| MRC |
Requirement Statement |
Characteristics |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| CQSX |
SHEAR STRENGTH |
26000 SINGLE POUNDS PER SQUARE INCH |
| AGAV |
III END ITEM IDENTIFICATION |
W/S:CLOSE IN WEAPON SYSTEM (CIWS-PHALANX); AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130); DEF COMM METEORL (AN/TMQ-028, AN/TCC-76, AN/TPS-068, AN-TCC-77); MISSILE, ADVANCED MEDIUM RANGE AIR-TO-AIR (AMRAAM)/AIM120A; SUPPORT EQUIPMENT, B-1 AIRCRAFT; SUPPORT EQUIPMENT, B-52 AIRCRAFT; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); TEAMMATE, AN/TRQ-32; RADAR SET, AN/PPS-5B |
| SUPP |
III SUPPLEMENTARY FEATURES |
FLIGHT SAFETY CRITICAL |
| AASK |
HEAD STYLE |
FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER) |
| AAZG |
HEAD MAJOR DIAMETER |
0.175 INCHES MINIMUM AND 0.183 INCHES MAXIMUM |
| SFTT |
SURFACE TREATMENT |
ANODIZE OR CHROMATE OVERALL |
| AASB |
FASTENER LENGTH |
0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM |
| FEAT |
SPECIAL FEATURES |
RIVET HAS 0.020 INCH MAXIMUM DEPTH DIMPLE IN HEAD, WITH A MAXIMUM DIAMETER OF 0.030 INCHES |
| AAZF |
SHANK STYLE |
STRAIGHT W/RADIUS CHAMFERED TIP |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OR MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE OVERALL |
| AAZE |
SHANK DIAMETER |
0.093 INCHES MINIMUM AND 0.097 INCHES MAXIMUM |
| CRSQ |
COUNTERSINK ANGLE |
100.0 DEGREES NOMINAL |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
SUPP |
| MATT |
MATERIAL |
ALUMINUM ALLOY 2117 OVERALL |
| HEAT |
HEAT TREATMENT |
T-4 SOLUTION HEAT TREATED OVERALL |
