# Service difficulty reports: N820SK

A list on [N820SK](https://openairdocs.org/aircraft/N820SK.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 4 · 193 reports

- [SDR SWIA20251226029](https://openairdocs.org/sdr/SWIA20251226029.md): Cleat · corroded · Oct 29, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER CLEAT AT FS295 STGR 19R. REMOVED AND REPLACED STRINGER CLEAT AT FS295 STGR 19R. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG# SH670-31630 SHEET 4 REV. K.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2D24) STRUCTURAL MAJOR R
- [SDR SWIA20251226016](https://openairdocs.org/sdr/SWIA20251226016.md): Rib · cracked · Oct 16, 2025 · N820SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RIGHT LWR TRANSCOWL HAS CRACKED LATCH FAIRING ATTACHMENT RIB. REPAIRED TRANSCOWL TO REO 690-54-21-605, REV -. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202512260014](https://openairdocs.org/sdr/SWIA202512260014.md): Seat Track · damaged · Oct 14, 2025 · N820SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > UPON REMOVAL OF RT SIDE SEAT RAIL TRIM RETAINER FOR REPLACEMENT FROM FS 785.00 TO FS 847+7, FOUND THE SEAT RAIL MOUNTING EXTRUSION DAMAGED AT FASTENER LOCATION, LOCATED AT FS 795.00. REWORKED SEAT RAIL MOUNTING EXTRUSION AT FASTENER LOCATION, LOCATED AT FS 79
- [SDR SWI2025F01910](https://openairdocs.org/sdr/SWI2025F01910.md): Stringer · corroded · Oct 11, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STGR 19RH BETWEEN FS295.00 TO FS310. REPLACED STGR 19RH BETWEEN FS295.00 TO FS310.00 REF REO 690-53-21-2043 REV.-. COMPIED WITH 51-900-1002-SKY. LEAK CHECKED GOOD.
- [SDR SWIA202512261011](https://openairdocs.org/sdr/SWIA202512261011.md): Stringer · corroded · Oct 11, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STGR 20RH BETWEEN FS 295 TO FS 310. REMOVED AND INSTALLED NEW STGR 20RH BETWEEN FS295.00 TO FS310.00 REF. CRJ900 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG SH670-31630 REV. K COMPLIED WITH 51-900-1002--SKY. LEAK CHECKS GOOD
- [SDR SWI2025F01909](https://openairdocs.org/sdr/SWI2025F01909.md): Angle · corroded · Oct 7, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON JOINT ANGLE AT FS 379.00 - FS 394.00 STGR 21R. REMOVED AND INSTALLED NEW DIAPHRAGM ANGLE AT FS 379.00 - FS 394.00 AT STGR 21R IAW DWG SH670-32280 REV. H SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY. L
- [SDR SWIA20251226007](https://openairdocs.org/sdr/SWIA20251226007.md): Angle · corroded · Oct 7, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON JOINT ANGLE AT FS 379.00 - FS 394.00 STGR 23R. LOCATED AND DRILLED NEW ANGLE AT STGR 23R BETWEEN FS 379.00 - FS 394.00 REF CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW DIAPHRAGM ANGLE AT FS 379.00 - FS 394.00 AT STGR 23R REF DWG SH670-32
- [SDR SWI2025F01908](https://openairdocs.org/sdr/SWI2025F01908.md): Angle · corroded · Oct 5, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AROUND FASTENER TAILS ON JOINT PIECE AT STGR 21R BETWEEN FS379 AND FS394. REMOVED AND REPLACED JOINT PIECE ANGLE AT STGR 21R BETWEEN FS 379.00 - 394.00 REF SRM 51-42-06-001-001-A01 AND DWG SH670-32280 REV -H, COMPLIED TASK CARD 51-900-1002-SK
- [SDR SWIA20251226005](https://openairdocs.org/sdr/SWIA20251226005.md): Frame · corroded · Oct 5, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME FS379 ATTACHING FLANGE AND WEB SECTION BETWEEN STGR 20R AND 21R. REPLACED FRAME FS379 ATTACHING FLANGE AND WEB SECTION BETWEEN STGR 20R AND 21R REF DWG SH670-32050 REV. J AND DWG SH670-32280 REV. H AND SRM 51-42-06-001-001-A01 AND S
- [SDR SWIA202512261004](https://openairdocs.org/sdr/SWIA202512261004.md): Drag Angle · cracked · Oct 4, 2025 · N820SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LEFT FWD VERTICAL STAB DRAG ANGLE CRACKED. PERFORMED REPAIR ON LT FWD VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
- [SDR SWIA202512260003](https://openairdocs.org/sdr/SWIA202512260003.md): Stringer · corroded · Oct 3, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 19R BETWEEN FS364 AND FS379. REMOVED AND INSTALLED NEW FWD AND AFT STRINGER 19R INSERTS BETWEEN FS349 AND FS477 AND REPAIR SPLICE AND SHIM BETWEEN FS379 AND FS394. REF. SRM 51-42-06-001-001-A01, REO 690-53-21-2042 REV. - AND DWG# S
- [SDR SWIA202512260927](https://openairdocs.org/sdr/SWIA202512260927.md): Frame · no discrepancy · Sep 27, 2025 · N820SK · Cndair CL6002D24 · Standard Practices/Structures
  > REMOVE FS485 FRAME SECTION FROM STGR 23L -STGR 26L TO FOM STGR 24L REPLACEMENT. REMOVED FRAME SECTION AND INSTALLED REPAIR PARTS AND FRAME SECTION AT FS 485 BETWEEN STGR 23L -STGR 26L REF. DWG SH690-33224, REV. B, CRJ-900, SRM 53-00-06-201-001-A03 REPAIR, REV
- [SDR SWIA202512260915](https://openairdocs.org/sdr/SWIA202512260915.md): Window Frame · cracked · Sep 15, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Structure
  > PILOT WINDSHIELD SIDEPOST CRACKED, R & R CRACKED PILOT WINDSHIELD SIDEPOST WITH NEW SIDEPOST USING ALL NEW SEALS AND FASTENERS PER SRM 51-42-21-001-001-A01 AND DWG 601R33007, REV U. ALL CHECKS GOOD.
- [SDR SWIA202512260913](https://openairdocs.org/sdr/SWIA202512260913.md): Door Frame · gouged · Sep 13, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Structure
  > DURING THE DVI OF THE AVIONICS BAY DOOR LANDING. THE INTERIOR SURFACE IS DISCOLORED AND HAS LIGHT GOUGES IN MULTIPLE AREAS AROUND THE OPENING. REMOVED DAMAGES ON AVIONIC DOOR SURROUND SKIN INNER SURFACE BETWEEN FS364.00-FS394.00 & STR25R-STR25L REF. SRM 51-12
- [SDR SWI2025F01884](https://openairdocs.org/sdr/SWI2025F01884.md): Slat Track · damaged · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Leading Edge Devices
  > RIGHT WING SLAT TRACK 2-1 HAS MULTIPLE GROOVE MARKS ON SURFACE. REMOVED AND INSTALLED NEW RT WING 2-1 SLAT TRACK WITH NEW IAW AMM 27-81-41-400-801-A01.OPS CHECKS GOOD.
- [SDR SWI2025F01883](https://openairdocs.org/sdr/SWI2025F01883.md): Stringer · corroded · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R BETWEEN FS613.00 AND FS 629.00 IS CORRODED. (MARKED) (S/N#00872) (C-CHECK RO 12/24/2025)REMOVED CORROSION ON STRINGER 26R BETWEEN FS613.00 AND FS 629.00 REF. CRJ900 SRM 51-21-06-001-001-A01. AFTER ENGINEERING EVALUATION, THE REWORKED CONDITION IS
- [SDR SWI2025F01882](https://openairdocs.org/sdr/SWI2025F01882.md): Slat Track · damaged · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Leading Edge Devices
  > LH WING SLAT TRACK 2-1 UNDERSIDE HAS GROOVES/WEAR. BLENDED AND TREATED THE WEAR/GROOVES ON THE UNDERSIDE OF THE LT WING SLAT TRACK 2-1 PER REO 690-57-42-1326 REV-. ALL STEPS OF THE REO COMPLIED WITH. SKYCARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWI2025F01881](https://openairdocs.org/sdr/SWI2025F01881.md): Tie Down · corroded · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > FWD CARGO TIE DOWN MACHINED BRACKET NEAR FS565.00 AND BETWEEN STRINGER 26R AND 27 IS CORRODED. REMOVED AND REPLACED FWD CARGO TIE DOWN MACHINED BRACKET NEAR FS565.00 AND BETWEEN STRINGER 26R AND 27 PER SRMS 51-42-22-001-001-A01, SRM 51-42-21-001-001-A01, SR
- [SDR SWI2025F01880](https://openairdocs.org/sdr/SWI2025F01880.md): Slat Track · grooved · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Leading Edge Devices
  > INBD AND OTBD SIDE OF LH SLAT TRACK 3-2 GROOVED. BLENDED AND TREATED INBD AND OTBD SIDE OF LH SLAT TRACK 3-2 PER MHIRJ REO 690-57-42-1327 REV--, DATED 2025-10-17. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY. SEE CONTINUATION STEPS FOR MORE DETAILS. ALL C
- [SDR SWI2025F01879](https://openairdocs.org/sdr/SWI2025F01879.md): Slat Track · corroded · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Leading Edge Devices
  > INBD SIDE OF LT SLAT TRACK 1-1 HAS CORROSION BLENDED AND TREATED CORROSION ON THE LH SLAT TRACK 1-1 PER MHIRJ REO 690-57-42-1328 REV --. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRTY. SEE CONTINUATION STEPS FOR FURTHER DETAILS. ALL CHECKS GOOD.COMPLIED WITH
- [SDR SWI2025F01878](https://openairdocs.org/sdr/SWI2025F01878.md): Tie Down · corroded · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > FWD CARGO TIE DOWN MACHINED BRACKET NEAR FS565.00 AND NEAR STRINGER 23L IS CORRODED. (MARKED) (S/N#00844) (C-CHECK RO 12/24/2025)REMOVED AND REPLACED FWD CARGO TIE DOWN MACHINED BRACKET PN SH670-33390-2 NEAR FS565.00 AND NEAR STRINGER 23L PER DWG NO SH690-336
- [SDR SWI2025F01877](https://openairdocs.org/sdr/SWI2025F01877.md): Hinge Fitting · gouged · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > THE PAX DOOR PIANO HINGE ON THE DOOR SIDE LAST LUG AROUND SPRING PIN HOLE IS GOUGED. COMPLIED WITH RECEIVED REO 670-52-11-511 REV.-E. TYPE I: DISPOSITION FOR OUTER OF LUGS (GOUGE, CHAFING). BLEND PERFORMED USING A TAPER RATIO 5:1. LUG WALL THICKNESS IS STIL
- [SDR SWI2025F01876](https://openairdocs.org/sdr/SWI2025F01876.md): Slat Track · damaged · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-3 UNDERSIDE HAS GROOVES/WEAR. BLENDED AND TREATED THE WEAR/GROOVES ON THE UNDERSIDE OF THE LT WING SLAT TRACK 3-3 IAW REO 690-57-42-1330, REV--. ALL STEPS OF THE REO COMPLIED WITH. SKYCARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWI2025F01875](https://openairdocs.org/sdr/SWI2025F01875.md): Slat Track · damaged · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-1 UNDERSIDE HAS GROOVES/WEAR. BLENDED AND TREATED THE WEAR/GROOVES ON THE UNDERSIDE OF THE LT WING SLAT TRACK 3-1 IAW REO 690-57-42-1329 REV--. ALL STEPS OF THE REO COMPLIED WITH.. SKYCARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWI2025F01874](https://openairdocs.org/sdr/SWI2025F01874.md): Slat Track · damaged · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-1 UNDERSIDE HAS GROOVES/WEAR. BLENDED AND TREATED THE WEAR/GROOVES ON THE UNDERSIDE OF THE LT WING SLAT TRACK 1-1 PER REO 690-57-42-1328 REV--. ALL STEPS OF THE REO COMPLIED WITH. SKYCARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWI2025F01873](https://openairdocs.org/sdr/SWI2025F01873.md): Bracket · corroded · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD CARGO TIE DOWN MACHINED BRACKET NEAR FS533.00 AND STRINGER 25L IS CORRODED. REMOVED AND INSTALLED FWD CARGO TIE DOWN MACHINED BRACKET NEAR BS 533 AND STRINGER 25 NEW BRACKET IAW SRM 51-42-21-001-001-A01, SRM 51-42-15-001-001-A01, SRM TASK 51-42-06-001-001
- [SDR SWI2025F01872](https://openairdocs.org/sdr/SWI2025F01872.md): Stringer Splice · corroded · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE ON 19R BETWEEN FS469.00 AND 485.00 IS CORRODED. (S/N#00850) (C-CHECK RO 12/24/2025)REMOVED AND INSTALLED NEW STRINGER SPLICE ON STGR 19R BETWEEN FS469.00 AND 485.00 PER REF RJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-30006 REV-A. SEE CONTINUA
- [SDR SWIA202512260001](https://openairdocs.org/sdr/SWIA202512260001.md): Stringer · corroded · Sep 12, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R BETWEEN FS597.00 AND FS 613.00 IS CORRODED. REPAIRED STRINGER 21R BETWEEN FS597.00 AND FS 613.00 REF CRJ900 SRM 53-00-03-201-001-A02 REPAIR S6294 TYPE Z6 STRINGER SPLICES - SOLUTION I - FS280.00 TO FS977.00 FIGURE 53-00-03-995-806, COMPLIED WITH
- [SDR SWI2025F01905](https://openairdocs.org/sdr/SWI2025F01905.md): Fitting · cracked · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Emergency Exits
  > THE RT AFT EMERGENCY DOOR UPPER AFT PROX SENSOR FITTING IS CRACKED. REPAIRED THE CRACKED UPPER PROX SENSOR FITTING ON THE RT AFT EMER DOOR PER REO 670-52-21-103 REV -. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY. SKYCARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWI2025F01904](https://openairdocs.org/sdr/SWI2025F01904.md): Fitting · cracked · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Structure
  > THE RT FWD EMERGENCY DOOR UPPER PROX SENSOR FITTING IS CRACKED. (C-CHECK RO 12/24/2025)REPAIRED THE CRACKED UPPER PROX SENSOR FITTING ON THE RH FWD EMER DOOR PER MHIRJ REO 670-52-21-103 REV. -- DATED 2024-11-06. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRE
- [SDR SWI2025F01903](https://openairdocs.org/sdr/SWI2025F01903.md): Fitting · cracked · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Structure
  > THE LEFT FWD EMER DOOR AFT UPPER PROX SENSOR FITTING IS CRACKED. REPAIRED THE CRACKED UPPER PROX SENSOR FITTING ON THE LT FWD EMER DOOR PER REO 670-52-21-103 REV-. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY. SKYCARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWI2025F01902](https://openairdocs.org/sdr/SWI2025F01902.md): Stand Off · cracked · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Engine Thrust Reverser
  > RIGHT LWR TRANSCOWL OTBD -A- BRACKET STANDOFF IS CRACKED. REMOVED CRACKED OTBD -A- BRACKET STANDOFF FROM RT LOWER TRANSCOWL AND INSTALLED ONE NEW OTBD -A- BRACKET STANDOFF ON RT LOWER TRANSCOWL IAW GREO 670-54-21-971 REV (-B) 2023-11-28 STEPS 1-3. COMPLIED WI
- [SDR SWI2025F01901](https://openairdocs.org/sdr/SWI2025F01901.md): Stand Off · cracked · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LEFT UPPER TRANSCOWL OTBD -A- BRACKET STANDOFF CRACKED. REMOVED CRACKED OTBD -A- BRACKET STANDOFF FROM LT UPPER TRANSCOWL AND INSTALLED 1EA NEW OTBD -A- BRACKET STANDOFF ON L/H UPPER TRANSCOWL IAW GREO 670-54-21-971 REV -B, STEPS 1-3. COMPLIED WITH SKY CARD
- [SDR SWI2025F01900](https://openairdocs.org/sdr/SWI2025F01900.md): Stand Off · cracked · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Engine Thrust Reverser
  > LEFT UPPER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED CRACKED INBD -A- BRACKET STANDOFF FROM LT UPPER TRANSCOWL AND INSTALLED 1EA NEW INBD -A- BRACKET STANDOFF ON LT UPPER TRANSCOWL REF. GREO 670-54-21-971 REV -B, STEPS 1-3. COMPLIED WITH SKY CARD
- [SDR SWI2025F01899](https://openairdocs.org/sdr/SWI2025F01899.md): Floor Support · corroded · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON RH FLOOR SUPPORT AT RBL 9 APPROX. BS 1070 - 985. REMOVED AND INSTALLED NEW REPLACEMENT RBL 9.0 FLOOR SUPPORT SECTION AND REPAIR PARTS PER SRM 53-00-41-201-001-A03, STEPS 5.B.(8) & (10) - (12) & REO 690-53-61-1686 REV -. STEPS
- [SDR SWI2025F01898](https://openairdocs.org/sdr/SWI2025F01898.md): Floor Support · corroded · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON LT FLOOR SUPPORT AT LBL9 APPROX. FS1000 - FS1088. REMOVED AND INSTALLED NEW REPLACEMENT FLOOR SUPPORT SECTION AND REPAIR PARTS IAW SRM 53-00-41-41-201-001-A03 AND SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 AND REO 690
- [SDR SWI2025F01897](https://openairdocs.org/sdr/SWI2025F01897.md): Strap · corroded · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Cargo/Baggage Doors
  > CORROSION ON JOINT STRAP COMMON TO INBD CORNER OF FWD CARGO DOOR SURROUND AND BS 562.36. REPLACED JOINT STRAP ON FWD. CARGO DOOR SURROUND AT BS 562.36 IAW SRM 51-42-27-001-001-A01, & DWG SH670-33750, REV Y. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202512260911](https://openairdocs.org/sdr/SWIA202512260911.md): Floor Support · corroded · Sep 11, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON LH FLOOR BEAM AT LBL27 APPROX. FS1000 - FS1047. REMOVED AND INSTALLED NEW FLOOR BEAM SECTION AT LBL 27.0 FROM F/S FS 977 TO F/S 1058 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND IAW SRM 51-42-21-001-001-A01AND SRM 51-42-06-001-001-A
- [SDR SWI2025F01896](https://openairdocs.org/sdr/SWI2025F01896.md): Drag Angle · cracked · Sep 10, 2025 · N820SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > RIGHT AFT VERTICAL STAB DRAG ANGLE HAS POSSIBLE CRACK (MARKED). (C-CHECK RO 12/24/2025)EVALUATED, REMOVED AND INSTALLED NEW RH AFT VERTICAL STAB DRAG ANGLE REF CRJ900 SRM 51-42-13-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-22-001-001-A01
- [SDR SWI2025F01895](https://openairdocs.org/sdr/SWI2025F01895.md): Strap · corroded · Sep 10, 2025 · N820SK · Cndair CL6002D24 · Cargo/Baggage Doors
  > CORROSION ON JOINT STRAP COMON TO INBD CORNER OF FWD CARGO DOOR SURROUND AND BS 519.64. REMOVED CORROSION ON JOINT STRAP COMMON TO INBD CORNER OF FWD CARGO DOOR SURROUND AND FS 519.64 REF SRM 51-21-06-001-001-A01. NOT ALLOWABLE DAMAGE ON AREA. REF SRM 53-31-2
- [SDR SWI2025F01894](https://openairdocs.org/sdr/SWI2025F01894.md): Stringer · corroded · Sep 10, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STGR 24L BETWEEN FS501.00 AND FS517.00. REMOVED AND REPLACED STGR 24L SECTION AT FS 447.21 -FS 517, REF. DWG SH690-333207, REV. A, SRM 51-42-06-001-001-A01, REV. 38 AND SRM 51-42-21-001-001-A01, REV. 38. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWI2025F01893](https://openairdocs.org/sdr/SWI2025F01893.md): Cleat · corroded · Sep 10, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CLEAT COMMON TO FS 927.00 INTERCOSTAL AT STGR 22LT HAS CORROSION. REMOVED DISCREPANT AND WET INSTALLED NEW REPLACEMENT CLEAT AT STGR 22L & FS.927 FRAME PER CRJ900 SRM TASK 51-42-06-001-001-A01 REF. BOMBARDIER DWG. SH690-37060 REV. AC.COMPLIED WITH SKYCARD 51-
- [SDR SWIA202512260910](https://openairdocs.org/sdr/SWIA202512260910.md): Drag Angle · cracked · Sep 10, 2025 · N820SK · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LEFT AFT VERTICAL STAB DRAG ANGLE HAS POSSIBLE CRACK. PERFORMED REPAIR ON LH AFT VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01913](https://openairdocs.org/sdr/SWI2025F01913.md): Skin · corroded · Sep 9, 2025 · N820SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION AROUND MULTIPLE RIVET HEADS ON THE OUTER SKIN FS881.00-942.00 STGR27 -23R.. REPAIRED OUTER SKIN FS881.00-942.00 STGR27 -23R REF REO 690-53-51-518, REV.-B, COMPLIED WITH 51-900-1002-SKY. LEAK CHECKS GOOD
- [SDR SWI2025F01912](https://openairdocs.org/sdr/SWI2025F01912.md): Support · corroded · Sep 9, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BACKUP SILL STGR 21L FROM FS310.00 TO FS333.00. REMOVED AND REPLACED BACKUP SILL AT STGR 21L BETWEEN FS310 AND FS333. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 SHEET 9 REV. AE. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01911](https://openairdocs.org/sdr/SWI2025F01911.md): Support · corroded · Sep 9, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BACKUP SILL STGR 21L FROM FS333.00 TO 349.00. REMOVED AND REPLACED BACKUP SILL AT STGR 21L BETWEEN FS333 AND FS349. REF. SRM 51-42-06-001-001-A01 AND DWG SH670-31810 SHEET 9 REV. AE.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA202512260909](https://openairdocs.org/sdr/SWIA202512260909.md): Intercostal · corroded · Sep 9, 2025 · N820SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 20R FORWARD OF FS 319.70 IS CORRODED. REMOVED AND REPLACED CORRODED INTERCOSTAL AT STGR 20R FORWARD OF FS 319.70 WITH NEW INTERCOSTAL USING ALL NEW FASTENERS. REF SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31950 RE
- [SDR SWI2025F01889](https://openairdocs.org/sdr/SWI2025F01889.md): Bracket · corroded · Sep 8, 2025 · N820SK · Cndair CL6002D24 · Fuselage, Landing Gear Attach Fittings
  > CORRODED BRACKET NOTED IN THE LH WHEEL WELL, FWD SPAR, APPROXIMATELY WS10. REMOVED AND REPLACED CORRODED BRACKET ON THE SPAR IN THE LT WHEEL WELL WITH NEW BRACKET USING ALL NEW FASTENERS PER BOMBARDIER DWG CC670-10320 REV F AND SRM 51-42-21-001-001 A01. ALL
- [SDR SWI2025F01888](https://openairdocs.org/sdr/SWI2025F01888.md): Rod · dented · Sep 8, 2025 · N820SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RIGHT INBD FLAP INBD VANE ACTUATOR ROD HAS DENT. RT INBOARD FLAP INBD VANE ACTUATOR ROD END REPAIRED REF REO 670-57-52-257, REV -B, SYSTEM OPS TESTED GOOD. SKYWEST TASKCARD 51-900-1002-SKY COMPLETED.
- [SDR SWI2025F01887](https://openairdocs.org/sdr/SWI2025F01887.md): Rod · dented · Sep 8, 2025 · N820SK · Cndair CL6002D24 · Trailing Edge Flap Control System
  > RT INBD FLAP 2ND FROM OTBD VANE ACTUATOR ROD HAS DENT. RT INBOARD FLAP 2ND FROM OTBD VANE ACTUATOR ROD END REPAIRED REF REO 670-57-52-257, REV -B, SYSTEM OPS TESTED GOOD. SKYWEST TASKCARD 51-900-1002-SKY COMPLETED.

Next page: https://openairdocs.org/aircraft/N820SK/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 = 'N820SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N820SK/reports

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