رقم الجزء
تجريد
صلاحيه
UOM
NIIN
معلومات الجزء
Ains alignment kit
TXT
وصف:
Aircraft Maintenance Kit
MRC:
The means,other than a carrying case,provided for movement of the item.AFJS
Portability Method:
Fixed external handles
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
B-1b aircraft gyro stabilization system
MRC:
A measurement of the longest dimension of an item unencumbered by packaging or packing,in distinction from width.AJAF
Unpackaged Unit Length:
14.000 inches
MRC:
A measurement taken at right angles to the length of an item unencumbered by packaging or packing,in distinction from thickness.AJAG
Unpackaged Unit Width:
8.000 inches
MRC:
A measurement from the bottom to the top of an item unencumbered by packaging or packing,in distinction from depth.AJAH
Unpackaged Unit Height:
6.000 inches
MRC:
The originator /governmental,industrial,or otherwise/ of the available document which lists the component/s/ of the item.AJJX
Component Document Origin:
Industrial
MRC:
The commercial and government entity (cage) code of the government agency,industrial organization,or other source,which controls the document.AJJY
Document Source:
43999
MRC:
Indicates the type of document by the title.AJJZ
Document Type:
Support equipment requirement sheet
MRC:
The page number indicating the location of the component/s/ listed in the document.AJKB
Component Document Page Number:
30
MRC:
Indicates the type of container provided.ALQG
Container Type:
Case
MRC:
The number or symbol/s/ used to identify the document.AYDR
Document Identification:
73a62c0123
MRC:
Those unusual or unique characteristics or qualities of an item not covered in the other requirements and which are determined to be essential for identification.FEAT
Special Features:
Consists of case containing two electronic levels, adjustment block, two electronic level tool bars, and ains alignment adapter
MRC:
Describes the capabilities,intended use,and/or purpose for which the item is provided.FTLD
Functional Description:
Used during alignment of pitch, roll, and yaw axis adjustments of the attitude inertial navigation system (ains) within the aircraft
