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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

May 12, 1993 · Elliott B-80 · N42845

Amarillo, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 12, 1993
Injury Outcomes
No injuries (1 uninjured)
Location
Amarillo, TX
Aircraft
Elliott B-80
Tail Number
N42845
Operator
Benningfield Johnnie L
Injuries
None
Aircraft Damage
Destroyed
NTSB Number
FTW93LA152

DURING A DEPARTURE FROM A LOCAL AIRFIELD THE ENGINE LOST POWER AND THE PILOT EXECUTED A FORCED LANDING. DURING THE FORCED LANDING THE PILOT ATTEMPTED TO RETURN TO THE RUNWAY ENVIRONMENT. THE PILOT POSITIONED THE AIRCRAFT FOR LANDING WITH A 22 KNOT TAILWIND THAT WAS GUSTING TO 28 KNOTS. DURING THE POST ACCIDENT INVESTIGATION THE THROTTLE CABLE WAS FOUND TO HAVE FAILED AT THE THROTTLE ARM. THE FAILED CABLE CAUSED THE ENGINE TO GO TO AN IDLE CONDITION

NTSB Probable Cause

THE PILOT'S FAILURE TO COMPENSATE FOR WIND CONDITIONS. FACTORS WERE THE LOSS OF ENGINE POWER AND THE TAILWIND

Full Narrative

On May 12, 1993, at 1730 central daylight time (CDT) an Elliott B 80, N42845, was destroyed on ground impact, following a forced landing. The airline transport rated pilot, also the owner, was not injured. Weather for the local area flight was visual meteorological conditions. The pilot reported on the enclosed report and during an interview with a Federal Aviation Administration (FAA) inspector, that during his initial climb on a down wind leg the engine lost power. He further reported that he executed a forced landing and attempted to return to the runway. During the attempt to return to a runway environment the pilot positioned his aircraft for landing with a tailwind of 20 knots, with gusts to 28. An examination of the aircraft revealed that the throttle cable had disconnected from the throttle arm. Design specifications revealed that the engine would go to an idle situation.

Flight

Event TypeAccident
Event Time17:30 CDT
Nearest Airport0nm N
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftElliott B-80
Tail NumberN42845
Aircraft CategoryGyro
DamageDestroyed
OperatorBenningfield Johnnie L
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsSubaru · Reciprocating · 110
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 50 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind20° @ 22 kt, gusting 28 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point70 F / 46
Altimeter30.00 inHg
Weather SourceWIT

Appendix: Source Data