N734KG

Substantial
None

Cessna 172NS/N: 17268909

Accident Details

Date
Wednesday, May 22, 2002
NTSB Number
FTW02LA159
Location
Glen Rose, TX
Event ID
20020528X00745
Coordinates
32.244720, -97.726112
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to set the ignition key to the both magnetos position, which resulted in a loss of engine power. Contributing factors were the failure of the left magneto, the lack of suitable terrain for the forced landing, and the dark night.

Aircraft Information

Registration
N734KG
Make
CESSNA
Serial Number
17268909
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
172NC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AER MISTRAL
Address
PO BOX 79552
Status
Deregistered
City
SAGINAW
State / Zip Code
TX 76159
Country
United States

Analysis

On May 22, 2002, at 0005 central daylight time, a Cessna 172N single-engine airplane, N734KG, was substantially damaged when it impacted trees and terrain during a forced landing following a loss of engine power while in cruise flight near Glen Rose, Texas. The airplane was registered to Aer Mistral of Saginaw, Texas, and operated by Split S Aviation of Fort Worth, Texas. The private pilot and his passenger were not injured. Dark night visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations part 91 personal flight. The night cross-country flight originated from the Hicks Airfield Airport, near Fort Worth, Texas, at 2330, with San Antonio, Texas as the flights intended destination.

The 67-hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that during cruise flight at 2.000 feet, he initiated a climb to 3,000 feet. A few minutes later, the engine rpm dropped 200-300 rpm. The pilot stated he increased throttle to check for an rpm response. Subsequently, the engine lost power, and he initiated a forced landing. While approaching to land, he noticed trees in front of the airplanes flight path and started "looking for another place to land, but couldn't see anything because it was completely dark." Prior to landing, he decided to put 10-degrees of flaps down. The aircraft impacted tress coming to rest in the upright position.

Examination of the airplane by the FAA inspector who responded to the accident site, revealed that both wings were structurally damaged and the fuselage was wrinkled aft of the cabin area. An examination of the engine under the supervision of an FAA inspector, revealed the left magneto's internal gears did not rotate with the engine. Removal of the left magneto revealed only one of two rubber drive isolators inside the ignition harness cap. Internal inspection of the magneto revealed the contact points on the left hand side of the magneto did not open on rotation. Further examination of the airplane, revealed that the ignition key turned to the left magneto only. The pilot reported to the NTSB investigator-in-charge, that he did not touch any switch while exiting the aircraft.

A review of the aircraft logbooks revealed that the engine had accumulated 857 hours since the last major overhaul, which was completed on July 18, 2001. The airplane had accumulated 28 hours since the last 100-hour inspection, which was completed on May 14, 2002.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW02LA159