NYC83FU004

NTSB accident investigation · Vector 610 · Turners Falls, MA · May 11, 1983

Accident · FatalFinal report
Date
May 11, 1983, 18:05 local (22:05 UTC)
Place
Turners Falls, MA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
UNREGVector 610
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Case key
35126

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionManeuvering
Wing,wingtip - looseCause
Maintenance,major repair - improperPilot in commandCause
Maintenance,inspection - inadequatePilot in commandCause
Planning/decision - improperPilot in command
Impairment(alcohol)Pilot in commandFactor
Maneuver - performedPilot in commandFactor
Wing - failure,totalCause
Loss of control - in flightManeuvering
In flight collision with terrain/waterDescent - uncontrolled

Analysis

On 4/18/83, the ultralight vehicle was damaged by high winds. This necessitated the replacement of the front & rear spars as well as the battens which provided curvature to the upper wing surface. Prior to a test flt, a weighted tail wheel was also installed. Subsequently, a test plt took off to evaluate the ultralight. Witnesses observed that the plt climbed to about 1000 ft, then began a series of maneuvers. While performing a maneuver, similar to a lazy 8, with bank angles up to 60 to 90 deg, the ultralight's left wing folded. The vehicle then entered an uncontrolleddescent & crashed. An exam of the wreckage revealed that the aft spar tip had rotated around the aft spar in such a manner that the outboard wing panel had bent down & rearward. Holes had not been drilled & steel pop rivets had not been installed, per installation instructions, to prevent the spar tip from rotating. Also, the plt's blood alcohol level was found to be 95 mg%. The test plt also performed maintenance on the ultralight.

Aircraft

Registration
UNREG
Reported as
Vector 610
Category
Ultralight, amateur-built
Serial number
1244
Airframe hours
70
Engine
Zenoah G25B, 22 horsepower, reciprocating
Damage
Destroyed
Flight
Part 103
Registered owner
Aerodyne Systems, Inc.
Airport
runway 34, 3,000 × 75 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
35
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Center
Toxicology
Performed
Flight hours
2,480 total · 96 in this make and model · 2,330 as pilot in command · 57 in the last 90 days · 25 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 8 knots
Visibility
25 statute miles
Lowest ceiling
4,500 ft broken
Temperature
50 °F, dew point 43 °F
Altimeter
30.00 inHg
Observed at
BAF, 27 nm away