FTW93LA216

NTSB accident investigation · Cessna 172N · Purcell, OK · July 25, 1993

Accident · No injuriesLimited investigationFinal report
Date
July 24, 1993, 22:20 local (Jul 25, 1993, 03:20 UTC)
Place
Purcell, OK
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N4884GCessna 172N
Weather
Visual (VMC) · Night/bright
Status
Completed · report September 26, 1994
Report
Approved by Office Director
FAA report
19930724025399A
Case key
18796

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The lack of suitable terrain onto which to execute the forced landing which was neccesitated by the partial power loss. The power loss was a result of the fatigue failure of the exhaust valve rocker arm attachment stud. A factor was the night conditions.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfCruise - normal
Engine assembly,rocker arm/tappet - separationCause
Engine assembly,rocker arm/tappet - fatigueCause
Engine assembly,push rod - jammed
Forced landingDescent - emergency
Light condition - bright nightFactor
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - none suitableCause

Analysis

The airplane collided with rough terrain during a night forced landing following a partial power loss. The accident occurred during a night dual instructional flight and the instructor made the forced landing. Investigation revealed that the #3 exhaust valve rocker arm attachment stud had failed in fatigue. The separated stud subsequently lodged under the #3 intake valve mechanism and the corresponding push rod was bent. The engine and subject parts had accumulated a total of 2,903.5 hours.

Factual narrative

On July 24, 1993, at approximately 2220 central daylight time, a Cessna 172N, N4884G, was substantially damaged when it collided with rough terrain during a forced landing near Purcell, Oklahoma. The forced landing was executed following a partial loss of engine power. The airplane was on a night cross country dual instructional flight. A VFR flight plan was filed and visual meteorological conditions prevailed throughout the area. Neither the instructor pilot nor the rated student pilot were injured.

According to the instructor, the engine lost power down to 1,500 RPM while in cruise flight, about twenty minutes after takeoff from the Westheimer Airport in Norman, Oklahoma. The instructor stated that his efforts to regain power were unsuccessful and the airplane would not sustain level flight at the reduced power. He subsequently executed a forced landing to what appeared to be an open field. The airplane impacted rough terrain during the landing roll.

The number 3 cylinder exhaust rocker arm attachment stud had separated at the face of the cylinder head. The separated stud was found lodged under the number 3 intake valve mechanism. The number 3 intake valve push rod was bent. The operator stated that the stud was examined by a metallurgy lab at the University of Oklahoma and the failure mechanism was determined to be fatigue. The engine and subject parts had accumulated a total of 2,903.5 hours.

Neither the instructor nor the student submitted a pilot/operator accident report. Both subsequently left the country.

Aircraft

Registration
N4884G
Reported as
Cessna 172N
Category
Airplane
Serial number
17273431
Airframe hours
2,904
Engine
Lycoming O-320-H2AD, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Airman'S Flight School, Inc.
Airworthiness certificate
Standard, Normal
Departed
OUN · Norman, OK
Destination
GLE · Gainesville, TX
Flight plan
VFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
21
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
1,300 total · 200 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/bright
Wind
160° at 14 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 64 °F
Altimeter
29.00 inHg
Observed at
OKC, 20 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.