Price Quote Get an up to date pricing and availability quote for this product. Order online or over the phone.
Quality Commitment
Serving our customers with quality and safety first.
- AS9120 Certified
- Audited supply chain
- ITAR Registered
- DDTC Registered
- HAZMAT Certified
- Customer service objectives
- Every product 100% inspected
Datasheet. NAS626H21 specification
The national stock number or the identification information of the end equipment for which the item is a part.
C-17A aircraft
The name assigned to the item by the government agency or commercial organization controlling the design of the item.
bolt, shear
Answers.
1EA
FSC 5306 ⁓ Bolts
NSN 5306-01-528-4204 BOLT,SHEAR
Used on c-17a aircraft. bolt, shear
- NIIN
- 015284204
- NIIN Date
- 03/11/05
- Schedule B
- Name Code
- 15903
- FIIG
- A003B0
- QUP
- 1
- Historical Price
- $1.68 EA
- DEMIL / ITAR
- Uncontrolled item (Code A)
- Hazmat
- No hazard information available from HMIRS.
- MSDS
- N/A
- Precious Metals
- No precious metals
- Enviromental
- N/A
- Electrostatic ESD & EMI
- No ESD or EMI sensitivity
Major End Users Countries and entities
- - Department of The Air Force
Availability for NAS626H21 A member of our team will provide you with a price and availability quote
Request a Quote »Similar by Design Other bolts with similar characteristics
Nothing similar to this part number was found in our inventory
NAS626H21 / Bolt,shearWhat is the formal definition of this item?
A high strength, 160,000 pounds per square inch (1100 megapascals) minimum tensile strength externally threaded fastener designed for use in applications involving great shear stress. the head is designed to accommodate an external wrench or driver. the head is not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. the unthreaded portion is of specific grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015) of an inch (0.038 mm) or less. the nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the screw thread standards, fed std h28 and/or other nationally recognized standards. a locking feature may be incorporated in the design of the head or threads. see bolt, machine and bolt, clevis.
