رقم الجزء
تجريد
صلاحيه
UOM
NIIN
معلومات الجزء
Test set requires 28 vdc for operation which can be supplied by the aircraft at organization level maintenance
TXT
وصف:
Aircraft Engine Test Set
MRC:
A measurement taken at right angles to the length of an item,in distinction from thickness.ABGL
Width:
14.000 inches
MRC:
A measurement of the longest dimension of any object,in distinction from width.ABRY
Length:
12.000 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
Auxiliary power unit (apu)
MRC:
An indication of the feature/s/ of the inclosure.ANPZ
Inclosure Feature:
Multiple item w/carrying case
MRC:
Describes the capabilities,intended use,and/or purpose for which the item is provided.FTLD
Functional Description:
Aluminum case, interconnected cable and hose assembly stowed in the removeable cover, front panel uses led indicators to denote test data in units of measurement degrees celsius, rpm, and psi; front panel makes use of test point connection to facilitate test probing; performs a complete test of the c130h aircraft auxiliary power unit and gas turbine compressor systems including readings on exhaust gas temperatures, rpm, oil, fuel, and air pressure
MRC:
A measurement from the bottom to the top of an object,in distinction from depth.HGTH
Height:
18.000 inches
MRC:
Literature and references available for information pertaining to the item.RDAL
Reference Data And Literature:
Serd 49-92-0030
MRC:
Characteristics or qualities of an item,not covered in any other requirement,which are considered essential information for one or more functions excluding nsn assignment.SUPP
Supplementary Features:
Also system test c-130e gas turbine compressor 85-12/52/56/62/71 (with additional harness), c-130h gas turbine compressor gtcp85-180l, cp-140 gas turbine compressor grcp95-3, and p-3a, b, c gas turbine compressor gtcp95-2/3
