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NTSB Report

June 25, 2009 · Robinson Helicopter R44 II · N515DG

Lakeport, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 25, 2009
Injury Outcomes
No injuries (2 uninjured)
Location
Lakeport, CA
Aircraft
Robinson Helicopter R44 II
Tail Number
N515DG
Operator
Cutting Edge Helicopters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
WPR09LA312

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.

NTSB Probable Cause

Not determined-Not determined-(general)-(general)-Unknown/Not determined - C

Full 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.”

Flight

Event TypeAccident
Event Time15:00 PDT
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRobinson Helicopter R44 II
Tail NumberN515DG
Aircraft CategoryHeli
DamageSubstantial
OperatorCutting Edge Helicopters
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-AE1A5 · Reciprocating · 260
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 49 · Second Class · None
Crew 2Age 42 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind310° @ 11 kt
Visibility10 sm
CeilingBroken clouds 4500 ft
Temperature / Dew Point59 / 50
Altimeter29.95 inHg
Observation Time21:56
Weather SourceWFAC

Appendix: Source Data