Model: T56-A-427

Turbo-prop Aircraft Engine

Properties:

Mounting Type
Aircraft
Overall Length
146.000 inches
Overall Height
39.000 inches
Overall Width
22.500 inches
Current Type
Dc
Furnished Items
Ignition relay, anti-ice sol. Valve, ignition exciter, fuel pump, external scav. Pump, fuel control and coor dinator, speed sensitive valve, main oil pressure and scavenge pump, rgb pressure pump, prop feather pump, prop feather solinoid, thrust sensitive switch, nts bracket, accelerometer for gearbox, compressor, and turbine
Horsepower Rating
5100.0
Inclosure
Not included
Thrust
812.0 pounds
Voltage In Volts
28.0
Fuel Type
Jet fuel
Nondefinitive Specification/std Data
T56-a-427 model
NSN
2840-01-461-5450
Part Number
T56-A-427
Description
Engine,aircraft,turbo-prop
CAGE
63005

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 T56-A-427 NSN 2840-01-461-5450

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:
A
ESD:
A
ESD:
A
MMAC:
CRITL:
X

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Schedule B and Export
  • Schedule B: 8411224050
  • SITC: 71481
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Turbopropeller aircraft turbines (engines) other than for use in civil aircraft, of a power exceeding 1100 kw

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