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AN/ARN-147(V) VOR/ILS/GS/MB Receiver

Please view part numbers below under the "Typical System" tab.

Overview

The AN/ARN-147(V) system from Rockwell Collins combines all VHF Omni Ranging/Instrument Landing System (VOR/ILS) functions into one compact, lightweight, low-cost set. And, it’s the first militarized VHF navigation receiver to give you optional internal MIL-STD-1553B capability. The solid-state system is MIL-E-5400 class II qualified and meets international operability requirements by providing 50-kHz channel spacing for 160-VOR and 40-localizer/glideslope channels.

Digital and analog outputs of the AN/ARN-147 ensure compatibility with high-performance flight control systems and both digital and analog instruments. FM immunity per International Civil Aviation Organization (ICAO) Annex 10 is available with 622-6376-014, -015, -019 and -020, or as an upgrade for 622-6376-004, -005, -009 and -010.

Modular construction techniques give you quick access to all cards and modules to reduce repair time. In addition, part numbers 622-6376-019 and -020 provide unique analog deviation outputs for use in rotary-wing aircraft that use analog Command Instrument Systems processors.

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VOR/ILS/GS/MB Receiver (0.19Mb PDF)

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Features & Benefits
Specifications
Typical System
Related Documents
Training
Services & Support

Key Features & Benefits

  • Choose from analog or analog/digital receiver versions
  • Upgrade the analog version to MIL-STD-1553B with the addition of a single, field-installable circuit card
  • MIL-STD-1553B version retains analog interfaces, plus provides digital input/output functions
  • Qualifies to military specifications
  • Lightweight: 10.1 lb (4.6 kg) maximum for receiver, control and mount
  • Features low power consumption (45 watts)
  • Offers FM broadcast immunity to meet ICAO Annex 10 requirement (factory-ready or retrofit kits)
  • 7,700-hour mean time between failure predicted per MIL-HDBK-217, inhabited transport at 35°C
  • Provides helicopter rotor modulation suppression (connector selectable)
  • High- and low-level deviation and flag outputs
  • Solid state design
  • 160-channel VOR, 40-channel ILS
  • Features improved synchro instrument driver
Make a selection:
Performance
Physical Specs
Power
Environmental
Certificates

MTBF 

Airborne Inhabited Cargo

7,700 hours @ 35 degrees C

Airborne Rotary Wing

2,100 hours @ 55 degrees C

VOR/LOC Receiver

Frequency Range

108.00 – 117.95MHz

Frequency Control

MIL-STD-1553B or ARINC 2-out-of-5

VOR Channels

160

LOC Channels

40

Glideslope Receiver

Frequency Range

329.15 to 335.00MHz

Frequency Control

MIL-STD-1553B or ARINC 2-out-of-5 (paired with localizer channels)

Channels

40 with 150 kHz spacing

Marker Beacon Receiver

Frequency

75 MHz

Sensitivity

High: 200 to 1,000 V. (adjustable)
Low: 1,000 to 4,000 V. (adjustable)

Lamp Outputs

3 lamps output, +28 V dc lamp load, 340 mA maximum, strappable for single lamp

Audio Output

Not less than 100 mW into 150 ohm load, at 10 times lamp threshold

Name

 

Width*

 

Height*

 

Depth*

 

Weight

 

Receiver

 

104.6 (4.12)

 

127.3 (5.01)

 

338.6 (13.33)

 

3.6 kg (8.0 lb)**

 

Control

 

146.1 (5.75)

 

66.8 (2.63)

 

142.0 (5.59)

 

0.7 kg (1.5 lb)

 

Mount

 

110.7 (4.36)

 

50.8 (2.00)

 

353.1 (13.90)

 

0.27 kg (0.6 lb)

 

Note(s):

*Millimeters (inches)
**Weight with MIL-STD-1553 interface card

DC Power Requirements         

+28 VDC nominal per MIL-STD-704A, Notices 1, 2, and 3

DC Power Dissipation

A.  NON-1553 (622-6376-014) system; 20 watts DC maximum
B. 1553 MUX BUS (622-6376-015) system; 25 watts DC maximum

AC Power Requirements         

+26 VAC 400 Hz nominal per MIL-STD-704A, Notices 1, 2, and 3

AC Power Dissipation

Only necessary if RMI synchro driver function is utilized; 20 watts AC maximum

Temperature/Altitude

-54° C to +71° C up to 70,000 feet

Sand and Dust

MIL-E-5400T, Paragraph 3.2.24.7

Humidity

MIL-E-5400T, Paragraphs 3.2.17 and 3.2.24.4
(85% to 95% , +30°C to +65°C, 10 Days)

Salt Atmosphere

MIL-E-5400T, Paragraph 3.2.24.9

Explosive Atmosphere

MIL-E-5400T, Paragraph 3.2.24.10

Fungus

MIL-E-5400T, Paragraph 3.2.24.8

Operational Shock

15 G’s, 11 milliseconds duration, 6 shocks per axis

Crash Safety Shock

30 G’s, 11 milliseconds duration, 6 shocks per axis

Vibration

MIL-STD-810C, Method 514.2, Procedure 1A

Gunfire Vibration

MIL-STD-810C, Method 514.2, Procedure 1A

Environmental

MIL-E-5440 Class 2 and MIL-STD-810

Electromagnetic Interference

MIL-STD-461/462

FM Broadcast Immunity

RTCA/DO-195 and RTCA/DO-196 per ICAO Annex 10

MTBF 

Airborne Inhabited Cargo

7,700 hours @ 35 degrees C

Airborne Rotary Wing

2,100 hours @ 55 degrees C

VOR/LOC Receiver

Frequency Range

108.00 – 117.95MHz

Frequency Control

MIL-STD-1553B or ARINC 2-out-of-5

VOR Channels

160

LOC Channels

40

Glideslope Receiver

Frequency Range

329.15 to 335.00MHz

Frequency Control

MIL-STD-1553B or ARINC 2-out-of-5 (paired with localizer channels)

Channels

40 with 150 kHz spacing

Marker Beacon Receiver

Frequency

75 MHz

Sensitivity

High: 200 to 1,000 V. (adjustable)
Low: 1,000 to 4,000 V. (adjustable)

Lamp Outputs

3 lamps output, +28 V dc lamp load, 340 mA maximum, strappable for single lamp

Audio Output

Not less than 100 mW into 150 ohm load, at 10 times lamp threshold

Name

 

Width*

 

Height*

 

Depth*

 

Weight

 

Receiver

 

104.6 (4.12)

 

127.3 (5.01)

 

338.6 (13.33)

 

3.6 kg (8.0 lb)**

 

Control

 

146.1 (5.75)

 

66.8 (2.63)

 

142.0 (5.59)

 

0.7 kg (1.5 lb)

 

Mount

 

110.7 (4.36)

 

50.8 (2.00)

 

353.1 (13.90)

 

0.27 kg (0.6 lb)

 

Note(s):

*Millimeters (inches)
**Weight with MIL-STD-1553 interface card

DC Power Requirements         

+28 VDC nominal per MIL-STD-704A, Notices 1, 2, and 3

DC Power Dissipation

A.  NON-1553 (622-6376-014) system; 20 watts DC maximum
B. 1553 MUX BUS (622-6376-015) system; 25 watts DC maximum

AC Power Requirements         

+26 VAC 400 Hz nominal per MIL-STD-704A, Notices 1, 2, and 3

AC Power Dissipation

Only necessary if RMI synchro driver function is utilized; 20 watts AC maximum

Temperature/Altitude

-54° C to +71° C up to 70,000 feet

Sand and Dust

MIL-E-5400T, Paragraph 3.2.24.7

Humidity

MIL-E-5400T, Paragraphs 3.2.17 and 3.2.24.4
(85% to 95% , +30°C to +65°C, 10 Days)

Salt Atmosphere

MIL-E-5400T, Paragraph 3.2.24.9

Explosive Atmosphere

MIL-E-5400T, Paragraph 3.2.24.10

Fungus

MIL-E-5400T, Paragraph 3.2.24.8

Operational Shock

15 G’s, 11 milliseconds duration, 6 shocks per axis

Crash Safety Shock

30 G’s, 11 milliseconds duration, 6 shocks per axis

Vibration

MIL-STD-810C, Method 514.2, Procedure 1A

Gunfire Vibration

MIL-STD-810C, Method 514.2, Procedure 1A

Environmental

MIL-E-5440 Class 2 and MIL-STD-810

Electromagnetic Interference

MIL-STD-461/462

FM Broadcast Immunity

RTCA/DO-195 and RTCA/DO-196 per ICAO Annex 10

Make a selection:
Main Components
Part Numbers

Name

 

Type Number

 

Part Number

 

Receiver

 

R-XXXX(V)/ARN-147(V)

 

622-6376-01X*

 

Control

 

313N-6C

 

522-4408-XXX

 

Mount

 

MT-6313

 

622-6380-001

 

 

Note(s):

* Versions above -010 include FM Immunity

Receivers, Mounts and Controls

Type Number

Description

Part Number/ (NSN)

VIR-130A

VOR/ILS/GS/MB Receiver with analog instrumentation outputs only. Upgradeable to 1553B. Requires 28 V dc input power. RMI Driver Operation requires 26 V ac input power. Compatible with FM immunity requirements of ICAO Annex 10.

622-6376-014 (5826-01-467-6216)  

 

VIR-130A

VOR/ILS/GS/MB Receiver with analog instrumentation outputs and 1553B compatible. Requires 28 V dc input power. RMI Driver Operation requires 26-V ac input power. Compatible with the FM immunity requirements of ICAO Annex 10.

622-6376-015 (5826-01-467-6215) 

 

VIR-130A

VOR/ILS/GS/MB Receiver provides unique analog deviation outputs for use in Blackhawk helicopter applications. Upgradeable to 1553B. Requires 28 V dc input power. RMI Driver Operation requires 26 V ac input power. Compatible with the FM immunity requirements of ICAO Annex 10.

622-6376-019

R-2594/ARN-147

VOR/ILS/GS/MB Receiver provides unique analog deviation outputs for use in Blackhawk helicopter applications. Contains MIL-STD-1553B interface. Requires 28 V dc input power. RMI Driver Operation requires 26 V ac input power. Compatible with the FM immunity requirements of ICAO Annex 10.

622-6376-020 (5826-01-444-0314) 

 

NTN

Kit, upgrade AN/ARN-147 to 1553B consists of terminal circuit card, hardware and nameplate.

628-4552-001

NTN

Kit, upgrade 622-6376-004, -005, -009, and -010 to be compatible with FM immunity requirements of ICAO Annex 10. ARN-147 Service Bulletin A upgrades these receivers to -014, -015, -019 and -020, respectively.

988-5470-001

NTN

Kit, upgrade ARN-514 VOR/ILS receiver 622-6095- 001 to 622-6095- 002 for compatibility with FM immunity requirements of ICAO Annex 10.

988-5470-002

MT-2594

Retrofit mount for replacing ARN-123 with ARN-147

822-1479-001 (5975-01-465-1268)

MT-6313

Receiver mounting tray for solid mount

622-6380-001 (5975-01-235-5111)

313N-6C

VOR/ILS/GS/MB Control. 28-volt red lighting.

522-4408-005 (5826-01-475-8308)

C-11423

VOR/ILS/GS/MB Control. 5-volt blue-white lighting.

522-4408-010 (5826-01-198-1505)

 

313N-6C

VOR/ILS/GS/MB Control. 5-volt red lighting. Includes toggle switch for MB sensitivity (Hi-Low) and On/Off/Test toggle switch

522-4408-012 (5826-01-279-8177)

 

C-12550

VOR/ILS/GS/MB Control. 5-volts NVG compatible lighting.

522-4408-013 (5826-01-444-0317)

C-5302

VOR/ILS/GS/MB Control. 28-volt white lighting.

522-4408-207 (5826-01-376-4320)

Mating Connectors for Analog Receiver and Control

Name

Type Number

Part Number

Connector Kit consisting of:

NTN

986-4090-002

J1-Connector

MS3476W24-61S

359-7504-160

J1-Strain Relief

M85049/52-1-24W

359-0029-020

J2-Connector

M39012/16-0101

357-9292-000

J3-Connector

TED-4-10-107

357-7279-080

J4-Connector

TED-4-10-102

357-7279-090

313N-6C CONTROL 

Connector Kit consisting of:

NTN

986-4092-002

J1-Connector

MS3476W20-41S

359-7504-150

J1-Strain Relief

M85049/52-1-20W

359-0029-010

Mating Connectors for MIL-STD-1553B Receiver

Name

Type Number

Part Number

Connector Kit consisting of:

NTN

986-4091-002

J1-Connector

MS3476W24-61S

359-7504-160

J1-Strain Relief

M85049/52-1-24W

359-0029-020

J2-Connector

M39012/16-0101

357-9292-000

J3-Connector

TED-4-10-107

357-7279-080

J4-Connector

TED-4-10-102

357-7279-090

J5-Connector

MS27484T12F-35S

359-0645-030

J5-Strain Relief

M85049/49-2-12N

359-0125-120

Name

 

Type Number

 

Part Number

 

Receiver

 

R-XXXX(V)/ARN-147(V)

 

622-6376-01X*

 

Control

 

313N-6C

 

522-4408-XXX

 

Mount

 

MT-6313

 

622-6380-001

 

 

Note(s):

* Versions above -010 include FM Immunity

Receivers, Mounts and Controls

Type Number

Description

Part Number/ (NSN)

VIR-130A

VOR/ILS/GS/MB Receiver with analog instrumentation outputs only. Upgradeable to 1553B. Requires 28 V dc input power. RMI Driver Operation requires 26 V ac input power. Compatible with FM immunity requirements of ICAO Annex 10.

622-6376-014 (5826-01-467-6216)  

 

VIR-130A

VOR/ILS/GS/MB Receiver with analog instrumentation outputs and 1553B compatible. Requires 28 V dc input power. RMI Driver Operation requires 26-V ac input power. Compatible with the FM immunity requirements of ICAO Annex 10.

622-6376-015 (5826-01-467-6215) 

 

VIR-130A

VOR/ILS/GS/MB Receiver provides unique analog deviation outputs for use in Blackhawk helicopter applications. Upgradeable to 1553B. Requires 28 V dc input power. RMI Driver Operation requires 26 V ac input power. Compatible with the FM immunity requirements of ICAO Annex 10.

622-6376-019

R-2594/ARN-147

VOR/ILS/GS/MB Receiver provides unique analog deviation outputs for use in Blackhawk helicopter applications. Contains MIL-STD-1553B interface. Requires 28 V dc input power. RMI Driver Operation requires 26 V ac input power. Compatible with the FM immunity requirements of ICAO Annex 10.

622-6376-020 (5826-01-444-0314) 

 

NTN

Kit, upgrade AN/ARN-147 to 1553B consists of terminal circuit card, hardware and nameplate.

628-4552-001

NTN

Kit, upgrade 622-6376-004, -005, -009, and -010 to be compatible with FM immunity requirements of ICAO Annex 10. ARN-147 Service Bulletin A upgrades these receivers to -014, -015, -019 and -020, respectively.

988-5470-001

NTN

Kit, upgrade ARN-514 VOR/ILS receiver 622-6095- 001 to 622-6095- 002 for compatibility with FM immunity requirements of ICAO Annex 10.

988-5470-002

MT-2594

Retrofit mount for replacing ARN-123 with ARN-147

822-1479-001 (5975-01-465-1268)

MT-6313

Receiver mounting tray for solid mount

622-6380-001 (5975-01-235-5111)

313N-6C

VOR/ILS/GS/MB Control. 28-volt red lighting.

522-4408-005 (5826-01-475-8308)

C-11423

VOR/ILS/GS/MB Control. 5-volt blue-white lighting.

522-4408-010 (5826-01-198-1505)

 

313N-6C

VOR/ILS/GS/MB Control. 5-volt red lighting. Includes toggle switch for MB sensitivity (Hi-Low) and On/Off/Test toggle switch

522-4408-012 (5826-01-279-8177)

 

C-12550

VOR/ILS/GS/MB Control. 5-volts NVG compatible lighting.

522-4408-013 (5826-01-444-0317)

C-5302

VOR/ILS/GS/MB Control. 28-volt white lighting.

522-4408-207 (5826-01-376-4320)

Mating Connectors for Analog Receiver and Control

Name

Type Number

Part Number

Connector Kit consisting of:

NTN

986-4090-002

J1-Connector

MS3476W24-61S

359-7504-160

J1-Strain Relief

M85049/52-1-24W

359-0029-020

J2-Connector

M39012/16-0101

357-9292-000

J3-Connector

TED-4-10-107

357-7279-080

J4-Connector

TED-4-10-102

357-7279-090

313N-6C CONTROL 

Connector Kit consisting of:

NTN

986-4092-002

J1-Connector

MS3476W20-41S

359-7504-150

J1-Strain Relief

M85049/52-1-20W

359-0029-010

Mating Connectors for MIL-STD-1553B Receiver

Name

Type Number

Part Number

Connector Kit consisting of:

NTN

986-4091-002

J1-Connector

MS3476W24-61S

359-7504-160

J1-Strain Relief

M85049/52-1-24W

359-0029-020

J2-Connector

M39012/16-0101

357-9292-000

J3-Connector

TED-4-10-107

357-7279-080

J4-Connector

TED-4-10-102

357-7279-090

J5-Connector

MS27484T12F-35S

359-0645-030

J5-Strain Relief

M85049/49-2-12N

359-0125-120

Make a selection:
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