chualar plane crash

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  • 8/4/2019 Chualar Plane Crash

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    National Transportation Safety Board

    PRELIMINARY REPORT

    AVIATION

    NTSB ID:

    Occurrence Date:

    Occurrence Type:

    PRELIMINARY INFORMATION - SUBJECT TO CHANGE Pag

    Location/Time

    Most Critical Injury:

    Investigated By:

    This space for binding

    Nearest City/Place

    Aircraft Information

    Registration Number

    State Zip Code

    Aircraft Manufacturer

    Local Time Time Zone

    Model/Series Number

    Minor NoneSerious

    Amateur Built Aircraft?

    Air Medical Transport Flight:

    Fatal

    Type of Aircraft:

    Injury Summary:

    Revenue Sightseeing Flight:

    Narrative

    Brief narrative statement of facts, conditions and circumstances pertinent to the accident/incident:

    Printed on : 10/6/2011 5:10:24

    YesAirplane

    1

    On September 29, 2011, about 1850 Pacific daylight time, an experimental amateur-built Zivko/Poe

    Edge 540 aerobatic airplane, N42GP, was substantially damaged when it impacted the pilot's vineyard

    property in Chualar, California. The certificated private pilot/owner received fatal injuries. The

    personal flight was operated under the provisions of Title 14 Code of Federal Regulations Part 91.

    Visual meteorological conditions prevailed, and no flight plan was filed for the flight.

    The airplane was based at Salinas Airport (SNS), Salinas, California, and was one of several

    registered to the pilot. According to information provided by Lockheed Martin Flight Services

    (LMFS), the pilot did not contact them or the Direct User Automated Terminal System for weather or

    flight planning information. According to Federal Aviation Administration (FAA) information, the

    airplane departed SNS about 1841 PDT. Witnesses and family members reported that the pilot

    frequently performed aerobatics in that airplane in the airspace over his property. Witnesses

    reported that the airplane was performing aerobatics when the accident occurred.

    The initial impact point was evidenced by a ground scar on a dirt road that separated two planting

    areas in the vineyard. The ground scar measured about 20 feet long, and increased in width and

    depth along a magnetic heading of about 082 degrees. That scar terminated at a row of 3-inch

    diameter metal posts, spaced about 8 feet apart, that supported the vineyard trellises. Two posts

    were fracture-separated near their bases, and three more were bent over in the direction of the

    debris path. The primary debris field extended approximately 160 feet beyond the initial impact

    point. The airplane was highly fragmented, and most of the wreckage was entangled in the vineyard

    trellises and grapevines. The first two items in the ground scar were a segment of fuselage

    structural tubing and a propeller blade tip. One magneto, the tailwheel, and an aerodynamic surface

    balance weight were found about 500 feet beyond, and 150 feet above, the initial impact point. All

    major components of the engine and airplane, including all aerodynamic control surfaces, were

    accounted for at the accident site. A handheld global positioning system unit and an engine monitor

    were recovered from the wreckage and sent to the NTSB recorders laboratory in Washington, DC, for

    possible data download. The remainder of the wreckage was recovered to a secure facility for

    additional follow-up examination.

    FAA records indicated that the airplane was equipped with a Lycoming IO-540 series engine, and was

    first registered to the pilot's family in 2009. FAA records indicated that the pilot held a private

    pilot certificate with rotorcraft-helicopter, and single- and multi-engine land airplane ratings.

    His most recent FAA third-class medical certificate was issued in July 2011, and his most recent

    flight review was completed in September 2009.

    The 1853 automated weather observation at SNS, located about 9 miles north of the accident site,

    included winds from 320 degrees at 14 knots; visibility 10 miles; and an overcast cloud layer at

    1,100 feet above ground level.

    Updated on Oct 5 2011 1:12PM

    NoNo

    540POE G L/POE S YN42GP

    NTSB

    Fatal

    PDT185093925CAChualar

    Accident

    09/29/2011

    WPR11FA474

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    This space for binding

    National Transportation Safety Board

    PRELIMINARY REPORT

    AVIATION

    NTSB ID:

    Occurrence Date:

    Occurrence Type:

    Model/Series NumberAircraft ManufacturerRegistration Number

    Other Aircraft Involved

    Accident Information

    Aircraft Damage: Accident Occurred During:

    Certificate No. InjuryNameCrew

    Pilot

    2

    3

    4

    5

    6

    Operator Information

    Name

    Street Address

    Operator Designator Code

    City

    Doing Business As

    State Zip Code

    Observation Time (Local):

    Altimeter: "H

    Pag

    -Type of Certificate(s) Held:

    Air Carrier Operating Certificate(s):

    Operating Certificate:

    Regulation Flight Conducted Under:

    Type of Flight Operations Conducted:

    Operator Certificate:

    Flight Plan/Itinerary

    Type of Flight Plan Filed:

    Last Departure Point

    Destination

    State Airport Identifier

    Airport IdentifierState

    Weather Information

    Investigator's Source:

    Sky/Lowest Cloud Condition:

    Facility ID:

    Ft. AGL Visibility:

    Ft. AGL

    SM

    PRELIMINARY INFORMATION - SUBJECT TO CHANGE

    Lowest Ceiling:

    FatalOn FileOn File

    29.92101100Overcast

    1853SNSUnknown

    SNSCALocal Flight

    SNSCASalinas

    Unknown

    Personal

    Part 91: General Aviation

    None

    93901-1818CASALINAS

    Daniel L Franscioni

    Substantial

    Accident

    09/29/2011

    WPR11FA474

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    This space for binding

    National Transportation Safety Board

    PRELIMINARY REPORT

    AVIATION

    NTSB ID:

    Occurrence Date:

    Occurrence Type:

    Date

    Wind Direction:

    Weather Conditions at Accident Site:

    Weather Information (Continued from page 2)

    Temperature: C Dew Point:

    Wind Speed: Kts. Gusts:

    Administration Data

    Notification From

    C

    Kts.

    Investigator-In-Charge (IIC)FAA District Office/Coordinator

    PRELIMINARY INFORMATION - SUBJECT TO CHANGE Page

    FAA FSDOJeffrey Ebey

    FAA Comm Center

    Michael C. Huhn

    Visual Conditions14

    3201418

    Accident

    09/29/2011

    WPR11FA474