STANDARD AVIONICS PACKAGE Clause Samples

STANDARD AVIONICS PACKAGE. 1st PFD (Pilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data CFA October 2007 Page 24 Contract Number 160507 • 2nd PFD (Copilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data • 1st MFD (Pilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data • 2nd MFD (Copilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data • One Electronic Standby Instruments System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data) • Two Attitude and Heading Reference Systems (Mins) • Two Air Data Modules (ADMs) • Two flux valves • Two Display Controllers (DCs) • Two Cursor Control Devices (CCDs) • One Reversion Control Panel (RCP) • One Display Dimming Control Panel (DCP) • One Stability Augmentation System (SAS) control panel • Two Remote Instrument Controllers (RICs) • Two Modular Avionic Units (▇▇▇▇) incorporating the following major subsystems and/or functions: • Vehicle Monitoring System — VMS (dual) • Monitor Warning System — MWS (dual) • Aural Warning Generator — AWG (single) • Central Maintenance Computer — CMC (single) • 3—Axis Digital Automatic Flight Control System — DAFCS (dual) with autotrim function • Provision for CVR/FDR data interface (single) • Flight Director System (dual) • Pilot and copilot microphone and headset • Pilot and Copilot interphone control (cyclic grip and floor switches) • Left Modular Radio Cabinet (MRC) with the following modules: • One VHF Comm_ • One VOR/LOCJGS/MB • Right Modular Radio Cabinet (MRC) with the following modules: • One VHF Comm. • One Mode—S diversity transponder • One VOR/LOC/GS/M13 • One ADF • One DME • Two pedestal mounted MCDUs (Multi Control Function Display Units) • 1st Radar Altimeter (RT — 300) • 2nd Radar Altimeter System (RT — 300) • Emergency Locator Transmitter (ELT — 121.5/243/406 MHz) • One Flight Guidance Controller CFA October 2007 Page 25 Contract Number 160507 • Honeywell GPS module with Flight Plan Management System (FPMS) • Pilot and copilot digital audio panels with remote ICS audio port for ground operation Pilot clock (digital) • Cop...