NSN 6605-01-319-6483
Part Details | INERTIAL NAVIGATION UNIT
6605-01-319-6483 A self-contained Line Replaceable Unit that provides acceleration, velocity, and position data for land vehicles, watercraft or aircraft. It may also provide altitude information for aircraft. It is part of an INERTIAL NAVIGATION SYSTEM and may contain an INERTIAL REFERENCE UNIT, NAVIGATION.
Alternate Parts: SNU 841F16 REV B CH 1 15JUL92, SNU 84-1/F16 REV B CH 1 15JUL92, CN1674AASN, CN-1674A/ASN, CN1674ASN, CN-1674/ASN, SNU 841F16 REV B CH 1 15JUL92, SNU 84-1/F16 REV B CH 1 15JUL92, 890500201, 890500-201, 8905000201, 890500-0201, 6605-01-319-6483, 01-319-6483, 6605013196483, 013196483
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAY 11, 1990 | 01-319-6483 | 53294 ( INERTIAL NAVIGATION UNIT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6605-01-319-6483
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| SNU 84-1/F16 REV B CH 1 15JUL92 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| CN-1674A/ASN | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
| CN-1674/ASN | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
| SNU 84-1/F16 REV B CH 1 15JUL92 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 890500-201 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| 890500-0201 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
Technical Data | NSN 6605-01-319-6483
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 15.187 INCHES NOMINAL |
| OVERALL WIDTH | 6.750 INCHES NOMINAL |
| OVERALL HEIGHT | 7.625 INCHES NOMINAL |
| CURRENT TYPE | DC |
| VOLTAGE IN VOLTS | B115.0$$B200.0 |
| FREQUENCY IN HERTZ | 400.0 |
| SPECIAL FEATURES | RECEIVES 26 V, 400 HZ SINGLE PHASE SYNCHRO REFERENCE POWER; AIRCRAFT 28 VDC DISCRETE POWER EXCLUDING BATTERY BACK UP POWER AND HAS CRITICAL APPLICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SUPPLEMENTARY FEATURES | ELECTROSTATIC DISCHARGE SENSITIVE |
| FUNCTIONAL DESCRIPTION | CAPABLE OF DETERMINING POSITION, VELOCITY, HEADING, ACCELERATIONS, BODY RATES, AND ATTITUDE IN THE AUTONOMOUS MODE FROM TAKE OFF TO LANDING AFTER A GROUND ALIGNMENT IN THE FOLLOWING MODES: GYROCOMPASS, STORED HEADING, BEST AVAILABLE TRUE HEADING |
| END ITEM IDENTIFICATION | F-16 A TO D MODEL AIRCRAFT |
