Model: T-62T-40C7D

Nonaircraft Gas Turbine Engine

Special Features:

Shaft horsepower rating in rpm 61565.0; altitude at which horsepower is rated 20000.0 feet; inlet air temp at which horsepower is rated 400.0 degrees fahrenheit

Properties:

Power Output For Which Designed
Shaft
Fuel Type
Gasoline
NSN
2835-01-328-7477
Part Number
T-62T-40C7D
Description
Engine,gas Turbine,nonaircraft
CAGE
55820

A continuous combustion type engine. consists primarily of a compressor, nonaircraft gas turbine engine; chamber, combustion, nonaircraft gas turbine engine and a turbine assembly, nonaircraft gas turbine engine. it may have a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft and/or pneumatic power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.

Part T-62T-40C7D NSN 2835-01-328-7477

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50489
FIIG:
A526A0
Concept No.:
App. Key:
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:
CRITL:
X

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Schedule B and Export
  • Schedule B: 8411818000
  • SITC: 71489
  • End Use: Industrial engines
  • NAICS: 333611
  • USDA: 1

Freight Class: Gas turbine engine, except aircraft nesoi, of a power not exceeding 5,000 kw

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