Part Number
Part Number:
NSN:
NIIN:
Item Name:
BELL CRANK
Definition:
AN ITEM IN THE FORM OF TWO ARMS AT AN ANGLE, HAVING ITS FULCRUM AT THE APEX OF THE ANGLE, AND USED TO PROVIDE A MEANS OF CHANGING THE DIRECTION OR VARYING THE INTENSITY OF A PUSHING OR PULLING FORCE. SEE ALSO ARM (AS MODIFIED); AND LEVER (AS MODIFIED).
CAGE Information
Code | Company |
---|---|
81996 | U S ARMY AVIATION AND MISSILE COMMAN |
Federal Supply Class
Title
AIRFRAME STRUCTURAL COMPONENTS
Inclusions:
INCLUDES FLIGHT CONTROL SURFACES; INTERNAL AND EXTERNAL AUXILIARY FUEL TANKS; EXHAUST SYSTEMS; PYLONS, TRIM TABS; AIRCRAFT.
Exclusions:
EXCLUDES FITTED COVERS; HELICOPTER ROTOR BRAKE SYSTEM COMPONENTS; AIRCRAFT LOOSE EQUIPMENT AND ALTERNATE MISSION CONFIGURATION EQUIPMENT STORED ON BOARD THE AIRCRAFT.
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 4.000 INCHES NOMINAL 2ND END |
ADGE | BORE LENGTH | 0.802 INCHES MINIMUM AND 0.812 INCHES MAXIMUM |
CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 2.730 INCHES NOMINAL 1ST END |
CZLN | END HOLE/BALL DIAMETER | 0.2495 INCHES MINIMUM 2ND END AND 0.2500 INCHES MAXIMUM 2ND END |
CZLN | END HOLE/BALL DIAMETER | 0.3120 INCHES MINIMUM 1ST END AND 0.3125 INCHES MAXIMUM 1ST END |
ZZZV | FSC APPLICATION DATA | FUSELAGE SECT.,ACFT |
MATT | MATERIAL | ALUMINUM ALLOY |
ABXV | BORE DIAMETER | 0.8738 INCHES MINIMUM AND 0.8743 INCHES MAXIMUM |