You have reached this page because of your interest in the Gyroscope Displacement NSN parts we have available on NSN Domain. Here, you can submit a quote request for Ge Aviation Systems Ltd part number 153003-03-01, a component that can be located by searching for NSN 6615-01-326-4636 in our database. Apart from part number 153003-03-01, we also have an array of others, including military, defense, and aerospace parts that have been sourced from a wide range of trusted manufacturers on our Approved Vendor List (AVL). With this in mind, we invite you to explore our ever-expanding catalogs for in-demand items according to manufacturer, NSN, NIIN, and more.
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NSN Domain works with numerous government and defense agencies, so we take advantage of CAGE Codes like 35351 to uniquely identify items in a standardized manner. Moreover, we organize our stock according to various Federal Supply Classes (FSC), ensuring customers can find Ge Aviation Systems Ltd part number 153003-03-01, which can be found under the FSC 6615 Automatic Pilot Mechanisms and Airborne Gyro Components with ease. On that note, please complete the form below for NSN 6615-01-326-4636 and/or any others so we can see how we can find a solution to your needs. For a hands-on approach, call or email us at any time; our experts are on standby 24/7x365!
MRC | Criteria | Characteristic |
---|---|---|
ELEC | Voltage In Volts | 115.0 OR 28.0 |
ACUT | Direct Current Rating In Amps | 2 |
BBWD | Wheel Power Method | ELECTRIC |
BBWG | Gimbal Quantity | 2 |
BBWK | Torqued Gimbal Quantity | 2 |
BBWM | Temp Control Method | EXTERNALLY APPLIED |
BBWH | Axis Displacement Limitation In Deg | 360 DEGREE ROLL AND +82 DEGREE PITCH |
BBWJ | Gimbal Torque Application Method | SYNCHRO MOTOR |
BBWN | Instrument Type | UNFLOATED |
ABMK | Overall Width | 6.250 INCHES NOMINAL |
ABKW | Overall Height | 6.500 INCHES NOMINAL |
FAAZ | Phase | SINGLE/THREE |
FEAT | Special Features | HERMATICLY SEALED CASE, PROVISIONED FOR ROLL AND PITCH, DRIFT WILL NOT EXCEED .25 PER MINUTE AT ROOM TEMPERATURE AND .5 AT TEMPERATURE EXTREMES, SEPARATE BASE, DEVELOPS ELECTRICAL SIGNALS REPRESENTING ROLL AND PITCH FOR USE BY THE ATTITUDE INDICATORS AND NAVIGATIONAL EQUIPMENT, REPLACES THE MD-1 AND PB-60 AUTOPILOT GYRO EHEN THE RESPECTIVE BASES ARE USED |
APGF | Design Type | CAGEABLE |
BBWF | Freedom Axis Quantity | 2 |
BBWL | Sensing Output/Signal Level Method | STANDARD SYNCHRO |
MRC | Decoded Requirement | Clear Text Reply |
ACDC | Current Type | AC AND DC |
APQB | Unit Type | DIRECTIONAL |
AGBC | Shock Mount | PROVIDED |
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