NSN 9540-01-329-2168 · NIIN 013292168 · FSC 9540
NO DASHES 9540013292168
In Stock
ANGLE,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: B-1B AIRCRAFT
Technical characteristics
17 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 1.800 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 4.200 |
| ABRY | LENGTH | FEET MINIMUM 10.000 AND FEET MAXIMUM 12.000 |
| ADXL | LEFT SIDE FLANGE THICKNESS | INCHES NOMINAL 0.071 |
| AGAV | END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.125 |
| AJGP | BASE FLANGE THICKNESS | INCHES NOMINAL 0.071 |
| BRFD | WEIGHT PER UNIT MEASURE | POUNDS PER LINEAR FOOT 0.509 |
| CMZY | FIRST TIP STYLE | |
| 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 1ST MATERIAL RESPONSE QQ-A-200 TO 3 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | TEMPER T3511 |