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Контакты
Головной Офис Объединенные Арабские Эмираты Международный Аэропорт Шарджа
тел.: +971 6 5570710
факс: +971 6 5570495
По вопросам продаж: sales@trast-aero.com
The MK XXII Helicopter Enhanced Ground Proximity Warning System (EGPWS) brings state-of-the-art technology in Terrain Display, Situational Awareness, Terrain, and Obstacle Warning and Advisory Callouts to the Rotorcraft Pilot. The MK XXII is lightweight, compact and rugged computer that is easily installed in modern Helicopters.
Based on 30 years experience in the development and advancement of Ground Proximity Warning Systems for Air Transport, Regional and Commuter Airlines, Military aircraft and Corporate Aviation, Honeywell brings this vital safety technology to all segments of helicopter operations. Using our proprietary world-wide terrain database, obstacle database, runway/helipad database, state-of-the-art GPS technology, and proven Terrain Display with Alerting and Warning functions, the MK XXII provides the Helicopter Pilot with superior Situational Awareness with respect to terrain and known obstacles. In addition, the MK XXII contains the most advanced alerting and warning functionality to warn the pilot of danger with respect to terrain, man-made obstacles and other primary scenarios associated with the dangers of Controlled Flight Into Terrain (CFIT).
Спецификация
Basic Ground Proximity Warning
Altitude Awareness Callouts
Bank Angle Alert
Tail Strike Alert (only on applicable aircraft)
Enhanced features, Terrain and Obstacle Awareness Alerts and Warnings as well as optional display of this information, and "Peaks" mode.
Input signal processing (including filtering and signal monitoring).
Alert output processing (including alert prioritization, voice message synthesis, audio output and display and warning lamp drivers)
Built In Test and Monitoring including cockpit-activated self test.
PCMCIA interface for uploading software and databases (using a Smart Cable).
Front panel maintenance test connector for system checkout and troubleshooting.
System Status LED’s located on the LRU front panel to indicate External Fault, Computer O.K. and Computer Fail conditions.
Характеристики
Packaging: Non-ARINC
Dimension (H x W x L): 6.2 x 3.0 x 12.1 Inches (approx.)
Weight: 3.5 lbs. / 1.6 kg. Maximum
Power Requirement: 28 VDC 15 watts normal operation
Cooling: Per ARINC 600-6, forced air cooling not required
Environmental: Meets RTCA DO-160D
MTBF: 15,000 operating hours
Software: Meets RTCA DO-178B Level C and D
Certification TAWS: Designed and certified to TSO-C151a, Class A, GPWS and TAD functions are tailored uniquely to helicopter flight profiles
Data Loader: Databases and software updated via the front RS 232 Connector and Smart Cable PCMCIA Interface
