N4856Q

Substantial
Minor

CESSNA 188 S/N: 18802592T

Accident Details

Date
Tuesday, April 12, 1994
NTSB Number
ATL94LA080
Location
LATTA, SC
Event ID
20001206X01029
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

THE PILOT'S FAILURE TO OBTAIN FLYING SPEED AND THE PREMATURE LIFT OFF WHICH RESULTED IN A STALL.

Aircraft Information

Registration
N4856Q
Make
CESSNA
Serial Number
18802592T
Engine Type
Reciprocating
Model / ICAO
188 C188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TAYLOR LORETTA J DBA
Address
RR 1 BOX 128
Status
Deregistered
City
SELLERS
State / Zip Code
SC 29592
Country
United States

Analysis

On April 12, 1994, at 1515 eastern daylight time, a Cessna 188, N4856Q, collided with the ground during takeoff from a private airstrip near Latta, South Carolina. The aerial application flight operated under 14 CFR Part 137 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage; the pilot received minor injuries. The flight departed Latta at 1514 hours.

The initial reports of the accident stated that during takeoff roll, when the pilot rotated for liftoff, the airplane settled back on the 1800 foot long sod runway twice. It was further reported that the airplane became airborne, a wing struck the ground and the airplane cartwheeled through a field off the departure end of the runway. According to the Federal Aviation Administration Safety Inspector, the aircraft was loaded with 120 gallons of chemicals and the chemicals remained onboard throughout the sequence of events.

A subsequent report from the pilot stated that the engine lost power shortly after liftoff from a private airstrip. As the pilot maneuvered the airplane for a forced landing, he lost control of the airplane and collided with the ground. The subsequent examination of the airplane failed to disclose a mechanical problem. During the functional check of the engine, the engine was started using the aircraft fuel boost pump and installed systems. An engine speed of 1800 rpm was attained with normal acceleration noted (see attached FAA Inspector's Statement).

The pilot/operator failed to complete an NTSB Form 6120.1/2 provided by the NTSB.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL94LA080