N26934

Substantial
Serious

Grumman AA-5A S/N: AA5A 0820

Accident Details

Date
Sunday, September 10, 2000
NTSB Number
ATL00LA089
Location
ST. AUGUSTINE, FL
Event ID
20001212X21907
Coordinates
29.760677, -81.299285
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
3
Minor Injuries
0
Uninjured
0
Total Aboard
3

Probable Cause and Findings

The loss of engine power due to fuel system contamination.

Aircraft Information

Registration
N26934
Make
GRUMMAN
Serial Number
AA5A 0820
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
AA-5A AA5
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TRIFILENTTI JOHN J
Address
3452 N RIDE CIR S
Status
Deregistered
City
JACKSONVILLE
State / Zip Code
FL 32223
Country
United States

Analysis

On September 10, 2000, at 1815 eastern daylight time, a Grumman AA-5A, N26934, collided with the ground during a forced landing at the St. Augustine Airport in St. Augustine, Florida. The personal flight was operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage. The private pilot and her two passengers received serious injuries. The accident occurred during the takeoff from St. Augustine, Florida, at 1814.

The private pilot reported that the engine sputtered shortly after takeoff from runway 13 as the airplane climbed through 100 feet. The pilot then stated that she switched the fuel selector from the right tank to the left tank. The pilot reported a complete loss of engine power. The pilot elected to make a forced landing on the remaining runway. The airplane subsequently collided with the runway during touchdown, and skidded off the runway. The airplane came to rest in a marshy area several hundred feet left of the runway centerline.

Examination of the airframe and the engine assembly failed to disclose a mechanical malfunction or component failure. During the subsequent examination, necessary repairs were made to the engine assembly to facilitate a functional check. The engine operated normally up to 2100 rpm during the functional check. The post-crash examination of the airplane also revealed evidence of rust and water in the fuel boost pump.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL00LA089