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

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

Part #: 7510100-733 Manufactured by: Honeywell
$5,699.00
$5,699.00
1 in Stock
Condition: New-Surplus Original Box
Shipping calculated at checkout.
Product Overview
The 7510100-733 is a Honeywell integrated avionics navigation unit developed for Primus II SRZ-85X aircraft radio systems....  Read more
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Product Description P/N: 7510100-733

Description / Specifications

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.

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Description / Specifications

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.

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