NSN 1420-01-178-3485 · NIIN 011783485 · FSC 1420
NO DASHES 1420011783485
In Stock
ENGINE INLET ASSEMB
Guided Missile Components
Application: AGM-86B
Technical characteristics
7 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | AGM-86B |
| FTLD | FUNCTIONAL DESCRIPTION | ENGINE INLET FOR SECTION 55 |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| RDAL | REFERENCE DATA AND LITERATURE | 21M-AGM86-4-1 |
| RTSE | RELATIONSHIP TO SIMILAR EQUIPMENT | CONTROLLED REPLACEABLE ASSY 232-31554-1,-5 AND -6 |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CONTAINS HARDNESS CRITICAL COMPONENTS AND PROCESSES; ASSEMBLY INCLUDES CORE HOLE COVER 3; EMI STRIP 2; ANTI-ICE ASSY INLET LIP 1; E.C.S. DUCT 1; ADAPTER RING 1; R.A.M. INLET LIP 2; MACH. INLET ASSY 1; FLEXIBLE DUCT 1; AND ASSOC. HARDWARE |