N201DK

Substantial
None

Mooney M20J S/N: 24-0121

Accident Details

Date
Thursday, July 13, 2000
NTSB Number
DEN00LA143
Location
ESPANOLA, NM
Event ID
20001212X21447
Coordinates
36.000675, -106.059440
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The lack of suitable terrain for a forced landing. A factor was a complete loss of power due to mechanical failure.

Aircraft Information

Registration
N201DK
Make
MOONEY
Serial Number
24-0121
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
M20J M20P
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
VEC CORP OF DELAWARE DBA
Address
117 CENTRAL AVE
Status
Deregistered
City
HACKENSACK
State / Zip Code
NJ 07601-4207
Country
United States

Analysis

On July 13, 2000, at 1515 mountain daylight time, the pilot of a Mooney M20J, N201DK, made a forced landing near Espanola, New Mexico, when the engine lost all power. The aircraft sustained substantial damage and the commercial pilot and his passenger were not injured. Visual meteorological conditions prevailed for this cross-country flight operating under Title 14 CFR Part 91. A visual flight rules flight plan was filed. The flight originated from Los Alamos, New Mexico, at 1500 with a filed destination of Jefferson County Airport, Broomfield, Colorado.

According to the pilot, during climb following takeoff, he noticed the oil pressure was 0 PSI and the oil temperature was climbing. He said he initially reduced power to preserve engine life and began looking for a place to perform an emergency landing. His account states that the terrain in the area was rough, mountainous, and had heavy foliage. During this time, the pilot said the engine began to vibrate violently and he shut it down via the mixture control. He then spotted a field in which to land, lowered the landing gear and flaps, and did an emergency off airport landing. During landing roll, the nose landing gear collapsed due to stresses imposed by the uneven surface of the field. Substantial damage occurred to the engine firewall and surrounding airframe.

On August 13, 2000, an engine examination was performed at the facilities of Beegles Aircraft Services, Greeley, Colorado. The examination revealed that the number 3 cylinder rod bearing had failed due to lack of lubrication. This was followed by failure of the number 3 connecting rod, which penetrated the case. It was also found that the number 1 connecting rod bearing had failed due to heat stress brought on by reduced lubrication. The engine contained 7 quarts of oil at the time the examination was conducted and the internal oil distribution system showed no evidence of blockage.

According to part numbers recovered from the bearing, the correct parts were installed and the correct type oil was used. The oil pump was tested and operated normally. All filters and screens in the lubrication system contained metallic debris; however, none were blocked.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN00LA143