N43280 Houts Avid Mark IV accident

NTSB CEN12CA035 · 2011-10-21 · Hibbing, MN

Docket — crew, injuries and powerplant

Summary

The pilot reported that during the local flight the engine lost oil pressure and the cockpit began to fill with smoke. He immediately reduced engine power to idle and performed a forced landing to a nearby field. The airplane collided with a barbed wire fence during the landing roll and subsequently nosed over. The fuselage, right wing, and vertical stabilizer were substantially damaged. A postaccident inspection revealed that the oil supply line to the oil cooler had ruptured, which allowed oil to come in contact with the engine's hot exhaust, producing smoke. The rubber, automobile-style oil line had failed immediately adjacent to its respective oil cooler inlet fitting. The hose clamp used to secure the oil line to the inlet fitting was not properly positioned over the fitting, which allowed the unsupported hose clamp to abrade through the oil line.

Full narrative

The pilot reported that during the local flight the engine experienced a loss of oil pressure and the cockpit began to fill with smoke. He immediately reduced engine power to idle and performed a forced landing to a nearby field. The airplane collided with a barbed-wire fence during the landing rollout and subsequently nosed-over. The fuselage, right wing, and vertical stabilizer were substantially damaged. A postaccident inspection revealed that the oil supply line to the oil cooler had ruptured, which allowed oil to come in contact with the engine's hot exhaust producing smoke. The rubber, automobile-style, oil line had failed immediately adjacent to its respective oil cooler inlet fitting. The hose-clamp used to secure the oil line to the inlet fitting was not properly positioned over the fitting, which allowed the unsupported hose-clamp to abrade through the oil line.

Probable cause

The improper installation of a hose clamp, which resulted in an oil line rupture and subsequent loss of engine oil pressure. The National Transportation Safety Board determined the probable cause of this accident.

Circumstances

Event type
Accident
Highest injury
Minor
Weather conditions
Visual Meteorological Cond
Light condition
Day
Sky condition
NONE
Ceiling (ft)
0
Visibility (sm)
10
Wind direction
260
Wind speed (kt)
8
Temperature (F)
57
Distance from field
0.0

Aircraft

RegistrationMakeModelDamageFAR part
N43280 Houts Avid Mark IV SUBS 091

Sequence of events

#OccurrencePhase
1 Prior to flight Aircraft maintenance event Standing
2 Enroute Powerplant sys/comp malf/fail defining Climb
3 Enroute Fire/smoke (non-impact) Climb
4 Emergency descent Off-field or emergency landing Descent
5 Landing-landing roll Collision with terr/obj (non-CFIT) Cruise

Findings

Finding
Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng oil sys-Incorrect service/maintenance cause
Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng oil sys-Failure cause
Environmental issues-Physical environment-Object/animal/substance-Fence/fence post-Contributed to outcome factor
Personnel issues-Task performance-Maintenance-(general)-Maintenance personnel cause