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5340-01-476-7793
T Bracket
5340014767793 014767793 17P2D4111-501
A rigid item generally of flat material which resembles the letter T.It has two interior angles (usually right angles) which together equal 180 degrees (3.141 radians). It is designed to position, align and/or support an item(s) in relationship to another. Excludes PLATE, T and BEAM, STRUCTURAL. View more T Bracket
January 2023
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Related Documents 5340-01-476-7793 1+ Documents (More...)
United States (US) 4. 5340-01-476-7793 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 5340-01-476-7793 RQST Updated Every Day 5340-01-476-7793 RQST NE Restrictions
Restrictions 5340-01-476-7793
5340-01-476-7793 is a T 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 5340-01-476-7793
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5340-01-476-7793
- US Air Force (FBB5)
- Effective Date:
- 1 Jul 2000
Approved Sources 5340-01-476-7793
- Part Number
- Manufacturer
- Status
- 17P2D4111-501
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 5340-01-476-7793
- Characteristic
- Specifications
- FIIG
- Specifications
- A042A0
- Material [MATT]
- Nickel Alloy 625
- Material Document And Classification [MDCL]
- Ams 5666 Assn Std Single Material Response
- Style Designator [STYL]
- Center Projection
- Overall Length [ABHP]
- 1.920 Inches Nominal
- Overall Height [ABKW]
- 1.470 Inches Nominal
- Overall Width [ABMK]
- 2.000 Inches Nominal
- Base Thickness [ACYB]
- 0.080 Inches Nominal
- Leg Thickness [AJJP]
- 0.285 Inches Nominal
- Distance From End To Leg Along Length [CZFG]
- 0.818 Inches Nominal
- Angle [CRMK]
- 90.0 Degrees Nominal
- Hole Quantity [ASXK]
- 5
- Mounting Hole Type [ACHY]
- Plain
- Special Features [FEAT]
- Base Plate Is Curved, With 2 Slots On Each Side; Center Leg Consists Of Two Parallel 0.080 In. Thick Plates Spaced 0.125 In. Apart, With A Square Hole Through Each
- End Item Identification [AGAV]
- C-17 Acft; Support, Apu Exhaust Duct
Management Data 5340-01-476-7793
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- May 2010
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BA
- C-17 PROGRAM
- Price Validation Code:
- N
- The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of “L” or “F”, then it must be evaluated locally where purchased or fabricated.
- Expendability
Recoverability
Repairability: - N
- Expendable. Condemn at User. Stock Fund (except Munitions).
NATO Stock Numbers Related to 5340-01-476-7793
Freight Information 5340-01-476-7793
5340-01-476-7793 has freight characteristics.. 5340-01-476-7793 has a variance between NMFC and UFC when transported by rail and the description should be consulted.