Aircraft Accident/Incident Report

Columbus, Ohio 43224
Saturday, August 19, 2006 16:39 EDT

NTSB Narrative Summary Released at Completion of Accident

The public-use helicopter was conducting a routine patrol flight when it experienced an uncontained engine failure. The pilot immediately performed an autorotation and run-on landing to an open parking lot area without further incident. The helicopter was damaged with several punctures with outward deformation consistent with projectile damage originating from an uncontained engine failure. Inspection of the engine revealed that portions of the 1st-stage gas producer wheel had departed the engine. The gas producer turbine tie bolt (part number 23068265, serial number NM81907) was identified as the primary failed component. The tie bolt fractured immediately adjacent to the torque nut. Further examination revealed fracture features consistent with fatigue, initiating at the thread root radius. The microstructure, chemistry, and hardness of the turbine tie bolt met engineering drawing specifications. No material anomalies were detected at the fracture surface. Damage to the fracture surface precluded the determination if the failure was associated with low or high cycle fatigue. The tie bolt had completed 3,427 cycles, about 38 percent, of its published life limit of 9,000 cycles. The failure was the first documented since the tie bolt was redesigned during the late 1990s. The redesigned tie bolt incorporated a thicker and stiffer cross-section that had a higher resonant frequency. The manufacturer reviewed the testing and analysis that was preformed when the tie bolt was redesigned. Their review confirmed that the current life limit of 9,000 cycles was within design guidelines. Additionally, the stress modeling and analysis performed during the component redesign was reviewed and no discrepancies were noted. The manufacturer also reviewed the reengineered tie bolt service history and several tie bolts with between 5,000 and 9,000 cycles were taken out of service for examination. Component examinations and database reviews failed to show any similar failures within the fleet. The tie bolt installation required that the bolt length be measured in order to determine the exact stretch of the bolt after the nut was torqued to specification. The original stretch requirement was used with the redesigned tie bolt to eliminate confusion during assembly. A subsequent service bulletin and FAA airworthiness directive mandated that the older design be removed from service, but the installation stretch requirement was not modified. To mitigate future tie bolt fractures, Rolls-Royce reduced the stretch requirement on the tie bolt during the assembly process. As a result, the mean stress on the tie bolt was reduced. The reduced stretch is also expected to increase both high and low cycle fatigue margins in the part. The assembly instructions were updated with the new stretch callout during the first quarter of 2008.

NTSB Probable Cause Narrative

The uncontained engine failure due to the fatigue failure of the gas producer turbine tie bolt.

Event Information

Type of Event Accident
Event Date 8/19/2006
Event Day of the Week Saturday
Time of Event 1639
Event Time Zone Eastern Daylight Time
Event City Columbus
Event State OHIO
Event Country --
Zipcode of the event site 43224
Event Date Year 2006
Event Date Month 8
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 400408N
Event Location Longitude 0825806W
Event Location Airport --
Event Location Nearest Airport ID --
Indicates whether the acc/inc occurred off or on an airport Off Airport/Airstrip
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness --
Investigator's weather source Weather Observation Facility
Time of the weather observation 1653 Eastern Daylight Time
Direction of event from weather observation facility (degrees) 292
Weather Observation Facility ID OSU
Elevation of weather observation facility 905
Distance of event from weather observation facility (units?) 5
Time Zone of the weather observation EDT
Lighting Conditions Day
Lowest Ceiling Height 4700
Lowest Non-Ceiling Height 3600
Sky/Lowest/Cloud Conditions Scattered
Sky Condition for Lowest Ceiling Broken
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 28
Dew Point at event time (in degress fahrenheit) 21
Wind Direction (degrees magnetic) 310
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 11
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 29.91
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury None
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal --
Injury Total Minor --
Injury Total None 2
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 24574
NTSB Notification Source FAA
NTSB Notification Date Aug 19 2006 12:00AM
NTSB Notification Time --
Fiche Number and/or location -used to find docket information --
Date of most recent change to record Nov 12 2008 1:48PM
User who most recently changed record lema
Basic weather conditions Visual Meteorological Cond
FAA District Office Federal Aviation Adminstration - Columbus FSDO

Aircraft Involved

Aircraft #1

Aircraft Registration Number N554CP
NTSB Number CHI06GA241
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed Company VFR
Flight plan Was Activated? Yes
Damage Substantial
Aircraft Fire Ground and In-flight
Aircraft Explosion None
Aircraft Manufacturer's Full Name McDonnell Douglas Helicopters
Aircraft Model 369E
Aircraft Series Identifier --
Aircraft Serial Number 0542E
Certified Max Gross Weight 3000
Aircraft Category Helicopter
Aircraft Registration Class --
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 4
Number of Engines 1
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection 100 Hour
Date of Last Inspection Aug 1 2006 12:00AM
Airframe hours since last inspection 41.4
Airframe Hours 6639.7
ELT Installed No
ELT Activated Unknown
ELT Aided Location of Event Site Unknown
ELT Type --
Aircraft Owner Name City of Columbus Police Department
Aircraft Owner Street Address 120 Marconi Boulevard
Aircraft Owner City Columbus
Aircraft Owner State OH
Aircraft Owner Country USA
Aircraft Owner Zipcode 43215
Operator is an individual? No
Operator Name City of Columbus Police Department
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? Yes
Operator Street Address 120 Marconi Boulevard
Operator City Columbus
Operator State OH
Operator Country USA
Operator Zip code 43215
Operator Code --
Owner has at least one certificate None
Other Operator of large aircraft? No
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not --
Indicates Domestic or International Flight --
Operator carrying Pax/Cargo/Mail --
Type of Flying (Per_Bus / Primary) --
Second Pilot on Board No
Departure Point Same as Event Yes
Departure Airport Code OH52
Departure City Columbus
Departure State OH
Departure Country USA
Departure Time 1600
Departure Time Zone EDT
Destination Same as Local Flt dest & departure same, accident can occur anywhere
Destination Airport Code OH52
Destination City Columbus
Destination State OH
Destination Country USA
Specific Phase of Flight Emergency descent/landing
Report sent to ICAO? --
Evacuation occurred --
Date of most recent change to record Nov 12 2008 1:32PM
User who most recently changed record lema
Since inspection or accident Time of Accident
Event Location Runway Number and Location N/A
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --