NSN 5826-01-367-1307

Part Details | RADIO RECEIVER-TRANSMITTER

5826-01-367-1307 A single component capable of performing the functions of a RECEIVER, RADIO; and TRANSMITTER, RADIO.

Alternate Parts: RT1612ARC215(V), RT-1612/ARC-215(V), DAA3372P002107, DAA3372P002-107, 6227846003, 622-7846-003, DAA3372P001613, DAA3372P001-613, 5826-01-367-1307, 01-367-1307, 5826013671307, 013671307

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
58NOV 07, 199201-367-130719506 ( RECEIVER-TRANSMITTER, RADIO )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5826-01-367-1307
Part Number Cage Code Manufacturer
RT-1612/ARC-215(V)80058JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM
DAA3372P002-1071W025NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE
622-7846-00313499ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS
DAA3372P001-61313499ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS
Technical Data | NSN 5826-01-367-1307
Characteristic Specifications
ELECTRICAL POWER SOURCE RELATIONSHIP OPERATING
AC VOLTAGE RATINGV115.0
FREQUENCY RATINGE400.0
PHASEC
DC VOLTAGE RATINGV28.0
INTERNAL BATTERY ACCOMMODATIONC
OVERALL WIDTH15.290 INCHES NOMINAL
OVERALL DEPTH15.090 INCHES NOMINAL
OVERALL HEIGHT7.870 INCHES NOMINAL
JOINT ELECTRONICS TYPE DESIGNATION SYSTEM ITEM NAMERECEIVER-TRANSMITTER,RADIO
JOINT ELECTRONICS TYPE DESIGNATION SYSTEM ITEM TYPE NUMBERRT-1612/ARC-215(V)
TRANSMITTER EMISSION TYPE A3
POWER OUTPUT2.000 WATTS MINIMUM AND 50.000 WATTS MAXIMUM
OUTPUT FREQUENCY RATING118.000 MEGAHERTZ MINIMUM AND 399.975 MEGAHERTZ MAXIMUM
TRANSMITTER BAND QUANTITY2
TRANSMITTER CHANNEL QUANTITY851
RECEIVER EMISSION TYPE A3
INPUT FREQUENCY RATING108.000 MEGAHERTZ MINIMUM AND 399.975 MEGAHERTZ MAXIMUM
RECEIVER BAND QUANTITY2
RECEIVER CHANNEL QUANTITY891
SPECIAL FEATURESELECTROSTATIC DISCHARGE SENSITIVE; HAS HAVE QUICK COMPATABILITY IN UHF BAND; MONITORS BOTH VHF & UHF GUARD CHANNELS; HAS VOICE AND CRYPTO MODES
CRITICALITY CODE JUSTIFICATIONAFEAT$$ANHCF
NUCLEAR HARDNESS CRITICAL FEATURE HARDENED
END ITEM IDENTIFICATIONPACER SPECIAL
INSTALLATION DESIGN AIRBORNE
VEHICLE FOR WHICH DESIGNED AIRCRAFT