Whiteman Airport
Aircraft Accident/Incident Report

Pacoima, California 91331
Monday, August 30, 2004 12:40 PDT

NTSB Narrative Summary Released at Completion of Accident

The twin-engine helicopter's number 2 engine experienced an uncontained engine failure and liberated debris punctured the helicopter's firewall while in cruise flight. The pilot made an uneventful landing at a nearby airport. Examination of the engine revealed segments of the stage 2 aft cooling plate (S2ACP) exited the power turbine case. Further investigation determined that the gas generator rotor's forward curvic seal was not installed during the operator's replacement of the gas generator turbine (GGT) module 92 hours prior to the event. Manufacturer's analysis of the missing curvic seal revealed it would have caused the reversal of the secondary airflow in the B-sump, which eventually led to auto ignition of the B-sump oil and exposure of the B-sump hardware to elevated temperatures. The elevated temperatures resulted in the separation of several B-sump components, including the separation of the compressor shaft. The compressor shaft separation resulted in the GGT rotor to rub into the stator and extensive secondary damage, including the separation of the S2ACP. The GGT module was replaced 209 hours prior to the event. According to the manufacturer, the forward curvic seal is part of the engine assembly rather than part of either the GGT rotor assembly or the high pressure compressor rotor assembly. According to General Electric (GE), if the curvic seal was removed from the engine during removal of the previous GGT rotor-stator assembly, and either discarded, or returned to GE's service facility with the rotor, a new seal would not have been included with the new GGT rotor-stator assembly, and the GGT could have been reinstalled without it. The manufacturer also reported that the maintenance manuals did not call for the verification of curvic seal installation during GGT replacement. This military engine was not a Federal Aviation Administration (FAA) certificated engine, but did share similar design features of other FAA certificated engines. The manufacturer reported that the civilian certificated engine maintenance manuals do call for the verification of curvic seal installation following a GGT replacement. The engine was removed from the event helicopter 92 hours prior to the event and was shipped to an engine service center for an internal leak at the number 3 labyrinth seal (located in the front frame of the engine). The service center repaired the inlet guide vanes, which, according to the manufacturer, was a typical repair when oil is observed leaking in the flow path in front of the compressor. However, their analysis of the missing curvic seal indicates that it too would have resulted in an oil leak in the front frame.

NTSB Probable Cause Narrative

the failure of the operator's mechanics to install the turboshaft engine's forward curvic seal during a gas generator turbine (GGT) replacement. Contributing factors to the incident were the failure of the manufacturer to provide a forward curvic seal with the replacement GGT, and the lack of a curvic seal installation verification inspection in the maintenance manuals following the GGT installation.

Event Information

Type of Event Incident
Event Date 8/30/2004
Event Day of the Week Monday
Time of Event 1240
Event Time Zone Pacific Daylight Time
Event City Pacoima
Event State CALIFORNIA
Event Country --
Zipcode of the event site 91331
Event Date Year 2004
Event Date Month 8
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 341535N
Event Location Longitude 1182449W
Event Location Airport Whiteman
Event Location Nearest Airport ID WHP
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 Pilot
Time of the weather observation
Direction of event from weather observation facility (degrees) --
Weather Observation Facility ID --
Elevation of weather observation facility --
Distance of event from weather observation facility (units?) --
Time Zone of the weather observation --
Lighting Conditions Day
Lowest Ceiling Height --
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions Clear
Sky Condition for Lowest Ceiling None
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 32
Dew Point at event time (in degress fahrenheit) --
Wind Direction (degrees magnetic) 210
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 2
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) --
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 3
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 19900
NTSB Notification Source FAA
NTSB Notification Date Sep 1 2004 12:00AM
NTSB Notification Time 1330
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Jun 28 2006 1:30PM
User who most recently changed record NTSB\JOHB
Basic weather conditions Visual Meteorological Cond
FAA District Office Federal Aviation Administration Van Nuys FSDO

Aircraft Involved

Aircraft #1

Aircraft Registration Number N160LA
NTSB Number LAX04IA311
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed Company VFR
Flight plan Was Activated? Yes
Damage Minor
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Sikorsky
Aircraft Model S-70A
Aircraft Series Identifier --
Aircraft Serial Number 702453
Certified Max Gross Weight 22000
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 --
Number of Engines 2
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection Continuous Airworthiness
Date of Last Inspection Jul 1 2003 12:00AM
Airframe hours since last inspection 89
Airframe Hours 1493
ELT Installed Yes
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name County of Los Angeles Fire Department
Aircraft Owner Street Address 12605 Osborne Street
Aircraft Owner City Pacoima
Aircraft Owner State CA
Aircraft Owner Country --
Aircraft Owner Zipcode 91331
Operator is an individual? No
Operator Name --
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? Yes
Operator Street Address --
Operator City --
Operator State --
Operator Country --
Operator Zip code --
Operator Code --
Owner has at least one certificate None
Other Operator of large aircraft? --
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) Public Use
Second Pilot on Board No
Departure Point Same as Event No
Departure Airport Code NA
Departure City Pacoima
Departure State CA
Departure Country USA
Departure Time 1235
Departure Time Zone PDT
Destination Same as Local Flt --
Destination Airport Code PMD
Destination City Palmdale
Destination State CA
Destination Country USA
Specific Phase of Flight Cruise - normal
Report sent to ICAO? Yes
Evacuation occurred No
Date of most recent change to record Jun 22 2006 11:07AM
User who most recently changed record JOHB
Since inspection or accident Time of Accident
Event Location Runway Number and Location NA
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --