N98SW is a 1976 Cessna 177RG. It is a fixed-wing single-engine aircraft with 4 seats, powered by a Lycoming IO-360-A1B6D rated at 200 horsepower. The registration is active, with the registrant based in Ventura, CA. Its standard airworthiness certificate was issued in Dec 1976. It has been registered to its current owner since Jul 2014. This page also carries 1 NTSB event.
- 50 years old
- 1 of 819 Cessna 177RG
2014
1976
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N98SW's record changes.
On April 4, 2020, about 1900 Pacific daylight time, a Cessna 177RG airplane, N98SW, was substantially damaged when it was involved in an accident at Santa Paula Airport (SZP), Santa Paula, California. The pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
According to the pilot, he had planned an approximate 30-minute flight to maintain currency in the accident airplane, which was his personal airplane that he had not flown in several months. He performed a preflight inspection, during which time he observed a total fuel quantity of about 10 gallons, evenly balanced between the left- and right-wing fuel tanks. The pilot observed that the fuel gauges indicated "just above empty," and did not look inside the fuel tanks to visually confirm the fuel level. He then sumped the fuel tanks and discovered that the right fuel tank contained some water, but he eventually observed water-free fuel samples after he sumped the right wing about three times.
The pilot started the airplane and taxied to runway 22 where he performed an engine run-up and did not observe any anomalies. During the initial climb on his fourth touch and go maneuver, the pilot experienced a loss of engine power as the airplane reached about 100 ft above ground level. He immediately began a left turn with the intention of landing on runway 04. The engine momentarily regained power multiple times during the descent as the nose of the airplane dropped, but the pilot was unable to successfully restore and maintain engine power. The airplane impacted a dry riverbed and came to rest upright in an area of dense vegetation.
Postaccident photographs provided by the Federal Aviation Administration showed substantial damage to the stabilator.
Recovery personnel reported no evidence of a fuel spill and that neither fuel tank was breached. After the airplane was recovered, the recovery team drained about 2 gallons of fuel from the right wing and noted that the left wing was devoid of fuel. The fuel strainer was free of debris and contained a few ounces of uncontaminated fuel.
Examination of the engine revealed no evidence of preimpact malfunctions or anomalies. The engine was subsequently test run, during which time it sounded smooth and continuous through various power settings.
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