# Service difficulty reports: N767SK

A list on [N767SK](https://openairdocs.org/aircraft/N767SK.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 · 109 reports

- [SDR SWIA2025033100115](https://openairdocs.org/sdr/SWIA2025033100115.md): Floorbeam · corroded · Jan 15, 2025 · N767SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT- FLOOR BEAM AT LBL 27 FROM F.S.1000 TO 1031, THERE IS SIGNS OF CORROSION. (C-CHECK RO 03/29/2024)REMOVED AND REPLACED NEW SECTION FLOOR BEAM ON AFT CARGO COMPARTMENT AT LBL27 FROM FS1000 TO FS1031 IAW CRJ700 SRM 53-00-41, 53-61-43, AMM 20
- [SDR SWIA2025033100114](https://openairdocs.org/sdr/SWIA2025033100114.md): Rib · cracked · Jan 14, 2025 · N767SK · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > L/H FIXED LEADING EDGE RIB AT W.S.58.41 CRACKED (C-CHECK RO 03/29/2024)REPAIRED DAMAGED RIB ON LH WING LEADING EDGE AT WS58.41 IAW REO 670-57-41-611 REV-P1 DATE 2025-03-06 AND REV-- DATE 2025-03-20 AND CRJ700 SRM 57-00-01.
- [SDR SWIA2025033100108](https://openairdocs.org/sdr/SWIA2025033100108.md): Drag Angle · cracked · Jan 8, 2025 · N767SK · Cndair CL6002C10 · Vertical Stabilizer
  > AFT DRAG ANGLE CRACKED ON RH SIDE OF VERTICAL STABLIZER (C-CHECK RO 03/29/2024)REPAIRED DAMAGED AFT DRAG ANGLE ON RH SIDE OF VERTICAL STABILIZER IAW CRJ700 SRM 51-25-16 AND REO 670-55-31-018 REV-A DATE 2016-11-10, REO 670-55-31-180 REV-- DATE 2024-08-29. NDT P
- [SDR SWIA2024072900008](https://openairdocs.org/sdr/SWIA2024072900008.md): Sensor · failed · Jul 28, 2024 · N767SK · Cndair CL6002C10 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE ON CLIMB OUT, ALL GEAR STAYED DOWN AND LOCKED WHILE GEAR LEVER WAS IN UP POSITION. RAN THROUGH QRH, AND RETURNED TO FIELD. (FLIGHT 4290 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28601999 WITH THE FOLLOWING CORRE
- [SDR SWIA202266427](https://openairdocs.org/sdr/SWIA202266427.md): None · failed · Sep 5, 2022 · N767SK · Cndair CL6002C10 · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF WHEN LANDING GEAR LEVER WAS SELECTED UP. MESSAGE CLEARED AFTER DOING QRH. (FLIGHT #4967 FILED CLOSED) PLEASE REFERENCE AML 986814 FOR TROUBLESHOOTING OF GEAR DISAGREE WARNING MESSAGE. / PERFORMED OPERATIONAL CHE
- [SDR SWIA202163083](https://openairdocs.org/sdr/SWIA202163083.md): None · none · Oct 31, 2021 · N767SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > NEW RH FLOOR SILL PILOT HOLE MISDRILLED, BACK DRILL NEW FLOOR SILL FOR FS 310.00-319.00 (C-CHECK RO 12/07/2021) ORDERED & RECEIVED NEW R/H FLOOR SILL, SILL INSTALLED ON JOB 710233104 OP39 CO 23615286
- [SDR SWIA202163082](https://openairdocs.org/sdr/SWIA202163082.md): None · cracked · Oct 30, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Frame
  > ATTACH ANGLE ON R/H FS 280 CROSS BEAM TO RBL 12 INTERCOSTAL CRACKED (C-CHECK RO 12/07/2021) INSTALLED ATTACH ANGLE ON FS280 CROSS BEAM RBL 12 REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. CC670-34010 REV. K. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202163081](https://openairdocs.org/sdr/SWIA202163081.md): None · corroded · Oct 27, 2021 · N767SK · Cndair CL6002C10 · Doors
  > PAX DOOR LOWER SILL AFT CAP ANGLE CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 12/07/2021) REPLACED AND INSTALLED NEW AFT CAP ANGLE P/N SH670-31821-6 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV. -Y. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202163080](https://openairdocs.org/sdr/SWIA202163080.md): None · cracked · Oct 27, 2021 · N767SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT LBL 12 AT FS 274.00 IS CRACKED. (C-CHECK RO 12/07/2021) REPAIRED COCKPIT FLOOR BEAM AT LBL 12.00 FS 274.00 REF CRJ700 SRM 51-43-11-201-003-A01 COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM MM-337, SEE CONTINUE CARD FOR MORE DETAILS
- [SDR SWIA202163079](https://openairdocs.org/sdr/SWIA202163079.md): None · cracked · Oct 27, 2021 · N767SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT RBL 12 AT FS 274.00 IS CRACKED (C-CHECK RO 12/07/2021) REPAIRED COCKPIT FLOOR BEAM AT RBL 12.00 FS 274.00 REF CRJ700 SRM 53-11-43-201-003-A01 COMPLIED WITH TASK CARD 51-900-1002-SKY AND FORM MM-337, SEE CONTINUE CARD FOR MORE DETAILS
- [SDR SWIA202163078](https://openairdocs.org/sdr/SWIA202163078.md): None · corroded · Oct 22, 2021 · N767SK · Cndair CL6002C10 · Doors
  > PAX DOOR LOWER SILL CLOSING FITTING AT FS 314.00 IS CORRODED. (C-CHECK RO 12/07/2021) REMOVED AND REPLACED NEW PAX DOOR LOWER SILL CLOSING FITTING AT FS 314.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV Y. COMPLIED WIT TASK CARD 51-900-
- [SDR SWIA202163077](https://openairdocs.org/sdr/SWIA202163077.md): None · corroded · Oct 22, 2021 · N767SK · Cndair CL6002C10 · Doors
  > PAX DOOR LOWER SILL KICKPLATE ANGLE IS CORRODED IN MULTIPLE SPOTS. (C-CHECK RO 12/07/2021) REPLACED AND INSTALLED NEW PAX DOOR LOWER SILL KICKPLATE ANGLE P/N SH670-31875-7S REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV. -Y. COMPLIED WITH 5
- [SDR SWIA202163076](https://openairdocs.org/sdr/SWIA202163076.md): None · corroded · Oct 21, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Frame
  > L/H CROSS BEAM AT FS 280 LBL 9 HAS CORROSION (C-CHECK RO 12/07/2021) REMOVED AND REPLACED NEW LH CROSSBEAM AT FS 280.00 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 CRJ 700 SRM 51-42-22-001-001-A01 AND DWG CC670-34010 REV K. CO
- [SDR SWIA202163075](https://openairdocs.org/sdr/SWIA202163075.md): None · corroded · Oct 18, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON INTERCOSTAL @ STA 394-409 @ STR 26R (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE INTERCOSTAL AT STGR 26R AT FS394.00-FS409.00. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01,AND DWG SH670-32050 REV
- [SDR SWIA202163074](https://openairdocs.org/sdr/SWIA202163074.md): None · corroded · Oct 18, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON INTERCOSTAL @ FS 394-409 @ STR 26L (C-CHECK RO 12/07/2021) REMOVED AND REPLACED INTERCOSTAL @FS 394-409 @STR26L. IAW CRJ700 SRM 51-42-06-001-001-A01, AND CRJ 700 SRM 51-42-21-001-001-A01, AND DWG #SH670-32050 REVJ / COMPLIED WITH SKYW
- [SDR SWIA202163073](https://openairdocs.org/sdr/SWIA202163073.md): None · corroded · Oct 16, 2021 · N767SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > RIGHT WING SLAT TRACK 3-3 HAS EVIDENCE OF POSSIBLE CORROSION ON UPPER AND LOWER SIDE OF TRACK AND ERROSION OF PROTECTIVE COATING (C-CHECK RO 12/07/2021) REPAIRED THE RH WING SLAT TRACK 3-3 AS PER REO 670-57-42-1261 REV --DATE 2021-11-08, ALL STEPS COMPL
- [SDR SWIA202163072](https://openairdocs.org/sdr/SWIA202163072.md): None · corroded · Oct 16, 2021 · N767SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > RIGHT WING SLAT TRACK 1-1 HAS EVIDENCE OF POSSIBLE CORROSION ON UPPER SIDE OF TRACK AND ERROSION OF PROTECTIVE COATING (C-CHECK RO 12/07/2021) BLENDED CORROSION ON THE RH SLAT TRACK 1-1 "WITHIN LIMITS" REF MHIRJ REO 670-57-42-1263 REV -- 2021-11-15, ALL
- [SDR SWIA202163071](https://openairdocs.org/sdr/SWIA202163071.md): None · corroded · Oct 16, 2021 · N767SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > LEFT WING SLAT TRACK 3-1 HAS EVIDENCE OF CORROSION ON TOP AND BTM SIDE AND ERROSION OF PROTECTIVE COATING (C-CHECK RO 12/07/2021) BLENDED CORROSION ON THE LH SLAT TRACK 3-1 "WITHIN LIMITS" REF MHIRJ REO 670-57-42-1264 REV -- 2021-11-10, ALL STEPS COMPLI
- [SDR SWIA202163070](https://openairdocs.org/sdr/SWIA202163070.md): None · corroded · Oct 15, 2021 · N767SK · Cndair CL6002C10 · Doors
  > *PASSENGER DOOR €“ DD7A HAS CORROSION BETWEEN FS315.00 & FS320.00. (MARKED) (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL AT DD7A. REF DWG 601R31702 REV-N AND CRJ 700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020. COM
- [SDR SWIA202163069](https://openairdocs.org/sdr/SWIA202163069.md): None · gouged · Oct 15, 2021 · N767SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > *PASSENGER DOOR €“ HINGE ON THE FUSELAGE LAND #27 SIDE IS GOUGED. (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR HINGE. REF CRJ700 SRM 53-21-23-201-007-A01 REV.38 JUL 25/2020 AND DWG SH670-31810 REV-Y. COMPLIED WITH FORM M-337
- [SDR SWIA202163068](https://openairdocs.org/sdr/SWIA202163068.md): None · chafed · Oct 15, 2021 · N767SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > *PASSENGER DOOR €“ HINGE ON THE DOOR SIDE LUGS 2 €“ 27 HAVE CHAFING DAMAGE. (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR HALF HINGE. REF CRJ700 SRM 52-11-01-201-002-A01 REV 38 JUL 25/2020, CRJ700 SRM 51-42-06-001-001-A01 REV
- [SDR SWIA202163067](https://openairdocs.org/sdr/SWIA202163067.md): None · corroded · Oct 14, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Keel
  > *CORROSION FOUND ON STR24L FROM FS517.00-FS535.00. (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE STR24L FROM FS517.00-FS535.00. REF DWG SH670-33200 REV G. AND CRJ 700 SRM 51-42-06-001-001-A01 REV 38 DATED JUL 25 2020. COMPLIED WITH FORM
- [SDR SWIA202163066](https://openairdocs.org/sdr/SWIA202163066.md): None · corroded · Oct 13, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Frame
  > * CORROSION FOUND ON FS517.00 FRAME LOWER SECTOR FROM APPROX. STR26L-STR22L (C-CHECK RO 12/07/2021) REMOVED, FABRICATED NEW & REPLACED THE FS 517. LH LOWER FRAME SECTOR REF. CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH6
- [SDR SWIA202163065](https://openairdocs.org/sdr/SWIA202163065.md): None · corroded · Oct 13, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Frame
  > * CORROSION FOUND ON SUB FRAME AT FS517.00 BETWEEN STR27-STR26L. (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE SUB FRAME AT FS517.00 BETWEEN STGR 27L-26L. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-33200 REV G. COMPLIED WITH FORM
- [SDR SWIA202163064](https://openairdocs.org/sdr/SWIA202163064.md): None · worn · Oct 11, 2021 · N767SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > LH SLAT TRACK 3-3 HAS VISIBLE WEAR MARKS (C-CHECK RO 12/07/2021) REPAIRED THE LH SLAT TRACK 3-3 AS PER REO 670-57-42-1262 REV -- DATED 2021-11-08. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202163063](https://openairdocs.org/sdr/SWIA202163063.md): None · worn · Oct 10, 2021 · N767SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > * L/H SIDE SLAT TRACK 1-1 HAS WEAR MARKS ON DRIVEN TRACKS. (C-CHECK RO 12/07/2021) REPAIRED THE L/H SIDE SLAT TRACK 1-1 HAS WEAR MARKS ON DRIVEN TRACK AS PERREO 670-57-42-1276 REV. -- DATED, 2021-11-15 ALL STEPS COMPLIED WITH & CRJ 700 SRM 51-12-00-001-
- [SDR SWIA202163062](https://openairdocs.org/sdr/SWIA202163062.md): None · corroded · Oct 10, 2021 · N767SK · Cndair CL6002C10 · Galley Doors
  > *SVC DOOR LOWER SEAL STRIKER HAS MULTIPLE SPOTS OF CORROSION AROUND THE FASTENER HOLES (MARKED) (C-CHECK RO 12/07/2021) REMOVED SERVICE DOOR LOWER SEAL STRIKER P/N SH670-31412-5 REF CRJ700 SRM 51-42-06-001-001-A01. / AND INSTALLED NEW SERVICE DOOR LOWE
- [SDR SWIA202163061](https://openairdocs.org/sdr/SWIA202163061.md): None · corroded · Oct 10, 2021 · N767SK · Cndair CL6002C10 · Galley Doors
  > *SVC DOOR LOWER KICKPLATE MOUNTING ANGLE HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICE DOOR LOWER KICKPLATE MOUNTING ANGLE REF CRJ700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DWG N
- [SDR SWIA202163060](https://openairdocs.org/sdr/SWIA202163060.md): None · corroded · Oct 10, 2021 · N767SK · Cndair CL6002C10 · Galley Doors
  > *SVC DOOR KICKPLATE ANGLE HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICE DOOR KICKPLATE LOWER SILL ANGLE P/N SH670-31986-1 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DWG NO
- [SDR SWIA202163059](https://openairdocs.org/sdr/SWIA202163059.md): None · corroded · Oct 8, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON AVIONICS SURROUND STUCTURAL SUPPORT INTERCOSTAL JUST LEFT OF STR 27 BTW F/S 394-409 (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE INTERCOSTAL JUST LEFT OF STGR27 AT FS394.00-FS409.00. CRJ700 SRM 51-42-21-001-001-A01,
- [SDR SWIA202163058](https://openairdocs.org/sdr/SWIA202163058.md): None · corroded · Oct 8, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON AVIONICS SURROUND STUCTURAL SUPPORT INTERCOSTAL JUST RIGHT OF STR 27 BTW F/S 349-364 (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE INTERCOSTAL JUST RIGHT OF STGR27 AT FS349.00-FS364.00. CRJ700 SRM 51-42-21-001-001-A01,
- [SDR SWIA202163057](https://openairdocs.org/sdr/SWIA202163057.md): None · corroded · Oct 8, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CROSS BEAM AT STA. 280 LBL9 - RBL9 CORRODED FLIGHT DECK SIDE (C-CHECK RO 12/07/2021) REMOVED AND REPLACED NEW RH CROSSBEAM AT FS 280.00 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 CRJ 700 SRM 51-42-22-001-001-A01 AND DWG CC67
- [SDR SWIA202163056](https://openairdocs.org/sdr/SWIA202163056.md): None · corroded · Oct 8, 2021 · N767SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > R/H FLOOR SILL BTW F/S 310-319.7 HAS MULTIPLE AREAS WITH EVIDENCE OF CORROSION (C-CHECK RO 12/07/2021) REMOVED AND INSTALLED NEW FLOOR SILL FROM FS 280.00 TO FS 319.00 REF. BOMBARDIER DWG NO. SH670-30002 REV A, BOMBARDIER DWG NO. SH670-32170 REV M,CRJ 7
- [SDR SWIA202163055](https://openairdocs.org/sdr/SWIA202163055.md): None · corroded · Oct 7, 2021 · N767SK · Cndair CL6002C10 · Doors
  > *AFT BAGGAGE BAY DOOR LOWER SILL (APPROX. FS.1000-FS.1047) HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 12/07/2021) REMOVED AND REPLACED NEW AFT CARGO DOOR LOWER SILL REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01 AND CRJ700 SRM 51
- [SDR SWIA202163054](https://openairdocs.org/sdr/SWIA202163054.md): None · corroded · Oct 7, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Frame
  > *FS.280 CROSSBEAM FLOOR PANEL SUPPORT ANGLE IS CORRODED (C-CHECK RO 12/07/2021) REMOVED AND REPLACED NEW FLOOR PANEL SUPPORT ANGLE AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. DWG CC670-34010 REV K. COMPLIED WITH
- [SDR SWIA202163053](https://openairdocs.org/sdr/SWIA202163053.md): None · corroded · Oct 5, 2021 · N767SK · Cndair CL6002C10 · Doors
  > PAX DOOR LOWER SILL FWD CAP ANGLE CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 12/07/2021) REPLACED AND INSTALLED NEW FWD CAP ANGLE P/N SH670-31821-5 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV. -Y. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202163052](https://openairdocs.org/sdr/SWIA202163052.md): None · corroded · Oct 5, 2021 · N767SK · Cndair CL6002C10 · Doors
  > PAX DOOR LOWER SILL MID CAP ANGLE CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 12/07/2021) REPLACED WITH NEW PAX DOOR LOWER SILL MID CAP ANGLE P/N SH670-31825-9S.REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV -Y. / C/W TASK CARD 51-900
- [SDR SWIA202163051](https://openairdocs.org/sdr/SWIA202163051.md): None · gouged · Oct 5, 2021 · N767SK · Cndair CL6002C10 · Doors
  > * PAX DOOR SEAL STRIKER AT LOWER SILL GOUGED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 12/07/2021) REMOVED AND REPLACED PAX DOOR LOWER SILL SEAL STRIKER WITH NEW P/N SH670-31886-3S REF. CRJ700 SRM 51-42-21-001-001-A01. AND DWG SH670-31810 REV. -Y. COMPLI
- [SDR SWIA202163050](https://openairdocs.org/sdr/SWIA202163050.md): None · corroded · Oct 5, 2021 · N767SK · Cndair CL6002C10 · Fuselage Main, Frame
  > * PANEL 642AZ FWD IB PANEL LANDING CORRODED IN MULTIPLE SPOTS (FLAGGED). (C-CHECK RO 12/07/2021) REPLACED RH FWD ANGLE P/N CC670-10338-2 COMMON TO PANEL 642AZ PANEL. REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG CC670-10320 REV F. COMPLIED WITH TASK CARD
- [SDR SWIA202163084](https://openairdocs.org/sdr/SWIA202163084.md): None · cracked · Sep 24, 2021 · N767SK · Cndair CL6002C10 · Window/Windshield System
  > D: REF AC MX LOG # 561123. CAPTAIN SIDE FRONT WINDSHIELD DISCOLORED ALONG THE TOP SIDE, LEFT SIDE AND BOTTOM RIGHT FROM THE COCKPIT VIEW. ALONG THE TOP LEFT EDGE THERE APPEARS TO BE SMALL CRACKS IN THE GLASS BETWEEN THE PANES. / UPON INSPECTION OF CA SIDE WIN
- [SDR SWIA202163049](https://openairdocs.org/sdr/SWIA202163049.md): None · dented · Sep 24, 2021 · N767SK · Cndair CL6002C10 · Fuselage Structure (General)
  > ADM 7321 - L/H FWD FUSELAGE 1.3" AFT OF FS235 AND 1" ABOVE STRINGER 21L HAS DENT WITH GOUGE DAMAGE. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 12/07/2021) PERFOR
- [SDR SWIA202163048](https://openairdocs.org/sdr/SWIA202163048.md): None · dented · Sep 24, 2021 · N767SK · Cndair CL6002C10 · Ailerons
  > ADM 5026 - CENTER OF LT INBOARD FLAP BETWEEN HINGE ARMS DENTED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RO 12/07/2021) CUTOUT & REMOVED DAMAGED L/H INBD FLAP SKI
- [SDR SWIA202163086](https://openairdocs.org/sdr/SWIA202163086.md): None · worn · Aug 13, 2021 · N767SK · Cndair CL6002C10 · Wing, Longeron/Stringer
  > REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR PER AMM (C-CHECK RO 12/07/2021) REMOVED OLD BUSHING AND REPLACED WITH NEW BUSHING AND HARDWARE ON R/H AILERON WING AFT SPAR, IAW CRJ 700 AMM 20-31-00-400-805-A01
- [SDR SWIA202163085](https://openairdocs.org/sdr/SWIA202163085.md): None · worn · Aug 13, 2021 · N767SK · Cndair CL6002C10 · Wing, Longeron/Stringer
  > REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR PER AMM (C-CHECK RO 12/07/2021) REMOVED OLD BUSHINGS AND INSTALLED NEW BUSHINGS IN L/H AILERON WING AFT SPR MOUNTS IAW CRJ 700 AMM 20-31-00-400-801-A01
- [SDR SWIA202053348](https://openairdocs.org/sdr/SWIA202053348.md): Hydraulic System · overheated · Oct 19, 2020 · N767SK · Cndair CL6002C10 · Hydraulic System, Main
  > HYD 2 HI TEMP CAUTION MESSAGE SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH PROCEDURE AND RETURNED TO FIELD. TEMP REACHED A MAXIMUM OF 98 DEGREES C. IT COOLED DOWN A BIT AFTER QRH PROCEDURE, THEN BEGAN TO INCREASE AGAIN ON APPROACH TO LANDING, REACHING 93 DEGREE
- [SDR SWIA2019091346313](https://openairdocs.org/sdr/SWIA2019091346313.md): Intercostal · corroded · Sep 1, 2019 · N767SK · Cndair CL6002C10 · Passenger/Crew Doors
  > THE PASSENGER DOOR INNER SKIN AND PULLEY ASSIST BRACKET ARE PULLING AWAY FROM THE PASSENGER DOOR AFT FORMER AT DOOR DATUM 4 AND FOUND PASSENGER DOOR INTERCOSTALS DD2 AND DD6 CORRODED. (C-CHECK) RO: 09/12/2019 REPAIRED PASSENGER DOOR INNER SKIN, PULLEY ASSIST B
- [SDR SWIA2019091346312](https://openairdocs.org/sdr/SWIA2019091346312.md): Attach Angle · cracked · Aug 17, 2019 · N767SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND RT FWD & AFT UPLOCK ATTACHMENT ANGLES CRACKED. (C-CHECK) RO: 09/12/2019 REMOVED AND REPLACED ANGLES IAW SRM.
- [SDR SWIA2019091346311](https://openairdocs.org/sdr/SWIA2019091346311.md): Post · damaged · Aug 11, 2019 · N767SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AT FS847.00 RBL9 POST, LBL9 POST AND LBL27 POST WERE GOUGED AND DAMAGED UPON REMOVAL OF AFT SILL ANGLE AND PRESSURE BOXES. (C-CHECK) RO: 09/12/2019 REPAIRED POSTS AT FS847.00 RBL9, LBL9 AND LBL 27 IAW REO.
- [SDR SWIA2019091346310](https://openairdocs.org/sdr/SWIA2019091346310.md): Post · gouged · Aug 11, 2019 · N767SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AT FS847.00 AFT LBL18.0 POST FOUND DAMAGE GOUGES IN POST. (C-CHECK) RO: 09/12/2019 REPAIRED POST AT FS847.00 LBL 18 IAW REO.
- [SDR SWIA2019091346309](https://openairdocs.org/sdr/SWIA2019091346309.md): Post · damaged · Aug 11, 2019 · N767SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON CLEANING OF FWD POST AT FS 693.00 FOR NDT, FOUND POST LBL18, RBL18 AND BL0 POST DAMAGED AND GOUGED IN RADIUS UPON REMOVAL. (C-CHECK) RO: 09/12/2019 REPAIRED POSTS FS 693.00 LBL18, RBL18 AND BL0 IAW REO.

Next page: https://openairdocs.org/aircraft/N767SK/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 = 'N767SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N767SK/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.