This is an Automatic Direction Finding receiver, which covers 100 KHz to 1750 KHz in four bands. The equipment can be used a radio compass or other stations can be monitored to obtain weather reports or it may be used as a communications receiver.

A BFO is used with the equipment in Antenna or Loop operation. A fixed frequency of 455.9 KHz is used for band 1 and 143.4 KHz for bands 2, 3, and 4. A tone oscillator is used when the equipment is used in Compass operation . The tone oscillator is set for 900 Hz and modulates the CW signal as is passes through the IF stages.

Frequency Range:

Band 1    100- 200 kHz    (IF = 465 KHz)
Band 2    200- 410 kHz    (IF = 142.5 KHz)
Band 3    410- 850 kHz    (IF = 142.5 KHz)
Band 4    850-1750 kHz   (IF = 142.5 KHz)

Power Input: 26.5 VDC at 4.0 amps.
Weight: 60 lb for a complete system.
Receiver Dimensions and Weight: 7 5/16H x 11 3/8W x 15 7/16 D ; 34.75 pounds
Manufacturer:  Bendix or Magnavox Company, Ft Wayne, Indiana, USA.
Circa: 1950

AN/ARN-6 principal components. Mounting MT-273/ARN-6  is an aluminum frame with a built in junction board and a control switch relay at the base. MT-274 is identical to MT-273 except that the control relay is not included. This is the mounting for single remote control applications.  Mounting MT-275 is a rectangular shaped aluminum box with an open top into which the control box mounts. (US Navy pictorial via HNSA)

CONTROL BOX

Control Box C-149/ARN-6 is a rectangular shaped aluminum box with the necessary circuit elements and controls for complete control of the radio compass unit. That is the unit depicted in the principal components pictorial. C1514/A below, is the control box which lacks the S-meter. There were at least 3 control panels that were a standard cockpit mounting system (a standardized panel system like the 19 inch rack) and one stand alone control box.

C-1514/A rack mount control panel.  (Courtesy Google books)

Another style of control panel made by Gables. Shown for reference only.  (Photo by John Mackesy VK3XAO)

Radio Compass unit R101/ARN-6 is contained within an aluminum housing with removable top and bottom covers. It is comprised of the compass circuit, a 16 tube superheterodyne receiver, the automatic loop control circuit and the vibrator power supply unit. Tube lineup: 6 x 12SK7, 1 x 12SY7, 1 x 12SW7, 4 x 12SX7GT, 2 x 26A7GT and 2 x 2050.

The vibrator/transformer power supply  produces AC for the 2050 thyratrons and the autosyn loop position transmission and indication system.

This was the actual installation of the AN/ARN-6 receiver in a Canadian Tracker. (Photo by Jerry Proc)

R101/ARN-6 receiver on an MT-273 mount.

Cover off front view.

Cover off - side view.

All photos in this table by John Mackesy VK3XAO

LOOP ANTENNA

Loop antenna AS313/ARN-6 is an iron core loop which is rotated by a drive motor through a reducing gear train. A compensator, which can be adjusted externally, is used to correct for radio compass deviation error. An autosyn transmitter is geared through the compensator to the rotatable loop and supplies loop position information to the remote indicator system. The entire loop unit is sealed and filled with dry nitrogen. It cannot be opened without special equipment. Electrically speaking, the loop antenna uses a low impedance iron core loop of nine turns, is electrically centre-tapped by means of a shut coil of 12 turns and electrostatically shielded. It is directional in that the voltage induced in the loop is maximum when the line of travel of the received radio wave lies in the plane of the loop coil . The resultant voltage induced in the loop is 90 degrees out of phase with the non-directional antenna and leads or lags according to which edge the loop coil is nearer to the signal source.

Sense antenna- The non-directional antenna input circuit of the receiver is designed to operate from a low capacity transmission line connected through the proper matching circuit to a conventional 40 to 1000 picofarad antenna having an effective height of from 0.05 to .5 meter.

Coupling Unit CU-65/ARN-6 provides a female connector for the antenna transmission line and an antenna input terminal.

AS-313/ARN-6 loop antenna without radome. This is a compact servo-operated directional loop aerial sealed into a nitrogen-filled glass-topped housing.  (Antenna photo courtesy BPB Surplus)

AS313/ARN6 in test jig with indicator. (Photo by John Mackesy VK3XAO)

Tracker ARN-6 loop antenna. The duct in the foreground is an air outlet for cooling the avionics equipment. A black/red bar holds the folded wing in place.  (Photo by Jerry Proc)

ARN-6 sense antenna placement on a Canadian Tracker. The inset shows the detail of the feed through method. (Photo by Jerry Proc)

ID-90/ARN-6 is an autosyn driven device which indicates the angular position of the autosyn transmitter located in the loop and gives the bearing of a radio transmitter when the loop is at a true null. It does not have luminescent materials on the pointer and numerals. (3.25 inches square x 5 13/16 inches deep; Weight is 2.1 lbs)

ID-91/ARN-6 is identical to ID90/ARN-6 but it uses luminescent materials on the pointer and numerals. (3.25 inches square x 5 13/16 inches deep; Weight is 2.1 lbs)

ID-92 /ARN-6 is similar to indicator ID90/ARN-6 except that a larger scale is used. The scale is graduated every degree and every 10 degree graduation is indicated by the proper numeral. (3.25 inches square x 5 13/16 inches deep; Weight is 2.1 lbs)

ID231/ARN-6 is identical to indicator ID90/ARN-6 except that the pointer is set at 270 degrees azimuth when the indicator rotor is at its electrical zero position. This indicator is only used in special installations which require the loop to be mounted with its zero heading at 270 degrees.  (5.5 inches square x 6 inches deep; Weight is 3.06 lbs)

This is the ID91B/ARN-6 indicator, one of four types available for the system. (Photo by John Mackesy VK3XAO)

Also available was the dual pointer Type ID-250/ARN indicator. 3-1/8" size . Made by Bendix Aviation Corp.(Photo by John Mackesy VK3XAO)

The Course Indicator (now called Radio Magnetic Indicator or RMI ) ID-250 has 3 synchro motors. One rotates the compass dial card such that the flight direction is on top, Pointer 1 can be connected to the differential synchro from an ID-307 which then points in the direction of the TACAN beacon. Pointer 2 can point to a VHF OmniRange beacon (VOR) or an automatic direction finder (ADF) through a suitable receiver. This was not fitted in the Argus aircraft.

Radio collector Tom Brent indicates that there is yet a third type of control panel, however its part number is not known at this time. AN/ARN-44 is the improved version of the ARN-6. Two receivers in his collection bear the following nameplate data.

DEPT. OF NAT'L DEFENCE - CANADA
RECEIVER, RADIO
R-713/ARN-44
PART NO. R101A(MOD)

A second receiver has the following nameplate data.

CONVERTED BY
PRESENTEY ENGINEERING
PRODUCTS LIMITED
OTTAWA  14/11/68  CANADA

It is believed that the part of the improvements package was providing coverage from  to 2.0 - 3.5 MHz. This is still awaiting confirmation.  The AN/ARN-59 was the successor to the ARN-6.  Many of the Trackers being scrapped at Abbotsford BC airport are fitted with the ARN-44.

MANUAL

AN 16-30/ARN-6 manual. (Courtesy Lostpaper.com)

Back To Tracker Equipment Listing

Credits and References:

1)  ARN-6 antenna:  BPB Surplus
     http://www.bpbsurplus.com/lc/cart.php?target=product&product_id=17071&category_id=341
2) Ian Snow  RCAF/CF retired.<va3qt-4(at)sympatico.ca>
3) John Mackesy VK3XAO  <mack(at)melbpc.org.au>
4) AN/ARN-6 Summary    http://www.hnsa.org/doc/ecat/cat-0033.htm
5) ARN-6 manual photo   http://lostpaper.com/toshop/index.php?main_page=popup_image&pID=5953
6) ARN-6 info    http://www.vk2bv.org/museum/arn6.htm
7) ARN-6 info    http://mcgp.cellmail.com/database/back%20mail/Backmails/MCGP%20Backmail%2037.htm
8) Tom  Brent <tgb@telus.net>

 
Feb 25/09