20031016034579A

Accident · Substantial damage

FAA accident report · Bell UH-1B · Durham, CA · October 16, 2003

Date
October 16, 2003 · 13:30 local
Place
Durham, CA
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Operator
P8QG
Damage
Substantial damage
Aircraft
N234SJ
NTSB investigation
NTSBLAX04LA015
Reported as
Bell UH1B
Reported engine
Lycoming T53L11D
People aboard
2
Fatal injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Mr. Porter was simulating part 136 spray operations as a demonstration for the 1st grade class of Durham elementary school. The class was on a field trip and was watching the simulated spraying of a field by Mr. Porter. After the 3rd pass of the field, while preparing to land, the helicopter lost power. Mr. Porter performed an autorotation into the field. The left landing gear skid failed and the helicopter rolled onto its left side. Substantial damage was done to the forward left side of the fuselage, the left horizontal stabilizer and the transmission mounting structure. The main rotor blades were destroyed by contact with the ground. Initial inspection of the engine showed failure of the power turbine wheel. No operation unit coordination at this time. Operations inspector not assigned at this time. FAA iic not assigned at this time. This report will be amended as further information is received.

As the FAA filed it

(-23) MR. PORTER WAS SIMULATING PART 136 SPRAY OPERATIONS AS A DEMONSTRATION FOR THE 1ST GRADE CLASS OF DURHAM ELEMENTARY SCHOOL. THE CLASS WAS ON A FIELD TRIP AND WAS WATCHING THE SIMULATED SPRAYING OF A FIELD BY MR. PORTER. AFTER THE 3RD PASS OF THE FIELD, WHILE PREPARING TO LAND, THE HELICOPTER LOST POWER. MR. PORTER PERFORMED AN AUTOROTATION INTO THE FIELD. THE LEFT LANDING GEAR SKID FAILED AND THE HELICOPTER ROLLED ONTO ITS LEFT SIDE. SUBSTANTIAL DAMAGE WAS DONE TO THE FORWARD LEFT SIDE OF THE FUSELAGE, THE LEFT HORIZONTAL STABILIZER AND THE TRANSMISSION MOUNTING STRUCTURE. THE MAIN ROTOR BLADES WERE DESTROYED BY CONTACT WITH THE GROUND. INITIAL INSPECTION OF THE ENGINE SHOWED FAILURE OF THE POWER TURBINE WHEEL. NO OPERATION UNIT COORDINATION AT THIS TIME. OPERATIONS INSPECTOR NOT ASSIGNED AT THIS TIME. FAA IIC NOT ASSIGNED AT THIS TIME. THIS REPORT WILL BE AMENDED AS FURTHER INFORMATION IS RECEIVED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N234SJ · 1

Matched to the same aircraft by N-number and date.