N6051U

Substantial
None

CESSNA R172ES/N: R172-0183

Accident Details

Date
Saturday, November 5, 2022
NTSB Number
CEN23LA027
Location
Aguilar, CO
Event ID
20221107106255
Coordinates
37.401634, -104.655590
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Failure of the engine cylinder assembly, which resulted in a loss of engine power during cruise flight and an impact with a fence during the forced landing.

Aircraft Information

Registration
Make
CESSNA
Serial Number
R172-0183
Engine Type
Reciprocating
Model / ICAO
R172EC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
R172E

Registered Owner (Current)

Name
VIGIL GABRIEL M
Address
PO BOX 766
City
MORA
State / Zip Code
NM 87732-0766
Country
United States

Analysis

On November 5, 2022, about 0821 mountain daylight time, a Cessna R172E, N6051U, was substantially damaged when it was involved in an accident near Aguilar, Colorado. The private pilot was uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that he climbed the airplane from 9,000 ft mean sea level (msl) to 10,000 ft msl to overfly Raton Pass and Fischer Peak, Colorado. He encountered wind shear and high turbulence and simultaneously felt a pop or shudder. The airplane started to shake, and oil began to cover the windshield. He then performed a forced landing to a field, during which the airplane struck a fence. The airplane sustained substantial damage to both wings.

Postaccident examination of the engine by a Federal Aviation Administration inspector revealed that the engine’s No. 2 cylinder head was cracked. The cylinder head and barrel assembly, with 358.9 hours since new, was manufactured by Engine Components International and was subject to airworthiness directive (AD) 2009-26-12, which requires initial and repetitive visual inspections and compression tests to detect cracks at the head-to-barrel interface. The last cylinder compression check was performed in July 2022 and its pressure tested at 70 psi.

There were no other mechanical anomalies that would have precluded normal airplane operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA027