NSN 1560-01-019-2782 · NIIN 010192782 · FSC 1560
NO DASHES 1560010192782
In Stock
PANEL,STRUCTURAL,AIRCRAFT
Airframe Structural Components
Technical characteristics
5 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 |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL ASSEMBLY - UPPER |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | E-3A |
| FEAT | SPECIAL FEATURES | AFTER PRE-FIT, BOND PER BAC5514-580 AND D6-23434; AFTER BONDING, PLUG VENT HOLES IN BEADS AND APPLY ALODINE 1000 TO ENTIRE ASSEMBLY PER BAC5719 CLASS B, METHOD 1 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| SPCL | SPECIAL TEST FEATURES | CONSISTS OF: P/N -7, SKIN - UPPER, .016 X 36.0 X 47.5", FINISH: F-2.10(QTY1);P/N-11 SKIN BEADED STA0-10.26 TO STA 4.44,.016X 15.0 X 38.7", FINISH: F-2.10 (QTY 1); P/N -13, SKIN BEADED STA 4.44 TO STA 25.55, .016 X 21.3 X 37.5", FINISH: F-2.10 (QTY 1);P/N -15, DOUBLER - STA 0.10.26, .032 X 1.6 X 36.5", FINISH: F-2.10 (QTY 1); P/N -16, DOUBLER - STA 4.44, .032 X 3.1, X 35.0, FINISH: F-2.10 (QTY 1); P/N -17, DOUBLER - STA 25.58, .032 X 1.7 X 33.5", FINISH: F-2.10 (QTY 1); P/N -18, DOUBLER, STA 0-10.26 TO STA 25.58, .016 X 5.8 X 36.0", FINISH: F-2.10 (QTY 1); |