N440EM

Substantial
Minor

ROBINSON HELICOPTER COMPANY R44 IIS/N: 13503

Accident Details

Date
Saturday, August 3, 2019
NTSB Number
CEN19LA250
Location
Lyons, NE
Event ID
20190803X74951
Coordinates
41.937500, -96.473052
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The engine's low cylinder compression, which resulted in low rotor rpm and a subsequent dynamic rollover following landing on soft terrain.

Aircraft Information

Registration
N440EM
Make
ROBINSON HELICOPTER COMPANY
Serial Number
13503
Engine Type
Reciprocating
Year Built
2013
Model / ICAO
R44 IIR44
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
ILLINOIS VALLEY REGIONAL AIRPORT
4241 E ED URBAN DR
Status
Deregistered
City
PERU
State / Zip Code
IL 61354-9357
Country
United States

Analysis

On August 3, 2019, at 1615 central daylight time, a Robinson Helicopter Company R44 II helicopter, N440EM, experienced a loss of engine power during an aerial application of a field near Lyons, Nebraska. The helicopter impacted the ground during an attempted recovery by the pilot. The helicopter sustained substantial damage. The airline transport pilot received minor injuries. The helicopter was registered to an individual and operated by Wallin Agricultural Aviation under Title 14 Code of Federal Regulations Part 137 as an agricultural flight that was not operating on a flight plan. Day visual meteorological conditions prevailed at the time of the accident. The flight originated from an unknown location and an unknown time.

The pilot stated that he entered a field to be sprayed and about 100-120 ft agl, the low rotor rpm annunciation sounded. As he attempted to recover rotor rpm, the rpm continued to decay rapidly. He then used the remaining rotor rpm to cushion a landing onto the field. As the helicopter touched down, it slid about 150-200 ft before the skid dug into soft dirt and the helicopter rolled over.

Post-accident examination of the engine by the operator revealed that the no. 6 cylinder had more leakage/lower compression than the previous 100-hour recorded compression checks. At the previous recorded compression check, the no. 6 cylinder had a 8.75% of leakage (73 psi held from a reference of 80 psi). The no. 6 cylinder had 35% leakage (52 psi held from a reference of 80 psi) during the examination. No further examination of the cylinder was performed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN19LA250