Thank you for taking interest in The Boeing Company part number 204-91950-1, which is listed with the NSN 4920-01-018-2408 and a product description of “Adapter Assembly In.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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MRC | Criteria | Characteristic |
---|---|---|
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | TILT TABLE ADAPTER |
AJAF | III UNPACKAGED UNIT LENGTH | 23.000 INCHES NOMINAL |
RDAL | III REFERENCE DATA AND LITERATURE | TO 35-1-251-1 & 1E-3A-2-22-1 |
FTLD | III FUNCTIONAL DESCRIPTION | USED TO MOUNT THE INERTIAL NAVIGATION SYSTEM (INS) UNIT 1 OR 2 ON THE 2TSJ60B00002 TILT TABLE DURING UNSCHEDULED MAINTENANCE FOR FUNCTIONAL TEST AND FAULT ISOLATION OF THE AUTOMATIC FLIGHT CONTROLS. THE TILT TABLE ADAPTER ALSO PROVIDES COOLING AIR FOR THE INS UNIT, WITH PROVISIONS FOR CUTTING POWER IF INADEQUATE COOLING AIR IS BEING PROVIDED |
AJAG | III UNPACKAGED UNIT WIDTH | 19.000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | E-3A AWACS AGE. |
AJAH | III UNPACKAGED UNIT HEIGHT | 9.000 INCHES NOMINAL |
FEAT | SPECIAL FEATURES | INTERCONNECTING CABLES ARE PROVIDED FOR OPERATING THE INS UNIT DURING THE FUNCTIONAL TEST AND FAULT ISOLATION OF THE AUTOMATIC FLIGHT CONTROLS |
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