- Date
- June 25, 2009, 15:00 local (22:00 UTC)
- Place
- Lakeport, CA
- Injuries
- 2 uninjured
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N515DGRobinson Helicopter R44 II
- Defining event
- Maneuvering: Loss of engine power (total)
- Weather
- Visual (VMC) · Day
- Status
- Completed · report April 22, 2010
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- Federal Aviation Administration
- FAA report
- 20090625013569A
- Case key
- 74137
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
A loss of engine power while maneuvering for undetermined reasons.
Findings · 1
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 certified flight instructor (CFI) and pilot undergoing instruction (PUI) were on a local instructional flight. The helicopter was fueled about 15 minutes prior and they were initiating a 180-degree autorotation with a power recovery. The helicopter entered into a glide and they made the turn onto the final segment. The CFI noticed that the oil and auxiliary fuel pump lights were on. The CFI then looked at the tachometer and attempted to increase the throttle. The power did not return and the CFI force-landed the helicopter. During the landing the main rotor blade impacted the tail boom. Post accident examination of the helicopter and test run of the engine revealed no operational anomalies.
Factual narrative
On June 25, 2009, at 1500 Pacific daylight time, a Robinson R44 II, N515DG, landed hard during a forced landing approximately 7 miles west-northwest of Lakeport, California. Cutting Edge Helicopters was operating the helicopter under the provisions of 14 Code of Federal Regulations Part 91. The certified flight instructor (CFI) and private pilot undergoing instruction (PUI) were not injured. The helicopter was substantially damaged. Visual meteorological conditions prevailed and no flight plan was filed. The CFI reported that the helicopter had been fueled to capacity prior to takeoff. They were conducting a 180-degree autorotation with a power recovery. They entered the helicopter into a glide and as they made the turn, the CFI noticed that the oil and auxiliary fuel pump lights were on. The CFI then looked at the tachometer and attempted to increase the throttle. The power did not return so the CFI committed to a landing. During the landing, the main rotor blades impacted the tail boom. The helicopter and engine were examined following their recovery from the accident site. The spark plugs were removed and examined. Their condition was consistent with normal operation when compared to a Champion Check-A-Plug chart. With the engine still installed on the helicopter and using the original fuel onboard the helicopter, it was powered. The engine test ran and no pre-impact anomalies were identified. According to Robinson Helicopter Company (RHC) Safety Notice SN-38, Practice Autorotations Cause Many Training Accidents, “There have been instances where the engine has quit during practice autorotation. To avoid inadvertent engine stoppage, do not roll the throttle to full idle. Reduce throttle firmly for a small visible needle split, then hold throttle firmly to override governor. Recover immediately if engine is rough or engine RPM continues to drop.”
Aircraft
- Registration
- N515DG
- Reported as
- Robinson Helicopter R44 II
- Category
- Helicopter
- Serial number
- 11503
- Airframe hours
- 501
- Engine
- Lycoming IO-540-AE1A5, 260 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Instructional · Part 91
- Operator
- Cutting Edge Helicopters
- Registered owner
- Metro Mailing Service Inc
- Airworthiness certificate
- Standard, Normal
- Last inspection
- 100 hour · June 17, 2009 · 29 hours before
- Departed
- UKI · Ukiah, CA
- Destination
- SMF · Sacramento, CA
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 · 2
As NTSB recorded them. NTSB leaves out names.
- Role
- Flight instructor
- Age
- 49
- Injuries
- None
- Certificates
- Commercial, Flight instructor
- Instrument ratings
- Helicopter
- Medical
- Class 2, Without waivers/limitations
- Last flight review
- February 22, 2009
- Seat
- Left
- Flight hours
- 746 total · 104 in this make and model · 659 as pilot in command · 80 in the last 90 days · 54 in the last 30 days
- Role
- Pilot
- Age
- 42
- Injuries
- None
- Certificate
- Private
- Medical
- Class 2, Without waivers/limitations
- Last flight review
- November 22, 2008
- Seat
- Right
- Flight hours
- 290 total · 160 in this make and model · 84 as pilot in command · 66 in the last 90 days · 32 in the last 30 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 310° at 11 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- 4,500 ft broken
- Temperature
- 59 °F, dew point 50 °F
- Altimeter
- 29.95 inHg
- Observed at
- UKI, 7 nm away
Docket · 7
The files NTSB released with the investigation on November 6, 2009, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.5 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.