# Service difficulty reports: N809TA

A list on [N809TA](https://openairdocs.org/aircraft/N809TA.md).

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

- [SDR 2021F00104](https://openairdocs.org/sdr/2021F00104.md): Overheat Sensor · dirty · May 4, 2021 · N809TA · Boeing 737209 · Overheat Detection
  > IN FLIGHT, CREW HAD WHEEL WELL OVERHEAT LIGHT AS WELL AS MASTER FIRE WARNING LIGHTS ILLUMINATE. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS EXTENDED. UPON LANDING, MAINTENANCE INSPECTION DETERMINED OVERHEAT SENSING LOOP CONNECTION WAS DIRTY, CLEANED AND PERFORME
- [SDR FY4Y202009118008](https://openairdocs.org/sdr/FY4Y202009118008.md): Skin · corroded · Sep 1, 2020 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT LT WING BOTTOM SKIN LOWER SURFACE AT WS 475 TO WS 525.
- [SDR FY4Y202008013](https://openairdocs.org/sdr/FY4Y202008013.md): Battery · failed · Aug 28, 2020 · N809TA · Boeing 737209 · Emergency Lighting
  > EMERGENCY LIGHT INOPERABLE ON FWD ENTRY DOOR AND FWD GALLEY SERVICE DOOR.
- [SDR FY4Y202008012](https://openairdocs.org/sdr/FY4Y202008012.md): Battery · inoperative · Aug 28, 2020 · N809TA · Boeing 737209 · Emergency Lighting
  > EMERGENCY LIGHT INOPERABLE ON FWD ENTRY DOOR AND FWD GALLEY SERVICE DOOR.
- [SDR FY4Y2020009118007](https://openairdocs.org/sdr/FY4Y2020009118007.md): Skin · corroded · Aug 28, 2020 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT AT LT WING BOTTOM SKIN LOWER SURFACE AT WS 315 TO WS 475.
- [SDR FY4Y202009118006](https://openairdocs.org/sdr/FY4Y202009118006.md): Skin · corroded · Aug 28, 2020 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > CORROSION WAS FOUND AT LT WING BOTTOM SKIN LOWER SURFACE AT INBOARD TO WS 195.
- [SDR FY4Y202009118005](https://openairdocs.org/sdr/FY4Y202009118005.md): Spar · corroded · Aug 26, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 135.
- [SDR FY4Y202009108002](https://openairdocs.org/sdr/FY4Y202009108002.md): Frame · corroded · Aug 26, 2020 · N809TA · Boeing 737209 · Fuselage Main, Frame
  > CORROSION WAS FOUND AT AFT CARGO FWD BULKHEAD LOWER CHORD AT BS 727 BETWEEN S-25L AND 25R.
- [SDR FY4Y202009118011](https://openairdocs.org/sdr/FY4Y202009118011.md): Lug · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Horizontal Stabilizer Structure
  > CORROSION WAS FOUND AT FWD & AFT SURFACE OF RT SIDE HORIZONTAL STABILIZER REAR SPAR UPPER LUG.
- [SDR FY4Y202009118010](https://openairdocs.org/sdr/FY4Y202009118010.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT RT WING FRONT SPAR LOWER CHORD AT FSS 442.3.
- [SDR FY4Y202009118009](https://openairdocs.org/sdr/FY4Y202009118009.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT RT WING FRONT SPAR LOWER CHORD AT FSS 416.8.
- [SDR FY4Y202009118004](https://openairdocs.org/sdr/FY4Y202009118004.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 422.
- [SDR FY4Y202009118003](https://openairdocs.org/sdr/FY4Y202009118003.md): Spar · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Wing Spar
  > CORROSION WAS FOUND AT LT WING LEADING EDGE FRONT SPAR LOWER CHORD HORIZONTAL LEG AT FSS 307.
- [SDR FY4Y202009108001](https://openairdocs.org/sdr/FY4Y202009108001.md): Keelbeam · corroded · Aug 25, 2020 · N809TA · Boeing 737209 · Fuselage Main, Keel
  > CORROSION WAS FOUND AT KEEL BEAM LOWER CHORD AT AFT CARGO BS 727 S-27L (LENGTH: 3" WIDTH: 1"). REFER TO NRC CA1174-02-010.
- [SDR JRAA2017081100446](https://openairdocs.org/sdr/JRAA2017081100446.md): Skin · corroded · Nov 10, 2016 · N809TA · Boeing 737209 · Wing, Plate/Skin
  > DURING A C1 CHECK, FOUND THE LEFT WING UPPER SURFACE WAS CORRODED ON REAR SPAR BETWEEN WS 150 - 205. CORROSION WAS BLENDED OUT BEYOND SRM LIMIT. REPAIRED IAW DOCUMENT ROO3 REV 01.
- [SDR JRAA2017081100445](https://openairdocs.org/sdr/JRAA2017081100445.md): Skin · corroded · Oct 31, 2016 · N809TA · Boeing 737209 · Fuselage Main, Plate/Skin
  > DURING INSPECTION IAW CARD 53-30-00-101, FOUND FUSELAGE SKIN AT BS 1016 BETWEEN STRINGERS 24R - 25R WAS CORRODED. A REPAIR WAS CARRIED OUT IAW DOCUMENT 2016R002.
- [SDR 2017FA0000444](https://openairdocs.org/sdr/2017FA0000444.md): Skin · corroded · Oct 29, 2016 · N809TA · Boeing 737209 · Fuselage Main, Plate/Skin
  > DURING A C1 CHECK, IAW TASK CARD 53-30-00-101, FOUND A CRACK ON FUSELAGE SKIN AT BS 937, STRINGER 24L. REPAIRED IAW REPAIR PLAN DOCUMENT 2016R001.
- [SDR 2017FA0000443](https://openairdocs.org/sdr/2017FA0000443.md): Stringer Fitting · corroded · Oct 7, 2016 · N809TA · Boeing 737209 · Fuselage Main, Longeron/Stringer
  > DURING A C1 CHECK, DURING INSPECTION IAW TASK CARD53-88-80-101, FOUND BS 1016 STRINGER 17R FITTING CORRODED. THE STRINGER FITTING WAS REPLACED IAW ENGINEERING AUTHORIZATION B737-53-00-8.

## 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 = 'N809TA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N809TA/reports

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