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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 14, 1995 · Grumman-Schweizer G-164A · N9506

Joes, CO

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 14, 1995
Injury Outcomes
No injuries (1 uninjured)
Location
Joes, CO
Aircraft
Grumman-Schweizer G-164A
Tail Number
N9506
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW95LA202

WHILE PERFORMING AN AERIAL APPLICATION FLIGHT, A TOTAL LOSS OF POWER OCCURRED. THE PILOT CONDUCTED A FORCED LANDING IN A SOFT FIELD. DURING LANDING ROLL, THE AIRCRAFT NOSED OVER. EXAMINATION OF THE AIRCRAFT PROVIDED EVIDENCE OF FUEL EXHAUSTION. EXAMINATION OF THE FUEL SYSTEM PROVIDED EVIDENCE THAT THE FUEL GAUGE INDICATED 15 GALLONS WHEN THE TANKS WERE EMPTY.

NTSB Probable Cause

A TOTAL LOSS OF POWER DUE TO FUEL EXHAUSTION. FACTORS WERE: A MALFUNCTION IN THE FUEL MEASURING SYSTEM, THE PILOT'S FAILURE TO PERFORM FUEL CONSUMPTION CALCULATIONS, AND SOFT AND UNSUITABLE TERRAIN FOR A FORCED LANDING.

Full Narrative

On May 14, 1995, at 1100 mountain daylight time, a Grumman/Schweizer G-164A, N9506, was substantially damaged during a forced landing, approximately 14 miles north of Joes, Colorado. The pilot was not injured. Visual meteorological conditions prevailed for this 14 CFR Part 137 flight. No flight plan was filed. The pilot stated that the engine quit while on an aerial application run and he conducted a forced landing in a soft field. The aircraft nosed over during landing roll. Examination of the aircraft by a repair facility provided information that the engine quit due to fuel exhaustion. Examination of the fuel system by the repair facility provided evidence that the fuel gauge, which is a float type gauge, read 15 gallons when the tanks were empty. The pilot provided information that the fuel gauge and measuring system components were original equipment and had approximately 5,311 hours in service with no overhaul, which is not required. The pilot also provided information that he had not conducted any fuel consumption calculations and relied on his fuel gauge.

Flight

Event TypeAccident
Event Time11:00 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGrumman-Schweizer G-164A
Tail NumberN9506
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsP&W · R-1340 · Reciprocating · 600
Seats1

People & Injuries

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

Conditions

ConditionsVMC
LightDaylight
Wind140° @ 3 kt
Visibility10 sm
CeilingOvercast 2000 ft
Temperature / Dew Point63 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data