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MRC | Criteria | Characteristic |
---|---|---|
AAGR | CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
AAUB | HOLE DIAMETER | 0.880 INCHES MINIMUM AND 0.900 INCHES MAXIMUM |
ABMW | PERIPHERAL SHAPE STYLE | ROUND |
ABMX | CENTER HOLE SHAPE STYLE | ROUND |
ABNM | THICKNESS | 0.080 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
ADAV | OVERALL DIAMETER | 1.495 INCHES MINIMUM AND 1.520 INCHES MAXIMUM |
AGAV | III END ITEM IDENTIFICATION | W/S:DEEP SUBMERGENCE SYSTEMS PROGRAMS (DSSP); AVIATION ENGINE TEST SYSTEMS (AETS); HELICOPTER, MH-53E; ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); AIRCRAFT, T-39; AIRCRAFT, C-2A (REPROCURED); SUPPORT EQUIPMENT, B-1 AIRCRAFT; ENGINE, AIRCRAFT, T56-A |
MATT | MATERIAL | STEEL OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-7952 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL OR QQ-S-698 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
SFTT | SURFACE TREATMENT | CADMIUM OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
NAS 1091A30H | NAS 1143-16 | NAS 1023D4 | NAS 1057 |
NAS 1006-78A | NAS 1023D4 | NAS 1142-4 | NAS 1201 D6A10A |
NAS 1023D4 | NAS-1100-FWEX-FA | NAS 1142-6 | NAS 1010 26A |
NAS 124Y-125 | NAS 1143 14 | NAS 1063 | NAS 124 |
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