# Service difficulty reports: N131FL

A list on [N131FL](https://openairdocs.org/aircraft/N131FL.md).

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

- [SDR VGCA20150428013](https://openairdocs.org/sdr/VGCA20150428013.md): Doubler · corroded · Apr 28, 2015 · N131FL · Cvac 580 · Cargo/Baggage Doors
  > FOUND CORROSION ON AFT CARGO DOOR ACTUATOR DOUBLER.
- [SDR VGCA20150428012](https://openairdocs.org/sdr/VGCA20150428012.md): Angle · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Cargo/Baggage Doors
  > REPLACED CRACKED CARGO DOOR ACTUATOR MOUNT ANGLES.
- [SDR VGCA20150428011](https://openairdocs.org/sdr/VGCA20150428011.md): Hinge · corroded · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage, Door Hinge
  > FOUND CORROSION ON CARGO DOOR HINGE. REPLACED DOOR HINGE.
- [SDR VGCA20150428010](https://openairdocs.org/sdr/VGCA20150428010.md): Stringer · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Main, Longeron/Stringer
  > STRINGER 30 CRACKED AT STATION 661.
- [SDR VGCA20150428009](https://openairdocs.org/sdr/VGCA20150428009.md): Structure · corroded · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Miscellaneous Structure
  > FOUND STRINGER TO SKIN CORROSION AT RT FS 210 - 227.
- [SDR VGCA20150428008](https://openairdocs.org/sdr/VGCA20150428008.md): Stringer · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Wing, Longeron/Stringer
  > RIGHT WING STRINGER IN DRY BAY BETWEEN RIB 0 - 1 CRACKED.
- [SDR VGCA20150428004](https://openairdocs.org/sdr/VGCA20150428004.md): Stringer · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Wing, Longeron/Stringer
  > RIGHT WING STRINGER IN DRY BAY BETWEEN RIB 0 - 1 CRACKED.
- [SDR VGCA20150428007](https://openairdocs.org/sdr/VGCA20150428007.md): Structure · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Miscellaneous Structure
  > FOUND CRACKS IN NOSE WW AT STATION 26 RT.
- [SDR VGCA20150428006](https://openairdocs.org/sdr/VGCA20150428006.md): Structure · corroded · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AROUND RT PRESS VESSEL ELEC PASS THROUGH.
- [SDR VGCA20150428005](https://openairdocs.org/sdr/VGCA20150428005.md): Longeron · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Main, Longeron/Stringer
  > LEFT SLIDING WINDOW LONGERON CRACKED.
- [SDR VGCA201504280004](https://openairdocs.org/sdr/VGCA201504280004.md): Skin · corroded · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Main, Plate/Skin
  > REMOVED PREVIOUS REPAIR BETWEEN STRINGERS 15 - 16 DUE TO CORROSION. CLEANED CORROSION, PRIMED, RESEALED & REINSTALLED.
- [SDR VGCA20150428003](https://openairdocs.org/sdr/VGCA20150428003.md): Structure · corroded · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Miscellaneous Structure
  > REMOVED PREVIOUS REPAIR BETWEEN STRINGERS 18 - 19 DUE TO CORROSION. CLEANED CORROSION, PRIMED, RESEALED & REINSTALLED.
- [SDR VGCA20150428002](https://openairdocs.org/sdr/VGCA20150428002.md): Rib · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Wing, Rib/Bulkhead
  > LEFT WING DRY BAY RIB 2 CRACKED.
- [SDR VGCA20150428001](https://openairdocs.org/sdr/VGCA20150428001.md): Longeron · cracked · Apr 28, 2015 · N131FL · Cvac 580 · Fuselage Main, Longeron/Stringer
  > LEFT SLIDING WINDOW LOWER LONGERON FRAME STATION 64 IS CRACKED.
- [SDR VGCA20130403001](https://openairdocs.org/sdr/VGCA20130403001.md): Spar · corroded · Apr 3, 2013 · N131FL · Cvac 580 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER LWR REAR SPAR CORRODED.
- [SDR VGCA20130312001](https://openairdocs.org/sdr/VGCA20130312001.md): Regulator · damaged · Mar 12, 2013 · N131FL · Cvac 340CVAC · Engine (Turbine/Turboprop)
  > NR 2 ENGINE RPM FLUCTUATION IN FLIGHT. FOUND REGULATOR DAMAGED.
- [SDR VGC2009F00000](https://openairdocs.org/sdr/VGC2009F00000.md): Spar · corroded · Mar 15, 2009 · N131FL · Cvac 340CVAC · Horizontal Stabilizer, Spar/Rib
  > CORROSION ON LT HORIZONTAL STABILIZER REAR SPAR. (K)
- [SDR 2006002](https://openairdocs.org/sdr/2006002.md): Clamp · failed · Aug 25, 2006 · N131FL · Cvac 340CVAC · Engine Collector/Tailpipe/Nozzle
  > EXHAUST CLAMP FAILURE.
- [SDR VGC2005F00000](https://openairdocs.org/sdr/VGC2005F00000.md): Element · chafed · Dec 22, 2004 · N131FL · Cvac 340CVAC · Fire Detection
  > AFTER DEPARTING SDF CLIMBING THROUGH 8500 FT, NR 2 ENGINE ZONE 2, FIRE INDICATION LIGHT ILLUMINATED. CREW PERFORMED CHECKLISTS (IE PERFORMED ENGINE SHUTDOWN) AS REQUIRED AND RETURNED TO SDF. CREW REPORTED THAT NO VISUAL INDICATIONS OF FIRE, AND AFTER ENGINE

## 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 = 'N131FL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N131FL/reports

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