LAX92LA365

NTSB accident investigation · Christen Industries Eagle II · Point Reyes Stn, CA · February 23, 1992

Accident · FatalLimited investigationFinal report
Date
February 23, 1992, 15:45 local (23:45 UTC)
Place
Point Reyes Stn, CA
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N24CEChristen Industries Eagle II
Weather
Visual (VMC) · Day
Status
Completed · report March 24, 1993
Report
Approved by Office Director
FAA report
19920223038589A
Case key
27745

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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Probable cause

Improper preflight planning by the pilot in command by exceeding the airplane's maximum acrobatic gross weight and exceeding the aft aerobatic center of gravity limit. Contributing to the accident was the pilot's decision to perform acrobatic maneuvers which resulted in a inadvertent stall from which recovery was not possible.

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.

Loss of control - in flightManeuvering
Preflight planning/preparation - improperPilot in commandCause
Aerobatics - performedPilot in command
Stall/spin - inadvertentPilot in commandFactor
In flight collision with terrain/waterDescent - uncontrolled
Remedial action - not possiblePilot in commandFactor

Analysis

A christen eagle ii lost control during acrobatic maneuvers, collided with coastal waters and was never recovered. The airplane was observed in a steep climb, did a wing over, and then entered a spin. After 4 to 5 rotations in the spin the airplane started to pull out. The airplane was then observed rotating as if in a spin and simultaneously flipping nose over until its tail struck the water. The pilot's total documented aeronautical experience in the accident airplane make and model was 14 flight hours. Investigators determined that the airplane's weight exceeded the maximum normal and aerobatic allowable gross weight. The center of gravity (CG) exceeded the aft limit of the airplane's aerobatic allowable CG. The airplane flight manual publishes a warning which states in part; 'pilots must take weight and balance responsibilities seriously. All aircraft must be loaded so that the aircraft CG will remain within safe limits at all times. All spin recovery procedures depend on having the CG remain within design limits.'

Aircraft

Registration
N24CE
Reported as
Christen Industries Eagle II
Category
Airplane, amateur-built
Serial number
WRIGHT-0001
Engine
Lycoming IO-360-A1D, 200 horsepower, reciprocating
Damage
Destroyed
Fire
Unknown
Flight
Personal · Part 91
Operator
Raouls, Bernard H.
Registered owner
Raouls, Bernard H.
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 2, 1991
Departed
STS · Sonoma, CA

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
39
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Flight hours
437 total · 14 in this make and model · 275 as pilot in command · 6 in the last 90 days · 5 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 4 knots
Visibility
30 statute miles
Lowest ceiling
None
Temperature
68 °F, dew point 54 °F
Altimeter
30.00 inHg
Observed at
STS, 37 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.