N9001G

Substantial
None

Cessna 182N S/N: 18260541

Accident Details

Date
Sunday, June 30, 1996
NTSB Number
FTW96LA280
Location
TRUTH OR CONSEQ, NM
Event ID
20001208X05996
Coordinates
33.129844, -107.239234
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The loss of engine power due to the fatigue failure of the number one piston. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N9001G
Make
CESSNA
Serial Number
18260541
Engine Type
Reciprocating
Model / ICAO
182N C182
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RUST BRUCE
Address
4110 N CAMINO CARDENAL
Status
Deregistered
City
TUCSON
State / Zip Code
AZ 85718
Country
United States

Analysis

On June 30, 1996, at 1400 mountain daylight time, a Cessna 182N, N9001G, was substantially damaged during a forced landing near Truth or Consequences, New Mexico. The instrument rated private pilot and his passenger were not injured. The aircraft was registered to and operated by a private owner, under Title 14 CFR Part 91. The cross country flight originated from Tucson International Airport near Tucson, Arizona, two hours before the accident. Visual meteorological conditions prevailed for the flight and no flight plan was filed for the flight to Amarillo, Texas.

The pilot reported in written statements to the FAA and on his Pilot/Operator Aircraft Accident Report that while cruising at 11,500 feet MSL over 10,000 foot terrain, he "noticed the oil pressure gauge was reading 0." Approximately 5 minutes later, the engine "clanked and started to break apart internally." Subsequently, a "few minutes" after that, the engine seized. The pilot landed the airplane between trees, on a rocky ridge top. During the landing roll, the airplane hit a rock, nosed over and came to rest inverted.

A post-crash teardown examination of the engine by an FAA inspector revealed extensive internal damage. The parts were sent to a metallurgical laboratory for analysis. It was determined that the number one piston had developed in-service fatigue cracks and subsequently disintegrated (see attached Failure Analysis of Engine Components report).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW96LA280