| AIRCRAFT MISSION DESIGN SERIES | F18 E/F |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| FURNISHED ITEMS | ADHESIVE |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5581 MIL SPEC SINGLE MATERIAL RESPONSE |
| MATERIAL | NICKEL ALLOY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | DUCT ASSEMBLY - L.H. RIGID, KEEL |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| SPECIAL FEATURES | MATERIAL INCONEL 625; OPERATING PRESSURE 135 PSIG AT 1060 F; MAX OPERATING PRESSURE 515 PSIG AT 1060 F; BURST PRESSURE 773 PSIG AT 1160 F |