Model: 34A12105

Cam Shaft Cap

Properties:

End Application
J-57 aircraft engine
General Description
O/a w across flats 0.554 to 0.564 in.; o/a h 0.530 to 0.550 in.; 2 holes 0.045 to 0.055 in. Diameter bore through 0.450 in. C to c; holes 0.140 to 0.160 in. From outer edge; spherical head 0.203 to0.234 in.; internal bore diameter 0.269 to 0.275 to lg 0.250 in.Threaded 0.312-24 nf 3b; 90 degrees countersink to 0.320 to 0.360 in; matl steel ams 4120
Fsc Application Data
Control, compressor bleed p/n a12140ky
NSN
2995-00-983-6732
Part Number
34A12105
Description
Cap,cam Shaft
CAGE
11599

Material Classification

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

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
095190
UFC:
49790
LTL:
RATING VARIABLE
LCL:
70.0
WCC:
713
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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