| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
J-57 AIRCRAFT ENGINE |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
AGAV |
| AAGR |
CROSS-SECTIONAL SHAPE STYLE |
STRAIGHT FACE, BOTTOM RELIEF |
| MATT |
III MATERIAL |
IRON OVERALL |
| ADTE |
JOINT STYLE |
VERTICAL JOINT |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS7310 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ACXF |
RADIAL WALL THICKNESS |
0.1800 INCHES MINIMUM AND 0.1900 INCHES MAXIMUM |
| RDAL |
REFERENCE DATA AND LITERATURE |
T.O.2J-J57-54 |
| ACXD |
RING STYLE |
EXPANDING CONCENTRIC |
| ABKV |
OUTSIDE DIAMETER |
6.399 INCHES NOMINAL |
| ACXJ |
OVERALL WIDTH |
0.1225 INCHES MINIMUM AND 0.1240 INCHES MAXIMUM |
| FEAT |
SPECIAL FEATURES |
LOAD REQ'D TO CLOSE TO DIA SHOWN IS 1.70 - 3.40 LBS |
| SFTT |
SURFACE TREATMENT |
CHROMIUM OVERALL |
