Manuel d'utilisation / d'entretien du produit Mark III du fabricant Honeywell
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HONEYWELL Aerospace Electronic Systems Page 1 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 2 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 3 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 4 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. • Define uplink and downlink message formats • Define the format of printed messages • Specify trigger logic (i.
HONEYWELL Aerospace Electronic Systems Page 5 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. time and money. However, to deliver the future datalink capability required by the airlines, both ground and airborne systems must have a transition to the next generation architecture.
HONEYWELL Aerospace Electronic Systems Page 6 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. includes such services as Providing world-wide Weather messages to the aircraft, as well as being an FAA approved distributor of messages such as Pre-Departure Clearances and ATIS.
HONEYWELL Aerospace Electronic Systems Page 7 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 8 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Figure 1 Mark III CMU Front Panel ARINC 607 defines the Aircraft Personality Module (APM) which contains all aircraft and system configuration information.
HONEYWELL Aerospace Electronic Systems Page 9 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Portable Data Loader 615 High speed ARINC 429 1 Baseline Ethernet Data Loader 615A Ethernet 10BaseT note 2 Growth PCMCIA --- PCMCIA 1 Baseline Notes: 1.
HONEYWELL Aerospace Electronic Systems Page 10 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 11 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Control and Display Unit (CDU) In the business jet and regional aircraft market place, there is limited cockpit pedestal real estate.
HONEYWELL Aerospace Electronic Systems Page 12 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 13 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. an extensive amount of ARINC 429 broadcast data providing aircraft performance related data.
HONEYWELL Aerospace Electronic Systems Page 14 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 15 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. through an automated code generation system specific to the target environment. Automated test scripts are also derived from the model database.
HONEYWELL Aerospace Electronic Systems Page 16 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Figure 7 Database Design The Flexible Input Data Base (FIDB) contains a list of all I/O parameters available for all aircraft within a fleet.
HONEYWELL Aerospace Electronic Systems Page 17 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 2.4 Certification Honeywell received the 1 st FAA certification in December 2001. This initial certification was for Embraer aircraft.
HONEYWELL Aerospace Electronic Systems Page 18 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 3 FUNCTIONAL OVERVIEW The Mark III CMU is designed to provide complete datalink capability, providing interfaces and support to today’s installed equipment.
HONEYWELL Aerospace Electronic Systems Page 19 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 20 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Once an AOC message has been viewed by the flight crew (and any required user action has been taken), it can be placed in one of 8 user defined review categories.
HONEYWELL Aerospace Electronic Systems Page 21 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Once the downlink message has been sent, the message will be placed in the user defined review category specified for the message.
HONEYWELL Aerospace Electronic Systems Page 22 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. • Maintenance Memory Integrity: Verify that faults that are written to the maintenance memory are correctly retained in memory.
HONEYWELL Aerospace Electronic Systems Page 23 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. kbps. 3 D8PSK TDMS Same as Mode 2 except the voice is now digitized and the Medium Access changes.
HONEYWELL Aerospace Electronic Systems Page 24 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. support as part of the baseline the text Weather uplinks which has become standard use within the Air transport industry.
HONEYWELL Aerospace Electronic Systems Page 25 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. the addition of encryption algorithms in the future. As part of this work, Honeywell is currently under contract with the U.
HONEYWELL Aerospace Electronic Systems Page 26 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 4 DATABASES Honeywell pioneered the concept of airline reconfiguration and partitioned software for datalink systems in the early 1990s.
HONEYWELL Aerospace Electronic Systems Page 27 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Figure 10 FIDB Architecture The FIDB defines the same name for a given aircraft parameter (i.
HONEYWELL Aerospace Electronic Systems Page 28 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Figure 11 AMI/HGI Generation The GST offers a robust set of capabilities that allow the user to completely customize their AOC application.
HONEYWELL Aerospace Electronic Systems Page 29 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 4.2.1 Menus Since the AOC application is completely customizable, the user can define the set of menus that navigate through the various AOC datalink pages.
HONEYWELL Aerospace Electronic Systems Page 30 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Screens, including menus, can consist of multiple (up to 9) pages. Note the 1/2 in the upper right corner of the Main Menu display indicating page 1 of 2.
HONEYWELL Aerospace Electronic Systems Page 31 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 32 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. This discussion of the GBST and how it is used is equally applicable to both the AMI and the HGI.
HONEYWELL Aerospace Electronic Systems Page 33 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. In addition to the AOC screens defined by the AMI, and ATC screens defined by the HGI, there are additional menus screens within the Mark III CMU, referred to as System screens.
HONEYWELL Aerospace Electronic Systems Page 34 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 4.2.2 Uplinks For uplink messages, the user can define both the screen layout and the uplink message format.
HONEYWELL Aerospace Electronic Systems Page 35 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 36 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Figure 19 Clearance Message References If a crew response is required, the user would typically create response action prompts, such as the ACCEPT and REJECT prompts shown in Figure 17.
HONEYWELL Aerospace Electronic Systems Page 37 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. The user can also specify a REJECT REASONS action prompt, which allows the flight crew to specify the reason for rejecting the Clearance (see Figure 20).
HONEYWELL Aerospace Electronic Systems Page 38 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. There are a number of different types of objects that can be placed on a display. As an example, for the Main Menu, page prompts are used to link to other pages.
HONEYWELL Aerospace Electronic Systems Page 39 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 40 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 41 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 42 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 4.2.4 Print Definition The user can define the print format for a message by specifying the field names and associated parameters.
HONEYWELL Aerospace Electronic Systems Page 43 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Logic units can be used to specify OOOI conditions. OOOI logic can be as simple or as complex as the user requires.
HONEYWELL Aerospace Electronic Systems Page 44 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. to use for message transmission. The user also can specify the set of VHF frequencies to use for that region.
HONEYWELL Aerospace Electronic Systems Page 45 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 46 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Figure 30 Areas The Mark III CMU GBST provides the next generation in Airline reconfiguration.
HONEYWELL Aerospace Electronic Systems Page 47 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 48 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 5.1.2 Processor CCA The processor circuit card assembly contains the MARK III core microprocessor, supporting logic circuits, and memory devices.
HONEYWELL Aerospace Electronic Systems Page 49 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. • Patented multi-layer microstrip/fiberglass high reliability printed wiring board (PWB • Analog Output Discretes • PCI BUS-based Connector 5.
HONEYWELL Aerospace Electronic Systems Page 50 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 51 Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
HONEYWELL Aerospace Electronic Systems Page 52 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 5.3 Mechanical Packaging 5.3.1 Unit Weight The MARK III LRU maximum weight is twelve pounds.
HONEYWELL Aerospace Electronic Systems Page 53 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 5.4 Environmental Specifications The following DO-160D categories will be used for the MARK III: Temperature and Altitude (DO-160D Section 4.
HONEYWELL Aerospace Electronic Systems Page 54 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Waterproofness (DO-160D Section 10.0) Category X, Not Applicable Fluids Susceptibility (DO-160D Section 11.
HONEYWELL Aerospace Electronic Systems Page 55 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Category A2, Pin Injection Tests (DO-160C Section 22.5.1) Waveform 3 (DO-160D Section 22, Figure 22-4), Voc/Isc = 250V/10A, and Frequency = 1 Mhz + 20%.
HONEYWELL Aerospace Electronic Systems Page 56 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. Nominal +27.5 Vdc Minimum +20.5 Vdc Maximum +32.2 Vdc Nominal 50 Watts Maximum 100 Watts 5.
HONEYWELL Aerospace Electronic Systems Page 57 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. 6 SUMMARY The Mark III CMU is a high-end system which provides the latest in both hardware and software technology, unequalled in the industry.
HONEYWELL Aerospace Electronic Systems Page 58 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. The Mark III CMU has also been designed to support a future upgrade for new Gatelink technology.
HONEYWELL Aerospace Electronic Systems Page 59 Use or disclosure of information on this page is subject to the restrictions on the title page of this document. The Mark III CMU is designed to provide airlines with a hardware platform with the best growth potential of any system in the market.
Un point important après l'achat de l'appareil (ou même avant l'achat) est de lire le manuel d'utilisation. Nous devons le faire pour quelques raisons simples:
Si vous n'avez pas encore acheté Honeywell Mark III c'est un bon moment pour vous familiariser avec les données de base sur le produit. Consulter d'abord les pages initiales du manuel d'utilisation, que vous trouverez ci-dessus. Vous devriez y trouver les données techniques les plus importants du Honeywell Mark III - de cette manière, vous pouvez vérifier si l'équipement répond à vos besoins. Explorant les pages suivantes du manuel d'utilisation Honeywell Mark III, vous apprendrez toutes les caractéristiques du produit et des informations sur son fonctionnement. Les informations sur le Honeywell Mark III va certainement vous aider à prendre une décision concernant l'achat.
Dans une situation où vous avez déjà le Honeywell Mark III, mais vous avez pas encore lu le manuel d'utilisation, vous devez le faire pour les raisons décrites ci-dessus,. Vous saurez alors si vous avez correctement utilisé les fonctions disponibles, et si vous avez commis des erreurs qui peuvent réduire la durée de vie du Honeywell Mark III.
Cependant, l'un des rôles les plus importants pour l'utilisateur joués par les manuels d'utilisateur est d'aider à résoudre les problèmes concernant le Honeywell Mark III. Presque toujours, vous y trouverez Troubleshooting, soit les pannes et les défaillances les plus fréquentes de l'apparei Honeywell Mark III ainsi que les instructions sur la façon de les résoudre. Même si vous ne parvenez pas à résoudre le problème, le manuel d‘utilisation va vous montrer le chemin d'une nouvelle procédure – le contact avec le centre de service à la clientèle ou le service le plus proche.
