Part Number
Definition:
A STRAIGHT SHAFT HAVING TWO OR MORE OF THE FOLLOWING CONDITIONS: A SPECIFIED SURFACE FINISH DESIGNATION IN THE RANGE OF 1 TO 125 MICROINCHES (O.O25 TO 3.2 MICROMETERS), ARITHMETICAL AVERAGE (AA), MACHINED PERIPHERAL FLAT(S), CIRCULAR GROOVE (S), KEYWAY(S), SPLINES, THREADS, OR HOLES. IT IS NOT DESIGNED FOR USE IN ALIGNING BY FITTING INTO CORRESPONDING HOLES OF ANOTHER ITEM. IT MAY BE DRILLED FOR LUBRICATING HOLES. FOR ITEMS HAVING AN INTEGRAL GEAR(S) OR WORM(S), SEE GEARSHAFT (AS MODIFIED). FOR ITEMS DESIGNED TO SUPPORT ROTATING MEMBERS SEE AXLE(1), STRAIGHT. FOR ITEMS NOT HAVING THE ABOVE CONDITIONS SEE PIN, STRAIGHT, HEADLESS. FOR ITEMS HAVING MACHINED ENDS WHICH CONSTITUTE STEPS SEE SHAFT(1), SHOULDERED; AXLE(1), SHOULDERED; AND BOLT, FLUID PASSAGE.
CAGE Information
| Code | Company |
|---|---|
| 82918 | THE BOEING COMPANY GLOBAL SERVICES & |
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 |
|---|---|---|
| AAGZ | FIRST END STYLE | PLAIN |
| AMDL | FIRST END DIAMETER | 1.0000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT, STRATOLIFTER C-135 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | WW-T-700 FED SPEC SINGLE MATERIAL RESPONSE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | DRIVE SHAFT R.H. INBOARD SECTION EMER. L.G. EXTENSION |
| ABHP | OVERALL LENGTH | 26.670 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | ASSEMBLY INCLUDES THE -2 SLEEVE, RUBBING WHICH IS MADE OF PLASTIC; USED ON THE EMERGENCY EXTENSION, LANDING GEAR, GEARBOX ASSEMBLY |
| AAHN | END SIMILARITY | IDENTICAL |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |