FTW97LA021

NTSB accident investigation · Hughes 369D · Watkins, CO · October 19, 1996

Accident · No injuriesLimited investigationFinal report
Date
October 19, 1996, 13:45 local (19:45 UTC)
Place
Watkins, CO
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N34CMHughes 369D
Weather
Visual (VMC) · Day
Status
Completed · report February 1, 1997
Report
Approved by Office Director
FAA report
19961019033099A
Case key
20097

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 flight instructor's improper decision to attempt a hovering autorotation during gusty wind conditions. A factor was the gusty wind.

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.

Miscellaneous/otherLanding
Weather condition - gustsFactor
In-flight planning/decision - improperPilot in command(cfi)Cause

Analysis

The instructor was demonstrating autorotation techniques to his student. He stated at a speed of less than 10 knots, he entered a 'hovering auto(rotation)' to runway 17 from an altitude of 3 feet agl. He estimated the wind to be from 170 degrees at 12 to 15 knots. Recorded wind at Denver International Airport, located 10 miles northwest of the accident site, was from 290 degrees at 12 knots. The helicopter touched down and the main rotor blades struck the tail boom. The pilot said this was a 'fairly common occurrence' with this particular helicopter make and model operating under 'low rotor rpm and gusty wind.' A spokesman for the helicopter manufacturer said that if the helicopter had been landed upwind, the accident would not have occurred. He added that if gusty wind conditions were present, autorotation demonstrations should not have been attempted.

Factual narrative

On October 19, 1996, approximately 1345 mountain daylight time, a Hughes 369D, N34CM, was substantially damaged when its main rotor blades struck the tail boom while landing at Watkins, Colorado. The certified flight instructor and private pilot receiving instruction were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for this training flight conducted under Title 14 CFR Part 91.

The following is based on the Pilot/Operator Aircraft Accident Report. The instructor said he was demonstrating autorotation techniques to his student. He wrote, "During slow forward flight (less than 10 knots), hovering auto(rotation) was initiated at approximately 3 feet agl. Following a normal touch down, and deceleration, blades contacted tail boom." The instructor added, "Fairly common occurrence with 500 series helicopter under similar circumstances, i.e. low rotor rpm and gusty wind."

According to a spokesman for the McDonnell Douglas Helicopter Company's Flight Safety Department, the accident is not a common occurrence. The spokesman said if the helicopter had landed upwind, the accident should not have occurred. He also stated that if gusty wind conditions were present, autorotation demonstrations should not have been performed.

The pilot pilot said he landed on runway 17 and estimated the wind to be from 170 degrees at 12 to 15 knots. Recorded wind at Denver International Airport, located 10 miles northwest of Front Range Airport, was from 290 degrees at 12 knots.

Aircraft

Registration
N34CM
Reported as
Hughes 369D
Category
Helicopter
Serial number
1194D
Airframe hours
5,931
Engine
Allison 250-C20B, 375 horsepower, turbo shaft
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
James L. Dean
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 11, 1996 · 40 hours before
Departed
APA · Englewood, CO
Destination
FTG
Airport
FTG · Front Range, runway 17, 8,001 × 100 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
22
Certificates
Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
2,600 total · 100 in this make and model · 2,400 as pilot in command · 131 in the last 90 days · 39 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
290° at 12 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 45 °F
Altimeter
29.00 inHg
Observed at
DEN, 10 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.