MATERIAL | COPPER ALLOY 172 OR |
| COPPER ALLOY 173 OVERALL |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-C-530,COND H FED SPEC ALL MATERIAL RESPONSES OVERALL |
SURFACE TREATMENT | CADMIUM OVERALL |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | ,FSCM 36659 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
STYLE DESIGNATOR | SOLID, EXTERNAL FLANGE ONE END |
OVERALL LENGTH | 0.8230 INCHES MINIMUM AND |
| 0.8530 INCHES MAXIMUM |
BODY OUTSIDE DIAMETER | 1.4400 INCHES NOMINAL |
BODY INSIDE DIAMETER | 1.2200 INCHES NOMINAL |
FLANGE OUTSIDE DIAMETER | 1.6200 INCHES NOMINAL |
FLANGE WIDTH | 0.0530 INCHES MINIMUM AND |
| 0.0630 INCHES MAXIMUM |
CORNER SHAPE | SQUARE ALL CORNERS |
ANTIROTATION/LUBRICATION TYPE AND QUANTITY | 8 HOLE |
HOLE DIAMETER | 0.0690 INCHES MINIMUM AND |
| 0.0740 INCHES MAXIMUM FIRST |
SURFACE FINISH | 125.0 MICROINCHES OVERALL |
LUBRICANT ACCOMMODATION STYLE | GROOVED CIRCULAR AND |
| GROOVED CLOSED BOTH ENDS |
SURFACE GROOVE LOCATION AND QUANTITY | 2 INTERNAL AND |
| 1 EXTERNAL AND |
| 4 EXTERNAL |
SPECIAL FEATURES | THIS ITEM IS CRITICAL TO THE FUNCTION OF THE C-5 LANDING GEAR. ALL SPECIFIC ACTIONS, DIMENSIONS AND TOLERANCES PERTAINING TO THIS ITEM MUST BE MET TO ENSURE PROPER FUNCTION OF THIS ITEM AND THE LANDING GEAR. ESA REQUIRES STRICT OVERSIGHT TO ENSURE THAT ALL TECH REQUIRMENTS ARE CURRENT |
CRITICALITY CODE JUSTIFICATION | ABHP AND |
| ADAR AND |
| ADAS |
THE MANUFACTURERS DATA | |
MANUFACTURERS CODE | 98897 |
DESIGN CONTROL REFERENCE | 4G13005-123A |