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Aviation safety reports, made easier to study

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NTSB Report

August 20, 1995 · Cessna 172P · N55404

Port Washington, WI

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 20, 1995
Injury Outcomes
4 injuries (4 minor injuries)
Location
Port Washington, WI
Aircraft
Cessna 172P
Tail Number
N55404
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
CHI95LA290

The pilot reported that the engine lost power during a local flight and he made a forced landing onto a farm field. During the landing roll, the nose wheel dug into the soil and the airplane came to rest in an inverted position. Postaccident investigation revealed that the #2 cylinder had fractured as a result of fatigue cracking.

NTSB Probable Cause

the failure of the #2 cylinder due to fatigue cracking. A factor was the soft terrain.

Full Narrative

On August 20, 1995, at 1415 central daylight time (cdt), a Cessna 172P, N55404, operated by Waukesha Flying Service, Inc., of Waukesha, Wisconsin, was substantially damaged following a loss of engine power and subsequent forced landing in Port Washington, Wisconsin. The commercially certificated pilot and three passengers reported minor injuries. The local 14 CFR Part 91 pleasure flight departed Waukesha County Airport, Waukesha, Wisconsin, at 1330 cdt. No flight plan was filed and visual meteorological conditions existed at the time of the accident. In a detailed written statement, the pilot reported the engine began to run rough approximately 45 minutes after departure. The pilot stated that he immediately applied carburetor heat and performed a magneto check, but the engine roughness became progressively worse. The pilot stated that the oil temperature gauge showed a rapid increase, the oil pressure gauge showed a rapid decrease, and white smoke began to emit from the front of the engine cowling. The pilot selected a field to make a forced landing on and briefed the passengers. After clearing tension wires which lined the approach end of the field, the airplane touched down on the field. The nose wheel dug into the soil and the airplane came to rest in an inverted position. Postaccident investigation revealed the number two cylinder, P/N 78475, had fractured. The cylinder was sent to the NTSB Materials Laboratory, Washington, D.C., for examination. The laboratory reported the cylinder barrel was cracked through an arc of approximately 300 degrees. The largest opening of the crack was between the fourth and fifth cooling fins. Examination of the cleaned fracture revealed crack arrest positions of fatigue cracking. See attached NTSB Metallurgist's Factual Report and Textron Lycoming Technical Report. The airplane logbook shows the last inspection was an annual inspection performed on August 8, 1995. The airplane has logged 19 hours of flight time since the inspection.

Flight

Event TypeAccident
Event Time14:15 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 172P
Tail NumberN55404
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-D2J · Reciprocating · 160
Seats4

People & Injuries

Injury Summary4 injuries (4 minor injuries)
Fatal0
Serious0
Minor4
Uninjured0
Total4
Crew 1Age 37 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind50° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F
Altimeter30.00 inHg
Observation Time18:56
Weather SourceWFAC

Appendix: Source Data