ERA09CA482

NTSB accident investigation · Bell 206 · Gumboro Township, DE · August 24, 2009

Accident · No injuriesData collectionFinal report
Date
August 24, 2009, 17:36 local (21:36 UTC)
Place
Gumboro Township, DE
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Standing
Aircraft
N98KRBell 206
Defining event
Standing-engine(s) operating: Ground handling event
Weather
Visual (VMC) · Day
Status
Completed · report December 29, 2009
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20090824048849A
Case key
74597

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

The pilot’s failure to secure the flight controls before exiting the running helicopter. Contributing to the accident was the operator’s practice of exiting the helicopter while it was still running.

Findings · 3

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Parking/securingAircraft › Aircraft handling/service · Incorrect use/operationBell Helicopter Textron 206L-1: 1 caseAll aircraft: 11 casesProbable cause
Use of equip/infoPersonnel issues › Task performance · PilotBell Helicopter Textron 206L-1: 1 caseAll aircraft: 111 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The helicopter pilot stated that he was completing an aerial application flight due to deteriorating weather. After landing on a wet, elevated platform, he exited the running helicopter, which was a common company practice during refueling and reloading operations. Moments later, the helicopter yawed to the right, slid off the platform and landed on the mast, resulting in substantial damage to the rotor assembly, left side fuselage, and tail boom. The pilot later stated that he did not recall securing the flight controls before exiting the helicopter. A Federal Aviation Administration examination of the accident scene revealed that the flight control friction locks were not tight, and that the landing platform was not level. A representative of the helicopter manufacturer stated that there was nothing published by the company that restricted a pilot from exiting a helicopter while it was running. However, there is a note in the pilot’s operating handbook for the engine shutdown procedure that states, “Pilot -- remain at flight controls until rotor has come to a complete stop.” A representative of the National Agricultural Aviation Association stated that although the practice of hot refueling was common in the industry, the practice of exiting a running helicopter was not.

Factual narrative

The helicopter pilot stated that he was conducting an aerial application flight before landing due to deteriorating weather. After landing on a wet, elevated platform, he exited the running helicopter, which was a common company practice during refueling and reloading operations. Moments later, the helicopter yawed to the right, slid off the platform and landed on the mast, resulting in substantial damage to the rotor assembly, left side fuselage, and tail boom. The pilot later stated that he did not recall securing the flight controls before exiting the helicopter. A Federal Aviation Administration examination of the accident scene revealed that the flight control friction locks were not tight, and that the landing platform was not level. A representative of the helicopter manufacturer stated that there was nothing published by the company that restricted a pilot from exiting a helicopter while it was running. However, there is a note in the pilot’s operating handbook for the engine shutdown procedure that states, “Pilot -- remain at flight controls until rotor has come to a complete stop.” A representative of the National Agricultural Aviation Association stated that although the practice of hot refueling was common in the industry, the practice of exiting a running helicopter was not.

Aircraft

Registration
N98KR
Reported as
Bell 206 (L1)
Category
Helicopter
Serial number
45683
Airframe hours
7,144
Engine
Rolls Royce 250-C30P, turbo shaft
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
Helicopter Applicators Inc
Registered owner
Helicopter Applicators Inc
Airworthiness certificate
Special, Restricted (Special)
Last inspection
100 hour · August 6, 2009 · 6 hours before
Departed
Gumboro Township, DE
Destination
Gumboro Township, DE

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
62
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, With waivers/limitations
Last flight review
January 14, 2009
Flight hours
16,000 total · 250 in this make and model · 15,800 as pilot in command · 100 in the last 90 days · 25 in the last 30 days · 6 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
7 statute miles
Lowest ceiling
10,000 ft broken
Temperature
86 °F, dew point 66 °F
Altimeter
30.04 inHg

Docket · 5

The files NTSB released with the investigation on October 23, 2009, on NTSB’s docket system: statements, records, photos and specialists’ reports. 549 KB 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.