SEA83FYK04

NTSB accident investigation · Homebuilt Christen Eagle II · Bend, OR · June 5, 1983

Accident · FatalFinal report
Date
June 5, 1983, 13:56 local (20:56 UTC)
Place
Bend, OR
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N4GTHomebuilt Christen Eagle II
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19830605022549A
Case key
39646

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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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.

In flight collision with terrain/waterManeuvering
Aerobatics - performedPilot in commandFactor
Weather condition - high density altitudeFactor
Proper altitude - not selectedPilot in commandCause

Analysis

Upon completion of his routine during an airshow, the plt stated to the show announcer that he would do a low pass down the rwy followed by a vertical climb to a hammerhead stall & then into a lomcevak aerobatic maneuver. This maneuver is aclimbing outside snap roll that is performed in such a way that the acft's upward inertia overcomes its normal aerodynamic snap roll tendencies, causing it to tumble end-over-end briefly before it deteriorates into a flat inverted spin. Entry into the maneuver with acft such as the eagle iiis at an altitude of at least 1,000 AGL at sea level. The entry altitude must be increased to compensate for the reduction of the acft's vertical penetration which occurs when the maneuver is performed at higher altitudes. A videotape of the accident showed that the plt initiated the maneuver ata pull-up altitude of 500-600 ft AGL. The density altitude at the altitude that the plt entered the maneuver was 6,800 ft.

Aircraft

Registration
N4GT
Reported as
Homebuilt Christen Eagle II (CHRISTEN E)
Category
Airplane, amateur-built
Serial number
T-0033
Airframe hours
366
Engine
Lycoming IO-360-A1B6D, 200 horsepower, reciprocating
Damage
Destroyed
Flight
Part 91
Registered owner
Gerald Virgil Thom
Last inspection
Annual · January 31, 1983 · 45 hours before
Airport
S07 · Bend Muni, runway 34, 3,803 × 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
46
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Rear
Toxicology
Performed
Flight hours
1,022 total · 366 in this make and model · 930 as pilot in command · 25 in the last 90 days · 17 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
340° at 10 knots
Visibility
45 statute miles
Lowest ceiling
20,000 ft broken
Temperature
70 °F, dew point 36 °F
Altimeter
30.00 inHg
Observed at
RDM, 15 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.