NSN 5340-01-066-7130 · NIIN 010667130 · FSC 5340
NO DASHES 5340010667130
In Stock
BRACKET,ANGLE
Hardware, Commercial
Application: W/S:ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D)
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 |
|---|---|---|
| ACHY | MOUNTING HOLE TYPE | COUNTERBORED |
| ADLL | SECOND LEG LENGTH | INCHES NOMINAL 1.105 |
| AGAV | END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D) |
| AHLF | SECOND LEG WIDTH | INCHES NOMINAL 1.881 |
| AHLK | FIRST LEG HOLE DIAMETER | INCHES NOMINAL 0.221 |
| AHLN | SECOND LEG HOLE DIAMETER | INCHES NOMINAL 0.281 |
| AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | INCHES NOMINAL 1.381 |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | INCHES NOMINAL 0.250 |
| AHPW | FIRST LEG THICKNESS | INCHES MINIMUM 0.045 AND INCHES MAXIMUM 0.055 |
| AHPX | SECOND LEG THICKNESS | INCHES NOMINAL 0.050 |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | DEGREES NOMINAL 90.0 |
| MATT | MATERIAL | TITANIUM ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASSN STD SINGLE MATERIAL RESPONSE A-S 4911 |
| STYL | STYLE DESIGNATOR |