N6123P

Destroyed
Minor

Dawe ARNET PEREYRA AV II S/N: AP2A 0043

Accident Details

Date
Monday, April 26, 1999
NTSB Number
CHI99LA134
Location
FREMONT, MI
Event ID
20001205X00443
Coordinates
43.459308, -85.949829
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the seizure of the powerplant.

Aircraft Information

Registration
N6123P
Make
DAWE
Serial Number
AP2A 0043
Engine Type
Reciprocating
Year Built
1998
Model / ICAO
ARNET PEREYRA AV II SBM3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
WISCONSIN AVIATION MUSEUM INC
Address
85 N PIONEER RD STE 101
Status
Deregistered
City
FOND DU LAC
State / Zip Code
WI 54935-9400
Country
United States

Analysis

On April 26, 1999, at 1530 eastern daylight time, a Dawe Arnet Pereyra AV II, N6123P, piloted by a private pilot, sustained substantial damage during a forced landing, following a loss of power, during initial climb from Peck Lake, near Fremont, Michigan. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR Part 91 and was not on a flight plan. The pilot reported minor injuries. The flight was originating at the time of the accident and had the intended destination of Fremont Municipal Airport, Fremont, Michigan.

According to the pilot's written statement, he taxied the airplane around Peck Lake for a period of three to four minutes then departed the lake on a westerly heading. The pilot stated that during the initial climb, at an altitude of approximately 120 feet above ground level (agl), the engine seized. The pilot reported that the airplane collided with a top of a tree while maneuvering for an open field. The pilot stated that the aircraft impacted the terrain nose first and came to rest in an inverted position.

During the post accident investigation an engine teardown and inspection was conducted. Inspection of the magneto cylinder and piston revealed scoring along cylinder and piston walls. The piston face, from the magneto cylinder, was distorted in appearance when compared to the power-takeoff piston face. The power-takeoff piston wall and skirt exhibited a blue colored discoloration.

Inspection of the pilot's logbooks revealed that the pilot did not possess a single-engine sea rating.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI99LA134