N2226T

Substantial
Serious

Piper PA-28R-200 S/N: 28R-7135171

Accident Details

Date
Monday, March 31, 1997
NTSB Number
LAX97LA137
Location
CONTINENTAL, AZ
Event ID
20001208X07589
Coordinates
31.810522, -110.919235
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

loss of engine power as a result of detonation in the number 2 cylinder for undetermined reasons. A factor in the accident was the unsuitable nature of the forced landing area.

Aircraft Information

Registration
Make
PIPER
Serial Number
28R-7135171
Engine Type
Reciprocating
Year Built
1971
Model / ICAO
PA-28R-200 P28R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28R-200

Registered Owner (Current)

Name
REGISTRATION PENDING
Address
8466 N TREECE WAY
City
TUCSON
State / Zip Code
AZ 85742-8219
Country
United States

Analysis

On March 31, 1997, at 0839 hours mountain standard time, a Piper PA-28R-200, N2226T, lost engine power and landed gear up off the airport near Continental, Arizona. The airplane was being operated as an instructional flight by Leading Edge Aviation, Tucson, Arizona. The airplane was substantially damaged. The certified flight instructor received minor injuries and the certificated commercial pilot/student received serious injuries. The local flight originated in Tucson about 0820. Visual meteorological conditions prevailed at the time.

The pilots reported the airplane lost engine oil pressure followed by seizure of the engine. The flight instructor attempted to glide to a nearby private landing strip but had insufficient altitude and elected to land gear up on rough level terrain.

After the accident, the engine was disassembled and examined by the Federal Aviation Administration (FAA) Airworthiness Inspector. According to the FAA, there was evidence of detonation in the number 2 cylinder. The number 2 piston was found damaged, and aluminum from the piston was found in the engine oil screen restricting the flow of oil. The number 2 piston rod bearing exhibited evidence of heat distress and appeared to the inspector to have failed as a result of loss of lubrication. One of the bolts to the number 2 piston rod cap was found broken, jamming the rotation of the crankshaft. According to the FAA inspector, the reason for the detonation in the number 2 cylinder could not be determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX97LA137