Model: PT6A-41

Turbo-prop Aircraft Engine

Properties:

End Application
Ru-21-j aircraft
NSN
2840-01-093-5018
Part Number
PT6A-41
Description
Engine,aircraft,turbo-prop
CAGE
00198

A combustion type power unit, may be with or without container, designed to use superheated air to spin a turbine rotor attached to the propeller shaft through reduction gears.

Part PT6A-41 NSN 2840-01-093-5018

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
15342
FIIG:
T197-B
Concept No.:
App. Key:
BB
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:
U
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
120800
UFC:
61410
LTL:
RATING VARIABLE
LCL:
100.0
WCC:
672
TCC:
Z
SHC:
R
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411214050
  • SITC: 71481
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Turbopropeller aircraft turbines (engines) other than for civil aircraft, of a power not exceeding 1100 kw

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