Aircraft Spruce Canada
Brantford, ON Canada
Corona, CA | Peachtree City, GA
Chicago, IL | Wasilla, AK
Aircraft Spruce Canada- Wishlists
- 1-877-795-2278
- Contact Us
Contact Us
Call Us
Sign In
- Photo may represent series and not specific product
- SHARE
Clevis Bolt Drilled AN24-11
- JUMP TO
- Overview
- Reviews
- Q&A
- View in Catalog
| Dash No. | Grip | Length |
|---|---|---|
| -11 | 3/8 | 23/32 |
Overview
| Clevis bolts have a slotted brazier type head. They are special-purpose bolts for use where a large shearing stress occurs (never in tension). Manufactured and cadmium plated in same manner as AN3 - AN8 aircraft bolts. Minimum tensile strength 125,000 PSI. Available with drilled or undrilled shank. Add letter "A" after dash number for undrilled shank. Prices fluctuate on clevis bolts. |
Reviews
Verified Purchase
Clevis Bolt Drilled AN24-11 (Pack Of 5)
Looks ok.
Verified Purchase
Clevis Bolt Drilled AN24-11
Verified Purchase
Clevis Bolt Drilled AN24-11
Bolts worked as expected but very expensive.
i purchased the same clevis bolt from another aircraft supply house in the Midwest. It was not cad plated. It just did not look nice for the project. This bold looks crisp and appropriate for the restoration. Much higher quality product.
These bolts were purchased to replace previous purchase of same bolts. Previous bolts threads were so damaged, it was impossible to thread a castellated nut onto them. The newly purchased bolts had the same problem, just not as damaged. Threading the nut was difficult, but not impossible. Also, why are these almost $10 each?
Q&A
Please note, Aircraft Spruce Canada's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce Canada assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.
The grip length is measured from under the head to the start of the threads.
