| MRC |
Requirement Statement |
Characteristics |
| APGF |
DESIGN TYPE |
FRICTION |
| AGAV |
END ITEM IDENTIFICATION |
W/S: TORPEDO SYSTEMS, MK 50 ENGINE, AIRCRAFT, T56-A-7/15 (C-130B/E/H/N/P) MISSILE, ADVANCED MEDIUM RANGE AIR-TO-AIR (AMRAAM)/AIM120A MISSILE, AIR-TO-AIR, SPARROW (AIM-7) SUPPORT EQUIPMENT, B-1 AIRCRAFT AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130) M |
| MATT |
MATERIAL |
PLASTIC POLYETHYLENE |
| BZMQ |
INSIDE DIAMETER LENGTH |
0.594 INCHES MINIMUM AND 0.656 INCHES MAXIMUM |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
L-P-390, TYPE 1, CLASS L, GRADE OPTIONAL FED SPEC SINGLE MATERIAL RESPONSE |
| BZMX |
ROUND CAP OUTSIDE SURFACE CONDITION |
SMOOTH |
| ADAV |
OVERALL DIAMETER |
1.094 INCHES MINIMUM AND 1.156 INCHES MAXIMUM |
| ACSV |
TUBE OUTSIDE DIAMETER FOR WHICH DESIGNED |
0.883 INCHES MINIMUM AND 1.003 INCHES MAXIMUM |
