| MRC |
Requirement Statement |
Characteristics |
| CWPC |
THREAD FORM QUANTITY |
4 |
| CWPP |
PRESSURE ANGLE |
20.0000 DEGREES |
| CWRM |
FACE NOMINAL WIDTH |
1.000 INCHES |
| AGJS |
PITCH DIAMETER |
0.6250 INCHES NOMINAL |
| CWCD |
NOMINAL OUTSIDE DIAMETER |
0.750 INCHES |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-STD-171 MIL STD SINGLE TREATMENT RESPONSE OVERALL |
| AGAV |
III END ITEM IDENTIFICATION |
F-404 ENGINE; F/A-18 HORNET AIRCRAFT |
| STYL |
STYLE DESIGNATOR |
PROTRUDING HUB |
| CWPZ |
HELIX ANGLE |
21.8000 DEGREES |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
ASTM A108 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ABSX |
ATTACHMENT METHOD |
MOUNTING HOLE |
| CWTX |
HUB NOMINAL DIAMETER |
0.460 INCHES FIRST END |
| MATT |
MATERIAL |
STEEL OVERALL |
| CWZK |
MOUNTING HOLE NOMINAL DIAMETER |
0.110 INCHES TRANSVERSELY THROUGH HUB, SECOND END |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| ANTP |
BORE STYLE |
PLAIN BOTH ENDS |
| SFTT |
SURFACE TREATMENT |
CADMIUM OVERALL |
| CWQL |
NOMINAL DISTANCE BETWEEN BODY FACE AND PROTRUDING HUB END |
0.250 INCHES FIRST END |
| FEAT |
SPECIAL FEATURES |
ALTERED DRAWING |
| CTQY |
MOUNTING HOLE TYPE AND QUANTITY |
2 PLAIN TRANSVERSELY THROUGH HUB, SECOND END |
| CWRS |
BORE NOMINAL DIAMETER |
0.258 INCHES BOTH ENDS |
| CWPH |
THREAD FORM DIRECTION |
RIGHT-HAND |
| CWTR |
HUB STYLE DESIGNATOR |
PINNED SECOND END |
| ALPN |
FACE TYPE |
STRAIGHT |
