N19AG

Substantial
None

Piper PA-28R-180S/N: 28R-180

Accident Details

Date
Saturday, April 3, 2004
NTSB Number
NYC04LA101
Location
Elyria, OH
Event ID
20040412X00443
Coordinates
41.331390, -82.099998
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A loss of engine power for undetermined reasons.

Aircraft Information

Registration
N19AG
Make
PIPER
Serial Number
28R-180
Engine Type
Reciprocating
Year Built
2012
Model / ICAO
PA-28R-180P28R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AIRCRAFT GUARANTY CORP TRUSTEE
Address
PO BOX 2549
Status
Deregistered
City
ONALASKA
State / Zip Code
TX 77360-2549
Country
United States

Analysis

On April 3, 2004, about 1050 eastern standard time, a Piper PA-28R-180, N19AG, was substantially damaged during a forced landing, while on approach to the Elyria Airport (1G1), Elyria, Ohio. The certificated flight instructor (CFI) and a private pilot were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the instructional flight conducted under 14 CFR part 91.

The CFI and private pilot had been flying for about 50 minutes, when they decided to return to 1G1. The airplane was on approach to runway 27, a 3,053-foot-long, 48-foot-wide, asphalt runway.

According to the CFI, the private pilot was flying the airplane when the engine experienced a power loss, about 2 miles from the runway. The engine did not sputter, and the propeller continued to windmill. The CFI assumed control of the airplane and attempted to glide to the airport; however, the airplane struck the ground about 700 feet prior to the runway. The landing gear collapsed and the airplane's left wing struck a tree stump.

The private pilot reported that earlier in the day, he topped off both the left and right fuel tanks, and had flown in the airplane with another pilot for about 45 minutes, without any problems.

The airplane had been operated for about 2.5 hours since it's most recent annual inspection, which was performed about 5 days prior to the accident.

Examination of the airplane and engine by a Federal Aviation Administration inspector did not reveal any pre-impact mechanical malfunctions. Control continuity was confirmed for the propeller, throttle, and mixture controls. The airplane was equipped with an IO-360 series engine. Piston and valve train continuity were observed when the propeller was rotated by hand. Both the left and right magnetos produced spark when rotated. The engine-driven and fuel boost pumps operated normally, and the fuel system was absent of contamination.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC04LA101