# Service difficulty reports: N778SK

A list on [N778SK](https://openairdocs.org/aircraft/N778SK.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 · 209 reports

- [SDR SWIA2026102477797](https://openairdocs.org/sdr/SWIA2026102477797.md): Heater · warning message · Oct 24, 2026 · N778SK · Cndair CL6002C11 · Windshield/Door Rain/Ice Removal
  > LEFT WINDOW HEAT CAUTION MESSAGE DURING DESCENT. FLIGHT 4260. R & R THE LEFT WINDOW COMPLIED WITH COCKPIT SIDE WINDOWTASK CARD 56-220-1000-SKY.
- [SDR SWIA2026092077223](https://openairdocs.org/sdr/SWIA2026092077223.md): Windshield · cracked · Sep 20, 2026 · N778SK · Cndair CL6002C11 · Flight Compartment Windows
  > LEFT WINDSHIELD HEAT CAUTION MESSAGE. WINDSHIELD CRACKED A FEW MINUTES AFTER THE MESSAGE CAME ON. FLIGHT 4312. LT WINDSHIELD REMOVED AND REPLACED IAW TASK CARD 56-220-1000-SKY, OPS CHKD GOOD, PRESSURIZATION CHKD GOOD.
- [SDR SWIA2026082876970](https://openairdocs.org/sdr/SWIA2026082876970.md): Ballast · failed · Aug 28, 2026 · N778SK · Cndair CL6002C11 · Passenger Compartment Lighting
  > PASSENGER LIGHT OVER 1 A BEGAN FLICKERING AND SMOKE BEGAN TO COME OUT OF THE LIGHT AREA. (FLIGHT 4324)TROUBLESHOT SMOKE IN CABIN IAW FIM 21-22-00-810-806. PERFORMED OPS CHECK OF AC DISTRIBUTION SYSTEM IN REFERENCE TO AMM 21-51-00 PER FIM. NO SMOKE OR ABNORMAL
- [SDR SWIA2026050676003](https://openairdocs.org/sdr/SWIA2026050676003.md): Wire Splice · damaged · May 6, 2026 · N778SK · Cndair CL6002C10 · Landing Gear System Wiring
  > ANTISKI INBOARD CAUTION, PARKING BRAKE SOV CAUTION, AND PARKING BRAKE WARNING MESSAGE ON UPWIND OUT OF DETROIT. (FLIGHT 3936)TROUBLESHOT IAW FIM 32-45-16. FOUND SPLICES TO MICROSWITCHES HAD PINS PULL OUT OF SPLICE SP62. REPLACED SPLICE SP62 AT PARKING BRAKE M
- [SDR SWIA2026050475998](https://openairdocs.org/sdr/SWIA2026050475998.md): Shutoff Valve · faulted · May 4, 2026 · N778SK · Cndair CL6002C10 · Landing Gear Brake System
  > PARKING BRAKE WARNING IN CRUISE. PERSISTED MOST OF FLIGHT. PERFORMED OPS TEST OF PARKING BRAKE IAW AMM 32-45-00. COULD NOT DUPLICATE FAULT WITH PARKING BRAKE RELEASED. INTERROGATED MDC FOUND FAULT CODE B1-007492 FLAGGING PARKING BRAKE SIGNAL DISAGREE & CODE B
- [SDR SWIA2026020975235](https://openairdocs.org/sdr/SWIA2026020975235.md): Landing Gear · warning message · Feb 9, 2026 · N778SK · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON DEPARTURE. RIGHT MLG RED. LEFT AND NOSEWHEEL UP AND LOCKED. RAN QRH. LANDING GEAR STAYED DOWN FOR REST OF THE FLIGHT. LANDING NORMALC:MEL 32-30-1CAT "A" DUE 1 FLT DAYMX ACTION COMPLIED WITH (FLIGHT 350)FEB 09, 2026 STATION: GRR--DEFERRED LA
- [SDR SWIA2026021075235](https://openairdocs.org/sdr/SWIA2026021075235.md): Landing Gear · warning message · Feb 9, 2026 · N778SK · Cndair CL6002C10 · Landing Gear Position and Warning
  > DUE TO ODI EVENT SMOD APPROVAL REQUIRED FOR RTS, CAT II DOWNGRADED. GEAR DISAGREE ON DEPARTURE. RIGHT MLG RED. LT AND NOSEWHEEL UP AND LOCKED. RAN QRH. LANDING GEAR STAYED DOWN FOR REST OF THE FLIGHT. LANDING NORMAL. MEL 32-30-1CAT A DUE 1 FLT DAY, MX ACT
- [SDR SWIA2025040700004](https://openairdocs.org/sdr/SWIA2025040700004.md): Oxygen System · warning message · Apr 4, 2025 · N778SK · Cndair CL6002C10 · Crew Oxygen System
  > CRUISING AT 370FL RECEIVED O2 LOW MSG OBSERVED O2 LEVEL 900 PSI DROPPING 10 LBS EVERY 40 SECS, LOWEST LEVEL WAS 500 PSI. ON THE GRD ITS SITTING AT 1660 PSI (FLIGHT 3676 - FILED CLOSED)PLEASE REFERENCE AML 1575104 TROUBLESHOT DISCREPANCY IN REF TO CRJ 700 FIM 3
- [SDR SWI2025F00283](https://openairdocs.org/sdr/SWI2025F00283.md): Oxygen Bottle · low pressure · Mar 5, 2025 · N778SK · Cndair CL6002C10 · Crew Oxygen System
  > OXYGEN LO PRESS CAUTION MESSAGE IN CRUISE. PRESSURE WENT AS LOW AS 600PSI. PRESSURE WENT BACK TO NORMAL AFTER LANDING. MEL 35-12-1ACAT C, SMOD RTS APPROVAL REQUIRED DUE TO ODI EVENT. OXYGEN LO PRESS CAUTION MESSAGE IN CRUISE. PRESSURE WENT AS LOW AS 600PSI.
- [SDR SWIA20241220](https://openairdocs.org/sdr/SWIA20241220.md): Bracket · chafed · Dec 20, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > NLG, BEFORE INSTALLING SERVICEABLE GEAR, FOUND CHAFE ON AFT WALL BRACKET FOR THE LOCK LINK, HN00208689 (C-CHECK RO 1/29/2025) REMOVED CHAFE AT THE NLG AFT WALL BRACKET FOR THE LOCK LINK REF CRJ 700 SRM 51-12-00-001-001-A01 FOUND TO BE OUT OF LIMITS. REC
- [SDR SWI2025F00089](https://openairdocs.org/sdr/SWI2025F00089.md): Floor Support · corroded · Nov 27, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR BEAM ON TOP SURFACE HAVE CORROSION AT LBL9 BTW FS645 TO FS677 (MX 29228065) (C-CHECK RO 1/29/2025) --REPAIRED FLOOR BEAM SECTION AT LBL 9.0 BETWEEN F/S 639.00 TO F/S 686.00 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REF REO 670-53-31-983 REV -- DAT
- [SDR SWI2025F00081](https://openairdocs.org/sdr/SWI2025F00081.md): Stringer · corroded · Nov 22, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L HAS CORROSION FROM APPROX FS280 - FS333 MX 29199537 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW STR 26L FROM FS280 TO FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV KCOMPLIED WITH SKYWES
- [SDR SWI2025F00121](https://openairdocs.org/sdr/SWI2025F00121.md): Floorbeam · corroded · Nov 21, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON LH CROSSBEAM AT FS 280.00 TRANS #29193959 (C-CHECK RO 1/29/2025) REMOVED LH CROSSBEAM AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01. INSTALLED NEW LH CROSSBEAM AT FS 28
- [SDR SWIA20250130121](https://openairdocs.org/sdr/SWIA20250130121.md): Web · corroded · Nov 21, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH WEB AT FS 280.00 HAS CORROSION TRANS #29190182 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW LH LOWER WEB AT FS280 REF CRJ 700 SRM 53-11-10-201-004-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-10002-SKY
- [SDR SWI2025F00120](https://openairdocs.org/sdr/SWI2025F00120.md): Floorbeam · cracked · Nov 20, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CRACK ON COCKPIT FLOORBEAM AT LBL12.00 FS 280.00. TRANS #29187421 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW SECTION FLOOR BEAM AT LBL 12.00, ITEM -35 INBOARD UPPER ANGLE, ITEM -37 INBOARD LOWER ANGLE, -ITEM 39 OUTBOARD WEB ANGLE AND ITEM -4
- [SDR SWI2025F00119](https://openairdocs.org/sdr/SWI2025F00119.md): Floorbeam · cracked · Nov 20, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CRACK ON COCKPIT FLOORBEAM AT RBL12.00 FS 280.00. TRANS #29187403 (C-CHECK RO 1/29/2025) REMOVED RH FLOOR SUPPORT BETWEEN FS250.00 - FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01.INSTALLED SECTION FLOOR BEAM AT RBL 12.00, ITEM -36 INBOARD UPPER A
- [SDR SWI2025F00118](https://openairdocs.org/sdr/SWI2025F00118.md): Frame · corroded · Nov 20, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS310 BETWEEN STGR25L & STGR25R IS CORRODED (C-CHECK RO 1/29/2025) INSTALLED NEW LOWER FRAME SECTOR FS310 BETWEEN STGR25L & STGR25R REF CRJ-700 SRM 53-00-06-201-006-A01. PERFORMED PRESSURE LEAK CHECK IAW CRJ700 AMM 21-31-00-910-801-A01. PRESSURE
- [SDR SWIA2025013020](https://openairdocs.org/sdr/SWIA2025013020.md): Frame · corroded · Nov 20, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS295 BETWEEN STGR25L & STGR25R IS CORRODED (C-CHECK RO 1/29/2025) INSTALLED NEW LOWER FRAME SECTOR FS295 BETWEEN STGR25L & STGR25R REF CRJ-700 SRM 53-00-06-201-006-A01. PERFORMED PRESSURE LEAK CHECK IAW CRJ700 AMM 21-31-00-910-801-A01. PRESSURE
- [SDR SWI2025F00097](https://openairdocs.org/sdr/SWI2025F00097.md): Slat Track · cracked · Nov 14, 2024 · N778SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK CANISTER 1-3 IS CRACKED (C-CHECK RO 1/29/2025) REMOVED LH WING SLAT #1 REF CRJ 700 AMM 27-81-17-000-801-A01. PERFORMED ALL STEPS OF REO 670-57-42-577 REV -- DATED 2016-12-02 TO PERFORM REPAIR OF LH SLAT TRACK CANISTER 1-3. INSTALLED LH WIN
- [SDR SWI2025F00117](https://openairdocs.org/sdr/SWI2025F00117.md): Floor Support · cracked · Nov 13, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT HAND COCKPIT FLOOR BEAM AT APPROX. RBL 12 AND JUST AFT OF FS 202.00 IS CRACKED. HN00200833 (C-CHECK RO 1/29/2025) RECEIVED AND COMPLIED WITH REO 670-53-11-2052 REV -- DATED 2024-11-15 REPAIR TO COCKPIT FLOOR BEAM RBL12 BETWEEN FS.220-FS.226. COMPL
- [SDR SWI2025F00116](https://openairdocs.org/sdr/SWI2025F00116.md): Hinge · gouged · Nov 13, 2024 · N778SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE (DOOR SIDE) HAS MULTIPLE GOUGES ON THE LUG LANDS, IN THE LUG TO LAND RADIUS AND ON THE SIDES OF THE LUGS. (C-CHECK RO 1/29/2025) BLENDED AND EVAL'D PAX DOOR PIANO HINGE LUG LANDS (DOOR SIDE), FOUND TO BE WITHIN LIMITS REF MHIRJ REO
- [SDR SWI2025F00115](https://openairdocs.org/sdr/SWI2025F00115.md): Hinge · gouged · Nov 13, 2024 · N778SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (FUSELAGE SIDE) LAST LAND LUG GOUGED FROM PROTRUDING ROLL PIN. (C-CHECK RO 1/29/2025) REMOVED, EVALUATED AND REPAIRED GOUGE AT PAX DOOR HINGE LAND LUG, WAS FOUND WITHIN LIMITS REF REO 670-53-21-582 REV-G DATE:2024-02-18. ALL STEPS OF RE
- [SDR SWI2025F00114](https://openairdocs.org/sdr/SWI2025F00114.md): Skin · damaged · Nov 13, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > RH ICE DETECTOR SKIN CUT OUT, FASTENER HOLE HAS DRILL DAMAGE, EGG SHAPED AND OVERSIZED (MARKED) (C-CHECK RO 1/29/2025) REPAIRED PER MHIRJ REO 670-53-11-2053 REV -- 2024-11-23. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYPERFORMED PRESSURE LEAK CHECK
- [SDR SWIA202501300013](https://openairdocs.org/sdr/SWIA202501300013.md): Floor Support · gouged · Nov 13, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL BETWEEN FS437.00 TO FS453.00 HAS GOUGED (MARKED) (C-CHECK RO 1/29/2025) BLENDED GOUGE AT R/H FLOOR SILL BETWEEN FS437.00 TO FS453.00 REF CRJ700 SRM 51-12-00-001-001-A01 EVALUATED BLEND AT R/H FLOOR SILL BETWEEN FS437.00 TO FS453.00, THE B
- [SDR SWI2025F00113](https://openairdocs.org/sdr/SWI2025F00113.md): Intercostal · corroded · Nov 12, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL HAS CORROSION, AFT OF FS661.00 STGR19R. (MARKED) (C-CHECK RO 1/29/2025) EVALUATED INTERCOSTAL (DIAPHRAGM) AT FS661.15+2" AND STGR19R. FOUND EXFOLIATION AND MATERIAL LOSS ON DIAPHRAGM, IS OUT OF LIMITS, MUST BE REPLACED PER CRJ700 SRM TASK 5
- [SDR SWI2025F00112](https://openairdocs.org/sdr/SWI2025F00112.md): Floorbeam · cracked · Nov 12, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACKED ANGLE ATTACHED TO OTBD SIDE OF FLOOR BEAM LBL 12 AND AFT FACE OF FS 280.00 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW ANGLE AT OTBD SIDE OF FLOOR BEAM LBL 12 AND AFT FACE OF FS 280.00 REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG CC670-34010
- [SDR SWI2025F00111](https://openairdocs.org/sdr/SWI2025F00111.md): Floorbeam · cracked · Nov 12, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACKED ANGLE ATTACHED TO OTBD SIDE OF FLOOR BEAM RBL 12 AND AFT FACE OF FS 280.00 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW ANGLE ATTACHED TO OTBD SIDE OF FLOOR BEAM RBL 12 AND AFT FACE OF FS 280.00 REF CRJ700 SRM 51-42-21-001-001-A01. AND DWG C
- [SDR SWI2025F00110](https://openairdocs.org/sdr/SWI2025F00110.md): Hinge · damaged · Nov 12, 2024 · N778SK · Cndair CL6002C10 · Engine Thrust Reverser
  > FABRICATE R/H UPPER TRANSCOWL HINGE HALF CN624-2030-207 (C-CHECK RO 1/29/2025) FABRICATED HINGE HALF REF EO CL-600-2C10-53-L08541 REV A 2024-11-23 USING 15-5PH HT1025 PO# 5-42720 DWG CN624-2030 REV C COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWI2025F00109](https://openairdocs.org/sdr/SWI2025F00109.md): Bracket · corroded · Nov 12, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET AT FS364.0 STGR27 AS MARKED (C-CHECK RO 1/29/2025) REMOVED CORROSION ON STGR27 (NOT A BRACKET) ON SKIN FLANGE (AFT END OF STGR27) REF CRJ-700 SRM 51-21-06-001-001-A01. STGR LOSS 100% OF MATERIALREMOVED AND REPLACED STR 27 FROM FS333
- [SDR SWIA20250130112](https://openairdocs.org/sdr/SWIA20250130112.md): Stringer · corroded · Nov 12, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR25R BETWEEN FS319.0 AND FS333.0 AS MARKED (C-CHECK RO 1/29/2025) INSTALLED NEW STR 25R FROM FS280 TO FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND SH670-31630 REV K. PERFORMED PRESSURE LEAK CHECK IAW CRJ700
- [SDR SWI2025F00108](https://openairdocs.org/sdr/SWI2025F00108.md): Floor Support · corroded · Nov 11, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CABIN FLOOR BEAM AT RBL9 BETWEEN FS1015.00 TO FS1051.30 HAS CORROSION AS MARKED (C-CHECK RO 1/29/2025) REMOVED CORROSION ON CABIN FLOOR BEAM AT RBL9 BETWEEN FS1015.00 TO FS1051.30 REF CRJ-700 SRM 51-21-06-001-001-A01FLOOR BEAM IS OUT OF LIMITS. NO DAM
- [SDR SWI2025F00107](https://openairdocs.org/sdr/SWI2025F00107.md): Floor Support · corroded · Nov 11, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CABIN FLOOR BEAM AT LBL27 BETWEEN FS1000.00 TO 1051.30 HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW FLOOR SECTION AT LBL27 BETWEEN FS1000.00 TO 1037.00 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND COMPLIED WITH
- [SDR SWI2025F00106](https://openairdocs.org/sdr/SWI2025F00106.md): Stiffener · loose · Nov 11, 2024 · N778SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE PULLED LOOSE (C-CHECK RO 1/29/2025) REPAIRED INNER SKIN COMMON TO ZED STIFFENER P/N CN624-2038-204 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-1687, REV. --, 2024-11-19. COMPLIED WITH MAJOR REPAIR M-337 AND SK
- [SDR SWI2025F00105](https://openairdocs.org/sdr/SWI2025F00105.md): Floor Support · corroded · Nov 11, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CABIN FLOOR BEAM AT LBL9 BETWEEN FS1015.00 TO FS1051.30 HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW FABRICATED FLOOR BEAM AND REPAIR PARTS AT LBL9 BETWEEN FS1015.00 AND FS1051.30 REF CRJ 700 SRM 53-00-41-2
- [SDR SWIA2025013001](https://openairdocs.org/sdr/SWIA2025013001.md): Stand Off · cracked · Nov 11, 2024 · N778SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 1/29/2025) INSTALLED 1 EA. NEW A-BRACKET P/N CN624-2082-201 ON INBD. SIDE OF THE L/H UPPER TRANSCOWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3, AND COMPLIED
- [SDR SWIA20250130109](https://openairdocs.org/sdr/SWIA20250130109.md): Slat Track · worn · Nov 9, 2024 · N778SK · Cndair CL6002C10 · Leading Edge Devices
  > * L/H WING LEADING EDGE SLAT TRACK 1-1 NOTED WEAR MARKS TWO PLACES. FLAGGED. MX # 29127834. (C-CHECK RO 1/29/2025) REMOVED 2EA DAMAGE AT L/H WING LEADING EDGE SLAT TRACK 1-1 REF CRJ700 SRM 51-12-00-001-001-A01 AND PERFORMED REPAIR PER REO 670-57-42-18
- [SDR SWI2025F00104](https://openairdocs.org/sdr/SWI2025F00104.md): Skin · dented · Nov 6, 2024 · N778SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH INBD FLAP, THE BOTTOM INBD SKIN HAS SEVERAL DENTS (MARKED) (C-CHECK RO 1/29/2025) RH I/B FLAP BOTTOM I/B SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-802, SHEET 1 AND 2. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED F
- [SDR SWI2025F00103](https://openairdocs.org/sdr/SWI2025F00103.md): Skin · dented · Nov 6, 2024 · N778SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH INBD FLAP, THE BOTTOM INBD SKIN HAS SEVERAL DENTS (MARKED) (C-CHECK RO 1/29/2025) L/H I/B FLAP, BOTTOM I/B SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG 57-52-01-995-802, SHEET 1 AND 2. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED
- [SDR SWIA202501300002](https://openairdocs.org/sdr/SWIA202501300002.md): Skin · dented · Nov 6, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FS1015.00- 1031.00 STRG 23LH - 24LH, 2EA DENTS ON FUSELAGE EXTERIOR SKIN (MARKED) (C-CHECK RO 1/29/2025) DENT #1- LENGTH: 3.745", WIDTH: 0.854", DEPTH: 0.003". DENT #2- LENGTH: 3.670", WIDTH: 0.795", DEPTH- 0.002". USED CALIBRATED TOOL 101030TUC CAL DUE
- [SDR SWIA202501300001](https://openairdocs.org/sdr/SWIA202501300001.md): Skin · cracked · Nov 5, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > RH TRU DOOR CUT OUT, THE LOWER AFT CORNER OF THE FUSELAGE SKIN HAS POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 1/29/2025) VERFIFIED CRACK ON RH FWD LOWER FUSELAGE SKIN UNDER TRU DOOR CUTOUT. REMOVED FWD SKIN PANEL ADG AT RIGHT SIDE REF CRJ700 SRM
- [SDR SWIA20250130104](https://openairdocs.org/sdr/SWIA20250130104.md): Skin · dented · Nov 4, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EVALUATE DENT ON EXTERNAL AIRCRAFT EXTERNAL SKIN AT FASTENER ON STGR 25R, FS 549.00 - 533.00 (C-CHECK RO 1/29/2025) PERFORMED ALL STEPS REO 670-53-31-974 REV--DATED 202412-03 FOR REPAIR. COMPLIED WITH TASK CAD 51-900-1002-SKY. THIS REO REPAIR ADRESSES 2
- [SDR SWI2025F00102](https://openairdocs.org/sdr/SWI2025F00102.md): Bracket · bent · Nov 4, 2024 · N778SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FWD TRACK ASSY BRACKET (P/N CC670-38813-1) ATTACHED TO UPPER ROLLER GUIDE IS BENT (C-CHECK RO 1/29/2025) REMOVED AND REPLACED AFT CARGO DOOR FWD TRACK ASSY BRACKET (P/N CC670-38813-1). REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 5
- [SDR SWI2025F00101](https://openairdocs.org/sdr/SWI2025F00101.md): Track · worn · Nov 4, 2024 · N778SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD TRACK ASSY LOWER ROLLER GUIDE HAS WEAR ALONG UPPER EDGE. MARKED (C-CHECK RO 1/29/2025) REMOVED AND REPLACED LOWER FWD. ROLLER GUIDE P/N CC670-38809-1SB. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAW
- [SDR SWI2025F00100](https://openairdocs.org/sdr/SWI2025F00100.md): Track · worn · Nov 4, 2024 · N778SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD TRACK ASSY UPPER ROLLER GUIDE HAS WEAR ALONG LOWER EDGE. MARKED (C-CHECK RO 1/29/2025) REMOVED AND REPLACED UPPER FWD. ROLLER GUIDE P/N CC670-38810-1SB. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAW
- [SDR SWI2025F00099](https://openairdocs.org/sdr/SWI2025F00099.md): Track · worn · Nov 4, 2024 · N778SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT TRACK ASSY LOWER ROLLER GUIDE HAS WEAR ALONG UPPER EDGE. MARKED (C-CHECK RO 1/29/2025) REMOVED AND REPLACED AFT CARGO DOOR AFT TRACK ASSY LOWER ROLLER GUIDE P/N CC670-38811-1. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-2
- [SDR SWI2025F00098](https://openairdocs.org/sdr/SWI2025F00098.md): Skin · dented · Nov 4, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EVALUATE 2EA DENTS ON EXTERNAL AIRCRAFT EXTERNAL SKIN, FS 501.00 - 517.00, STGR 25R - 26R (C-CHECK RO 1/29/2025) DRESSED BACK 2EA DENTS ON EXTERNAL AIRCRAFT SKIN AT FS501-FS517 STGR 25R-26R AND ADDRESSED PREVIOUS BLEND OUT PER REO 670-53-31-975 REV -- D
- [SDR SWI2025F0000098](https://openairdocs.org/sdr/SWI2025F0000098.md): Skin · dented · Nov 4, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EVALUATE 2EA DENTS ON EXTERNAL AIRCRAFT EXTERNAL SKIN, FS 501.00 - 517.00, STGR 25R - 26R (C-CHECK RO 1/29/2025) DRESSED BACK 2EA DENTS ON EXTERNAL AIRCRAFT SKIN AT FS501-FS517 STGR 25R-26R AND ADDRESSED PREVIOUS BLEND OUT PER REO 670-53-31-975 REV -- D
- [SDR SWIA20250130102](https://openairdocs.org/sdr/SWIA20250130102.md): Skin · dented · Nov 2, 2024 · N778SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > RHS OF FWD. FUSELAGE AT APPROXIMATELY FS202, ABOVE WL79.50, (ABOVE RVSM RED CORNER MARKING), THE SKIN APPEARS TO BE DENTED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK R
- [SDR SWIA2023062200019](https://openairdocs.org/sdr/SWIA2023062200019.md): Windshield · cracked · Jun 19, 2023 · N778SK · Cndair CL6002C10 · Flight Compartment Windows
  > TRANSFER FROM EAML 1159516: L WSHLD HEAT CAUTION MESSAGE IN FLIGHT. QRH COMPLETED AND MESSAGE CLEARED. L WSHLD HEAT CAUTION MESSAGE REAPPEARED. (FLT 3292 FILED CLOSED)REMOVED AND REPLACED LEFT WINDSHIELD IAW AMM 30-42-09 AND TASK CARD 56-220-1000-SKY
- [SDR SWIA202301167115](https://openairdocs.org/sdr/SWIA202301167115.md): Windshield · cracked · Jan 13, 2023 · N778SK · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT WINDSHIELD OUTER LAYER CRACKED. REMOVED AND REPLACED RH WINDSHIELD IAW AMM 56-11-01. PERFORMED PRESSURIZE AND DEPRESSURIZE OF THE AIRCRAFT FOR MAINTENANCE IAW AMM 21-31-00. NO LEAKS FOUND, AIRCRAFT OK TO RETURN TO SERVICE.

Next page: https://openairdocs.org/aircraft/N778SK/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 = 'N778SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N778SK/reports

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