N8303G

Substantial
None

PIPER PA-44-180 S/N: 44-8195003

Accident Details

Date
Saturday, April 2, 1994
NTSB Number
MIA94LA109
Location
BUNNELL, FL
Event ID
20001206X01149
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

FAILURE OF THE INSTRUCTOR PILOT (CFI) TO MAINTAIN MINIMUM CONTROL SPEED (VMC) DURING THE GO-AROUND, WHICH RESULTED IN A LOSS OF CONTROL. A FACTOR RELATED TO THE ACCIDENT WAS: THE DELAY BY THE DUAL STUDENT TO EXTEND THE LANDING GEAR.

Aircraft Information

Registration
N8303G
Make
PIPER
Serial Number
44-8195003
Engine Type
Reciprocating
Model / ICAO
PA-44-180 PA44
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
PHOENIX EAST AVIATION INC
Address
561 PEARL HARBOR DRIVE
Status
Deregistered
City
DAYTONA BEACH
State / Zip Code
FL 32114
Country
United States

Analysis

On April 2, 1994, about 1217 eastern standard time, a Piper PA-44-180, N8303G, registered to and operated by Phoenix East Aviation, Inc., was substantially damaged while landing at the Flagler County Airport, Bunnell, Florida, while on a 14 CFR Part 91 instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The certified flight instructor (CFI), pilot-rated student, and observer were not injured. The flight originated from the Daytona Beach Regional Airport, Daytona Beach, Florida, about 1030.

The CFI stated that after departure the student performed airwork then a full stop landing at the Flagler County Airport. During the upwind leg the CFI pulled the left engine mixture control to the cutoff position. The flight turned downwind then base during which the CFI feather the left engine propeller. The airplane turned final and during the flare for landing, the pilot of another airplane in the traffic pattern advised the flight that the landing gear was not extended. The student lowered the landing gear selector handle and the CFI applied full throttle on the right engine. The airplane rolled to the left and impacted the ground left wing low followed by the nose and right wing, coming to rest upright.

Postaccident examination of the airplane by FAA certificated A & P mechanic revealed that the landing gear warning horn operated normally.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA94LA109