# NTSB FTW93LA095: Beech 65-A90, N800VT, Midlothian, TX, March 5, 1993

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Limited investigation · Final report
- Date: March 5, 1993, 02:00 local (08:00 UTC)
- Place: Midlothian, TX
- Coordinates: 32.400424, -96.849128 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=32.4004&lon=-96.8491&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 5 uninjured
- Status: Completed, report October 25, 1993
- Report: Approved by Office Director
- NTSB case key (mKey): 18706
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=FTW93LA095
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/18706/pdf
- Page: https://openairdocs.org/ntsb/FTW93LA095

## Probable cause

THE LOSS OF ENGINE POWER AND THE PILOT'S FAILURE TO REFUEL. A FACTOR WAS THE INADVERTENT STALL DURING THE FLARE TOUCHDOWN

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- Loss of engine power(total) - nonmechanical, cruise - normal
  - all engines
  - fluid,fuel - exhaustion (cause)
  - refueling - not performed, pilot in command (cause)
- Forced landing, descent - emergency
- In flight collision with terrain/water, landing - flare/touchdown
  - stall - inadvertent, pilot in command (contributing factor)

## Analysis

DURING A CROSS COUNTRY FLIGHT AT NIGHT THE AIRPLANE EXPERIENCED A LOSS OF ENGINE POWER TO BOTH ENGINES WHILE CRUISING AT 6,000 FEET. THE FLIGHT ENCOUNTERED  HIGH HEADWINDS ALONG THEIR FLIGHT ROUTE. BOTH FUEL PUMPS LIGHTS ILLUMINATED PRIOR TO THE LOSS OF POWER. THE PILOT IDENTIFIED A LOCAL AIRPORT WITH ITS RUNWAY LIGHTS ILLUMINATED AND ATTEMPTED TO LAND. TOUCHDOWN WAS MADE 90 DEGREES FROM THE LONG AXIS OF THE RUNWAY. AN EXAMINATION OF THE AIRPLANE REVEALED 2 PINTS OF FUEL IN THE FUEL SYSTEM. A PASSENGER REPORTED HEARING THE STALL WARNING HORN PRIOR TO GROUND CONTACT. THE AIRPLANE CAME TO REST ABOUT 100 FEET FROM THE INITIAL IMPACT POINT

## Factual narrative

On March 5, 1993, at approximately 0200 central standard time a Beech      65 A90, N800VT, was substantially damaged following a forced landing near Midlothian, Texas. The airplane was owned by the Roever Evangelistic Association Incorporated and was on an instrument flight rules flight plan from Crestview, Florida, to Fort Worth, Texas. Neither the commercial pilot, the co pilot or his 3 passengers were injured.

The pilot reported to a Federal Aviation Administration (FAA) inspector that the airplane experienced a dual engine failure following the illumination of the left and right fuel boost pump at approximately 6,000 feet. He also reported that he was in contact with an FAA controller and informed him that he had the runway lights of the Midlothian airport in sight and entered a downwind leg at the Midlothian airport in an attempt to land. The pilot reported that he experienced high head winds enroute from Crestview, Florida, and was forced to fly at a lower altitude than he planned. Prior to departing Crestview the pilot stated that he added 140 gallons to the existing 160 gallons of jet fuel.

An examination of the accident scene by the FAA inspector revealed that the airplane impacted the ground 80 feet short of the runway and 90 degrees perpendicular to the runway intended for landing. The inspector measured the total distance from the initial impact to the final resting place; he determined it had travelled approximately 100 feet. During the impact the left main landing gear collapsed and was separated from the airplane and the right wing sustained damage. A passenger reported that prior to impact with the ground he heard the stall warning horn. The FAA inspector determined that there was no evidence of fuel spillage at the accident scene. An examination of the fuel system by the inspector revealed no usable fuel, however, a total of 2 pints of jet fuel was captured from both fuel supply systems.

The FAA inspector examined the airplane following the recovery and he found no fuel in any fuel cells or associated systems and no anomalies in the functional systems.

## Aircraft

- Registration: [N800VT](https://openairdocs.org/deregistered/N800VT-1995-12-07), registration cancelled 1995-12-07, S/N LJ249 (OpenAirDocs)
- Reported make and model: BEECH 65-A90
- Registry model: [Beech 65-A90](https://openairdocs.org/model/beech-65-a90) (registry code 1152908) (OpenAirDocs)
- Category: Airplane
- Serial number: LJ-249
- Airframe hours: 8375
- Engines: P&W PT6-20 550 horsepower turbo prop
- Damage: Substantial damage
- Flight: Executive/Corporate, Part 91
- Operator: Roever Evangelistic
- Registered owner: Roever Evangelistic
- Airworthiness certificate: Standard, Normal
- Last inspection: Continuous airworthiness, January 20, 1993, 59 hours before
- Departed: CEW, CRESTVIEW, FL
- Destination: FTW, FORT WORTH, TX
- Flight plan: IFR
- Airport: 4T6, Midlothian, runway 36, 5,000 × 75 ft, concrete

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 49; airline transport, flight instructor; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, valid medical--w/ waivers/lim; seat: left; flight hours: 5,148 total, 156 in this make and model, 4,566 as pilot in command, 98 in the last 90 days, 52 in the last 30 days, 4 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Night/dark
- Wind: 320° at 12 knots
- Visibility: 7 statute miles
- Lowest ceiling: none
- Temperature: 45 °F, dew point 37 °F
- Altimeter: 30.00 inHg

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 19930305004339A](https://openairdocs.org/incident/19930305004339A), Mar 5, 1993: Beech 65A90, Midlothian/Waxa, TX, Substantial damage. Both engines quit near destination. Diverted but landed off airport from base leg. No fuel onboard.

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.

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