LAX05CA313

NTSB accident investigation · Hiller UH 12-E · Five Points, CA · September 22, 2005

Accident · No injuriesData collectionFinal report
Date
September 21, 2005, 22:00 local (Sep 22, 2005, 05:00 UTC)
Place
Five Points, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N141HAHiller UH 12-E
Weather
Visual (VMC) · Night/bright
Status
Completed · report January 31, 2006
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20050921020819A
Case key
62549

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

The pilot's failure to refuel the helicopter, which resulted in fuel exhaustion.

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 power(total) - nonmechanicalManeuvering
Refueling - not performedPilot in commandCause
Fluid,fuel - exhaustionCause
Forced landingEmergency descent/landing
Hard landingEmergency landing
Terrain condition - open field

Analysis

All engine power was lost while the pilot was maneuvering at a low altitude during an aerial application flight. The pilot made a hard forced landing in an open field and bounced. Thereafter, the main rotor blades severed the tail boom. The accident occurred during the third aerial application flight. For the first flight he had refueled with 25 gallons of fuel, and the helicopter was carrying a full load of insecticide. On the second flight he took on only insecticide. On the third (accident flight), he again only took on insecticide. The pilot reported that his normal procedure is to refuel on the second flight, which he did not do. He reported that with 25 gallons of fuel on board he could fly about 20 minutes with a 10-minute reserve. The pilot acknowledged that he should have refueled after the second application, but failed to do so and experienced fuel exhaustion. No mechanical anomalies were reported with the helicopter.

Factual narrative

On September 21, 2005, at 2200 Pacific daylight time, the pilot flying a Hiller UH 12-E, N141HA, made a hard forced landing near Five Points, California. The pilot owned the helicopter, and he operated it under the provisions of 14 CFR Part 137 as an aerial application flight. The helicopter sustained substantial damage, and the commercial helicopter pilot was not injured. Visual meteorological conditions prevailed for the flight that departed about 30 minutes prior to the accident. No flight plan had been filed.

A Federal Aviation Administration (FAA) inspector interviewed the pilot. The pilot reported to the FAA inspector that he had just finished spraying a biological organic insecticide and was returning to the truck to reload and refuel. He was making a left pedal turn, and returning to the truck when the engine lost all power. At the time the helicopter's airspeed was about zero miles per hour, and the helicopter was about 75 feet about the ground. The pilot reported that he leveled the skids and landed hard on the flat open field. Thereafter, the helicopter bounced into the air, landed again, spun around two times, and finally came to rest on its right skid supported by the main rotor blades. The pilot reported that during the accident sequence the main rotor blades chopped off the tail boom.

According to the pilot, he had sprayed two 25-acre blocks prior to the accident. For the first flight he had refueled with 25 gallons of fuel, and the helicopter was carrying a full load of insecticide. On the second flight he took on only insecticide. On the third (accident flight), he again only took on insecticide. The pilot reported that his normal procedure is to refuel on the second flight, which he did not do. He reported that with 25 gallons of fuel on board he could fly about 20 minutes with a 10-minute reserve.

The pilot told the FAA that he should have refueled after the second block, and he ran out of fuel. He further reported that there were no mechanical anomalies noted with the helicopter.

Aircraft

Registration
N141HA
Reported as
Hiller UH 12-E
Category
Helicopter
Serial number
HA 3041
Engine
Lycoming VO-540-C2A, 305 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
Huron AG Helicopter Inc.
Registered owner
Clay H. McBain
Airworthiness certificate
Special, Restricted (Special)
Departed
Five Points, CA
Destination
Five Points, CA

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
60
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2
Seat
Center
Flight hours
8,000 total · 6,000 in this make and model · 100 in the last 90 days · 40 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/bright
Wind
315° at 2 knots
Visibility
25 statute miles
Lowest ceiling
None
Temperature
158 °F
Altimeter
29.89 inHg

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.