LAX01LA058

NTSB accident investigation · Robinson R22 Beta · North Las Vegas, NV · December 14, 2000

Accident · Minor injuriesLimited investigationFinal report
Date
December 14, 2000, 14:02 local (22:02 UTC)
Place
North Las Vegas, NV
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N7189KRobinson R22 Beta
Weather
Visual (VMC) · Day
Status
Completed · report November 6, 2001
Report
Approved by Office Director
FAA report
20001214041039A
Case key
50781

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-in-command's inadequate supervision of the second pilot and delay taking control of the aircraft and implementing remedial action. A factor in the accident was the second pilot's interference with the pilot-in-command's operation of the collective flight control.

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.

Hard landingLanding - flare/touchdown
Autorotation - intentional
Rotor rpm - lowCopilot/second pilot
Airspeed - lowCopilot/second pilot
Remedial action - delayedPilot in commandCause
Lowering of collective - restrictedCopilot/second pilotFactor
Supervision - inadequatePilot in commandCause

Analysis

During the practice 180-degree autorotation landing, the helicopter touched down hard, the main rotor severed the tail boom, and the helicopter rolled on its side. The first pilot reported that, during four of six prior autorotations performed by the second pilot, it was necessary for the him to assume control of the helicopter and make power recoveries due to high landing flares, improper airspeed, and improper rotor rpm. During the seventh autorotation, the landing approach that resulted in the accident, the first pilot stated that the second pilot first let the main rotor rpm get too high, then too low, and then let airspeed get low. The first pilot again took control and applied engine power, but this time, as the ground approached more rapidly than before due to recovery from a low airspeed and low rpm condition, the second pilot "began to scream" and interfered with the first pilot's control by pulling up on the collective. The first pilot could not overpower him, the rotor rpm decayed further, and a hard landing resulted. The first pilot reported there were no mechanical problems with the helicopter. The second pilot reported that, as he initiated the final autorotation, the first pilot said "hold on, hold on," and the second pilot thought he was again taking the controls and relinquished them to him. As the helicopter continued the descent, the first pilot continued to say "hold on, hold on," and the second pilot became worried because the ground approached rapidly and the low rpm horn had been on for several seconds. When the second pilot realized they were going to crash and the first pilot wasn't doing anything to arrest the situation, he (the second pilot) took the controls and tried to flare and pulled full up collective to cushion the landing.

Factual narrative

On December 14, 2000, at 1402 hours Pacific standard time, a Robinson R22 Beta, N7189K, was substantially damaged during a practice 180-degree autorotation landing to a flood control basin, 8 miles northwest of the North Las Vegas, Nevada airport. During the landing the helicopter touched down hard, the main rotor severed the tail boom, and the helicopter rolled over. The commercial certificated flight instructor/first pilot received minor injuries and the commercial certificated flight instructor/second pilot was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the instructional flight that originated at North Las Vegas about 1330. The flight was operated under 14 CFR Part 91 by West Air Helicopters.

The first pilot was a senior instructor, and the purpose of the flight was to evaluate the second pilot for hire as a flight instructor. They proceeded to a floodwater retention basin that the operator used as a practice area. The elevation was 3,400 feet mean sea level. The first pilot reported there were no mechanical problems with the helicopter.

In his report to the Safety Board, the first pilot reported that he asked the second pilot to demonstrate some straight in and 180-degree autorotation landings. During four of six autorotations it was necessary for the first pilot to assume control of the helicopter and make power recoveries due to high landing flares, improper airspeed, and improper rotor rpm. During the seventh autorotation, the landing approach that resulted in the accident, the first pilot stated that the second pilot first let the main rotor rpm get too high, then too low, and then let airspeed get low. The first pilot took control and applied engine power, but this time, as the ground approached more rapidly than before due to recovery from a low airspeed and low rpm condition, the second pilot "began to scream" and interfered with the first pilot's control by pulling up on the collective. The first pilot could not overpower him, the rotor rpm decayed, and a hard landing resulted.

In his report to the Safety Board, the second pilot reported that, as he initiated the final autorotation, the first pilot said "hold on, hold on," and the second pilot thought he was again taking the controls and relinquished them to him. As the helicopter continued the descent, the first pilot continued to say "hold on, hold on," and the second pilot became worried because the ground approached rapidly and the low rpm horn had been on for several seconds. When the second pilot realized they were going to crash and the first pilot wasn't doing anything to arrest the situation, he (the second pilot) took the controls and tried to flare and pulled full up collective to cushion the landing.

Aircraft

Registration
N7189K
Reported as
Robinson R22 Beta
Category
Helicopter
Serial number
3118
Airframe hours
225
Engine
Lycoming O-360-J2A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
West Air Helicopters
Registered owner
Spitzer Helicopter Leasing Co
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · December 5, 2000 · 22 hours before
Departed
VGT

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
25
Certificate
Commercial
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
657 total · 654 in this make and model · 600 as pilot in command · 305 in the last 90 days · 86 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
135 °F, dew point 95 °F
Altimeter
30.00 inHg
Observed at
VGT, 8 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.