Model: 519982

Metal Tube Assembly

Special Features:

Used on: tf30-p-103 engine // t.O.2j-tf30-14 f.21 i.15

Properties:

Wall Thickness
Between 0.031 inches and 0.039 inches
Overall Length
Between 7.071 inches and 7.129 inches
Mating End Quantity
2 single end
End Application
F-111 aircraft
Tubing Material
Nickel alloy, specification ams 5582 & rockwell c30 min tube hardness
End Connection Style
Miscellaneous first end
End Connection Style
Swivel nut, flare second end
Design Form
Prebent
Tube Outside Diameter
Between 0.375 inches and 0.379 inches
NSN
4710-00-947-0690
Part Number
519982
Description
Tube Assembly,metal
CAGE
77445

Part 519982 NSN 4710-00-947-0690

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
21989
FIIG:
T383-D
Concept No.:
App. Key:
DA
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:
PQ
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
052190
UFC:
30000
LTL:
RATING VARIABLE
LCL:
50.0
WCC:
576
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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