# Service difficulty reports: N806SK

A list on [N806SK](https://openairdocs.org/aircraft/N806SK.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 · 226 reports

- [SDR SWIA2026062976355](https://openairdocs.org/sdr/SWIA2026062976355.md): Unknown · odor · Jun 29, 2026 · N806SK · Cndair CL6002D24 · Air Distribution System
  > DISTINCT ELECTRICAL BURNING SMELL INFLIGHT AROUND 5000 FT. STAYED FOR ABOUT 60 SECS BEFORE GOING AWAY. NO OTHER INDICATIONS. (FLIGHT 4103) PERFORMED FAULT CONFIRMATION PER FIM 21-21-00 AND FIM 21-22-00 WITH APU AND LT AND RT ENGINES INDIVIDUALLY. INSPECTED C
- [SDR SWIA2025100600828](https://openairdocs.org/sdr/SWIA2025100600828.md): Exhaust Duct · damaged · Aug 28, 2025 · N806SK · Cndair CL6002D24 · Air Distribution System
  > DAMAGED AC EXHAUST. REMOVED AND REPAIRED FWD GALLEY AC EXHAUST DUCT IAW REO 690-21-23-030.
- [SDR SWI2025F01405](https://openairdocs.org/sdr/SWI2025F01405.md): Stringer · corroded · Jul 8, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L HAS MULTIPLE AREAS OF CORROSION FROM FS 954 TO FS 1047. (C-CHECK RO 10/04/2025)REMOVED AND REPLACED STRG 26L FROM F.S. 847 TO F.S. 1098.20 IAW CRJ900 SRM 51-42-06 AND CRJ900 SRM 51-42-20 NO FURTHER ACTION IS REQUIRED, JOB COMPLETED. TASK CARD 5
- [SDR SWI2025F01404](https://openairdocs.org/sdr/SWI2025F01404.md): Stringer · corroded · Jul 8, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 27 HAS MULTIPLE AREAS OF CORROSION FROM FS 927 TO FS 1031. (C-CHECK RO 10/04/2025)REMOVED AND REPLACED STRG 27 FS913 TO FS977 FWD P/N SH690-370-68-5 AND STRG 27 FS977 TO FS1098 AFT P/N SH690-37067-3S, IAW CRJ900, SRM 51-42-06, SRM 51-42-20 NO F
- [SDR SWI2025F01403](https://openairdocs.org/sdr/SWI2025F01403.md): Frame · corroded · Jul 8, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AFT FUSELAGE WET AREA AT FS 1051.30 BETWEEN STR 26R AND STR 26L HAS CORROSION, (C-CHECK RO 10/04/2025)COMPLIED WITH REO 690-53-61-1647 FOR THE REPAIR OF FS 1051.30 BETWEEN STRG 26R AND STRG 26L NO FURTHER ACTION IS REQUIRED, JOB COMPLETED. TASK CARD 51-900-
- [SDR SWI2025F01402](https://openairdocs.org/sdr/SWI2025F01402.md): Frame · corroded · Jul 8, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AFT FUSELAGE WET AREA AT FS 969 BETWEEN STR 26R ABD STR 26L HAS CORROSION. (C-CHECK RO 10/04/2025)REMOVED AND REPLACED AFT FUSELAGE FRAME 969 IAW CRJ900 SRM 51-42-06 AND CRJ900 SRM 51-42-21 NO FURTHER ACTION IS REQUIRED, JOB COMPLETED.
- [SDR SWIA2025100600708](https://openairdocs.org/sdr/SWIA2025100600708.md): Stringer · corroded · Jul 8, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R HAS MULTIPLE AREAS OF CORROSION FROM FS 954 TO FS 1047. (C-CHECK RO 10/04/2025)REMOVED AND REPLACED STRINGER 26R FROM FRAME STATION 855 TO 1051.30 IAW CRJ900 SRM 51-42-06 AND CRJ900 SRM 51-42-21 NO FURTHER ACTION IS REQUIRED, JOB COMPLETED. TASK
- [SDR SWI2025F01411](https://openairdocs.org/sdr/SWI2025F01411.md): Frame · corroded · Jun 26, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AFT FUSELAGE, WET AREA FS 847.00+16 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-51-490 FOR REPAIR OF FRAME 847.00+16 NO FURTHER ACTION IS REQUIRED,
- [SDR SWI2025F01410](https://openairdocs.org/sdr/SWI2025F01410.md): Frame · corroded · Jun 26, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AFT FUSELAGE, WET AREA FS 1031.00 BETWEEN STRG 26L TO 26R HAS CORROSION. COMPLIED WITH REO 690-53-61-1647 FOR REPAIR OF FS 1031.00 BETWEEN STRG 26L AND 26R NO FURTHER ACTION IS REQUIRED,
- [SDR SWI2025F01409](https://openairdocs.org/sdr/SWI2025F01409.md): Structure · corroded · Jun 26, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT FUSELAGE, WET AREA FS 942.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-51-486 AND CRJ900 SRM 53-00-06-201-001-A03 FIGURE 53-00-06-991-868 FOR REPAIR OF AFT FUSELAGE WET AREA FS 942.00 BETWEEN STRG 26L TO STRG 26R NO FURTHER
- [SDR SWIA2025F01408](https://openairdocs.org/sdr/SWIA2025F01408.md): Structure · corroded · Jun 26, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT FUSELAGE, WET AREA FS 1000.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-61-1647 AND CRJ900 SRM 53-00-06-201-001-A03 FOR REPAIR OF FRAME 1000.00 BETWEEN STRG 26L AND 26R NO FURTHER ACTION IS REQUIRED,
- [SDR SWIA2025F01407](https://openairdocs.org/sdr/SWIA2025F01407.md): Structure · corroded · Jun 26, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT FUSELAGE, WET AREA FS 927.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-51-486 AND CRJ900 SRM 53-00-06-201-001-A03 FIGURE 53-00-06-991-868 FOR REPAIR OF AFT FUSELAGE WET AREA FS 927.00 BETWEEN STRG 26L TO STRG 26R NO FURTHER
- [SDR SWIA2025F01406](https://openairdocs.org/sdr/SWIA2025F01406.md): Structure · corroded · Jun 26, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT FUSELAGE, WET AREA FS 954.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-51-486 AND CRJ900 SRM 53-00-06-201-001-A03 FIGURE 53-00-06-991-868 FOR REPAIR OF AFT FUSELAGE WET AREA FS 954.00 BETWEEN STRG 26L TO STRG 26R.
- [SDR SWIA2025100600026](https://openairdocs.org/sdr/SWIA2025100600026.md): Structure · corroded · Jun 26, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT FUSELAGE, WET AREA FS 1049.00 BETWEEN STRG 26L TO 26R HAS CORROSION DAMAGED. COMPLIED WITH REO 690-53-61-1647 FOR REPAIR OF FS 1047.00 BETWEEN STRG 26L AND 26R AND CRJ900 SRM 53-00-06-201-001-A03 NO FURTHER ACTION IS REQUIRED.
- [SDR SWIA2025100600010](https://openairdocs.org/sdr/SWIA2025100600010.md): Frame · corroded · Jun 10, 2025 · N806SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AFT FS 1015.00 BETWEEN STGR 27 AND STGR 26R FOUND RIVETS WITH CORROSION REQ REMOVAL AND EVAL. COMPLIED WITH REO 690-53-61-1647 AMD CRJ900 SRM 53-00-06-201-001-A03 FOR REPAIR OF FRAME 1015.00 BETWEEN STRG 27 AND STRG 26R NO FURTHER ACTION IS REQUIRED,
- [SDR SWI2025F00074](https://openairdocs.org/sdr/SWI2025F00074.md): Light · smoke · Jan 19, 2025 · N806SK · Cndair CL6002D24 · Flight Compartment Lighting
  > SOUND OF ELECTRICAL ARC IN COCKPIT FOLLOWED BY LIGHT SMOKE WHICH DISSIPATED AFTER 10 MINUTES. OCCURRED IN CRUISE AT FL330 30 MINUTES FROM LANDING. FA€™S REPORTED SIMILAR CONDITIONS AND SOME PASSENGERS LOST SEAT POWER. (FLIGHT 3942) PLEASE REFERENCE A
- [SDR SWIA2024081500011](https://openairdocs.org/sdr/SWIA2024081500011.md): Wire Harness · faulted · Aug 11, 2024 · N806SK · Cndair CL6002D24 · Landing Gear System Wiring
  > GEAR DISAGREE WARNING MESSAGE ON DEPARTURE FOLLOWED BY NOSEWHEEL STEERING INOP CAUTION MESSAGE AND WOW INPUT CAUTION MESSAGE AND GND PROX SYS FAULT 1. RAN QRH. GEAR DISAGREE AND WOW INPUT MESSAGES CLEARED AND GND PROX SYS FAULT MESSAGES CLEARED. (FLIGHT 4211
- [SDR SWIA2024081200011](https://openairdocs.org/sdr/SWIA2024081200011.md): Landing Gear · warning message · Aug 11, 2024 · N806SK · Cndair CL6002D24 · Landing Gear Steering System
  > GEAR DISAGREE WARNING MESSAGE ON DEPARTURE FOLLOWED BY NOSEWHEEL STEERING INOP CAUTION MESSAGE AND WOW INPUT CAUTION MESSAGE AND GND PROX SYS FAULT 1. RAN QRH. GEAR DISAGREE AND WOW INPUT MESSAGES CLEARED AND GND PROX SYS FAULT MESSAGES CLEARED. (FLIGHT 4211
- [SDR SWIA202264455](https://openairdocs.org/sdr/SWIA202264455.md): None · cracked · Feb 18, 2022 · N806SK · Cndair CL6002D24 · Window/Windshield System
  > CLIMBING THROUGH 18,500€™ WE HEARD A POP AND A CRACK AND SIMULTANEOUSLY HAD A R WINDOW HEAT CAUTION MESSAGE. THE RIGHT WINDSCREEN COMPLETELY CRACKED. THE PRESSURIZATION REMAINED THE SAME AND WE FOLLOWED THE QRH AND RETURNED TO FIELD. FLIGHT 3741 - FILED CL
- [SDR SWIA2021080259962](https://openairdocs.org/sdr/SWIA2021080259962.md): Attach Angle · corroded · Jul 18, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > ATTACH ANGLE TO R/H JACK SUPPORT INTERCOSTAL CORRODED (C-CHECK RO 7/28/2021) REPLACED ATTACH ANGLE TO RH JACK SUPPORT INTERCOSTAL REF DWG CC670-32050 REV. NC. / CRJ900 SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2021080259961](https://openairdocs.org/sdr/SWIA2021080259961.md): Skin · dented · Jul 17, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > 2 EA DENTS AND 1 EA GOUGE (FORWARD OF 2 EA DENTS) NOTED ON FUSELAGE EXTERNAL SKIN AFT OF FS202.75, BETWEEN STRINGER 19R & 21R. (C-CHECK RO 7/28/2021) REPAIRED 2 EA DENTS AND 1 EA GOUGE AT FS202.75, STRINGER 19R-21R PER REO 690-53-11-1348, REV --, DATED
- [SDR SWIA2021080260007](https://openairdocs.org/sdr/SWIA2021080260007.md): Floorboard · corroded · Jul 8, 2021 · N806SK · Cndair CL6002D24 · Fuselage Floor Panel
  > THE PASSENGER CABIN FLOORBOARD #231BLF HAS A CORRODED DOUBLER ON ITS FWD LOWER EDGE (MARKED). (C-CHECK RO 7/28/2021) REMOVED AND REPLACED DOUBLER PAASENGER CABIN FLOORBOARD #231BLF ON FORWARD LOWER END IAW CRJ 900 SRM 51-42-13-001-001-A01. (SEE CONTINUA
- [SDR SWIA2021080260006](https://openairdocs.org/sdr/SWIA2021080260006.md): Floorboard · corroded · Jul 8, 2021 · N806SK · Cndair CL6002D24 · Fuselage Floor Panel
  > THE PASSENGER CABIN FLOORBOARD #232BRF HAS A CORRODED DOUBLER ON THE LOWER FWD END (MARKED). (C-CHECK RO 7/28/2021) REMOVED AND REPLACED DOUBLER ON PASSENGER CABIN FLOORBOARD #232BRF ON LOWER FORWARD END IAW CRJ 900 SRM 51-42-13-001-001-A01. ( SEE CONTI
- [SDR SWIA2021080259959](https://openairdocs.org/sdr/SWIA2021080259959.md): Frame · corroded · Jun 6, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Frame
  > ANGLE CLIP AT FRAME 349.00 COMMON TO BACK UP SILL HAS CORROSION (C-CHECK RO 7/28/2021) REPLACED ANGLE CLIP AT FRAME COMMON TO BACKUP SILL REF DWG SH670-31810 REV.AE AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202159958](https://openairdocs.org/sdr/SWIA202159958.md): Plate · gouged · Jun 6, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > PLATE AT FS319.00, STGR 21L IS GOUGED (C-CHECK RO 7/28/2021) REPLACED BACK-UP GUSSET (PLATE) AT FS319.00, STRINGER 21L PER SRM 51-42-21-001-001-A01 & DRAWING SH670-31810 REV AE. SEE CONTINUATION CARD FOR DETALS. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021080259957](https://openairdocs.org/sdr/SWIA2021080259957.md): Doubler · corroded · Jun 2, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON PRESSURE FLOOR DOUBLER AT APROX F/S 797 AND LBL 39 (C-CHECK RO 7/28/2021) REPAIRED PRESSURE FLOOR DOUBLER AT APPROX. FS797 AND LBL 39 REF REO 690-53-41-270 REV.-A DATED 2021-07-26 AND CRJ900 SRM 51-21-06-001-001-A01. LEAK CHECK GOOD. COMPLI
- [SDR SWIA2021080259956](https://openairdocs.org/sdr/SWIA2021080259956.md): Support Angle · cracked · Jun 1, 2021 · N806SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND CRACKED SUPPORT ANGLE AT APPROX RBL 18 AFTER REMOVING R/H LOWER FS280 WEB (C-CHECK RO 7/28/2021) INSTALLED NEW SUPPORT ANGLE P/N CC670-34117-6 ON FS280 BULKHEAD. DWG CC670-34010, REV: K, CRJ900 SRM 51-42-06-001-001-A01. SEE CONTINUATION CARD FO
- [SDR SWIA2021080259955](https://openairdocs.org/sdr/SWIA2021080259955.md): Bulkhead Web · corroded · Jun 1, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > R/H LOWER FS280 WEB HAS EXFOLIATION CORROSION AT DOOR OPENING. (C-CHECK RO 7/28/2021) REPAIRED R/H LOWER FS280 BULKHEAD WEB. REF: CRJ900 SRM 53-11-10-201-004-A01. COMPLIED WITH 51-900-1002-SKY. COMPLETED FROM M-337.
- [SDR SWIA2021080259954](https://openairdocs.org/sdr/SWIA2021080259954.md): Stringer Splice · corroded · May 30, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY MANUFACTURE SPLICE CORRODED AT STR 22R FS333 (C-CHECK RO 7/28/2021) REPLACED STRINGER 22R SPLICE @ FS333.00 PER SRM 51-42-06-001-001-A01 & DRAWING SH670-32420 REV E. SEE CONTINUATION CARD FOR DETAILS. CHECKS GOOD. COMPLIED WITH TASK
- [SDR SWIA2021080259953](https://openairdocs.org/sdr/SWIA2021080259953.md): Diaphragm · corroded · May 29, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > PACKER UNDER DIAPHRAGMS AT FRAME FS.661.00+90 STGR 19R HAS CORROSION. (C-CHECK RO 7/28/2021) THE CORRODED PACKER UNDER DIAPHRAGMS AT FRAME 661.00+90 AT STRINGER 19R HAS BEEN REPLACED WITH NEW. REF DWG SH690-39100 REV G, CRJ900 SRM 51-42-06-001-001-A01 A
- [SDR SWIA2021080259952](https://openairdocs.org/sdr/SWIA2021080259952.md): Diaphragm · corroded · May 29, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > DIAPHRAGM JUST FWD OF FRAME FS.661.00+90 STGR 19R HAS CORROSION. (C-CHECK RO 7/28/2021) THE CORRODED DIAPHRAGM JUST FWD OF FRAME 661.00+90 AT STRINGER 19R HAS BEEN REPLACED WITH NEW, REF DWG SH690-39100 REV G, CRJ900 SRM 51-42-06-001-001-A01. COMPLIED
- [SDR SWIA2021080259951](https://openairdocs.org/sdr/SWIA2021080259951.md): Diaphragm · corroded · May 29, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION FOUND BETWEEN FS.661.00+90.00 AND FS.677.00 STGR19 RH JUST FWD OF ECS DUCT INCLUDES FRAME TO STRINGER CLIP. (C-CHECK RO 7/28/2021) REPLACED DIAPHRAGM JUST AFT OF FRAME @ FS661.00+90 & STRINGE 19R PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001
- [SDR SWIA2021080259950](https://openairdocs.org/sdr/SWIA2021080259950.md): Stringer · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 18R CORRODED BETWEEN FS280.00 AND FS310.00 (C-CHECK RO 7/28/2021) REPLACED STRINGER 18R FROM FS280.00-319.00 PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV K. SEE CONTINUATION CARD FOR DETAILS. CH
- [SDR SWIA2021080259949](https://openairdocs.org/sdr/SWIA2021080259949.md): Stringer · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 25L CORRODED BETWEEN FS280.00 AND FS295.00 (C-CHECK RO 7/28/2021) REPLACED STRINGER 25L FROM FS280.00-333.00 PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV K. SEE CONTINUATION CARD FOR DETAILS. CH
- [SDR SWIA2021080259948](https://openairdocs.org/sdr/SWIA2021080259948.md): Stringer · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 26L CORRODED BETWEEN FS280.00 AND FS295.00 (C-CHECK RO 7/28/2021) REPLACED STRINGER 26L FROM FS280.00-333.00 PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV K. SEE CONTINUATION CARD FOR DETAILS. CH
- [SDR SWIA2021080259947](https://openairdocs.org/sdr/SWIA2021080259947.md): Stringer · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 22R CORRODED BETWEEN FS280.00 AND FS295.00 (C-CHECK RO 7/28/2021) REPLACED STRINGER 22R FROM FS280.00-333.00 PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV K. SEE CONTINUATION CARD FOR DETAILS. CH
- [SDR SWIA2021080259946](https://openairdocs.org/sdr/SWIA2021080259946.md): Stringer · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS280.00 AND FS295.00 (C-CHECK RO 7/28/2021) REPLACED STRINGER 21R, FS280.00-FS333.00 PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021080259945](https://openairdocs.org/sdr/SWIA2021080259945.md): Stringer · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 22L CORRODED BETWEEN FS333.00 AND FS349. (C-CHECK RO 7/28/2021) REPLACED MAIN AVIONICS BAY STR 22L BETWEEN FS333.00 AND FS349.00 REF DWG SH670-31350 REV. A, CRJ900 SRM 53-00-03-201-001-A02, AND CRJ900 SRM 51-42-06-001-001-A01. CHEC
- [SDR SWIA202159944](https://openairdocs.org/sdr/SWIA202159944.md): Stringer Splice · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 22L SPLICE AT FS333.00 CORRODED (C-CHECK RO 7/28/2021) REPLACED STRINGER 22L SPICE AT FS333.00 PER SRM 51-42-06-001-001-A01 & DRAWING SH670-32420 REV E. SEE CONTINUATION CARD FOR DETAILS. CHECKS GOOD. COMPLIED WITH TASK CARD 51-
- [SDR SWIA2021080259943](https://openairdocs.org/sdr/SWIA2021080259943.md): Stringer · corroded · May 28, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 22L CORRODED BETWEEN FS310.00 AND FS333.00 (C-CHECK RO 7/28/2021) REPLACED STRINGER 22L, FS280.00-FS333.00 PER SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV K. SEE CONTINUATION CARD FOR DETAILS. CH
- [SDR SWIA2021080259941](https://openairdocs.org/sdr/SWIA2021080259941.md): Attach Angle · corroded · May 25, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > *PAX ENTRY LOWER ATTACH ANGLE COMMON TO MID CAP CORRODED AT MULTIPLE AREAS BETWEEN FS310.00 - FS349.00 (C-CHECK RO 7/28/2021) REPLACED PAX ENTRY LOWER ATTACH ANGLE COMMONT TO MID CAP BETWEEN FS310-FS349 REF DWG SH670-31810 REV. Y, CRJ900 SRM 51-42-21-
- [SDR SWIA2021080259940](https://openairdocs.org/sdr/SWIA2021080259940.md): Slat Track · damaged · May 24, 2021 · N806SK · Cndair CL6002D24 · Leading Edge Devices
  > RH WING SLAT TRACK 2-2 HAS SLAT ROLLER MARKS ON BOTH I/B AND OB SIDES OF TRACK. (C-CHECK RO 7/28/2021) ROLLER MARKS REMOVED FROM RH SLAT TRACK 2-2 PER SRM 51-12-00-001-001-A01. DAMAGE WAS FOUND BEYOND LIMITS OF SRM, AS THERE ARE NO DAMAGE TOLERANCES GIV
- [SDR SWIA2021080260005](https://openairdocs.org/sdr/SWIA2021080260005.md): Attach Angle · corroded · May 23, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CORROSION NOTED ON ATTACHING ANGLES (3 EA.) COMMON TO SERVICE DOOR THRESHOLD BRACKETS AND SILL ANGLE AT FS321, FS329 AND FS338. (C-CHECK RO 7/28/2021) REMOVED AND REPLACED 3 EA. ATTACHING ANGLES P/N SH670-31982-1 COMMON TO SERVICE DOOR THRESHOLD BRACKET
- [SDR SWIA2021080259939](https://openairdocs.org/sdr/SWIA2021080259939.md): Bulkhead Web · corroded · May 23, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > L/H LOWER FS280 BULKHEAD WEB CORRODED THROUGH AT DOOR OPENING. (C-CHECK RO 7/28/2021) REPAIRED L/H LOWER FS280 BULKHEAD WEB. REF: CRJ900 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK 51-900-1002-SKY. COMPLETED FORM M-337
- [SDR SWIA2021080259938](https://openairdocs.org/sdr/SWIA2021080259938.md): Floorbeam · corroded · May 23, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH CROSSBEAM ATTACHING TO FS280 BULKHEAD CORRODED (C-CHECK RO 7/28/2021) REPLACED THE LH FS280 CROSS BEAM WITH NEW BEAM REF CRJ-900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG CC670-34010 REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021080259937](https://openairdocs.org/sdr/SWIA2021080259937.md): Floorbeam · corroded · May 23, 2021 · N806SK · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH CROSSBEAM ATTACHING TO FS280 BULKHEAD CORRODED (C-CHECK RO 7/28/2021) REPLACED THE RH FS280 CROSS BEAM WITH NEW BEAM REF CRJ-900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG CC670-34010 REV K. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2021080260004](https://openairdocs.org/sdr/SWIA2021080260004.md): Seat Track · corroded · May 22, 2021 · N806SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK RBL 9 APPROX. FS 988.00 €“ FS 1000.00 IS CORRODED. (C-CHECK RO 7/28/2021) FLOOR SEAT TRACK RBL 9 APPROX. FS 988.00 - FS 1000 REPLACED WITH NEW SEAT TRACK AND INSTALLED IAW CRJ900 AMM 53-00-49-400-802-A02 / TUC6038 DUE DATE 30 JUN 2022
- [SDR SWIA2021080260003](https://openairdocs.org/sdr/SWIA2021080260003.md): Seat Track · corroded · May 22, 2021 · N806SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK LBL 9 APPROX. FS 988.00 €“ FS 1000.00 IS CORRODED. (C-CHECK RO 7/28/2021) REMOVED AND REPLACED FLOOR SEAT TRACK P/N: BA670-45074-3 AT LBL 9 APPROXIMATELY FS988.00 -FS 1000.00 REF. CRJ-900 AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-
- [SDR SWIA2021080260002](https://openairdocs.org/sdr/SWIA2021080260002.md): Seat Track · corroded · May 22, 2021 · N806SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK LBL 9 APPROX. FS 849.00 €“ FS 988.00 IS CORRODED. (C-CHECK RO 7/28/2021) FLOOR SEAT TRACK AT LBL 9, APPROX. FS849.00 TO FS988.00 WAS FOUND TO BE CORRODED OUT OF LIMITS & WAS REPLACED WITH A NEW SEAT TRACK. REF: CRJ 900 SRM 53-51-49-10
- [SDR SWIA2021080260001](https://openairdocs.org/sdr/SWIA2021080260001.md): Seat Track · corroded · May 22, 2021 · N806SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK RBL 9 APPROX. FS 849.00 €“ FS 988.00 IS CORRODED. (C-CHECK RO 7/28/2021) FLOOR SET TRACK AT RBL 9, APPROX. FS849.00 TO FS988.00 WAS FOUND TO BE CORRODED OUT OF LIMITS & WAS REPLACED WITH A NEW SEAT TRACK. REF: CRJ 900 SRM 53-51-49-101

Next page: https://openairdocs.org/aircraft/N806SK/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 = 'N806SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N806SK/reports

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