Premium Information is available for this item - Upgrade for $1 a day
5340-01-476-5277
Angle Bracket
5340014765277 014765277 376419-1
A ridge item, usually of flat material, formed into a dihedral angle (generally a right angle) which may be reinforced; it is designed to position, align, or support an item(s) in relation to another. Excludes BRACE (as modified); BRACKET (1), MOUNTING; and BRACKET, SHELF. View more Angle Bracket
![]()
January 2023
4



Marketplace 5340-01-476-5277
Request a Quotation from participating marketplace vendors
Related Documents 5340-01-476-5277 2+ Documents (More...)
5340-01-476-5277 RQST Updated Every Day 5340-01-476-5277 RQST NE Related Documents 5340-01-476-5277
5340014765277014765277 (Identification) 1/3 NSN 5340-01-476-5277 (Identification) 2/3 NSN 5340-01-476
Angle Bracket 5340014765277 014765277 Upgrade for $1 a day Upgrade your Account Upgrade 5340-01
-476-5277Angle Bracket5340014765277 014765277 376419 Request a Quotation from participating marketplace
Restrictions 5340-01-476-5277
5340-01-476-5277 is a Angle Bracket that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 5340-01-476-5277
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5340-01-476-5277
- United Kingdom (ZK01)
- Effective Date:
- 1 Jul 2000
Approved Sources 5340-01-476-5277
- Part Number
- Manufacturer
- Status
- 376419-1
- Manufacturer
- 98897 - Lockheed Martin Corp (Active)
- Primary Buy
- Primary Buy
Datasheet 5340-01-476-5277
- Characteristic
- Specifications
- FIIG
- Specifications
- A042A0
- End Item Identification [AGAV]
- C130j Aircraft
- First Leg Angle [CSSQ]
- 0.22 Radians Nominal
- First Leg Distance From Edge To Hole Center Along Width [AHRA]
- 0.410 Inches Nominal
- First Leg End Width [AHQQ]
- 0.320 Inches Nominal
- First Leg Hole Arrangement Style [AKAU]
- Two Holes
- First Leg Hole Diameter [AHLK]
- 0.195 Inches Minimum And 0.203 Inches Maximum
- First Leg Distance Between Hole Centers Along Length [AHQX]
- 0.780 Inches Nominal
- First Leg Distance From Edge To Hole Center Along Length [AHRB]
- 0.410 Inches Nominal
- First Leg Style [AJZU]
- Angle
- First Leg Thickness [AHPW]
- 0.063 Inches Nominal
- First Leg Width [AHQN]
- 0.920 Inches Nominal
- First Leg Length [ADLK]
- 0.920 Inches Nominal
- Material Document And Classification [MDCL]
- Qq-A-362, Cond T3 Fed Spec Single Material Response
- Material [MATT]
- Aluminum Alloy 2024
- Second Leg Distance Between Hole Centers Along Length [AHLS]
- 0.780 Nominal Inches
- Second Leg Hole Diameter [AHLN]
- 0.195 Inches Minimum And 0.203 Inches Maximum
- Second Leg Length [ADLL]
- 0.920 Inches Nominal
- Second Leg Distance From Edge To Hole Center Along Length [AHLW]
- 0.410 Inches Nominal
- Second Leg Distance From Edge To Hole Center Along Width [AHLV]
- 0.410 Inches Nominal
- Second Leg End Width [AHLH]
- 0.320 Inches Nominal
- Second Leg Width [AHLF]
- 0.920 Inches Nominal
- Second Leg Relationship To First Leg [CSSP]
- Identical
- Second Leg Thickness [AHPX]
- 0.063 Inches Nominal
- Part Name Assigned By Controlling Agency [CXCY]
- Clip-Cargo Net Box, Fus Sta 836.0, Lh Side, Upper
- Style Designator [STYL]
- Angle
Similar Supply Items to 5340-01-476-5277


















Freight Information 5340-01-476-5277
5340-01-476-5277 has freight characteristics managed by the Bureau of Accounts.. 5340-01-476-5277 has a variance between NMFC and UFC when transported by rail and the description should be consulted.