NIIN Output Data
Definition:
A SHAFT HAVING TWO OR MORE DIFFERENT DIAMETERS (GREATER THAN 0.031 INCHES (0.79 MILLIMETER)) ALONG ITS LENGTH. IT MUST HAVE ONE OR MORE OF THE FOLLOWING CONDITIONS: A SPECIFIED SURFACE FINISH DESIGNATION IN THE RANGE 1 TO 125 MICROINCHES (0.025 TO 3.2 MICROMETERS) ARITHMETICAL AVERAGE (AA), MACHINED PERIPHERAL FLAT(S), CIRCULAR GROOVE(S), KEYWAY(S), SPLINES, THREADS, OR HOLES. THE ENDS AND/OR SHOULDERS MAY BE MACHINED TO ACCOMMODATE BEARINGS, COUPLINGS, AND THE LIKE. IT IS NOT DESIGNED FOR USE IN ALIGNING BY FITTING INTO CORRESPONDING HOLES OF ANOTHER ITEM. FOR ITEMS USED TO SUPPORT ROTATING MEMBERS SEE AXLE(1), SHOULDERED. FOR ITEMS NOT HAVING ANY OF THE ABOVE CONDITIONS SEE PIN, SHOULDER, HEADLESS. EXCLUDES SHAFT(1), STRAIGHT; AND AXLE(1), STRAIGHT.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 1534AS431 | 09245 | A | 5 | 2 | 5 | ZZ | ||
| 1534AS431 | 31645 | A | 5 | 9 | 6 | ZZ | ||
| D014189-501 | 88277 | A | 5 | 9 | 1 | KE | ||
| 1534AS431 | 32067 | A | 5 | 2 | 5 | ZZ | ||
| D014189-501 | 57928 | A | 5 | 9 | 5 | KE | ||
| D014189-501 | 8V613 | A | C | 1 | 5 | ZZ | AC | |
| 1534AS431 | 072E5 | A | 5 | 2 | 6 | ZZ | ||
| 1534AS431 | 05DN8 | A | 5 | 2 | 6 | ZZ | ||
| 1534AS431 | 30003 | A | 3 | 2 | 1 | KE |
CAGE Information
| Code | Company |
|---|---|
| 05DN8 | KLUNE INDUSTRIES INC. |
| 09245 | SOLO ENTERPRISE CORP. DBA SOLO GOLF |
| 31645 | GOODRICH CORPORATION DBA GOODRICH CA |
| 88277 | BOEING COMPANY THE DBA BOEING |
| 32067 | MARVIN ENGINEERING CO. INC. |
| 57928 | SONIC INDUSTRIES INC. |
| 8V613 | BOEING COMPANY THE DIV DEFENSE SPACE |
| 072E5 | RAYTHEON TECHNICAL SERVICES COMPANY |
| 30003 | NAVAL AIR SYSTEMS COMMAND |
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 |
|---|---|---|
| CSPY | LARGEST STEP DIAMETER | 0.781 INCHES NOMINAL |
| ABHP | OVERALL LENGTH | 4.239 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL. |
| AAHN | END SIMILARITY | NOT IDENTICAL |
| AAHP | SECOND END STYLE | EXTERNAL THREADED |
| ATPC | STEP QUANTITY | 8 |
| AMHA | SECOND END EXTERNAL THREAD LENGTH | 0.283 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F/A-18 HORNET AIRCRAFT. |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE |
| AAGZ | FIRST END STYLE | EXTERNAL THREADED |
| ZZZV | FSC APPLICATION DATA | RACK,BOMB EJECTOR AIRCRAFT BRU-32A |
| AMFZ | SECOND END DIAMETER | 0.3750 INCHES NOMINAL |
| AMDL | FIRST END DIAMETER | 0.1900 INCHES NOMINAL |
| AMEA | FIRST END EXTERNAL THREAD LENGTH | 0.378 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| MATT | MATERIAL | NICKEL ALLOY |