N2007C

Substantial
None

BEECH C24R S/N: MC-594

Accident Details

Date
Saturday, August 19, 1995
NTSB Number
FTW95LA354
Location
MINEOLA, TX
Event ID
20001207X04253
Coordinates
32.659191, -95.480079
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

THE PILOT'S INADEQUATE PREFLIGHT PLANNING/PREPARATION, AND HIS FAILURE TO OBTAIN THE REQUIRED AIRCRAFT PERFORMANCE DATA FOR THE FLIGHT. A FACTOR WAS THE HIGH DENSITY ALTITUDE.

Aircraft Information

Registration
N2007C
Make
BEECH
Serial Number
MC-594
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
C24R BE24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BROOKS NEAL S
Address
1520 ROBIN ST
Status
Deregistered
City
MINEOLA
State / Zip Code
TX 75773-1113
Country
United States

Analysis

On August 19, 1993, at 1130 central daylight time, a Beech C24R, N2007C, was substantially damaged during takeoff from the Mineola Wisener Field near Mineola, Texas. The commercial pilot and his three passengers were not injured. The aircraft was being operated as a personal flight under Title 14 CFR Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the planned cross country flight to Sulphur Springs, Texas.

According to the pilot, following an engine run up, a takeoff was attempted from Runway 35 with the flaps set at 10 degrees. The pilot added that after rotation, the airplane became airborne and attained an altitude of 15 to 20 feet above the runway. During a telephone interview, the pilot further stated that "he did not think that the airplane was going to clear the 80 foot trees at the departure end of the 3,197 foot runway, so he elected to abort the takeoff."

Subsequently, the airplane touched down hard on the left main landing gear, collapsing the gear. Control was lost and the airplane departed the left side of the runway. Damage was sustained by the leading edge and underside of the left wing, and the engine mounts and firewall.

Weight and balance calculations were performed using figures provided by the pilot. At the time of the accident, the airplane was found to be 188 pounds below its maximum weight for takeoff. The pilot did not check the aircraft performance data prior to departure, since he had "previously made similar flights in the same aircraft configuration."

On the enclosed NTSB Form 6120.1/2, the pilot describes the weather as "humid and hot." The density altitude was calculated at 3,200 feet.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA354