If your operations demand part number 34078600-312, an item produced by Honeywell International Inc and listed with the description “Inertial Navigation,” look no further than this page. At your convenience, you can complete the Request for Quote (RFQ) form below with details like your budget, desired quantity, and anticipated fulfillment timeline to receive customized procurement options on part number 34078600-312. Our representatives will happily treat you to competitive pricing and swift lead times upon their receipt and review of a completed form, regularly responding in 15 minutes or less.
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If you are interested, be sure to explore our website further for related CAGE Code 0BFA5 items or other various products manufactured by Honeywell International Inc. We also present a catalog of all related FSC 6605 Navigational Instruments parts that we currently carry for your perusal. Regardless of what you decide to purchase from us, we will work closely with you to provide dependable, authentic products while ensuring that we address every requirement possible. This being said, get started on requesting quotes for part number 34078600-312 and any other NSN parts you need on Sky Forge Components to experience our unrivaled fulfillment services.
MRC | Criteria | Characteristic |
---|---|---|
ABMK | OVERALL WIDTH | 6.750 INCHES NOMINAL |
SR-1 | SPEC/STD CONTROLLING DATA | |
FEAT | SPECIAL FEATURES | RECEIVES 26 V, 400 HZ SINGLE PHASE SYNCHRO REFERENCE POWER; AIRCRAFT 28 VDC DISCRETE POWER EXCLUDING BATTERY BACK UP POWER |
ABKW | OVERALL HEIGHT | 7.625 INCHES NOMINAL |
SUPP | III SUPPLEMENTARY FEATURES | ELECTROSTATIC DISCHARGE SENSITIVE |
ACDC | CURRENT TYPE | DC |
AGAV | III END ITEM IDENTIFICATION | F-16 A TO D MODEL AIRCRAFT |
FREQ | FREQUENCY IN HERTZ | 400.0 |
ABHP | OVERALL LENGTH | 15.187 INCHES NOMINAL |
ELEC | VOLTAGE IN VOLTS | 115.0 AND 200.0 |
SR-1 | NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | SNU 84-1/F16 REV B CH 1 15JUL92 |
SR-1 | MANUFACTURERS CODE | 81349 |
FTLD | III 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 |
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