# Service difficulty reports: N797SK

A list on [N797SK](https://openairdocs.org/aircraft/N797SK.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 · 118 reports

- [SDR SWIA2026083177025](https://openairdocs.org/sdr/SWIA2026083177025.md): Striker · corroded · Aug 31, 2026 · N797SK · Cndair CL6002C11 · Service Doors
  > GALLEY SERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AROUND MULTIPLE OUTBOARD FASTENER HOLES. REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER STRIKER IAW DWG SH670-31950, DWG SH670-31412, AND REO 670-53-21-2965 REV-- COMPLIED WITH MIP TASKCARD 51-900-1002-SKY
- [SDR SWIA2026083177024](https://openairdocs.org/sdr/SWIA2026083177024.md): Angle · corroded · Aug 31, 2026 · N797SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > AFTER REMOVING SELF LEVELING GREEN FRON GALLEY SERVICE DOOR SURROUND FOUND CORROSION ON INBOARD ANGLE BETWEEN BS 31970- BS 33300 ON STRINGER 17R. REMOVED AND REPLACED GALLEY SERVICE DOOR SURROUND INBOARD ANGLE BETWEEN BS 31970- 33300, STRINGER 17R REF DWG S
- [SDR SWIA2026050476106](https://openairdocs.org/sdr/SWIA2026050476106.md): Skin · damaged · May 4, 2026 · N797SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED B
- [SDR SWIA2026050476105](https://openairdocs.org/sdr/SWIA2026050476105.md): Skin · damaged · May 4, 2026 · N797SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATE
- [SDR SWIA2026050476104](https://openairdocs.org/sdr/SWIA2026050476104.md): Skin · damaged · May 4, 2026 · N797SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE
- [SDR SWIA2026050476103](https://openairdocs.org/sdr/SWIA2026050476103.md): Skin · damaged · May 4, 2026 · N797SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE
- [SDR SWIA2026050476102](https://openairdocs.org/sdr/SWIA2026050476102.md): Skin · damaged · May 4, 2026 · N797SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847.00 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN
- [SDR SWIA2026031275620](https://openairdocs.org/sdr/SWIA2026031275620.md): Wire · arced · Mar 12, 2026 · N797SK · Cndair CL6002C10 · Electrical Power System Wiring
  > LEFT PYLON SUPPORT HAS BURN DAMAGE FROM ARCING IDG WIRE. IAW SRM 54-51-06, ITEM 59. REF CP 31870931 FOR IDG WIRE. COMPLIED WITH PERMANENT REPAIR ON LT PYLON SUPPORT AT FS 1088.200 AND PBL69.300 IN REFERENCE TO REO 670-54-51-090, REV -, AND STRUCTURAL MAJOR RE
- [SDR SWIA20251223017](https://openairdocs.org/sdr/SWIA20251223017.md): Engine · failed · Dec 17, 2025 · N797SK · Cndair CL6002C10 · Engine Oil Quantity
  > RIGHT ENGINE OIL PRESSURE WARNING MESSAGE IN FLIGHT. LEAD TO LOSS OF ENGINE INFLIGHT HAD TO RETURN TO TUS SINGLE ENGINE LANDING. (FLIGHT 6088) REPLACED RT ENGINE WITH SERVICABLE ENGINE IAW AMM 71-00-00-400-801-A02. OPS CHECKED GOOD. LEAK CHECKED GOOD. COMPL
- [SDR SWIA2025121800017](https://openairdocs.org/sdr/SWIA2025121800017.md): Warning Message · illuminated · Dec 17, 2025 · N797SK · Cndair CL6002C10 · Engine Oil Pressure
  > RIGHT ENGINE OIL PRESSURE WARNING MESSAGE IN FLIGHT. LEAD TO LOSS OF ENGINE INFLIGHT HAD TO RETURN TO TUS SINGLE ENGINE LANDING. (FLIGHT 6088) OPEN.
- [SDR SWIA2025121900120](https://openairdocs.org/sdr/SWIA2025121900120.md): Frame · corroded · Nov 20, 2025 · N797SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT BS 863 IS CORRODED BETWEEN S26L AND S26R. REMOVED DAMAGED SECTION OF FRAME AND PERFORMED CUTTING TRIMMING OF EDGES IAW SRM 51-42-06-001-001-A01, AND SRM 51-24-36-001-001-A01. PERFORMED REPAIRS IAW REO 670-53-51-368, REV -. ALL STEPS OF REO COMPLIED W
- [SDR SWI2025F01832](https://openairdocs.org/sdr/SWI2025F01832.md): Frame · damaged · Nov 3, 2025 · N797SK · Cndair CL6002C10 · Fuselage Main, Frame
  > SIDE FRAME AT LT BS 847, HAS 4 ELONGATED HOLES WHERE SITS AFT SEALING ANGLE AND SILL BEAM. PERFORMED REPAIR FOR ELONGATED HOLES AT LT SIDE BS 847 IAW ALL STEPS OF REO 670-53-41-770 REV-B. COMPLIED WITH TASK CARD 51-900-1002-SKY. PRESSURE CHECK GOOD.
- [SDR SWIA2025121900103](https://openairdocs.org/sdr/SWIA2025121900103.md): Beam · mismatched · Nov 3, 2025 · N797SK · Cndair CL6002C10 · Fuselage Main, Structure
  > MISDRILLED LT SILL BEAM AND INBD BEAM FITTING AT 2 EA. HOLE LOCATIONS COMMON TO REAR SPAR AT LBL 36. PERFORMED REPAIR FOR MISDRILLED HOLES TO PRESSURE FLOOR STRUCTURE AT BS 797 & LBL 36 IAW SRM 51-42-21-001-001-A01,AND ALL STEPS OF REO 670-53-41-771 REV--. CO
- [SDR SWIA2025081800015](https://openairdocs.org/sdr/SWIA2025081800015.md): Warning Message · illuminated · Aug 15, 2025 · N797SK · Cndair CL6002C10 · Overheat Detection
  > D:AFTER TAKE OFF RECEIVED GEAR OVHT FOLLOWED BY BRAKE OVHT. BOTH EXTINGUISHED AND RE ILLUMINATED. (BELIEVE TO BE ERRONEOUS BECAUSE OF HISTORY AND AFTER RUNNING QRH BTMS OFFENDING #4 ONLY SHOWED TEMP OF 1). RETURN TO DENVER EXTENDING GEAR BRAKE OVHT WARNING TR
- [SDR SWI2025F00714](https://openairdocs.org/sdr/SWI2025F00714.md): Control Unit · faulted · Jun 6, 2025 · N797SK · Cndair CL6002C10 · Stabilizer Position Indicating
  > UNCOMMANDED ND TRIM (FLIGHT 4650 - FILED CLOSED)ARRIVED AT AIRCRAFT AND FOUND PITCH TRIM INDICATION AT ND 3.4. INTERROGATED MDC AND FOUND NO PRESENT NOR HISTORIC FAULTS RELATED TO PITCH TRIM. TOOK PITCH TRIM THROUGH FULL TRAVEL ON BOTH CA AND FO SIDE. VISUALL
- [SDR SWIA2025051914](https://openairdocs.org/sdr/SWIA2025051914.md): Pressure Blkhd · cracked · May 14, 2025 · N797SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > DURING THE REMOVAL OF J616 FOUND CRACK IN THE RH WHEEL BAY ON THE PRESSURE BULKHEAD PANEL WHERE THE PLUG AND JACK CONNECT TOGETHER. (FILED CLOSED)REMOVED AND REPLACED THE PRESSURE BULKHEAD PANEL AT J616 IN THE RH WHEEL BAY ON THE PRESSURE BULKHEAD WITH A SER
- [SDR SWIA20250515001](https://openairdocs.org/sdr/SWIA20250515001.md): Pressure Blkhd · cracked · May 14, 2025 · N797SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > DURING THE REMOVAL OF J616 FOUND CRACK IN THE RH WHEEL BAY ON THE PRESSURE BULKHEAD PANEL WHERE THE PLUG AND JACK CONNECT TOGETHER. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20230601529](https://openairdocs.org/sdr/SWIA20230601529.md): Brake · warning message · May 29, 2023 · N797SK · Cndair CL6002C10 · Landing Gear Brake System
  > D: BRAKE OVHT ON CLIMB OUT. CAME ON TWICE, RAN QRH MESSAGE CLEARED THEN DECIDED TO RETURN TO DEN.C: MEL 32-46-1CCAT C DUE 06/08/2023**** DUE TO ODI EVENT****MANAGEMENT APPROVAL IS REQUIRED VIA MXC SUPERVISOR PRIOR TO RETURN TO SERVICE AFTER CLEARING THIS DEFER
- [SDR SWIA2023053029](https://openairdocs.org/sdr/SWIA2023053029.md): Unknown · warning message · May 29, 2023 · N797SK · Cndair CL6002C10 · Landing Gear System
  > D: BRAKE OVHT ON CLIMB OUT. CAME ON TWICE, RAN QRH MESSAGE CLEARED THEN DECIDED TO RETURN TO DEN.C: MEL 32-46-1CCAT C DUE 06/08/2023**** DUE TO ODI EVENT****MANAGEMENT APPROVAL IS REQUIRED VIA MXC SUPERVISOR PRIOR TO RETURN TO SERVICE AFTER CLEARING THIS DEFER
- [SDR SWIA20230328001](https://openairdocs.org/sdr/SWIA20230328001.md): Unknown · cracked · Mar 27, 2023 · N797SK · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT WINDSHIELD SHATTERED. RETURNED TO FIELD. (FLIGHT 4732 FILED CLOSED) PLEASE REFERENCE AML 1111103 PLEASE REFERENCE AML 1111104. REMOVED AND REPLACED RH WINDSHIELD PER CRJ-700 AMM 56-11-01. OPS CHECK GOOD. TASK CARD 56-220-1000-SKY COMPLETED.TORQUE WRE
- [SDR SWIA202162954](https://openairdocs.org/sdr/SWIA202162954.md): None · corroded · Nov 6, 2021 · N797SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > THE R/H WINDSCREEN HAS A CORRODED DOUBLER BEHIND THE INBD FLOOR MOUNT FITTING. (C-CHECK RO 11-27-21) REPLACED R/H WINDSCREENS INBD FLOOR MOUNT FITTING DOUBLER WITH A SERVICEABLE DOUBLER (P/N=9395015-1) REFERENCING CRJ 700 SRM 51-41-02-001-001-A01. / TORQ
- [SDR SWIA202162923](https://openairdocs.org/sdr/SWIA202162923.md): None · elongated · Oct 26, 2021 · N797SK · Cndair CL6002C10 · Rudder Tab Control System
  > PRIOR TO INSTALLING THE CO-PILOTS FWD RUDDER PEDAL PIVOT ASSY. FOUND ELONGATED HOLE ON RUDDER PEDAL PIVOT ASSY. MOUNTING PLATE AND OTBD LOWER CHANNEL AT BL26.00 (C-CHECK RO 11-27-21) REPLACED WITH NEW CO-PILOT FWD RUDDER PEDAL PIVOT ASS'Y MOUNTING PLATE
- [SDR SWIA202162922](https://openairdocs.org/sdr/SWIA202162922.md): None · corroded · Oct 22, 2021 · N797SK · Cndair CL6002C10 · Fuselage Floor Panel
  > PASSENGER DOOR SURROUND LOWER AFT CAP ANGLE IS CORRODED (C-CHECK RO 11-27-21) PASSENGER DOOR SURROUND LOWER AFT CAP ANGLE IS CORRODED ON MULTIPLE ELEMENTS AND OVER FASTENER HOLES AND IS OUT OF LIMITS REF CRJ700 SRM 53-21-23-101-001-A01. REMOVED AFT CAP AN
- [SDR SWIA202162921](https://openairdocs.org/sdr/SWIA202162921.md): None · corroded · Oct 22, 2021 · N797SK · Cndair CL6002C10 · Fuselage Floor Panel
  > PASSENGER DOOR SURROUND LOWER MID CAP ANGLE IS CORRODED (C-CHECK RO 11-27-21) PASSENGER DOOR SURROUND LOWER MID CAP ANGLE IS CORRODED ON MULTIPLE ELEMENTS AND OVER FASTENER HOLES AND IS OUT OF LIMITS REF CRJ700 SRM 53-21-23-101-001-A01. REMOVED MID CAP AN
- [SDR SWIA202162920](https://openairdocs.org/sdr/SWIA202162920.md): None · corroded · Oct 22, 2021 · N797SK · Cndair CL6002C10 · Fuselage Structure (General)
  > PASSENGER DOOR SURROUND LOWER FWD CAP ANGLE IS CORRODED (C-CHECK RO 11-27-21) PASSENGER DOOR SURROUND LOWER FWD CAP ANGLE IS CORRODED ON MULTIPLE ELEMENTS AND OVER FASTENER HOLES AND IS OUT OF LIMITS REF CRJ700 SRM 53-21-23-101-001-A01. REMOVED BAD FWD CA
- [SDR SWIA202162919](https://openairdocs.org/sdr/SWIA202162919.md): None · corroded · Oct 22, 2021 · N797SK · Cndair CL6002C10 · Doors
  > PASSENGER DOOR SURROUND FWD CLOSING FITTING FS314.00 IS CORRODED. (C-CHECK RO 11-27-21) PASSENGER DOOR SURROUND FWD CLOSING FITTING FS314.00 IS CORRODED 100% THROUGH PART AND IS OUT OF LIMITS REF CRJ700 SRM 53-21-23-101-001-A01. REMOVED BAD PASSENGER DOOR
- [SDR SWIA202162918](https://openairdocs.org/sdr/SWIA202162918.md): None · cracked · Oct 22, 2021 · N797SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > PASSENGER DOOR SURROUND LOWER KICKPLATE ANGLE IS CORRODED. (C-CHECK RO 11-27-21) REMOVED AND REPLACED PASSENGER DOOR SURROUND LOWER KICKPLATE. REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DWG SH670-31810 REV AE. COMPLIED WIT
- [SDR SWIA202162949](https://openairdocs.org/sdr/SWIA202162949.md): None · corroded · Oct 15, 2021 · N797SK · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > MID CABIN SIDE SEAT RAIL AT FS797.00 ON RIGHTHAND SIDE CORRORED (C-CHECK RO 11-27-21) MUTIPLE ELEMNTS OF DAMAGE FOUND TO BE IN CROSS SECTION ON ENTIRE LENGHT OF SIDE SEAT RAIL WHICH IS NOT ALLOWED SIDE SEAT RAIL FOUND TO BE OUT OF LIMITS. REPLACED R/H SID
- [SDR SWIA202162953](https://openairdocs.org/sdr/SWIA202162953.md): None · corroded · Oct 14, 2021 · N797SK · Cndair CL6002C10 · Nacelle/Pylon Structure
  > THE GALLEY #1 HAS CORRODED DOUBLER LOCATED BEHIND THE FLOOR FITTING AT THE FWD EDGE/OTBD FITTING. (C-CHECK RO 11-27-21) REPLACED THE CORRODED DOUBLER LOCATED BEHIND THE FLOOR FITTING AT THE FWD EDGE/OTBD FITTING ON THE GALLEY #1 WITH A SERVICEABLE DOUBLER
- [SDR SWIA202162952](https://openairdocs.org/sdr/SWIA202162952.md): None · corroded · Oct 14, 2021 · N797SK · Cndair CL6002C10 · Nacelle/Pylon Structure
  > THE GALLEY #1 HAS A CORRODED DOUBLER LOCATED BEHIND THE FLOOR MOUNT FITTING AT THE INBD EDGE/AFT LOCATION. (C-CHECK RO 11-27-21) REPLACED THE CORRODED DOUBLER LOCATED BEHIND THE FLOOR MOUNT FITTING AT THE INBD EDGE/AFT LOCATION WITH A SERVICEABLE DOUBLER
- [SDR SWIA202162948](https://openairdocs.org/sdr/SWIA202162948.md): None · corroded · Oct 14, 2021 · N797SK · Cndair CL6002C10 · Fuselage Structure (General)
  > THE GALLEY #1 HAS A CORRODED DOUBLER BEHIND THE FWD EDGE/INBD FLOOR FITTING. (C-CHECK RO 11-27-21) REPLACED THE GALLEY #1'S DOUBLER BEHIND THE FWD EDGE/INBD FLOOR FITTING (P/N=9331071-1 AND 8EA SCREWS P/N=NAS517-3-1) WITH A SERVICABLE FITTING REFERENCING
- [SDR SWIA202162917](https://openairdocs.org/sdr/SWIA202162917.md): None · cracked · Oct 9, 2021 · N797SK · Cndair CL6002C10 · Fuselage Structure (General)
  > * CO-PILOT SIDE WINDSHIELD OB POST LOWER AFT MOUNTING BRACKET HAS A SUSPECTED CRACK (FLAGGED). (C-CHECK RO 11-27-21) REMOVED AND REPLACED LOWER AFT MOUNTING BRACKET ON CO-PILOT SIDE WINDSHIELD OB POST REF. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33
- [SDR SWIA202162916](https://openairdocs.org/sdr/SWIA202162916.md): None · cracked · Oct 9, 2021 · N797SK · Cndair CL6002C10 · Fuselage Structure (General)
  > * PILOT SIDE WINDSHIELD OB POST LOWER AFT MOUNTING BRACKET HAS A SUSPECTED CRACK (FLAGGED). (C-CHECK RO 11-27-21) REMOVED AND REPLACED LOWER AFT MOUNTING BRACKET ON PILOT SIDE WINDSHIELD OB POST REF. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 RE
- [SDR SWIA202162947](https://openairdocs.org/sdr/SWIA202162947.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Ailerons
  > L/H #1 FLAP VANE ACTUATOR HAS CORRODED HARDWARE AT CONNECTION COMMON TO FLAP (C-CHECK RO 11-27-21) REMOVED AND REPLACED WITH NEW HARDWARE L/H #1 FLAP VANE ACTUATOR HAS CORRODED HARDWARE AT CONNECTION COMMON TO FLAP REF CRJ-700 AMM 27-52-23-400-801-A01. OP
- [SDR SWIA202162946](https://openairdocs.org/sdr/SWIA202162946.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Ailerons
  > L/H #2 FLAP VANE ACTUATOR HAS CORRODED HARDWARE AT CONNECTION COMMON TO FLAP (C-CHECK RO 11-27-21) REMOVED AND REPLACED 10EA BOLTS AT THE LH IB FLAP #2 FLAP VANE ACTUATOR IAW CRJ700 AMM 27-52-23-400-801-A01. TOOL #: TUC4964 CAL DUE 30-JUN-22.
- [SDR SWIA202162945](https://openairdocs.org/sdr/SWIA202162945.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Ailerons
  > L/H #3 FLAP VANE ACTUATOR HAS CORRODED HARDWARE AT CONNECTION COMMON TO FLAP (C-CHECK RO 11-27-21) REMOVED AND REPLACED 10EA BOLTS AT THE LH IB FLAP #3 FLAP VANE ACTUATOR IAW CRJ700 AMM 27-52-23-400-801-A01. TOOL #: TUC4964 CAL DUE 30-JUN-22.
- [SDR SWIA202162944](https://openairdocs.org/sdr/SWIA202162944.md): None · worn · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > R/H WING SLAT TRACK 3-2 SIDE ROLLERS AT ALL FOUR LOCATIONS ARE WORN/FLAT SPOTS (C-CHECK RO 11-27-21) REMOVED AND REPLACED RH WING SLAT TRACK 3-2 SIDE ROLLERS WITH SERVICEABLE ROLLERS IAW CRJ-700-AMM TASK 27-81-44-400-803-A01 (OPS TEST PASSED)
- [SDR SWIA202162943](https://openairdocs.org/sdr/SWIA202162943.md): None · worn · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > R/H WING SLAT TRACK 2-2 SIDE ROLLERS AT ALL FOUR LOCATIONS HAVE WEAR/FLAT SPOTS/SEIZED BEARING (C-CHECK RO 11-27-21) REMOVED AND REPLACED R/H WING SLAT TRACK 2-2 SIDE ROLLERS AT ALL FOUR LOCATIONS REF CRJ 700 AMM TASK 27-81-44-400-802-A01,GAP AND OPS CHEC
- [SDR SWIA202162942](https://openairdocs.org/sdr/SWIA202162942.md): None · worn · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > L/H WING SLAT TRACK 1-2 SIDE ROLLERS AT ALL FOUR LOCATIONS HAVE SIGNS OF WEAR/FLAT SPOTS/PLAY IN THE BEARING (C-CHECK RO 11-27-21) REMOVED AND REPLACED LH SLAT TACK 1-2 SIDE ROLLERS REF. CRJ-700 AMM 27-81-44-000-801-A01 AND 27-81-44-400-801-A01. OPS CHECK
- [SDR SWIA202162941](https://openairdocs.org/sdr/SWIA202162941.md): None · worn · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > L/H WING SLAT TRACK 2-2 SIDE ROLLERS AT ALL FOUR LOCATIONS SHOW SIGNS OF WEAR/FLAT SPOTS/PLAY IN THE BEARING (C-CHECK RO 11-27-21) REMOVED AND REPLACED LH SLAT TACK 2-2 SIDE ROLLERS REF. CRJ-700 AMM 27-81-44-000-802-A01 AND 27-81-44-400-802-A01. OPS CHECK
- [SDR SWIA202162940](https://openairdocs.org/sdr/SWIA202162940.md): None · worn · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > L/H WING SLAT TRACK 3-2 SIDE ROLLERS AT ALL FOUR LOCATIONS SHOW SIGNS OF WEAR/FLAT SPOTS (C-CHECK RO 11-27-21) REMOVED AND REPLACED LH SLAT TACK 3-2 SIDE ROLLERS REF. CRJ-700 AMM 27-81-44-000-803-A01 AND 27-81-44-400-803-A01. OPS CHECKED GOOD
- [SDR SWIA202162915](https://openairdocs.org/sdr/SWIA202162915.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > L/H SLAT TRACK 3-3 HAS DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED LH SLAT TRACK 3-3 IN LIMITS REF CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-57-42-1232 REV.-- DATE 2021-10-21 ALL STEPS COMPLETED. RIG AND OPS CHECKS GOOD. COMPLIED
- [SDR SWIA202162914](https://openairdocs.org/sdr/SWIA202162914.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > L/H SLAT TRACK 3-2 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED RH SLAT TRACK 3-2 IN LIMITS REF REO 670-57-42-1237 REV.-- DATED 2021-10-25 ALL STEPS COMPLETED. RIG AND OPS CHECK GOOD. COMPLIED WITH 51-900
- [SDR SWIA202162913](https://openairdocs.org/sdr/SWIA202162913.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > L/H SLAT TRACK 3-1 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED LH SLAT TRACK 3-1 REF CRJ700 SRM 51-12-00-001-001-A01, IN LIMITS REF REO 670-57-42-1236 REV.-- DATED 2021-10-25 ALL STEPS COMPLETED. RIG AND
- [SDR SWIA202162912](https://openairdocs.org/sdr/SWIA202162912.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > L/H SLAT TRACK 2-3 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED CORROSION ON LH SLAT TRACK 2-3 AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1247 REV-A DATED 2021-11-15. COMPLIED WITH TASK CARD 51-900-100
- [SDR SWIA202162911](https://openairdocs.org/sdr/SWIA202162911.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > L/H SLAT TRACK 2-2 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED LH SLAT TRACK 2-2 IN LIMITS REF REO 670-57-42-1233 REV.-- DATED 2021-11-05 ALL STEPS COMPLETED. RIG AND OPS CHECK GOOD. COMPLIED WITH 51-900
- [SDR SWIA202162910](https://openairdocs.org/sdr/SWIA202162910.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > L/H SLAT TRACK 2-1 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED LH SLAT TRACK 2-1 IN LIMITS REF REO 670-57-42-1230 REV.-- DATED 2021-11-03 ALL STEPS COMPLETED. RIG AND OPS CHECK GOOD. COMPLIED WITH 51-900
- [SDR SWIA202162909](https://openairdocs.org/sdr/SWIA202162909.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > L/H SLAT TRACK 1-3 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED LH SLAT TRACK 1-3 IN LIMITS REF CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-57-42-1229 REV.-- DATED 2021-10-21 ALL STEPS COMPLETED. RIG AND
- [SDR SWIA202162908](https://openairdocs.org/sdr/SWIA202162908.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > L/H SLAT TRACK 1-2 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) REMOVED CORROSION FROM SLAT TRACK 1-2 REF CRJ700 SRM 51-12-00-001-001-A01 AND COMPLETED ALL STEPS OF REO 670-57-42-1228 REV-- DATED 2021-10-20. COM
- [SDR SWIA202162907](https://openairdocs.org/sdr/SWIA202162907.md): None · corroded · Oct 7, 2021 · N797SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > L/H SLAT TRACK 1-1 HAS EVIDENCE OF CORROSION AND DETERIORATION OF PROTECTIVE COATING (C-CHECK RO 11-27-21) BLENDED LH SLAT TRACK 1-1 IN LIMITS REF REO 670-57-42-1231 REV.-- DATED 2021-10-21 ALL STEPS COMPLETED. RIG AND OPS CHECK GOOD. COMPLIED WITH 51-900

Next page: https://openairdocs.org/aircraft/N797SK/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 = 'N797SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N797SK/reports

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