FTW97LA116

NTSB accident investigation · Cessna 172P · Cleveland, OK · March 10, 1997

Accident · No injuriesLimited investigationFinal report
Date
March 10, 1997, 16:45 local (22:45 UTC)
Place
Cleveland, OK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N65753Cessna 172P
Weather
Visual (VMC) · Day
Status
Completed · report August 25, 1997
Report
Approved by Office Director
FAA report
19970310006379A
Case key
20167

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 pilot/mechanic's improper installation of the spark plug, resulting in its separation from the engine. A factor was the unsuitable terrain available in the runway's overrun area.

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) - nonmechanicalTakeoff - initial climb
Ignition system,spark plug - separationCause
Maintenance,installation - improperOther maintenance personnelCause
Forced landingEmergency landing after takeoff
OverrunLanding - roll
Terrain condition - none suitableFactor
Nose overLanding - roll
Terrain condition - rough/unevenFactor

Analysis

The pilot, who is also an A&P mechanic, installed and torqued a new helicoil and spark plug. A satisfactory engine run was completed. During takeoff climb, at 300 feet AGL, 'the engine popped and lost power.' The pilot executed a 180-degree turn, and 'landed fast downwind.' During the landing roll, the aircraft overran the end of the runway and 'encountered a rut and flipped over' damaging both wings. An examination of the airplane revealed that the newly installed spark plug was hanging by its ignition wire.

Factual narrative

On March 10, 1997, at 1645 central standard time, a Cessna 172P, N65753, registered to Christiansen Aviation, Inc., and operated by the Oklahoma State University Flight School, was substantially damaged during a forced landing, following a loss of engine power near Cleveland, Oklahoma. Visual meteorological conditions prevailed for the proposed positioning flight to Stillwater, Texas, and a flight plan was not filed. The commercial pilot, the sole occupant, was not injured. The flight was originating from Cleveland Municipal Airport at the time of the accident.

The pilot, who is also a certificated mechanic, reported that he had installed and torqued a new helicoil and spark plug. A satisfactory engine run was completed. During takeoff climb from runway 18, while at 300 feet AGL, "the engine popped and lost power." He executed a 180 degree turn, and "landed fast downwind" on runway 36. During the landing roll, the aircraft overran the end of the runway and "encountered a rut and flipped over."

An examination of the airplane by a FAA inspector revealed that the newly installed spark plug was hanging by its ignition wire, and both wings were structurally damaged.

Aircraft

Registration
N65753
Reported as
Cessna 172P
Category
Airplane
Serial number
17275858
Airframe hours
6,047
Engine
Lycoming O-320-D2J, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Positioning · Part 91
Operator
Oklahoma State University
Registered owner
Christiansen Aviation
Airworthiness certificate
Standard, Utility
Last inspection
Annual · February 14, 1997 · 28 hours before
Departed
95F
Destination
SWO · Stillwater, OK
Airport
95F · Cleveland Municipal, runway 18, 4,000 × 60 ft, asphalt

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
27
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
311 total · 39 in this make and model · 167 as pilot in command · 1 in the last 90 days · 1 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 30 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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