N6811V

Substantial
Serious

AEROSTAR ACFT CORP OF TEXAS M20FS/N: 22-0003

Accident Details

Date
Saturday, December 26, 2015
NTSB Number
WPR16LA043
Location
Nogales, AZ
Event ID
20151228X02331
Coordinates
31.431110, -110.841392
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
4
Minor Injuries
0
Uninjured
0
Total Aboard
4

Probable Cause and Findings

The airplane’s impact with a hillside shortly after takeoff for reasons that could not be determined.

Aircraft Information

Registration
N6811V
Make
AEROSTAR ACFT CORP OF TEXAS
Serial Number
22-0003
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
M20FAC52
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
TAMAYAMA MITSUO
Address
2270 PALMER CIR
Status
Deregistered
City
FAIRFIELD
State / Zip Code
CA 94534-7546
Country
United States

Analysis

On December 26, 2015, about 1340 mountain standard time, an Aerostar Aircraft Corporation of Texas M20F airplane, N6811V, was substantially damaged when it was involved in an accident near Nogales, Arizona. The pilot and three passengers were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Shortly after departure from Nogales International Airport (OLS), Nogales, Arizona, for a cross-country flight, the airplane impacted a hillside about .5 miles east of the airport and then came to rest upright on its belly. No mayday call was received from the pilot.

During postaccident examination of the airplane, one of the landing gears was found separated, and the engine was found partially separated from the airframe, but it remained in its relative normal position. The airframe was substantially damaged. Fuel was observed leaking from the airplane, no holes were found in the engine case, and no evidence of leaking oil was found. The propeller assembly remained attached to the engine. One propeller blade was missing the tip, and the other propeller blade exhibited chordwise striations and was bent near the propeller hub. Examination of the airplane revealed no evidence of any preaccident mechanical malfunctions or failures that would have precluded normal operation; however, the engine was not examined.

The pilot did not return the National Transportation Safety Board Pilot/Operator Report Form 6120.1 nor did he provide a statement about the accident sequence.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR16LA043