| MRC |
Requirement Statement |
Characteristics |
| AZDC |
DISTANCE FROM LOOP CENTER TO TONGUE END |
1.620 INCHES MINIMUM AND 1.710 INCHES MAXIMUM |
| AKZC |
CENTER TO CENTER DISTANCE BETWEEN FIRST AND SECOND HOLES |
0.615 INCHES MINIMUM AND 0.635 INCHES MAXIMUM |
| AZCY |
CENTER TO CENTER DISTANCE BETWEEN LOOP AND MOUNTING HOLE |
1.380 INCHES MINIMUM AND 1.450 INCHES MAXIMUM |
| ABMZ |
DIAMETER |
0.213 INCHES MINIMUM AND 0.224 INCHES MAXIMUM |
| AGAV |
END ITEM IDENTIFICATION |
W/S:AIRCRAFT, GALAXY C-5 ENGINE, AIRCRAFT, TF39-GE-1 (C5A) SUPPORT EQUIPMENT, C-5 AIRCRAFT |
| ABPX |
MATERIAL THICKNESS |
0.050 INCHES NOMINAL |
| MATT |
MATERIAL |
STEEL COMP 321 BAND |
| BZTN |
LOOP INSIDE DIAMETER |
0.625 INCHES NOMINAL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5510 ASSN STD SINGLE MATERIAL RESPONSE BAND |
| ABMK |
OVERALL WIDTH |
0.500 INCHES NOMINAL |
| AAAL |
TONGUE HOLE TYPE |
ROUND, UNTHREADED |
| STYL |
STYLE DESIGNATOR |
SINGLE LOOP |
