Honeywell 7510100-733 Primus II SRZ-85X Integrated Aircraft Navigation Unit with DME

Honeywell · Industrial Automation & Electrical

Description The Honeywell 7510100-733 Integrated Navigation Unit is an avionics navigation module designed for the Primus II SRZ-85X Integrated Radio System used in fixed-wing and helicopter aircraft applications. This unit combines VOR, localizer, glideslope, marker beacon scanning, and Distance Measuring Equipment (DME) functionality into a self-contained aerospace navigation assembly. Engineered for demanding aviation environments, the Honeywell 7510100-733 delivers reliable navigation signal processing, high-altitude operational capability, and compatibility with advanced aircraft radio systems.     Technical Specifications  Condition New/Never Used Surplus Brand Honeywell Category Avionics Part Number 7510100-733 Subcategory Integrated Navigation Units Product Type Integrated Navigation Unit System Compatibility Primus II SRZ-85X Integrated Radio System Navigation Functions VOR, Localizer, Glideslope, Marker Beacon, DME Power Requirement 28 VDC Power Consumption 55 Watts Nominal AC Input Requirement 26 V, 400 Hz, 0.026 VA Maximum Communication Bus Radio System Bus (RSB) Digital Audio Outputs 2 Audio Output Buses Operating Temperature -55°C to +70°C Maximum Operating Altitude 70,000 ft Decompression Range 8,000 to 70,000 ft Overpressure Capability -15,000 ft Environmental Standard DO-160B TSO Certifications C34d, C35d, C36d, C40b, C66b Mounting Compatibility P/N 7510124-910 or 7510124-911 Dimensions 14.01" L x 8.90" W x 3.38" H Weight 11.9 lb Aircraft Compatibility Fixed Wing and Helicopter Platforms Connector Type Ribbon Cable Interface   Information About 7510100-733 The 7510100-733 is an integrated avionics navigation unit developed by Honeywell as part of the Primus II SRZ-85X Integrated Radio System architecture. It contains multiple navigation subsystems including VOR, localizer, glideslope, marker scanning, and DME modules housed within a compact self-contained assembly that interfaces with the cluster module through ribbon cable connections. Designed to meet stringent aerospace environmental and performance standards, the unit supports operation in fixed-wing aircraft, helicopters, turboprop, turbojet, and reciprocating engine platforms. With compliance to multiple TSO certifications and DO-160B environmental specifications, this navigation module is engineered for dependable operation in commercial and specialized aviation environments. Key Features: Integrated Navigation System: Combines multiple avionics navigation functions into one compact module. Primus II SRZ-85X Compatibility: Designed specifically for Honeywell Primus II integrated radio systems. VOR Navigation Support: Provides VHF Omnidirectional Range navigation capability. Localizer and Glideslope Functions: Supports precision instrument landing system operations. Integrated DME Module: Includes Distance Measuring Equipment for accurate range information. Marker Beacon Scanning: Supports marker beacon signal detection and processing. Self-Contained Module Design: Each navigation subsystem is integrated within a dedicated housing. Ribbon Cable Connectivity: Interfaces with cluster modules through reliable ribbon cable connections. Aerospace Environmental Compliance: Meets DO-160B aviation environmental requirements. High Altitude Capability: Supports operation up to 70,000 feet altitude. Wide Temperature Range: Operates from -55°C to +70°C for demanding flight conditions. Multi-Aircraft Compatibility: Suitable for fixed-wing aircraft, helicopters, turboprop, and turbojet platforms. The 7510100-733 delivers the reliability and precision required for aircraft navigation, instrument landing operations, and integrated avionics communication systems.

Brand: Honeywell · Category: Industrial Automation & Electrical

Key features

• Integrated Navigation System: Combines multiple avionics navigation functions into one compact module.
• Primus II SRZ-85X Compatibility: Designed specifically for Honeywell Primus II integrated radio systems.
• VOR Navigation Support: Provides VHF Omnidirectional Range navigation capability.
• Localizer and Glideslope Functions: Supports precision instrument landing system operations.
• Integrated DME Module: Includes Distance Measuring Equipment for accurate range information.
• Marker Beacon Scanning: Supports marker beacon signal detection and processing.
• Self-Contained Module Design: Each navigation subsystem is integrated within a dedicated housing.
• Ribbon Cable Connectivity: Interfaces with cluster modules through reliable ribbon cable connections.
• Aerospace Environmental Compliance: Meets DO-160B aviation environmental requirements.
• High Altitude Capability: Supports operation up to 70,000 feet altitude.
• Wide Temperature Range: Operates from -55°C to +70°C for demanding flight conditions.
• Multi-Aircraft Compatibility: Suitable for fixed-wing aircraft, helicopters, turboprop, and turbojet platforms.

Specifications

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