| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
HELICOPTER, SEAHAWK, H-60 AIRCRAFT, STRATOLIFTER C-135 HELICOPTER, LAMPS MARK III, SH-60B AIRCRAFT, T-38 AIRCRAFT, HARRIER AV-8B |
| ABPX |
MATERIAL THICKNESS |
0.002 INCHES MINIMUM AND 0.022 INCHES MAXIMUM |
| MATT |
MATERIAL |
COPPER ALLOY OVERALL |
| ACSZ |
MATING MEMBER DIAMETER ACCOMMODATED |
0.138 INCHES NOMINAL |
| ADEA |
NUT HEIGHT |
0.678 INCHES MINIMUM AND 0.698 INCHES MAXIMUM |
| ADED |
NUT WIDTH |
0.271 INCHES MINIMUM AND 0.291 INCHES MAXIMUM |
| ACVN |
NUT LENGTH |
0.661 INCHES MINIMUM AND 0.681 INCHES MAXIMUM |
| ACTA |
NUT STYLE |
SHEET SPRING |
| ADEE |
PANEL THICKNESS |
0.302 INCHES MINIMUM AND 0.322 INCHES MAXIMUM |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
QQ-P-416,TYPE 1,CLASS 2 FED SPEC 1ST TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 2ND TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 3RD TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 4TH TREATMENT RESPONSE OVERALL OR QQ-Z-325 FED SPEC 5TH TREATMENT |
| SFTT |
SURFACE TREATMENT |
CADMIUM OVERALL OR ZINC OVERALL AND CHROMATE OVERALL OR ZINC OVERALL AND PHOSPHATE OVERALL |
