LAX97LA179

NTSB accident investigation · Hiller UH-12E · Truckee, CA · May 14, 1997

Accident · Serious injuriesLimited investigationFinal report
Date
May 14, 1997, 11:59 local (18:59 UTC)
Place
Truckee, CA
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N7082DHiller UH-12E
Weather
Visual (VMC) · Day
Status
Completed · report April 10, 1998
Report
Approved by Office Director
FAA report
19970514010989A
Case key
29787

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

A loss of engine power for undetermined reasons. A factor in the accident was the unsuccessful attempt to release the long line from the belly hook after it became entangled in a tree.

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 powerTakeoff - initial climb
Reason for occurrence undeterminedCause
Forced landingEmergency landing after takeoff
In flight collision with terrain/waterEmergency landing after takeoff
External load cable/hook - entangledCause
Object - tree(s)Factor
Emergency procedure - restrictedPilot in commandFactor
Diverted attentionPilot in commandFactor

Analysis

The pilot reported that the purpose of the accident flight was to move a 200-foot long line to a new clearing area. After takeoff from the dirt strip, the pilot heard a change in the sound of the engine. He stated that he was turning back to make an emergency landing and attempted to release the long line; however, it became entangled around a tree and the helicopter impacted the ground. FAA inspectors examined the helicopter and the long line, but could not make a determination of when the long line became entangled in the tree; during takeoff or upon returning to land. Examination of the engine revealed continuity throughout, with no preexisting malfunctions noted.

Factual narrative

On May 14, 1997, about 1159 hours Pacific daylight time, a Hiller UH-12E, N7082D, crashed during an emergency landing 7 miles northeast of Truckee, California. The helicopter was substantially damaged, and the commercial instrument rated pilot was seriously injured. Visual meteorological conditions existed for the 14 CFR Part 133 external load operation, and no flight plan was filed. The flight was originating from a private dirt helipad in Truckee at the time for the purpose of moving a 200-foot long line to a work site.

The pilot stated that after physically "hooking up the long line to the belly hook, I climbed back in and started the aircraft." He stated that the primary mission for this flight was to drop off the long line at a new site and pick up the woodcutters. The pilot reported that the preflight and engine start appeared normal. After lifting to a hover, he repositioned the aircraft over the long line. He said that "As I transitioned to forward flight, I experienced a left yaw and decreasing aircraft noises." The pilot then picked out a place to make an emergency landing and then moved his attention back inside the aircraft, trying to switch his radio from FM to VHF to transmit on the Truckee Unicom. Prior to trying to switch the radio frequency ". . .the RPM rapidly increased causing the aircraft to yaw to the right and increase in forward speed." The pilot reported that corrective action was taken and he then attempted to release the long line; however, it became entangled around a tree and the helicopter impacted the ground.

FAA inspectors from the Reno, Nevada, Flight Standards District Office responded to the accident site and examined both the long line and the helicopter. According to their report, they could not make a determination of when the long line became entangled in the tree; during takeoff or upon returning to land.

The wreckage was removed to the operator's home base in White City, Oregon, where an engine inspection was accomplished. An FAA inspector from the Hillsboro, Oregon, Flight Standards District Office was present at the engine inspection. Engine continuity was established and no preexisting malfunctions were noted. See attached report.

Aircraft

Registration
N7082D
Reported as
Hiller UH-12E
Category
Helicopter
Serial number
5193
Airframe hours
2,802
Engine
Allison 250-C20B, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Positioning · Part 133
Registered owner
Croman Corporation
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · April 24, 1997 · 60 hours before
Airport
Private Dirt Strip

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
37
Certificates
Military, Commercial
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
3,878 total · 855 in this make and model · 2,934 as pilot in command · 169 in the last 90 days · 27 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 8 knots, gusting 18
Visibility
30 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point 37 °F
Altimeter
30.00 inHg
Observed at
TRK, 7 nm away

FAA reports on this event · 1

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