Avionics Clause Samples

The Avionics clause defines the requirements and standards for the electronic systems used in an aircraft, such as navigation, communication, and control equipment. It typically outlines the specifications that the avionics must meet, the procedures for installation and testing, and any applicable regulatory compliance. By clearly setting these expectations, the clause ensures that all avionics components are reliable, compatible, and safe, thereby reducing the risk of malfunction and ensuring operational integrity.
Avionics. Any proposal for avionics work is subject to Haven MRO (formerly Flight Mechanix)’s review of the aircrafts wiring diagrams, availability of adequate space and power on the aircraft, the aircrafts compatibility with the system to be installed and an explanation of Customer’s expectations and mission requirements. Haven MRO (formerly Flight Mechanix) requires that Customer send avionics drawing, a photograph of the instrument panels and pedestal and an equipment list.
Avionics. ‌ The Stratos 714 will have an integrated all-glass avionics suite. There will be two primary flight displays and a single multi function display. The functions of the integrated avionics suite will satisfy all certification requirements and much more. The avionics suite will be easy to use and enhance situational awareness. Key features will include: • Display of air data information • Display of attitude, heading, and slip/skid. • Weather and traffic information (Satellite based) (optional, subscription) • Moving map. • Airport diagrams (subscription) • GPS-WAAS navigation. • Flight director. • Terrain awareness and terrain warning (subscription) • Mode S transponder. • Dual VHF communication radios. • VOR/ILS navigation. • Display of engine parameters. • Warning systems (aural and visual) including master caution/warning. • Autopilot (integral to the avionics suite). • Intercom (for all occupants). • ELT (406 MHz). • Airborne weather radar (optional) As of this revision of the technical description, the avionics suite supplier has not yet been selected. In addition to satisfying all the specific requirements, the avionics suite will be a proven system with an operational history.
Avionics. The Contractor shall provide technical and management expertise for the effective planning and coordination of resources necessary for satisfaction of SOW requirements of the delivered LDPE avionics subsystem components and system from ATP through BL-BFT and through Phase-2 if option is exercised.
Avionics. Any proposal for avionics work is subject to Jet East’s review of the aircraft’s wiring diagrams, availability of adequate space and power on the aircraft, the aircraft’s compatibility with the system to be installed and an explanation of Customer’s expectations and mission requirements. Jet East requires that Customer provides current avionics drawing, a photograph of the instrument panels and pedestal and an equipment list.
Avionics. Seller represents that the FMS and all other avionics on the Aircraft shall be equipped with the latest software version available and certified for installation and operation (for its intended use) on the Falcon 2000EX EASy as of the Delivery Date at no additional expense to Buyer.
Avionics. Updated Avionics to comply with and meet requirements for Automatic Dependent Surveillance- Broad Cast.
Avionics. Safety regulations impose a high degree of reliability of all aeronautics equipment. It covers among others, the manufacturing process, the functionality correctness, the fault tolerance, the lifecycle management. The certification process is standardized worldwide and is declined in several levels for both software and hardware equipment. For software the DO-178 B is an international standard and covers a range of levels from A (most critical systems) to E (less critical systems). In order to achieve compliance to most critical levels (A to C), it is common practice to have multiple redundant systems providing the same function. Integrated Modular Avionics (IMA) has provided a great benefit by introducing the capability of coexistence of several functions on the same equipment, with the strong requirement to be able to prove functional independence, including in case of failure. In particular a failure of a function shall not trigger failure for other functions coexisting on the same equipment. The ARINC 653 norm, elaborated in order to specify the properties needed by the IMA platform in order to support such applications is an example of platform virtualization for applications, based on a temporal share of hardware resources. Determinism of execution of applications is the main resulting capability provided by IMA. However, the IMA approach already addresses specifically the coexistence of functions with mixed criticality levels (for instance mixing level B and level D functions), since it states that the most critical level imposes its compliance. Virtualization in avionics provides the necessary capabilities to mix several criticality levels. Today in most planes all electronic equipment has to be switched off at specific phases of flight (takeoff and landing). In-flight entertainment systems, although part of the aircraft, are similarly not usable during these phases. Cabin crew resources and IFE (In-Flight Entertainment) resources are usually completely separate although they use a number of similar functions such as message broadcast and call notification. Virtualization with adequate priority handling mechanisms is able to provide mutualization of these functions (cabin crew first, IFE next), as well as a potential for more services (multicasting, geographical routing on large planes), not achievable with currently separate systems. External communications are very limited from an airplane. Similarly to what is now possible with high-speed trains...
Avionics. C▇▇▇▇▇▇ IDS-850 4-Tube EFIS Rosemount Temp. Probe Dual C▇▇▇▇▇▇ VHF-422B Comms w/8.33 SpacingCollins FCS-850 Flight Control System Dual C▇▇▇▇▇▇ VIR-432 Navs KHF-950 HF Radio w/Selcal C▇▇▇▇▇▇ ADF-462 ADF C▇▇▇▇▇▇ ALT-55B Radio Altimeter Dual C▇▇▇▇▇▇ DME-442 DME’s Dual Channel Magnastar C- 2000 FlightPhone Dual C▇▇▇▇▇▇ TDR-94D Transponders Universal Cockpit Voice Recorder C▇▇▇▇▇▇ TWR-850 Radar System Allied Signal M▇▇▇ V EGPWS Dual Universal UNS-1C FMS -w/ Windshear Alert TCAS II w/ Change 7 406 ELT with Nav Interface RVSM Compliant UniLink In-Flight Information System
Avionics. With respect to Avionics, the Asset Transfer Date will occur on the Avionics Closing Date.

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