N3873Y

Substantial
None

BEECH 77S/N: WA-265

Accident Details

Date
Thursday, August 12, 2021
NTSB Number
WPR21LA316
Location
Stanley, NM
Event ID
20210813103693
Coordinates
35.167793, -105.968720
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A loss of engine performance due to lead fouling of the lower spark plugs, which resulted in an off airport forced landing.

Aircraft Information

Registration
N3873Y
Make
BEECH
Serial Number
WA-265
Engine Type
Reciprocating
Year Built
1981
Model / ICAO
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
GILLETT DREW A
Address
84 FENTON AVE
Status
Deregistered
City
LACONIA
State / Zip Code
NH 03246-3364
Country
United States

Analysis

On August 12, 2021, about 1100 mountain daylight time, a Beech 77, N3873Y, was substantially damaged when it was involved in an accident near Stanley, New Mexico. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot departed Double Eagle II Airport (KAEG), Albuquerque, New Mexico, about 1000. The atmospheric conditions at the time of departure resulted in a density altitude of about 8,000 ft. The pilot reported that, during the climb, the airplane maintained a 200 foot per minute (fpm) rate of climb; however, 3 days earlier, under similar atmospheric conditions and airplane loading, the airplane maintained a climb rate of 500 fpm.

The pilot further reported that the airplane would not climb higher than 6,700 ft mean sea level, and he decided to maneuver the airplane toward the destination airport. About 300 ft above the ground, as he maneuvered to the southeast to follow a road, the pilot noticed that the terrain was rising and elected to perform a forced landing. Shortly after touchdown, the airplane impacted a cattleguard post and the slid about 200 feet to a stop, resulting in substantial damage to the right wing.

Performance calculations for the accident takeoff from the pilots operating handbook indicated that, given a pressure altitude of 5,527 ft, outside air temperature of 24°C, airplane weight of 1,645 lbs, flaps 0°, mixture leaned to maximum rpm, and power at full throttle, the airplane’s rate of climb should have been about 475 fpm.

A postaccident examination of the airframe revealed no anomalies or malfunctions. Examination of the engine established mechanical continuity throughout the engine and valve train. The top spark plugs were carbon fouled and displayed black, sooty deposits, while the lower spark plugs were heavily lead fouled, and displayed hard, cinder-like globules of lead around the firing end and cavity. (see figure 1.) According to the pilot, he believed that he had an undetected fouled plug.

Figure 1. Top: View of lower spark plugs; Left: Close-up view of no. 1 & 3 spark plugs; Right: View of no. 2 & 4 spark plugs

According to Champion Aerospace Aviation Service Manual for spark plugs:

Severely fouled spark plugs will operate colder, causing misfires, and will also misfire at higher power because of the conductive nature of the deposits at elevated temperatures.

According to the engine logbooks, all spark plugs were cleaned and gapped during the most recent annual inspection about 1 year before the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR21LA316