FTW03LA070

NTSB accident investigation · Cessna T207 · Brownsville, TX · December 30, 2002

Accident · No injuriesLimited investigationFinal report
Date
December 30, 2002, 14:40 local (20:40 UTC)
Place
Brownsville, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N1599UCessna T207
Weather
Visual (VMC) · Day
Status
Completed · report June 2, 2004
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20021230035879A
Case key
56263

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerClimb - to cruise
Engine assembly,crankshaft - separationCause
Forced landingEmergency descent/landing
On ground/water collision with objectEmergency landing
Terrain condition - none suitableFactor

Analysis

The 2,900-hour pilot stated that the airplane lost engine power during climb to cruise. The pilot went through the emergency procedures, and made about a 130 degree left turn for the best place to land. Post examination of the engine revealed that the crankshaft was found to be separated between the number 2 and 3 journals. It had no heat discoloration.

Factual narrative

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.

Aircraft

Registration
N1599U
Reported as
Cessna T207
Category
Airplane
Serial number
20700199
Airframe hours
9,568.6
Engine
Continental TSIO-520-M, 310 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Alexandru Neacsu
Registered owner
Comercializadora Cano Inc.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 7, 2002 · 116.3 hours before
Departed
BRO · Brownsville, TX
Destination
TAM · Tampico
Flight plan
VFR
Airport
BRO · Brownsville/South Padre Island, runway 17, 6,000 × 150 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
45
Injuries
None
Certificates
Airline transport, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Last flight review
April 17, 2002
Seat
Left
Flight hours
2,900 total · 500 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 23 knots, gusting 27
Visibility
6 statute miles
Lowest ceiling
1,600 ft broken
Temperature
75 °F, dew point 70 °F
Altimeter
29.68 inHg
Observed at
BRO, 4 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.