WPR09LA312

NTSB accident investigation · Robinson Helicopter R44 II · Lakeport, CA · June 25, 2009

Accident · No injuriesLimited investigationFinal report
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.

Not determinedNot determined › Not determined · Unknown/Not determinedRobinson Helicopter R44 II: 24 casesAll aircraft: 2,247 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 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.