Plane Crash List

Vangilder CHRISTEN EAGLE II N5JV

22 March 2001 · Ogden, Utah, United States · Fatal

Summary

On 22 March 2001 at about 22:18 local time, a Vangilder CHRISTEN EAGLE II registered N5JV was involved in an accident near Ogden, Utah, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 22:18
Classification
Accident
Location
Ogden, Utah, United States
Coordinates
41.3208, -112.1633
Aircraft
Vangilder CHRISTEN EAGLE II
Registration
N5JV
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Instructional
Phase of flight
Not recorded
Route
Ogden → Unknown
Aircraft damage
Destroyed
Weather
VMC
Light
Day
NTSB number
DEN01FA074

People

2 people died.

On board Died Serious Minor Uninjured
2 2 0 0 0

Probable cause

the flight instructor's failure to maintain aircraft control while maneuvering and the subsequent inadvertent stall/spin. A contributing factor was the flight instructor's lack of familiarity with the airplane.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

On the day of the accident, the flight instructor, who had not previously flown the homebuilt, experimental airplane, flew the airplane twice, once with the previous owner and once with the current owner. They both reported that during their respective flights with the flight instructor, they flew to a practice area and performed slow flight and stalls at an altitude of approximately 2,500 feet agl. The flight instructor then flew with the commercial pilot receiving instruction to the practice area where radar data indicates that they were maneuvering at the time the airplane disappeared from radar. There were no witnesses to the accident. Examination of the accident site indicated the airplane impacted the ground in a near vertical descent. Examination of the airplane revealed no evidence of any pre-existing mechanical discrepancies that would have prevented normal operation. The airplane's designer recommended a maximum gross weight for aerobatic flight of 1,520 pounds and for normal flight of 1,600 pounds; the airplane's estimated total weight at the time of takeoff was 1,610 pounds.

Quoted verbatim from the NTSB record.

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