LAX05LA064

NTSB accident investigation · Jimmy Hill Lancair 235 · El Cajon, CA · January 12, 2005

Accident · FatalLimited investigationFinal report
Date
January 12, 2005, 14:38 local (22:38 UTC)
Place
El Cajon, CA
Injuries
1 fatal, 1 serious
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N124JHJimmy Hill Lancair 235
Weather
Visual (VMC) · Day
Status
Completed · report March 28, 2006
Report
Approved by Office Director
Parties
Textron-Lycoming, Federal Aviation Administration
FAA report
20050112001689A
Case key
60860

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

the pilot's failure to maintain the proper glidepath to avoid obstacles and terrain.

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 objectApproach - vfr pattern - final approach
Object - fence
Proper glidepath - not maintainedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground

Analysis

The airplane collided with an airport boundary fence about 500 feet short of the runway's approach end while on final approach for landing. A witness driving a pickup truck said that she saw the airplane cross in front of her truck about 10 feet above the ground going very fast and low. Immediately after the airplane crossed her path, it struck the airport boundary fence with its right main landing gear and impacted the dirt terrain beyond. The wreckage was about 500 feet from the approach end of the runway, and about 1,800 feet from the runway's displaced threshold. The passenger of the airplane said that this was her first flight with the pilot. She recalls that the flight was very pleasant, and the pilot did not express any concerns regarding the airplane or the environment. As they approached the runway for landing the pilot said to her "Do you see the runway? I will reduce some power for landing." Moments after that statement the airplane collided with the airport boundary fence. Examination of the airplane revealed no evidence of a preimpact malfunction or failure of the control system or power plant.

Factual narrative

On January 12, 2005, at 1438 Pacific standard time, a Lancair 235, N124JH, collided with a fence while on final approach for landing at Gillespie Field, El Cajon, California. The commercial pilot/owner operated the airplane under the provisions of 14 CFR Part 91. The pilot was fatally injured and the passenger was seriously injured; the airplane was substantially damaged. Visual meteorological conditions prevailed, and a flight plan had not been filed. The flight originated in Yuma, Arizona, about 1330.

A witness driving a pickup truck told the National Transportation Safety Board investigator that she saw the airplane cross in front of her truck about 10 feet above the ground going very fast and low. Immediately after the airplane crossed her path, it struck the airport boundary fence with the right main landing gear, and impacted the dirt terrain beyond. The airport manager said that the wreckage was about 500 feet from the approach end of runway 27 right, and about 1,800 feet from the runway's displaced threshold.

The passenger of the airplane stated that this was her first flight with the pilot. She recalls that the flight was very pleasant, and the pilot did not express any concerns regarding the airplane or the environment. As they approached the runway for landing the pilot said to her "Do you see the runway? I will reduce some power for landing." Moments after that statement the airplane collided with the airport boundary fence.

On January 24, 2005, the Safety Board investigator and Textron-Lycoming technical representative examined the airplane and engine. The airplane's flight control cables and connections were traced from the cockpit to their respective control surfaces, demonstrating continuity. The right main landing gear sheared half off at mid strut, and the left main landing gear strut was intact. Seven gallons of fuel was recovered from the left fuel tank and 12 gallons were recovered from the right tank. During the engine exam, they achieved thumb compression on all cylinders, all valves lifted an appropriate amount and in firing order, and magneto timing on both magnetos was determined to be 25 degrees. The spark plugs were gray in color, which corresponded to normal service wear according to the Champion Aviation Check-A-Plug chart (AV-27), and they did not exhibit any mechanical damage.

Aircraft

Registration
N124JH
Reported as
Jimmy Hill Lancair 235
Category
Airplane, amateur-built
Serial number
001
Engine
Textron Lycoming O-320, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
James G Thompson Jr
Airworthiness certificate
Special, Experimental (Special)
Departed
KYUM · Yuma, AZ
Destination
SEE · El Cajon, CA
Airport
KSEE · Gillespie Field, runway 27R, 5,341 × 100 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
67
Injuries
Fatal
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
289 total · 96 in this make and model · 194 as pilot in command · 15 in the last 90 days · 6 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 6 knots
Visibility
25 statute miles
Lowest ceiling
None
Temperature
57 °F, dew point 43 °F
Altimeter
30.12 inHg
Observed at
KSEE

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.