Aircraft Accident/Incident Report

New Port Richey, Florida 34654
Thursday, January 2, 2003 19:51 EST

NTSB Narrative Summary Released at Completion of Accident

The pilot stated that after takeoff while in a left turn climbing through 600 feet at 60 knots indicated airspeed, he heard a loss of engine power. He stopped the turn and noted that the engine was at flight idle as indicated by the dual tachometer. He verified the throttle was full open, and maneuvered the helicopter towards an open area. He bled off main rotor rpm to clear obstacles that were ahead, and decelerated at 10 feet above ground level. The helicopter touched down with little forward movement, coming to rest upright with the skids and tailboom separated. The helicopter was found to contain a sufficient quantity of fuel to sustain engine operation; no contaminants were reported. Examination of the engine revealed the fuel inlet line "B" nut was found loose by 2 1/2 flats at the fuel inlet nozzle. The fuel inlet line was drained and found to contain approximately 1 teaspoon of fuel while the fuel filter was full of fuel. The engine control rigging was found to be in limits. An abnormal sound was heard during testing of the aircraft fuel shutoff valve. Operational testing of the valve revealed it was operational but rotation of the valve body occurred with rotation of the valve. The engine was removed from the helicopter and transported to the manufacturer's facility. Prior to the engine run, the bleed air valve was found failed in the closed position; the internal spring was found unwound. The engine was operated in the presence of an FAA airworthiness inspector with a new bleed valve and the accident bleed valve installed; no appreciable difference was noted with respect to starting temperature, acceleration times, or stabilized operation. A customer bleed line that attaches to the scroll was found loose, it was tightened followed by engine operation. The line was loose when checked following the engine run. No significant findings were noted during the engine runs. Safety concerns prevented operation of the engine with the as-found position of the loose "B" nut at the fuel nozzle; however, a valve was installed to divert fuel from the fuel nozzle simulating the as-found position of the loose "B" nut. During the engine run, the valve was opened 1/4 and the engine operated normally. The valve was opened to 1/2 then 3/4, the engine continued to operate normally though the fuel flow increased. The valve was then fully opened and the engine flamed out. Several hours before the accident, a mechanic performed a compressor wash. It was common practice for the mechanic to clean the fuel nozzle when he performed a compressor wash.

NTSB Probable Cause Narrative

The pilot's inadequate preflight of the helicopter following maintenance he observed, and failure of maintenance personnel to tighten the "B" nut at the fuel nozzle following a compressor wash resulting in the total loss of engine power. Also, the pilot's intentional decay of main rotor rpm while attempting to clear obstructions and unsuitable terrain encountered during the forced landing resulting in a hard landing.

Event Information

Type of Event Accident
Event Date 1/2/2003
Event Day of the Week Thursday
Time of Event 1951
Event Time Zone Eastern Standard Time
Event City New Port Richey
Event State FLORIDA
Event Country --
Zipcode of the event site 34654
Event Date Year 2003
Event Date Month 1
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 281629N
Event Location Longitude 0823756W
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 Unknown
Investigator's weather source Weather Observation Facility
Time of the weather observation 1953 Eastern Standard Time
Direction of event from weather observation facility (degrees) --
Weather Observation Facility ID KTPA
Elevation of weather observation facility 26
Distance of event from weather observation facility (units?) --
Time Zone of the weather observation EST
Lighting Conditions Night/Dark
Lowest Ceiling Height 25000
Lowest Non-Ceiling Height 3000
Sky/Lowest/Cloud Conditions Few
Sky Condition for Lowest Ceiling Overcast
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 18
Dew Point at event time (in degress fahrenheit) 17
Wind Direction (degrees magnetic) 190
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 4
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 29.99
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) 15359
NTSB Notification Source FAA Comm Center
NTSB Notification Date Jan 2 2003 12:00AM
NTSB Notification Time 2059
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Apr 28 2004 3:34PM
User who most recently changed record NTSB\MONR
Basic weather conditions Visual Meteorological Cond
FAA District Office Tampa, Florida

Aircraft Involved

Aircraft #1

Aircraft Registration Number N317LC
NTSB Number MIA03TA036
Missing Aircraft Indicator --
Federal Aviation Reg. Part Public Use
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 OH-6
Aircraft Series Identifier --
Aircraft Serial Number 68-17310
Certified Max Gross Weight 2550
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 100 Hour
Date of Last Inspection Oct 29 2002 12:00AM
Airframe hours since last inspection 49.8
Airframe Hours 5649.3
ELT Installed Yes
ELT Activated Yes
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Pasco County Sheriff's Office
Aircraft Owner Street Address 8903 Airway Blvd.
Aircraft Owner City New Port Richey
Aircraft Owner State FL
Aircraft Owner Country USA
Aircraft Owner Zipcode 34654
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 Yes
Departure Airport Code FA40
Departure City New Port Richey
Departure State FL
Departure Country USA
Departure Time 1945
Departure Time Zone EST
Destination Same as Local Flt dest & departure same, accident can occur anywhere
Destination Airport Code FA40
Destination City New Port Richey
Destination State FL
Destination Country USA
Specific Phase of Flight Emergency descent/landing
Report sent to ICAO? No
Evacuation occurred Yes
Date of most recent change to record Mar 5 2004 2:23PM
User who most recently changed record KENJ
Since inspection or accident Time of Accident
Event Location Runway Number and Location --
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --