# Service difficulty reports: N814SK

A list on [N814SK](https://openairdocs.org/aircraft/N814SK.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 · 110 reports

- [SDR SWIA2019030545580](https://openairdocs.org/sdr/SWIA2019030545580.md): Unknown · smoke · Feb 28, 2019 · N814SK · Cndair CL6002D24 · Air Distribution System
  > SMOKE FWD LAV MASTER WARNING ON TAXI FOLLOWING DEICE PROCESS OF TYPE 1 AND TYPE 4 FLUID AND SUBSEQUENT ENGINE RUN UP. SMOKE ALARMS WERE AUDIBLE AND THE FWD FA NOTIFIED ME THAT WE NEED TO GET OFF THE PLANE IMMEDIATELY. SHE AND THE AFT FA SAID THEY SMELLED SMOKE
- [SDR SWIA2019020145495](https://openairdocs.org/sdr/SWIA2019020145495.md): Unknown · odor · Jan 31, 2019 · N814SK · Cndair CL6002D24 · Air Distribution System
  > FWD LAV SMOKE WARNING MESSAGE ON TAKEOFF. SMELLED POSSIBLE BURNING DEICE FLUID. MESSAGE CLEARED AFTER SEVERAL MINUTES AND SMELL CLEARED AS WELL. (FLT#4810) RAN PACKS OFF OF ENGINES AND APU BLEEDS, NO SMELL/SMOKE NOTED AT THIS TIME. INTERROGATED SMELL/SMOKE IN
- [SDR SWIA2018061844793](https://openairdocs.org/sdr/SWIA2018061844793.md): Intercostal · corroded · Jun 8, 2018 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON THE INTERCOSTAL AT STRINGER 21L, BETWEEN BS 333 - 349. REPLACED THE INTERCOSTAL IAW SRM.
- [SDR SWIA2018061844800](https://openairdocs.org/sdr/SWIA2018061844800.md): Stringer Splice · corroded · Jun 7, 2018 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 26L AT BS 333 WAS CORRODED. REPLACED THE STRINGER SPLICE IAW SRM.
- [SDR SWIA2018061844799](https://openairdocs.org/sdr/SWIA2018061844799.md): Stringer Splice · corroded · Jun 3, 2018 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 26R AT BS 333 WAS CORRODED. REPLACED THE STRINGER SPLICE IAW SRM.
- [SDR SWIA2018061844798](https://openairdocs.org/sdr/SWIA2018061844798.md): Stringer Splice · corroded · Jun 3, 2018 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 25R AT BS 333 WAS CORRODED. REPLACED THE STRINGER SPLICE IAW SRM.
- [SDR SWIA2018061844797](https://openairdocs.org/sdr/SWIA2018061844797.md): Stringer · corroded · Jun 3, 2018 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L, BETWEEN BS 333 AND 349 WAS CORRODED. REPLACED THE STRINGER IAW SRM.
- [SDR SWIA2018061844796](https://openairdocs.org/sdr/SWIA2018061844796.md): Stringer · corroded · Jun 3, 2018 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 27, BETWEEN BS 310 AND 319 WAS CORRODED. REPLACED THE STRINGER.
- [SDR SWIA2018061844795](https://openairdocs.org/sdr/SWIA2018061844795.md): Stringer · corroded · Jun 3, 2018 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R, BETWEEN BS 295 - 333 WAS CORRODED. REPLACED THE STRINGER.
- [SDR SWIA2018061844794](https://openairdocs.org/sdr/SWIA2018061844794.md): Stringer · corroded · Jun 3, 2018 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L, BETWEEN BS 280 - 333 HAD CORROSION. REPLACED THESTRINGER IAW SRM.
- [SDR SWIA201642329](https://openairdocs.org/sdr/SWIA201642329.md): Seal · damaged · Jul 21, 2016 · N814SK · Cndair CL6002D24 · Pneumatic Distribution System
  > LEFT BLEED DUCT MASTER WARNING. AFTER 30 SECS CHANGED TO LEFT BLEED DUCT CAUTION. BOTH PACKS OFF AND PRESSURIZATION WOULD NOT HOLD. CAUTION MESSAGE WENT AWAY AFTER VALVES WERE CLOSED. DECLARED AN EMERGENCY AND DIVERTED. REPLACED LT PYLON LOOPS MT 202/203 AND
- [SDR SWIA201641929](https://openairdocs.org/sdr/SWIA201641929.md): Door Sill · corroded · Feb 18, 2016 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL HAS CORROSION AROUND THE FWD LOWER FITTING. R & R IAW SRM.
- [SDR SWIA201641928](https://openairdocs.org/sdr/SWIA201641928.md): Support Angle · corroded · Feb 2, 2016 · N814SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD SUPPORT ANGLE CORRODED. INSTALLED A NEW SUPPORT ANGLE IAW SRM.
- [SDR SWIA201641927](https://openairdocs.org/sdr/SWIA201641927.md): Intercostal · corroded · Feb 2, 2016 · N814SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER CENTER INTERCOSTAL HAD CORROSION. REMOVED AND REPLACED THE INTERCOSTA IAW SRM. NO LEAKS NOTED.
- [SDR SWIA201641926](https://openairdocs.org/sdr/SWIA201641926.md): Intercostal · corroded · Feb 2, 2016 · N814SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER INTERCOSTAL HAD CORROSION. REPAIRED IAW EA. LEAK CHECKED GOOD.
- [SDR SWIA201641925](https://openairdocs.org/sdr/SWIA201641925.md): Intercostal · corroded · Feb 2, 2016 · N814SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER INTERCOSTAL HAD CORROSION. REPAIRED IAW EA. LEAK CHECKED GOOD.
- [SDR SWIA201641924](https://openairdocs.org/sdr/SWIA201641924.md): Intercostal · corroded · Feb 2, 2016 · N814SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER INTERCOSTAL HAD CORROSION. REPAIRED IAW EA.
- [SDR SWIA201641914](https://openairdocs.org/sdr/SWIA201641914.md): Floor Panel · cracked · Feb 2, 2016 · N814SK · Cndair CL6002D24 · Fuselage Floor Panel
  > RT TRU BAY FLOOR CRACKED. PERFORMED REPAIR OF RT TRU BAY FLOOR CRACK AT BS 193 IAW REO.
- [SDR SWIA201641913](https://openairdocs.org/sdr/SWIA201641913.md): Floor Panel · cracked · Feb 2, 2016 · N814SK · Cndair CL6002D24 · Fuselage Floor Panel
  > LEFT TRU BAY FLOOR CRACKED. REPAIRED LT TRU BAY FLOOR CRACK AT FS 193 IAW REO.
- [SDR SWIA201641923](https://openairdocs.org/sdr/SWIA201641923.md): Stringer · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R BETWEEN BS 280 - 333 HAD CORROSION AROUND FASTENERS. REMOVED AND REPLACED THE STRINGER IAW SRM. LEAK CHECKED GOOD.
- [SDR SWIA201641922](https://openairdocs.org/sdr/SWIA201641922.md): Frame · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT BS 295 BETWEEN STRINGERS 25L - 26R HAD CORROSION AROUND FASTENERS. BLENDED CORROSION ON FRAME IAW SRM. REPAIRED THE FRAME IAW REO. LEAK CHECKED GOOD.
- [SDR SWIA201641921](https://openairdocs.org/sdr/SWIA201641921.md): Frame · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT BS 310 BETWEEN STRINGER 25L - 25R HAD CORROSION AROUND FASTENERS. REPAIRED THE FRAME IAW REO. NO LEAKS NOTED.
- [SDR SWIA201641920](https://openairdocs.org/sdr/SWIA201641920.md): Frame · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT BS 319 BETWEEN STRINGERS 25L - 26R HAD CORROSION AROUND FASTENERS. REPAIRED THE FRAME IAW REO. NO LEAKS NOTED.
- [SDR SWIA201641919](https://openairdocs.org/sdr/SWIA201641919.md): Stringer · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R BETWEEN BS 280 - 333 HAS CORROSION AROUND FASTENERS. R & R THE STRINGER IAW SRM. LEAK CHECKED GOOD.
- [SDR SWIA201641918](https://openairdocs.org/sdr/SWIA201641918.md): Frame · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT BS 333 BETWEEN STRINGERA 26R - 26L HAS CORROSION AROUND FASTENERS. PERFORMED FRAME SECTOR REPAIR IAW REO. PRESSURIZATION LEAK CHECKED GOOD.
- [SDR SWIA201641917](https://openairdocs.org/sdr/SWIA201641917.md): Frame · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT BS 349 BETWEEN STRINGERS 26R - 26L HAS CORROSION AROUND FASTENERS. REMOVED AND INSTALLED A NEW FRAME IAW SRM. NO LEAKS NOTED.
- [SDR SWIA201641916](https://openairdocs.org/sdr/SWIA201641916.md): Stringer · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R BETWEEN BS 333 AND 364 HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED THE STRINGER IAW SRM. PERFORMED PRESSURE LEAK CHECK OF REPAIRED AREA IAW SRM AND AMM. LEAK CHECKED GOOD.
- [SDR SWIA201641915](https://openairdocs.org/sdr/SWIA201641915.md): Vane · chafed · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE L/E CHAFED AT THE OTBD VANE ACTUATOR. REPLACED PANEL 584HT IAW SRM.
- [SDR SWIA201641912](https://openairdocs.org/sdr/SWIA201641912.md): Stringer · corroded · Jan 31, 2016 · N814SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L BETWEEN BS 333 AND 364 CORRODED AROUND FASTENERS. REMOVED THE STRINGER AND INSTALLED A NEW SERVICEABLE STRINGER IAW SRM. PERFORMED PRESSURE LEAK CHECK OF REPAIRED AREA IAW SRM AND AMM. LEAK CHECKED GOOD.
- [SDR SWIA201439143](https://openairdocs.org/sdr/SWIA201439143.md): Warning Light · false indication · Aug 17, 2014 · N814SK · Cndair CL6002D24 · Central Warning
  > RT & LT TRANSFER SHUTOFF VALVE CAUTION INFLIGHT. PERFORMED THE FIM LRU CHECK WITH NO FURTHER FAULTS.
- [SDR SWIA201437773](https://openairdocs.org/sdr/SWIA201437773.md): Lens · damaged · May 24, 2014 · N814SK · Cndair CL6002D24 · Emergency Lighting
  > FORWARD LT EMERGENCY EXIT LIGHT ASSEMBLY AND LENS DAMAGED. R & R FORWARD LT EMERGENCY EXIT LIGHT ASSEMBLY AND LENS IAW AMM.
- [SDR SWIA201437694](https://openairdocs.org/sdr/SWIA201437694.md): Lamp · burned out · May 19, 2014 · N814SK · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY OVERHEAD LIGHT IS BURNED OUT, REPLACED THE LAMP.
- [SDR SWIA201437554](https://openairdocs.org/sdr/SWIA201437554.md): Lamp · burned out · May 12, 2014 · N814SK · Cndair CL6002D24 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT JUST AFT OF SERVICE DOOR IS BURNED OUT. R & R LAMP IAW AMM.
- [SDR SWIA201437130](https://openairdocs.org/sdr/SWIA201437130.md): Connector · loose · Apr 14, 2014 · N814SK · Cndair CL6002D24 · Light System Wiring
  > EMERGENCY EXIT LIGHT FRONT WALL IS INOPERATIVE. CONNECTED LOOSE CONNECTOR P341 BEHIND G3 GALLEY.
- [SDR SWIA201437048](https://openairdocs.org/sdr/SWIA201437048.md): Seat Track · corroded · Mar 30, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK BS 379-483 CORRODED. C-CHECK, R & R RT SEAT TRACK IAW AMM.
- [SDR SWIA201437037](https://openairdocs.org/sdr/SWIA201437037.md): Seat Track · corroded · Mar 30, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT TRACK BS 661+14 - 661+90 CORRODED, C-CHECK, R & R RT SEAT TRACK IAW AMM.
- [SDR SWIA201437027](https://openairdocs.org/sdr/SWIA201437027.md): Intercostal · corroded · Mar 30, 2014 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR CUTOUT INTERCOSTAL, STGR 27, IS CORRODED. C-CHECK, REPLACED AVIONICS BAY DOOR CUTOUT FWD INTERCOSTAL, WITH NEW IAW SRM.
- [SDR SWIA201437026](https://openairdocs.org/sdr/SWIA201437026.md): Attach Angle · corroded · Mar 30, 2014 · N814SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > AVIONICS BAY DOOR CUTOUT ATTACH ANGLE, STRINGER 26R, IS CORRODED. C-CHECK, CORROSION ON DISCREPANT AREA OF AVIONICS BAY DOOR CUTOUT ATTACHMENT ANGLE, STGR 26R 100 PERCENT THROUGH PART, LOCATED AND DRILLED FULL SIZE ALL HOLES COMMON TO REPLACEMENT ANGLE AND
- [SDR SWIA201437025](https://openairdocs.org/sdr/SWIA201437025.md): Intercostal · corroded · Mar 30, 2014 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR CUTOUT INTERCOSTAL, STRINGER 27, IS CORRODED. C-CHECK, INTERCOSTAL IAW SRM.
- [SDR SWIA201437038](https://openairdocs.org/sdr/SWIA201437038.md): Door Sill · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX ENTRY, MID CAP ANGLE CORRODED BEYOND LIMITS. C-CHECK, R & R PAX DOOR SILL MID CAP ANGLE IAW SRM.
- [SDR SWIA201437036](https://openairdocs.org/sdr/SWIA201437036.md): Seat Track · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > MID FLOOR SEAT TRACK CORRODED BS 640. C-CHECK, BLENDED CORRODED AREA IAW REO.
- [SDR SWIA201437035](https://openairdocs.org/sdr/SWIA201437035.md): Seat Track · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK CORRODED BS 699. C-CHECK, BLENDED CORRODED AREA IAW REO.
- [SDR SWIA201437034](https://openairdocs.org/sdr/SWIA201437034.md): Seat Track · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK CORRODED AT BS 750. C-CHECK, BLENDED CORRODED AREA IAW REO.
- [SDR SWIA201437033](https://openairdocs.org/sdr/SWIA201437033.md): Seat Track · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE, SEAT TRACK CORRODED BS 797 - 812 C-CHECK BLENDED CORRODED AREA IAW REO.
- [SDR SWIA201437032](https://openairdocs.org/sdr/SWIA201437032.md): Seat Track · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK CORRODED BS 812 - 744. C-CHECK, BLENDED CORRODED AREA IAW REO.
- [SDR SWIA201437031](https://openairdocs.org/sdr/SWIA201437031.md): Seat Track · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK CORRODED AT BS 662. C-CHECK, BLENDED CORRODED AREA IAW REO.
- [SDR SWIA201437030](https://openairdocs.org/sdr/SWIA201437030.md): Floor Support · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AVIONICS BAY FWD CRAWL FLOOR, FWD MOUNT ANGLE HAS SURFACE CORROSION AT THE AFT SIDE OF FS 280. C-CHECK, CORROSION ON DISCREPANT AREA OF AVIONICS BAY FORWARD CRAWL FLOOR FORWARD MOUNT ANGLE IS 100 PERCENT THROUGH PART, LOCATED AND DRILLED FULL SIZE ALL HOLES CO
- [SDR SWIA201437029](https://openairdocs.org/sdr/SWIA201437029.md): Floor Support · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE NEAR SERVICE DOOR HAS CORROSION IN THREE LOCATIONS. C-CHECK, R & R SERVICE DOOR FLOOR SUPPORT ANGLE IAW SRM.
- [SDR SWIA201437028](https://openairdocs.org/sdr/SWIA201437028.md): Floor Support · corroded · Mar 29, 2014 · N814SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT FORWARD FLOOR SUPPORT, NEAR THE FWD SIDE OF SERVICE DOOR, IS CORRODED. C-CHECK, REMOVED AND INSTALLED NEW FLOOR SUPPORT FWD OF SERVICE DOOR IAW SRM.
- [SDR SWIA201437040](https://openairdocs.org/sdr/SWIA201437040.md): Skin · corroded · Mar 28, 2014 · N814SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AFT CARGO BAY, BELOW FLOOR 281KLF, SKIN CORRODED AROUND NUTPLATE, C-CHECK. REPAIRED CORRODED SKIN IAW REO.

Next page: https://openairdocs.org/aircraft/N814SK/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 = 'N814SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N814SK/reports

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