Overview: The ACS 2002 is an advanced engine monitoring system designed for experimental aircraft with 4 or 6 cylinder engines. It provides comprehensive monitoring and data acquisition capabilities, displaying all engine data on a customizable, sunlight-readable color LCD.

Key Features:

• Engine Instruments: Monitors manifold pressure, RPM, fuel flow, fuel PSI, oil temperature, oil PSI, volts, amps, and carburetor temperature.
• Cylinder Temperature Analyzer: Includes EGT, CHT, and EGT peak detection.
• Fuel Monitoring System: Tracks fuel computer data, tank levels, gallons used, gallons remaining, and hours remaining, with cross-checking capabilities.
• Voice Alerts: Provides alerts for critical conditions like oil temperature and fuel levels.
• Flight Timer: Records last flight and total flight times for the day.
• Data Logging: Stores all instrument readings every 5 seconds for post-flight analysis.
• User Inputs and Configurations: Includes four user inputs and configurable ranges for alerts and checklists.
• System Clock: Displays time, date, and Zulu time.

Specifications:

• Display: 6.25” x 5” x 2.25” with reflective and backlight dimmable to 0 nits.
• Controller: 8.5” x 5.5” x 1.25”, weighing 1.5 lbs.
• Temperature Range: Operating from -30°C to +65°C, non-operating from -30°C to +85°C.
• Power Requirements: 9 to 36 Volts, 1 Amp @ 12 Volts.

Additional Features:

• Active Checklists: Stores up to 10 user checklist pages, accessible with a button press.
• Fuel Tank Functions: Calibrated for both level and tail-down positions, works with float or capacitance senders.
• Aircraft Functions: Monitors flap, elevator trim, and aileron positions.

Warranty: Comes with a limited one-year warranty covering defects in materials and workmanship, excluding consequential damages.

Usage Limitation: This instrument is intended for use in experimental aircraft only and is not approved for aircraft with FAA type certificates.