Aircraft Engine Maintenance Stand

Model PWA53180

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End Application:

F100pw100/200 engine
Functional Description:

Used to test the main fuel control; augmentor fuel control; compressor inlet variable vane control and cylinder; rear compressor variable vane cylinder; compressor bleed actuator; augmentor pump control and the compressor inlet temperature probe; calibration; characteristics: operation in hazardous area with ambient air temperatures ranging from 70 to 113 degree f; microprocessor; pneumatic required 80-110 psig, 10 scfm, 35 degree dew point, 60 to 80 degree f; high pressure gn2 750 psig 5 scfm, 30 degree f dew point, bottled

Machines and mechanical appliances having individual functions, not specified or included elsewhere in chapter 84

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

06393

FIIG:

T361-C

Concept No.:

App. Key:

Cond. Code:

Status:

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

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