Textron Aviation Inc. - Machine Bolt, Magnetic Inspected - 130909B170
Genuine OEM Part
Description: Machine Bolt, Magnetic Inspected
Part Number: 130909B170
Alternate Part Numbers: 0278, 1443709, 2018924, A239, AN4-12
Product Overview
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 inches (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 inches (0.038 mm) or less, bolt, shear. See also screw, cap, hexagon head and screw, machine.
Item Specification
| Thread Class | 3A | |
| Thread Direction | Right-hand | |
| Thread Length | 0.469 inches minimum | |
| Fastener Length | 1.281 inches nominal | |
| Head Style | Hexagon | |
| Head Height | 0.140 inches minimum and 0.172 inches maximum | |
| Width Between Flats | 0.428 inches minimum and 0.440 inches maximum | |
| Shank Unthreaded Hole Diameter | 0.076 inches minimum first hole | |
| Nominal Thread Diameter | 0.250 inches | |
| Grip Length | 0.812 inches nominal | |
| Features Provided | Finished head | |
| Thread Quantity per Inch | 28 | |
| Minimum Tensile Strength | 125000 pounds per square inch | |
| Hardness Rating | 26.0 rockwell C minimum overall and 32.0 rockwell C maximum overall | |
| Distance from Head Largest Bearing Surface to Shank Hole Center | 1.124 inches nominal first hole | |
| Material | Steel comp 4037 overall or steel comp 4130 overall or steel comp 8630 overall or steel comp 8735 overall or steel comp 8740 overall or steel comp 4140 overall | |
| Material Document and Classification | MIL-B-6812 mil spec all material responses overall | |
| Surface Treatment | Cadmium overall and chromate overall | |
| Surface Treatment Document and Classification | QQ-P-416, ty 2, cl 3 fed spec single treatment response overall | |
| Thread Series Designator | UNF |
Fits in
- Dassault Falcon 2000 all variants
- Dassault Falcon 900 all variants
- Embraer Legacy 600-650
- Textron Aviation Beechcraft King Air 100 - all variants
- Textron Aviation Beechcraft King Air 200 - all variants
- Textron Aviation Beechcraft King Air 300 - all variants
- Textron Aviation Beechcraft King Air 90 - all variants
- Textron Aviation Bell 206 Jetranger/Longranger
- Textron Aviation Cessna 500 Citation I-ISP
- Textron Aviation Cessna 510 Citation Mustang
- Textron Aviation Cessna 525 Citation Citationjet
- Textron Aviation Cessna 550 Citation I-II-Bravo
- Textron Aviation Cessna 560 Citation V-Ultra-Encore-Excel-XLS
- Textron Aviation Cessna 680 Citation Sovereign
- Textron Aviation Cessna 750 Citation X
- Textron Aviation Hawker 800XP-850XP
Hawker Beechcraft Corporation F33/G33/F33A/F33C Illustrated Parts Catalog [ Click Here ]
See Page 34, Figure 03, Item 40
| Additional info | |
|---|---|
| Colors | Gold |
| Dimensions | |
|---|---|
| Dimensions (W x H x D) | 3.85" x 5.55" x 0.95" inches |
| Length | 5.55" inches |
| Weight | 0.25 lb |
| Specifications | |
|---|---|
| 8130-3 Eligible | Yes |
| ATA Chapter | 32 ATA Landing Gear |
| Available Conditions | NE / NS / OH / AR |
| Cage Code | 7EK50 |
| Country of origin | United States of America |
| ECCN / USML | EAR99 |
| FAA Approval Code | PC |
| Grip | 0.469 inches minimum |
| Hazmat Code | Not Applicable |
| Hazmat(Y/N) | N |
| Material | Steel Overall |
| NSN | 5306-01-506-2214 |
| Schedule B | 7318.16.0000 |
| Thread | 3A |
| Total Shelf Life (days) | Not Applicable |
| Type | Bolt |
| Units of Measure (UoM) | Each |
| Brand | Textron Aviation |
| Color | Gold |
| Condition status | AR – As Removed |