| MRC |
Requirement Statement |
Characteristics |
| AMDX |
FIRST END HOLE DIAMETER |
3.200 INCHES NOMINAL |
| CKSD |
DESIGN CHARACTERISTICS |
SINGLE ACTING SINGLE CYLINDER |
| AGAV |
III END ITEM IDENTIFICATION |
VOUGHT CORPORATION AIRCRAFT,MODEL F-8A,HYDRAULIC SYSTEM |
| AMQZ |
COMPRESSED LENGTH |
4.270 INCHES NOMINAL |
| SR-5 |
THE MANUFACTURERS DATA |
|
| ABXV |
BORE DIAMETER |
0.250 INCHES NOMINAL |
| CLLN |
(NON-CORE DATA) FIRST PISTON ROD END LUBRICATION FACILITY |
NOT INCLUDED |
| AAHB |
FIRST END OUTSIDE DIAMETER |
4.580 INCHES NOMINAL |
| AMPC |
FIRST END THICKNESS AT MOUNTING HOLES |
ANY ACCEPTABLE |
| CKRM |
INTEGRAL VALVE OPERATION METHOD |
HYDRAULIC |
| AAFZ |
BODY MATERIAL |
ALUMINUM ALLOY, QQ-A-225/6, ALLOY 2024 |
| CLLZ |
(NON-CORE DATA) SECOND PISTON ROD END LUBRICATION FACILITY |
NOT INCLUDED |
| ATEM |
EXTENDED LENGTH |
ANY ACCEPTABLE |
| SR-5 |
MANUFACTURERS CODE |
99215 |
| CKSF |
FIRST PISTON ROD END STYLE |
RING TYPE |
| SR-5 |
DESIGN CONTROL REFERENCE |
CV15-601699-2 |
