N731MB

Substantial
Minor

CESSNA A188BS/N: 18802991T

Accident Details

Date
Saturday, July 25, 2015
NTSB Number
ERA15LA281
Location
Albertson, NC
Event ID
20150725X03453
Coordinates
35.120277, -77.784721
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot’s failure to maintain clearance from wires during takeoff due to his impairment from alcohol use.  

Aircraft Information

Registration
N731MB
Make
CESSNA
Serial Number
18802991T
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
A188BC188
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AERIAL SPRAYING SERVICE INC
Address
265 SHELTON HARDY LN
Status
Deregistered
City
ALBERTSON
State / Zip Code
NC 28508-9488
Country
United States

Analysis

On July 25, 2015, about 0815 eastern daylight time, a Cessna A188B, N731MB, was substantially damaged when it was involved in an accident near Albertson, North Carolina. The commercial pilot sustained minor injuries. The flight was conducted as a Title 14 Code of Federal Regulations Part 137 agricultural application flight.

The pilot stated that he was departing with full fuel tanks and 105 gallons of spray mixture, which was a lighter load than the previous day. A preflight inspection and engine run-up revealed no anomalies, and the pilot initiated the takeoff from the turf runway with the wing flaps extended 10°. The airplane lifted off the runway about 70 mph, and at 85 mph, the pilot established a "shallow" climb. He stated that as the airplane neared the end of the runway, it began to lose altitude. The left main landing gear impacted a power line and the airplane subsequently descended into terrain, resulting in substantial damage to the wings and fuselage.

A law enforcement officer who responded to the accident noticed the smell of alcohol around the pilot and performed a breathalyzer test about 45 minutes after the accident. The result was a blood alcohol content (BAC) of 0.07 gm/dL. The pilot was subsequently taken to the police station, where breathalyzer tests revealed 0.05 and 0.04 gm/dL about 1 hour, 45 minutes after the accident.

Postaccident examination of the engine by a Federal Aviation Administration inspector revealed that the intake manifold was damaged during the accident sequence. Spark was produced by each magneto, and piston movement was observed on all cylinders when the propeller was rotated by hand.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA15LA281