NSN 9540-01-072-9576 · NIIN 010729576 · FSC 9540
NO DASHES 9540010729576
In Stock
ANGLE,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: F-16 AIRCRAFT
Technical characteristics
21 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 |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 1.200 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 2.750 |
| ABRY | LENGTH | FEET MINIMUM 10.000 AND FEET MAXIMUM 12.000 |
| ADXL | LEFT SIDE FLANGE THICKNESS | INCHES NOMINAL 0.080 |
| AGAV | END ITEM IDENTIFICATION | F-16 AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.125 |
| AJGM | OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.030 |
| AJGP | BASE FLANGE THICKNESS | INCHES NOMINAL 0.080 |
| BRFD | WEIGHT PER UNIT MEASURE | POUNDS PER LINEAR FOOT 0.374 |
| CMZY | FIRST TIP STYLE | |
| CNBD | FIRST TIP INNER RADIUS | INCHES NOMINAL 0.030 |
| CNBJ | FIRST TIP OUTER RADIUS | INCHES NOMINAL 0.030 |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CQHP | LEFT INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE A-S-QQ-A-200 TO 3 |
| ZZZK | SPECIFICATION/STANDARD DATA | MANUFACTURERS STANDARD 81755-K10 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 2024 AND TEMPER T3511 |