Aerospace Engineering Solutions is proud to offer immediate purchasing options on Honeywell International Inc part number PMU-69-E, a Pump Unit Test Stat product we carry that is listed with the NSN 4920-01-430-9645 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Honeywell International Inc through the CAGE Code 06848, as well as categorized under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment based on the first four digits of the NSN 4920-01-430-9645. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number PMU-69-E and other NSN items of need.
MRC | Criteria | Characteristic |
---|---|---|
FEAT | SPECIAL FEATURES | THE RANGE OF HYDRAULIC FLUID PRESSURES ARE GREATER FOR THIS PUMP UNIT THAN FOR THE PUMP UNIT, TEST STATION, PMU-64/E (LOW PRESSURE PUMP MODULE) |
AGAV | III END ITEM IDENTIFICATION | AFATS |
RDAL | III REFERENCE DATA AND LITERATURE | SERD NO. 1064 |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | INCLUDES AN OPERATOR INTERFACE WITH A DISPLAY, CONTROL SWITCHES, & A KEYBOARD WHICH WILL ALLOW MANUAL CONTROLOF THE PUMP MODULE IF THE LOCAL COMMUNICATION NETWORK IS INOPERABLE; THE HIGH PRESSURE PUMP MODULE INTERFACES WITHTHE TEST STATIONS VIA DISTRIBUTION PIPING & WILL MODULATE THE OUTPUT BASED ON COMBINED TEST STATION REQUIREMENTS |
FTLD | III FUNCTIONAL DESCRIPTION | USED TO SUPPLY HYDRAULIC FLUID TOTHE TEST STATIONS UNDER VARIOUS FILTERED, MONITORED, & FLOW CONDITIONS TO TEST AIRCRAFT FUEL ACCESSORIES; AN AUTOMATED, FIX INSTALLATION, HYDRAULIC PUMPING UNIT UNDER THE CONTROL OF AN EMBEDDED COMPUTER |
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