# Service difficulty reports: N815SK

A list on [N815SK](https://openairdocs.org/aircraft/N815SK.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 2 · 88 reports

- [SDR SWIA2018070644852](https://openairdocs.org/sdr/SWIA2018070644852.md): Post · corroded · Jun 19, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FS 280.00 FLOOR POST RBL11.16 P/N CC670-34180 HAS PITTING CORROSION. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW FS 280.00 RT FLOOR POST AT RBL 11.16 IAW SRM.
- [SDR SWIA2018070644851](https://openairdocs.org/sdr/SWIA2018070644851.md): Web · corroded · Jun 19, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FS 280.00 LOWER WEB IS CORRODED AT DRIP CAP AND CROSSBEAM AREAS. (C-CHECK) RO: 07/01/2018 REMOVED RT FS 280.00 LOWER WEB AND INSTALLED NEW RT FS 280.00 LOWER WEB IAW SRM.
- [SDR SWIA2018070644850](https://openairdocs.org/sdr/SWIA2018070644850.md): Web · corroded · Jun 19, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LT FS 280.00 LOWER WEB IS CORRODED AT DRIP CAP AND CROSSBEAM AREAS. (C-CHECK) RO: 07/01/2018 REMOVED LT FS 280.00 LOWER WEB AND INSTALLED LT FS 280.00 LOWER WEB IAW SRM.
- [SDR SWIA2018070644849](https://openairdocs.org/sdr/SWIA2018070644849.md): Door Sill · corroded · Jun 18, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL AFT OF FS 280.00 IS CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED & REPLACED THE RT FLOOR SILL FS 280.00 TO FS 319.00 IAW SRM. ALL CHECKS GOOD.
- [SDR SWIA2018070644848](https://openairdocs.org/sdr/SWIA2018070644848.md): Intercostal · corroded · Jun 18, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED AT FS 310 - FS 333 STR 21L. (C-CHECK) RO: 07/01/2018 REMOVED & INSTALLED NEW INTERCOSTAL AT FS 310-FS 333 STR 21 IAW SRM. LEAK CHECK GOOD.
- [SDR SWIA2018070644847](https://openairdocs.org/sdr/SWIA2018070644847.md): Strap · corroded · Jun 18, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280.00 CROSSBEAM TOP STRAP LBL 9.0 TO RBL 9.0 IS CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW FS 280.00 TOP STRAP P/N CC670-34097-1SB IAW SRM.
- [SDR SWIA2018070644846](https://openairdocs.org/sdr/SWIA2018070644846.md): Crossbeam · corroded · Jun 18, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LT FS 280.00 CROSSBEAM HAS CORROSION. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW LT FS 280.00 CROSSBEAM P/N CC670-34094-1 IAW SRM.
- [SDR SWIA2018070644845](https://openairdocs.org/sdr/SWIA2018070644845.md): Crossbeam · corroded · Jun 18, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FS 280.00 CROSSBEAM IS CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW RT FS280.00 CROSSBEAM P/N CC670-34094-4 IAW SRM.
- [SDR SWIA2018070644844](https://openairdocs.org/sdr/SWIA2018070644844.md): Angle · corroded · Jun 17, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL ANGLE SHOWS EVIDENCE OF CORROSION BETWEEN FS310.00 & FS349.00. (C-CHECK) RO: 07/01/2018 REPLACED PAX DOOR SURROUND KICK PLATE AND MID CAP ANGLE WITH NEW. P/N: SH670-31875-3S & SH670-31825-7. INSTALLED NEW PAX DOOR KICK PLATE ANGLE AND INSTALLED N
- [SDR SWIA2018070644843](https://openairdocs.org/sdr/SWIA2018070644843.md): Floor Support · corroded · Jun 17, 2018 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280.00 CENTER COCKPIT FLOOR SUPPORT ANGLE CORRODED. (C-CHECK) RO: 07/01/2018 REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE P/N CC670-34095-1SB IAW SRM.
- [SDR SWIA201844128](https://openairdocs.org/sdr/SWIA201844128.md): Sensor · out of adjust · Jan 5, 2018 · N815SK · Cndair CL6002D24 · Landing Gear Position and Warning
  > NOSE DOOR OPEN WARNING MESSAGE AFTER TAKEOFF. ADJUSTED PX31 AND PERFORMED NOSE GEAR SWING IAW AMM. CHECKED GOOD.
- [SDR SWIA201642223](https://openairdocs.org/sdr/SWIA201642223.md): Packing · failed · Jun 13, 2016 · N815SK · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE AFTER TAKEOFF AND NWS IN-OP CAUTION MESSAGE. REPACKED NLG STRUT AND PERFORMED FULL STRUT SERVICE AND PERFORMED LANDING GEAR SWINGS. LEAK CHECK AND OPS CHECKED GOOD.
- [SDR SWIA201642070](https://openairdocs.org/sdr/SWIA201642070.md): Frame · corroded · Mar 24, 2016 · N815SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AVIONICS BAY LOWER FRAME AT BS 295 CORRODED. INSTALLED A NEW FRAME IAW SRM AND REO. PRESSURIZATION CHECKED GOOD.
- [SDR SWIA201642068](https://openairdocs.org/sdr/SWIA201642068.md): Frame · corroded · Mar 24, 2016 · N815SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AVIONICS BAY LOWER FRAME AT BS 333 CORRODED. INSTALLED A NEW FRAME IAW SRM AND REO. PRESSURIZATION CHECK GOOD AT THIS TIME.
- [SDR SWIA201642067](https://openairdocs.org/sdr/SWIA201642067.md): Frame · corroded · Mar 24, 2016 · N815SK · Cndair CL6002D24 · Fuselage Main, Frame
  > AVIONICS BAY LOWER FRAME AT BS 349 CORRODED. R & R THE FRAME IAW SRM. PRESSURE CHECKS GOOD AT THIS TIME.
- [SDR SWIA201642072](https://openairdocs.org/sdr/SWIA201642072.md): Stringer · corroded · Mar 21, 2016 · N815SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R BS 661+90 CORRODED. R & R THE STRINGER IAW SRM.
- [SDR SWIA201642071](https://openairdocs.org/sdr/SWIA201642071.md): Intercostal · corroded · Mar 21, 2016 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL IN AVIONICS BAY BS 364 - 349, STR 27L CORRODED. R & R THE INTERCOSTAL IAW SRM. PRESSURE CHECKED GOOD.
- [SDR SWIA201642069](https://openairdocs.org/sdr/SWIA201642069.md): Doubler · corroded · Mar 21, 2016 · N815SK · Cndair CL6002D24 · Fuselage Main, Structure
  > TCAS ANTENNA DOUBLER IN AVIONICS BAY CORRODED. R & R TCAS ANTENNA DOUBLER IAW AMM. PRESSURE CHECKED GOOD.
- [SDR SWIA201642066](https://openairdocs.org/sdr/SWIA201642066.md): Intercostal · corroded · Mar 21, 2016 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED INTERCOSTAL IN AVIONICS BAY BS 364 - 349, STR 27R. R & R THE INTERCOSTAL IAW SRM. PRESSURE CHECKS GOOD AT THIS TIME.
- [SDR SWIA201642065](https://openairdocs.org/sdr/SWIA201642065.md): Intercostal · corroded · Mar 18, 2016 · N815SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL CORRODED. R & R IAW SRM. PRESSURE CHECK GOOD.
- [SDR SWIA201540940](https://openairdocs.org/sdr/SWIA201540940.md): Skin · dented · Mar 27, 2015 · N815SK · Cndair CL6002C10 · Leading Edge Devices
  > RT WING L/E NR 1 SLAT HAS DENT FROM BIRDSTRIKE. DENT IS APPROXIMATELY 3 FT FROM INBD AND 2" FROM BOTTOM OF SLAT. DENT IS APPROX 2.5" IN DIAMETER AND.035" DEEP. RO: 03/27/2015, FILLED DENT IAW REO.
- [SDR SWIA201439666](https://openairdocs.org/sdr/SWIA201439666.md): Skin · dented · Oct 23, 2014 · N815SK · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > RT ENGINE COWL IS DENTED OUT OF LIMITS. REPLACED IAW AMM.
- [SDR SWIA201438939](https://openairdocs.org/sdr/SWIA201438939.md): Battery Pack · inoperative · Aug 2, 2014 · N815SK · Cndair CL6002D24 · Emergency Equipment
  > FORWARD F/A FLASHLIGHT DOES NOT BLINK. R & R FWD F/A FLASHLIGHT BATTERY, OPS CHECKED GOOD IAW AMM.
- [SDR SWIA201437715](https://openairdocs.org/sdr/SWIA201437715.md): Bulb · inoperative · May 20, 2014 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > RT NR 3 OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT AFT OVERWING SECTION EMERGENCY LIGHT BULB AND CRACKED LENS COVER IAW AMM.
- [SDR SWIA201437626](https://openairdocs.org/sdr/SWIA201437626.md): Seat Track · corroded · May 7, 2014 · N815SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT FLOOR SEAT RAIL AT FS477.00 THRU 573.00 CORRODED. C-CHECK, R & R RT FLOOR SEAT RAIL AT FS477.00 - FS 573.00 IAW AMM.
- [SDR SWIA201437621](https://openairdocs.org/sdr/SWIA201437621.md): Angle · corroded · May 7, 2014 · N815SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR MID-CAP ANGLE HAS CORROSION. C-CHECK, REPLACED NEW PAX DOOR MID CAP ANGLE, PN SH670-31825-7 IAW SRM.
- [SDR SWIA201437622](https://openairdocs.org/sdr/SWIA201437622.md): Structure · chafed · May 4, 2014 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BOTTOM OF FUSELAGE CHAFED AT APPROXIMATELY FS969, STGR27, C-CHECK, BLENDED CHAFE ON FUSELAGE A FS 969, STR 27 IAW REO.
- [SDR SWIA201437629](https://openairdocs.org/sdr/SWIA201437629.md): Striker · dented · May 3, 2014 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR EXTERNAL SURROUND STRUCTURE AT FS 310, UPPER SECTION HAS A DENT. C-CHECK, REPAIRED PASSENGER DOOR SURROUND SEAL STRIKER IAW REO.
- [SDR SWIA201437628](https://openairdocs.org/sdr/SWIA201437628.md): Striker · dented · May 3, 2014 · N815SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR EXTERIOR SURROUND STRUCTURE AT FS 349, UPPER SECTION HAS DENT. C-CHECK, REPAIRED PASSENGER DOOR SURROUND SEAL STRIKER IAW REO.
- [SDR SWIA201437627](https://openairdocs.org/sdr/SWIA201437627.md): Seat Track · corroded · May 3, 2014 · N815SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL HAS CORROSION AT APPROXIMATELY FS 746.00 ON STG 15L. C-CHECK, REPAIRED SIDE SEAT RAIL AT APPROXIMATELY FS 746.00 ON STG 15L. LARGEST MATERIAL LOSS FOUND AT LOACTION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.459", MATERIAL REMOVED- 0.039", WI
- [SDR SWIA201437625](https://openairdocs.org/sdr/SWIA201437625.md): Seat Track · corroded · May 3, 2014 · N815SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 612.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 612.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.430", MATERI
- [SDR SWIA201437624](https://openairdocs.org/sdr/SWIA201437624.md): Seat Track · corroded · May 3, 2014 · N815SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 661.00 + 82.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 661.00 + 82.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING
- [SDR SWIA201437623](https://openairdocs.org/sdr/SWIA201437623.md): Seat Track · corroded · May 3, 2014 · N815SK · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE FLOOR SEAT TRACK HAS CORROSION AT APPROXIMATELY FS 693.00 ON LBL 9.00. C-CHECK, REPAIRED LT SIDE FLOOR SEAT TRACK AT APPROXIMATELY FS 693.00 ON LBL 9.00. LARGEST MATERIAL LOSS FOUND AT LOCATION "Z". STARTING GAP- 0.420", REMAINING GAP- 0.429", MATER
- [SDR SWIA201437638](https://openairdocs.org/sdr/SWIA201437638.md): Support Arm · chafed · May 2, 2014 · N815SK · Cndair CL6002D24 · Cargo/Baggage Doors
  > FWD BAGGAGE BAY DOOR FWD LOWER SUPPORT ARM CHAFED ON TOP SIDE. C-CHECK, BLENDED CHAFE ON FWD BAGGAGE BAY DOOR FWD LOWER SUPPORT ARM TOP SIDE IAW SRM AND STS EA.
- [SDR SWIA201437637](https://openairdocs.org/sdr/SWIA201437637.md): Rod · chafed · May 2, 2014 · N815SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684AB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684AB, AND FOUND TO BE WITHIN LIMITS IAW REO.
- [SDR SWIA201437636](https://openairdocs.org/sdr/SWIA201437636.md): Rod · chafed · May 2, 2014 · N815SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684CB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684CB, AND FOUND TO BE WITHIN LIMITS, IAW REO.
- [SDR SWIA201437635](https://openairdocs.org/sdr/SWIA201437635.md): Rod · chafed · May 2, 2014 · N815SK · Cndair CL6002D24 · Trailing Edge Flaps
  > RT INBD FLAP VANE ACTUATOR ROD UNDER ACCESS PANEL 684DB CHAFED ON CHROME SURFACE. C-CHECK, BLENDED CHAFE ON RT INBD FLAP VANE ACTUATOR ROD UNDER PANEL 684DB, AND FOUND TO BE WITHIN LIMITS IAW REO AND AMM.
- [SDR SWIA201437634](https://openairdocs.org/sdr/SWIA201437634.md): Lever · chafed · May 2, 2014 · N815SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED CHAFED AREA, REQUESTED NDT FOR CRACK CHECK NO DEFECTS WERE NOTED. ORIGINAL MATERIAL THICKNESS WAS 1.700". AFTER RE-WORK MATERIAL THICKNESS IS 1.665". A TOTAL LOSS OF.035. TOTAL ALLOWABLE LOSS IS.050".
- [SDR SWIA201437633](https://openairdocs.org/sdr/SWIA201437633.md): Structure · corroded · May 2, 2014 · N815SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD LOWER CAM LATCH HAS CORROSION UNDERNEATH. C-CHECK, REMOVED CORROSION FROM UNDERNEATH FWD LOWER CAM LATCH OF PAX DOOR IAW SRM.
- [SDR SWIA201437632](https://openairdocs.org/sdr/SWIA201437632.md): Attach Bracket · cracked · May 2, 2014 · N815SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT ANGLE BRACKET CRACKED NEXT TO PULL-IN CABLE ASSIST WHEEL BRACKET. C-CHECK, REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO.
- [SDR SWIA201437631](https://openairdocs.org/sdr/SWIA201437631.md): Support · chafed · May 2, 2014 · N815SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR SUPPORT WHEEL CHAFED. C-CHECK, BLENDED CHAFE ON PAX DOOR SUPPORT WHEEL IAW STS EA.
- [SDR SWIA201437630](https://openairdocs.org/sdr/SWIA201437630.md): Support · chafed · May 2, 2014 · N815SK · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT HAND RAIL OTBD SUPPORT ARM CHAFED FROM PAX DOOR SUPPORT WHEEL. C-CHECK, BLENDED CHAFE ON PAX DOOR AFT HANDRAIL OTBD SUPPORT ARM ORIGINAL MATERIAL THICKNESS.083" REMAINING MATERIAL THICKNESS.078" MATERIAL LOSS OF.005" IS WITHIN LIMITS IAW STS
- [SDR SWIA201436677](https://openairdocs.org/sdr/SWIA201436677.md): Engine · vibration · Mar 4, 2014 · N815SK · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > AT FL 380, ROUGHLY 30 SECONDS AFTER REDUCING TL TO CRUISE SETTING A SIGNIFICANT VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. REPLACED LT ENGINE ASSY IAW AMM.
- [SDR SWIA201334963](https://openairdocs.org/sdr/SWIA201334963.md): Light · inoperative · Oct 19, 2013 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#4503 RELAMPED.
- [SDR SWIA201334795](https://openairdocs.org/sdr/SWIA201334795.md): Light · inoperative · Oct 2, 2013 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > NR 5 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#4693 RELAMPED.
- [SDR SWIA201333484](https://openairdocs.org/sdr/SWIA201333484.md): Lamp · burned out · May 13, 2013 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT ROW 14 BURNED OUT, REPLACED LAMPS.
- [SDR SWIA201333173](https://openairdocs.org/sdr/SWIA201333173.md): Light · inoperative · Apr 6, 2013 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT AT ROW 8 IS BURNED OUT. (FLT 4661) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332690](https://openairdocs.org/sdr/SWIA201332690.md): Light · inoperative · Jan 28, 2013 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > THIRD FROM REAR OVERHEAD CABIN EMERGENCY LIGHT IS BURNED OUT. (FLT 4618) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201231598](https://openairdocs.org/sdr/SWIA201231598.md): Light · inoperative · Aug 23, 2012 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > OVERWING EXIT ROW LIGHT PARTIALLY INOPERATIVE AT ROW 13 ON THE RIGHT SIDE. (FLT 4618) RELAMPED EMERGENCY LIGHTS AT FOOT LEVEL AT ROW 13C/D SIDE IN REFERENCE TO AMM.
- [SDR SWIA201231069](https://openairdocs.org/sdr/SWIA201231069.md): Light · inoperative · Jun 21, 2012 · N815SK · Cndair CL6002D24 · Emergency Lighting
  > AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4452) RELAMPED EMERGENCY LIGHT.

Next page: https://openairdocs.org/aircraft/N815SK/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 = 'N815SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N815SK/reports

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