# NTSB LAX98LA254: Girgen Kitfox II, N62KF, Peoria, AZ, June 6, 1998 - Type: NTSB accident investigation - Classification: Accident · Minor injuries · Limited investigation · Final report - Date: June 6, 1998, 10:14 local (17:14 UTC) - Place: Peoria, AZ - Coordinates: 33.570968, -112.250419 (estimated) - Nearby events: https://openairdocs.org/map.md?lat=33.5710&lon=-112.2504&mi=10 - Phase of flight: [Maneuvering](https://openairdocs.org/ntsb-phases/450) (OpenAirDocs' grouping) - Highest injury: Minor injuries - Injuries: 2 minor - Status: Completed, report March 31, 2000 - Report: Approved by Office Director - NTSB case key (mKey): 43639 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=LAX98LA254 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/43639/pdf - Page: https://openairdocs.org/ntsb/LAX98LA254 ## Probable cause An engine failure due to a broken rotary valve for unknown reasons. Contributing factors to the accident was an inadequate inspection by the owner of a previously damaged engine during maintenance overhaul prior to installation in the airframe. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of engine power(total) - mech failure/malf, maneuvering - engine assembly,valve,intake - previous damage (contributing factor) - maintenance,overhaul - inadequate, owner/builder (contributing factor) - engine assembly,valve,intake - fractured (cause) - reason for occurrence undetermined (cause) - Forced landing, emergency descent/landing - On ground/water encounter with terrain/water, landing - roll - terrain condition - berm ## Analysis The pilot stated that the purpose of the flight was to fly to a different airport with another aircraft to have coffee. He stated that after completing a 360-degree turn to wait for the other aircraft, the engine lost power. He chose an open dirt field to make the emergency landing. After touchdown the landing gear was sheared off after colliding with a dirt berm. The pilot stated that all engine instruments were indicating normal and no discrepancies were noted. According to the manufacturer of the engine, this engine had been installed on a 1989 Ski-Doo Mach 1 snowmobile, which had been involved in an accident. The engine manufacturer further stated that this particular model was not originally intended for use in an aircraft. The owner inspected the engine following purchase and prior to installation in the airframe. No discrepancies noted during the preinstallation inspection. Examination of the engine by the owner following the accident revealed that the rotary valve had broken. ## Factual narrative On June 6, 1998, at 1014 hours mountain standard time, an experimental Girgen Kitfox II aircraft, N62KF, experienced a loss of engine power while maneuvering. The pilot made a forced landing in an open dirt field near Peoria, Arizona. The aircraft, operated under the provisions of 14 CFR Part 91, sustained substantial damage. The private pilot/owner/builder and one passenger, the sole occupants, received minor injuries. Visual meteorological conditions existed for the personal flight and no flight plan was field. The flight originated from McGill Flight Park, Phoenix, Arizona, at 1000, and was scheduled to terminate at the Glendale, Arizona, airport. The pilot stated he and his passenger and another aircraft were traveling to Glendale airport for coffee. After takeoff, the two aircraft could not establish radio communications so they returned to McGill Flight Park to rectify the situation. Approximately 10 minutes later both aircraft took off with radio communications established. The pilot stated that after completing a 360-degree turn to wait for the other aircraft, the "engine came to a complete stop." The pilot stated that he was at 2,500 feet agl and he pushed the aircraft nose down to maintain airspeed and look for a place to land. He stated that he setup for an emergency landing in an open dirt field. The pilot said that he landed in a flat area about 300 yards long. After touchdown the landing gear was sheared off after colliding with a dirt berm. The aircraft traveled approximately 150 feet before coming to rest. The pilot exited the aircraft on his own, and helped his passenger out of the aircraft. The pilot reported that when the engine quit he had approximately 12 gallons of fuel onboard. An inspector from the Federal Aviation Administration (FAA) stated that the engine had been previously installed in a snowmobile. The snowmobile had been involved in an accident prior to installation of the engine in the accident aircraft. The owner inspected the engine following purchase and prior to installation in the airframe. No discrepancies were noted during the preinstallation inspection. Examination of the engine by the owner after the aircraft accident revealed that the rotary valve had broken under unknown circumstances. The engine manufacturer reported that the rotary valve is a circular plate made of heavy-duty aluminum located inside the engine. The plate has a hole matching the intake ports in each cylinder. As the plate rotates, the hole lines up with the intake port and allows the fuel/air mixture to enter the cylinder. According to the manufacturer, this engine had originally been installed on a 1989 Ski-Doo Mach 1 snowmobile, with a rated power of 100 horsepower. The engine manufacturer further stated that this particular model was not originally intended for use in an aircraft. Maintenance performed on the engine is a function of weekly, monthly, and yearly, or based on mileage (maintenance schedule appended to file). A general inspection should be conducted on a monthly basis, or every 500 miles. ## Aircraft - Registration: [N62KF](https://openairdocs.org/deregistered/N62KF-2001-02-03), registration cancelled 2001-02-03, S/N 1 (OpenAirDocs) - Reported make and model: Girgen KITFOX II - Registry model: [Girgen Frank G JR GIRGEN KITFOX](https://openairdocs.org/model/girgen-frank-g-jr-girgen-kitfox) (registry code 056161M) (OpenAirDocs) - Category: Airplane, amateur-built - Serial number: 001 - Airframe hours: 269 - Engines: Rotax 583 80 horsepower reciprocating - Damage: Substantial damage - Flight: Personal, Part 91 - Registered owner: Frank G. Girgen Jr. - Airworthiness certificate: Special, Experimental (Special) - Last inspection: Annual, February 2, 1998, 8 hours before - Departed: PHOENIX, AZ ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 69; private; airplane ratings: single-engine land; medical: class 3, valid medical--w/ waivers/lim; seat: left; flight hours: 870 total, 289 in this make and model, 870 as pilot in command, 36 in the last 90 days, 1 in the last 30 days, 1 in the last 24 hours ## Weather - Conditions: Visual (VMC), Day - Wind: 140° at 6 knots - Visibility: 10 statute miles - Lowest ceiling: none - Temperature: 84 °F, dew point 37 °F - Altimeter: 29.00 inHg - Observed at: PHX, 30 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 (OpenAirDocs). - [Accident 19980606012529A](https://openairdocs.org/incident/19980606012529A), Jun 6, 1998: Amtr KITFOXII, Phoenix, AZ, Substantial damage. Experimental acft engine quit, pilot made emerg landing in a field. Deer valley, AZ. (-23) on June 8, 1998 I investigated an aircraft accident on a kit fox ii… From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.