| MRC |
Requirement Statement |
Characteristics |
| BFGX |
SHAFT END THICKNESS |
0.720 INCHES MINIMUM AND 0.800 INCHES MAXIMUM |
| BFGY |
LINK END THICKNESS |
0.500 INCHES NOMINAL |
| SR-5 |
MANUFACTURERS CODE |
0JRC1 |
| ADGE |
BORE LENGTH |
0.690 INCHES NOMINAL |
| MATT |
MATERIAL |
MAGNESIUM ALLOY |
| SR-5 |
THE MANUFACTURERS DATA |
|
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-M-55, COMP AZ91C-T6 FED SPEC SINGLE MATERIAL RESPONSE |
| SR-5 |
DESIGN CONTROL REFERENCE |
2-13468-1 |
| ASBP |
BORE TYPE |
PLAIN STRAIGHT |
| ABXV |
BORE DIAMETER |
1.600 INCHES NOMINAL |
| AGAV |
III END ITEM IDENTIFICATION |
T-6 AIRCRAFT |
| BFHA |
LINK END HOLE DIAMETER |
0.190 INCHES MINIMUM AND 0.194 INCHES MAXIMUM |
| STYL |
STYLE DESIGNATOR |
CLEVIS LINK END, SECURING HOLE(S) SHAFT END |
