N880SF

Unknown
None

BELL 230S/N: 23024

Accident Details

Date
Wednesday, July 1, 2009
NTSB Number
CEN09IA618
Location
Peoria, IL
Event ID
20110111X90812
Coordinates
40.664165, -89.693054
Aircraft Damage
Unknown
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The loss of the number one hydraulic system fluid and hydraulic pressure during cruise due to the failure of the bolts that secure the hydraulic pump's cover.

Aircraft Information

Registration
Make
BELL
Serial Number
23024
Engine Type
Turbo-shaft
Model / ICAO
230B230
Aircraft Type
Rotorcraft
No. of Engines
2
Seats
11
FAA Model
230

Registered Owner (Current)

Name
MAGNUM AVIATION LLC
Address
PO BOX 26
City
GOFF
State / Zip Code
KS 66428-0026
Country
United States

Analysis

On July 1, 2009, at 1815 central daylight time, a Bell 230 helicopter, N880SF, sustained no damage during a forced landing at the General Downing - Peoria International Airport (PIA), near Peoria, Illinois, after it lost fluid in its number one hydraulic system during cruise flight. The commercial helicopter pilot, two emergency medical services (EMS) crewmembers, and the patient were not injured. Visual meteorological conditions prevailed and no flight plan was filed. The local non-scheduled domestic 14 Code of Federal Regulations Part 135 EMS transport flight departed PIA at time unknown.

According to the operator’s incident report, the pilot observed a caution light for the number one hydraulic system and a corresponding complete loss of hydraulic system pressure for that system. The pilot declared an emergency and performed a run-on landing. Examination of the system's hydraulic pump revealed that two of its cover attachment bolts had separated. The separated bolt heads were retained by safety wire. This hydraulic pump manufacturer’s part number was 65132-1. The Bell Helicopter part number is 222-380-009-105, which is also usable on the Bell 222 series and 430 model helicopters. The bolts that sustained the separation were part number MS24678-17.

According to the helicopter manufacturer, these hydraulic pumps do not have a scheduled overhaul cycle and the pumps are replaced on-condition. The manufacturer does not track the service times of these pumps. Reportedly, this was the first failure of the hydraulic pump cover attachment bolts.

The pump manufacturer had the failed bolts examined. The bolt heads fractured in tension from their shanks via intergranular cracks initiating at the filet radius between the bead and the shank. The bolt fractures exhibited intergranular fracture features over 90 percent of the surface.

According to the operator, the incident pump accumulated 269 hours of time prior to the bolt failures. The operator’s incident report safety recommendation indicated, “Recommend pump cover bolts be replaced at overhaul.”

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN09IA618