N7052A

Substantial
Minor

Hughes 269A S/N: 880956

Accident Details

Date
Monday, August 19, 1996
NTSB Number
CHI96TA306
Location
CEDAR RAPIDS, IA
Event ID
20001208X06481
Coordinates
41.919731, -91.699516
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

partial blocking of the fuel injection control, and a fracture of the induction air ducting for reasons undetermined. A factor was trees.

Aircraft Information

Registration
N7052A
Make
HUGHES
Serial Number
880956
Model / ICAO
269A

Registered Owner (Historical)

Name
CITY OF CEDAR RAPIDS
Address
CITY HALL
Status
Deregistered
City
CEDAR RAPIDS
State / Zip Code
IA 52401
Country
United States

Analysis

On August 19, 1996, at 1804 central daylight time, a Hughes 269A, N7052A, sustained substantial damage during an autorotational landing following a loss of engine power in cruise flight. The pilot stated the engine stopped suddenly after a loud "pop." The accident occurred in the City of Cedar Rapids, Iowa. The flight was a public use operation by the Cedar Rapids Police Department. The flight was being conducted in visual meteorological conditions. No flight plan was on file. The pilot reported minor injuries. The local flight departed Cedar Rapids about 1730.

The pilot stated that he was on a routine police patrol and was responding to a call in the southeastern part of the city. He said he was cruising at an altitude of about 1,400 feet mean sea level, in level flight when he heard a loud noise and the helicopter yawed to the left. He stated that he immediately lowered the collective control and initiated an autorotational landing. He found he was over a residential area and selected two trees which turned out to be about three to three and one half inches in diameter and measured by the police depart, to be 26 feet tall. The main rotor system impacted the trees and the helicopter continued to the ground. The pilot stated that the engine was not running during the forced landing.

An examination of the engine from the accident helicopter was conducted on September 4, 1996. The engine was test run. The engine ran within manufacturer's specification during the examination. The report of the examination is attached to this report.

During the preparation for the engine run the #3 and #4 induction tubes were removed for replacement, due to impact damage. Inside each tube was one piece of plastic. When placed together the two pieces fit together. The inlet induction housing was inspected and the pieces were determined to be from that housing. There were several splits in the housing in the area where the plastic pieces originated. The reason for their separation was not determined. It was possible to lay the two pieces over the fuel control induction unit and block the air tubes. See photos attached to this report.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96TA306