N518EG

MINR
None

ENSTROM 280S/N: 2101

Accident Details

Date
Monday, June 27, 2016
NTSB Number
CEN16IA238
Location
Zeeland, MI
Event ID
20160630X70958
Coordinates
42.809444, -85.981666
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The exhaust band clamp failure, which resulted in an engine fire due to hot exhaust gases entering the engine compartment.

Aircraft Information

Registration
Make
ENSTROM
Serial Number
2101
Engine Type
Reciprocating
Model / ICAO
280EN28
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
3
FAA Model
F-28F

Registered Owner (Current)

Name
STYER DAVID B
Address
4906 NW A AVE
City
PENDLETON
State / Zip Code
OR 97801-4632
Country
United States

Analysis

On June 27, 2016, about 1430 eastern daylight time, an Enstrom 208FX helicopter, N518EG, experienced an engine fire while preparing for departure from the Ottawa Executive airport (Z98), Zeeland, Michigan. The flight instructor and student pilot were not injured and the helicopter sustained minor fire damage. The helicopter was registered to and operated by Blue Sun Air, LLC, Zeeland, Michigan, under the provisions of 14 Code of Federal Regulations Part 91 as an instructional flight. Day visual meteorological conditions prevailed at the time.

The flight instructor reported that the student pilot was on his first flight. After a preflight inspection, they started the helicopter's engine and prepared for takeoff. Before increasing collective, the instructor noticed the lights on the panel flicker and smelled smoke. About the same time, the instructor also observed ground personnel running toward the helicopter. Both he and the student exited the helicopter and ground personnel were able to extinguish an engine fire.

An examination by a Federal Aviation Administration (FAA) inspector noted that the exhaust pipe had separated from the engine turbocharger. The helicopter had sustained damage to the engine access door, electrical wires, and smoke/thermal damage to the engine compartment.

The helicopter's turbocharger, exhaust clamp, and scavenge pump were sent to the National Transportation Safety Board (NTSB) Materials Laboratory in Washington, DC for further examination.

The materials laboratory noted that the band clamp assembly contained a strap portion and two U-shaped retainers. The bottom end of each U-shaped retainer were joined by several spot welds to the inner side of the strap portion. Examination of the band clamp assembly revealed the two U-shaped retainer portions fractured at the spot weld locations.

The NTSB's Materials Laboratory's Factual report is located in the public docket for this accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN16IA238