IAD02LA033

NTSB accident investigation · Hughes 269C · Lorain, OH · February 19, 2002

Accident · No injuriesLimited investigationFinal report
Date
February 19, 2002, 15:10 local (20:10 UTC)
Place
Lorain, OH
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N9296FHughes 269C
Weather
Visual (VMC) · Day
Status
Completed · report April 8, 2003
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20020219004849A
Case key
54212

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 NTSB’s determination of the probable cause, and any contributing factors.

The pilot's failure to maintain directional control during takeoff.

Analysis

The accident occurred during the pilot's second solo takeoff in a helicopter, and his first takeoff from a platform. After quickly lifting off, the helicopter began a 360-degree "aggravated spin" to the right. The pilot then "chopped" the throttle and the collective, and the helicopter "dropped fast." The helicopter impacted the platform, then rolled onto its left side and impacted the ground. Examination of the helicopter revealed no mechanical discrepancies.

Factual narrative

On February 19, 2002, at 1510 eastern standard time, a Hughes 269C helicopter, N9296F, was substantially damaged during a takeoff attempt from a platform at the Lorain County Regional Airport (LPR), Lorain, Ohio. The certificated private pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the instructional flight conducted under 14 CFR Part 91.

In a telephone interview, the pilot reported that during the takeoff, he lifted the helicopter "quickly" off the platform. As the helicopter gained altitude, it began a turn to the right, and the pilot applied left pedal. As the pilot continued to increase the collective, the helicopter began a 360-degree "aggravated spin" to the right.

The pilot then "chopped" the throttle and the collective, and the helicopter "dropped fast." He added a slight amount of collective before landing, and the spin to the right became more aggravated. The helicopter then impacted the platform, and rolled over, onto its side.

Several witnesses observed the helicopter "spinning" after liftoff from the platform, then impact the ground on its left side.

A Federal Aviation Administration (FAA) inspector examined the helicopter after the accident. The tail rotor blades were rotated by hand and control continuity was confirmed to the main rotor blades. Control continuity was also confirmed from the cyclic and collective to the main rotor blades, and from the pedals to the tail rotor blades. All belts in the tail boom pulley assembly were in place, and the tail rotor drive shaft was twisted aft of the upper pulley assembly. The clutch switch and actuator were observed in the engaged position, and the belt tension pulley was engaged. The magneto switch was observed in the "both" position. Substantial damage was observed to the main rotor and tail rotor blades.

The pilot reported 173 hours of total flight experience, and 30 hours of rotary wing flight time. He had 10 flight hours in make and model, and this was his second solo takeoff, and first time taking off from a platform.

The winds reported at the airport, at 1453, were from 160 degrees at 8 knots.

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 control - in flightTakeoff
Directional control - not maintainedPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground

Aircraft

Registration
N9296F
Reported as
Hughes 269C
Category
Helicopter
Serial number
350407
Airframe hours
2,053.2
Engine
Lycoming RL-21866-51A, 190 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Hurst Aviation
Registered owner
Rapidturn Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · December 27, 2001 · 21.9 hours before
Departed
LPR
Destination
LPR
Airport
LPR · Lorain County Regional Airport

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Last flight review
November 15, 2000
Seat
Left
Flight hours
173 total · 10 in this make and model · 42 as pilot in command · 14 in the last 90 days · 10 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
160° at 8 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
45 °F, dew point 27 °F
Altimeter
30.04 inHg
Observed at
LPR

Docket · 6

The files NTSB released with the investigation on December 24, 2002, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.0 MB in all.

FAA reports on this event · 1

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