N1209V

Substantial
Minor

Cessna R172K IIS/N: R1722140

Accident Details

Date
Saturday, July 15, 2006
NTSB Number
LAX06LA232
Location
Hagatna
Event ID
20061025X01556
Coordinates
13.483333, 144.800003
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
3
Uninjured
0
Total Aboard
3

Probable Cause and Findings

The failure of the number four connecting rod during takeoff-initial climb.

Aircraft Information

Registration
N1209V
Make
CESSNA
Serial Number
R1722140
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
R172K IIC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MICRONESIAN AVIATION SYSTEMS INC
Address
PO BOX 10438
Status
Deregistered
City
TAMUNING
State / Zip Code
GU 96931-0438
Country
United States

Analysis

On July 15, 2006, about 1810 coordinated universal time, a pilot ditched a Cessna R172K II, N1209V, near Hagatna, Guam. Micronesia Aviation Systems, Inc., was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The certificated commercial pilot and two passengers sustained minor injuries; the airplane sustained substantial damage to the firewall. The local sight seeing flight departed Guam International Airport in Hagatna about 1805. Visual meteorological conditions prevailed, and no flight plan had been filed.

The pilot reported to the Federal Aviation Administration that the airplane was climbing through 1,500 feet. The engine began to run rough, and he tried to smooth it out using the mixture. It began sputtering as he tried to return to the airport for a landing on runway 06L. However, it's condition worsened, and then the engine quit producing power. He ditched in a nearby bay.

A Federal Aviation Inspector supervised examination of the airframe and engine. The airplane sustained damage to the firewall where the engine cradle attaches to the airframe. The cradle tweaked to the right, wrinkling the airframe just a little aft of the firewall. He observed a hole in the top of the case at the number four cylinder. He noted that the number four connecting rod fractured and separated. After being in the salt water, he reported that the engine had corroded and could not be further disassembled. The engine had been flown 1,500 hours past the manufacturer's recommended time between 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# LAX06LA232