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September 5, 2007 · Higher Class Aviation Sport Hornet · N155HC

Santa Paula, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 5, 2007
Injury Outcomes
2 injuries (2 serious injuries)
Location
Santa Paula, CA
Aircraft
Higher Class Aviation Sport Hornet
Tail Number
N155HC
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
SEA07LA248

The flight instructor and his student were flying a newly manufactured special light sport airplane to the state of Washington. On their initial departure, the engine lost power and they landed straight ahead on the remaining runway. A new fuel flow meter with a restriction had been installed in the airplane. This unit was removed and a ground run up test along with a flight test was performed. They departed at 1700 and flew for approximately 2 hours with no difficulties. A witness said that the airplane was landing on runway 22, and appeared to be "too fast." He said the airplane aborted the landing and during the go-around, the engine began to sputter. The witness said the airplane started a turn back towards the runway when the airplane "spun" into a nearby river. The flight instructor said that when the power loss occurred at approximately 200 to 300 feet above ground level, he took control of the airplane and turned towards an open area to his left. As he banked, the airplane impacted terrain. Several structural pieces of the fuselage were bent or broken. A post accident examination of the engine identified no abnormalities and the reason for the loss of engine power was not determined.

NTSB Probable Cause

A loss of engine power during a go-around for undetermined reasons. Contributing to the accident was the flight instructor's failure to maintain adequate airspeed while maneuvering following the loss of power.

Full Narrative

On September 4, 2007, at 1914 Pacific daylight time, a Higher Class Aviation Sport Hornet, light sport aircraft, N155HC, was substantially damaged when it impacted terrain following a loss of control during a VFR go-around at Santa Paula Airport (SZP), Santa Paula, California. The flight instructor and his student were seriously injured. The student/owner was operating the airplane under 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the cross-country flight, which originated from Ramona, California, approximately 2 hours before the accident. No flight plan had been filed. The flight instructor said that they were transporting the newly manufactured airplane to the state of Washington. On their initial departure from Ramona, the engine lost power and they landed straight ahead on the remaining runway. A new fuel flow meter with a restriction had been installed in the airplane. This unit was removed and a ground run up test along with a flight test was performed. They departed at 1700 and flew for approximately 2 hours with no difficulties. A witness said that the airplane was landing on runway 22, and appeared to be "too fast." He said the airplane aborted the landing and during the go-around, the engine began to sputter. The witness said the airplane started a turn back towards the runway when the airplane "spun into the Santa Clara River." The flight instructor said that when the power loss occurred, at approximately 200 to 300 feet above ground level, he took control of the airplane and turned towards an open area to his left. As he banked, the airplane impacted terrain. Several structural pieces of the fuselage were bent or broken. A post accident examination of the engine by a National Transportation Safety Board investigator, an engine manufacturer's representative and the owner was accomplished on December 13, 2007. They identified no abnormalities with the engine; the reason for the loss of engine power was not determined.

Flight

Event TypeAccident
Event Time19:14 PDT
Nearest AirportSanta Paula Airport (0nm)
Runway22
Runway Length2665 ft
Runway Width60 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHigher Class Aviation Sport Hornet
Tail NumberN155HC
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 912 ULS · Reciprocating · 100
Seats2

People & Injuries

Injury Summary2 injuries (2 serious injuries)
Fatal0
Serious2
Minor0
Uninjured0
Total2
Crew 1Age 40 · First Class · Serious
Crew 2Age 31 · None · Serious

Conditions

ConditionsVMC
LightDusk
Wind240° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point57
Altimeter29.67 inHg
Observation Time01:55
Weather SourceWFAC

Appendix: Source Data