N892CP

Substantial
None

Schweizer 269C S/N: 1423

Accident Details

Date
Thursday, March 20, 1997
NTSB Number
IAD97GA054
Location
CLEVELAND, OH
Event ID
20001208X07559
Coordinates
41.519775, -81.680557
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The engine failure from the rod cap bolt being sheared and the separation of the number two cylinder separating from the crankcase.

Aircraft Information

Registration
N892CP
Make
SCHWEIZER
Serial Number
1423
Engine Type
Reciprocating
Year Built
1989
Model / ICAO
269C H269
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
OWENS AIR SERVICE INC
Address
3528 S AIRPORT RD
Status
Deregistered
City
INVERNESS
State / Zip Code
FL 34450-7283
Country
United States

Analysis

On March 19, 1997, at about 2313 eastern standard time, a Schweitzer 268C helicopter, N892CP, operated by the City of Cleveland as a police helicopter, crashed into a vacant parking lot while on routine patrol in Cleveland, Ohio. The flight was conducted under the provisions of Title 14 CFR 91. The pilot and passenger both stated that they heard a loud noise and the engine quit. The pilot executed an autorotation into a parking lot causing substantial damage to the helicopter. The private pilot and passenger were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the local flight.

The pilot stated while on patrol over the city of Cleveland "at about 500 feet above ground level, the helicopter experienced major engine failure". The pilot attempted to autorotate the helicopter to a vacant parking lot. Upon impact, the tail rotor snapped off and the helicopter turned 180 degrees to the left.

Examination of the engine by NTSB, Textron Lycoming, G&W aircraft, and Cleveland Police Department found the number two cylinder had separated from the engine block and the rod cap bolt had been sheared. There were indications of wear to the number two cylinder deck and number two barrel flange. There was also heavy fretting to the number two and number three bearing crankcase saddles. Maintenance records show the removal and reinstallation of the number one cylinder at 646.2 hours since overhaul which was 66.6 hours prior to the 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# IAD97GA054