Model: 692057

Gas Turbine Engine Starter

Properties:

General Description
Solid propellent cartridge, af type mxu-4/a, w/provisions for air turbine starting, 50.0 psi air inlet pressure, 95.0 lb per min flow, max elec data, 32 v, 3 amp, dc, ccw drive rotation viewing output shaft, drive spline data, 24 teeth, 20/30 pitch, 1.200 in. Pitch dia, 1.900 in. Min dia, 1.264 in. Max diameter 0.700 in. Lg, mtg data, std mtg, an, and10266, type xvi&a, w/quick detachable mtg
Fsc Application Data
Starter, engine, gas turbine
NSN
2995-00-077-3474
Part Number
692057
Description
Starter,engine,gas Turbine
CAGE

An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. The combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. May have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.

Part 692057 NSN 2995-00-077-3474

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
21907
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
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

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
7,710.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F000773474
SPI Rev.:
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
92.5
LCL:
100.0
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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