N5679X

Substantial
None

AERO COMMANDER S2RS/N: 1879R

Accident Details

Date
Tuesday, February 9, 2021
NTSB Number
CEN21LA133
Location
Alamo, TX
Event ID
20210223102661
Coordinates
26.153131, -98.135008
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The partial loss of engine power due to water-contaminated fuel.

Aircraft Information

Registration
Make
AERO COMMANDER
Serial Number
1879R
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
S2RL29
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
S2R

Registered Owner (Current)

Name
VANDERPOOL GARY W
Address
2919 UNLAND DR
City
ALAMO
State / Zip Code
TX 78516-7261
Country
United States

Analysis

On February 9, 2021, about 1730 central standard time, an Aero Commander S2R airplane, N5679X, was substantially damaged when it was involved in an accident near Alamo, Texas. The commercial pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

The pilot departed from Mid-Valley Dusters Inc. Airport (43TX) on the last flight of the day and noticed an abnormal sound from the engine as the airplane reached an altitude of about 25 ft above ground level. He elected to make an immediate precautionary landing rather than risk having the engine lose power over obstacles farther along the departure path that included a high traffic highway and a low power line. During the landing roll, both wings sustained substantial damage due to impact with trees.

Examination of engine cylinders, spark plugs, induction tubes, exhaust stacks, and magnetos did not reveal any anomalies that would have precluded normal operation. The fuel tank sumps, header tank sumps, and manual auxiliary fuel pump sumps were drained with no contamination noted. The rear carburetor bowl drain was removed, and a small amount of water-contaminated fuel was observed.

The engine was started and accelerated to 1,800 rpm with no anomalies noted. A normal rpm drop occurred when the magnetos were checked, and the propeller cycled normally. No smoke was produced when the engine was returned to idle power, which was consistent with normal functioning of the blower seal.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA133