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Part Number

Part Number:
NSN:
NIIN:
Item Name:
MOUNT , RESILIENT , WEAPON SYSTEM

Definition:

AN ITEM MADE OF MATERIAL HAVING ELASTIC PROPERTIES. IT MAY HAVE RIGID MOUNTING FACILITIES SUCH AS A FLANGE(S), SLEEVE(S), STUD(S) OR THE LIKE. IT IS DESIGNED TO ISOLATE OR DAMPEN SHOCK AND/OR VIBRATION OF A CONTINUOUS OR INTERMITTENT ORIGIN AND SERVE AS A SUPPORT FOR A WEAPON SYSTEM COMPONENT TO BE ISOLATED. EXCLUDES MOUNT, RESILIENT, GENERAL PURPOSE; SPRING (AS MODIFIED); BUMPER, NONMETALLIC; BUMPER, RUBBER; BUSHING, NONMETALLIC; HYDRAULIC AND PNEUMATIC SHOCK ABSORBERS, DASH-POTS, GROMMETS, AND SHOCK PADS.

CAGE Information

Code Company
76301 BOEING COMPANY THE DBA BOEING

Federal Supply Class

Title

HARDWARE, WEAPON SYSTEM

Inclusions:

INCLUDES ADAPTERS; ANCHOR PLATES AND STRAPS; ANODES; BELLOWS; COUPLINGS; CONTROL RODS; ACCESS DOORS; FAIRLEADS; MOUNTS; TIE RODS; YOKES.

Exclusions:

EXCLUDES COMMERCIAL HARDWARE (FSC 5340).

Characteristics (Decoded)

MRC Requirements Statement Clear Text Reply
AGFF FLANGE WIDTH 1.250 INCHES NOMINAL
BXCQ FLANGE MOUNTING HOLE DIAMETER 0.195 INCHES MINIMUM AND 0.205 INCHES MAXIMUM
BXDM RESILIENT MEMBER MATERIAL SILICONE RUBBER
SFTT SURFACE TREATMENT CHROMATE CORE
AYXK MAXIMUM LOAD RATING 2.0 POUNDS
AFQN FLANGE LENGTH 1.752 INCHES MINIMUM AND 1.758 INCHES MAXIMUM
MATT MATERIAL ALUMINUM ALLOY BASE PLATE
ABUJ THREAD SIZE 10-32 ALL THREADED PORTIONS
ABKU FLANGE THICKNESS 0.140 INCHES NOMINAL
MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/8, ALLOY 5052, TEMPER H32 FED SPEC SINGLE MATERIAL RESPONSE BASE PLATE
MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/8, ALLOY 5052, TEMPER O FED SPEC SINGLE MATERIAL RESPONSE CUP
AFQM DISTANCE BETWEEN MOUNTING HOLE CENTERS 1.399 INCHES MINIMUM AND 1.429 INCHES MAXIMUM
MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-225/6, ALLOY 2024, TEMPER T4 FED SPEC SINGLE MATERIAL RESPONSE CORE
MATT MATERIAL ALUMINUM ALLOY CORE
MATT MATERIAL ALUMINUM ALLOY CUP
STYL STYLE DESIGNATOR ROUND TWO-HOLE FLANGE
STDC SURFACE TREATMENT DOCUMENT AND CLASSIFICATION MIL-C-5541, CLASS 1A MIL SPEC SINGLE TREATMENT RESPONSE CORE

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