Gustine Airport
Aircraft Accident/Incident Report

Gustine, California 95322
Wednesday, May 11, 2005 9:45 PDT

NTSB Narrative Summary Released at Completion of Accident

The helicopter landed hard and rolled over after the nut/bolt assembly connecting the left cyclic push-pull tube to the swashplate came loose, causing a loss of roll control during takeoff. No mechanical anomalies were noted during the preflight. The certificated flight instructor (CFI) and student departed to do training at another airport. During takeoff to return to their home base, the CFI heard a clicking noise coming from the helicopter and decided to make a precautionary landing; however, the helicopter began a roll to the right. The CFI attempted to correct the roll to the right with the application of left cyclic, but there was no corresponding response. The right skid contacted the ground and the helicopter rolled over, coming to rest on its left side. Following the accident, the bolt, nut, and two spacers that connected the left cyclic push-pull tube to the swashplate were located on the runway. When the Federal Aviation Administration inspector arrived, he also walked the accident area and found the self-locking nut. A review of the aircraft logbook indicated that the left rib at the top of the mast fairing had been installed at the last 100-hour inspection, 2.5 hours before the accident. In order to remove the left rib (bulkhead), the bolt and nut assembly that attaches the left cyclic push-pull tube to the left lug of the non-rotating swashplate had to be disassembled, and then reassembled after the rib (bulkhead) replacement. According to the manufacturer's Illustrated Parts Catalog, left cyclic push-pull tube connection to the non-rotating swashplate assembly requires a bolt and self-locking nut, 3 spacers (2 of the 3 spacers were found at the accident site), a washer, and a locking palnut, were not found. A metallurgical examination of the swashplate assembly, left push-pull tube, left rib (bulkhead), nut and bolt and associated hardware was conducted. All of the fracture surfaces examined revealed no preexisting damage. The absence of the bolt between the left cyclic push-pull tube and the non-rotating swashplate after the accident and the thread imprints within the hole of the left lug of the non-rotating swashplate indicated that the bolt had been backing out of the hole over time. The bolt and nut that were recovered were in good condition, and the hole in the left lug of the non-rotating swashplate was not significantly ovalized, indicating that the bolted connection was not subjected to excessive loads of any kind. The loss of the nut (and subsequent backing out of the bolt) indicates that the connection was not properly assembled following the recent maintenance, which required the bolted connection to be disassembled.

NTSB Probable Cause Narrative

the improper installation of the nut/bolt assembly connecting the left cyclic push-pull tube to the non-rotating swashplate by maintenance personnel, which led to a loss of roll control during takeoff.

Event Information

Type of Event Accident
Event Date 5/11/2005
Event Day of the Week Wednesday
Time of Event 945
Event Time Zone Pacific Daylight Time
Event City Gustine
Event State CALIFORNIA
Event Country --
Zipcode of the event site 95322
Event Date Year 2005
Event Date Month 5
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 371545N
Event Location Longitude 1205747W
Event Location Airport GUSTINE
Event Location Nearest Airport ID 3O1
Indicates whether the acc/inc occurred off or on an airport On Airport
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation 75
Weather Briefing Completeness --
Investigator's weather source Weather Observation Facility
Time of the weather observation 953 Pacific Daylight Time
Direction of event from weather observation facility (degrees) 265
Weather Observation Facility ID MCE
Elevation of weather observation facility 156
Distance of event from weather observation facility (units?) 22
Time Zone of the weather observation PDT
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) 18
Dew Point at event time (in degress fahrenheit) 8
Wind Direction (degrees magnetic) 330
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 9
Wind Velocity Indicator --
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 30.03
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) 20177
NTSB Notification Source FAA
NTSB Notification Date May 11 2005 12:00AM
NTSB Notification Time --
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Aug 29 2006 3:49PM
User who most recently changed record NTSB\JOHB
Basic weather conditions Visual Meteorological Cond
FAA District Office WP-FAT-FSDO

Aircraft Involved

Aircraft #1

Aircraft Registration Number N144SM
NTSB Number LAX05LA164
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 Robinson
Aircraft Model R44
Aircraft Series Identifier --
Aircraft Serial Number 1098
Certified Max Gross Weight 2400
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 May 1 2005 12:00AM
Airframe hours since last inspection 2.5
Airframe Hours 1601.8
ELT Installed Yes
ELT Activated Yes
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Helimark LLC
Aircraft Owner Street Address 1002 Airport Rd., Suite B
Aircraft Owner City Los Banos
Aircraft Owner State CA
Aircraft Owner Country USA
Aircraft Owner Zipcode 93635
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) Instructional
Second Pilot on Board Yes
Departure Point Same as Event No
Departure Airport Code LSN
Departure City Los Banos
Departure State CA
Departure Country USA
Departure Time 930
Departure Time Zone PDT
Destination Same as Local Flt dest & departure same, accident can occur anywhere
Destination Airport Code LSN
Destination City --
Destination State --
Destination Country --
Specific Phase of Flight Takeoff - roll/run
Report sent to ICAO? --
Evacuation occurred --
Date of most recent change to record Jun 12 2006 6:36PM
User who most recently changed record COOS
Since inspection or accident Last Inspection
Event Location Runway Number and Location 36
Runway Length 3200
Runway Width 60
Sight Seeing flight No
Air Medical Flight No
Medical Flight --