# Accident 19920606018419A: Beech V35B, Panguitch, UT, June 6, 1992

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: June 6, 1992, 18:00 local time
- Place: Panguitch, UT
- Airport: Panguitch Municipal Airport
- Damage: Substantial damage
- Phase of flight: Forced Landing
- Operating rules: General operating rules (Part 91)
- Location: 37.8610° N, 112.3390° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=37.8610&lon=-112.3390&mi=10
- Aircraft: N9035V, a cancelled registration (https://openairdocs.org/deregistered/N9035V-2014-11-20) (OpenAirDocs)
- Registry model: Beech V35B (registry code 1151548, https://openairdocs.org/model/beech-v35b) (OpenAirDocs)
- Registry engine: Continental IO-520 series (registry code 17032, https://openairdocs.org/engine/continental-io-520-series) (OpenAirDocs)
- Reported make and model: BEECH V35B
- Reported engine: LYC TIO540J2BD
- People aboard: 1
- Fatal injuries: 0
- Pilot flight hours: 2,490 total, 1,327 in this make and model, 102 in the last 90 days
- NTSB investigation: [NTSB SEA92LA120](https://openairdocs.org/ntsb/SEA92LA120) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19920606018419A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

LOST POWER ON BASE LEG WHILE LANDING. NOSE GEAR FAILED LANDING SHORT. FOUND. BARE IGNITION HARNESS GROUNDED SYSTEM.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA92LA120](https://openairdocs.org/ntsb/SEA92LA120), Jun 7, 1992: Beech V35B (N9035V), Panguitch, UT, substantial damage. Probable cause: SHORTING OF THE GROUNDING WIRE (P LEAD) TO THE MAGNETOS FOLLOWED BY OVERLOADING OF THE NOSE WHEEL STRUT. A FACTOR CONTRIBUTING TO THE ACCIDENT WAS: ROUGH/UNEVEN TERRAIN.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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