Aircraft Communication Addressing and Reporting System (or ACARS) is a digital datalink system for transmission of small messages between aircraft and ground stations via radio or satellite. The protocol was defined in the 1970s and uses telex formats. It will be superseded by the Aeronautical Telecommunications Network (ATN) protocol.
Prior to the introduction of datalink, all communication between the aircraft (i.e., the flight crew)and personnel on the ground was performed using voice communication. This communication used either VHF or HF voice radios, which was further augmented with SATCOM in the early 1990s.
The airlines, in an effort to reduce crew workload and improve data integrity, introduced the ACARS system in the late 1980’s. (A few initial ACARS systems were introduced before the late 1980's, but ACARS did not start to get any widespread use by the major airlines until the later part of the 1980's.) Although the term ACARS is often taken into context as the datalink avionics Line-replaceable unit installed on the aircraft, the term actually refers to a complete air and ground system. On the aircraft, the ACARS system was made up of an avionics computer called an ACARS Management Unit (MU) and a CDU (Control Display Unit). The MU was designed to send and receive digital messages from the ground using existing VHF radios. On the ground, the ACARS system was made up of a network of radio transceivers, which would receive (or transmit) the datalink messages, as well as route them to various airlines on the network.
Note that the initial ACARS systems were designed to the ARINC standard 597. This system was later upgraded in the late 1980’s to the ARINC 724 characteristic. ARINC 724 addressed aircraft installed with avionics supporting digital data bus interfaces. This was subsequently revised to ARINC 724B, which was the primary characteristic used during the 1990s for all digital aircraft. With the introduction of the 724B specification, the ACARS MUs were also coupled with industry standard protocols for operation with flight management system MCDUs using the ARINC 739 protocol, and printers using the ARINC 740 protocol. The industry has defined a new ARINC characteristic, called ARINC 758, which is for CMU systems, the next generation of ACARS MUs.
In addition to the FMS and FDAMS interfaces, the industry started to upgrade the on-board Maintenance Computers in the 1990s to support the transmission of maintenance related information real-time through ACARS. This enabled airline maintenance personnel to receive real-time data associated with maintenance faults on the aircraft. When coupled with the FDAMS data, airline maintenance personnel could now start planning repair and maintenance activities while the aircraft was still in flight.
As an example, the flight crew could pull up a MCDU screen that allowed them to send to the ground a request for various weather information. Upon entering in the desired locations for the weather information and the type of weather information desired, the ACARS would then transmit the message to the ground. In response to this request message, ground computers would send the requested weather information back to the ACARS MU, which would be displayed and/or printed.
Airlines began adding new messages to support new applications (Weather, Winds, Clearances, Connecting Flights…) and ACARS systems became customized to support airline unique applications, and unique ground computer requirements. This results in each airline having their own unique ACARS application operating on their aircraft. Some airlines have more than 75 MCDU screens for their flight crews, where other airlines may have only a dozen different screens. In addition, since each airline’s ground computers were different, the contents and formats of the messages sent by an ACARS MU were different for each airline.
ATC messages are used to communicate between the aircraft and Air traffic control. These messages are defined in ARINC Standard 623. ATC messages are used by aircraft crew to request clearances, and by ground controllers to provide those clearances.
AOC and AAC messages are used to communicate between the aircraft and its base. These messages are defined by the users, but must meet the guidelines of ARINC Standard 618. Various types of messages are possible and these include fuel consumption, engine performance data, and aircraft position as well as free text data.
It should be noted that the majority of ACARS messages are typically only 100 to 200 characters in length. Such messages are made up of a one-block transmission from (or to) the aircraft. One ACARS block is constrained to be no more that 220 characters within the body of the message. For downlink messages which are longer than 220 characters, the ACARS unit will split the message into multiple blocks, transmitting each block to the RGS (there is a constraint that no message may be made up of more than 16 blocks). For these multi-block messages, the RGS collects each block until the complete message is received before processing and routing the message. The ACARS also contains protocols to support retry of failed messages or retransmission of messages when changing service providers.
Once the RGS receives the complete message, the RGS forwards the message to the datalink service provider's (DSP) main computer system. The DSP ground network uses landlines to link the RGS to the DSP. The DSP uses information contained in their routing table to forward the message to the airlines or other destinations. This table is maintained by the DSP and identifies each aircraft (by tail number), and the types of messages that it can process. (Each airline must tell its service provider(s) what messages and message labels their ACARS systems will send, and for each message, where they want the service provider to route the message. The service provider then updates their routing tables from this information.) Each type of message sent by the CMU has a specific message label, which is contained in the header information of the message. Using the label contained in the message, the DSP looks up the message and forwards to the airline’s computer system. The message is then processed by the airline’s computer system.
This processing performed by an airline may include reformatting the message, populating databases for later analysis, as well as forwarding the message to other departments, such as flight operations, maintenance, engineering, finance or other organizations within an airline. In the example of a delay message, the message may be routed via the airline’s network to both their operations department as well as to a facility at the aircraft’s destination notifying them of a potential late arrival.
The transmission time from when the flight crew presses the send key to send the message, to the time that it is processed within an airline’s computer system varies, but is generally on the order of 6 to 15 seconds. The messages that are sent to the ground from the CMU are referred to as a downlink message.
The DSP transmits the message over their ground network to a VHF remote ground station in the vicinity of the aircraft. The remote ground station broadcasts the message over the VHF frequency. The on-board VHF radio receives the VHF signal and passes the message to the CMU (with the internal modem transforming the signal into a digital message). The CMU validates the aircraft registration number, and processes the message.
The processing performed on the uplink message by the CMU depends on the specific airline requirements. In general, an uplink is either forwarded to another avionics computer, such as an FMS or FDAMS, or is processed by the CMU. For messages which the CMU is the destination, such as a weather report uplink, the flight crew can go to a specific MCDU screen which contains a list of all of the received uplink messages. The flight crew can then select the weather message, and have the message viewed on the MCDU. The ACARS unit may also print the message on the cockpit printer (either automatically upon receiving the message or upon flight crew pressing a PRINT prompt on the MCDU screen).
There are 3 major components to the ACARS datalink system:
Aircraft equipment consists of airborne end systems and a router. End systems are the source of ACARS downlinks and the destination for uplinks. The MU/CMU is the router. Its function is to route a downlink by means of the most efficient air-ground subnetwork. In many cases, the MU/CMU also acts as an end system for AOC messages.
Typical airborne end systems are the Flight management system (FMS), datalink printer, maintenance computer, and cabin terminal. Typical datalink functions are:
ACARS messages are transmitted over one of three air-ground subnetworks.
The router function built into the MU/CMU determines which subnetwork to use when routing a message from the aircraft to the ground. The airline operator provides a routing table that the CMU uses to select the best subnetwork.
Because the ACARS network is modeled after the point-to-point telex network, all messages come to a central processing location. The DSP routes the message to the appropriate end system using its network of land lines and ground stations. Before the days of computers, messages would come in to the central processing location and be punched to paper tape. The tape would be physically carried to the machine connected to the intended destination. Today the routing function is done by computer, but the model remains the same.
There are currently two primary service providers of ground networks in the world (ARINC and SITA), although specific countries have implemented their own network, with the help of either ARINC or SITA. ARINC operates a network in North America, and have also recently started operating a network in Europe. ARINC has also assisted the CAAC in China, as well as Thailand and South America with the installation of VHF networks. SITA has operated the network in Europe, Middle East, South America and Asia for many years. They have also recently started a network in the US to compete with ARINC.
Until recently, each area of the world was supported by a single service provider. This is changing, and both ARINC and SITA are competing and installing networks that cover the same regions.
This product is now been extended into the eFlight concept for integrated airlines operations see eFlight
ARINC 607 – Design Guidance for Avionics Equipment. Includes definition of Aircraft Personality Module (APM), required for ARINC 758 CMU installation.
ARINC 429 – specification for receiving and broadcasting ARINC 429 broadcast data (data received from other avionics LRUs).
ARINC 618 – Defines the air / ground protocols for communicating between the ACARS / CMU and VHF ground systems. Also defines the format of the ACARS messages sent by the ACARS / CMU as well as received by the ACARS CMU. The format of this message is called a Type A message. This characteristic has been updated to define the future VDL Mode 2 AOA operation.
ARINC 619 – Defines the protocols for the ACARS / CMU to use to transfer file data between other avionics in the aircraft. ARINC 619 covers file protocols that are used to interface with FMS, FDAMS, Cabin Terminal, Maintenance Computers, SATCOM systems and HF Voice Data Radios.
ARINC 620 – Defines ground-to-ground communication protocols. This includes the message format of messages routed between a service provider and an airline or other ground system. This is referred to as a Type B message (the air/ground Type A message is reformatted to a Type B message for ground transmissions).
ARINC 622 – Describes the processing associated with sending ATC application messages over today’s ACARS links (including ARINC 623 ATC messages).
ARINC 623 – This characteristic identifies ATC related messages that can be generated or received by an ACARS MU / CMU system (does not include FANS-1 or FANS-A messages that are processed by the FMS)
ARINC 724B – specification for an ACARS MU for ARINC 724B wiring.
ARINC 739 – Specification for interfacing with Multi-purpose Cockpit Display Units
ARINC 740 and 744 – Specification for interfacing to cockpit Printers.
ARINC 758 – Specification for a CMU relative to ARINC 758 wiring. This specification actually identifies various levels of functionality, these defining future growth phases for the CMU. Initial CMU systems which perform today’s ACARS functions are classified as Level OA.
ACARS | Aircraft Communications Addressing and Reporting System
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