Method and system for synchronizing a flight management system with an external device

1. An avionics system for an aircraft, the avionics system comprising:

a flight management system (FMS); and

an electronic flight bag (EFB) having a processor and communication link, and configured to:

generate at least one specialized message including multiple labels within the specialized message;

transmit at least one specialized header frame to a data network, the at least one specialized header frame including identification information relating to an impending transmission of a set of conforming data frames;

generate the set of conforming data frames, wherein each of the set of conforming data frames is indicated as one of the sets of conforming data frames by a single bit indicator relating the respective conforming data frame to the specialized header frame; and

transmit at least a subset of the set of conforming data frames to the data network;

wherein the FMS is configured to:

receive a transmission of data from the EFB;

attempt to load a portion of the transmission into a flight plan of the FMS;

determine if the load was successful;

generate a status message related thereto;

periodically output groups of data including a sequence number and a status message related to the sequence number; and

operate the aircraft according to the flight plan.

2. The avionics system of claim 1 wherein the FMS further outputs a description of a failure.

3. The avionics system of claim 2 wherein the FMS outputs the description periodically or upon a request from the EFB.

4. The avionics system of claim 1 , further comprising a Communications Management Unit (CMU) operably coupled to the FMS and communicatively coupled to the EFB and wherein the CMU uplinks the data and provides it to the FMS.

5. The avionics system of claim 4 , wherein the transmission of data from the EFB is routed through the Communications Management Unit (CMU) before reaching the FMS.

6. The avionics system of claim 1 , wherein the transmission of data from the EFB includes a description included with the sequence number.

7. The avionics system of claim 6 , wherein the description includes a waypoint, an airway, or procedure information.

8. The avionics system of claim 7 , wherein when the waypoint has duplicate identifiers and the status message includes a retransmit request or an ordered list of potential duplicates.

9. The avionics system of claim 8 , wherein the status message includes one or more error messages.

10. The avionics system of claim 6 , wherein the transmission of data further comprises a status identifier.

11. The avionics system of claim 10 , wherein the status message includes one or more error messages.

12. The avionics system of claim 1 , wherein when the attempt to load is unsuccessful, the FMS predicts a flight plan with unloaded data and the status message includes results for the predicted flight plan.

13. The avionics system of claim 1 , wherein the EFB is configured to transmit a version counter either periodically or upon request of the receiving.

14. The avionics system of claim 13 , wherein the version counter includes a log of changes to the flight plan done through the FMS and indicate to the EFB the changes which were made.

15. An avionics system for an aircraft, the avionics system comprising:

a flight management system (FMS); and

an electronic flight bag (EFB) having a processor and communication link, and configured to:

generate at least one specialized message including multiple labels within the specialized message;

transmit at least one specialized header frame to a data network;

generate a set of conforming data frames, wherein each of the set of conforming data frames is indicated as one of the sets of conforming data frames by a single bit indicator; and

transmit at least a subset of the set of conforming data frames to the data network;

wherein the FMS is configured to:

receive a transmission of data from the EFB;

attempt to load a portion of the transmission into a flight plan of the FMS;

determine if the load was successful;

generate a status message related thereto;

periodically output groups of data including a sequence number and a status message related to the sequence number;

receive an edit to the flight plan and provide a downlink to the EFB based thereon; and

operate the aircraft according to the flight plan.

16. An avionics system for an aircraft, the avionics system comprising:

a flight management system (FMS); and

a device external the FMS, the device external the FMS having a processor and communication link, and configured to:

generate at least one specialized message including multiple labels within the specialized message;

transmit at least one specialized header frame to a data network, the at least one specialized header frame including identification information relating to an impending transmission of a set of conforming data frames;

generate the set of conforming data frames, wherein each of the set of conforming data frames is indicated as one of the sets of conforming data frames by a single bit indicator relating the respective conforming data frame to the specialized header frame; and

transmit at least a subset of the set of conforming data frames to the data network;

wherein the FMS is configured to:

receive a transmission of data from the device;

attempt to load a portion of the transmission into a flight plan of the FMS;

determine if the load was successful;

generate a status message related thereto;

periodically output groups of data including a sequence number and a status message related to the sequence number; and

operate the aircraft according to the flight plan.

17. The avionics system of claim 16 , wherein the device is an electronic flight bag.

18. The avionics system of claim 16 , wherein the FMS further outputs a description of a failure.

19. The avionics system of claim 16 , further comprising a Communications Management Unit (CMU) operably coupled to the FMS and communicatively coupled to the device and wherein the CMU uplinks the data and provides it to the FMS.

20. The avionics system of claim 16 , wherein the FMS is further configured to receive an edit to the flight plan and provide a downlink to the device based thereon.