N5114VMorrisey 2150A2006-10-18 NTSB Accident Report

Substantial
Minor

Morrisey 2150AS/N: SP14

Summary

On October 18, 2006, a Morrisey 2150A (N5114V) was involved in an accident near Chandler, AZ. The accident resulted in 2 minor injuries. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this accident to be: Loss of engine power during cruise flight due to a crack in the oil cooler and subsequent loss of engine oil.

On October 18, 2006, at 0950 mountain standard time, a Morrisey (Varga) 2150A airplane, N5114V, impacted terrain during a forced landing near the Stellar Airpark, Chandler, Arizona. The forced landing was precipitated by a loss of engine power. The airplane sustained substantial damage; the commercial pilot and pilot-rated passenger sustained minor injuries. The pilot operated the airplane under the provisions of 14 CFR Part 91 as a personal flight. The local flight originated from the Chandler Municipal Airport (CHD) about 15 minutes prior to the accident and was destined for the Stellar Airpark (P19). Visual meteorological conditions prevailed, and a flight plan had not been filed for the flight.

This accident is documented in NTSB report LAX07LA011. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N5114V.

Accident Details

Date
Wednesday, October 18, 2006
NTSB Number
LAX07LA011
Location
Chandler , AZ
Event ID
20061026X01562
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

Loss of engine power during cruise flight due to a crack in the oil cooler and subsequent loss of engine oil.

Aircraft Information

Registration
Make
MORRISEY
Serial Number
SP14
Year Built
1961
Model / ICAO
2150A

Registered Owner (Historical)

Name
SALE REPORTED
Address
260 RIO RD
Status
Deregistered
City
ARROYO GRANDE
State / Zip Code
CA 93420-9636
Country
United States

Analysis

On October 18, 2006, at 0950 mountain standard time, a Morrisey (Varga) 2150A airplane, N5114V, impacted terrain during a forced landing near the Stellar Airpark, Chandler, Arizona. The forced landing was precipitated by a loss of engine power. The airplane sustained substantial damage; the commercial pilot and pilot-rated passenger sustained minor injuries. The pilot operated the airplane under the provisions of 14 CFR Part 91 as a personal flight. The local flight originated from the Chandler Municipal Airport (CHD) about 15 minutes prior to the accident and was destined for the Stellar Airpark (P19). Visual meteorological conditions prevailed, and a flight plan had not been filed for the flight.

According to the pilot-rated passenger, who was the registered owner of the airplane, the aircraft had departed CHD when one of the pilots smelled "something kind of funny." The commercial pilot noticed that the oil pressure indicator was not registering any pressure, so he instructed the pilot-rated passenger to monitor the oil temperature gauge. Both pilots began scanning the surrounding terrain in case of a forced landing. The engine then began to "buck" and then lost power. The commercial pilot declared an emergency to CHD's air traffic control tower and informed them that they were making a forced landing near P19. The airplane touched down in rough terrain short of runway 35, which resulted in substantial damage to the wings and fuselage.

The Federal Aviation Administration inspector who responded to the accident site reported that engine oil was present on the left side of the cowling, over the left wing, and down the belly of the airplane. He opened the cowling and noted that the oil dipstick was in place and the oil filter remained secured to the engine.

The aircraft engine was inspected by a National Transportation Saftey Board investigator, who discoved that oil was dripping from the base of the oil cooler. Closer examination of the oil cooler revealed a bulge in the metal between the fifth and sixth base cap. In the bulged area there was a .4 centimeter crack in the metal, through which oil was leaking out.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX07LA011