SEA00LA157

NTSB accident investigation · Hamer Lancair 235 · Chiloquin, OR · August 10, 2000

Accident · No injuriesLimited investigationFinal report
Date
August 10, 2000, 16:00 local (23:00 UTC)
Place
Chiloquin, OR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N84LHHamer Lancair 235
Weather
Visual (VMC) · Day
Status
Completed · report May 18, 2001
Report
Approved by Office Director
FAA report
20000810009779A
Case key
49987

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

Loss of engine power due to a fracture and separation of the engine's crankshaft. A factor was a vehicle on the roadway.

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 engine powerCruise
Engine assembly,crankshaft - failureCause
Forced landingDescent - emergency
In flight collision with objectEmergency descent/landing
Object - vehicleFactor

Analysis

Shortly after takeoff, at an altitude of approximately 150 feet above ground level (AGL), the airplane developed a rough running engine and the pilot initiated a forced landing to a nearby highway. The pilot stated that he planned on landing the airplane on a non-congested area of the highway, however, the aircraft collided with a flatbed tractor-trailer combination that was traveling on the Interstate. Post-accident inspection and teardown of the airplane's engine revealed that the engine's crankshaft was fractured and had separated between the number three and number four crankpins.

Factual narrative

On August 10, 2000, about 1600 Pacific daylight time, a Hamer Lancair 235, N84LH, sustained substantial damage during an off airport forced landing following a loss of engine power near Chiloquin, Oregon. The airplane is owned by the pilot and was being operated as a personal flight under the provisions of Title 14 CFR Part 91, when the accident occurred. The private pilot, who was the sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed and no flight plan was filed. There was no fire and no report of ELT activation. The flight originated from Chiloquin, Oregon.

In a telephone interview and written statement, the pilot reported that the aircraft's engine "...began running rough" and he subsequently made a precautionary landing to a nearby airport. After landing, the pilot inspected the airplane and determined that the rough running engine was the result of improper ignition timing. A certified mechanic retimed the magnetos to fire 25 degrees before top-dead-center. After a ground run and recheck of the ignition timing, the pilot chose to test fly the airplane before continuing the cross-country flight. Shortly after takeoff, at an altitude of approximately 150 feet above ground level (AGL), the airplane again developed a rough running engine and the pilot initiated a forced landing to a nearby highway. The pilot stated that he planned on landing the airplane on a non-congested area of the highway; however, while maneuvering for the landing the airplane collided with a flatbed tractor-trailer combination that was traveling on Interstate Highway 97. The airplane came to rest on top of the forward most section of the trailer, against the tractor. The driver of the semi-truck was not injured.

Post-accident inspection and teardown of the airplane, by the pilot and representatives for the Sacramento, California, Flight Standards District Office (FSDO), revealed that the engine's crankshaft was fractured and had separated between the number three and number four crankpins.

The aircraft was powered by a modified Lycoming O-290-G series engine. According to the engine manufacture, the O-290-G series engines were designed and built specifically for ground power applications.

Aircraft

Registration
N84LH
Reported as
Hamer Lancair 235 (LANCAIR 23)
Category
Airplane, amateur-built
Serial number
173
Airframe hours
450
Engine
Lycoming O-290-G, 165 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Howard A. Hamer
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · May 12, 2000 · 16 hours before
Departed
2S7 · Chiloquin, OR
Destination
2S7

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
64
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
768 total · 606 in this make and model · 768 as pilot in command · 11 in the last 90 days · 5 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
20° at 11 knots
Visibility
10 statute miles
Lowest ceiling
25,000 ft broken
Temperature
75 °F, dew point 45 °F
Altimeter
30.00 inHg
Observed at
KLM, 180 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.