N1599U

Substantial
None

Cessna T207S/N: 20700199

Accident Details

Date
Monday, December 30, 2002
NTSB Number
FTW03LA070
Location
Brownsville, TX
Event ID
20030107X00024
Coordinates
25.920444, -97.480140
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of engine power due to the separation of the crankshaft. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N1599U
Make
CESSNA
Serial Number
20700199
Engine Type
Turbo-shaft
Year Built
1971
Model / ICAO
T207C07T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
FR SKYDIVE INC
Address
1323 CHOPTANK RD
Status
Deregistered
City
MIDDLETOWN
State / Zip Code
DE 19709
Country
United States

Analysis

On December 30, 2002, at 1440 central standard time, a Cessna T207 single-engine airplane, N1599U, was substantially damaged during a forced landing following a loss of engine power during climb to cruise from the Brownsville/South Padre Island International Airport (BRO) near Brownsville, Texas. The airplane was registered to and operated by Comercializadora Cano, Inc., of Brownsville. The airline transport pilot, sole occupant, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulation Part 91 personal flight. The flight originated from BRO at 1435, and was destined for Tampico, Mexico.

On the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the 2,900-hour pilot stated that about 3.5 miles south of BRO, while climbing through 950 feet AGL, lost engine power, went through the emergency procedures, and made about a 130 degree left turn to attempt to reach a suitable place to land.

Examination of the airplane, by the FAA inspector who responded to the accident site, revealed that the right main landing gear had collapsed, the right wing spar and right horizontal stabilizer sustained damage, and fuselage bulkheads were buckled.

Post examination of the 310-horsepower Continental TSIO-520-M engine (serial number 513430) revealed that the crankshaft was separated between the number 2 and 3 journals. No evidence or signs of heat discoloration was found.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW03LA070