- Date
- February 10, 1994, 11:13 local (18:13 UTC)
- Place
- Tucson, AZ
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Initial climb
- Aircraft
- N187ESGansheimer Evans VP2
- Weather
- Visual (VMC) · Day
- Status
- Completed · report December 19, 1994
- Report
- Approved by Office Director
- FAA report
- 19940210001989A
- Case key
- 28658
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
the pilot's failure to attain and maintain sufficient flying speed during the first flight test of his experimental homebuilt. A factor in the accident was the pilot's selection of a propeller inadequate for the airframe and engine combination.
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.
Analysis
The pilot reported that the takeoff seemed fine until the aircraft got out of ground effect. The aircraft began oscillating in roll and did not want to climb. The pilot noted that the engine was producing full power throughout the sequence. According to the pilot, the aircraft 'mushed back to the ground at 500 feet per minute' and impacted the ground in a slight nose- high attitude about 300 feet off the end of the runway. The pilot said he believes the roll oscillation was caused by an impending stall buffet and the lack of thrust was due to the propeller being of insufficient size.
Factual narrative
On February 10, 1994, at 1113 mountain standard time, a homebuilt experimental Gansheimer Evans VP2 airplane, N187ES, experienced a thrust deficiency in the takeoff initial climb from runway 6L at Ryan Field, Tucson, Arizona. The aircraft subsequently stalled and mushed into the ground about 300 feet beyond the departure end of the runway. The aircraft was on the first test flight following construction completion and Federal Aviation Administration (FAA) certification in the experimental category. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft incurred substantial damage. The certificated private pilot, the sole occupant, was not injured. The flight was originating at the time of the mishap as a local area test flight.
The pilot reported that the takeoff seemed fine until the aircraft got out of ground effect. The aircraft began oscillating in roll and did not want to climb. The pilot noted that the engine was producing full power throughout the sequence. According to the pilot, the aircraft "mushed back to the ground at 500 feet per minute" and impacted the ground in a slight nose- high attitude about 300 feet off the end of the runway.
The pilot said he believes the roll oscillation was caused by an impending stall buffet and the lack of thrust was due to the propeller being of insufficient size.
Aircraft
- Registration
- N187ES
- Reported as
- Gansheimer Evans VP2
- Category
- Airplane, amateur-built
- Serial number
- VP-2-187
- Airframe hours
- 10
- Engine
- Gansheimer VW-1835-CC, 60 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Operator
- Gansheimer, Edger L.
- Registered owner
- Gansheimer, Edger L.
- Airworthiness certificate
- Special, Experimental (Special)
- Last inspection
- Annual · December 27, 1993 · 5 hours before
- Airport
- RYN · Ryan Field, runway 6L, 4,900 × 75 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
- 48
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Medical
- Class 3, Valid Medical--w/ waivers/lim
- Seat
- Center
- Flight hours
- 179 total · 10 in this make and model · 128 as pilot in command · 6 in the last 90 days · 1 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- Calm
- Visibility
- 50 statute miles
- Lowest ceiling
- None
- Temperature
- 64 °F, dew point 55 °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.