# Accident 19930807028329A: Amtr GLASAIR, Blanding, UT, August 7, 1993

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: August 7, 1993, 14:20 local time
- Place: Blanding, UT
- Damage: Destroyed
- Phase of flight: Fcd/Prec Ldg From Cruise
- Operating rules: General operating rules (Part 91)
- Location: 37.5694° N, 110.3205° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=37.5694&lon=-110.3205&mi=10
- Aircraft: N365WB, a cancelled registration (https://openairdocs.org/deregistered/N365WB-2013-06-07) (OpenAirDocs)
- Registry model: Brauch Walter GLASAIR (registry code 05655JL, https://openairdocs.org/model/brauch-walter-glasair) (OpenAirDocs)
- Registry engine: Amateur-built UNKNOWN ENG (registry code 99999, https://openairdocs.org/engine/amateur-built-unknown-eng) (OpenAirDocs)
- Reported make and model: AMTR GLASAIR
- Reported engine: LYC IO360A1B
- People aboard: 2
- Fatal injuries: 2
- Pilot flight hours: 30,000 total, 83 in this make and model
- NTSB investigation: [NTSB SEA93LA174](https://openairdocs.org/ntsb/SEA93LA174) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19930807028329A

## Narrative

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

ENGINE QUIT EN ROUTE AFTER TOPPING FUEL TANKS. CRASHED IN ROUGH TERRAIN. FUEL FOR 4HRS. FUEL LINE CONNECTORS LOOSE.

## 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 SEA93LA174](https://openairdocs.org/ntsb/SEA93LA174), Aug 7, 1993: Brauch Glasair (N365WB), Blanding, UT, destroyed, 2 fatal. Probable cause: THE LOSS OF ENGINE POWER RESULTING FROM INADEQUATE MAINTENANCE INSPECTION BY THE PILOT, A LEAK FROM LOOSE FUEL SYSTEM LINE FITTINGS, AND FUEL EXHAUSTION. A FACTOR RELATING TO THE ACCIDENT WAS THE…

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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