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7510100-731 | Honeywell Primus II RNZ-85X Integrated Navigation Unit
- Regular price
- $4,789.00
- Sale price
- $4,789.00
- Regular price
-
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Product Description P/N: 7510100-731
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.
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.