LAX97LA206

NTSB accident investigation · Bell UH-1B · Heron, CA · June 11, 1997

Accident · No injuriesLimited investigationFinal report
Date
June 10, 1997, 18:30 local (Jun 11, 1997, 01:30 UTC)
Place
Heron, CA
Injuries
1 uninjured
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N888SJBell UH-1B
Weather
Visual (VMC) · Day
Status
Completed · report May 21, 1998
Report
Approved by Office Director
FAA report
19970610013749A
Case key
29808

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

partial loss of engine power for undetermined reasons. A factor relating to the accident was that the engine lost power when the helicopter was outside (below) the limits of the height/velocity curve.

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 powerManeuvering - aerial application
Reason for occurrence undeterminedCause
Forced landingEmergency descent/landing
Autorotation - initiatedPilot in command
In flight collision with terrain/waterEmergency landing
Terrain condition - crop
Height/velocity curve - belowFactor

Analysis

The pilot experienced a partial loss of engine power at a low elevation above ground level, while spraying a tomato field. He initiated an autorotative landing, and the helicopter touched down hard in the field. During the landing sequence, a main rotor blade severed the tail boom. The engine continued operating for between 10 and 12 minutes. Wreckage examination was limited due to extensive fire damage, and the reason for the power loss was not determined.

Factual narrative

On June 10, 1997, at 1830 hours Pacific daylight time, a Bell UH-1B, N888SJ, owned and operated by San Joaquin Helicopters, experienced a partial loss of engine power while spraying a field of tomatoes near Heron, California. The pilot reported that he was flying at a low altitude over the field when power was lost. He autorotated and landed hard in the field. During the touchdown sequence, a main rotor blade severed the tail boom. The helicopter was destroyed by ground fire. The engine continued to operate for between 10 and 12 minutes following touchdown. The commercial pilot was not injured. Visual meteorological conditions prevailed at the time, and no flight plan was filed. The flight originated from the bed of a truck near the field around 1820.

According to the Federal Aviation Administration coordinator, no wires or other obstructions were noted in the vicinity of the accident site. The wreckage examination was limited because of extensive fire damage to the helicopter. No findings were noted concerning the loss of engine power.

Aircraft

Registration
N888SJ
Reported as
Bell UH-1B
Category
Helicopter
Serial number
1021
Airframe hours
6,947
Engine
Lycoming T-53-L-110, 900 horsepower, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Aerial application · Part 137
Registered owner
San Joaquin Helicopters
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · March 4, 1997 · 60 hours before

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
48
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Right
Flight hours
17,350 total · 3,000 in this make and model · 16,000 as pilot in command · 175 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
20° at 9 knots
Visibility
10 statute miles
Lowest ceiling
25,000 ft broken
Temperature
90 °F, dew point 50 °F
Altimeter
29.00 inHg

FAA reports on this event · 1

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