Abstract: A portable electronic device for assessing an affected area of an aircraft is disclosed. A reference marker having a known size is located on the aircraft. The portable electronic device includes a processor in communication with a structural database, where the structural database includes a template that defines a maximum allowable size of damage to the aircraft. The processor executes instructions for determining an actual size of the affected area based on the known size of the reference marker. The processor also executes instructions for comparing the actual size of the affected area with the maximum allowable size of damage to the aircraft. The processor further executes instructions for determining that the actual size of the affected area exceeds the maximum allowable size of damage to the aircraft.

Abstract: Tread profile of a pneumatic vehicle tyre—in particular for commercial vehicles—comprising a regroovable tread profile with radially raised profile elements (1, 2, 3, 4, 5) and with grooves (6, 7, 8, 9), which respectively separate two adjacent profile elements (1, 2, 3, 4, 5) from one another, wherein the grooves (6, 7, 8, 9) are bounded inwards in the radial direction R by a groove base (10) and on both sides in the axial direction by a profile element flank, forming the groove wall (12, 13), and wherein at least one regrooving indicator (14) for indicating the regrooving depth is respectively formed in one or more grooves (3), characterized in that, in at least one groove (8), all of the regrooving indicators (14) formed therein are formed in a groove wall (12) at a height H measured in the radial direction R of H>0 mm above the groove base (10), wherein the height H corresponds to the maximum radial abrasion position of the tyre for regrooving.

Abstract: A portable electronic device for assessing an affected area of an aircraft is disclosed. A reference marker having a known size is located on the aircraft. The portable electronic device includes a processor in communication with a structural database, where the structural database includes a template that defines a maximum allowable size of damage to the aircraft. The processor executes instructions for determining an actual size of the affected area based on the known size of the reference marker. The processor also executes instructions for comparing the actual size of the affected area with the maximum allowable size of damage to the aircraft. The processor further executes instructions for determining that the actual size of the affected area exceeds the maximum allowable size of damage to the aircraft.

Abstract: A system for assessing an affected area of an aircraft is disclosed. A reference marker having a known size is placed along an exterior of the aircraft. The system includes a portable electronic device including a processor in communication with a structural database. The structural database includes a template that defines a maximum allowable size of damage to the aircraft. The processor executes an instruction for determining an actual size of the affected area based on the known size of the reference marker. The processor executes an instruction for comparing the actual size of the affected area of the aircraft with the maximum allowable size of damage to the aircraft. The processor executes an instruction for determining if the actual size of the affected area exceeds the maximum allowable size of damage to the aircraft. The processor executes an instruction for determining a further action.

Abstract: Methods and systems for augmenting situational awareness using a controllable window are described. An environmental condition within a field of view of the controllable window is determined. Light transmissivity of the controllable window is selectively changed based on the determined environmental condition. In some implementations, multiple points of view can be provided to multiple viewers.

Abstract: A method includes receiving visual flight rules (VFR) data and determining a suggested path of approach for an aircraft based on the VFR data. The suggested path of approach may correspond to a flight path of the aircraft to a runway of an airport. The method includes highlighting a representation of the suggested path of approach at a display device.

Abstract: A method and apparatus for predicting fuel for an aircraft. Remaining amounts of fuel that will be present for types of fuel use for the aircraft at a destination are predicted. Flight times for the types of fuel use are calculated from the remaining amounts of fuel predicted for the types of fuel use for the aircraft at the destination. Graphical indicators are displayed indicating the types of fuel use and the flight times for the types of fuel use.

Abstract: A system for assessing an affected area of an aircraft is disclosed. A reference marker having a known size is placed along an exterior of the aircraft. The system includes a portable electronic device including a processor in communication with a structural database. The structural database includes a template that defines a maximum allowable size of damage to the aircraft. The processor executes an instruction for determining an actual size of the affected area based on the known size of the reference marker. The processor executes an instruction for comparing the actual size of the affected area of the aircraft with the maximum allowable size of damage to the aircraft. The processor executes an instruction for determining if the actual size of the affected area exceeds the maximum allowable size of damage to the aircraft. The processor executes an instruction for determining a further action.

Abstract: A method and apparatus for predicting fuel for an aircraft. Remaining amounts of fuel that will be present for types of fuel use for the aircraft at a destination are predicted. Flight times for the types of fuel use are calculated from the remaining amounts of fuel predicted for the types of fuel use for the aircraft at the destination. Graphical indicators are displayed indicating the types of fuel use and the flight times for the types of fuel use.

Abstract: A system for determining an anchoring location of a marine vessel. The system includes a first computing device configured to capture location data of the marine vessel along a route of the marine vessel, and a second computing device. The second computing device including a memory area, a location component that determines location data of a marine vessel, and a processor. The processor is programmed to receive, from the first computing device, the location data of the marine vessel, determine, from the location data, a location along a route of the marine vessel that the marine vessel traveled a distance less than a maximum threshold distance over a predefined period of time, and identify the location along the route of the marine vessel that the marine vessel traveled a distance less than the anchoring threshold distance over the predefined period of time as an anchoring location.

Abstract: Methods and systems for augmenting situational awareness using a controllable window are described. An environmental condition within a field of view of the controllable window is determined Light transmissivity of the controllable window is selectively changed based on the determined environmental condition. In some implementations, multiple points of view can be provided to multiple viewers.

Abstract: A method includes receiving visual flight rules (VFR) data and determining a suggested path of approach for an aircraft based on the VFR data. The suggested path of approach may correspond to a flight path of the aircraft to a runway of an airport. The method includes highlighting a representation of the suggested path of approach at a display device.

Abstract: A method and apparatus for managing a map of an airport. The map of the airport is displayed on a display device. A movement of a number of fingers with respect to a number of aeronautical objects on the map of the airport is detected. Information generated by an operation based on the number of aeronautical objects on the map of the airport is displayed in response to detecting the movement of the number of fingers with respect to the number of aeronautical objects on the map of the airport.

Abstract: A system for display management based on operator stress level employs a biosensor detecting stress level of an operator. A biomonitoring system receives input from the biosensor and provides an output responsive to a threshold of stress. An operational display control receives the output from the biomonitoring system and modifies an information display based on the stress threshold.

Abstract: A system for determining an anchoring location of a marine vessel. The system includes a first computing device configured to capture location data of the marine vessel along a route of the marine vessel, and a second computing device. The second computing device including a memory area, a location component that determines location data of a marine vessel, and a processor. The processor is programmed to receive, from the first computing device, the location data of the marine vessel, determine, from the location data, a location along a route of the marine vessel that the marine vessel traveled a distance less than a maximum threshold distance over a predefined period of time, and identify the location along the route of the marine vessel that the marine vessel traveled a distance less than the anchoring threshold distance over the predefined period of time as an anchoring location.

Abstract: A method and apparatus for managing a route for an aircraft or managing a map of an airport. The map is displayed on a display device. A movement of a number of fingers with respect to a number of aeronautical objects on the map is detected. The route for the aircraft is changed or information generated by an operation based on the number of aeronautical objects on the map is displayed in response to detecting the movement of the number of fingers with respect to the number of aeronautical objects on the map.

Abstract: A system for display management based on operator stress level employs a biosensor detecting stress level of an operator. A biomonitoring system receives input from the biosensor and provides an output responsive to a threshold of stress. An operational display control receives the output from the biomonitoring system and modifies an information display based on the stress threshold.

Abstract: A computer implemented method, apparatus, and computer usable program code for proposing an update for a navigation chart displayed in an aircraft data processing system. A selection of a navigation object is received in the navigation chart through the aircraft data processing system. In response to receiving the selection, a set of attributes is presented for the navigation object, wherein each attribute can be selected containing a discrepancy. In response to receiving user input to change an attribute in the set of attributes, the attribute is changed using the user input. A discrepancy report is directly sent to the data provider via a datalink.

Abstract: A method and apparatus for managing a route for an aircraft or managing a map of an airport. The map is displayed on a display device. A movement of a number of fingers with respect to a number of aeronautical objects on the map is detected. The route for the aircraft is changed or information generated by an operation based on the number of aeronautical objects on the map is displayed in response to detecting the movement of the number of fingers with respect to the number of aeronautical objects on the map.

Abstract: A computer implemented method, apparatus, and computer usable program code for proposing an update for a navigation chart displayed in an aircraft data processing system. A selection of a navigation object is received in the navigation chart through the aircraft data processing system. In response to receiving the selection, a set of attributes is presented for the navigation object, wherein each attribute can be selected containing a discrepancy. In response to receiving user input to change an attribute in the set of attributes, the attribute is changed using the user input. A discrepancy report is directly sent to the data provider via a datalink.