Aircraft Accident/Incident Report

Yuma, Arizona 85365
Friday, November 23, 2007 19:30 MST

NTSB Narrative Summary Released at Completion of Accident

While conducting an aerial application flight, the pilot reported that he was initiating a turn over a set of power lines at an altitude of about 60 feet above ground level (agl). As the helicopter crossed over a series of power lines, the pilot heard a "loud pop" and felt an extreme vibration. The pilot maneuvered the helicopter away from the power lines and initiated a forced landing to an open field. He reported that control of the helicopter was "marginal" as the helicopter descended. Shortly before touchdown, the helicopter began to drift (un commanded) to the left and the pilot lowered the collective. The helicopter touched down hard, pivoted to the left and rolled over onto its right side. Post accident examination of the helicopter revealed that a control rotor had separated from the rotor system. The separated control rotor was found in the area where the vibration started. Examination of the control rotor assembly revealed the tubular spar of the blue control rotor was circumferentially fractured at the outboard cuff bolt location. Magnified examinations of the outboard fracture surfaces revealed surface features consistent with fatigue progression in two fronts around the spar. Fatigue initiation locations were identified on opposite sides of one of the outboard bolt holes in the spar. One fatigue origin was identified on the bore surface of the bolt hole and the other was mechanically damaged preventing determination of its exact location. The bore surface was rough and no obvious corrosion was noted in the hole. From the bolt hole the fatigue propagated almost entirely around the spar with very small overstress regions connecting the fatigue to the opposite bolt hole in the spar. No corrosion was noted in the originating bolt hole, however, the exterior surface of the spar exhibited wide spread pitting corrosion and fretting on the faying surfaces with the control rotor cuff. Additional localized corrosion was noted on the interior faying surface of the cuff. Maintenance records indicated that the most recent 100-hour inspection was conducted about 77 hours prior to the accident. The logbook entry associated with the inspection indicated that Airworthiness Directive AD 97-10-16 had been complied with. AD 97-10-16 (effective date 6/26/97) states, in part,: "To prevent separation of the control rotor blade assembly and subsequent loss of control of the helicopter, accomplish the following: (a) Within the next 100 hours time-in-service (TIS) after the effective date of the AD, unless previously accomplished within the last 100 hours TIS, and thereafter at intervals not to exceed 100 hours TIS from the date of the last inspection, or at the next annual inspection, whichever occurs first, inspect the blade spar tube and cuff for corrosion or cracks, or elongation, corrosion, burrs, pitting or fretting of the bolt holes, and repair, as necessary..."

NTSB Probable Cause Narrative

Fatigue fracture of the control rotor blade spar and failure of maintenance personnel to follow maintenance directives.

Event Information

Type of Event Accident
Event Date 11/23/2007
Event Day of the Week Friday
Time of Event 1930
Event Time Zone Mountain Standard Time
Event City Yuma
Event State ARIZONA
Event Country --
Zipcode of the event site 85365
Event Date Year 2007
Event Date Month 11
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 323923N
Event Location Longitude 1143621W
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 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 Night
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) --
Air Temperature at event time (in degrees celsius) 15
Dew Point at event time (in degress fahrenheit) --
Wind Direction (degrees magnetic) 315
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) 3
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 1
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 23393
NTSB Notification Source FAA-ROC
NTSB Notification Date Nov 23 2007 12:00AM
NTSB Notification Time --
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Apr 30 2008 1:28PM
User who most recently changed record NTSB\johb
Basic weather conditions Visual Meteorological Cond
FAA District Office Scottsdale, Arizona

Aircraft Involved

Aircraft #1

Aircraft Registration Number N104EA
NTSB Number SEA08LA038
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 137: Agricultural
Type of Flight Plan filed None
Flight plan Was Activated? No
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Hiller
Aircraft Model UH-12E
Aircraft Series Identifier --
Aircraft Serial Number HA3028
Certified Max Gross Weight 3100
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 3
Number of Engines 1
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection AAIP
Date of Last Inspection Oct 1 2007 12:00AM
Airframe hours since last inspection --
Airframe Hours 8251.5
ELT Installed No
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name Tri-Rotor Spray & Chemical
Aircraft Owner Street Address --
Aircraft Owner City Ulysses
Aircraft Owner State AZ
Aircraft Owner Country USA
Aircraft Owner Zipcode 67880
Operator is an individual? Yes
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 --
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation Agriculture
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) Aerial Application
Second Pilot on Board No
Departure Point Same as Event No
Departure Airport Code --
Departure City Yuma
Departure State AZ
Departure Country USA
Departure Time 1920
Departure Time Zone PST
Destination Same as Local Flt dest & departure same, accident can occur anywhere
Destination Airport Code --
Destination City --
Destination State --
Destination Country --
Specific Phase of Flight Landing
Report sent to ICAO? --
Evacuation occurred --
Date of most recent change to record Mar 31 2008 7:22PM
User who most recently changed record STAM
Since inspection or accident Last Inspection
Event Location Runway Number and Location NA
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --