Premium Information is available for this item - Upgrade for $1 a day
5342-01-352-8177
Grooved Clamp Coupling
5342013528177 013528177 DAA3122P019-107 2610619-101
A metal loop having either a V or U cross section or channelled segment(s). It may be attached to a flat band. It is designed to create a fluid tight joint and/or connect pipe, tubing, tank cover(s), duct(s) and the like, by mating with flanged or beaded ferrule(s), flared, or beaded ends. It may or may not have a sealing inner liner. A latch or latches of the quick coupling type, nut or bolt type, or threaded trunnion type is (are) used to lock and adjust the band. Excludes COUPLING, CLAMP, PIPE and RING, LOCKING, METAL DRUM COVER. View more Grooved Clamp Coupling
June 2023
7
Marketplace 5342-01-352-8177
Request a Quotation from participating marketplace vendors
Related Documents 5342-01-352-8177 1+ Documents (More...)
5342-01-352-8177 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-53/fsc-5342/us 5342-01-352-8177
Grooved Clamp Coupling 5342013528177 DAA3122P019-107 A metal loop having either a V or U cross section
Restrictions 5342-01-352-8177
5342-01-352-8177 is a Grooved Clamp Coupling 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 is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 5342-01-352-8177
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5342-01-352-8177
- US Air Force (FNN5)
- Effective Date:
- 1 Jul 2003
- Former MOE Rule:
- FXCX
Approved Sources 5342-01-352-8177
- Part Number
- Manufacturer
- Status
- DAA3122P019-107
- Manufacturer
- 80378 - Triumph Aerostructures, Llc (Active)
- Source Control
- Source Control
- 2610619-101
- 98769 - Senior Operations Llc (Active)
- Primary Buy
- Primary Buy
- DAA3122P019-107
- 98769 - Senior Operations Llc (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 5342-01-352-8177
- Characteristic
- Specifications
- FIIG
- Specifications
- A25400
- Cross-Sectional Shape Style [AAGR]
- Grooved Retainer
- Height [HGTH]
- 0.290 Inches Nominal
- Nut Type [ALDS]
- Self-Locking Hexagon
- Included Angle In Deg [AKZZ]
- 38.5
- Inside Length [ADJU]
- 12.350 Inches Nominal
- Inside Width [ADJT]
- 6.100 Inches Nominal
- Latch Style [AGPR]
- Double
- Material And Location [ANNQ]
- Iron Alloy, Ams 5737, Comp 660 T Bolt
- Material And Location [ANNQ]
- Steel,Ams 5604,17-4Ph Band
- Retainer Thickness [ADTJ]
- 0.110 Inches Nominal
- Retainer Width [ALEB]
- 0.540 Inches Nominal
- Root Width [ALEC]
- 0.180 Inches Nominal
- Sealing Inner Liner [ALDW]
- Included
- Segment Quantity [ALDT]
- 2
- Shape [SHPE]
- Oblong
- Surface Treatment And Location [ANNR]
- Passivated Band
- Temp Rating [ABJH]
- -81.0 Deg Fahrenheit And 198.0 Deg Fahrenheit
Management Data 5342-01-352-8177
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Oct 2006
- Department of the Air Force (DF)
- EA
- Subscribe
- EA
Air Force
- Budget:
- S
- 57X3010 - Aircraft Replenishment Spares
- Aggregation Code:
- BQ
- B-2 TSSP, NORTHROP GRUMMAN
- 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 5342-01-352-8177
Freight Information 5342-01-352-8177
5342-01-352-8177 has freight characteristics.. 5342-01-352-8177 has a variance between NMFC and UFC when transported by rail and the description should be consulted.