# Service difficulty reports: N826SK

A list on [N826SK](https://openairdocs.org/aircraft/N826SK.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SWIA202304260004](https://openairdocs.org/sdr/SWIA202304260004.md): Unknown · cracked · Apr 19, 2023 · N826SK · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND 2 CRACKS ON PAX DOOR, AFT SIDE PANEL, UNDER PAX DOOR MOTOR ASSIST BRACKET. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR IN REF TO CRJ 900 SRM 52-11-04 AND REO 690-52-11-835 REV -- DATED 2023-04-19.
- [SDR SWIA202304260003](https://openairdocs.org/sdr/SWIA202304260003.md): Unknown · dented · Apr 17, 2023 · N826SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SMALL DENT FOUND ABOUT 2 INCHES FWD OF NOSE FUSELAGE JACK PAD. (FILED CLOSED)PERFORMED REPAIR OF DENTED AREA FWD OF NOSE FUSELAGE JACK PAD REF REO 690-53-11-1552 REV -- DATED 2023-04-20 FOR THE REPAIR TO LOWER FUSELAGE STRUCTURE BTW FS 265- FS 280 AND BTW SSTR
- [SDR SWIA202266698](https://openairdocs.org/sdr/SWIA202266698.md): None · broken · Oct 9, 2022 · N826SK · Cndair CL6002D24 · Fuselage, Door Hinge
  > BROKEN CLIP ATTACH TO STR 7L BETWEEN FS1144.00 AND FS1162.00, INSIDE AFT EQUIPMENT BAY. (C-CHECK RO 10/29/2022) REMOVED AND REPLACED 1 EACH CLIP P/N: MM670-97107-001 AT STR 7L BETWEEN FS1144.00 AND FS1162.00, INSIDE AFT EQUIPMENT BAY REF. CRJ-900 SRM 51
- [SDR SWIA202266697](https://openairdocs.org/sdr/SWIA202266697.md): None · corroded · Sep 29, 2022 · N826SK · Cndair CL6002D24 · Ailerons
  > * R/H INBOARD FLAP HAS MULTIPLE AREAS OF INTERNAL CORROSION AND DETERIORATED COATINGS, IN THE 4 BAYS OUT FROM THE INBOARD EDGE, FROM APPROX. MID CHORD TO THE TRAILING EDGE. (C-CHECK RO 10/29/2022) REMOVED AND INSTALLED R/H INBD FLAP REF CRJ-900 AMM 27-
- [SDR SWIA202266690](https://openairdocs.org/sdr/SWIA202266690.md): None · gouged · Sep 26, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > GOUGE ON EXTERNAL FUSELAGE SKIN BETWEEN FS 349.00 - 364.00, STGR 22R - 23R (C-CHECK RO 10/29/2022) / COMPLIED WITH ALL STEPS OF REO 690-53-21-1551 REV -- DATED 2022-10-11 DISPOSITION FOR BLENDED CHAFE DAMAGE TO FUSELAGE LOWER SKIN BETWEEN FS349.00 AND
- [SDR SWIA202266689](https://openairdocs.org/sdr/SWIA202266689.md): None · gouged · Sep 26, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > GOUGES ON EXTERNAL FUSELAGE SKIN FS 379.00 - 394.00, STGR 22R - 23R (C-CHECK RO 10/29/2022) / REPAIRED GOUGES ON EXTERNAL FUSELAGE SKIN AT FS 379.00 - 394.00, STGR 22R - 23R REF REO 690-53-21-1551 REV -- DATED 2022-10-11 COMPLIED WITH ALL STEPS, SEE CO
- [SDR SWIA202266688](https://openairdocs.org/sdr/SWIA202266688.md): None · chafed · Sep 26, 2022 · N826SK · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME FS 1144.00 IN AFT EQUIPMENT BAY HAS CHAFING WEAR FROM HYDRAULIC LINE. FLAGGED (C-CHECK RO 10/29/2022) / REPAIRED FRAME FS1144.00 CHAFING WEAR REF REO 690-53-61-1120 REV -- DATED 2022-10-04 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY SEE CONTI
- [SDR SWIA202266696](https://openairdocs.org/sdr/SWIA202266696.md): None · chafed · Sep 24, 2022 · N826SK · Cndair CL6002D24 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT TRACK AT APPROXIMATELY FS945 HAS CHAFE MARKS. (DAMAGE AREA MARKED WITH RED GREASE PENCIL) (C-CHECK RO 10/29/2022) REMOVED OUT OF LIMITS LH SIDE SEAT TRACK BETWEEN FS 913.00 AND FS 969.00 TO FOM NEW REPLACEMENT REF CRJ900 AMM 53-00-49-00-801
- [SDR SWIA202266695](https://openairdocs.org/sdr/SWIA202266695.md): None · scratched · Sep 24, 2022 · N826SK · Cndair CL6002D24 · Fuselage, Powerplant Attach Fittings
  > LH FLOOR SEAT TRACK AT LBL27 HAS SCRATCHES BETWEEN FS434 AND FS452 (MARKED). (C-CHECK RO 10/29/2022) REMOVED OUT OF LIMITS SEAT TRACK FROM LBL 27.00, FS 434.00 - 452.00 TO FOM NEW REPLACEMENT REF CRJ900 AMM 53-00-49-00-801-A12. / INSTALLED NEW REPLACEME
- [SDR SWIA202266694](https://openairdocs.org/sdr/SWIA202266694.md): None · scratched · Sep 23, 2022 · N826SK · Cndair CL6002D24 · Fuselage, Powerplant Attach Fittings
  > RH FLOOR SEAT TRACK AT RBL9 HAS SCRATCHES BETWEEN FS434 AND FS477 (MARKED). (C-CHECK RO 10/29/2022) REMOVED AND INSTALLED NEW R/H SEAT TRACK, RBL9. P/N:BBDREF005772127. BETWEEN FS.364 AND FS485. PER CRJ900, AMM.53-00-49-400-801. (CONFIG A12). SEE MX# 25
- [SDR SWIA202266693](https://openairdocs.org/sdr/SWIA202266693.md): None · corroded · Sep 23, 2022 · N826SK · Cndair CL6002D24 · Fuselage, Powerplant Attach Fittings
  > RH FLOOR SEAT TRACK AT RBL9 HAS CORROSION ON FORWARD END AND SIDES BETWEEN FS349 AND FS359 (C-CHECK RO 10/29/2022) REMOVED AND INSTALLED NEW R/H SEAT TRACK, RBL9. P/N:BA690-31111-19. BETWEEN FS349 AND FS359 PER CRJ900, AMM.53-00-49-400-801. (CONFIG A12
- [SDR SWIA202266687](https://openairdocs.org/sdr/SWIA202266687.md): None · gouged · Sep 23, 2022 · N826SK · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > PAX DOOR FWD UPPER SEAL STRIKER IS GOUGED AS MARKED (C-CHECK RO 10/29/2022) REPAIRED PAX DOOR FWD UPPER SEAL STRIKER REF CRJ900 SRM 53-21-23-201-003-A01, LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202266692](https://openairdocs.org/sdr/SWIA202266692.md): None · corroded · Sep 22, 2022 · N826SK · Cndair CL6002D24 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT TRACK BETWEEN FS693 AND FS720 HAS CORROSION AND CHAFING (MARKED IN RED GREASE PENCIL). (C-CHECK RO 10/29/2022) REMOVED OUT OF LIMITS LH SIDE SEAT TRACK BETWEEN FS693.00 AND FS720.00 TO FOM NEW REPLACEMENT REF CRJ900 AMM 53-00-49-00-801-A12.
- [SDR SWIA202266691](https://openairdocs.org/sdr/SWIA202266691.md): None · chafed · Sep 22, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > FWD CARGO DOOR INNER SKIN AND AFT FRAME CHAFED ON AFT END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) FWD CARGO DOOR INNER SKIN AND AFT FRAME CHAFE ON AFT END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED AND COMPLIED WIT
- [SDR SWIA202266686](https://openairdocs.org/sdr/SWIA202266686.md): None · chafed · Sep 22, 2022 · N826SK · Cndair CL6002D24 · Doors
  > FORWARD CARGO DOOR SURROUND - FORWARD AND AFT GUIDE FITTINGS CHAFED (MARKED). (C-CHECK RO 10/29/2022) COMPLIED WITH REO 690-53-31-664 REV -- DATED 2022-09-27 REPAIR OF CHAFING ON FORWARD CARGO DOOR SURROUND - FORWARD AND AFT GUIDE FITTINGS. OPS CHECK G
- [SDR SWIA202266685](https://openairdocs.org/sdr/SWIA202266685.md): None · chafed · Sep 22, 2022 · N826SK · Cndair CL6002D24 · Doors
  > CENTER CARGO DOOR SURROUND - FORWARD AND AFT GUIDE FITTINGS CHAFED (MARKED). (C-CHECK RO 10/29/2022) BLENDED CENTER CARGO DOOR SURROUND - FORWARD AND AFT GUIDE FITTINGS REF. CRJ900 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLI
- [SDR SWIA202266684](https://openairdocs.org/sdr/SWIA202266684.md): None · chafed · Sep 22, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > CENTER CARGO DOOR INNER SKIN AND AFT FRAME CHAFED ON AFT END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) CENTER CARGO DOOR INNER SKIN AND AFT FRAME CHAFE ON AFT END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED AND COMPLI
- [SDR SWIA202266683](https://openairdocs.org/sdr/SWIA202266683.md): None · chafed · Sep 22, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > CENTER CARGO DOOR INNER SKIN AND FORWARD FRAME CHAFED ON FORWARD END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) CENTER CARGO DOOR INNER SKIN AND FWD FRAME CHAFE ON FWD END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED AN
- [SDR SWIA202266682](https://openairdocs.org/sdr/SWIA202266682.md): None · chafed · Sep 22, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > FWD CARGO DOOR INNER SKIN AND FORWARD FRAME CHAFED ON FORWARD END OF DOOR (MARKED). (C-CHECK RO 10/29/2022) FWD CARGO DOOR INNER SKIN AND FWD FRAME CHAFE ON FWD END OF DOOR FOUND TO BE OUT OF LIMITS REF CRJ 900 SRM 52-35-01-101-001-A01 RECEIVED AND COMP
- [SDR SWIA202266681](https://openairdocs.org/sdr/SWIA202266681.md): None · dented · Sep 15, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > FOUND DENT ABOVE LEFT SIDE ICE DETECTOR, MEASURED.7 LONG X.4 WIDE AND.025 DEEP DENT FOUND TO BE IN LIMITS IN REFERENCE TO CRJ900 SRM 53-00-01. BELOW THE STANDBY PITOT TUBE ABOVE THE WL 75.50 (C-CHECK RO 10/29/2022) REPAIRED DENT ABOVE LEFT SIDE ICE
- [SDR SWIA202265117](https://openairdocs.org/sdr/SWIA202265117.md): None · damaged · Feb 23, 2022 · N826SK · Cndair CL6002D24 · Fuselage Structure (General)
  > AIRCRAFT STAIRS STAND CONTACTED AIRCRAFT CAUSING DAMAGE AT FS 231 & WL 79.50. DAMAGE MEASURES 5.5 INCHES IN WIDTH AND 7 INCHES IN LENGTH. (FILED - CLOSED)REPAIRED DAMAGE AT FS 220.00-FS235.00 AND STR 14R-STR16R PER REO 690-53-11-1403 REV "--" DATED 2022-03-1
- [SDR SWIA202265116](https://openairdocs.org/sdr/SWIA202265116.md): None · missing · Feb 15, 2022 · N826SK · Cndair CL6002D24 · Landing Gear System
  > FOUND LH MLG AFT TRUNNION BEARING LOCKNUT/LOCK WASHER NOT INSTALLED ON AFT BEARING, AFT BEARING MIGRATED OUT OF TRUNNION. (FILED - CLOSED) REFERENCE CP 24359791 AND CP 24405101 FOR CORRECTIVE ACTION OF REMOVAL AND REPLACMENT OF LH TRUNNION AFT BEARING ASSE

## 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 = 'N826SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N826SK/reports

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