We appreciate your interest in Honeywell International Inc part number CN-1689-V-9-ASN, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number CN-1689-V-9-ASN is listed with the NSN 6605-01-426-8522 and description “Inertial Navigation.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Honeywell International Inc under the CAGE Code 0BFA5 or that similarly fall under the FSC 6605 Navigational Instruments, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 6605-01-426-8522 parts and Inertial Navigation items your operations require, so request a quote today.
| MRC | Criteria | Characteristic |
|---|---|---|
| ABFY | OVERALL DEPTH | 9.800 INCHES NOMINAL |
| SUPP | III SUPPLEMENTARY FEATURES | CONTAINS 3 RING LASER GYROS AND 3 ACCELEROMETERS IN A STRAP DOWN CONFIGURATION, EMBEDED GLOBAL POSITIONING SYSTEM RECIEVER |
| ABMK | OVERALL WIDTH | 7.000 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | C/KC-135 AIRCRAFT |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVIGATION UNIT, INERTIAL-SATELITE SIGNALS |
| TMDN | III TYPE/MODEL DESIGNATION | CN-1689(V)9/ASN |
| ACDC | CURRENT TYPE | DC |
| FTLD | III FUNCTIONAL DESCRIPTION | EMBEDDED GPS/INS (EGI) UNIT IS A SELF-CONTAINED ALL-ATTITUDE NAVIGATION LINE REPLACEABLE UNIT PROVIDING OUTPUTS OF ACCELERATION, ATTITUDE (AZIMUTH, PITCH, ROLL), ATTITUDE RATES, HEADING, POSITION, VELOCITY, ASSOCIATED TIME TAG INFORMATION, AND UNIVERSAL TIME COORDINATED (UTC) SYNCHRONIZED TIME VIA EXTERNALLY CONTROLLED MIL-STD-1553B DUAL MULTIPLEX DATA BUS WHICH REQUESTS DATA & TRANSMITS UPDATED DATA BASED UPON THE REQUIREMENTS OF THE INTERFACING AVIONICS SYSETEMS. EGI PROVIDES SIMULTANEOUS INS ONLY, BLENDED GPS/INS & GPS ONLY POSITION SOLUTIONS. |
| ELEC | VOLTAGE IN VOLTS | 28.0 |
| AXGY | MOUNTING METHOD | FIXED FLANGE |
| RTSE | III RELATIONSHIP TO SIMILAR EQUIPMENT | 5 CHANNEL VS 12 CHANNEL P/N 34209200-40H4 |
| ABKW | OVERALL HEIGHT | 7.000 INCHES NOMINAL |
| RDAL | III REFERENCE DATA AND LITERATURE | DD FORM 61 |
| FEAT | SPECIAL FEATURES | 2/3A C-CELL GPS BATTERY INSTALLED;FRONT CONNECTOR PANEL:BUILT IN TEST; ELECTROSTATIC DISCHARGE SENSITIVE |
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