N4737D

Substantial
None

CESSNA 172NS/N: 17272345

Accident Details

Date
Friday, February 17, 2012
NTSB Number
ERA12LA191
Location
Flat Rock, VA
Event ID
20120222X92352
Coordinates
37.520278, -77.820274
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The partial loss of engine power due to the failure of the exhaust valve spring seat for reasons that could not be determined.

Aircraft Information

Registration
N4737D
Make
CESSNA
Serial Number
17272345
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
172NC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
GREEN HAT AVIATION LLC
Address
11918 HADDON LN
Status
Deregistered
City
WOODBRIDGE
State / Zip Code
VA 22192-6059
Country
United States

Analysis

On February 17, 2012, about 1652 eastern standard time, a Cessna 172N, N4737D, made a force land following a partial loss of engine power near Flat Rock, Virginia. The airplane sustained substantial damaged and the private pilot was not injured. The airplane was registered to Green Hat Aviation LLC, and operated by an individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight originated from Manassas Regional Airport/Harry P. Davis Field (HEF), Manassas, Virginia at 1549.

According to the pilot, he was at an altitude of 4,500 feet when the engine began losing power. He noticed a strong vibration in the throttle control and began to notice an "oily smell." The engine power decreased to 1,500 rpm but continued to run. The pilot contacted the air traffic controller (ATC) and declared an emergency. He advised ATC of his intention to land in a field, and ATC suggested a private grass strip. The pilot advised ATC that he did not have enough altitude to make it to the strip and continued towards the field. The pilot made a forced landing in the field, and during the landing roll the airplane collided with an embankment.

Examination of the airplane by a Federal Aviation Administration inspector confirmed structural damage to the firewall, fuselage and both wings. During an examination of the engine, it was noted that the No. 4 cylinder exhaust valve spring seat had broken. As a result of the broken valve spring seat, the push rod became dislodged.

A review of the maintenance records revealed that airworthiness directive (AD 80-04-03 R2) was performed, which instructs the replacement of the upper exhaust valve spring seats and the exhaust hydraulic lifters. According to the Lycoming Service Instruction 1009AU, the recommended time between overhaul (TBO) periods is 2,000 hours or 12 years, whichever comes first. The last engine overhaul was conducted on August 29, 2005, and 134.66 hours remained on the engine before the next recommended overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA12LA191