NSN 5340-00-856-9078 · NIIN 008569078 · FSC 5340
NO DASHES 5340008569078
In Stock
BRACKET,ANGLE
Hardware, Commercial
Application: W/S: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); AIRCRAFT, C-18A, EC-18B; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B52H); JOINT STARS TARGET RADAR SYSTEM; AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, HERCULES C-130; AIRCRAFT, AWACS, E-3A
Technical characteristics
28 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 |
|---|---|---|
| AKBU | SECOND LEG STYLE | |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | |
| AHPX | SECOND LEG THICKNESS | INCHES NOMINAL 0.059 |
| AHLF | SECOND LEG WIDTH | INCHES NOMINAL 0.625 |
| AHLK | FIRST LEG HOLE DIAMETER | INCHES NOMINAL 0.344 |
| AHPW | FIRST LEG THICKNESS | INCHES NOMINAL 0.059 |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | |
| ADLK | FIRST LEG LENGTH | INCHES NOMINAL 0.926 |
| ADLL | SECOND LEG LENGTH | INCHES NOMINAL 1.129 |
| AGAV | END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); AIRCRAFT, C-18A, EC-18B; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B52H); JOINT STARS TARGET RADAR SYSTEM; AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, HERCULES C-130; AIRCRAFT, AWACS, E-3A |
| AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | INCHES NOMINAL 0.250 |
| AJFP | FIRST LEG END RADIUS | INCHES NOMINAL 0.500 |
| AJFQ | SECOND LEG END RADIUS | INCHES NOMINAL 0.500 |
| AJZU | FIRST LEG STYLE | |
| AHQN | FIRST LEG WIDTH | INCHES NOMINAL 0.625 |
| MATT | MATERIAL | STEEL COMP 410 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED STD SINGLE MATERIAL RESPONSE 66 |
| SFTT | SURFACE TREATMENT | PASSIVATE |
| STYL | STYLE DESIGNATOR | |
| AHLN | SECOND LEG HOLE DIAMETER | INCHES NOMINAL 0.219 |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | INCHES NOMINAL 0.312 |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | INCHES NOMINAL 0.310 |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | INCHES NOMINAL 0.312 |
| ZZZV | FSC APPLICATION DATA | ENGINE,ACFT,TURBO-FAN |
| CSSQ | FIRST LEG ANGLE | DEGREES NOMINAL 75.0 |
| FEAT | SPECIAL FEATURES | THIS PART MEETS THE Y REQUIREMENTS DUE TO CRITICAL FEATURES, TOLERANCES, FIT RESTRICTIONS, MATERIAL PROPERTIES AND MANUFACTURING PROCESS. FAILURE COULD RESULT IN LOSS OR SUBSTANTIAL DAMAGE TO WEAPON SYSTEM, DEATH OR SERIOUS INJURY |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |