565.00 REF REO 670-53-31-916 REV -- 2024-08-12, REO 670-53-31-918 REV -- 2024-08-12 A
- [SDR SWIA202409200025](https://openairdocs.org/sdr/SWIA202409200025.md): Floor Support · corroded · Jul 11, 2024 · N784SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > R/H FLOOR SILL BETWEEN FS280.00 TO FS295.00 HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) BLENDED REPORTED CORRODED AREAS FROM R/H FLOOR SILL BETWEEN FS 280 AND FS 295, FOUND BLENDED AREAS OUT LIMITS PER REF CRJ 700 SRM 53-00-00-101-001-A01. REMOVED
- [SDR SWIA2024092000014](https://openairdocs.org/sdr/SWIA2024092000014.md): Floor Support · corroded · Jul 11, 2024 · N784SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL BETWEEN FS349.00 TO FS364.00 HAS CORROSION (MARKED) (C-CHECK RO 9/19/2024) REPAIRED R/H FLOOR SILL BETWEEN FS349.00 TO FS364 REF REO 670-53-21-1806 REV--2020-08-27 AND DWG SH670-32170 REV V COMPLIED WITH TASK CARD 51-900-1002-SKY LEAK
- [SDR SWIA20240920024](https://openairdocs.org/sdr/SWIA20240920024.md): Hinge · chafed · Jul 9, 2024 · N784SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE DOOR SIDE, ALL LUG LANDS HAVE CHAFFING AND LUGS HAVE VARIOUS CHAFES AND SCRATCHES AT THE HIGH POINT OF THE LUG AND THE LUG BASE NEAR THE SEAL SIDE. HN00173018 (C-CHECK RO 9/19/2024) BLENDED AND EVAL'D PAX DOOR HINGE LUGS ON DOOR SIDE, FOU
- [SDR SWIA20240920023](https://openairdocs.org/sdr/SWIA20240920023.md): Hinge · chafed · Jul 9, 2024 · N784SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE FUSELAGE SIDE, ALL LUG LANDS HAVE CHAFFING AND ALL LUGS HAVE SOME DEGREE OF CHAFFING AND SCRATCHES. HN00173016 (C-CHECK RO 9/19/2024) REMOVED AND REPLACED PASSENGER DOOR HINGE (FUSELAGE SIDE) REF. CRJ 700 SRM 53-21-23-201-007-A01, AND DWG
- [SDR SWIA2024092000016](https://openairdocs.org/sdr/SWIA2024092000016.md): Stand Off · cracked · Jul 9, 2024 · N784SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 9/19/2024) INSTALLED 1 EA. NEW A BRACKET P/N CN624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3 AND COMPLIED WITH 51-900-1002-
- [SDR SWIA2024092000015](https://openairdocs.org/sdr/SWIA2024092000015.md): Stand Off · cracked · Jul 9, 2024 · N784SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 9/19/2024) INSTALLED NEW R/H UPPER TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. SEE CONTINUATION SHEET FOR DETAILS.
- [SDR SWIA2024092000013](https://openairdocs.org/sdr/SWIA2024092000013.md): Transcowl · cracked · Jul 9, 2024 · N784SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 9/19/2024) REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY. REF. CAM
- [SDR SWIA202409200023](https://openairdocs.org/sdr/SWIA202409200023.md): Hinge Fitting · gouged · Jul 2, 2024 · N784SK · Cndair CL6002C10 · Ailerons
  > RH AILERON #1 HINGE FITTING OUTBOARD LUG GOUGED (C-CHECK RO 9/19/2024) COMPLIED WITH ALL STEPS OF REO 670-57-51-562 REV --, DATED 2024-08-15. BLEND REPAIR WITH EXCEPTANCE OF REPORTED MATERIAL DIMENSIONS RH AILERON #1 HINGE FITTING. SEE CONTINUE CARD FOR
- [SDR SWIA202409200022](https://openairdocs.org/sdr/SWIA202409200022.md): Hinge Fitting · gouged · Jul 2, 2024 · N784SK · Cndair CL6002C10 · Ailerons
  > RH AILERON #2 HINGE FITTING OUTBOARD LUG AND LOWER INBOARD SIDE HAS GOUGES (C-CHECK RO 9/19/2024) REPAIRED RH AILERON #2 HINGE FITTING GOUGES THROUGH COMPLIANCE WITHL STEPS OF REO 670-57-51-562 REV --, DATED 2024-08-15, BLEND REPAIR AND DAMAGE ALLOWNAC
- [SDR SWIA202409200021](https://openairdocs.org/sdr/SWIA202409200021.md): Hinge Fitting · gouged · Jul 2, 2024 · N784SK · Cndair CL6002C10 · Ailerons
  > RH AILERON #3 HINGE FITTING INBOARD LUG AND LOWER INBOARD SIDE HAS GOUGES (C-CHECK RO 9/19/2024) REPAIRED GOUGES ON RH AILERON HINGE FITTING #3 BY COMPLYING WITH ALL STEPS OF REO 670--57-51-562 REV -- DATED 2024-08-15, BLEND ALLOWANCE REPAIR, STEPS 1-4
- [SDR SWIA202409200020](https://openairdocs.org/sdr/SWIA202409200020.md): Hinge Fitting · gouged · Jul 2, 2024 · N784SK · Cndair CL6002C10 · Ailerons
  > RH AILERON #4 HINGE FITTING INBOARD AND OUTBOARD LUG HAS GOUGES (C-CHECK RO 9/19/2024) REMOVED DAMAGE FROM R/H AILERON #4 HINGE I/B AND O/B LUG IAW CRJ700 SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-51-562 REV --, DATED 2024-08-15. C
- [SDR SWIA2024092000019](https://openairdocs.org/sdr/SWIA2024092000019.md): Skin · dented · Jun 27, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MULTIPLE DENTS,NICKS, GOUGES,ON AFT FUSELAGE SKIN IN BETWEEN APPROX FS 1000 TO FS 1051 BETWEEN STR 21R AND STR 27 IN AREA OF GROUND A/C SERVICE DOOR. (C-CHECK RO 9/19/2024) REPAIRED MULTIPLE DENTS,NICKS, GOUGES,ON AFT FUSELAGE SKIN BETWEEN FS 1000 TO
- [SDR SWIA202409200018](https://openairdocs.org/sdr/SWIA202409200018.md): Skin · dented · Jun 22, 2024 · N784SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND DENT ON RHS OF REAR FUSELAGE, AFT OF GROUND AIR DOOR, APPROXIMATELY 13 INCH, PARALLEL TO AFT LOWER CORNER RADIUS.OF DOOR CUT-OUT. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES.
- [SDR SWIA2024060400528](https://openairdocs.org/sdr/SWIA2024060400528.md): Engine · odor · May 28, 2024 · N784SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > STRONG FUEL ODOR OBSERVED IN CABIN DURING DESCENT AND LANDING. GROUND CABIN OBSERVED WHITE/BLUE SMOKE COMING FROM LEFT ENGINE AS AIRCRAFT APPROACHED THE GATE WITH BOTH ENGINES RUNNING. SMOKE DECREASED IN INTENSITY AFTER ENGINE WAS SHUT DOWN, BUT WHITE SMOKE CO
- [SDR SWIA2024053000028](https://openairdocs.org/sdr/SWIA2024053000028.md): Engine · smoke · May 28, 2024 · N784SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > STRONG FUEL ODOR OBSERVED IN CABIN DURING DESCENT AND LANDING. GROUND CABIN OBSERVED WHITE/BLUE SMOKE COMING FROM LEFT ENGINE AS AIRCRAFT APPROACHED THE GATE WITH BOTH ENGINES RUNNING. SMOKE DECREASED IN INTENSITY AFTER ENGINE WAS SHUT DOWN, BUT WHITE SMOKE CO
- [SDR SWI2024051300400](https://openairdocs.org/sdr/SWI2024051300400.md): Unknown · fumes · May 8, 2024 · N784SK · Cndair CL6002C10 · Air Distribution System
  > 2 MINUTES AFTER TAKEOFF RECEIVED A CALL FROM FA THAT THE AFT CABIN HAD FUMES/VERY LIGHT SMOKE EMITTING FROM THE OVERHEAD VENTS. BLEEDS OPEN TAKEOFF. QRH CLEARED FUMES. NO EICAS MSGS. (FLIGHT 5402 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 2820
- [SDR SWI2024080900396](https://openairdocs.org/sdr/SWI2024080900396.md): Unknown · fumes · May 8, 2024 · N784SK · Cndair CL6002C10 · Air Distribution System
  > 2 MINUTES AFTER TAKEOFF RECEIVED A CALL FROM FA THAT THE AFT CABIN HAD FUMES/VERY LIGHT SMOKE EMITTING FROM THE OVERHEAD VENTS. BLEEDS OPEN TAKEOFF. QRH CLEARED FUMES. NO EICAS MSGS. (FLIGHT 5402 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.
- [SDR SWIA202264552](https://openairdocs.org/sdr/SWIA202264552.md): None · damaged · Feb 18, 2022 · N784SK · Cndair CL6002C10 · Window/Windshield System
  > LEFT WINDSHIELD OUTER MOST PAIN SHATTERED IN FLIGHT (FLIGHT 5702 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24366878 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 24369201-1 FOR REMOVAL OF LH WINDSHIELD. INSTALLED SERVICEABLE CA SIDE WIN
- [SDR SWIA2021071659585](https://openairdocs.org/sdr/SWIA2021071659585.md): Windshield · cracked · Jul 15, 2021 · N784SK · Cndair CL6002C10 · Flight Compartment Windows
  > NOTICEABLE CRACKING IN THE UPPER RIGHT CORNER AND TO A LESSER EXTENT IN THE LOWER LEFT CORNER OF THE RIGHT SIDE WINDSHIELD. PRESSURIZATION WAS NORMAL DURING FLIGHT. (FLIGHT 4743 - FILED CLOSED) REMOVED AND REPLACED FO'S WINDSHIELD, OPS CHECK GOOD OF WINDS
- [SDR SWIA202155936](https://openairdocs.org/sdr/SWIA202155936.md): Windshield · cracked · Feb 2, 2021 · N784SK · Cndair CL6002C10 · Flight Compartment Windows
  > LEFT WINDOW CRACKED FLIGHT 5344 - FILED CLOSED REMOVED AND REPLACED THE CAPTAIN'S SIDE WINDOW WITH A SERVICEABLE UNIT REF AMM 56-12-01 AND TASK CARD 56-220-1000-SKY. NEW CAPTAIN'S SIDE WINDOW OPS AND LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA202052654](https://openairdocs.org/sdr/SWIA202052654.md): Strip · corroded · Sep 15, 2020 · N784SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > JOINER STRIP BETWEEN PANELS 195DL AND 195DR CORRODED. C-CHECK RO 9/20/2020. EVALUATED FAIRING JOINT STRAP BETWEEN PANELS 195DL AND 195DR, 100% MATERIAL LOSS, OUT OF LIMITS. FABRICATED NEW JOINT STRAP, REF BOMBARDIER. REMOVED CORRODED STRAP INSD INSTALLED N
- [SDR SWIA202052653](https://openairdocs.org/sdr/SWIA202052653.md): Mount · damaged · Sep 12, 2020 · N784SK · Cndair CL6002C10 · Passenger Compartment Equipment
  > SEAT 20AB HAS A MISSING SEAT TRACK MOUNT ON THE INBOARD AFT SIDE, MARKED. C-CHECK RO 9/20/2020. REMOVED AND INSTALLED NEW SEAT TRACK MOUNT P/N 41581074-505 PO T52686 /31 INBOARD AFT SIDE ON SEAT 20AB, REF ZODIAC AEROSPACE CMM.
- [SDR SWIA202052652](https://openairdocs.org/sdr/SWIA202052652.md): Mount · damaged · Sep 12, 2020 · N784SK · Cndair CL6002C10 · Passenger Compartment Equipment
  > SEAT 15AB HAS A MISSING SEAT TRACK MOUNT ON THE FWD INBOARD SIDE, MARKED. C-CHECK RO 9/20/2020. INSTALLED NEW SEAT TRACK MOUNT (STUD ASSY FRONT) P/N 41581161-501, REF CRJ 700 CMM. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202052651](https://openairdocs.org/sdr/SWIA202052651.md): Panel · damaged · Aug 30, 2020 · N784SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > THE LT FLOOR SILL HAS TWO DECOMPRESSION PANELS WITH TORN OR MISSING DIAPHRAGMS. THE FIRST IS LOCATED BETWEEN FS 364 AND FS379 AND THE SECOND IS LOCATED BETWEEN FS 453 AND FS 469 THAT REQUIRED REBULID TO INSTALL NEW DIAPHRAGMS. C-CHECK RO 9/20/2020. REMOVED
- [SDR SWIA202052650](https://openairdocs.org/sdr/SWIA202052650.md): Hinge Fitting · corroded · Aug 24, 2020 · N784SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > AFT NLG DOOR RT HINGE MOUNT CORRODED. C-CHECK RO 9/20/2020. REMOVED DAMAGED RT NLG DOOR FITTING, REF CRJ-700 SRM. INSTALLED NEW LT HINGE FITTING P/N CC670-32212-7, REF CRJ-700 SRM AND DRAWING. C/W SKYWEST ST STRUCTURE MAJOR REPAIR. SEE CONTINUE CARD FOR D
- [SDR SWIA202052649](https://openairdocs.org/sdr/SWIA202052649.md): Hinge Fitting · corroded · Aug 24, 2020 · N784SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > AFT NLG DOOR LT HINGE MOUNT CORRODED. C-CHECK RO 9/20/2020. REMOVED DAMAGED LT NLG DOOR FITTING, REF: CRJ-700 SRM. INSTALLED NEW LT HINGE FITTING P/N CC670-32212-7, REF CRJ-700 SRM AND DRAWING. C/W SKYWEST ST STRUCTURE MAJOR REPAIR. SEE CONTINUE CARD FOR
- [SDR SWIA202052648](https://openairdocs.org/sdr/SWIA202052648.md): Angle · corroded · Aug 24, 2020 · N784SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CAP ANGLE AT STGR 18L IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED AFT CAP ANGLE AT STGR 18L, IAW CRJ700 SRM.
- [SDR SWIA202052647](https://openairdocs.org/sdr/SWIA202052647.md): Angle · corroded · Aug 24, 2020 · N784SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD CAP ANGLE AT STGR 18L IS CORRODED. C-CHECK RO 9/20/2020. REMOVED AND REPLACED FWD CAP ANGLE AT STGR 18L, IAW CRJ700 SRM.
- [SDR SWIA202052646](https://openairdocs.org/sdr/SWIA202052646.md): Angle · corroded · Aug 24, 2020 · N784SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LOWER SILL ANGLE PART NUMBER SH670-31986-1 EVIDENCE OF CORROSION. C-CHECK RO 9/20/2020. REPLACED LOWER SILL ANGLE P/N SH670-31986-1, REF DWG AND CRJ-700 SRM. COMPLIED WITH SKYWEST TASK CARD.

Next page: https://openairdocs.org/aircraft/N784SK/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 = 'N784SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N784SK/reports

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