STEVEN BRENT WILLHOITE
Pilots at Rockville Rd, Louisburg, KS
License number
Kansas A2697092
Issued Date
Jan 2016
Expiration Date
Jan 2018
Category
Airmen
Type
Authorized Aircraft Instructor
Address
Address
33964 Rockville Rd, Louisburg, KS 66053
Professional information
Avionics Control And Display Unit
US Patent:
8570192, Oct 29, 2013
Filed:
Sep 10, 2012
Appl. No.:
13/608816
Inventors:
Frank A. McLoughlin - Leawood KS, US
Steven B. Willhoite - Louisburg KS, US
Walter J. Rolston - Overland Park KS, US
Joseph E. Gepner - Overland Park KS, US
Kevin C. Parmenter - Overland Park KS, US
Cory N. Douthat - Kansas City MO, US
Ryan C. Stark - Olathe KS, US
Steven B. Willhoite - Louisburg KS, US
Walter J. Rolston - Overland Park KS, US
Joseph E. Gepner - Overland Park KS, US
Kevin C. Parmenter - Overland Park KS, US
Cory N. Douthat - Kansas City MO, US
Ryan C. Stark - Olathe KS, US
Assignee:
Garmin International, Inc. - Olathe KS
International Classification:
G08B 21/00
US Classification:
340973, 340945, 340971, 701 3, 701 14
Abstract:
A multi-product avionics control and display unit (CDU). In implementations, the CDU may include a display and a processor coupled with the display. The processor is configurable to operate in a first mode to cause the display to present standby primary flight information associated with the aircraft and a second mode to control and display operation of one or more aircraft systems associated with the aircraft.
Avionics Control And Display Unit
US Patent:
8264376, Sep 11, 2012
Filed:
Jun 3, 2009
Appl. No.:
12/477280
Inventors:
Frank A. McLoughlin - Leawood KS, US
Steven B. Willhoite - Louisburg KS, US
Walter J. Rolston - Overland Park KS, US
Joseph E. Gepner - Olathe KS, US
Steven B. Willhoite - Louisburg KS, US
Walter J. Rolston - Overland Park KS, US
Joseph E. Gepner - Olathe KS, US
Assignee:
Garmin International, Inc. - Olathe KS
International Classification:
G08B 21/00
US Classification:
340945, 340971, 340973, 340974, 701 14
Abstract:
A multi-product avionics control and display unit (CDU). In implementations, the CDU may include a display and a processor coupled with the display. The processor is configurable to operate in a first mode to cause the display to present standby primary flight information associated with the aircraft and a second mode to control and display operation of one or more aircraft systems associated with the aircraft.