# Service difficulty reports: N416SW, cancelled Feb 4, 2019

A list on [N416SW, cancelled Feb 4, 2019](https://openairdocs.org/deregistered/N416SW-2019-02-04.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 · 178 reports

- [SDR SWIA201642311](https://openairdocs.org/sdr/SWIA201642311.md): Module · failed · Jul 19, 2016 · N416SW · Cndair CL6002B19 · Cabin Pressure Control System
  > AT FL270, EN ROUTE, THE CABIN ALTITUDE WARNING CAME ON & ALL THE MASKS IN THE CABIN DEPLOYED. THE CREW & PASSENGERS DONNED THEIR OXYGEN MASKS. THE CREW DECLARED AN EMERGENCY & DIVERTED. R & R CABIN PRESSURE ACQUISITION MODULE IAW AMM. PN ON: 1027SB04C03, SN
- [SDR SWIA201541567](https://openairdocs.org/sdr/SWIA201541567.md): Pump · failed · Nov 16, 2015 · N416SW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > HYD 3A LOW PRESS CAUTION 1800 PSI. REQUIRED EMERGENCY GEAR EXTENSION. AFTER EXTENSION DOWN TO 1500 PSI QTY IN FLIGHT SHOWN 80 PERCENT BEFORE GEAR EXTENSION. ON GROUND WITH BOTH PUMPS ON QTY DOWN TO 5 PERCENT. FLUID AROUND RT MAIN GEAR. FO: REPLACED 3A PUMP
- [SDR SWIA201440498](https://openairdocs.org/sdr/SWIA201440498.md): Cover · unserviceable · Dec 27, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPPER SHROUD FOR LT WINDSCREEN ON INBD SIDE IS UNSERVICEABLE. REPAIRED TURNBUCKLE COVER IAW EA.
- [SDR SWIA201440497](https://openairdocs.org/sdr/SWIA201440497.md): Placard · cracked · Dec 27, 2014 · N416SW · Cndair CL6002B19 · Placards and Markings
  > APU ECU "NO STEP" COVER IS CRACKED. REPAIRED APU ECU "NO STEP" COVER IAW EA.
- [SDR SWIA201440496](https://openairdocs.org/sdr/SWIA201440496.md): Skin · dented · Dec 23, 2014 · N416SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT MIDDLE WING L/E 530JL HAS A DENT AT APPROXIMATE WS 200. HAND DRESSED THE DENT IAW REO.
- [SDR SWIA201440495](https://openairdocs.org/sdr/SWIA201440495.md): Skin · dented · Dec 23, 2014 · N416SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LT INBD WING L/E PANEL HAS TWO DENTS AT APPROXIMATE WS92.0 AND WS124.5. DRESSED BACK THE DENTS IAW REO.
- [SDR SWIA201440540](https://openairdocs.org/sdr/SWIA201440540.md): Hand Rail · damaged · Dec 15, 2014 · N416SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD HAND RAIL, DENTED FWD UPPER CORNER COVER AND DAMAGED ATTACH FASTENER. REPAIRED AND RESTORED FINISH IAW SRM AND REO.
- [SDR SWIA201440539](https://openairdocs.org/sdr/SWIA201440539.md): Hand Rail · damaged · Dec 15, 2014 · N416SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT HANDRAIL, DENTED AFT UPPER CORNER COVER AND DAMAGED ATTACH FASTENER. REPAIRED AND RESTORED FINISH IAW SRM AND REO.
- [SDR SWIA201440538](https://openairdocs.org/sdr/SWIA201440538.md): Post · cracked · Dec 12, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128 BL 0, RT SIDE OF POST CRACKED AT TOP. INSTALLED POST ASSEMBLY IAW SRM AND REO.
- [SDR SWIA201440537](https://openairdocs.org/sdr/SWIA201440537.md): Floor Support · gouged · Dec 11, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT BS 435, LBL 43 IS DAMAGED OUT OF LIMITS. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EA.
- [SDR SWIA201440536](https://openairdocs.org/sdr/SWIA201440536.md): Frame · cracked · Dec 8, 2014 · N416SW · Cndair CL6002B19 · Fuselage Main, Frame
  > LEFT INTERIOR FUSELAGE FRAME AT BS 559 + 32 AT STRINGER 6L IS CRACKED. INSTALLED REPAIR 6 IAW EA.
- [SDR SWIA201440535](https://openairdocs.org/sdr/SWIA201440535.md): Piccolo Tube · gouged · Dec 8, 2014 · N416SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WING OTBD PICCOLO TUBE IS GOUGED AT THE OTBD END. REPAIRED LT WING OTBD PICCOLO TUBE IAW EA.
- [SDR SWIA201440534](https://openairdocs.org/sdr/SWIA201440534.md): Duct · broken · Dec 8, 2014 · N416SW · Cndair CL6002B19 · Air Distribution System
  > RT PSU DUCT RISER AF BS 953 HAS A BROKEN DUCT ON THE AFT SIDE.: REPAIR COMPLETE IAW EA.
- [SDR SWIA201440533](https://openairdocs.org/sdr/SWIA201440533.md): Frame · cracked · Dec 8, 2014 · N416SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT BS 409+80 IS CRACKED AT STRINGER 6L. REPAIRED THE FRAME IAW SRM AND STS EA.
- [SDR SWIA201440532](https://openairdocs.org/sdr/SWIA201440532.md): Floor Support · corroded · Dec 6, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT FROM BS 473.15 - 513 HAS CORROSION. THE CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440531](https://openairdocs.org/sdr/SWIA201440531.md): Floor Support · corroded · Dec 6, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT FROM BS 409.128 - 473.15 HAS CORROSION. REMOVED THE CORROSION IAW REO.
- [SDR SWIA201440530](https://openairdocs.org/sdr/SWIA201440530.md): Floor Support · corroded · Dec 6, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT BS 409.128 - 473.15 HAS CORROSION. CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440529](https://openairdocs.org/sdr/SWIA201440529.md): Floor Support · corroded · Dec 6, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT ANGLE FROM BS 473.15 - 513 CORRODED. THE CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440528](https://openairdocs.org/sdr/SWIA201440528.md): Floor Support · corroded · Dec 6, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT ANGLE FROM BS 513 - 559 CORRODED. CORROSION WAS BLENDED IAW REO.
- [SDR SWIA201440527](https://openairdocs.org/sdr/SWIA201440527.md): Floor Panel · corroded · Dec 6, 2014 · N416SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT FLOOR PANEL FROM BS 409.128 - 559 HAS CORROSION. BLENDED CORROSION IAW REO.
- [SDR SWIA201440526](https://openairdocs.org/sdr/SWIA201440526.md): Floor Panel · corroded · Dec 6, 2014 · N416SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT FLOOR PANEL FROM BS 409.128 559 HAS CORROSION. REMOVED CORROSION IAW REO.
- [SDR SWIA201440525](https://openairdocs.org/sdr/SWIA201440525.md): Post · cracked · Dec 5, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128 VERTICAL POST AT LBL 18 INBD RADIUS CRACKED. INSTALLED A NEW VERTICAL POST ASSEMBLY IAW REO AND SRM.
- [SDR SWIA201440524](https://openairdocs.org/sdr/SWIA201440524.md): Post · cracked · Dec 5, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128 VERTICAL POST AT BL 0, CRACKED. INSTALLED A NEW POST ASSY IAW SRM AND REO.
- [SDR SWIA201440523](https://openairdocs.org/sdr/SWIA201440523.md): Bulkhead Web · cracked · Dec 5, 2014 · N416SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD WEB HAS ONE CRACK LOCATED AT LBL 18. INSTALLED A REPAIR IAW REO.
- [SDR SWIA201440522](https://openairdocs.org/sdr/SWIA201440522.md): Bulkhead Web · cracked · Dec 5, 2014 · N416SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD WEB HAS TWO CRACKS LOCATED AT BL 0. INSTALLED A REPAIR IAW REO.
- [SDR SWIA201440521](https://openairdocs.org/sdr/SWIA201440521.md): Bulkhead Web · cracked · Dec 5, 2014 · N416SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD WEB HAS ONE CRACK AT RBL 9.5. REPAIR DOUBLER, TRIPLER AND FILLER WERE FABRICATED AND INSTALLED IAW REO.
- [SDR SWIA201440520](https://openairdocs.org/sdr/SWIA201440520.md): Line · loose · Dec 5, 2014 · N416SW · Cndair CL6002B19 · Aircraft Fuel Distribution System
  > TWO MOTIVE FLOW LINES INSIDE THE FUEL PRESSURE BOX ARE LOOSE. REINFORCED THE FUEL LINES IN FUEL PRESSURE BOX IAW REO.
- [SDR SWIA201440519](https://openairdocs.org/sdr/SWIA201440519.md): Louver · loose · Dec 5, 2014 · N416SW · Cndair CL6002B19 · Cabin Cooling System
  > RIGHT RAM AIR EXHAUST DUCT HAS LOOSE LOUVERS. REPAIRED RIGHT ACM RAM AIR EXHAUST DUCT LOUVERS IAW REO.
- [SDR SWIA201440518](https://openairdocs.org/sdr/SWIA201440518.md): Louver · loose · Dec 4, 2014 · N416SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT RAM AIR EXHAUST DUCT HAS LOOSE LOUVERS. REPAIRED THE LEFT ACM RAM AIR EXHAUST DUCT LOUVERS, IAW REO.
- [SDR SWIA201440517](https://openairdocs.org/sdr/SWIA201440517.md): Floor Support · corroded · Dec 4, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT UPPER CAP BETWEEN BS 574 - 621 HAS CORROSION AT NUTPLATE LOCATIONS. INSTALLED NEW FLOOR SUPPORT CAP IAW SRM AND REO.
- [SDR SWIA201440516](https://openairdocs.org/sdr/SWIA201440516.md): Floor Support · corroded · Dec 4, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27, FLOOR SUPPORT UPPER CAP BETWEEN BS 574 - 621 HAS CORROSION AT NUTPLATE LOCATIONS. INSTALLED NEW FLOOR SUPPORT CAP IAW SRM AND REO.
- [SDR SWIA201440515](https://openairdocs.org/sdr/SWIA201440515.md): Seat Track · corroded · Dec 4, 2014 · N416SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK BETWEEN FS 559+112 AND FS 574 HAS CORROSION. C-CHECK, REPLACED SEAT TRACK AT LBL 9 FS 559+112 - FS574 IAW REO.
- [SDR SWIA201440514](https://openairdocs.org/sdr/SWIA201440514.md): Seat Track · corroded · Dec 4, 2014 · N416SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK AT BS 559+90 HAS CORROSION. REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA201440513](https://openairdocs.org/sdr/SWIA201440513.md): Seat Track · corroded · Dec 4, 2014 · N416SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK AT FS 615 HAS CORROSION AROUND FASTENERS. REPLACED SEAT TRACK AT LBL 9, FS 615 IAW REO.
- [SDR SWIA201440512](https://openairdocs.org/sdr/SWIA201440512.md): Striker · dented · Dec 3, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SEAL STRIKER REPAIR IN AFT UPPER CORNER IS BENT/DENTED. C-CHECK, R & R EXISTING REPAIR STRIP ON PAX DOOR SEAL STRIKER IN AFT UPPER CORNER IAW REO.
- [SDR SWIA201440511](https://openairdocs.org/sdr/SWIA201440511.md): Shroud · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Ailerons
  > LEFT LOWER AILERON SHROUD PANEL 599CB IS CHAFED. BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599CB IAW REO.
- [SDR SWIA201440510](https://openairdocs.org/sdr/SWIA201440510.md): Shroud · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Ailerons
  > LEFT LOWER AILERON SHROUD PANEL 599BB IS CHAFED. BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599BB IAW REO.
- [SDR SWIA201440509](https://openairdocs.org/sdr/SWIA201440509.md): Shroud · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Ailerons
  > LT LOWER AILERON SHROUD PANEL 599AB IS CHAFED., BLENDED CHAFE ON LT LOWER AILERON SHROUD PANEL 599AB IAW REO.
- [SDR SWIA201440508](https://openairdocs.org/sdr/SWIA201440508.md): Skin · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE, INBD OF INBD ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, INBD OF INBD ACTUATOR L/E SKIN IAW REO.
- [SDR SWIA201440507](https://openairdocs.org/sdr/SWIA201440507.md): Skin · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE, MIDWAY BETWEEN INBD AND CENTER ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, MIDWAY BETWEEN INBD AND CENTER ACTUATOR L/E SKIN IAW REO.
- [SDR SWIA201440506](https://openairdocs.org/sdr/SWIA201440506.md): Vane · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE, OTBD OF CENTER ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE ON LT INBD FLAP VANE, OTBD OF CENTER ACTUATOR L/E SKIN IAW REO.
- [SDR SWIA201440505](https://openairdocs.org/sdr/SWIA201440505.md): Vane · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE, BETWEEN OTBD AND CENTER ACTUATOR L/E SKIN CHAFED. C-CHECK, BLENDED CHAFE ON LT INBD FLAP VANE, BETWEEN OTBD AND CENTER ACTUATOR L/E SKIN IAW REO.
- [SDR SWIA201440504](https://openairdocs.org/sdr/SWIA201440504.md): Vane · chafed · Dec 2, 2014 · N416SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE, OTBD OF OTBD ACTUATOR L/E SKIN CHAFED. BLENDED CHAFE IAW REO.
- [SDR SWIA201440503](https://openairdocs.org/sdr/SWIA201440503.md): Panel · failed · Dec 1, 2014 · N416SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER VISOR PANEL 326BR RT LOWER. CONTOURED THE VISOR PANEL IAW REO.C.
- [SDR SWIA201440502](https://openairdocs.org/sdr/SWIA201440502.md): Panel · failed · Dec 1, 2014 · N416SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER VISOR PANEL 326BL, LT LOWER. CONTOURED THE VISOR PANEL IAW REO.
- [SDR SWIA201440501](https://openairdocs.org/sdr/SWIA201440501.md): Panel · failed · Dec 1, 2014 · N416SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER VISOR PANEL 326AR RT UPPER. CONTOURED THE VISOR PANEL IAW REO.
- [SDR SWIA201440500](https://openairdocs.org/sdr/SWIA201440500.md): Housing · gouged · Dec 1, 2014 · N416SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR EXTERIOR HANDLE HOUSING HAS A GOUGE. PAX DOOR EXTERIOR HANDLE HOUSING BLENDED OUT IAW EA.
- [SDR SWIA201440499](https://openairdocs.org/sdr/SWIA201440499.md): Skin · dented · Nov 30, 2014 · N416SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ONE DENT BS 654.5 - 672.2 S18-21L. COLDWORKED DENT TO ORIGINAL CONTOUR IAW EA.
- [SDR SWIA201439961](https://openairdocs.org/sdr/SWIA201439961.md): Frame · corroded · Nov 15, 2014 · N416SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME CORRODED. PAINT LIFTING AND BUBBLED AT STA 319 AND STRINGER 26 LT. REPAIRED IAW REO AND SRM.
- [SDR SWIA201438088](https://openairdocs.org/sdr/SWIA201438088.md): Bracket · loose · May 24, 2014 · N416SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT ENGINE HAS LOOSE 10TH STAGE BLEED DUCT ISOLATORS. C-CHECK, REPLACED ISOLATORS.

Next page: https://openairdocs.org/deregistered/N416SW-2019-02-04/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 = 'N416SW' AND deregistration_id = 'N416SW-2019-02-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N416SW-2019-02-04/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.