US 11,851,166 B2
System and method of determining and displaying procedures for an engine-out takeoff for an aircraft
Terry L. McDonough, Scottsdale, AZ (US); Garrett W. van Ark, Phoenix, AZ (US); and Scott E. Graham, Fountain Hills, AZ (US)
Assigned to AeroData, Inc., Scottsdale, AZ (US)
Filed by AeroData, Inc., Scottsdale, AZ (US)
Filed on Jun. 15, 2021, as Appl. No. 17/304,150.
Application 17/304,150 is a continuation of application No. 16/948,854, filed on Oct. 2, 2020, granted, now 11,066,181.
Claims priority of provisional application 62/910,084, filed on Oct. 3, 2019.
Prior Publication US 2021/0354808 A1, Nov. 18, 2021
This patent is subject to a terminal disclaimer.
Int. Cl. B64D 43/00 (2006.01); B64C 25/42 (2006.01); B64D 45/08 (2006.01); B60T 8/17 (2006.01)
CPC B64C 25/426 (2013.01) [B60T 8/1703 (2013.01); B64D 43/00 (2013.01); B64D 45/08 (2013.01)] 15 Claims
OG exemplary drawing
 
1. A system for displaying an engine failure awareness chart, comprising:
a user interface configured to display the engine failure awareness chart;
at least one processor configured to:
obtain an engine-out projected climb performance of the aircraft and a plurality of locations of ground-based obstacles; and
determine a distance between the aircraft and the locations of the ground-based obstacles; and
at least one display displaying the engine failure awareness chart by the at least one user interface, the engine failure awareness chart comprising a plurality of obstacle regions color coded based on the determined distance and the engine-out projected climb performance of the aircraft.