N5096U

Substantial
None

CESSNA 172RG S/N: 172RG0230

Accident Details

Date
Friday, February 17, 1995
NTSB Number
FTW95LA117
Location
PLANO, TX
Event ID
20001207X02966
Coordinates
33.060909, -96.729782
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE DISENGAGEMENT OF THE CRANKSHAFT GEAR DUE TO THE LOOSENING OF THE GEAR RETAINING BOLT AND THE SUBSEQUENT FRACTURE OF THE GEAR ALIGNMENT DOWEL. A FACTOR WAS THE LACK OF SUITABLE TERRAIN AVAILABLE FOR THE FORCED LANDING.

Aircraft Information

Registration
N5096U
Make
CESSNA
Serial Number
172RG0230
Engine Type
Reciprocating
Model / ICAO
172RG C72R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ZAPPOLO RICHARD A DBA
Address
2810 ROUNDROCK
Status
Deregistered
City
MCKINNEY
State / Zip Code
TX 75070
Country
United States

Analysis

On February 17, 1995, at 1235 central standard time, a Cessna 172RG, N5096U, was substantially damaged during a forced landing near Plano, Texas. The commercial pilot and his passenger were not injured. Visual meteorological conditions prevailed for the repositioning flight from McKinney, Texas, to Addison, Texas.

The airplane was in a descent 7 miles northeast of Addison Airport when the engine lost power. After attempting unsuccessfully to restart the engine, the pilot landed in a plowed field. According to the pilot, when the nose wheel touched down in the soft dirt it "dug in and broke off" and the "airplane performed a forward somersault and came to rest inverted." A Federal Aviation Administration inspector reported that the right wing spar was bent and the upper portions of the vertical stabilizer and rudder were crushed.

Examination and disassembly of the engine on 03/06/95 revealed a lack of gear train continuity. The crankshaft gear lockplate tang was sheared and the crankshaft gear retaining bolt had backed out of the crankshaft to the point where no threads were engaged. The crankshaft gear alignment dowel was fractured. An examination of the aircraft logbooks by a Federal Aviation Administration inspector revealed that the propeller had been replaced on 02/13/92 following a nose gear collapse. Airworthiness Directive (AD) 91-14-22 was not complied with at that time. The AD requires an inspection of the crankshaft gear following any propeller strike which results in sudden engine stoppage. According to the operator, the nose gear collapse did not result in sudden engine stoppage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA117