Model: R51054T121012

Tube Tee

Properties:

Thread Class
3b 3rd end
Maximum Operating Temp
275.0 degrees fahrenheit single response
End Application
F/a-18 e/f aircraft
Connection Style
Flared (tube) 1st end
Connection Style
Flared (tube) 2nd end
Connection Style
Swivel nut, gasket seal (tube) 3rd end
Leg Length
1.654 inches 3rd end
Leg Length
1.779 inches 1st end
Leg Length
1.929 inches 2nd end
Connection Type
Threaded external tube 3rd end
Connection Type
Unthreaded external tube 1st end
Connection Type
Unthreaded external tube 2nd end
Thready Qty Per Inch (tpi)
16 3rd end
Maximum Operating Pressure
5000.0 pounds per square inch single response
Thread Size
1.000 inches 3rd end
Seat Angle
90.0 degrees 1st end
Seat Angle
90.0 degrees 2nd end
Seat Angle
90.0 degrees 3rd end
Criticality Code Justification
Agav
Outside Diameter Tube Accommodated
0.625 inches 2nd end
Outside Diameter Tube Accommodated
0.750 inches 1st end
Outside Diameter Tube Accommodated
0.750 inches 3rd end
Part Name Assigned By Controlling Agency
(inavy) tee tube - axial swage, swivel nut on run, reducer, 5000 psi
Material
Titanium
Material Specification
Ams 4928 assn standard single material response
Thread Series Designator
Unj 3rd end
NSN
4730-01-465-2363
Part Number
R51054T121012
Description
Tee,tube
CAGE

Part R51054T121012 NSN 4730-01-465-2363

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
03809
FIIG:
A080B0
Concept No.:
App. Key:
A
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
Q
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
052190
UFC:
30000
LTL:
RATING VARIABLE
LCL:
--
WCC:
576
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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