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| 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 |
| 3.5-13-.1PCB | 3-5-12-39 | 3-5-12-39 | 3-5-116 |
| 3 5 15011 C 05 | 3.5-1600FSCG ITEM6 | 3 5 15011 C 03 | 3.5-15-53 |
| 3.5-150PGE E-N M | 3.5-13-.1PCB | 3 5 15 53 | 3 5 16 |
| 3.5-14-39 | 3.5-14-39 | 3-5-108X | 3-5-12-39 |
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