- 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.
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.