Model: TT118600-1

Water Injection Pump Assembly

Properties:

End Application
Pump installation, engine fuel system, boeing dwg no. 65-1023, c135 aircraft
Criticality Code Justification
Text
General Description
Approxiately 14.787 in. Min, 14.936 in. Max o/a lg, 6.00 in. Bolt circle dia, 2.9375 in. Od, 0.277 in. Min, 0.285 in. Max 6 holes equally spaced
NSN
2915-00-670-0640
Part Number
TT118600-1
Description
Pump Assembly,water Injection
CAGE
59875

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:
25.0 X 15.0 X 14.5
Paclk Weight:
39.1000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000004XE3
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
128000
UFC:
64870
LTL:
85.0
LCL:
--
WCC:
594
TCC:
1
SHC:
9
ACC:
Equipment for Aircraft

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