MRC | Criteria | Characteristic |
---|---|---|
CXCY | Part Name Assigned By Controlling Agency | MANIFOLD,ENGINE FUEL,RH ENG" |
AGAV | End Item Identification | T-38A AIRCRAFT ENGINE |
SUPP | Supplementary Features | FUEL PRESSURE WILL BE 50 PSIG,FLUID TEMPERATURE WILL RANGE FROM -65F TO 110F,AMBIENT TEMPERATURE WILL RANGE FROM -65F TO 200F" |
FEAT | Special Features | NO FLAMMABLE MATERIALS SHALL BE USED. DISSIMILAR METALS SHALL NOT BE USED. METALLIC SURFACES SHALL BE TREATED I/A/W MIL-F-7179 |
FTLD | Functional Description | USED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE |
Warrantied inventory at competitive prices
Search the world's largest inventory of electronic components by manufacturer, category or part number
All inventory ready to ship from our sellers
We sell only warrantied and traceable parts
If You’d Like to Stay Updated On Our Latest Promotions, You Can Download the ASAP Semiconductor App from the App Store and Google Play Store.
Request for Quote