Aircraft Accident/Incident Report

Fritch, Texas 79036
Sunday, December 22, 2002 14:45 CST

NTSB Narrative Summary Released at Completion of Accident

The helicopter was damaged during a forced landing after a loss of engine power while in cruise flight. The 14,700-hour pilot stated that at 5,100 feet MSL, the generator warning light illuminated. The pilot switched the generator "OFF" and back "ON" in an attempt to reset it, and was unable to reset the generator. The pilot then recycled the circuit breaker to try to reset the generator, and was still unable to reset the generator. The pilot pulled the generator circuit breaker and aborted the flight. Approximately 15 minutes after the generator failure, the engine out light illuminated and an audio warning came on, engine and rotor RPM started to decay and the pilot initiated autorotation. The auto re-ignition light illuminated during autorotation, but the engine would not spool back up to normal RPM. The pilot continued with the autorotation to a small clearing. During the final phase of the autorotation the pilot performed a cyclic flare to increase rotor RPM and arrest forward movement. The pilot leveled the helicopter a few feet off the ground and pulled the collective to arrest descent, at that point rotor RPM decayed and the helicopter dropped four feet AGL. The helicopter spun approximately 180 degrees from the original heading and impacted the ground nose first, on a heading of 30 degrees. Examination of the generator revealed that its drive-end bearing had failed. Bearing cage pieces fell out during disassembly. A Pc air leak test was performed and a air was detected emanating from the Pc air tube from the power turbine governor (PTG) to the engine fuel control unit (FCU). The tube was fractured approximately 90% circumferentially just above the coupling nut that attaches the tube to the FCU. A new Pc air tube (same part number) was installed and the engine was operated in a test cell. The engine was operated in accordance with the model 250-C20B Production Test Specifications. With the engine in the standard test configuration, response times were within normal limits and the engine met all performance parameters. Further metallurgical examination of the Pc tube revealed evidence of fatigue.

NTSB Probable Cause Narrative

The loss of engine power due to the failure of the generator input drive-end bearing, which resulted in excessive vibrations that induced a fatigue fracture of the Pc line leading to the engine fuel control unit. A contributing factor was the lack of suitable terrain for the forced landing.

Event Information

Type of Event Accident
Event Date 12/22/2002
Event Day of the Week Sunday
Time of Event 1445
Event Time Zone Central Standard Time
Event City Fritch
Event State TEXAS
Event Country --
Zipcode of the event site 79036
Event Date Year 2002
Event Date Month 12
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 354723N
Event Location Longitude 1015821W
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 3268
Weather Briefing Completeness Unknown
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) 7
Dew Point at event time (in degress fahrenheit) -8
Wind Direction (degrees magnetic) 180
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 12
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 30.05
Density Altitude (feet) 2968
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) 15138
NTSB Notification Source FAA Operations Center
NTSB Notification Date Dec 22 2002 12:00AM
NTSB Notification Time --
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Mar 30 2004 8:14AM
User who most recently changed record NTSB\MONR
Basic weather conditions Visual Meteorological Cond
FAA District Office Lubbock, Texas

Aircraft Involved

Aircraft #1

Aircraft Registration Number N5234Y
NTSB Number FTW03LA066
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed None
Flight plan Was Activated? No
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Hughes
Aircraft Model 369E
Aircraft Series Identifier --
Aircraft Serial Number 0167E
Certified Max Gross Weight 3000
Aircraft Category Helicopter
Aircraft Registration Class U.S. Registered/U.S. Soil
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 Annual
Date of Last Inspection Jul 26 2002 12:00AM
Airframe hours since last inspection --
Airframe Hours 1478
ELT Installed Unknown
ELT Activated Unknown
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Amistad Aviation Inc.
Aircraft Owner Street Address PO Box 279
Aircraft Owner City Amistad
Aircraft Owner State NM
Aircraft Owner Country USA
Aircraft Owner Zipcode 88410
Operator is an individual? No
Operator Name --
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? No
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) Business
Second Pilot on Board No
Departure Point Same as Event No
Departure Airport Code NONE
Departure City Syracuse
Departure State KS
Departure Country USA
Departure Time 1400
Departure Time Zone CST
Destination Same as Local Flt --
Destination Airport Code NONE
Destination City Gruver
Destination State TX
Destination Country USA
Specific Phase of Flight Cruise
Report sent to ICAO? --
Evacuation occurred No
Date of most recent change to record Jan 31 2004 12:33PM
User who most recently changed record CASH
Since inspection or accident --
Event Location Runway Number and Location NA
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --