Model: 5041T66P02

Inner Ring Coupling

Properties:

End Application
Aircraft engine tf34-ge-100
General Description
1.673 in. Min 1.678 in. Max w, 0.195 in. Min 0.205 in max w of both outside flanges, 0.3355 in. Min 0.3364 in. Max diameter of 40 holes eq sp, 0.3155 in. Min 0.3164 in. Max diameter of 20 holes on basis of 30 holes eq sp omitting every third hole, 0.301 in. Min 0.308 in. Max diameter of 20 holes on basis of 30 holes eq sp, 0.3155 in. Min 0.3164 in. Max diameter of 20 holes on basis of 30 holes eq sp 0.390 in. Min 0.410 in. Max diameter to 0.030 in. Through 0.035 in. Depth with 0.010 through 0.020 fillet rad of counterbore on last set of holes
NSN
2840-01-034-5820
Part Number
5041T66P02
Description
Coupling,inner Ring
CAGE
99207

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:
SX
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
3.4000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
051010
UFC:
29420
LTL:
65.0
LCL:
--
WCC:
736
TCC:
Z
SHC:
9
ACC:
Construction Materials

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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