| MRC |
Requirement Statement |
Characteristics |
| ABMX |
CENTER HOLE SHAPE STYLE |
ROUND |
| AAGR |
CROSS-SECTIONAL SHAPE STYLE |
RECTANGULAR |
| AAUB |
HOLE DIAMETER |
0.250 INCHES MINIMUM AND 0.261 INCHES MAXIMUM |
| AGAV |
III END ITEM IDENTIFICATION |
B757 AIRCRAFT |
| MATT |
MATERIAL |
IRON ALLOY 660 OVERALL |
| CQBC |
III MINIMUM TENSILE STRENGTH |
140000 POUNDS PER SQUARE INCH |
| CXCY |
III PART NAME ASSIGNED BY CONTROLLING AGENCY |
WASHER, PLAIN |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS5525 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ADAV |
OVERALL DIAMETER |
0.475 INCHES MINIMUM AND 0.495 INCHES MAXIMUM |
| ABMW |
PERIPHERAL SHAPE STYLE |
ROUND |
| FEAT |
SPECIAL FEATURES |
HEAT TREAT TO MINIMUM TENSILE STRENGTH PER AMS-H-6875 SERVICE TEMPERATURE 450.0 DEGREES F USED ON TRANSMISSION INSTALLATION-INBOARD T.E. FLAP DRIVE OUTBOARD (INBOARD T.E. FLAP TRANSMISSIONS ONLY) |
| SFTT |
SURFACE TREATMENT |
CADMIUM OVERALL |
| ABNM |
THICKNESS |
0.012 INCHES MINIMUM AND 0.020 INCHES MAXIMUM |
