N8485R

Substantial
None

PIPER PA-28-140S/N: 28-22395

Accident Details

Date
Saturday, November 8, 2008
NTSB Number
CEN09LA055
Location
Nacogdoches, TX
Event ID
20081112X43029
Coordinates
31.629516, -94.739624
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N8485R
Make
PIPER
Serial Number
28-22395
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
PA-28-140P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
JETER TIMOTHY L
Address
2620 CENTER RD
Status
Deregistered
City
NACOGDOCHES
State / Zip Code
TX 75961-5403
Country
United States

Analysis

On November 8, 2008, approximately 1000 central daylight time, a single-engine, Piper 140 airplane, N8485R, was substantially damaged during a forced landing following a loss of engine power, shortly after takeoff from the AL Mangham Jr. Regional Airport (KOCH), Nacogdoches, Texas. The airline transport rated pilot and flight instructor were not injured. The airplane was registered and operated by a private individual. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91, flight.

According to the flight instructor and airline transport pilot, they were performing a flight review. After about an hour of conducting several flight maneuvers, they proceeded to do a power-off landing. During the take-off from runway 18, the engine lost partial power and when it appeared that they would not be able to clear trees, they elected to conduct a forced landing. A Federal Aviation Administration (FAA) Inspector, who examined the airplane, reported that during the forced landing the airplane sustained substantial damage to the left wing.

The aircraft was recovered to a hangar. The flight instructor and FAA Inspector inspected the throttle and mixture controls before deciding to run the airplane's engine. The engine was started and allowed to warm briefly, before conducting a magneto check at 2,000-rpm. The magneto check was "good"; however, when the carburetor heat control was pulled, the engine started to run rough and not able to maintain 2,000-rpm. The reason for the loss of engine power was not identified.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09LA055