
ACFMS with Global Positioning System Interface
SEI’s Airframe Cumulative Fatigue Monitoring System (ACFMS) now comes with an integrated Global Positioning System (GPS) interface, adding another layer of precision to its fatigue monitoring capabilities.
Designed for low power consumption and ease of installation, the ACFMS uses the A1000 Cumulative Fatigue Recorder (CFR) to track key flight parameters like airspeed, altitude, and accelerations, while also recording GPS coordinates for location-specific analysis of structural stress and fatigue across your aircraft fleet.
Description
ACFMS is an advanced, low-cost data recording system capable of monitoring airspeed, altitude, and accelerations. The "heart" of the system is the Cumulative Fatigue Recorder (CFR) Model A1000, capable of recording eight analog and eight digital signals.
The CFR's low power consumption, light weight, and small size allow for easy aircraft installation. The ACFMS includes the Air Data Transducer (ADX) TR-359, which converts the aircraft's pitot and static pressures into CFR compatible signals.
Specifications
SUMMARY SPECIFICATIONS—ACFMS | |
Input Voltage: | +9 to 36 VDC |
Power Consumption: | < 3 Watts |
Weight: | < 2 pounds |
Memory Capacity: | 512k bytes |
Analog Channels: | 8 (0 to 5 VDC) |
Digital Channels: | 8 (CMOS) |
Date / Time: | Internal Real-Time-Clock |
Communications Interface: | RS-485 |
Download Interface: | RS-232 |
Voltage Outputs: | +5 and ±15 VDC |
Operating Environment: | -40ºC to +85ºC |