Docket Contents

Project Summary: Aviation Investigation - 25 Docket Items - WPR12FA001

Description: Pulsar 100, N91BV

Mode: Aviation

NTSB Number: WPR12FA001

Date of Accident: 10/04/2011

City: West Jordan

State / Region: UT

Country: United States

Project Type: Investigation


Docket Information

Creation Date: 12/12/11

Last Modified: 01/04/2013 10:41 AM

Public Release Date & Time: 01/04/2013 7:41 AM


Docket Items: 25

#

Title

Pgs

Photo

Type

1 GPS 17 - Specialist's Factual Report (6 Embedded Images) 8 6 Adobe PDF file
2 GPS 17 - Attachment 1 - Tabular Data (CSV) 0 0 Comma-delimited data file
3 Impact Area on Google 1 0 Adobe PDF file
4 Impact Location on Google 1 0 Adobe PDF file
5 Witness Statement - Silver 2 0 Adobe PDF file
6 Witness Statement - Bowles 2 0 Adobe PDF file
7 Witness Statement - McCullogh 1 0 Adobe PDF file
8 Witness Statement - Salazar 1 0 Adobe PDF file
9 Witness Statement - Harvey 1 0 Adobe PDF file
10 Record of Conversation (Previous Owner/Seller) 1 0 Adobe PDF file
11 Reports from Parties to the Investigation (Rotech Flight Safety) 5 0 Adobe PDF file
12 Statement of Party Representatives to NTSB Investigation 1 0 Adobe PDF file
13 Release of Aircraft Wreckage, NTSB Form 6120.15 1 0 Adobe PDF file
14 Toxicological Report 1 0 Adobe PDF file
15 Photo 1. View of accident site looking west from the initial impact scar. 1 0 Adobe PDF file
16 Photo 2. Engine prior to teardown examination, with propeller on the left and tuned-exhaust on the right. 1 0 Adobe PDF file
17 Photo 3. Fuel selector, showing it positioned in the FUEL (on) position. 1 0 Adobe PDF file
18 Photo 4. In-line fuel filter, showing it clear of any contamination. 1 0 Adobe PDF file
19 Photo 5. Propeller, showing its steel core rod bent against the direction of propeller rotation. 1 0 Adobe PDF file
20 Photo 6. Anti-abrasion strip on the propeller blade that did not fracture at is root, showing the leading edge impact damage. 1 0 Adobe PDF file
21 Photo 7. Anti-abrasion strip on the propeller blade that fractured at its root, showing the leading edge impact damage. 1 0 Adobe PDF file
22 Photo 8. Electrode end of the four sparkplugs, showing the heavy accumulation of soot. 1 0 Adobe PDF file
23 Photo 9. Close-up of one of the #180 jets installed in the carburetors. 1 0 Adobe PDF file
24 Photo 10. One of the carburetor jets, showing it incorrectly placed above the retaining cup instead of underneath the cup. 1 0 Adobe PDF file
25 Photo 11. Location of the alteration of the tuned exhaust system, showing its placement in the mid length of the inlet tube between the exhaust flange and the muffler. 1 0 Adobe PDF file