# Service difficulty reports: N75LV

A list on [N75LV](https://openairdocs.org/aircraft/N75LV.md).

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

- [SDR 2022FA0000463](https://openairdocs.org/sdr/2022FA0000463.md): None · inoperative · Aug 20, 2022 · N75LV · Beech B200 · Landing Gear System
  > RIGHT DOWN AND LOCKED MAIN LANDING GEAR INDICATION INOPERATIVE.
- [SDR 2021FA0000170](https://openairdocs.org/sdr/2021FA0000170.md): Wire · loose · Jun 12, 2021 · N75LV · Beech B200 · Electrical Power System Wiring
  > DURING CLIMB OUT FORM BASE PILOTS EXPERIENCED A PERCEIVED AN ELECTRICAL HOT ODOR. FLIGHT RETURNED TO BASE. TECHNICIANS TROUBLESHOT THE REPORTED ELECTRICAL ODOR AND FOUND THE OVERHEAD LIGHTING PANEL P.N. 100-364161-19 AND RIGHT CIRCUIT BREAKER LIGHTING PANEL
- [SDR HDNA20212601NW003](https://openairdocs.org/sdr/HDNA20212601NW003.md): Bearing · failed · Jan 26, 2021 · N75LV · Beech B200 · Landing Gear Actuator
  > DURING A CONTROLLED APPROACH WHEN THE LANDING GEAR WAS SELECTED DOWN THE GEAR UNSAFE LIGHT ILLUMINATED AND LANDING GEAR FAILED TO EXTEND. THE GEAR HANDLE WAS PLACED BACK IN THE RETRACTED POSITION AND THE GEAR UNSAFE LIGHT STAYED ILLUMINATED. THE PILOT COMPLI
- [SDR HDNA2020051300001](https://openairdocs.org/sdr/HDNA2020051300001.md): Uplock Switch · out of adjust · May 13, 2020 · N75LV · Beech B200 · Landing Gear Position and Warning
  > LANDING GEAR TRANSITION LIGHT STAYED ILLUMINATED AFTER LANDING GEAR WAS SELECTED UP.
- [SDR HDNA20191215001](https://openairdocs.org/sdr/HDNA20191215001.md): Skin · cracked · Dec 15, 2019 · N75LV · Beech B200 · Fuselage Main, Plate/Skin
  > FOUND DAMAGED WING-TO-FUSELAGE FILLET UNDER EMERGENCY EXIT. ONCE REMOVED, FOUND THAT SKIN-RH UPPER INBD CENTER SECTION L.E. (P/N 101-120017-11) HAD BEEN RUBBING ON THE FUSELAGE SKIN. FURTHER INSPECTION REVEALED A 1.75 INCH HORIZONTAL CRACK IN THE SKIN. THIS
- [SDR 2019F00208](https://openairdocs.org/sdr/2019F00208.md): Test Switch · worn · May 20, 2019 · N75LV · Beech B200 · Fire Bottle, Fixed
  > AS REPORTED BY THE PIC: WHILE IN FLIGHT NR 2 FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED IN FLIGHT. FIRE BOTTLE DID NOT DISCHARGE RETURNED TO BASE.
- [SDR HDNA2017030515](https://openairdocs.org/sdr/HDNA2017030515.md): Line · melted · Mar 5, 2017 · N75LV · Beech B200 · Engine Bleed Air System
  > PLASTIC TUBING "SENSE" LINE FOR BLEED AIR INDICATING ANNUNCIATION MELTED DUE TO IMPROPER ROUTING CAUSING THE BLEED AIR FAIL CAUTION TO ILLUMINATE.
- [SDR GNL2010F00000](https://openairdocs.org/sdr/GNL2010F00000.md): O-Ring · split · May 1, 2010 · N75LV · Beech B200 · Aircraft Fuel Distribution System
  > DURING A ROUTINE TRAINING FLIGHT, THE PILOT NOTICED THAT THE LT ENGINE TORQUE DROPPED FROM 2100 LBS TO 1600 LBS. HE INCREASED LT THROTTLE LEVER WITH NO RESPONSE NOTICED. HE LOOKED OUT THE SIDE WINDOW AND NOTICED WHAT SEEMED TO BE FUEL STREAMING FROM THE LT E
- [SDR 99ZZZX3298](https://openairdocs.org/sdr/99ZZZX3298.md): Compressor · seized · Jan 31, 1999 · N75LV · Beech B200 · Turbine Engine Compressor Section
  > COMPRESSOR LOCKED UP. REF: MCN NR 4.
- [SDR 98ZZZX182](https://openairdocs.org/sdr/98ZZZX182.md): Breaker · failed · Dec 1, 1997 · N75LV · Beech B200 · DC Power Distribution System
  > DUPLICATED A REPORTED FAILURE AND ISOLATED CIRCUIT BREAKERS ON NR 1 BUSS TO SHOW THAT THEY WERE FAULTY. INSTALLED 2 EACH NEW 50 AMP BREAKERS. FUNCTION CHECKED SATISFACTORY ON GROUND AND THEN PERFORMED MAINTENANCE FLIGHT CHECK. SUBMITTER STATED THE BREAKERS
- [SDR 97ZZZX1397](https://openairdocs.org/sdr/97ZZZX1397.md): Inverter · defective · Nov 16, 1996 · N75LV · Beech B200 · AC Inverter
  > AUTOPILOT DISCONNECTED, FOUND DEFECTIVE INVERTER.
- [SDR 96ZZZX5766](https://openairdocs.org/sdr/96ZZZX5766.md): Inverter · inoperative · Aug 17, 1996 · N75LV · Beech B200 · AC Inverter
  > INVERTER INOP. NO AC OUTPUT.
- [SDR 96ZZZX4671](https://openairdocs.org/sdr/96ZZZX4671.md): Tire · defective · Jun 2, 1996 · N75LV · Beech B200 · Tire
  > TIRE DEVEOPED BUMP. SUPSECT CORD SEPARATION.
- [SDR 95ZZZX3110](https://openairdocs.org/sdr/95ZZZX3110.md): Indicator · stuck · May 9, 1995 · N75LV · Beech B200 · Attitude Gyro and Indicating System
  > ADI STUCK IN PITCH AND RED FLAG 'ATT'. THIS IS SAME PROBLEM AS BEFORE.
- [SDR RMXA9520550](https://openairdocs.org/sdr/RMXA9520550.md): Tire · defective · Mar 26, 1995 · N75LV · Beech 200BEECH · Tire
  > HAS BUMP ON TIRE DUE TO CORD SEPARATION. THIS IS THE SECOND TIRE TO DO THIS. REMOVED AND REPAIRED.
- [SDR RMXA9520549](https://openairdocs.org/sdr/RMXA9520549.md): Tire · defective · Mar 26, 1995 · N75LV · Beech 200BEECH · Tire
  > KNOT ON TIRE (CORD SEPARATION) REMOVED AND REPLACED.

## 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 = 'N75LV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N75LV/reports

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