7510100-731 | Honeywell Primus II RNZ-85X Integrated Navigation Unit

Honeywell · Industrial Automation & Electrical

7510100-731 | Honeywell Primus II RNZ-85X Integrated Navigation Unit

Description  The Honeywell 7510100-731 is an Integrated Navigation Unit designed for the Primus II RNZ-85X Integrated Radio System. It combines VOR, localizer, glideslope, marker beacon, Distance Measuring Equipment (DME), and Automatic Direction Finder (ADF) functionality within a self-contained modular assembly. The 7510100-731 provides reliable navigation data and digital outputs for fixed-wing and rotorcraft avionics applications.   Technical Specifications  Condition New/Never Used Surplus Brand Honeywell Category Avionics Part Number 7510100-731 Subcategory Integrated Navigation Unit System Compatibility Primus II RNZ-85X Integrated Radio System Supply Voltage 28 VDC Additional Power Input 26 V, 400 Hz (depending on load) Nominal Power Consumption 69 W Dimensions 14.01" L × 8.90" W × 3.38" H Weight 13.6 lbs Operating Temperature -55°C to +70°C Maximum Altitude 70,000 ft DME Frequency Range 1025–1150 MHz (Tx), 962–1213 MHz (Rx) VOR Frequency Range 108.00–117.95 MHz Localizer Frequency Range 108.10–111.95 MHz Glideslope Frequency Range 329.15–335.00 MHz ADF Frequency Range 100.0–1799.5 kHz Data Interfaces RS-422, ARINC 568, RSB TSO Approvals C34d, C35d, C36d, C40b, C41d, C66b     Information About 7510100-731 The 7510100-731 Integrated Navigation Unit consists of multiple modules housed in a single chassis, including the NV-850 NAV Receiver, DM-850 DME Interrogator, DF-850 ADF Receiver, and XN-850 NAV Cluster Module. Each module connects through ribbon cabling and interfaces via the Radio System Bus (RSB) and RS-422 digital outputs. Operating on 28 VDC with additional 26 V, 400 Hz inputs depending on synchro load, the unit meets multiple TSO standards and DO-160B environmental requirements. It is designed for aircraft installation up to 70,000 feet with wide temperature tolerance from -55°C to +70°C. Key Features: Integrated Navigation System: Combines VOR, ILS (LOC/GS), Marker Beacon, DME, and ADF functions. Modular Architecture: Includes NV-850, DM-850, DF-850, and XN-850 modules within one housing. TSO Certified: Meets TSO C34d, C35d, C36d, C40b, C41d, and C66b requirements. High-Accuracy DME: Digital range accuracy of ±0.05 nmi ±0.1% of range. Wide Operating Envelope: Certified to 70,000 ft altitude and -55°C to +70°C. Digital & Analog Outputs: Supports RS-422, ARINC 568, synchro, and composite analog outputs. Robust Environmental Rating: Qualified to DO-160B environmental standards. Aircraft Mounting Options: Compatible with P/N 7510124-910 or 7510124-911 mounting hardware. The 7510100-731 delivers the reliability and precision required for integrated aircraft navigation and avionics systems.

Brand: Honeywell · Category: Industrial Automation & Electrical

Key features

Specifications

Manufacturer part number7510100-731
ConditionNew/Never Used Surplus
BrandHoneywell
CategoryAvionics
Part Number7510100-731
SubcategoryIntegrated Navigation Unit
System CompatibilityPrimus II RNZ-85X Integrated Radio System
Supply Voltage28 VDC
Additional Power Input26 V, 400 Hz (depending on load)
Nominal Power Consumption69 W
Dimensions14.01" L × 8.90" W × 3.38" H
Weight13.6 lbs
Operating Temperature-55°C to +70°C
Maximum Altitude70,000 ft
DME Frequency Range1025–1150 MHz (Tx), 962–1213 MHz (Rx)
VOR Frequency Range108.00–117.95 MHz
Localizer Frequency Range108.10–111.95 MHz
Glideslope Frequency Range329.15–335.00 MHz
ADF Frequency Range100.0–1799.5 kHz
Data InterfacesRS-422, ARINC 568, RSB
TSO ApprovalsC34d, C35d, C36d, C40b, C41d, C66b
Product typeAvionics

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