NSN 1560-01-718-1969 · NIIN 017181969 · FSC 1560
NO DASHES 1560017181969
In Stock
STIFFENER,AIRCRAFT
Airframe Structural Components
Application: V-22 AIRCRAFT
Technical characteristics
8 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 |
|---|---|---|
| BWJF | SIDE FOR WHICH DESIGNED | RIGHT SIDE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | STIFFENER |
| CZDJ | AIRCRAFT LOCATION | MID-PANEL AFT |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| FEAT | SPECIAL FEATURES | MATERIAL:FABRIC WOVEN,BMI RESIN IMPREGNATED,CARBON FIBER,TYPE 40,CLASS 3,(375 DEGREES CURE)PER BHTI 299-947-336(NOMINAL CURED PLY THICK .0082 PLUS/MINUS .0006);NHA C-00922; |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | V-22 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 1.100 |
| AGAV | END ITEM IDENTIFICATION | V-22 AIRCRAFT |