Part Number
Definition:
AN ITEM DESIGNED TO BE MOUNTED AROUND A SHAFT TO LIMIT AXIAL MOVEMENT OF THE SHAFT AND/OR ITS ASSEMBLED PARTS. IT IS SECURED DIRECTLY TO THE SHAFT BY USE OF A SETSCREW(S), PIN(S), OR THE LIKE, WHICH MAY BE A PART OF THE ITEM OF SUPPLY. A PILOT HOLE DRILLED IN OR THROUGH THE WALL(S) FOR DRILLING AND PINNING AT APPLICATION MAY BE CONSIDERED A METHOD OF SECURING. SOLID ITEMS HAVE A BEARING SURFACE ON ONE OR BOTH END(S) PERPENDICULAR TO THE AXIS. FOR ITEMS DESIGNED TO BE MOUNTED AROUND THE EXTENDED HUB PORTION OF A MOUNTED ITEM ON A SHAFT OR CLAMP AROUND A SHAFT, SEE CLAMP, HUB. SEE ALSO BEARING, SLEEVE; BUSHING, SLEEVE; SPACER, SLEEVE; AND COUPLING, SHAFT, RIGID.
CAGE Information
Code | Company |
---|---|
11449 | TURBO POWER & MARINE SYSTEM INC SUB |
Federal Supply Class
Title
MISCELLANEOUS POWER TRANSMISSION
Inclusions:
INCLUDES SHAFTS AND SHAFTING; COLLARS; GEARSHAFTS; BALL JOINTS; ACTUATING CYLINDERS.
Exclusions:
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
ABNM | THICKNESS | 0.295 INCHES MINIMUM AND 0.305 INCHES MAXIMUM |
ABNM | THICKNESS | 0.295 INCHES MINIMUM AND 0.305 INCHES MAXIMUM |
ABKV | OUTSIDE DIAMETER | 0.492 INCHES MINIMUM AND 0.502 INCHES MAXIMUM |
ABXV | BORE DIAMETER | 0.3200 INCHES MINIMUM AND 0.3240 INCHES MAXIMUM |
FEAT | SPECIAL FEATURES | NICKEL ALLOY AMS5754 |
AGAV | END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
AEUZ | LARGEST DIAMETER LENGTH | 0.220 INCHES NOMINAL |
STYL | STYLE DESIGNATOR | ROUND W/DOUBLE CHAMFER |
AATE | CHAMFER ANGLE IN DEG | 45.0 |