| MRC |
Requirement Statement |
Characteristics |
| SFTT |
SURFACE TREATMENT |
PASSIVATE OVERALL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5656 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CWFR |
NOMINAL OVERALL LENGTH |
2.700 INCHES |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL. GRUMMAN A-10 AIRCRAFT |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-S-5002 MIL SPEC SINGLE TREATMENT RESPONSE INSIDE MIL-F-14072,E300,TY2 MIL SPEC SINGLE TREATMENT RESPONSE OUTSIDE |
| MATT |
MATERIAL |
STEEL COMP XM-10 OVERALL |
| AWLS |
CONNECTION TYPE |
UNTHREADED INTERNAL TUBE ALL ENDS |
| CQGM |
MAXIMUM OPERATING PRESSURE |
3000.0 POUNDS PER SQUARE INCH SINGLE RESPONSE |
| AHNC |
CONNECTION STYLE |
SWAGED W/ GROOVES (TUBE) ALL ENDS |
| STYL |
STYLE DESIGNATOR |
SWAGED BOTH ENDS |
| CWFK |
TUBING WALL NOMINAL THICKNESS FOR WHICH DESIGNED |
0.109 INCHES ALL ENDS |
| CWFD |
NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED |
0.500 INCHES ALL ENDS |
| AGAV |
END ITEM IDENTIFICATION |
MH-53E HELICOPTER. FMS-A7 AIRCRAFT. C-135 STRATOLIFTER AIRCRAFT. F4S AIRCRAFT. F-4 PHANTOM AIRCRAFT. (AC-130H, MC-130H, EC-130E, HC-130) AIRCRAFT |
