N247PV

Substantial
None

WESTERN INTERNATIONAL AVIA INC UH 1HS/N: 65-9649

Accident Details

Date
Friday, October 13, 2017
NTSB Number
WPR18LA004
Location
Arbuckle, CA
Event ID
20171007X12417
Coordinates
39.051944, -122.090553
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A collective control malfunction for reasons that could not be determined.

Aircraft Information

Registration
Make
WESTERN INTERNATIONAL AVIA INC
Serial Number
65-9649
Engine Type
Turbo-shaft
Year Built
1965
Model / ICAO
UH 1HPGK1
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
15
FAA Model
UH-1H

Registered Owner (Current)

Name
PACIFIC VALLEY AVIATION INC
Address
PO BOX 247
City
ARBUCKLE
State / Zip Code
CA 95912-0247
Country
United States

Analysis

On October 13, 2017, about 1015 Pacific standard time, a Williams Helicopter Corporation UH-1H helicopter, N247PV, was substantially damaged when it was involved in an accident near Arbuckle, California. The pilot was not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 repositioning flight.

The pilot and mechanic reported that, before the accident, the mechanic had adjusted the main rotor track and balance. After the mechanic made the final adjustments, the pilot hovered the helicopter to a wash rack for cleaning. Subsequently, while the pilot was repositioning the helicopter to a nearby landing cart, the collective began an uncommanded surge up and down just as the front portion of the landing skids were over the cart. The skids struck the cart causing damage to the front tips. The pilot attempted to land the helicopter on the cart as the collective continued to oscillate. The right skid slid off the cart and the helicopter rolled onto its right side and impacted the ground.

The mechanic reported that all components prior to the accident were in good working order and that the track and balance adjustments had resulted in satisfactory monitoring equipment readings prior to the accident.

Examination of the helicopter revealed that the airframe was substantially damaged, and that the main transmission, tail rotor, and right horizontal stabilizer had fracture separated. The pitch change links were all bent, and the main rotor blades were destroyed. Examination of the helicopter did not reveal evidence of any preaccident mechanical malfunctions or failures that would have precluded normal operation.

The pilot did not submit a National Transportation Safety Board Pilot/Operator Aircraft Accident Report Form 6120.1.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR18LA004