NIIN Output Data
NIIN:
NSN:
Item Name:
BOLT , MACHINE
Definition:
AN EXTERNALLY THREADED FASTENER DESIGNED FOR INSERTION THROUGH HOLES IN ASSEMBLED PARTS AND NORMALLY INTENDED TO BE TIGHTENED OR RELEASED BY TORQUING A NUT. THE THREADED AND UNTHREADED PORTIONS ARE BOTH OF ONE NOMINAL DIAMETER OF 0.190 INCH (5 MM) OR LARGER. THE HEAD IS NOT DESIGNED TO BE HELD OR DRIVEN WITH AN INSERTED DRIVER OR BY THE THUMB AND FINGERS. A LOCKING FEATURE MAY BE INCORPORATED IN THE DESIGN OF THE HEAD OR THREADS. HEAD DIMENSIONS AND SIZES OF THREADED AND UNTHREADED PORTIONS SHALL CONFORM TO INTERNATIONALLY RECOGNIZED FASTENER STANDARDS. FOR ITEMS HAVING A GRIP LENGTH PORTION MACHINED TO A TOLERANCE OF 0.0015 INCH (0.038 MM) OR LESS, BOLT, SHEAR. SEE ALSO SCREW, CAP, HEXAGON HEAD AND SCREW, MACHINE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 932.19.21.003 | S4080 | A | 5 | 2 | 3 | ZN | ||
| 278-16 | 45934 | A | 5 | 9 | 5 | KZ | ||
| 35026 | 00198 | A | 3 | 2 | 4 | KZ | ||
| AN3-6 | K1789 | A | 5 | 2 | 4 | ZK | ||
| AN3-6 | 80205 | A | 3 | 2 | E | ZZ | ||
| Z00.N5106301006 | F0086 | A | 5 | 2 | 4 | ZF | ||
| 278-16 | 56705 | R | 5 | 9 | 5 | KZ | ||
| AN3-6 | 81352 | M | 5 | 2 | X | XX | ||
| 2018146 | 001JK | A | 5 | 2 | 5 | 9Z | ||
| 5858 | 55948 | F | 5 | 9 | 5 | TU | ||
| 35026 | 77445 | A | 5 | 9 | X | KZ | ||
| 2018146 | S4956 | R | 5 | 9 | 4 | ZF | ||
| 35026 | R1120 | A | 5 | 2 | 6 | ZG | ||
| AN3-6 | 88044 | M | 5 | 9 | E | XX | ||
| 400 053 | 77294 | A | 5 | 2 | 5 | 9Z |
CAGE Information
| Code | Company |
|---|---|
| 00198 | PRATT AND WHITNEY CANADA INC WHITNEY |
| S4080 | PILATUS AIRCRAFT LTD |
| 45934 | ONTIC ENGINEERING AND MANUFACTURING, |
| K1789 | PERMALI GLOUCESTER LTD |
| 80205 | NATIONAL AEROSPACE STANDARDS COMMITT |
| F0086 | EADS SOCATA |
| 56705 | DONALLCO INC |
| 81352 | AIR FORCE-NAVY AERONAUTICAL SPECIFIC |
| 001JK | EMBRAER S/A |
| 55948 | BOTOMAN MFG CO INC |
| 77445 | UNITED TECHNOLOGIES CORPORATION DBA |
| S4956 | EMBRAER EMPRESA BRASILEIRA DE AERONA |
| R1120 | SATAIR A/S |
| 88044 | AERONAUTICAL STANDARDS GROUP DEPT OF |
| 77294 | PIPER AIRCRAFT INC. |
Federal Supply Class
Title
BOLTS
Inclusions:
Exclusions:
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| AHYM | NOMINAL THREAD DIAMETER | 0.190 INCHES |
| AAWB | SHANK UNTHREADED HOLE DIAMETER | 0.070 INCHES NOMINAL FIRST HOLE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-B-6812 MIL SPEC ALL MATERIAL RESPONSES OVERALL |
| CBBL | FEATURES PROVIDED | FINISHED HEAD |
| AAJD | THREAD CLASS | 3A |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TYPE 2 CLASS 3 FED SPEC ALL TREATMENT RESPONSES OVERALL |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AATB | WIDTH BETWEEN FLATS | 0.365 INCHES MINIMUM AND 0.377 INCHES MAXIMUM |
| THSD | THREAD SERIES DESIGNATOR | UNF |
| MATT | MATERIAL | STEEL COMP 8740 OVERALL OR STEEL COMP 8735 OVERALL OR STEEL COMP 8630 OVERALL OR STEEL COMP 4130 OVERALL OR STEEL COMP 4037 OVERALL OR STEEL COMP 4140 OVERALL |
| CQBC | MINIMUM TENSILE STRENGTH | 125000 POUNDS PER SQUARE INCH |
| AASK | HEAD STYLE | HEXAGON |
| AASA | THREAD LENGTH | 0.406 INCHES MINIMUM |
| CRZS | DISTANCE FROM HEAD LARGEST BEARING SURFACE TO SHANK HOLE CENTER | 0.641 INCHES NOMINAL FIRST HOLE |
| SFTT | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMATE OVERALL |
| ANEE | GRIP LENGTH | 0.375 INCHES NOMINAL |
| CMLP | THREAD QUANTITY PER INCH | 32 |
| CQFM | HARDNESS RATING | 26.0 ROCKWELL C MINIMUM OVERALL AND 32.0 ROCKWELL C MAXIMUM OVERALL |
| AASB | FASTENER LENGTH | 0.781 INCHES NOMINAL |
| AASU | HEAD HEIGHT | 0.109 INCHES MINIMUM AND 0.141 INCHES MAXIMUM |
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