N57SJ

Substantial
None

Enstrom F28S/N: 278

Accident Details

Date
Tuesday, December 31, 2019
NTSB Number
CEN20LA051
Location
Danbury, TX
Event ID
20191231X03945
Coordinates
29.243888, -95.333053
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the engine's No.3 intake valve resulting is a loss of engine power and a rollover following the autorotation to soft ground.

Aircraft Information

Registration
N57SJ
Make
ENSTROM
Serial Number
278
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
F28EN28
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALAIKA TIMOTHY A
Address
PO BOX 757
Status
Deregistered
City
DANBURY
State / Zip Code
TX 77534-0757
Country
United States

Analysis

On December 31, 2019, about 1415 central standard time, an Enstrom F28A helicopter, N57SJ, sustained substantial damage when it nosed over during a forced landing following a partial loss of engine power. During the nose-over, the tailboom was separated and the main rotor system and fuselage were damaged. The student pilot and flight instructor were not injured. The helicopter was registered to and operated by a private individual under the provisions of Title 14 Code of federal Regulations Part 91 as an instructional flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from the Salaika Aviation Airport (07TA), Danbury, Texas, at an unconfirmed time.

The certificated flight instructor stated that he and his student had departed for a second pattern during a training mission. After the helicopter made the turn onto the crosswind leg of the traffic pattern the engine suddenly began to run rough and had lost a lot of power. He took the controls and executed an autorotation into a clearing, flared and touched down. The skids of the helicopter sunk into the soft mud, the rotor blades contacted the ground, and the helicopter rolled onto its side.

The operator reported that examination of the engine after the accident revealed that a portion of the intake valve for the No. 3 cylinder had broken off and had migrated into the No. 1 cylinder where it lodged between the No. 1 intake valve and seat, holding that valve in the open position.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN20LA051