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FTW97LA116

1997-03-10 · CLEVELAND, Oklahoma, United States · None · 1 aircraft · Status: Completed

Airport 95F

Current FAA registration · N65753

Make / Model
CESSNA 172P
Year of manufacture
1982 · 15 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19820729
ADS-B equipped
Yes — Mode-S A8A9DE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

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.

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. 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. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1997_FTW97LA116.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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