Portable GPS Flight Inspection System

System Features

• Simple aircraft installation
• Inspection and certification of GPS Non-Precision approaches
• High accuracy, real time differential GPS (DGPS) positioning
• No ground-based operator required
• Notebook computer processing, control and display
• Adaptation of U.S. FAA-proven GPS-NP inspection software
• Upgradeable to dual-frequency DGPS positioning

Airborne Unit

The airborne component consists of:

• IBM Thinkpad notebook computer or equivalent
• 12-channel GPS receiver
• 5-watt synthesized netlink radio data system (SNRDS)
• UHF data link
• All necessary cables and antennas
• Compact carry-on-board case

Ground Unit

The ground component, which is remotely activated and controlled from the aircraft, consists of:

• GPS and UHF units identical to the airborne component
• Internal battery charger
• All necessary cables and antennas
• Locking weather-proof case

Accessory Case

The accessory case is a locking case that provides: Storage space for all Antennas, Tripods, Cables and Other Accessories